Nokia Solutions and Networks T5EE1, T5DJ1 Users Manual

Abbreviated (All–inclusive) Acceptance Tests

68P64115A18–1

Table 4-7: All RX ATP Test Procedure

Step Action

NOTE

When testing diversity RX paths on companion frames, be sure to follow the RX test cable connection information in Table 4-1 or Table 4-2, as applicable, during this step.

Follow cable connection directions as they are displayed, and click the Continue button to begin testing.

– When the ATP process is completed, results will be displayed in the status report window.

12 Click the Save Results or Dismiss button.

NOTE

If Dismiss is used, the test results will not be saved in the test report file.

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Individual Acceptance Tests

The following individual ATP tests can be used to evaluate specific aspects of BTS operation against individual performance requirements. All testing is performed using the LMF GUI environment.

TX Testing

TX tests verify any given transmit antenna path and output power control. All tests are performed using the external, calibrated test equipment. All measurements are made at the appropriate BTS TX OUT connector(s).

TX tests verify TX operation of the entire CDMA forward link using selected BBXs assigned to respective sector antennas. Each BBX is keyed up to generate a CDMA carrier (using both at the CDF file–specified carrier output power level.

Individual Acceptance Tests68P64115A18–1

bbxlevel and BLO)

Individual Tests

RX Testing

RX testing verifies receive antenna paths for BBXs selected for the test. All tests are performed using the external, calibrated test equipment to inject a CDMA RF carrier with all zero longcode at the specified RX frequency at the appropriate BTS RX IN connector(s).

RX tests verify RX operation of the entire CDMA reverse link using all equipped MCCs assigned to all respective sector/antennas.

Spectral Purity TX Mask

This test verifies that the transmitted CDMA carrier waveform generated on each sector meets the transmit spectral mask specification (as defined in IS–97) with respect to the assigned CDF file values.

Waveform Quality (Rho)

This test verifies that the transmitted Pilot channel element digital waveform quality (rho) exceeds the minimum specified value in IS–97. Rho represents the correlation between the actual and perfect CDMA modulation spectrums. 1.0000 represents 100% (or perfect correlation).

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Pilot Time Offset

The Pilot Time Offset is the difference between the communications system test set measurement interval (based on the BTS system time reference) and the incoming block of transmitted data from the BTS (Pilot only, Walsh code 0).

Code Domain Power/Noise Floor

This test verifies the code domain power levels, which have been set for all ODD numbered Walsh channels, using the OCNS command. This is done by verifying that the ratio of PILOT divided by OCNS is equal to

2 dB, and, that the noise floor of all EVEN numbered “OFF”

10.2 +

Walsh channels measures < with respect to total CDMA channel power.

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Individual Acceptance Tests

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BTS FER

This test verifies the BTS receive FER on all traffic channel elements currently configured on all equipped MCCs (full rate at one percent FER) at an RF input level of –119 dBm on the main RX antenna paths using operator–selected, CDF–equipped MCCs and BBXs at the site. Diversity RX antenna paths are also tested using the lowest equipped MCC channel element ONLY.

NOTE

There are no pass/fail criteria associated with FER readings taken at levels below –119 dBm, other than to verify that the FER measurement reflects changes in the RX input signal level.

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TX Spectral Purity Transmit Mask Acceptance Test68P64115A18–1

TX Spectral Purity Transmit Mask Acceptance Test

Background

Overview – This test verifies the spectral purity of each operator–selected BBX carrier keyed up at a specific frequency specified in the current CDF. All tests are performed using the external, calibrated test equipment controlled by the same command. All measurements are made at the appropriate BTS TX antenna connector.

Test Patterns – There are four operator–selectable test patterns with which this acceptance test can be performed. The patterns, along with the channels tested and gain setting for each, are listed in Table 3-34. Refer to “TX Calibration and the LMF” in the Bay Level Offset Calibration section of Chapter 3 for more information on the test patterns.

Equipment Operation During Testing – At least one MCC must be selected to perform the Standard, CDF Pilot, and CDF test patterns. For these test patterns, forward links will be enabled for synch channel (SCH), paging channel (PCH), and traffic channel (TCH) elements from the selected MCC(s), as shown in Table 3-34. Gain will be set for the applicable channels on each antenna as shown in the table. The operator–selected BBXs will be keyed using a BLO–corrected value to generate a CDMA carrier. RF output power, as measured at the appropriate frame TX antenna connector, will be set to one of the following depending on the operating frequency spectrum:

bbxlvl

S 800 MHz: 33.5 dBm S 1.9 GHz: 31.0 dBm

Test Measurements – The test equipment will measure and return the attenuation level in dB of all spurious and IM products with respect to the mean power of the CDMA channel measured in a 1.23 MHz bandwidth, verifying that results meet system tolerances at the following test points (see also Figure 4-2):

S For 800 MHz:

– At least –45 dB @ + 750 kHz from center frequency – At least –45 dB @ – 750 kHz from center frequency – At least –60 dB @ – 1980 kHz from center frequency – At least –60 dB @ + 1980 kHz from center frequency

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S For 1.9 GHz:

– At least –45 dB @ + 885 kHz from center frequency – At least –45 dB @ – 885 kHz from center frequency – At least –55 dB @ – 1980 kHz from center frequency – At least –55 dB @ + 1980 kHz from center frequency

Redundant BBX Testing – The BBX will then de–key, and if selected, the redundant BBX will be assigned to the current TX antenna path under test. The test will then be repeated.

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TX Spectral Purity Transmit Mask Acceptance Test

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Spectral Purity TX Mask Acceptance Test

Follow the steps in Table 4-8 to verify the transmit spectral mask specification on the TX antenna paths for the selected BBXs.

Table 4-8: Test Spectral Purity Transmit Mask

Step Action

1 Set up the test equipment for TX acceptance tests per Table 4-3. 2 Select the BBXs to be tested. 3 If the Test Pattern to be used is Standard, CDFPilot, or CDF; select at least one MCC (Refer to

“Test Pattern Drop–down Pick List” on page 3-90.)

4 Click on Tests in the BTS menu bar, and select TX > TX Mask... from the pull–down menus. 5

Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the Channels/Carrier pick list.

NOTE

To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select multiple carrier(s)–sector(s).

Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.

NOTE

If necessary, the correct channel number may be manually entered into the Carrier # Channels box.

7 If at least one MCC was selected in Step 3, select the appropriate transfer rate (1 = 9600, 3 = 9600 1X)

from the drop–down list in the Rate Set box.

NOTE

The Rate Set selection of 3 is only available if 1X cards are selected for the test.

8 In the Test Pattern box, select the test pattern to use for the calibration from the drop–down list (refer

to “Test Pattern Drop–down Pick List” under “TX Calibration and the LMF” in the Bay Level Offset Calibration section of Chapter 3).

9 Click OK to display a status bar followed by a Directions pop-up window.

10 Follow the cable connection directions as they are displayed, and click the Continue button to begin

testing.

– As the ATP process is completed, results will be displayed in a status report window.

11 Click the Save Results or Dismiss button.

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NOTE

If Dismiss is used, the test results will not be saved in the test report file.

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TX Spectral Purity Transmit Mask Acceptance Test68P64115A18–1

Figure 4-2: TX Mask Verification Spectrum Analyzer Display

.5 MHz Span/Div Ampl 10 dB/Div

Mean CDMA Bandwidth

Power Reference

– 1980 kHz

– 885 kHz + 885 kHz

+ 1980 kHz

Center Frequency Reference

Attenuation level of all

spurious and IM products

with respect to the mean

power of the CDMA channel

– 750 kHz

+750 kHz

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TX Waveform Quality (Rho) Acceptance Test

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TX Waveform Quality (Rho) Acceptance Test

Background

Overview – This test verifies the transmitted pilot channel element digital waveform quality of each operator–selected BBX carrier keyed up at a specific frequency specified in the current CDF. All tests are performed using the external, calibrated test equipment controlled by the same command. All measurements are made at the appropriate TX antenna connector.

Equipment Operation During Testing – Pilot gain will be set to 262 for each antenna, and all TCH elements from the MCCs will be forward–link disabled. The selected BBXs will be keyed up using both

bbxlvl and BLO to generate a CDMA carrier (with pilot channel

element only, Walsh code 0). RF output power is set at 40 dBm as

measured at the appropriate BTS TX antenna connector.

Test Measurements – The test equipment will measure and return the pilot channel element digital waveform quality (rho) percentage, verifying that the result meets the following specification:

Waveform quality (Rho) should be >

0.912.

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TX Waveform Quality (Rho) Acceptance Test68P64115A18–1

Waveform Quality (Rho) Acceptance Test

Follow the steps in Table 4-9 to verify the pilot channel element waveform quality (rho) on the TX antenna paths for the selected BBXs.

Table 4-9: Test Waveform Quality (Rho)

Step Action

1 Set up the test equipment for TX acceptance tests per Table 4-3. 2 Select the BBXs to be tested. 3 Click on Tests in the BTS menu bar, and select TX > Rho... from the pull–down menus. 4

Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the Channels/Carrier pick list.

NOTE

To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select multiple carrier(s)–sector(s).

NOTE

If necessary, the correct channel number may be manually entered into the Carrier # Channels box.

6 Click OK to display a status bar followed by a Directions pop-up window. 7 Follow the cable connection directions as they are displayed, and click the Continue button to begin

testing.

– As the ATP process is completed, results will be displayed in a status report window.

8 Click the Save Results or Dismiss button.

NOTE

If Dismiss is used, the test results will not be saved in the test report file.

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TX Pilot Time Offset Acceptance Test

Background

Overview – This test verifies the transmitted pilot channel element Pilot Time Offset of each operator–selected BBX carrier keyed up at a specific frequency specified in the current CDF. All tests will be performed using the external, calibrated test equipment controlled by the same command. All measurements will be made at the BTS TX antenna connector.

Equipment Operation During Testing – The pilot gain will be set to 262 for each antenna and all TCH elements from the MCCs will be forward–link disabled. The selected BBXs will be keyed using both

bbxlvl and BLO to generate a CDMA carrier (with pilot channel

element only, Walsh code 0). TX power output is set at 40 dBm as measured at the TX output.

68P64115A18–1

Test Measurements – The test equipment will measure and return the Pilot Time Offset in ms, verifying that results meet the following specification:

Pilot Time Offset should be within 3 ms of the target PT Offset (zero ms).

NOTE

This test also executes and returns the TX Frequency and TX Waveform Quality (rho) ATP tests, however, only Pilot Time Offset results are written to the ATP test report.

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TX Pilot Time Offset Acceptance Test68P64115A18–1

Pilot Time Offset Acceptance Test

Follow the steps in Table 4-10 to verify the Pilot Time Offset on the TX antenna paths for the selected BBXs.

Table 4-10: Test Pilot Time Offset

Step Action

1 Set up the test equipment for TX acceptance tests per Table 4-3. 2 Select the BBXs to be tested. 3 Click on Tests in the BTS menu bar, and select TX > Pilot Time Offset... from the pull–down menus. 4

Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the Channels/Carrier pick list.

NOTE

To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select multiple carrier(s)–sector(s).

NOTE

If necessary, the correct channel number may be manually entered into the Carrier # Channels box.

6 Click OK to display a status bar followed by a Directions pop-up window. 7 Follow the cable connection directions as they are displayed, and click the Continue button to begin

testing.

– As the ATP process is completed, results will be displayed in a status report window.

8 Click the Save Results or Dismiss button.

NOTE

If Dismiss is used, the test results will not be saved in the test report file.

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TX Code Domain Power/Noise Floor Acceptance Test

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TX Code Domain Power/Noise Floor Acceptance Test

Background

Overview – This test verifies the Code Domain Power and Noise Floor of each operator–selected BBX carrier keyed at a specific frequency specified in the current CDF. All tests are performed using the external, calibrated test equipment controlled by the same command. All measurements are made at the appropriate BTS TX antenna connector.

CDMA Channel Test Set–up – Pilot gain will be set to 262 for each antenna and the selected MCCs will be configured to supply all odd–numbered Walsh code traffic channel elements by enabling Orthogonal Channel Noise Source (OCNS) on all odd MCC channel elements (maximum 32 full rate channels with an OCNS gain of 81). All even–numbered Walsh code traffic channel elements will not have

OCNS enabled, and are considered “OFF”. Selected MCCs will be forward–link enabled for the antenna (sector) under test.

Equipment Operation During Testing – The BBX will be keyed up using a BLO–corrected consisting of pilot and OCNS channels. RF output power, as measured at the appropriate frame TX antenna connector, is set at one of the following values depending on the operating frequency spectrum:

bbxlvl value to generate a CDMA carrier

NOTE

S 800 MHz: 33.5 dBm S 1.9 GHz: 31.0 dBm

Test Measurements – The test equipment will measure and return the channel element power in dB of all specified Walsh channels within the CDMA spectrum. Additional calculations will be performed to verify the following parameters are met (refer to Figure 4-3 for graphic representations):

S Traffic channel element power level will be verified by calculating the

ratio of Pilot power to OCNS gain of all traffic channels (root sum of the square (RSS) of each OCNS gain divided by the Pilot power). This value should be 10.2 dB +

2.0 dB.

S Noise floor (unassigned “OFF” even–numbered Walsh channels) is

verified to be < respect to total CDMA channel power

When performing this test using the LMF and the MCC is an MCC8E or MCC24E, the redundant BBX may fail or show marginal performance. This is due to a timing mismatch that the LMF does not address. Performing this test from the CBSC will not have this timing problem.

–27 dB for IS–95A/B and CDMA2000 1X with

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Redundant BBX Testing – The BBX will then de–key, and if selected, the redundant BBX will be assigned to the current TX antenna path under test. The test will then be repeated for the redundant BBX. Upon completion of the test, OCNS channels will be disabled on the specified MCC channel elements.

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TX Code Domain Power/Noise Floor Acceptance Test68P64115A18–1

Code Domain Power/Noise Floor Test

Follow the steps in Table 4-11 to verify the Code Domain Power/Noise floor of each selected BBX carrier keyed up at a specific frequency.

Table 4-11: Test Code Domain Power/Noise Floor

Step Action

1 Set up the test equipment for TX acceptance tests per Table 4-3. 2 Select the BBXs and MCCs to be tested. 3 Click on Tests in the BTS menu bar, and select TX > Code Domain Power... from the pull–down

menus.

Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the Channels/Carrier pick list.

NOTE

To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select multiple carrier(s)–sector(s).

NOTE

If necessary, the correct channel number may be manually entered into the Carrier # Channels box.

6 If at least one MCC was selected in Step 3, select the appropriate transfer rate (1 = 9600, 3 = 9600 1X)

from the drop–down list in the Rate Set box.

NOTE

The Rate Set selection of 3 is only available if 1X cards are selected for the test. 7 Click OK to display a status bar followed by a Directions pop-up window. 8 Follow the cable connection directions as they are displayed, and click the Continue button to begin

testing.

– As the ATP process is completed, results will be displayed in a status report window.

9 Click the Save Results or Dismiss button.

NOTE

If Dismiss is used, the test results will not be saved in the test report file.

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TX Code Domain Power/Noise Floor Acceptance Test

Figure 4-3: Code Domain Analyzer CD Power/Noise Floor Display Examples

68P64115A18–1

Pilot Channel

MAX OCNS

CHANNEL

Active channels

MIN OCNS

CHANNEL

MAX NOISE

FLOOR

8.2 dB 12.2 dB

PILOT LEVEL

MAX OCNS SPEC. MIN OCNS SPEC.

MAXIMUM NOISE FLOOR: < –27 dB FOR IS–95A/B AND CDMA2000 1X

Inactive channels

Walsh 0 1 2 3 4 5 6 7 ... 64

Code Domain Power/Noise Floor (OCNS Pass) Example

Pilot Channel

FAILURE – EXCEEDS

MAX OCNS SPEC.

Active channels

8.2 dB 12.2 dB

PILOT LEVEL

MAX OCNS SPEC. MIN OCNS SPEC.

FAILURE – DOES NOT

MEET MIN OCNS SPEC.

FAILURE – EXCEEDS MAX

NOISE FLOOR SPEC.

MAXIMUM NOISE FLOOR: < –27 dB FOR IS–95A/B AND CDMA2000 1X

Inactive channels

Walsh 0 1 2 3 4 5 6 7 ... 64

Code Domain Power/Noise Floor (OCNS Failure) Example

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RX FER Acceptance Test

Background

Overview – This test verifies the BTS Frame Erasure Rate (FER) on all TCHs currently configured on operator–selected MCCs (full rate at 1% FER) at –119 dBm. All tests are performed using the external, calibrated test equipment as the signal source controlled by the same command. Measurements are made at the specified BTS RX antenna connection.

Equipment Operation During Testing – The pilot gain on each MCC will be set to 262 for each TX antenna, and the forward link for all TCH elements from the MCCs will be enabled. Appropriate BBX(s) must be keyed in order to enable the RX receive circuitry. Operator–selected BBXs will be keyed using only with pilot channel element only. Transmit power output is set at –40 dBm. Test equipment output power is set so that the received power at the BBX is –119 dBm. The final output power setting of the test equipment takes into account the MPC type, BTS RF path losses, and test cable losses. If selected, the redundant BBX will be assigned to the current RX antenna paths under test.

RX FER Acceptance Test68P64115A18–1

bbxlvl, to generate a CDMA carrier

Test Measurements – The LMF will prompt the MCC channel element under test to measure all–zero longcode and provide the FER report on the selected active MCC on the reverse link for the main and, if selected, diversity RX antenna paths. Results are evaluated to ensure they meet the following specification:

FER returned less than 1% and Total Frames measured is 1500

Redundant BBX Testing – After the test, the BBX and the test equipment will be de–keyed to shut down the pilot signal and the active channel element, respectively. If the redundant BBX was tested, BBXR assignment to an active sector will also be reset.

Antenna Connections for Companion Frame RX Diversity Tests – At a site equipped with companion frames, RX diversity for each SC4812ET Lite frame is provided by the receive antennas for the collocated companion frame. Because of this, performing FER on companion frame diversity RX requires different RX test cable connections than on a starter frame. When performing companion frame diversity RX FER, use Figure 4-1 and Table 4-1 or Table 4-2 to determine the correct location for the RX test cable connections.

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RX FER Acceptance Test

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FER Acceptance Test

Follow the steps in Table 4-12 to verify the FER on RX antenna paths using selected MCCs and BBXs.

Table 4-12: Test FER

Step Action

1 Set up the test equipment for RX acceptance tests per Table 4-3. 2

If a companion frame is being tested and either BOTH or DIV is to be selected in step NO TAG,

perform the additional test equipment set–up in Table 4-4 for the diversity RX portion of the ATP.

NOTE

If the LMF has been logged into the BTS with a different Multi–Channel Preselector setting than the

one to be used for this test, the LMF must be logged out of the BTS and logged in again with the new

Multi–Channel Preselector setting. Using the wrong MPC setting can cause a false test failure. 3 Select the BBXs and MCCs to be tested.

4 Click on Tests in the BTS menu bar, and select RX > FER... from the pull–down menu. 5

Select the appropriate carrier(s) and sector(s) (carrier-bts#-sector#-carrier#) from those displayed in the

Channels/Carrier pick list.

NOTE

To select multiple items, hold down the Shift or Ctrl key while clicking on pick list items to select

multiple carrier(s)–sector(s). 6

Verify that the correct channel number for the selected carrier is shown in the Carrier # Channels

box. If it is not, obtain the latest bts–#.cdf (or bts–#.necf) and cbsc–#.cdf files from the CBSC.

NOTE

If necessary, the correct channel number may be manually entered into the Carrier # Channels box. 7 Select the appropriate RX branch (Both, Main, or Diversity) in the drop–down list.

NOTE

If a companion frame with the inter–frame diversity RX cabling disconnected is being tested do not

select BOTH in this step. The RX main and diversity paths must be tested separately for this

configuration because each requires a different Multi–Coupler Preselector type to provide the proper

test signal gain. 8

In the Rate Set box, select the appropriate data rate (1=9600, 2=14400, 3=9600 1X) from the

drop–down list.

NOTE

The Rate Set selection of 2 is only available if non–1X cards are selected for the test.

The Rate Set selection of 3 is only available if 1X cards are selected for the test. 9 Click OK to display a status bar followed by a Directions pop-up window.

NOTE

When testing diversity RX paths on companion frames, be sure to follow the RX test cable connection

information in Table 4-1 or Table 4-2, as applicable, during this step.

Follow cable connection directions as they are displayed, and click the Continue button to begin

testing. As the ATP process is completed, results will be displayed in the status report window.

11 Click the Save Results or Dismiss button. If Dismiss is used, the test results will not be saved in the

test report file.

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Generating an ATP Report

Background

Each time an ATP test is run, ATP data is updated and must be saved to an ATP report file using the Save Results button to close the status report window. The ATP report file will not be updated if the status reports window is closed using the Dismiss button.

ATP Report

A separate report is created for each BTS and includes the following for each test:

S Test name S PASS or FAIL S Description information (if applicable) S BBX number S Channel number

Generating an ATP Report68P64115A18–1

S Carrier number S Sector number S Upper test limit S Lower test limit S Test result S Time stamp S Details/Warning information (if applicable)

Follow the procedures in the Table 4-13 to view and create a printable file for the ATP report.

Table 4-13: Generating an ATP Report

Step Action

1 Click on the Login tab (if not in the forefront). 2 Click on the desired BTS in the Available Base Stations pick

list to select it.

3 Click on the Report button. 4 If a printable file is not needed, click on the Dismiss button.

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5 If a printable file is required, perform the following:

5a – Select the desired file type (text, comma–delimited,

HTML) for the report file from the drop–down list at the bottom of the screen.

5b – Click the Save button to save the file.

–– The file will be saved in the selected format in the

bts–# folder for the BTS selected.

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Generating an ATP Report

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Notes

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Chapter 5

Leaving the Site

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5-1

Updating Calibration Data Files

After completing the TX calibration and audit, updated CAL file information must be moved from the LMF Windows environment back to the CBSC, a Unix environment. The following procedures detail moving files from one environment to the other.

Copying CAL files from LMF to a Diskette

Follow the procedures in Table 5-1 to copy the CAL files from an LMF computer to a 3.5 diskette.

Table 5-1: Copying CAL Files to a Diskette

Step Action

1 With Windows running on the LMF computer, insert a disk into Drive A:\. 2 Launch the Windows Explorer application program from the Start > Programs menu list. 3 Select the applicable <x>:\<lmf home directory/cdma/bts–# folder. 4 Drag the bts–#.cal file to Drive A. 5 Repeat Steps 3 and 4, as required, for other bts–# folders.

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Table 5-2: Copying CAL Files from Diskette to the CBSC

Step Action

1 Log into the CBSC on the OMC–R Unix workstation using your account name and password. 2 Place the diskette containing calibration file(s) in the workstation diskette drive. 3 Type in eject –q and press the Enter key. 4 Type in mount and press the Enter key.

Copying CAL Files from Diskette to the CBSC

Follow the procedures in Table 5-2 to copy CAL files from a diskette to the CBSC.

NOTE

S Check to see that the message “floppy/no_name” is displayed on the last line.

S If the eject command was previously entered, floppy/no_name will be appended with a number.

Use the explicit floppy/no_name reference displayed.

5 Type in cd /floppy/no_name and press the Enter key. 6 Type in ls –lia and press the Enter key.

– Verify the bts–#.cal file filename appears in the displayed directory listing. 7 Type in cd and press the Enter key. 8 Type in pwd and press the Enter key.

– Verify the displayed response shows the correct home directory (/home/<user’s name>). 9 With Solaris versions of Unix, create a Unix–formatted version of the bts–#.cal file in the home

directory by performing the following:

. . . continued on next page

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Table 5-2: Copying CAL Files from Diskette to the CBSC

Step Action

9a – Type the following command:

dos2unix /floppy/no_name/bts–#.cal bts–#.cal Where: # = BTS number for which the CAL file was created

Updating Calibration Data Files68P64115A18–1

– Press the Enter key.

NOTE

Other versions of Unix do not support the dos2unix command. In these cases, use the Unix cp (copy) command. The copied files will contain DOS line feed characters which must be edited out with a Unix text editor.

10 Type in ls –l *.cal and press the Enter key. Verify the CAL files have been copied.

– Verify all CAL files to be transferred appear in the displayed listing.

11 Type eject, and press the Enter key. 12 Remove the diskette from the workstation.

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5-3

Prepare to Leave the Site

Removing External Test Equipment

Perform the procedure in Table 5-3 to disconnect the test equipment and configure the BTS for active service.

Table 5-3: Remove External Test Equipment

Step Action

n W ARNING

Be sure no BBXs are keyed before performing this step. Failure to do so can result in personal injury and damage to BTS LPAs.

Disconnect all external test equipment from all TX and RX connectors at the rear of the frame.

Reconnect and visually inspect all TX and RX antenna feed lines at the frame RF interface panel.

NOTE

Verify that all sector antenna feed lines are connected to the correct antenna connectors on the frame. Crossed antenna cables will degrade call processing.

68P64115A18–1

Reset All Devices and Initialize Site Remotely

Table 5-4: Reset BTS Devices and Remote Site Initialization

Step Action

1 Terminate the LMF session by following the procedures in Table 5-6. 2 Cycle BTS power off, as specified in Table 2-9 and Table 2-10, and on, as specified in Table 2-11 and

Table 2-12. 3 Reconnect spans by following the procedure in Table 5-7. 4 Notify the OMCR/CBSC to take control of the site and download code and data to the BTS. 5 Verify the CBSC can communicate with the GLIs.

Generally, devices in the BTS should not be left with data and code loaded from the LMF. The configuration data and code loads used for normal operation could be different from those stored in the LMF files. By resetting all devices, the required data and code can be loaded from the CBSC using the DLM when spans are again active.

To reset all devices and have the OMCR/CBSC bring up the site remotely, perform the procedure in Table 5-4.

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Bringing Modules into Service with the LMF

Prepare to Leave the Site68P64115A18–1

NOTE

If there is a reason code and/or data should or could not be loaded remotely from the CBSC, follow the steps outlined in Table 5-5 as required to bring BTS processor modules from OOS to INS state.

Table 5-5: Bring Modules into Service

Step Action

1 In the LMF GUI environment, select the device(s) to be enabled by clicking on each one.

Whenever possible, have the CBSC/MM bring up the site and enable all devices at the BTS.

NOTE

S The MGLI and CSM must be INS_ACT (bright green) before an MCC can be enabled.

S Processors which must be enabled and the order of enabling are as follows:

1. MGLI

2. CSMs

3. MCCs

Click on Device in the BTS menu bar, and select Enable from the pull–down list.

– A status report window is displayed.

NOTE

If a BBX is selected, a transceiver parameters window is displayed to collect keying information. Do

not enable the BBX.

3 Click Cancel to close the transceiver parameters window, if applicable. 4 Click OK to close the status report window.

– The color of devices which successfully change to INS will change bright green.

Terminating LMF Session/Removing Terminal

Perform the procedure in Table 5-6 as required to terminate the LMF GUI session and remove the LMF computer.

Table 5-6: Remove LMF

Step Action

2 In the Windows Task Bar, click Start and select Shutdown. 3 Click Yes when the Shut Down Windows message appears

! CAUTION

Do not power down the LMF terminal without performing the procedure below. Corrupted/lost data files may result.

Log out of all BTS sessions and exit LMF by clicking on File in the LMF window menu bar and selecting Logout and Exit from the pull–down list.

4 Wait for the system to shut down and the screen to go blank.

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5-5

Prepare to Leave the Site

Table 5-6: Remove LMF

Step Action

5 Disconnect the LMF terminal Ethernet port from the BTS frame. 6 Disconnect the LMF terminal serial port, the RS–232–to–GPIB interface box, and the GPIB

cables as required for equipment transport.

Connecting BTS T1/E1 Spans

Before leaving the site, connect any T1 or E1 span connectors removed previously to allow the LMF to control the BTS. Refer to Table 5-7 and Figure 3-2.

Table 5-7: Connect T1 or E1 Spans

Step Action

1 Re–connect any disconnected span connectors to the Span I/O A and B boards. 2 If equipped, ensure the CSU is powered on.

68P64115A18–1

3 Verify span status, ensuring the OMC–R/CBSC can communicate with the BTS.

Before Leaving the site

Be sure all requirements listed in Table 5-8 are completed before leaving the site.

Table 5-8: Check Before Leaving the Site

Step Action

1 When backup batteries are installed, all battery circuit breakers are ON (pushed in). 2 Both heat exchanger circuit breakers on the DC PDA are set to ON (pushed in), and the heat

exchanger blowers are running. 3 The External Blower Assembly (EBA) power cable is connected, and the EBA is running. 4 The MAP power switch is set to ON, and the POWER (green) LED is lighted. 5 The MAP TCP switch is set to ON. 6 The BATT TEST switch on the MAP is set to OFF, and the BATT. TEST (amber) LED is not lighted. 7 No alarm conditions are being reported to the CBSC with all frame doors closed.

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Chapter 6

Basic Troubleshooting

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6-1

Basic Troubleshooting: Overview

Overview

The information in this chapter addresses some of the scenarios likely to be encountered by Customer Field Engineering (CFE) team members while performing BTS optimization and acceptance testing. This troubleshooting guide was created as an interim reference document for use in the field. It provides “what to do if” basic troubleshooting suggestions when the BTS equipment does not perform according to the procedures documented in the manual.

Comments are consolidated from inputs provided by CFEs and information gained from experience in Motorola labs and classrooms.

68P64115A18–1

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Troubleshooting: Installation

Cannot Log into Cell-Site

Table 6-1: Login Failure Troubleshooting Procedures

n Step Action

1 If the MGLI LED is solid RED, it implies a hardware failure. Reset MGLI by re-seating it. If this

persists, install GLI card in MGLI slot and retry. A Red LED may also indicate no termination on an external LAN connector (power entry compartment at rear of frame).

2 Verify that the span line is disconnected at the Span I/O card. If the span is still connected, verify

the CBSC has disabled the BTS. 3 Try to ‘ping’ the MGLI. 4 Verify the LMF is connected to the primary LAN (LAN A) at the LAN shelf below the SCCP

cage. If LAN A is not the active LAN, force a LAN switch to LAN A by following the procedure

in Table 6-2. 5 Verify the LMF was configured properly. 6 If a Xircom parallel BNC LAN interface is being used, verify the BTS-LMF cable is RG-58

(flexible black cable less than 2.5 feet in length).

Troubleshooting: Installation68P64115A18–1

7 Verify the external LAN connectors are properly terminated (power entry compartment at rear of

frame). 8 Verify a T-adapter is not used on LMF computer side connector when connected to the primary

LAN at the LAN shelf. 9 Try connecting to the Ethernet Out port in the power entry compartment (rear of frame). Use a

TRB–to–BNC (triax–to–coax) adapter at the LAN connector for this connection.

10 Re-boot the LMF and retry. 11 Re-seat the MGLI and retry. 12 Verify GLI IP addresses are configured properly by following the procedure in Table 6-3.

Table 6-2: Force Ethernet LAN A to Active State as Primary LAN

n Step Action

1 If LAN A is not the active LAN, make certain all external LAN connectors are either terminated

with 50Ω loads or cabled to another frame. 2 If it has not already been done, connect the LMF computer to the stand–alone or starter frame, as

applicable (Table 3-5). 3 If it has not already been done, start a GUI LMF session and log into the BTS on the active LAN

(Table 3-6).

4 Remove the 50Ω termination from the LAN B IN connector in the power entry compartment at the

rear of the stand–alone or starter frame. The LMF session will become inactive. 5 Disconnect the LMF computer from the LAN shelf LAN B connector and connect it to the LAN A

connector.

. . . continued on next page

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Troubleshooting: Installation

Table 6-2: Force Ethernet LAN A to Active State as Primary LAN

n ActionStep

6 If the LAN was successfully forced to an active state (the cards in any cage can be selected and

statused), proceed to step 13. 7 With the 50Ω termination still removed from the LAN B IN connector, remove the 50Ω

termination from LAN B OUT connector. If more than one frame is connected to the LAN,

remove the termination from the last frame in the chain. 8 If the LAN was successfully forced to an active state (the cards in any cage can be selected and

statused), proceed to step 13. 9 With the 50Ω terminations still removed from LAN B, unseat each GLI card in each frame

connected to the LAN, until all are disconnected from the shelf backplanes.

10 Reseat each GLI card until all are reconnected. 11 Allow the GLIs to power up, and attempt to select and status cards in the CCP shelves. If LAN A

is active, proceed to step 13.

12 If LAN A is still not active, troubleshoot or continue troubleshooting following the procedures in

Table 6-1.

68P64115A18–1

13 Replace the 50Ω terminations removed from the LAN B IN and OUT connectors.

Table 6-3: GLI IP Address Setting

n Step Action

1 If it has not previously been done, establish an MMI communication session with the GLI card as

described in Table 3-10. 2 Enter the following command to display the IP address and subnet mask settings for the card:

config lg0 current

A response similar to the following will be displayed:

GLI2>config lg0 current

lg0: IP address is set to DEFAULT (configured based on card location)

lg0: netmask is set to DEFAULT (255.255.255.128)

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Troubleshooting: Installation68P64115A18–1

Table 6-3: GLI IP Address Setting

n ActionStep

3 If the IP address setting response shows an IP address rather than “Default (configured

based on card location),” enter the following:

config lg0 ip default

A response similar to the following will be displayed:

GLI2>config lg0 ip default

_param_config_lg0_ip(): param_delete(): 0x00050001 lg0: ip address set to DEFAULT

4 If the GLI subnet mask setting does not display as “DEFAULT (255.255.255.128),” set it to

default by entering the following command:

config lg0 netmask default

A response similar to the following will be displayed:

GLI2>config lg0 netmask default

_param_config_lg0_netmask(): param_delete(): 0x00050001 lg0: netmask set to DEFAULT

5 Set the GLI route default to default by entering the following command:

config route default default

A response similar to the following will be displayed:

GLI2>config route default default

_esh_config_route_default(): param_delete(): 0x00050001 route: default gateway set to DEFAULT

NOTE

Changes to the settings will not take effect unless the GLI is reset.

When changes are completed, close the MMI session, and reset the GLI card.

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Troubleshooting: Installation

n ActionStep

7 Once the GLI is reset, re–establish MMI communication with it and issue the following command

to confirm its IP address and subnet mask settings:

config lg0 current

A response similar to the following will be displayed:

GLI2>config lg0 current

lg0: IP address is set to DEFAULT (configured based on card location)

lg0: netmask is set to DEFAULT (255.255.255.128)

8 Repeat steps 1 through 7 for all remaining GLIs, including those in any additional,

inter–connected frames.

68P64115A18–1

Table 6-3: GLI IP Address Setting

Cannot Communicate with Power Meter

Table 6-4: Troubleshooting a Power Meter Communication Failure

n Step Action

1 Verify power meter is connected to LMF with GPIB adapter.

2 Verify cable connections as specified in Chapter 3. 3 Verify the GPIB address of the power meter is set to the same value displayed in the applicable

GPIB address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or

Table 3-24 and the Setting GPIB Addresses section of Appendix NO TAG for details. 4 Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation

section of Appendix NO TAG for details. 5 Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be

‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and

retry. 6 Verify the LMF computer COM1 port is not used by another application; for example, if a

HyperTerminal window is open for MMI, close it. 7 Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >

Reset from the pull–down lists.

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Cannot Communicate with Communications System Analyzer

Table 6-5: Troubleshooting a Communications System Analyzer Communication Failure

n Step Action

1 Verify analyzer is connected to LMF with GPIB adapter. 2 Verify cable connections as specified in Chapter 3. 3 Verify the analyzer GPIB address is set to the same value displayed in the applicable GPIB

address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or Table 3-24

and the Setting GPIB Addresses section of Appendix F for details. 4 Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation

section of Appendix NO TAG for details. 5 Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be

‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and

retry. 6 Verify the LMF computer COM1 port is not used by another application; for example, if a

HyperTerminal window is open for MMI, close it. 7 Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >

Reset from the pull–down lists.

Cannot Communicate with Signal Generator

Table 6-6: Troubleshooting a Signal Generator Communication Failure

n Step Action

1 Verify signal generator is connected to LMF with GPIB adapter. 2 Verify cable connections as specified in Chapter 3. 3 Verify the signal generator GPIB address is set to the same value displayed in the applicable GPIB

address box of the LMF Options window Test Equipment tab. Refer to Table 3-23 or Table 3-24

and the Setting GPIB Addresses section of Appendix NO TAG for details. 4 Verify the GPIB adapter DIP switch settings are correct. Refer to Test Equipment Preparation

section of Appendix NO TAG for details. 5 Verify the GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be

‘ON’ (Power and Ready). If any other LED is continuously ‘ON’, then cycle GPIB box power and

retry. 6 Verify the LMF computer COM1 port is not used by another application; for example, if a

HyperTerminal window is open for MMI, close it.

7 Reset all test equipment by clicking Util in the BTS menu bar and selecting Test Equipment >

Reset from the pull–down lists.

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Troubleshooting: Download

Table 6-7: Troubleshooting Code Download Failure

n Step Action

1 Verify T1 or E1 span is disconnected from the BTS at Site I/O boards (Figure 3-2). 2 Verify LMF can communicate with the BTS devices using the LMF Status function. 3 Communication with MGLI must first be established before trying to communicate with any other

BTS device. MGLI must be INS_ACT state (bright green). 4 Verify the target card is physically present in the cage and powered-up. 5 If the target card LED is solid RED, it implies hardware failure. Reset card by re-seating it. If LED

alarm persists, replace with same type of card from another slot and retry. 6 Re-seat card and try again. 7 If a BBX reports a failure message and is OOS_RAM, the code load was OK. Use the LMF

Status function to verify the load. 8 If the download portion completes and the reset portion fails, reset the device by selecting the

device and Reset.

68P64115A18–1

9 If a BBX or an MCC remains OOS_ROM (blue) after code download, use the LMF

Device > Status function to verify that the code load was accepted.

10 If the code load was accepted, use LMF Device > Download > Flash to load RAM code into flash

memory.

Cannot Download DATA to Any Device (Card)

Table 6-8: Troubleshooting Data Download Failure

n Step Action

1 Re-seat card and repeat code and data load procedure. 2 Verify the ROM and RAM code loads are of the same release by statusing the card. Refer to

Download the BTS section of Chapter G for more information.

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Cannot ENABLE Device

Before a device can be enabled (placed in service), it must be in the OOS_RAM state (yellow in LMF display) with data downloaded to the device. The color of the device on the LMF changes to green once it is enabled.

The four device states that can be displayed by the LMF are:

S Enabled (bright green, INS_ACT) S Stand–by (olive green, INS_SBY – redundant CSM and GLI only) S Disabled (yellow, OOS_RAM) S Reset (blue, OOS_ROM)

Table 6-9: Troubleshooting Device Enable (INS) Failure

n Step Action

1 Re-seat card and repeat code and data load procedure. 2 If CSM cannot be enabled, verify the CDF has correct latitude and longitude data for cell site

location and GPS sync.

Troubleshooting: Download68P64115A18–1

3 Ensure primary CSM is in INS_ACT (bright green) state.

NOTE

MCCs will not enable without the CSM being INS. 4 Verify 19.6608 MHz CSM clock is present; MCCs will not enable without it. 5 BBXs should not be enabled for ATP tests. 6 If MCCs give “invalid or no system time,” verify the CSM is enabled. 7 Log out of the BTS, exit the LMF, restart the application, log into the BTS, and re–attempt

device–enable actions.

LPA Errors

Table 6-10: LPA Errors

n Step Action

1 If LPAs give continuous alarms, cycle power with the applicable DC PDA circuit breakers. 2 Establish an MMI session with the LPA (Table 3-10), connecting the cable to the applicable MMI

port on the ETIB.

2a – Type alarms at the HyperTerminal window prompt and press Enter.

–– The resulting display may provide an indication of the problem.

2b – Call Field Support for further assistance.

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Troubleshooting: Calibration

Bay Level Offset Calibration Failure

Table 6-11: Troubleshooting BLO Calibration Failure

n Step Action

1 Verify the power meter or communications system analyzer is configured correctly (see the Test

Equipment Set–up section of Chapter 3), and is connected to the proper BTS TX antenna

connector. 2 If a power meter is being used:

2a – Re-calibrate the Power Meter and verify it is calibrated correctly with cal factors from the

power sensor (refer to Appendix F).

2b – Verify the power sensor is functioning properly by checking it with the 1–mW (0 dBm) Power

Ref signal.

2c – Verify communication between the LMF and Power Meter is working by checking that the

meter display is showing RES :

3 Verify the parameters in the bts–#.cdf file are set correctly for the BTS operating band as

follows:

For 1900 MHz:

Bandclass=1; Freq_Band=16

For 800 MHz:

Bandclass=0; Freq_Band=8

68P64115A18–1

4 Verify that no LPA on the carrier is in alarm state (rapidly flashing red LED).

4a – If any are, reset the LPA(s) by pulling the applicable circuit breaker on the DC PDA, and,

after 5 seconds, pushing back in.

5 Verify GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be ‘ON’

(Power and Ready). If any other LED is continuously ‘ON’, power-cycle (turn power off and on)

the GPIB Box and retry.

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Calibration Audit Failure

Table 6-12: Troubleshooting Calibration Audit Failure

n Step Action

1 Verify the power meter or communications system analyzer is configured correctly (see the Test

Equipment Set–up section of Chapter 3), and is connected to the proper BTS TX antenna

connector. 2 If a power meter is being used:

2a – Re-calibrate the Power Meter and verify it is calibrated correctly with cal factors from the

power sensor (refer to Appendix F).

2b – Verify the power sensor is functioning properly by checking it with the 1–mW (0 dBm) Power

Ref signal.

2c – Verify communication between the LMF and Power Meter is working by checking that the

meter display is showing RES :

3 Verify that no LPA on the carrier is in alarm state (rapidly flashing red LED).

3a – If any are, reset the LPA(s) by pulling the applicable circuit breaker on the DC PDA, and,

after 5 seconds, pushing back in.

Troubleshooting: Calibration68P64115A18–1

4 After calibration, the BLO data must be re-loaded to the BBXs before auditing. Click on the

BBX(s), and in the BTS menu bar select Device > Download >BLO.

Re-try the audit. 5 Verify GPIB adapter is not locked up. Under normal conditions, only 2 green LEDs must be ‘ON’

(Power and Ready). If any other LED is continuously ‘ON’, power-cycle (turn power off and on)

the GPIB Box and retry. 6 If calibration was being performed for the redundant BBX, be sure the Single–Sided BLO

checkbox was not checked in the CDMA Test Parameters test set–up window. 7 If additional items, such as directional couplers or combiners, have been installed in the TX path,

be sure that one of the following has been done:

S Verify BLO checkbox in the CDMA Test Parameters test set–up window is unchecked.

S The additional path losses have been added into each applicable sector using the Util > Edit >

TX Coupler Loss... function.

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Basic Troubleshooting: RF Path Fault Isolation

Overview

The optimization (RF path characterization or calibration) and post-calibration (audit) procedures measure and limit-check the BTS reported transmit and receive levels of the path from each BBX to the back of the frame. When a fault is detected, it is specific to a receive or transmit path. The troubleshooting process in this section determines the most probable cause of the fault.

As the calibration and audit tests are performed, results are displayed in the LMF test status report window. When faults are encountered, the test procedure in progress continues running and displaying any further faults. If it appears that there are major faults, the test can be aborted.

68P64115A18–1

The test results can be saved to a directory window using the Save Results button.

NOTE

If a test is re–run or a new calibration, audit, or test is run and the results are saved, the previous test results in the overwritten. To prevent losing previous test results in the file, refer to the procedure in Table 4-13 before performing further testing with the LMF.

If there are major faults, recheck the test equipment attachments for

errors. If none are found, close the test status report window using the Save Results button, and save the contents of the resulting file as described in Table 4-13. Also, note other specifics about the failure, and proceed with the fault isolation procedure.

\cdma\bts–# folder. To do this, close the test status report

Closing the test status report window with the Dismiss button will delete the test results without saving them.

bts–#.rpt file in the<x>:\<lmf home

bts–#.rpt file are

bts–#.rpt

If Every Test Fails

Check the calibration equipment for proper operation by manually setting the signal generator output attenuator to the lowest output power setting. Connect the output port to the spectrum analyzer RF input port. Set the signal generator output attenuator to –90 dBm, and switch on the RF output. Verify that the spectrum analyzer can receive the signal, indicate the correct signal strength (accounting for the cable insertion loss), and indicate the approximate frequency.

V erify BLO Checkbox

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When performing a calibration with the TX Calibration... or All Cal/Audit... functions, the Verify BLO checkbox should normally be

checked. When a calibration fails, determine if any items such as directional couplers or combiners have been added to the TX path. If additional items have been installed in the path, try re–running the calibration with Verify BLO unchecked. If calibration still does not pass, refer to the following paragraphs and use the TX output fault isolation flowchart to identify the most probable cause of the failure.

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Single–Sided BLO Checkbox

When performing a calibration with the TX Calibration... or All Cal/Audit... functions, the Single–Sided BLO checkbox should not be

checked when the redundant BBX is being calibrated. When a calibration fails with the redundant BBX selected, try re–running the calibration with the Single–Sided BLO checkbox unchecked. If the calibration still fails, refer to the following paragraphs and use the TX output fault isolation flowchart to identify the most probable cause of the failure.

If Faults Are Isolated

If the fault reports are isolated between successful path checks, the root cause of the faults most likely lies with one or more of the Field Replaceable Unit (FRU) modules. If more than one failure was reported, look for a common denominator in the data. For example, if any TX test fails on one sector only, the BBX assigned to that sector (Table 1-6) is a likely cause. Also, look at the severity of the failure. If the path loss is just marginally out of the relaxed specification limit during the post-calibration TX audit, suspect excessive cable loss. If limits are missed by a wide margin, suspect mis–wired cables or total device failure. Use the TX output fault isolation flowchart in Figure 6-1 to identify the strongest possible cause for a failed TX test.

Basic Troubleshooting: RF Path Fault Isolation68P64115A18–1

Fault Isolation Flowchart

Flowchart Prerequisites

The flowchart covers the transmit path. Transmit paths usually fail the lower test limit, indicating excessive loss in some component in the BTS site or mis–wiring. A failure of an upper limit usually indicates a problem with the test setup or external equipment. Before replacing a suspected FRU, always repeat and verify the test results to rule out a transient condition. If a BBX fails an upper limit in the post–calibration audit procedure, re–calibrate and verify the out–of–tolerance condition for that BBX and/or sector before replacement.

Before entering the fault isolation sequence outlined in the flowchart, be sure the following have been completed:

S GLIs, MCCs, and BBXs have been downloaded with the correct ROM

code, RAM code, and data (Table 3-12, Table 3-13, and Table 3-14).

S MGLI, CSMs, and MCCs are enabled (Table 3-13, Table 3-16, and

Table 3-17, respectively)

S Be sure the LED on the correct CCD card is solid green. S Be sure no alarms are being reported by opening an LMF alarm

window as outlined in Table 3-47.

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Basic Troubleshooting: RF Path Fault Isolation

TX Power Output Fault Isolation Flowchart

Figure 6-1: TX Output Fault Isolation Flowchart

Start

TX Power

Out of Limits

68P64115A18–1

High limit

Did TX Output

fail the High or

Low limit?

Low limit

failure.

If equipped, does a

BBX on the same

carrier but for a

different sector

pass?

No, next BBX on same carrier

fails on different sector .

failure.

Yes, it passes.

Does

redundant BBX

have the same

problem on the

same sector?

Yes

Does any other sector have the same problem?

Yes

Likely Cause: BBX card

Attempt re–calibration before replacement.

Likely Cause: External Power Measurement

Equipment and/or Set–up.

Also check: Switch card

External Attenuators & Pads, Check Site Documentation.

Likely Cause: CIO card

Carrier trunking module

Also check: CIO–trunking module cabling

TX filter/combiner cabling TX DRDC/TRDC cabling

Likely Cause: BBX card

Loose connections on CIO–trunking module cabling, TX filter/combiner cabling, or TX DRDC/TRDC cabling

Also check: CIO card

Carrier trunking module

If equipped, does a

BBX on a different

carrier but for the

same sector

6-14

pass?

No, everything fails

Likely Cause: Crossed TX cabling to include:

Yes, it passes.

Also check: Carrier trunking module

Likely Cause: CIO card not fully seated

– CIO–trunking module, – Trunking module–filter/combiner , – Filter/combiner–DRDC/TRDC Carrier LPAs

CIO card.

External Power Measurement Equipment and/or Set–up Crossed TX cabling to include: – CIO–trunking module, – Trunking module–filter/combiner , – Filter/combiner–DRDC/TRDC

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Troubleshooting: Transmit ATP68P64115A18–1

Troubleshooting: Transmit ATP

BTS Passed Reduced ATP Tests but Has Forward Link Problem in Normal Operation

Follow the procedure in Table 6-13 to troubleshoot a forward link problem during normal operation after passing a reduced ATP.

Table 6-13: Troubleshooting Forward Link Failure (BTS Passed Reduced ATP)

n Step Action

1 Perform the following additional tests to troubleshoot a forward link problem: 1a – TX mask 1b – TX rho 1c – TX code domain

Cannot Perform TX Mask Measurement

Table 6-14: Troubleshooting TX Mask Measurement Failure

n Step Action

1 Verify that TX audit passes for the BBX(s).

2 If performing manual measurement, verify analyzer setup.

3 Verify that no LPA in the sector is in alarm state (flashing red LED). Re-set the LPA by pulling the

circuit breaker, and, after 5 seconds, pushing it back in.

Cannot Perform Rho or Pilot Time Offset Measurement

Table 6-15: Troubleshooting Rho and Pilot Time Offset Measurement Failure

n Step Action

1 Verify presence of RF signal by switching to spectrum analyzer screen.

2 Verify PN offsets displayed on the analyzer is the same as the PN offset in the CDF file.

3 Re–load MGLI code and data and repeat the test.

4 If performing manual measurement, verify analyzer setup.

5 Verify that no LPA in the sector is in alarm state (flashing red LED). Reset the LPA by pulling the

circuit breaker, and, after 5 seconds, pushing back in.

6 If Rho value is unstable and varies considerably (e.g. .95,.92,.93), this may indicate that the GPS

is still phasing (trying to reach and maintain 0 freq. error). Go to the freq. bar in the upper right corner of the Rho meter and select Hz. Press <Shift–avg> and enter 10, to obtain an average Rho value. This is an indication the GPS has not stabilized before going INS and may need to be re-initialized.

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Troubleshooting: Transmit ATP

68P64115A18–1

Cannot Perform Code Domain Power and Noise Floor Measurement

Table 6-16: Troubleshooting Code Domain Power and Noise Floor Measurement Failure

n Step Action

1 Verify presence of RF signal by switching to spectrum analyzer screen on the communications

system analyzer. 2 Verify PN offset displayed on analyzer is same as PN offset being used in the CDF file. 3 Disable and re-enable MCC (one or more MCCs based on extent of failure).

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Troubleshooting: Receive ATP

Multi–FER Test Failure

Table 6-17: Troubleshooting Multi-FER Failure

n Step Action

1 Verify test equipment is configured correctly for a FER test. 2 Verify test equipment is locked to 19.6608 and even second clocks. On the HP 8921 analyzer, the

yellow LED (REF UNLOCK) must be OFF. 3 Verify MCCs have been loaded with data and are INS_ACT. 4 Disable and re-enable the MCC (1 or more based on extent of failure). 5 Disable, re-load code and data, and re-enable MCC (one or more MCCs based on extent of

failure). 6 Verify antenna connections to frame are correct based on the LMF directions messages. 7 For diversity RX FER failures in companion frame configurations, verify the following:

Troubleshooting: Receive ATP68P64115A18–1

7a – Inter–frame diversity RX cables are correctly connected between RX EXPANSION

connectors on each frame (refer to SC4812ET Lite Installation; 68P09253A36.

7b – The RX test cable is connected to the correct RX antenna connector on the opposite

companion frame (refer to Table 4-1).

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Troubleshooting: CSM Check–list

68P64115A18–1

Troubleshooting: CSM Check–list

Problem Description

Many Clock Synchronization Manager (CSM) board problems may be resolved in the field before sending the boards to the factory for repair. This section describes known CSM problems identified in field returns, some of which are field-repairable. Check these problems before returning suspect CSM boards.

Intermittent 19.6608 MHz Reference Clock / GPS Receiver Operation

If having any problems with CSM board kit numbers, SGLN1145 or SGLN4132, check the suffix with the kit number. If the kit has version “AB,” then replace with version ‘‘BC’’ or higher, and return model AB to the repair center.

No GPS Reference Source

Correct Hardware

Check the CSM boards for proper hardware configuration for the type of GPS in use and the cage slot where they are installed.

RF–GPS (Local GPS) – CSM kit SGLN1145, which should be installed in Slot l, has an on-board GPS receiver; while kit SGLN4132, in Slot 2, does not have a GPS receiver.

Remote GPS (RGPS) – Kit SGLN4132ED or later, which should be installed in both Slot 1 and Slot 2, does not have a GPS receiver.

Any incorrectly configured board must be returned to the repair center. Do not attempt to change hardware configuration in the field. Also,

verify the GPS antenna is not damaged and is installed per recommended guidelines.

RGPS Expansion Cabling

20–pair Punchblock Connections – For companion frame installations with RGPS, verify the 20–pair punchblock RGPS distribution connections in the RGPS expansion primary frame are correctly punched down in accordance with NO TAG.

50–pair Punchblock Connections – For companion frame installations with RGPS, verify the 50–pair punchblock RGPS distribution connections in both the RGPS expansion primary and secondary frames are correctly punched down in accordance with NO TAG and NO TAG.

Checksum Failure

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The CSM could have corrupted data in its firmware resulting in a non-executable code. The problem is usually caused by either electrical disturbance, or interruption of data during a download. Attempt another download with no interruptions in the data transfer. Return CSM board back to repair center if the attempt to reload fails.

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GPS Bad RX Message T ype

RF GPS

REMOTE

This is believed to be caused by a later version of CSM software (3.5 or higher) being downloaded, via LMF, followed by an earlier version of CSM software (3.4 or lower), being downloaded from the CBSC. Download again with CSM software code 3.5 or higher. Return CSM board back to repair center if attempt to reload fails.

CSM Reference Source Configuration Error

This is caused by incorrect reference (clock) source configuration performed in the field by software download. CSM kit SGLN1145 and SGLN4132 must have proper reference sources configured, as shown in Table 6-18, to function correctly.

Table 6-18: CSM Reference (Clock) Sources by GPS Type and Kit Number

Troubleshooting: CSM Check–list68P64115A18–1

Hardware

GPS Type CSM Kit No.

SGLN1145 With GPS Receiver 1 Primary = Local GPS

SGLN4132 Without GPS

SGLN4132ED

REMOTE

GPS

or later

Configuration

Receiver Without GPS

Receiver

Takes Too Long for CSM to Come INS

This may be caused by a delay in GPS acquisition. Check the accuracy flag status and/or current position. Refer to the CSM System Time/GPS and LFR/HSO Verification section of Chapter 3. At least one satellite should be visible and tracked for the “surveyed” mode, and four satellites should be visible and tracked for the “estimated” mode. Also, verify correct base site position data used in “surveyed” mode.

CSM

Slot No.

2 Primary = Mate GPS

1 Primary = Remote GPS

2 Primary = Remote GPS

Reference Source Configuration

Backup = Either LFR or HSO

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Troubleshooting: SCCP Backplane

Introduction

The SCCP backplane is a multi–layer printed circuit board that interconnects all the SCCP modules. The complexity of this board lends itself to possible improper diagnoses when problems occur.

Connector Functionality

The following connector overview describes the major types of backplane connectors along with the functionality of each. This will assist the CFE to:

S Determine which connector(s) is associated with a specific problem

type.

S Isolate problems to a specific cable or connector.

Span Line Connector

The span line input is an 8 pin RJ–45 connector that provides a primary and secondary (if used) span line interface to each GLI in the SCCP shelf. The span line is used for MM/EMX switch control of the Master GLI and also all the BBX traffic.

68P64115A18–1

Power Input (Return A and B connectors)

Provides 27 volt input for use by the power supply modules.

Power Supply Module Interface

Each power supply module has a series of three different connectors to provide the needed inputs/outputs to the SCCP backplane. These include a VCC/Ground input connector, a Harting–style multiple pin interface, and a +15V/Analog Ground output connector. The Transceiver Power Module converts 27/48 Volts to a regulated +15, +6.5, +5.0 volts to be used by the SCCP shelf cards.

GLI Connector

This connector consists of a Harting 4SU digital connector and a 6–conductor coaxial connector for RDM distribution. The connectors provide inputs/outputs for the GLIs in the SCCP backplane.

GLI Ethernet “A” and “B” Connections

These SMB connectors are located on the SCCP backplane and connect to the GLI board. This interface provides all the control and data communications over the Ethernet LAN between the master GLI, the redundant GLI, and the LMF.

6-20

BBX Connector

Each BBX connector consists of a Harting 2SU/1SU digital connector and two 6–conductor coaxial connectors. These connectors provide DC, digital, and RF inputs/outputs for the BBXs in the SCCP backplane.

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CIO Connectors

S RF RX antenna path signal inputs are routed through RX paths of the

DRDCs or TRDCs at the RF interface panel (rear of frame), and through coaxial cables to the two MPC modules. The three “A” (main) signals go to one MPC; the three “B” (diversity) to the other. The MPC outputs the low–noise–amplified signals through the SCCP backplane to the CIO where the signals are split and sent to the appropriate BBX.

S A digital bus then routes the baseband signal through the BBX, to the

backplane, and then on to the MCC slots.

S Digital TX antenna path signals originate at the MCCs. Each output is

routed from the MCC slot through the backplane to the appropriate BBX.

S TX RF path signal originates from the BBX, travels through the

backplane to the CIO, through the CIO, and then through multi-conductor coaxial cabling to the trunking module and LPAs in the LPA shelf.

SCCP Backplane T roubleshooting Procedure

Troubleshooting: SCCP Backplane68P64115A18–1

NOTE

The following tables provide standard procedures for troubleshooting problems that appear to be related to a defective SCCP backplane. The tables are broken down into possible problems and steps which should be taken in an attempt to find the root cause.

All steps in all tables should be followed before any attempt to replace the SCCP backplane.

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Troubleshooting: SCCP Backplane

68P64115A18–1

Digital Control Problems

No GLI Control via LMF (all GLIs)

Table 6-19: No GLI Control Through LMF (All GLIs)

Step Action

1 Check the Ethernet LAN for proper connection, damage, shorts, or opens. 2 Be sure the LAN IN and OUT connectors in the power entry compartment are properly terminated. 3 Be sure the proper IP address is entered in the Network Login tab of the LMF login screen. 4 Logout and Exit the LMF, restart the LMF, and re–login to the BTS. 5 Verify SCCP backplane Shelf ID DIP switch is set correctly. 6 Visually check the master GLI connectors (both module and backplane) for damage. 7 Replace the master GLI with a known good GLI.

No GLI Control through Span Line Connection (All GLIs)

Table 6-20: No GLI Control Through Span Line Connection (Both GLIs)

Step Action

1 Verify SCCP backplane Shelf ID DIP switch is set correctly. 2 Verify that the BTS and GLIs are correctly configured in the OMCR/CBSC database. 3 Verify the span configurations set in the GLIs match those in the OMC–R/CBSC database (refer to

Table 6-31).

4 Visually check the master GLI connectors (both module and backplane) for damage.

5 Replace the master GLI with a known good GLI. 6 Check the span line cabling from the punchblock to the master GLI for proper connection and damage.

Table 6-21: MGLI Control Good – No Control Over Co–located GLI

Step Action

1 Verify that the BTS and GLIs are correctly configured in the OMCR/CBSC data base. 2 Check the ethernet for proper connection, damage, shorts, or opens. 3 Visually check all GLI connectors (both module and backplane) for damage. 4 Replace the remaining GLI with a known good GLI.

No AMR Control (MGLI good)

Table 6-22: MGLI Control Good – No Control Over AMR

Step Action

1 Visually check the master GLI connectors (both module and backplane) for damage. 2 Replace the master GLI with a known good GLI. 3 Replace the AMR with a known good AMR.

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Troubleshooting: SCCP Backplane68P64115A18–1

No BBX Control in the Shelf

Table 6-23: MGLI Control Good – No Control over Co–located BBXs

Step Action

1 Visually check all GLI connectors (both module and backplane) for damage. 2 Replace the remaining GLI with a known good GLI. 3 Visually check BBX connectors (both module and backplane) for damage. 4 Replace the BBX with a known good BBX.

No (or Missing) Span Line Traffic

Table 6-24: BBX Control Good – No (or Missing) Span Line Traffic

Step Action

1 Visually check all GLI connectors (both module and backplane) for damage. 2 Replace the remaining GLI with a known good GLI. 3 Visually check all span line distribution (both connectors and cables) for damage. 4 If the problem seems to be limited to one BBX, replace the BBX with a known good BBX.

No (or Missing) MCC24E/MCC8E Channel Elements

Table 6-25: No MCC–1X/MCC24E/MCC8E Channel Elements

Step Action

1 Verify channel elements on a co–located MCC of the same type (CDF MccType codes: MCC8E = 0;

MCC24E = 2; MCC–1X = 3) 2 Check MCC connectors (both module and backplane) for damage. 3 If the problem seems to be limited to one MCC, replace it with a known good MCC of the same type. 4 If no channel elements on any MCC, verify clock reference to CIO.

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Troubleshooting: SCCP Backplane

DC Power Problems

68P64115A18–1

WARNING

Potentially lethal voltage and current levels are routed to the BTS equipment. This test must be carried out with a second person present, acting in a safety role. Remove all rings, jewelry, and wrist watches prior to beginning this test.

No DC Input Voltage to SCCP Shelf Power Supply Modules

Table 6-26: No DC Input Voltage to Power Supply Module

Step Action

1 Verify DC power is applied to the frame. Determine if any circuit breakers are tripped.

NOTE

If a breaker has tripped, remove all modules from the SCCP shelf and attempt to reset it.

– If breaker trips again, there is probably a cable or breaker problem within the frame or DC PDA. – If breaker does not trip, there is probably a defective module or sub–assembly within the shelf.

Perform the tests in Table 2-3 to attempt to isolate the module. 2 Verify that the PS1 and PS2 circuit breakers on the DC PDA are functional. 3 Remove the frame rear access panel (Figure 2-2), and use a voltmeter to determine if the input voltage

is being routed to the SCCP backplane. Measure the DC voltage level between:

S The PWR_IN_A and PWR_RTN_A contacts on the extreme right side at the rear of the backplane S The PWR_IN_B and PWR_RTN_B contacts on the extreme right side at the rear of the backplane

– If the voltage is not present, there is probably a cable or circuit breaker problem within the frame

or DC PDA.

4 If everything appears to be correct, visually inspect the PS1 and PS2 power supply module connectors. 5 Replace the power supply modules with known good modules. 6 If steps 1 through 4 fail to indicate a problem, an SCCP backplane failure has occurred (possibly an

open trace).

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Troubleshooting: SCCP Backplane68P64115A18–1

No DC Voltage (+5, +6.5, or +15 Volts) to a Specific GLI, BBX, or Switch Module

Table 6-27: No DC Input Voltage to any SCCP Shelf Module

Step Action

1 If it has not been done, perform the steps in Table 6-26. 2 Inspect SCCP shelf module connectors (both module and backplane) for damage. 3 Replace suspect modules with known good module.

TX and RX Signal Routing Problems

Table 6-28: TX and RX Signal Routing Problems

Step Action

1 Inspect all Harting cable connectors and backplane connectors for damage in all the affected board

slots.

2 Perform steps outlined in the RF path troubleshooting flowchart in Figure 6-1.

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Troubleshooting: RFDS

68P64115A18–1

Troubleshooting: RFDS

Introduction

The RFDS is used to perform Pre–Calibration Verification and Post-Calibration Audits which limit-check the RFDS-generate and reported receive levels of every path from the RFDS through the directional coupler coupled paths. In the event of test failure, refer to the following tables.

All Tests Fail

Table 6-29: RFDS Fault Isolation – All Tests Fail

Step Action

1 Check the TX calibration equipment for proper operation by manually setting the signal generator

output attenuator to the lowest output power setting and connecting the output port to the spectrum analyzer RF input port.

2 Set the signal generator output attenuator to –90 dBm, and switch on the RF output. Verify that the

spectrum analyzer can receive the signal, indicate the correct signal strength, (accounting for the cable insertion loss), and the approximate frequency.

3 Visually inspect RF cabling. Make sure each directional coupler forward and reflected port connects to

the RFDS antenna select unit on the RFDS.

4 Check the wiring against the site documentation wiring diagram or the SC4812ET Lite Installation;

68P09253A36. 5 Verify any changes to the RFDS parameter settings have been downloaded. 6 Status the TSU to verify the TSIC and SUA software versions are correct.

7 Check to see that all RFDS boards show green on the front panel LED indicators. Visually check for

external damage. 8 If any board LEDs do not show green, replace the RFDS with a known–good unit. Re–test after

replacement.

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Troubleshooting: RFDS68P64115A18–1

All RX and TX Paths Fail

If every receive or transmit path fails, the problem most likely lies with the rf converter board or the transceiver board. Replace the RFDS with a known–good unit and retest.

All Tests Fail on a Single Antenna

If all path failures are on one antenna port, forward and/or reflected, make the following checks.

Table 6-30: RFDS Fault Isolation – All Tests Fail on Single Antenna Path

Step Action

1 Visually inspect the frame internal RFDS cabling to the suspect TRDC or DRDC. 2 Verify the forward and reflected ports connect to the correct RFDS antenna select unit positions on the

RFDS ASU card. Refer to the RFDS installation manual for details. 3 Replace the RFDS with a known–good unit. 4 Replace the RF cables between the affected TRDC or DRDC and the RFDS.

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Module Front Panel LED Indicators and Connectors

Module Status Indicators

Each of the non-passive plug-in modules has a bi-color (green and red) LED status indicator located on the module front panel. The indicator is labeled PWR/ALM. If both colors are turned on, the indicator is yellow.

Each plug-in module, except for the fan module, has its own alarm (fault) detection circuitry that controls the state of the PWR/ALM LED.

The fan TACH signal of each fan module is monitored by the AMR. Based on the status of this signal the AMR controls the state of the PWR/ALM LED on the fan module.

Module LED Status (except GLI2, CSM, BBX, MCC)

PWR/ALM LED

The following list describes the states of the module status indicator.

S Solid GREEN – module operating in a normal (fault free) condition. S Solid RED – module is operating in a fault (alarm) condition due to

electrical hardware failure.

68P64115A18–1

Note that a fault (alarm) indication may or may not be due to a complete module failure and normal service may or may not be reduced or interrupted.

DC/DC Converter LED Status Combinations

The PWR CNVTR has its own alarm (fault) detection circuitry that controls the state of the PWR/ALM LED.

PWR/ALM LED

The following list describes the states of the bi-color LED.

S Solid GREEN – module operating in a normal (fault free) condition. S Solid RED – module is operating in a fault (alarm) condition due to

electrical hardware problem.

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CSM LED Status Combinations

PWR/ALM LED

The CSMs include on-board alarm detection. Hardware and software/firmware alarms are indicated via the front panel indicators.

After the memory tests, the CSM loads OOS–RAM code from the Flash EPROM, if available. If not available, the OOS–ROM code is loaded from the Flash EPROM.

S Solid GREEN – module is INS_ACT or INS_SBY no alarm. S Solid RED – Initial power up or module is operating in a fault (alarm)

condition.

S Slowly Flashing GREEN – OOS_ROM no alarm. S Long RED/Short GREEN – OOS_ROM alarm. S Rapidly Flashing GREEN – OOS_RAM no alarm or

INS_ACT in DUMB mode.

S Short RED/Short GREEN – OOS_RAM alarm. S Long GREEN/Short RED – INS_ACT or INS_SBY alarm. S Off – no DC power or on-board fuse is open.

Module Front Panel LED Indicators and Connectors68P64115A18–1

S Solid YELLOW – After a reset, the CSMs begin to boot. During

SRAM test and Flash EPROM code check, the LED is yellow. (If SRAM or Flash EPROM fail, the LED changes to a solid RED and the CSM attempts to reboot.)

Figure 6-2: CSM Front Panel Indicators & Monitor Ports

SYNC MONITOR

PWR/ALM Indicator

FREQ MONITOR

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Module Front Panel LED Indicators and Connectors

FREQ Monitor Connector

A test port provided at the CSM front panel via a BNC receptacle allows monitoring of the 19.6608 MHz clock generated by the CSM. When both CSM 1 and CSM 2 are in an in-service (INS) condition, the CSM 2 clock signal frequency is the same as that output by CSM 1.

The clock is a sine wave signal with a minimum amplitude of +2 dBm (800 mVpp) into a 50 Ω load connected to this port.

SYNC Monitor Connector

A test port provided at the CSM front panel via a BNC receptacle allows monitoring of the “Even Second Tick” reference signal generated by the CSMs.

At this port, the reference signal is a Transistor–Transistor Logic (TTL) active–high signal with a pulse width of 153 nanoseconds.

MMI Connector

Behind front panel – only accessible when card is partially extended from SCCP shelf slot. The RS–232 MMI port connector is intended to be used primarily in the development or factory environment, but may be used in the field for debug/maintenance purposes.

68P64115A18–1

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GLI2 LED Status Combinations

The GLI2 module indicators, controls, and connectors are described below and shown in Figure 6-3.

The indicators and controls consist of:

S Four LEDs S One pushbutton

ACTIVE LED

Solid GREEN – GLI2 is active. This means that the GLI2 has shelf control and is providing control of the digital interfaces.

Off – GLI2 is not active (i.e., Standby). The mate GLI2 should be active.

MASTER LED

S Solid GREEN – GLI2 is Master (sometimes referred to as MGLI2). S Off – GLI2 is non-master (i.e., Slave).

Module Front Panel LED Indicators and Connectors68P64115A18–1

ALARM LED

S Solid RED – GLI2 is in a fault condition or in reset. S While in reset transition, STATUS LED is OFF while GLI2 is

performing ROM boot (about 12 seconds for normal boot).

S While in reset transition, STATUS LED is ON while GLI2 is

performing RAM boot (about 4 seconds for normal boot).

S Off – No Alarm.

STATUS LED

S Flashing GREEN– GLI2 is in service (INS), in a stable operating

condition.

S On – GLI2 is in OOS RAM state operating downloaded code. S Off – GLI2 is in OOS ROM state operating boot code.

SPANS LED

S Solid GREEN – Span line is connected and operating. S Solid RED – Span line is disconnected or a fault condition exists.

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Module Front Panel LED Indicators and Connectors

GLI2 Pushbuttons and Connectors

RESET Pushbutton – Depressing the RESET pushbutton causes a partial reset of the CPU and a reset of all board devices. GLI2 will be placed in the OOS_ROM state (blue).

MMI Connector – The RS–232MMI port connector is intended primarily for development or factory use but may be used in the field for debug/maintenance purposes.

Figure 6-3: GLI2 Front Panel Operating Indicators

LED OPERATING STATUS

STATUS OFF − operating normally

ON − briefly during powerup when the Alarm LED turns OFF. SLOW GREEN − when the GLI2 is INS (inservice)

All functions on the GLI2 are reset when pressing and releasing the switch.

ON − briefly during powerup when the Alarm LED turns OFF. SLOW GREEN − when the GLI2 is INS (inservice)

STATUS LED

RESET PUSHBUTTON

STATUS RESET ALARM SPANS MASTER MMI ACTIVE

RESET

ALARM OFF − operating normally

68P64115A18–1

ALARM LED

SPANS LED

MASTER LED

MMI PORT CONNECTOR

ACTIVE LED

SPANS

MASTER

MMI PORT CONNECTOR

ACTIVE

OFF − card is powered down, in initialization, or in standby GREEN − operating normally YELLOW − one or more of the equipped initialized span s is receiving a remote alarm indication signal from the far end RED − one or more of the equipped initialized spans is in an alarm state

The pair of GLI2 cards include a redundant status. The card in the top shelf is designated by hardware as the active card; the card in the bottom shelf is in the standby mode.

ON − operating normally as active card OFF − operating normally as standby card

An RS232, serial, asynchronous communications link for use as an MMI port. This port supports 300 baud, up to a maximum of 115,200 baud communications.

Shows the operating status of the redundant cards. The redundant card toggles automatically if the active card is removed or fails

ON − active card operating normally OFF − standby card operating normally

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BBX LED Status Combinations

PWR/ALM LED

The BBX2 and BBX–1X modules have their own alarm (fault) detection circuitry that controls the state of the PWR/ALM LED.

The following list describes the states of the bi-color PWR/ALM LED for both BBX2 and BBX–1X cards:

S Solid GREEN – INS_ACT no alarm S Solid RED Red – initializing or power-up alarm S Slowly Flashing GREEN – OOS_ROM no alarm S Long RED/Short GREEN – OOS_ROM alarm S Rapidly Flashing GREEN – OOS_RAM no alarm S Short RED/Short GREEN – OOS_RAM alarm S Long GREEN/Short RED – INS_ACT alarm

MCC LED Status Combinations

Module Front Panel LED Indicators and Connectors68P64115A18–1

The MCC24E and MCC–1X modules have bi–color LED indicators and two connectors as described below. See Figure 6-4. Note that the figure does not show the connectors because they are concealed by the removable lens.

The LED indicators and their states are as follows:

PWR/ALM LED

S RED – fault on module

ACTIVE LED

S Off – module is inactive, off-line, or not processing traffic. S Slowly Flashing GREEN – OOS_ROM no alarm. S Rapidly Flashing Green – OOS_RAM no alarm. S Solid GREEN – module is INS_ACT, on-line, processing traffic.

PWR/ALM and ACTIVE LEDs

S Solid RED – module is powered but is in reset or the Board Control

Processor (BCP) is inactive.

Mar 2003

MMI Connectors

S The RS–232 MMI port connector (four-pin) is intended primarily for

development or factory use but may be used in the field for debugging purposes.

S The RJ–45 Ethernet port connector (eight-pin) is intended primarily

for development use but may be used in the field for high data rate debugging purposes.

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Module Front Panel LED Indicators and Connectors

Figure 6-4: MCC24 and MCC–1X Front Panel LEDs and LED Indications

PWR/ALM ACTIVE

PWR/ALM L E D

LED OPERATING STATUSCOLOR

68P64115A18–1

PWR/ALM OFF – Operating normally

LENS (REMOVABLE)

ACTIVE LED

RED

An alarm is generated in the event of a failure

GREENACTIVE

RED

ON – Briefly during power–up and during failure conditions

RAPIDLY FLASHING – Card is code–loaded but not enabled

SLOW FLASHING – Card is not code–loaded ON – Card is code–loaded and enabled (INS_ACT)

ON – 1) Briefly during power–up

2) Continuously during fault conditions

SLOW FLASHING (alternately with green) – Concentration Highway Interface (CHI) bus inactive on power–up

4812ETL0030–1

LPA LED Status Combinations

LPA Module LED

Each LPA module is provided with a bi–color LED on the ETIB module next to the MMI connector. Interpret this LED as follows:

6-34

S GREEN — LPA module is active and is reporting no alarms (Normal

condition).

S Flashing GREEN/RED — LPA module is active but is reporting an

low input power condition. If no BBX is keyed, this is normal and does not constitute a failure.

S Flashing RED — LPA is in alarm.

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Troubleshooting: Span Control Link

Span Problems (No Control Link)

Table 6-31: Troubleshoot Control Link Failure

n Step Action

1 Connect the LMF computer to the MMI port on the applicable MGLI2/GLI2 as shown in

Figure 6-5.

2 Start an MMI communication session with the applicable MGLI2/GLI2 by using the Windows

desktop shortcut icon (refer to Table 3-10).

3 Once the connection window opens, press the LMF computer Enter key until the GLI2> prompt

is obtained. At the GLI2> prompt, enter:

config ni current <cr> (equivalent of span view command)

The system will respond with a display similar to the following:

The frame format in flash is set to use T1_2. Equalization: Span A – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span B – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span C – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span D – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span E – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span F – Default (0–131 feet for T1/J1, 120 Ohm for E1)

Troubleshooting: Span Control Link68P64115A18–1

Linkspeed: Default (56K for T1 D4 AMI, 64K otherwise) Currently, the link is running at the default rate The actual rate is 0

NOTE

Defaults for span equalization are 0–131 feet for T1/J1 spans and 120 Ohm for E1. Default linkspeed is 56K for T1 D4 AMI spans and 64K for all other types. There is no need to change from defaults unless the OMCR/CBSC span configuration requires it.

5 The span configurations loaded in the GLI must match those in the OMCR/CBSC database for the

BTS. If they do not, proceed to Table 6-32. 6 Repeat steps 1 through 5 for all remaining GLIs. 7 If the span settings are correct, verify the edlc parameters using the show command.

Any alarm conditions indicate that the span is not operating correctly.

S Try looping back the span line from the DSX panel to the MM, and verify that the looped signal

is good.

S Listen for control tone on the appropriate timeslot from the Base Site and MM.

8 Exit the GLI MMI session and HyperTerminal connection by selecting File from the connection

window menu bar, and then Exit from the pull–down menu.

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Troubleshooting: Span Control Link

Figure 6-5: MGLI/GLI Board MMI Connection Detail

68P64115A18–1

STATUS LED

8–PIN

To MMI port

8–PIN TO 10–PIN RS–232 CABLE (P/N 30–09786R01)

STATUS RESET ALARM SPANS MASTER MMI ACTIVE

RESET Pushbutton

ALARM LED

SPANS LED

MASTER LED

MMI Port Connector

ACTIVE LED

NULL MODEM

BOARD

(TRN9666A)

LMF COMPUTER

COM1

COM2

RS–232 CABLE

DB9–TO–DB25 ADAPTER

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Set BTS Site Span Configuration

Troubleshooting: Span Control Link68P64115A18–1

NOTE

Perform the following procedure ONLY if span configurations loaded in the MGLI2/GLI2s do not match those in the OMCR/CBSC data base, AND ONLY when the exact configuration data is available. Loading incorrect span configuration data will render the site inoperable.

Table 6-32: Set BTS Span Parameter Configuration

n Step Action

1 If not previously done, connect the LMF computer to the MMI port on the applicable

MGLI2/GLI2 as shown in Figure 6-5. 2 If there is no MMI communication session in progress with the applicable MGLI2/GLI2, initiate

one by using the Windows desktop shortcut icon (refer to Table 3-10). 3 At the GLI2> prompt, enter:

config ni format <option> <cr>

The terminal will display a response similar to the following:

COMMAND SYNTAX: config ni format option Next available options: LIST – option : Span Option E1_1 : E1_1 – E1 HDB3 CRC4 no TS16 E1_2 : E1_2 – E1 HDB3 no CRC4 no TS16 E1_3 : E1_3 – E1 HDB3 CRC4 TS16 E1_4 : E1_4 – E1 HDB3 no CRC4 TS16 T1_1 : T1_1 – D4, AMI, No ZCS T1_2 : T1_2 – ESF, B8ZS J1_1 : J1_1 – ESF, B8ZS (Japan) – Default J1_2 : J1_2 – ESF, B8ZS T1_3 : T1_3 – D4, AMI, ZCS>

NOTE

With this command, all active (in–use) spans will be set to the same format.

To set or change the span type, enter the correct option from the list at the entry prompt (>), as

shown in the following example:

> T1_2 <cr>

NOTE

The entry is case–sensitive and must be typed exactly as it appears in the list. If the entry is typed

incorrectly, a response similar to the following will be displayed:

CP: Invalid command GLI2>

5 An acknowledgement similar to the following will be displayed:

The value has been programmed. It will take effect after the next reset. GLI2>

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6-37

Troubleshooting: Span Control Link

Table 6-32: Set BTS Span Parameter Configuration

n ActionStep

6 If the current MGLI/GLI span rate must be changed, enter the following MMI command:

config ni linkspeed <cr>

The terminal will display a response similar to the following:

Next available options: LIST – linkspeed : Span Linkspeed 56K : 56K (default for T1_1 and T1_3 systems)

64K : 64K (default for all other span configurations) >

NOTE

With this command, all active (in–use) spans will be set to the same linkspeed.

To set or change the span linkspeed, enter the required option from the list at the entry prompt (>),

as shown in the following example:

> 64K <cr>

68P64115A18–1

NOTE

The entry is case–sensitive and must be typed exactly as it appears in the list. If the entry is typed

incorrectly, a response similar to the following will be displayed:

CP: Invalid command

GLI2>

8 An acknowledgement similar to the following will be displayed:

The value has been programmed. It will take effect after the next reset. GLI2>

9 If the span equalization must be changed, enter the following MMI command:

config ni equal <cr>

The terminal will display a response similar to the following:

COMMAND SYNTAX: config ni equal span equal Next available options: LIST – span : Span a : Span A b : Span B c : Span C d : Span D e : Span E f : Span F >

. . . continued on next page

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Troubleshooting: Span Control Link68P64115A18–1

Table 6-32: Set BTS Span Parameter Configuration

n ActionStep

10 At the entry prompt (>), enter the designator from the list for the span to be changed as shown in

the following example:

> a <cr>

The terminal will display a response similar to the following:

COMMAND SYNTAX: config ni equal a equal Next available options: LIST – equal : Span Equalization 0 : 0–131 feet (default for T1/J1) 1 : 132–262 feet 2 : 263–393 feet 3 : 394–524 feet 4 : 525–655 feet 5 : LONG HAUL 6 : 75 OHM 7 : 120 OHM (default for E1) >

11 At the entry prompt (>), enter the code for the required equalization from the list as shown in the

following example:

> 0 <cr>

The terminal will display a response similar to the following:

> 0 The value has been programmed. It will take effect after the next reset. GLI2>

12 Repeat steps 9 through 11 for each in–use span. 13

* IMPORTANT

After executing the config ni format, config ni linkspeed, and/or config ni equal

commands, the affected MGLI/GLI board MUST be reset and reloaded for changes to take effect.

Although defaults are shown, always consult site specific documentation for span type and

linkspeed used at the site.

Press the RESET button on the MGLI2/GLI2 for changes to take effect.

. . . continued on next page

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Troubleshooting: Span Control Link

68P64115A18–1

Table 6-32: Set BTS Span Parameter Configuration

n ActionStep

14 Once the MGLI/GLI has reset, execute the following command to verify span settings are as

required:

config ni current <cr> (equivalent of span view command)

The system will respond with a display similar to the following:

The frame format in flash is set to use T1_2. Equalization: Span A – 0–131 feet Span B – 0–131 feet Span C – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span D – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span E – Default (0–131 feet for T1/J1, 120 Ohm for E1) Span F – Default (0–131 feet for T1/J1, 120 Ohm for E1)

Linkspeed: 64K Currently, the link is running at 64K The actual rate is 0

15 If the span configuration is not correct, perform the applicable step from this table to change it and

repeat steps 13 and 14 to verify required changes have been programmed.

16 Return to step 6 of Table 6-31.

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Appendix A

Data Sheets

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A-1

Optimization (Pre–ATP) Data Sheets

68P64115A18–1

Optimization (Pre–ATP) Data Sheets

Verification of Test Equipment Used

T able A-1: Verification of Test Equipment Used

Manufacturer Model Serial Number

Comments:________________________________________________________ __________________________________________________________________

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Site Checklist

T able A-2: Site Checklist

OK Parameter Specification Comments

− Deliveries Per established procedures

− Floor Plan Verified

Inter Frame Cables:

−

− Site Temperature

− Dress Covers/Brackets

Ethernet

Frame Ground

Power

Factory Data:

BBX

Test Panel

RFDS

Per procedure Per procedure Per procedure

Preliminary Operations

T able A-3: Preliminary Operations

OK Parameter Specification Comments

− Frame ID DIP Switches Per site equipage

− Ethernet LAN verification Verified per procedure

Comments:_________________________________________________________

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Optimization (Pre–ATP) Data Sheets

68P64115A18–1

Pre–Power and Initial Power Tests

Table A3a: Pre–power Checklist

OK Parameter Specification Comments

− Pre–power–up tests Table 2-3 Table 2-4

Internal Cables:

−

Span CSM Power Ethernet Connectors

LAN A ohms LAN B ohms LAN A shield LAN B shield LAN A IN & OUT terminators LAN B IN & OUT terminators

Ethernet Boots

verified verified verified

verified verified isolated isolated installed installed installed

− Air Impedance Cage (single cage) installed

− Initial power–up tests Table 2-4

Table 2-6 Table 2-7

−

Frame fans LEDs

operational illuminated

Comments:_________________________________________________________

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General Optimization Checklist

Table A3b: General Optimization Checklist

OK Parameter Specification Comments

Preparing the LMF

−

Load LMF software Create site–specific BTS directory Create HyperTerminal connection

LMF–to–BTS Connection Verify GLI2 ethernet address settings Ping LAN A Ping LAN B

Verify ROM code loads for software release

Download/Enable MGLI2 Download/Enable GLI2 Set Site Span Configuration Set CSM clock source Enable CSMs Download/Enable MCCs (24/8E/1X) Download BBXs (2 or 1X) Program TSU NAM

Table 3-1 Table 3-2 Table 3-3

Table 3-5 Table 6-3 Table 3-11 Table 3-11

Table 3-12

Table 3-13 Table 3-13 Table 6-31 Table 3-15 Table 3-16 Table 3-14 Table 3-14 Table 3-46

−

Test Set Calibration

−

Test Cable Calibration

Comments:_________________________________________________________

Table 3-25 Table 3-26

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Optimization (Pre–ATP) Data Sheets

68P64115A18–1

GPS Receiver Operation

T able A-4: GPS Receiver Operation

OK Parameter Specification Comments

− GPS Receiver Control Task State:

tracking satellites

− Initial Position Accuracy: Verify Estimated

− Current Position:

lat lon height

− Current Position: satellites tracked Estimated:

(>4) satellites tracked,(>4) satellites visible

Surveyed:

1) satellite tracked,(>4) satellites visible

− GPS Receiver Status:Current Dilution of Precision (PDOP or HDOP): (<30)

Verify parameter

or Surveyed RECORD in

msec and cm also convert to deg min sec

Verify parameter as appropriate:

Verify parameter

− Current reference source:

Verify parameter

Number: 0; Status: Good; Valid: Yes

Comments:_________________________________________________________

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LFR Receiver Operation

T able A-5: LFR Receiver Operation

OK Parameter Specification Comments

− Station call letters M X Y Z

assignment.

− SN ratio is > 8 dB

− LFR Task State: 1fr

locked to station xxxx

− Current reference source:

Number: 1; Status: Good; Valid: Yes

Comments:_________________________________________________________

As specified in site documentation

Verify parameter

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Optimization (Pre–ATP) Data Sheets

Specification

68P64115A18–1

LPA IM Reduction

T able A-6: LPA IM Reduction

Parameter Comments

LPA

− 1A C1 C1 No Alarms

− 1B C1 C1 No Alarms

− 1C C1 C1 No Alarms

− 1D C1 C1 No Alarms

− 3A C2 C2 No Alarms

− 3B C2 C2 No Alarms

− 3C C2 C2 No Alarms

− 3D C2 C2 No Alarms

Comments:_________________________________________________________

CARRIER

2:1

3–SectorBP3–Sector

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carrier 1

carrier 2

TX Bay Level Offset / Power Output V erification for 3–Sector Configurations

1–Carrier 2–Carrier Non–adjacent Channels

T able A-7: TX BLO Calibration (3–Sector: 1–Carrier and 2–Carrier Non–adjacent Channels)

OK Parameter Specification Comments

−

Calibrate

carrier 1

Calibrate

carrier 2

TX Bay Level Offset = 42 dB (+5 dB) prior to calibration

BBX2–1, ANT–1A = dB BBX2–r, ANT–1A = dB

BBX2–2, ANT–2A = dB BBX2–r, ANT–2A = dB

BBX2–3, ANT–3A = dB BBX2–r, ANT–3A = dB

BBX2–4, ANT–1B = dB BBX2–r, ANT–1B = dB

BBX2–5, ANT–2B = dB BBX2–r, ANT–2B = dB

BBX2–6, ANT–3B = dB BBX2–r, ANT–3B = dB

−

Calibration

−

Comments:________________________________________________________

__________________________________________________________________

Audit

carrier 1

Calibration

Audit

carrier 2

0 dB (+0.5 dB) for gain set resolution post–calibration

BBX2–1, ANT–1A = dB BBX2–r, ANT–1A = dB

BBX2–2, ANT–2A = dB BBX2–r, ANT–2A = dB

BBX2–3, ANT–3A = dB BBX2–r, ANT–3A = dB

BBX2–4, ANT–1B = dB BBX2–r, ANT–1B = dB

BBX2–5, ANT–2B = dB BBX2–r, ANT–2B = dB

BBX2–6, ANT–3B = dB BBX2–r, ANT–3B = dB

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Optimization (Pre–ATP) Data Sheets

carrier 1

carrier 2

68P64115A18–1

2–Carrier Adjacent Channel

T able A-8: TX Bay Level Offset Calibration (3–Sector: 2–Carrier Adjacent Channels)

OK Parameter Specification Comments

−

Calibrate

carrier 1

Calibrate

carrier 2

Calibration

Audit

carrier 1

TX Bay Level Offset = 42 dB (typical), 38 dB (minimum) prior to calibration

0 dB (+0.5 dB) for gain set resolution post calibration

BBX2–1, ANT–1A = dB BBX2–r, ANT–1A = dB

BBX2–2, ANT–2A = dB BBX2–r, ANT–2A = dB

BBX2–3, ANT–3A = dB BBX2–r, ANT–3A = dB

BBX2–4, ANT–1B = dB BBX2–r, ANT–1B = dB

BBX2–5, ANT–2B = dB BBX2–r, ANT–2B = dB

BBX2–6, ANT–3B = dB BBX2–r, ANT–3B = dB

BBX2–1, ANT–1A = dB BBX2–r, ANT–1A = dB

BBX2–2, ANT–2A = dB BBX2–r, ANT–2A = dB

BBX2–3, ANT–3A = dB BBX2–r, ANT–3A = dB

−

Calibration

−

Comments:________________________________________________________

__________________________________________________________________

Audit

carrier 2

0 dB (+0.5 dB) for gain set resolution post calibration

BBX2–4, ANT–1B = dB BBX2–r, ANT–1B = dB

BBX2–5, ANT–2B = dB BBX2–r, ANT–2B = dB

BBX2–6, ANT–3B = dB BBX2–r, ANT–3B = dB

TX Antenna VSWR

T able A-9: TX Antenna VSWR

OK Parameter Specification Data

−

VSWR – Antenna 1A

VSWR – Antenna 2A

< (1.5 : 1)

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T able A-9: TX Antenna VSWR

OK DataSpecificationParameter

−

VSWR – Antenna 3A

VSWR – Antenna 1B

VSWR – Antenna 2B

VSWR – Antenna 3B

< (1.5 : 1)

Comments:________________________________________________________

__________________________________________________________________

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68P64115A18–1

RX Antenna VSWR

T able A-10: RX Antenna VSWR

OK Parameter Specification Data

VSWR –

−

Antenna 1A VSWR –

−

Antenna 2A VSWR –

−

Antenna 3A VSWR –

−

Antenna 1B VSWR –

−

Antenna 2B VSWR –

−

Antenna 3B

Comments:_________________________________________________________

< (1.5 : 1)

Alarm Verification

T able A-11: CDI Alarm Input Verification

OK Parameter Specification Data

Verify CDI alarm input operation per NO TAG.

−

Comments:_________________________________________________________

BTS Relay #XX – Contact Alarm Sets/Clears

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Site Serial Number Check List68P64115A18–1

Site Serial Number Check List

Date Site

SCCP Shelf

NOTE: For BBXs and MCCs, enter the type as well as serial number; for example, BBX2, BBX–1X, MCC8, MCC24, MCC–1X.

Site I/O A & B SCCP Shelf

CSM–1 CSM–2 HSO/LFR CCD–1 CCD–2 AMR–1 AMR–2 MPC–1 MPC–2 Fans 1–2 GLI2–1 GLI2–2 BBX–1 BBX–2 BBX–3 BBX–4 BBX–5 BBX–6 BBX–R1 MCC–1 MCC–2 MCC–3 MCC–4 CIO SWITCH PS–1 PS–2

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A-13

Site Serial Number Check List

68P64115A18–1

LPAs

LPA 1A LPA 1B LPA 1C LPA 1D LPA 3A LPA 3B LPA 3C LPA 3D

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Appendix B

PN Offset/I & Q Offset Register

Programming Information

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B-1

PN Offset Programming Information

PN Offset Background

All channel elements transmitted from a BTS in a particular 1.25 MHz CDMA channel are orthonogonally spread by 1 of 64 possible Walsh code functions; additionally, they are also spread by a quadrature pair of PN sequences unique to each sector.

Overall, the mobile uses this to differentiate multiple signals transmitted from the same BTS (and surrounding BTS) sectors, and to synchronize to the next strongest sector.

The PN offset per sector is stored on the BBXs, where the corresponding I & Q registers reside.

The PN offset values are determined by BTS sector (antenna) based on the applicale CDF data field content. A breakdown of this information is found in Table B-1.

PN Offset Usage

There are three basic RF chip delays currently in use. It is important to determine what RF chip delay is valid to be able to test the BTS functionality. This can be done by ascertaining if the CDF value was set to “on” when the MCC was downloaded with “image data”. The delay (approximately 20 mS) in the BTS using any type of mobile meeting IS–97 specifications.

FineTxAdj value is used to compensate for the processing

68P64115A18–1

FineTxAdj

NOTE

Observe the following guidelines:

S If the FineTxAdj value in the CDF is 101 (65 HEX), the FineTxAdj

has not been set. The I and Q values from the 0 table MUST be used.

FineTxAdj value in the cdf file is 213 (D5 HEX), FineTxAdj has

If the been set for the 14 chip table.

S If the FineTxAdj value in the CDF file is 197 (C5 HEX), FineTxAdj

has been set for the 13 chip table.

CDF file I and Q values can be represented in DECIMAL or HEX. If using HEX, add 0x before the HEX value. If necessary, convert HEX values in Table B-1 to decimal before comparing them to cdf file I & Q value assignments.

– If a Qualcomm mobile is used, select I and Q values from the 13

chip delay table.

– If a mobile is used that does not have the 1 chip offset problem,

(any mobile meeting the IS–97 specification), select from the 14 chip delay table.

If the wrong I and Q values are used with the wrong FineTxAdj parameter, system timing problems will occur. This will cause the energy transmitted to be “smeared” over several Walsh codes (instead of the single Walsh code that it was assigned to), causing erratic operation. Evidence of smearing is usually identified by Walsh channels not at correct levels or present when not selected in the Code Domain Power Test.

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Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

0 17523 23459 4473 5BA3 29673 25581 73E9 63ED 4096 4096 1000 1000 1 32292 32589 7E24 7F4D 16146 29082 3F12 719A 9167 1571 23CF 0623 2 4700 17398 125C 43F6 2350 8699 092E 21FB 22417 7484 5791 1D3C 3 14406 26333 3846 66DD 7203 32082 1C23 7D52 966 6319 03C6 18AF 4 14899 4011 3A33 0FAB 19657 18921 4CC9 49E9 14189 2447 376D 098F 5 17025 2256 4281 08D0 28816 1128 7090 0468 29150 24441 71DE 5F79 6 14745 18651 3999 48DB 19740 27217 4D1C 6A51 18245 27351 4745 6AD7 7 2783 1094 0ADF 0446 21695 547 54BF 0223 1716 23613 06B4 5C3D 8 5832 21202 16C8 52D2 2916 10601 0B64 2969 11915 29008 2E8B 7150 9 12407 13841 3077 3611 18923 21812 49EB 5534 20981 5643 51F5 160B 10 31295 31767 7A3F 7C17 27855 28727 6CCF 7037 24694 28085 6076 6DB5 11 7581 18890 1D9D 49CA 24350 9445 5F1E 24E5 11865 18200 2E59 4718 12 18523 30999 485B 7917 30205 29367 75FD 72B7 6385 21138 18F1 5292 13 29920 22420 74E0 5794 14960 11210 3A70 2BCA 27896 21937 6CF8 55B1 14 25184 20168 6260 4EC8 12592 10084 3130 2764 25240 25222 6298 6286 15 26282 12354 66AA 3042 13141 6177 3355 1821 30877 109 789D 006D 16 30623 11187 779F 2BB3 27167 23525 6A1F 5BE5 30618 6028 779A 178C 17 15540 11834 3CB4 2E3A 7770 5917 1E5A 171D 26373 22034 6705 5612 18 23026 10395 59F2 289B 11513 23153 2CF9 5A71 314 15069 013A 3ADD 19 20019 28035 4E33 6D83 30409 30973 76C9 78FD 17518 4671 446E 123F 20 4050 27399 0FD2 6B07 2025 31679 07E9 7BBF 21927 30434 55A7 76E2 21 1557 22087 0615 5647 21210 25887 52DA 651F 2245 11615 08C5 2D5F 22 30262 2077 7636 081D 15131 18994 3B1B 4A32 18105 19838 46B9 4D7E 23 18000 13758 4650 35BE 9000 6879 2328 1ADF 8792 14713 2258 3979 24 20056 11778 4E58 2E02 10028 5889 272C 1701 21440 241 53C0 00F1 25 12143 3543 2F6F 0DD7 18023 18647 4667 48D7 15493 24083 3C85 5E13 26 17437 7184 441D 1C10 29662 3592 73DE 0E08 26677 7621 6835 1DC5 27 17438 2362 441E 093A 8719 1181 220F 049D 11299 19144 2C23 4AC8 28 5102 25840 13EE 64F0 2551 12920 09F7 3278 12081 1047 2F31 0417 29 9302 12177 2456 2F91 4651 23028 122B 59F4 23833 26152 5D19 6628 30 17154 10402 4302 28A2 8577 5201 2181 1451 20281 22402 4F39 5782 31 5198 1917 144E 077D 2599 19842 0A27 4D82 10676 21255 29B4 5307 32 4606 17708 11FE 452C 2303 8854 08FF 2296 16981 30179 4255 75E3 33 24804 10630 60E4 2986 12402 5315 3072 14C3 31964 7408 7CDC 1CF0 34 17180 6812 431C 1A9C 8590 3406 218E 0D4E 26913 115 6921 0073 35 10507 14350 290B 380E 17749 7175 4555 1C07 14080 1591 3700 0637 36 10157 10999 27AD 2AF7 16902 23367 4206 5B47 23842 1006 5D22 03EE 37 23850 25003 5D2A 61AB 11925 32489 2E95 7EE9 27197 32263 6A3D 7E07 38 31425 2652 7AC1 0A5C 27824 1326 6CB0 052E 22933 1332 5995 0534 39 4075 19898 0FEB 4DBA 22053 9949 5625 26DD 30220 12636 760C 315C 40 10030 2010 272E 07DA 5015 1005 1397 03ED 12443 4099 309B 1003 41 16984 25936 4258 6550 8492 12968 212C 32A8 19854 386 4D8E 0182 42 14225 28531 3791 6F73 18968 31109 4A18 7985 14842 29231 39FA 722F 43 26519 11952 6797 2EB0 25115 5976 621B 1758 15006 25711 3A9E 646F 44 27775 31947 6C7F 7CCB 26607 28761 67EF 7059 702 10913 02BE 2AA1 45 30100 25589 7594 63F5 15050 32710 3ACA 7FC6 21373 8132 537D 1FC4 46 7922 11345 1EF2 2C51 3961 22548 0F79 5814 23874 20844 5D42 516C 47 14199 28198 3777 6E26 19051 14099 4A6B 3713 3468 13150 0D8C 335E 48 17637 13947 44E5 367B 29602 21761 73A2 5501 31323 18184 7A5B 4708 49 23081 8462 5A29 210E 31940 4231 7CC4 1087 29266 19066 7252 4A7A 50 5099 9595 13EB 257B 22565 23681 5825 5C81 16554 29963 40AA 750B

. . . continued on next page

Mar 2003

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

B-3

PN Offset Programming Information

68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

51 32743 4670 7FE7 123E 28195 2335 6E23 091F 22575 6605 582F 19CD 52 7114 14672 1BCA 3950 3557 7336 0DE5 1CA8 31456 29417 7AE0 72E9 53 7699 29415 1E13 72E7 24281 30543 5ED9 774F 8148 22993 1FD4 59D1 54 19339 20610 4B8B 5082 29717 10305 7415 2841 19043 27657 4A63 6C09 55 28212 6479 6E34 194F 14106 17051 371A 429B 25438 5468 635E 155C 56 29587 10957 7393 2ACD 26649 23386 6819 5B5A 10938 8821 2ABA 2275 57 19715 18426 4D03 47FA 30545 9213 7751 23FD 2311 20773 0907 5125 58 14901 22726 3A35 58C6 19658 11363 4CCA 2C63 7392 4920 1CE0 1338 59 20160 5247 4EC0 147F 10080 17411 2760 4403 30714 5756 77FA 167C 60 22249 29953 56E9 7501 31396 29884 7AA4 74BC 180 28088 00B4 6DB8 61 26582 5796 67D6 16A4 13291 2898 33EB 0B52 8948 740 22F4 02E4 62 7153 16829 1BF1 41BD 23592 28386 5C28 6EE2 16432 23397 4030 5B65 63 15127 4528 3B17 11B0 19547 2264 4C5B 08D8 9622 19492 2596 4C24 64 15274 5415 3BAA 1527 7637 17583 1DD5 44AF 7524 26451 1D64 6753 65 23149 10294 5A6D 2836 31974 5147 7CE6 141B 1443 30666 05A3 77CA 66 16340 17046 3FD4 4296 8170 8523 1FEA 214B 1810 15088 0712 3AF0 67 27052 7846 69AC 1EA6 13526 3923 34D6 0F53 6941 26131 1B1D 6613 68 13519 10762 34CF 2A0A 19383 5381 4BB7 1505 3238 15969 0CA6 3E61 69 10620 13814 297C 35F6 5310 6907 14BE 1AFB 8141 24101 1FCD 5E25 70 15978 16854 3E6A 41D6 7989 8427 1F35 20EB 10408 12762 28A8 31DA 71 27966 795 6D3E 031B 13983 20401 369F 4FB1 18826 19997 498A 4E1D 72 12479 9774 30BF 262E 18831 4887 498F 1317 22705 22971 58B1 59BB 73 1536 24291 0600 5EE3 768 24909 0300 614D 3879 12560 0F27 3110 74 3199 3172 0C7F 0C64 22511 1586 57EF 0632 21359 31213 536F 79ED 75 4549 2229 11C5 08B5 22834 19046 5932 4A66 30853 18780 7885 495C 76 17888 21283 45E0 5323 8944 26541 22F0 67AD 18078 16353 469E 3FE1 77 13117 16905 333D 4209 18510 28472 484E 6F38 15910 12055 3E26 2F17 78 7506 7062 1D52 1B96 3753 3531 0EA9 0DCB 20989 30396 51FD 76BC 79 27626 7532 6BEA 1D6C 13813 3766 35F5 0EB6 28810 24388 708A 5F44 80 31109 25575 7985 63E7 27922 32719 6D12 7FCF 30759 1555 7827 0613 81 29755 14244 743B 37A4 27597 7122 6BCD 1BD2 18899 13316 49D3 3404 82 26711 28053 6857 6D95 26107 30966 65FB 78F6 7739 31073 1E3B 7961 83 20397 30408 4FAD 76C8 30214 15204 7606 3B64 6279 6187 1887 182B 84 18608 5094 48B0 13E6 9304 2547 2458 09F3 9968 21644 26F0 548C 85 7391 16222 1CDF 3F5E 24511 8111 5FBF 1FAF 8571 9289 217B 2449 86 23168 7159 5A80 1BF7 11584 17351 2D40 43C7 4143 4624 102F 1210 87 23466 174 5BAA 00AE 11733 87 2DD5 0057 19637 467 4CB5 01D3 88 15932 25530 3E3C 63BA 7966 12765 1F1E 31DD 11867 18133 2E5B 46D5 89 25798 2320 64C6 0910 12899 1160 3263 0488 7374 1532 1CCE 05FC 90 28134 23113 6DE6 5A49 14067 25368 36F3 6318 10423 1457 28B7 05B1 91 28024 23985 6D78 5DB1 14012 24804 36BC 60E4 9984 9197 2700 23ED 92 6335 2604 18BF 0A2C 23951 1302 5D8F 0516 7445 13451 1D15 348B 93 21508 1826 5404 0722 10754 913 2A02 0391 4133 25785 1025 64B9 94 26338 30853 66E2 7885 13169 29310 3371 727E 22646 4087 5876 0FF7 95 17186 15699 4322 3D53 8593 20629 2191 5095 15466 31190 3C6A 79D6 96 22462 2589 57BE 0A1D 11231 19250 2BDF 4B32 2164 8383 0874 20BF 97 3908 25000 0F44 61A8 1954 12500 07A2 30D4 16380 12995 3FFC 32C3 98 25390 18163 632E 46F3 12695 27973 3197 6D45 15008 27438 3AA0 6B2E 99 27891 12555 6CF3 310B 26537 22201 67A9 56B9 31755 9297 7C0B 2451 100 9620 8670 2594 21DE 4810 4335 12CA 10EF 31636 1676 7B94 068C

B-4

. . . continued on next page

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

Mar 2003

PN Offset Programming Information68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

101 6491 1290 195B 050A 23933 645 5D7D 0285 25414 12596 6346 3134 102 16876 4407 41EC 1137 8438 18087 20F6 46A7 7102 19975 1BBE 4E07 103 17034 1163 428A 048B 8517 19577 2145 4C79 20516 20026 5024 4E3A 104 32405 12215 7E95 2FB7 28314 23015 6E9A 59E7 19495 8958 4C27 22FE 105 27417 7253 6B19 1C55 25692 16406 645C 4016 17182 19143 431E 4AC7 106 8382 8978 20BE 2312 4191 4489 105F 1189 11572 17142 2D34 42F6 107 5624 25547 15F8 63CB 2812 32729 0AFC 7FD9 25570 19670 63E2 4CD6 108 1424 3130 0590 0C3A 712 1565 02C8 061D 6322 30191 18B2 75EF 109 13034 31406 32EA 7AAE 6517 15703 1975 3D57 8009 5822 1F49 16BE 110 15682 6222 3D42 184E 7841 3111 1EA1 0C27 26708 22076 6854 563C 111 27101 20340 69DD 4F74 25918 10170 653E 27BA 6237 606 185D 025E 112 8521 25094 2149 6206 16756 12547 4174 3103 32520 9741 7F08 260D 113 30232 23380 7618 5B54 15116 11690 3B0C 2DAA 31627 9116 7B8B 239C 114 6429 10926 191D 2AAE 23902 5463 5D5E 1557 3532 12705 0DCC 31A1 115 27116 22821 69EC 5925 13558 25262 34F6 62AE 24090 17502 5E1A 445E 116 4238 31634 108E 7B92 2119 15817 0847 3DC9 20262 18952 4F26 4A08 117 5128 4403 1408 1133 2564 18085 0A04 46A5 18238 15502 473E 3C8E 118 14846 689 39FE 02B1 7423 20324 1CFF 4F64 2033 17819 07F1 459B 119 13024 27045 32E0 69A5 6512 31470 1970 7AEE 25566 4370 63DE 1112 120 10625 27557 2981 6BA5 17680 31726 4510 7BEE 25144 31955 6238 7CD3 121 31724 16307 7BEC 3FB3 15862 20965 3DF6 51E5 29679 30569 73EF 7769 122 13811 22338 35F3 5742 19241 11169 4B29 2BA1 5064 7350 13C8 1CB6 123 24915 27550 6153 6B9E 24953 13775 6179 35CF 27623 26356 6BE7 66F4 124 1213 22096 04BD 5650 21390 11048 538E 2B28 13000 32189 32C8 7DBD 125 2290 23136 08F2 5A60 1145 11568 0479 2D30 31373 1601 7A8D 0641 126 31551 12199 7B3F 2FA7 27727 23023 6C4F 59EF 13096 19537 3328 4C51 127 12088 1213 2F38 04BD 6044 19554 179C 4C62 26395 25667 671B 6443 128 7722 936 1E2A 03A8 3861 468 0F15 01D4 15487 4415 3C7F 113F 129 27312 6272 6AB0 1880 13656 3136 3558 0C40 29245 2303 723D 08FF 130 23130 32446 5A5A 7EBE 11565 16223 2D2D 3F5F 26729 16362 6869 3FEA 131 594 13555 0252 34F3 297 21573 0129 5445 12568 28620 3118 6FCC 132 25804 8789 64CC 2255 12902 24342 3266 5F16 24665 6736 6059 1A50 133 31013 24821 7925 60F5 27970 32326 6D42 7E46 8923 2777 22DB 0AD9 134 32585 21068 7F49 524C 28276 10534 6E74 2926 19634 24331 4CB2 5F0B 135 3077 31891 0C05 7C93 22482 28789 57D2 7075 29141 9042 71D5 2352 136 17231 5321 434F 14C9 28791 17496 7077 4458 73 107 0049 006B 137 31554 551 7B42 0227 15777 20271 3DA1 4F2F 26482 4779 6772 12AB 138 8764 12115 223C 2F53 4382 22933 111E 5995 6397 13065 18FD 3309 139 15375 4902 3C0F 1326 20439 2451 4FD7 0993 29818 30421 747A 76D5 140 13428 1991 3474 07C7 6714 19935 1A3A 4DDF 8153 20210 1FD9 4EF2 141 17658 14404 44FA 3844 8829 7202 227D 1C22 302 5651 012E 1613 142 13475 17982 34A3 463E 19329 8991 4B81 231F 28136 31017 6DE8 7929 143 22095 19566 564F 4C6E 31479 9783 7AF7 2637 29125 30719 71C5 77FF 144 24805 2970 60E5 0B9A 24994 1485 61A2 05CD 8625 23104 21B1 5A40 145 4307 23055 10D3 5A0F 22969 25403 59B9 633B 26671 7799 682F 1E77 146 23292 15158 5AFC 3B36 11646 7579 2D7E 1D9B 6424 17865 1918 45C9 147 1377 29094 0561 71A6 21344 14547 5360 38D3 12893 26951 325D 6947 148 28654 653 6FEE 028D 14327 20346 37F7 4F7A 18502 25073 4846 61F1 149 6350 19155 18CE 4AD3 3175 27477 0C67 6B55 7765 32381 1E55 7E7D 150 16770 23588 4182 5C24 8385 11794 20C1 2E12 25483 16581 638B 40C5

Mar 2003

. . . continued on next page

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

B-5

PN Offset Programming Information

68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

151 14726 10878 3986 2A7E 7363 5439 1CC3 153F 15408 32087 3C30 7D57 152 25685 31060 6455 7954 25594 15530 63FA 3CAA 6414 97 190E 0061 153 21356 30875 536C 789B 10678 29297 29B6 7271 8164 7618 1FE4 1DC2 154 12149 11496 2F75 2CE8 18026 5748 466A 1674 10347 93 286B 005D 155 28966 24545 7126 5FE1 14483 25036 3893 61CC 29369 16052 72B9 3EB4 156 22898 9586 5972 2572 11449 4793 2CB9 12B9 10389 14300 2895 37DC 157 1713 20984 06B1 51F8 21128 10492 5288 28FC 24783 11129 60CF 2B79 158 30010 30389 753A 76B5 15005 30054 3A9D 7566 18400 6602 47E0 19CA 159 2365 7298 093D 1C82 21838 3649 554E 0E41 22135 14460 5677 387C 160 27179 18934 6A2B 49F6 25797 9467 64C5 24FB 4625 25458 1211 6372 161 29740 23137 742C 5A61 14870 25356 3A16 630C 22346 15869 574A 3DFD 162 5665 24597 1621 6015 23232 32310 5AC0 7E36 2545 27047 09F1 69A7 163 23671 23301 5C77 5B05 32747 25534 7FEB 63BE 7786 26808 1E6A 68B8 164 1680 7764 0690 1E54 840 3882 0348 0F2A 20209 7354 4EF1 1CBA 165 25861 14518 6505 38B6 25426 7259 6352 1C5B 26414 27834 672E 6CBA 166 25712 21634 6470 5482 12856 10817 3238 2A41 1478 11250 05C6 2BF2 167 19245 11546 4B2D 2D1A 29766 5773 7446 168D 15122 552 3B12 0228 168 26887 26454 6907 6756 25939 13227 6553 33AB 24603 27058 601B 69B2 169 30897 15938 78B1 3E42 28040 7969 6D88 1F21 677 14808 02A5 39D8 170 11496 9050 2CE8 235A 5748 4525 1674 11AD 13705 9642 3589 25AA 171 1278 3103 04FE 0C1F 639 18483 027F 4833 13273 32253 33D9 7DFD 172 31555 758 7B43 02F6 27761 379 6C71 017B 14879 26081 3A1F 65E1 173 29171 16528 71F3 4090 26921 8264 6929 2048 6643 21184 19F3 52C0 174 20472 20375 4FF8 4F97 10236 27127 27FC 69F7 23138 11748 5A62 2DE4 175 5816 10208 16B8 27E0 2908 5104 0B5C 13F0 28838 32676 70A6 7FA4 176 30270 17698 763E 4522 15135 8849 3B1F 2291 9045 2425 2355 0979 177 22188 8405 56AC 20D5 11094 24150 2B56 5E56 10792 19455 2A28 4BFF 178 6182 28634 1826 6FDA 3091 14317 0C13 37ED 25666 19889 6442 4DB1 179 32333 1951 7E4D 079F 28406 19955 6EF6 4DF3 11546 18177 2D1A 4701 180 14046 20344 36DE 4F78 7023 10172 1B6F 27BC 15535 2492 3CAF 09BC 181 15873 26696 3E01 6848 20176 13348 4ED0 3424 16134 15086 3F06 3AEE 182 19843 3355 4D83 0D1B 30481 18609 7711 48B1 8360 30632 20A8 77A8 183 29367 11975 72B7 2EC7 26763 22879 688B 595F 14401 27549 3841 6B9D 184 13352 31942 3428 7CC6 6676 15971 1A14 3E63 26045 6911 65BD 1AFF 185 22977 9737 59C1 2609 32048 23864 7D30 5D38 24070 9937 5E06 26D1 186 31691 9638 7BCB 25A6 27701 4819 6C35 12D3 30300 2467 765C 09A3 187 10637 30643 298D 77B3 17686 30181 4516 75E5 13602 25831 3522 64E7 188 25454 13230 636E 33AE 12727 6615 31B7 19D7 32679 32236 7FA7 7DEC 189 18610 22185 48B2 56A9 9305 25960 2459 6568 16267 12987 3F8B 32BB 190 6368 2055 18E0 0807 3184 19007 0C70 4A3F 9063 11714 2367 2DC2 191 7887 8767 1ECF 223F 24247 24355 5EB7 5F23 19487 19283 4C1F 4B53 192 7730 15852 1E32 3DEC 3865 7926 0F19 1EF6 12778 11542 31EA 2D16 193 23476 16125 5BB4 3EFD 11738 20802 2DDA 5142 27309 27928 6AAD 6D18 194 889 6074 0379 17BA 20588 3037 506C 0BDD 12527 26637 30EF 680D 195 21141 31245 5295 7A0D 30874 29498 789A 733A 953 10035 03B9 2733 196 20520 15880 5028 3E08 10260 7940 2814 1F04 15958 10748 3E56 29FC 197 21669 20371 54A5 4F93 31618 27125 7B82 69F5 6068 24429 17B4 5F6D 198 15967 8666 3E5F 21DA 20223 4333 4EFF 10ED 23577 29701 5C19 7405 199 21639 816 5487 0330 31635 408 7B93 0198 32156 14997 7D9C 3A95 200 31120 22309 7990 5725 15560 26030 3CC8 65AE 32709 32235 7FC5 7DEB

B-6

. . . continued on next page

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

Mar 2003

PN Offset Programming Information68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

201 3698 29563 0E72 737B 1849 30593 0739 7781 23557 30766 5C05 782E 202 16322 13078 3FC2 3316 8161 6539 1FE1 198B 17638 5985 44E6 1761 203 17429 10460 4415 28DC 29658 5230 73DA 146E 3545 6823 0DD9 1AA7 204 21730 17590 54E2 44B6 10865 8795 2A71 225B 9299 20973 2453 51ED 205 17808 20277 4590 4F35 8904 27046 22C8 69A6 6323 10197 18B3 27D5 206 30068 19988 7574 4E14 15034 9994 3ABA 270A 19590 9618 4C86 2592 207 12737 6781 31C1 1A7D 18736 17154 4930 4302 7075 22705 1BA3 58B1 208 28241 32501 6E51 7EF5 26360 28998 66F8 7146 14993 5234 3A91 1472 209 20371 6024 4F93 1788 30233 3012 7619 0BC4 19916 12541 4DCC 30FD 210 13829 20520 3605 5028 19154 10260 4AD2 2814 6532 8019 1984 1F53 211 13366 31951 3436 7CCF 6683 28763 1A1B 705B 17317 22568 43A5 5828 212 25732 26063 6484 65CF 12866 31963 3242 7CDB 16562 5221 40B2 1465 213 19864 27203 4D98 6A43 9932 31517 26CC 7B1D 26923 25216 692B 6280 214 5187 6614 1443 19D6 23537 3307 5BF1 0CEB 9155 1354 23C3 054A 215 23219 10970 5AB3 2ADA 31881 5485 7C89 156D 20243 29335 4F13 7297 216 28242 5511 6E52 1587 14121 17663 3729 44FF 32391 6682 7E87 1A1A 217 6243 17119 1863 42DF 24033 28499 5DE1 6F53 20190 26128 4EDE 6610 218 445 16064 01BD 3EC0 20750 8032 510E 1F60 27564 29390 6BAC 72CE 219 21346 31614 5362 7B7E 10673 15807 29B1 3DBF 20869 8852 5185 2294 220 13256 4660 33C8 1234 6628 2330 19E4 091A 9791 6110 263F 17DE 221 18472 13881 4828 3639 9236 21792 2414 5520 714 11847 02CA 2E47 222 25945 16819 6559 41B3 25468 28389 637C 6EE5 7498 10239 1D4A 27FF 223 31051 6371 794B 18E3 28021 16973 6D75 424D 23278 6955 5AEE 1B2B 224 1093 24673 0445 6061 21490 32268 53F2 7E0C 8358 10897 20A6 2A91 225 5829 6055 16C5 17A7 23218 17903 5AB2 45EF 9468 14076 24FC 36FC 226 31546 10009 7B3A 2719 15773 23984 3D9D 5DB0 23731 12450 5CB3 30A2 227 29833 5957 7489 1745 27540 17822 6B94 459E 25133 8954 622D 22FA 228 18146 11597 46E2 2D4D 9073 22682 2371 589A 2470 19709 09A6 4CFD 229 24813 22155 60ED 568B 24998 25977 61A6 6579 17501 1252 445D 04E4 230 47 15050 002F 3ACA 20935 7525 51C7 1D65 24671 15142 605F 3B26 231 3202 16450 0C82 4042 1601 8225 0641 2021 11930 26958 2E9A 694E 232 21571 27899 5443 6CFB 31729 30785 7BF1 7841 9154 8759 23C2 2237 233 7469 2016 1D2D 07E0 24390 1008 5F46 03F0 7388 12696 1CDC 3198 234 25297 17153 62D1 4301 24760 28604 60B8 6FBC 3440 11936 0D70 2EA0 235 8175 15849 1FEF 3DE9 24103 20680 5E27 50C8 27666 25635 6C12 6423 236 28519 30581 6F67 7775 26211 30086 6663 7586 22888 17231 5968 434F 237 4991 3600 137F 0E10 22639 1800 586F 0708 13194 22298 338A 571A 238 7907 4097 1EE3 1001 24225 17980 5EA1 463C 26710 7330 6856 1CA2 239 17728 671 4540 029F 8864 20339 22A0 4F73 7266 30758 1C62 7826 240 14415 20774 384F 5126 19959 10387 4DF7 2893 15175 6933 3B47 1B15 241 30976 24471 7900 5F97 15488 25079 3C80 61F7 15891 2810 3E13 0AFA 242 26376 27341 6708 6ACD 13188 31578 3384 7B5A 26692 8820 6844 2274 243 19063 19388 4A77 4BBC 29931 9694 74EB 25DE 14757 7831 39A5 1E97 244 19160 25278 4AD8 62BE 9580 12639 256C 315F 28757 19584 7055 4C80 245 3800 9505 0ED8 2521 1900 23724 076C 5CAC 31342 2944 7A6E 0B80 246 8307 26143 2073 661F 16873 32051 41E9 7D33 19435 19854 4BEB 4D8E 247 12918 13359 3276 342F 6459 21547 193B 542B 2437 10456 0985 28D8 248 19642 2154 4CBA 086A 9821 1077 265D 0435 20573 17036 505D 428C 249 24873 13747 6129 35B3 24900 21733 6144 54E5 18781 2343 495D 0927 250 22071 27646 5637 6BFE 31435 13823 7ACB 35FF 18948 14820 4A04 39E4

Mar 2003

. . . continued on next page

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

B-7

PN Offset Programming Information

68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

251 13904 1056 3650 0420 6952 528 1B28 0210 23393 1756 5B61 06DC 252 27198 1413 6A3E 0585 13599 19710 351F 4CFE 5619 19068 15F3 4A7C 253 3685 3311 0E65 0CEF 22242 18507 56E2 484B 17052 28716 429C 702C 254 16820 4951 41B4 1357 8410 18327 20DA 4797 21292 31958 532C 7CD6 255 22479 749 57CF 02ED 31287 20298 7A37 4F4A 2868 16097 0B34 3EE1 256 6850 6307 1AC2 18A3 3425 17005 0D61 426D 19538 1308 4C52 051C 257 15434 961 3C4A 03C1 7717 20444 1E25 4FDC 24294 3320 5EE6 0CF8 258 19332 2358 4B84 0936 9666 1179 25C2 049B 22895 16682 596F 412A 259 8518 28350 2146 6EBE 4259 14175 10A3 375F 27652 6388 6C04 18F4 260 14698 31198 396A 79DE 7349 15599 1CB5 3CEF 29905 12828 74D1 321C 261 21476 11467 53E4 2CCB 10738 22617 29F2 5859 21415 3518 53A7 0DBE 262 30475 8862 770B 229E 27221 4431 6A55 114F 1210 3494 04BA 0DA6 263 23984 6327 5DB0 18B7 11992 16999 2ED8 4267 22396 6458 577C 193A 264 1912 7443 0778 1D13 956 16565 03BC 40B5 26552 10717 67B8 29DD 265 26735 28574 686F 6F9E 26087 14287 65E7 37CF 24829 8463 60FD 210F 266 15705 25093 3D59 6205 20348 32574 4F7C 7F3E 8663 27337 21D7 6AC9 267 3881 6139 0F29 17FB 22084 17857 5644 45C1 991 19846 03DF 4D86 268 20434 22047 4FD2 561F 10217 25907 27E9 6533 21926 9388 55A6 24AC 269 16779 32545 418B 7F21 28949 29100 7115 71AC 23306 21201 5B0A 52D1 270 31413 7112 7AB5 1BC8 27786 3556 6C8A 0DE4 13646 31422 354E 7ABE 271 16860 28535 41DC 6F77 8430 31111 20EE 7987 148 166 0094 00A6 272 8322 10378 2082 288A 4161 5189 1041 1445 24836 28622 6104 6FCE 273 28530 15065 6F72 3AD9 14265 21328 37B9 5350 24202 6477 5E8A 194D 274 26934 5125 6936 1405 13467 17470 349B 443E 9820 10704 265C 29D0 275 18806 12528 4976 30F0 9403 6264 24BB 1878 12939 25843 328B 64F3 276 20216 23215 4EF8 5AAF 10108 25451 277C 636B 2364 25406 093C 633E 277 9245 20959 241D 51DF 17374 26323 43DE 66D3 14820 21523 39E4 5413 278 8271 3568 204F 0DF0 16887 1784 41F7 06F8 2011 8569 07DB 2179 279 18684 26453 48FC 6755 9342 32150 247E 7D96 13549 9590 34ED 2576 280 8220 29421 201C 72ED 4110 30538 100E 774A 28339 22466 6EB3 57C2 281 6837 24555 1AB5 5FEB 23690 25033 5C8A 61C9 25759 12455 649F 30A7 282 9613 10779 258D 2A1B 17174 23345 4316 5B31 11116 27506 2B6C 6B72 283 31632 25260 7B90 62AC 15816 12630 3DC8 3156 31448 21847 7AD8 5557 284 27448 16084 6B38 3ED4 13724 8042 359C 1F6A 27936 28392 6D20 6EE8 285 12417 26028 3081 65AC 18832 13014 4990 32D6 3578 1969 0DFA 07B1 286 30901 29852 78B5 749C 28042 14926 6D8A 3A4E 12371 30715 3053 77FB 287 9366 14978 2496 3A82 4683 7489 124B 1D41 12721 23674 31B1 5C7A 288 12225 12182 2FC1 2F96 17968 6091 4630 17CB 10264 22629 2818 5865 289 21458 25143 53D2 6237 10729 32551 29E9 7F27 25344 12857 6300 3239 290 6466 15838 1942 3DDE 3233 7919 0CA1 1EEF 13246 30182 33BE 75E6 291 8999 5336 2327 14D8 16451 2668 4043 0A6C 544 21880 0220 5578 292 26718 21885 685E 557D 13359 25730 342F 6482 9914 6617 26BA 19D9 293 3230 20561 0C9E 5051 1615 26132 064F 6614 4601 27707 11F9 6C3B 294 27961 30097 6D39 7591 26444 29940 674C 74F4 16234 16249 3F6A 3F79 295 28465 21877 6F31 5575 26184 25734 6648 6486 24475 24754 5F9B 60B2 296 6791 23589 1A87 5C25 23699 24622 5C93 602E 26318 31609 66CE 7B79 297 17338 26060 43BA 65CC 8669 13030 21DD 32E6 6224 22689 1850 58A1 298 11832 9964 2E38 26EC 5916 4982 171C 1376 13381 3226 3445 0C9A 299 11407 25959 2C8F 6567 18327 31887 4797 7C8F 30013 4167 753D 1047 300 15553 3294 3CC1 0CDE 20400 1647 4FB0 066F 22195 25624 56B3 6418

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1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

Mar 2003

PN Offset Programming Information68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

301 17418 30173 440A 75DD 8709 29906 2205 74D2 30380 10924 76AC 2AAC 302 14952 15515 3A68 3C9B 7476 20593 1D34 5071 15337 23096 3BE9 5A38 303 52 5371 0034 14FB 26 17473 001A 4441 10716 22683 29DC 589B 304 27254 10242 6A76 2802 13627 5121 353B 1401 13592 10955 3518 2ACB 305 15064 28052 3AD8 6D94 7532 14026 1D6C 36CA 2412 17117 096C 42DD 306 10942 14714 2ABE 397A 5471 7357 155F 1CBD 15453 15837 3C5D 3DDD 307 377 19550 0179 4C5E 20844 9775 516C 262F 13810 22647 35F2 5877 308 14303 8866 37DF 22A2 19007 4433 4A3F 1151 12956 10700 329C 29CC 309 24427 15297 5F6B 3BC1 32357 21468 7E65 53DC 30538 30293 774A 7655 310 26629 10898 6805 2A92 26066 5449 65D2 1549 10814 5579 2A3E 15CB 311 20011 31315 4E2B 7A53 30405 29461 76C5 7315 18939 11057 49FB 2B31 312 16086 19475 3ED6 4C13 8043 26677 1F6B 6835 19767 30238 4D37 761E 313 24374 1278 5F36 04FE 12187 639 2F9B 027F 20547 14000 5043 36B0 314 9969 11431 26F1 2CA7 17064 22639 42A8 586F 29720 22860 7418 594C 315 29364 31392 72B4 7AA0 14682 15696 395A 3D50 31831 27172 7C57 6A24 316 25560 4381 63D8 111D 12780 18098 31EC 46B2 26287 307 66AF 0133 317 28281 14898 6E79 3A32 26348 7449 66EC 1D19 11310 20380 2C2E 4F9C 318 7327 23959 1C9F 5D97 24479 24823 5F9F 60F7 25724 26427 647C 673B 319 32449 16091 7EC1 3EDB 28336 20817 6EB0 5151 21423 10702 53AF 29CE 320 26334 9037 66DE 234D 13167 24474 336F 5F9A 5190 30024 1446 7548 321 14760 24162 39A8 5E62 7380 12081 1CD4 2F31 258 14018 0102 36C2 322 15128 6383 3B18 18EF 7564 16971 1D8C 424B 13978 4297 369A 10C9 323 29912 27183 74D8 6A2F 14956 31531 3A6C 7B2B 4670 13938 123E 3672 324 4244 16872 1094 41E8 2122 8436 084A 20F4 23496 25288 5BC8 62C8 325 8499 9072 2133 2370 16713 4536 4149 11B8 23986 27294 5DB2 6A9E 326 9362 12966 2492 32A6 4681 6483 1249 1953 839 31835 0347 7C5B 327 10175 28886 27BF 70D6 16911 14443 420F 386B 11296 8228 2C20 2024 328 30957 25118 78ED 621E 28070 12559 6DA6 310F 30913 12745 78C1 31C9 329 12755 20424 31D3 4FC8 18745 10212 4939 27E4 27297 6746 6AA1 1A5A 330 19350 6729 4B96 1A49 9675 17176 25CB 4318 10349 1456 286D 05B0 331 1153 20983 0481 51F7 21392 26311 5390 66C7 32504 27743 7EF8 6C5F 332 29304 12372 7278 3054 14652 6186 393C 182A 18405 27443 47E5 6B33 333 6041 13948 1799 367C 23068 6974 5A1C 1B3E 3526 31045 0DC6 7945 334 21668 27547 54A4 6B9B 10834 31729 2A52 7BF1 19161 12225 4AD9 2FC1 335 28048 8152 6D90 1FD8 14024 4076 36C8 0FEC 23831 21482 5D17 53EA 336 10096 17354 2770 43CA 5048 8677 13B8 21E5 21380 14678 5384 3956 337 23388 17835 5B5C 45AB 11694 27881 2DAE 6CE9 4282 30656 10BA 77C0 338 15542 14378 3CB6 382A 7771 7189 1E5B 1C15 32382 13721 7E7E 3599 339 24013 7453 5DCD 1D1D 32566 16562 7F36 40B2 806 21831 0326 5547 340 2684 26317 0A7C 66CD 1342 32090 053E 7D5A 6238 30208 185E 7600 341 19018 5955 4A4A 1743 9509 17821 2525 459D 10488 9995 28F8 270B 342 25501 10346 639D 286A 24606 5173 601E 1435 19507 3248 4C33 0CB0 343 4489 13200 1189 3390 22804 6600 5914 19C8 27288 12030 6A98 2EFE 344 31011 30402 7923 76C2 27969 15201 6D41 3B61 2390 5688 0956 1638 345 29448 7311 7308 1C8F 14724 16507 3984 407B 19094 2082 4A96 0822 346 25461 3082 6375 0C0A 24682 1541 606A 0605 13860 23143 3624 5A67 347 11846 21398 2E46 5396 5923 10699 1723 29CB 9225 25906 2409 6532 348 30331 31104 767B 7980 27373 15552 6AED 3CC0 2505 15902 09C9 3E1E 349 10588 24272 295C 5ED0 5294 12136 14AE 2F68 27806 21084 6C9E 525C 350 32154 27123 7D9A 69F3 16077 31429 3ECD 7AC5 2408 25723 0968 647B

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1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

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B-9

PN Offset Programming Information

68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

351 29572 5578 7384 15CA 14786 2789 39C2 0AE5 13347 13427 3423 3473 352 13173 25731 3375 6483 18538 31869 486A 7C7D 7885 31084 1ECD 796C 353 10735 10662 29EF 29A6 17703 5331 4527 14D3 6669 24023 1A0D 5DD7 354 224 11084 00E0 2B4C 112 5542 0070 15A6 8187 23931 1FFB 5D7B 355 12083 31098 2F33 797A 17993 15549 4649 3CBD 18145 15836 46E1 3DDC 356 22822 16408 5926 4018 11411 8204 2C93 200C 14109 6085 371D 17C5 357 2934 6362 0B76 18DA 1467 3181 05BB 0C6D 14231 30324 3797 7674 358 27692 2719 6C2C 0A9F 13846 19315 3616 4B73 27606 27561 6BD6 6BA9 359 10205 14732 27DD 398C 16958 7366 423E 1CC6 783 13821 030F 35FD 360 7011 22744 1B63 58D8 23649 11372 5C61 2C6C 6301 269 189D 010D 361 22098 1476 5652 05C4 11049 738 2B29 02E2 5067 28663 13CB 6FF7 362 2640 8445 0A50 20FD 1320 24130 0528 5E42 15383 29619 3C17 73B3 363 4408 21118 1138 527E 2204 10559 089C 293F 1392 2043 0570 07FB 364 102 22198 0066 56B6 51 11099 0033 2B5B 7641 6962 1DD9 1B32 365 27632 22030 6BF0 560E 13816 11015 35F8 2B07 25700 29119 6464 71BF 366 19646 10363 4CBE 287B 9823 23041 265F 5A01 25259 22947 62AB 59A3 367 26967 25802 6957 64CA 25979 12901 657B 3265 19813 9612 4D65 258C 368 32008 2496 7D08 09C0 16004 1248 3E84 04E0 20933 18698 51C5 490A 369 7873 31288 1EC1 7A38 24240 15644 5EB0 3D1C 638 16782 027E 418E 370 655 24248 028F 5EB8 20631 12124 5097 2F5C 16318 29735 3FBE 7427 371 25274 14327 62BA 37F7 12637 21959 315D 55C7 6878 2136 1ADE 0858 372 16210 23154 3F52 5A72 8105 11577 1FA9 2D39 1328 8086 0530 1F96 373 11631 13394 2D6F 3452 18279 6697 4767 1A29 14744 10553 3998 2939 374 8535 1806 2157 070E 16763 903 417B 0387 22800 11900 5910 2E7C 375 19293 17179 4B5D 431B 29822 28593 747E 6FB1 25919 19996 653F 4E1C 376 12110 10856 2F4E 2A68 6055 5428 17A7 1534 4795 5641 12BB 1609 377 21538 25755 5422 649B 10769 31857 2A11 7C71 18683 28328 48FB 6EA8 378 10579 15674 2953 3D3A 17785 7837 4579 1E9D 32658 25617 7F92 6411 379 13032 7083 32E8 1BAB 6516 17385 1974 43E9 1586 26986 0632 696A 380 14717 29096 397D 71A8 19822 14548 4D6E 38D4 27208 5597 6A48 15DD 381 11666 3038 2D92 0BDE 5833 1519 16C9 05EF 17517 14078 446D 36FE 382 25809 16277 64D1 3F95 25528 20982 63B8 51F6 599 13247 0257 33BF 383 5008 25525 1390 63B5 2504 32742 09C8 7FE6 16253 499 3F7D 01F3 384 32418 20465 7EA2 4FF1 16209 27076 3F51 69C4 8685 30469 21ED 7705 385 22175 28855 569F 70B7 31391 30311 7A9F 7667 29972 17544 7514 4488 386 11742 32732 2DDE 7FDC 5871 16366 16EF 3FEE 22128 28510 5670 6F5E 387 22546 20373 5812 4F95 11273 27126 2C09 69F6 19871 23196 4D9F 5A9C 388 21413 9469 53A5 24FD 30722 23618 7802 5C42 19405 13384 4BCD 3448 389 133 26155 0085 662B 20882 32041 5192 7D29 17972 4239 4634 108F 390 4915 6957 1333 1B2D 22601 17322 5849 43AA 8599 20725 2197 50F5 391 8736 12214 2220 2FB6 4368 6107 1110 17DB 10142 6466 279E 1942 392 1397 21479 0575 53E7 21354 26575 536A 67CF 26834 28465 68D2 6F31 393 18024 31914 4668 7CAA 9012 15957 2334 3E55 23710 19981 5C9E 4E0D 394 15532 32311 3CAC 7E37 7766 28967 1E56 7127 27280 16723 6A90 4153 395 26870 11276 68F6 2C0C 13435 5638 347B 1606 6570 4522 19AA 11AA 396 5904 20626 1710 5092 2952 10313 0B88 2849 7400 678 1CE8 02A6 397 24341 423 5F15 01A7 32346 20207 7E5A 4EEF 26374 15320 6706 3BD8 398 13041 2679 32F1 0A77 18600 19207 48A8 4B07 22218 29116 56CA 71BC 399 23478 15537 5BB6 3CB1 11739 20580 2DDB 5064 29654 5388 73D6 150C 400 1862 10818 0746 2A42 931 5409 03A3 1521 13043 22845 32F3 593D

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1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

Mar 2003

PN Offset Programming Information68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

401 5850 23074 16DA 5A22 2925 11537 0B6D 2D11 24457 28430 5F89 6F0E 402 5552 20250 15B0 4F1A 2776 10125 0AD8 278D 17161 8660 4309 21D4 403 12589 14629 312D 3925 18758 21166 4946 52AE 21314 2659 5342 0A63 404 23008 29175 59E0 71F7 11504 30407 2CF0 76C7 28728 8803 7038 2263 405 27636 13943 6BF4 3677 13818 21767 35FA 5507 22162 19690 5692 4CEA 406 17600 11072 44C0 2B40 8800 5536 2260 15A0 26259 22169 6693 5699 407 17000 29492 4268 7334 8500 14746 2134 399A 22180 8511 56A4 213F 408 21913 5719 5599 1657 31516 17687 7B1C 4517 2266 17393 08DA 43F1 409 30320 7347 7670 1CB3 15160 16485 3B38 4065 10291 11336 2833 2C48 410 28240 12156 6E50 2F7C 14120 6078 3728 17BE 26620 13576 67FC 3508 411 7260 25623 1C5C 6417 3630 31799 0E2E 7C37 19650 22820 4CC2 5924 412 17906 27725 45F2 6C4D 8953 30746 22F9 781A 14236 13344 379C 3420 413 5882 28870 16FA 70C6 2941 14435 0B7D 3863 11482 20107 2CDA 4E8B 414 22080 31478 5640 7AF6 11040 15739 2B20 3D7B 25289 8013 62C9 1F4D 415 12183 28530 2F97 6F72 17947 14265 461B 37B9 12011 18835 2EEB 4993 416 23082 24834 5A2A 6102 11541 12417 2D15 3081 13892 16793 3644 4199 417 17435 9075 441B 2373 29661 24453 73DD 5F85 17336 9818 43B8 265A 418 18527 32265 485F 7E09 30207 28984 75FF 7138 10759 4673 2A07 1241 419 31902 3175 7C9E 0C67 15951 18447 3E4F 480F 26816 13609 68C0 3529 420 18783 17434 495F 441A 30079 8717 757F 220D 31065 10054 7959 2746 421 20027 12178 4E3B 2F92 30413 6089 76CD 17C9 8578 10988 2182 2AEC 422 7982 25613 1F2E 640D 3991 31802 0F97 7C3A 24023 14744 5DD7 3998 423 20587 31692 506B 7BCC 31205 15846 79E5 3DE6 16199 17930 3F47 460A 424 10004 25384 2714 6328 5002 12692 138A 3194 22310 25452 5726 636C 425 13459 18908 3493 49DC 19353 9454 4B99 24EE 30402 11334 76C2 2C46 426 13383 25816 3447 64D8 19443 12908 4BF3 326C 16613 15451 40E5 3C5B 427 28930 4661 7102 1235 14465 18214 3881 4726 13084 11362 331C 2C62 428 4860 31115 12FC 798B 2430 29433 097E 72F9 3437 2993 0D6D 0BB1 429 13108 7691 3334 1E0B 6554 16697 199A 4139 1703 11012 06A7 2B04 430 24161 1311 5E61 051F 32480 19635 7EE0 4CB3 22659 5806 5883 16AE 431 20067 16471 4E63 4057 30433 28183 76E1 6E17 26896 20180 6910 4ED4 432 2667 15771 0A6B 3D9B 21733 20721 54E5 50F1 1735 8932 06C7 22E4 433 13372 16112 343C 3EF0 6686 8056 1A1E 1F78 16178 23878 3F32 5D46 434 28743 21062 7047 5246 27123 10531 69F3 2923 19166 20760 4ADE 5118 435 24489 29690 5FA9 73FA 32260 14845 7E04 39FD 665 32764 0299 7FFC 436 249 10141 00F9 279D 20908 24050 51AC 5DF2 20227 32325 4F03 7E45 437 19960 19014 4DF8 4A46 9980 9507 26FC 2523 24447 25993 5F7F 6589 438 29682 22141 73F2 567D 14841 25858 39F9 6502 16771 3268 4183 0CC4 439 31101 11852 797D 2E4C 28014 5926 6D6E 1726 27209 25180 6A49 625C 440 27148 26404 6A0C 6724 13574 13202 3506 3392 6050 12149 17A2 2F75 441 26706 30663 6852 77C7 13353 30175 3429 75DF 29088 10193 71A0 27D1 442 5148 32524 141C 7F0C 2574 16262 0A0E 3F86 7601 9128 1DB1 23A8 443 4216 28644 1078 6FE4 2108 14322 083C 37F2 4905 7843 1329 1EA3 444 5762 10228 1682 27F4 2881 5114 0B41 13FA 5915 25474 171B 6382 445 245 23536 00F5 5BF0 20906 11768 51AA 2DF8 6169 11356 1819 2C5C 446 21882 18045 557A 467D 10941 27906 2ABD 6D02 21303 11226 5337 2BDA 447 3763 25441 0EB3 6361 22153 32652 5689 7F8C 28096 16268 6DC0 3F8C 448 206 27066 00CE 69BA 103 13533 0067 34DD 8905 14491 22C9 389B 449 28798 13740 707E 35AC 14399 6870 383F 1AD6 26997 8366 6975 20AE 450 32402 13815 7E92 35F7 16201 21703 3F49 54C7 15047 26009 3AC7 6599

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1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

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B-11

PN Offset Programming Information

68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

451 13463 3684 3497 0E64 19355 1842 4B9B 0732 17460 5164 4434 142C 452 15417 23715 3C39 5CA3 20428 24685 4FCC 606D 17629 17126 44DD 42E6 453 23101 15314 5A3D 3BD2 31950 7657 7CCE 1DE9 10461 21566 28DD 543E 454 14957 32469 3A6D 7ED5 19686 29014 4CE6 7156 21618 21845 5472 5555 455 23429 9816 5B85 2658 31762 4908 7C12 132C 11498 28149 2CEA 6DF5 456 12990 4444 32BE 115C 6495 2222 195F 08AE 193 9400 00C1 24B8 457 12421 5664 3085 1620 18834 2832 4992 0B10 16140 19459 3F0C 4C03 458 28875 7358 70CB 1CBE 27061 3679 69B5 0E5F 13419 7190 346B 1C16 459 4009 27264 0FA9 6A80 22020 13632 5604 3540 10864 3101 2A70 0C1D 460 1872 28128 0750 6DE0 936 14064 03A8 36F0 28935 491 7107 01EB 461 15203 30168 3B63 75D8 19553 15084 4C61 3AEC 18765 25497 494D 6399 462 30109 29971 759D 7513 27422 29877 6B1E 74B5 27644 29807 6BFC 746F 463 24001 3409 5DC1 0D51 32560 18580 7F30 4894 21564 26508 543C 678C 464 4862 16910 12FE 420E 2431 8455 097F 2107 5142 4442 1416 115A 465 14091 20739 370B 5103 19029 26301 4A55 66BD 1211 4871 04BB 1307 466 6702 10191 1A2E 27CF 3351 24027 0D17 5DDB 1203 31141 04B3 79A5 467 3067 12819 0BFB 3213 21549 22325 542D 5735 5199 9864 144F 2688 468 28643 19295 6FE3 4B5F 26145 27539 6621 6B93 16945 12589 4231 312D 469 21379 10072 5383 2758 30737 5036 7811 13AC 4883 5417 1313 1529 470 20276 15191 4F34 3B57 10138 21399 279A 5397 25040 8549 61D0 2165 471 25337 27748 62F9 6C64 24748 13874 60AC 3632 7119 14288 1BCF 37D0 472 19683 720 4CE3 02D0 30625 360 77A1 0168 17826 8503 45A2 2137 473 10147 29799 27A3 7467 16897 29711 4201 740F 4931 20357 1343 4F85 474 16791 27640 4197 6BF8 28955 13820 711B 35FC 25705 15381 6469 3C15 475 17359 263 43CF 0107 28727 20159 7037 4EBF 10726 18065 29E6 4691 476 13248 24734 33C0 609E 6624 12367 19E0 304F 17363 24678 43D3 6066 477 22740 16615 58D4 40E7 11370 28239 2C6A 6E4F 2746 23858 0ABA 5D32 478 13095 20378 3327 4F9A 18499 10189 4843 27CD 10952 7610 2AC8 1DBA 479 10345 25116 2869 621C 17892 12558 45E4 310E 19313 18097 4B71 46B1 480 30342 19669 7686 4CD5 15171 26710 3B43 6856 29756 20918 743C 51B6 481 27866 14656 6CDA 3940 13933 7328 366D 1CA0 14297 7238 37D9 1C46 482 9559 27151 2557 6A0F 17275 31547 437B 7B3B 21290 30549 532A 7755 483 8808 28728 2268 7038 4404 14364 1134 381C 1909 16320 0775 3FC0 484 12744 25092 31C8 6204 6372 12546 18E4 3102 8994 20853 2322 5175 485 11618 22601 2D62 5849 5809 25112 16B1 6218 13295 26736 33EF 6870 486 27162 2471 6A1A 09A7 13581 19183 350D 4AEF 21590 10327 5456 2857 487 17899 25309 45EB 62DD 29477 32594 7325 7F52 26468 24404 6764 5F54 488 29745 15358 7431 3BFE 27592 7679 6BC8 1DFF 13636 7931 3544 1EFB 489 31892 17739 7C94 454B 15946 27801 3E4A 6C99 5207 5310 1457 14BE 490 23964 12643 5D9C 3163 11982 22157 2ECE 568D 29493 554 7335 022A 491 23562 32730 5C0A 7FDA 11781 16365 2E05 3FED 18992 27311 4A30 6AAF 492 2964 19122 0B94 4AB2 1482 9561 05CA 2559 12567 6865 3117 1AD1 493 18208 16870 4720 41E6 9104 8435 2390 20F3 12075 7762 2F2B 1E52 494 15028 10787 3AB4 2A23 7514 23341 1D5A 5B2D 26658 15761 6822 3D91 495 21901 18400 558D 47E0 31510 9200 7B16 23F0 21077 12697 5255 3199 496 24566 20295 5FF6 4F47 12283 27039 2FFB 699F 15595 24850 3CEB 6112 497 18994 1937 4A32 0791 9497 19956 2519 4DF4 4921 15259 1339 3B9B 498 13608 17963 3528 462B 6804 27945 1A94 6D29 14051 24243 36E3 5EB3 499 27492 7438 6B64 1D0E 13746 3719 35B2 0E87 5956 30508 1744 772C 500 11706 12938 2DBA 328A 5853 6469 16DD 1945 21202 13982 52D2 369E

B-12

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1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

DRAFT

Mar 2003

PN Offset Programming Information68P64115A18–1

Table B-1: PnMaskI and PnMaskQ Values for PilotPn

14–Chip Delay 13–Chip Delay 0–Chip Delay

Pilot I Q I Q I Q I Q I Q I Q PN (Dec.) (Hex.) (Dec.) (Hex.) (Dec.) (Hex.)

501 14301 19272 37DD 4B48 19006 9636 4A3E 25A4 11239 25039 2BE7 61CF 502 23380 29989 5B54 7525 11690 29870 2DAA 74AE 30038 24086 7556 5E16 503 11338 8526 2C4A 214E 5669 4263 1625 10A7 30222 21581 760E 544D 504 2995 18139 0BB3 46DB 21513 27985 5409 6D51 13476 21346 34A4 5362 505 23390 3247 5B5E 0CAF 11695 18539 2DAF 486B 2497 28187 09C1 6E1B 506 14473 28919 3889 70F7 19860 30279 4D94 7647 31842 23231 7C62 5ABF 507 6530 7292 1982 1C7C 3265 3646 0CC1 0E3E 24342 18743 5F16 4937 508 20452 20740 4FE4 5104 10226 10370 27F2 2882 25857 11594 6501 2D4A 509 12226 27994 2FC2 6D5A 6113 13997 17E1 36AD 27662 7198 6C0E 1C1E 510 1058 2224 0422 08B0 529 1112 0211 0458 24594 105 6012 0069 511 12026 6827 2EFA 1AAB 6013 17257 177D 4369 16790 4534 4196 11B6

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B-13

PN Offset Programming Information

Notes

68P64115A18–1

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Appendix C

FRU Optimization/ATP Test Matrix

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C-1

FRU Optimization/ATP Test Matrix

Usage & Background

Periodic maintenance of a site may also mandate re–optimization of specific portions of the site. An outline of some basic guidelines is included in the following tables.

68P64115A18–1

NOTE

Re–optimization steps listed for any assembly detailed in the tables below must be performed anytime an RF cable associated with it is replaced.

Detailed Optimization/ATP Test Matrix

Table C-1 outlines in more detail the tests that would need to be performed if one of the BTS components were to fail and be replaced. It is also assumes that all modules are placed OOS–ROM via the LMF until full redundancy of all applicable modules is implemented.

The following guidelines should also be noted when using this table:

NOTE

Passive BTS components (such as the bandpass filters and 2:1 combiners) only require a TX calibration audit to be performed in lieu of a full path calibration. If the TX path calibration audit fails, the entire RF path calibration will need to be repeated. If the RF path calibration fails, further troubleshooting is warranted.

Not every procedure required to bring the site back in service is indicated in Table C-1. It is meant to be used as a guideline ONLY. The table assumes that the user is familiar enough with the BTS Optimization/ATP procedure to understand which test equipment set ups, calibrations, and BTS site preparation will be required before performing the Table # procedures referenced.

C-2

NOTE

When the CIO is replaced, the SCCP shelf remains powered up. The BBX boards may need to be removed, then re–installed into their original slots, and re–downloaded (code and BLO data). RX and TX calibration audits should then be performed on the affected carrier sectors.

1X SC 4812T Lite BTS Optimization/ATP Software Release R2.16.1.x

If any significant change in signal level results from any component being replaced in the RX or TX signal flow paths, it would be identified by re–running the RX and TX calibration audit command.

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Doc

Tbl

FRU Optimization/ATP Test Matrix68P64115A18–1

Table C-1: SC 4812ET Lite BTS Optimization and ATP Test Matrix

Description

RX Cables

DRDC or TRDC

MPC / EMPC

TX Cables

CIO

SCCP Shelf Assembly (Backplane)

BBX2/BBX–1X

CSM/GPS

LFR

50–pair Punchblock (with RGPS)

HSO/HSOX

MCC24E/MCC8E/MCC–1X

RGD/20–pair Punchblock with RGD

GLI2

CCD Card

ETIB or Associated Cables

LPA or LPA Trunking Module

LPAC Cable

LPA Bandpass Filter or Combiner

Switch Card

RFDS

RFDS Cables

Table 3-13/ Table 3-14/

Table 3-16 Table 3-19

Table 3-20 Table 3-35 Table 3-36 Table 3-37

Table 3-45

Table 4-8 Table 4-9

Table 4-10 Table 4-11 Table 4-12

NO TAG

through

NO TAG

Download Code/Data D D D D D D

Enable CSMs D D D D 9 GPS & HSO Initialization

/ Verification LFR Initialization /

Verification TX Path Calibration 4 4 1 1 4 * 3 3 4 7 Download Offsets to

BBX TX Path Audit 4 4 1 1 4 * 3 4 7 RFDS Path Calibration

and Offset Data Download

Spectral Purity TX Mask 4 1 4 * * * * Waveform Quality (rho) 4 * 1 4 * Pilot Time Offset 4 * 1 4 *

Code Domain Power / Noise Floor

FER Test 5 5 5 2 2 5 8 8 8 8 * 7

Alarm Tests

4 1 4 *

6 5

4 1 4 8 8 8 8 * * *

D D D D D D D 9

D D D

1 1 6

* 3

* 10 * *

* * *

6 6

. . . continued on next page

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C-3

FRU Optimization/ATP Test Matrix

68P64115A18–1

Table C-1: SC 4812ET Lite BTS Optimization and ATP Test Matrix

Doc

Tbl

Description

DRDC or TRDC

OPTIMIZATION AND TEST LEGEND:

MPC / EMPC

RX Cables

TX Cables

SCCP Shelf Assembly (Backplane)

CIO

BBX2/BBX–1X

MCC24E/MCC8E/MCC–1X

LFR

CSM/GPS

HSO/HSOX

50–pair Punchblock (with RGPS)

RGD/20–pair Punchblock with RGD

GLI2

CCD Card

ETIB or Associated Cables

LPA or LPA Trunking Module

LPAC Cable

LPA Bandpass Filter or Combiner

Switch Card

D Required

* Perform if determined necessary for addtional fault isolation, repair assurance, or required for site certification.

1. Perform on all carrier and sector TX paths to the SCCP cage.

2. Perform on all carrier and sector main and diversity RX paths to the SCCP cage.

3. Perform on all primary and redundant TX paths of the affected carrier. (LPAC replacement affects all carriers.)

4. Perform on the affected carrier and sector TX path(s) (BBXR replacement affects all carrier and sector TX paths).

5. Perform on the affected carrier and sector RX path(s) (BBXR replacement affects all carrier RX paths).

6. Perform on all RF paths of the affected carrier and sector (RFDS replacement affects all carriers).

7. Perform with redundant BBX for at least one sector on one carrier.

8. Verify performance by performing on one sector of one carrier only.

9. Perform only if RGD/RGPS, LFR antenna, or HSO or LFR expansion was installed.

10. Verify performance by performing testing on one sector of each carrier.

RFDS

RFDS Cables

C-4

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Appendix D

BBX Gain Set Point vs. BTS Output

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D-1

BBX Gain Set Point vs. BTS Output

Usage & Background

Table D-1 outlines the relationship between the total of all code domain channel element gain settings (digital root sum of the squares) and the BBX Gain Set Point between 33.0 dBm and 44.0 dBm. The resultant RF output (as measured in dBm at the BTS antenna connector) is shown in the table. The table assumes that the BBX Bay Level Offset (BLO) values have been calculated.

As an illustration, consider a BBX keyed up to produce a CDMA carrier with only the Pilot channel (no MCCs forward link enabled). Pilot gain is set to 262. In this case, the BBX Gain Set Point is shown to correlate exactly to the actual RF output anywhere in the 33 to 44 dBm output range. (This is the level used to calibrate the BTS).

68P64115A18–1

Table D-1: BBX Gain Set Point vs. Actual BTS Output (in dBm)

dBm’

Gainb

541 – – – – – – – 43.3 42.3 41.3 40.3 39.3 533 – – – – – – – 43.2 42.2 41.2 40.2 39.2 525 – – – – – – – 43 42 41 40 39 517 – – – – – – – 42.9 41.9 40.9 39.9 38.9 509 – – – – – – – 42.8 41.8 40.8 39.8 38.8 501 – – – – – – – 42.6 41.6 40.6 39.6 38.6 493 – – – – – – 43.5 42.5 41.5 40.5 39.5 38.5 485 – – – – – – 43.4 42.4 41.4 40.4 39.4 38.4 477 – – – – – – 43.2 42.2 41.2 40.2 39.2 38.2 469 – – – – – – 43.1 42.1 41.1 40.1 39.1 38.1 461 – – – – – – 42.9 41.9 40.9 39.9 38.9 37.9 453 – – – – – – 42.8 41.8 40.8 39.8 38.8 37.8 445 – – – – – 43.6 42.6 41.6 40.6 39.6 38.6 37.6

44 43 42 41 40 39 38 37 36 35 34 33

437 – – – – – 43.4 42.4 41.4 40.4 39.4 38.4 37.4 429 – – – – – 43.3 42.3 41.3 40.3 39.3 38.3 37.3 421 – – – – – 43.1 42.1 41.1 40.1 39.1 38.1 37.1 413 – – – – – 43 42 41 40 39 38 37 405 – – – – – 42.8 41.8 40.8 39.8 38.8 37.8 36.8 397 – – – – 43.6 42.6 41.6 40.6 39.6 38.6 37.6 36.6 389 – – – – 43.4 42.4 41.4 40.4 39.4 38.4 37.4 36.4

. . . continued on next page

D-2

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BBX Gain Set Point vs. BTS Output68P64115A18–1

Table D-1: BBX Gain Set Point vs. Actual BTS Output (in dBm)

dBm’

Gainb

381 – – – – 43.3 42.3 41.3 40.3 39.3 38.3 37.3 36.3 374 – – – – 43.1 42.1 41.1 40.1 39.1 38.1 37.1 36.1 366 – – – – 42.9 41.9 40.9 39.9 38.9 37.9 36.9 35.9 358 – – – – 42.7 41.7 40.7 39.7 38.7 37.7 36.7 35.7 350 – – – 43.5 42.5 41.5 40.5 39.5 38.5 37.5 36.5 35.5 342 – – – 43.3 42.3 41.3 40.3 39.3 38.3 37.3 36.3 35.3 334 – – – 43.1 42.1 41.1 40.1 39.1 38.1 37.1 36.1 35.1 326 – – – 42.9 41.9 40.9 39.9 38.9 37.9 36.9 35.9 34.9 318 – – – 42.7 41.7 40.7 39.7 38.7 37.7 36.7 35.7 34.7 310 – – 43.5 42.5 41.5 40.5 39.5 38.5 37.5 36.5 35.5 34.5 302 – – 43.2 42.2 41.2 40.2 39.2 38.2 37.2 36.2 35.2 34.2 294 – – 43 42 41 40 39 38 37 36 35 34 286 – – 42.8 41.8 40.8 39.8 38.8 37.8 36.8 35.8 34.8 33.8

333435363738394041424344

278 – 43.5 42.5 41.5 40.5 39.5 38.5 37.5 36.5 35.5 34.5 33.5 270 – 43.3 42.3 41.3 40.3 39.3 38.3 37.3 36.3 35.3 34.3 33.3 262 – 43 42 41 40 39 38 37 36 35 34 33 254 – 42.7 41.7 40.7 39.7 38.7 37.7 36.7 35.7 34.7 33.7 32.7 246 43.4 42.4 41.4 40.4 39.4 38.4 37.4 36.4 35.4 34.4 33.4 32.4 238 43.2 42.2 41.2 40.2 39.2 38.2 37.2 36.2 35.2 34.2 33.2 32.2 230 42.9 41.9 40.9 39.9 38.9 37.9 36.9 35.9 34.9 33.9 32.9 31.9 222 42.6 41.6 40.6 39.6 38.6 37.6 36.6 35.6 34.6 33.6 32.6 31.6 214 42.2 41.2 40.2 39.2 38.2 37.2 36.2 35.2 34.2 33.2 32.2 31.2

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D-3

BBX Gain Set Point vs. BTS Output

Notes

68P64115A18–1

D-4

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Appendix E

CDMA Operating Frequency

Information

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E-1

Nokia Solutions and Networks T5EE1, T5DJ1 Users Manual

Specifications and Main Features

Frequently Asked Questions

User Manual