Whelen 7097001 User Manual

®

ENGINEERING COMPANY INC.

Route 145, Winthrop Road,
Chester, Connecticut 06412
Phone: [phone]
Fax: [phone]
Internet: www.whelen.com
Sales/Service e-mail: [e-mail]

Installati on Guide:

Models 7097001 (Green) and 7097002 (Red)

P/N:01-0770970-01 and 01-0770970-02,

LED Forward Position Light for

90159( ) or 90206( )

TSO-C30c
TYPE I & II
APPROVED

Model Shown:
7101102

OPERATING INSTRUCTIONS:

Nominal Voltage: . . . . . . . . . . . . 28 VDC

Input Current:. . . . . . . . . . . . . . . 0.3 Amps

Weight: . . . . . . . . . . . . . . . . . . . . 0.17 lbs.

Removal Procedure...

1. Remove retainer screws, retainer, lens and
gasket from the wingtip assembly. Save these
components.

2. Remove and save the two position light
retainer screws.

3. Remove the position light retainer, lens, lamp
and lens gasket. These items may be saved
for use as spares.

MADE IN THE U.S.A.

The conditions and tests required for TSO approval of this
article are minimum performance standards. It is the
responsibility of those installing this article either on or
within a specific type or class of aircraft to determine that
the aircraft installation conditions are within the TSO
standards. TSO articles must have separate approval for
installation in aircraft. The article may be installed only if
performed under 14 CFR part 43 or the applicable
airworthiness requirements.

EQUIPMENT LIMITATIONS: The LED position light is approved as an
incandescent lamp replacement module, for installation in Whelen Model
90159( ) or Whelen Model 90206( ).

CONTINUED AIRWORTHINESS: The LED position light is designed with 6
LED’s. If any one LED fails, the unit must be repaired or replaced. Inspect
the lens for excessive scratches or pitting. Replace if necessary.

Remove

these
items

Gasket

Lens

Retainer

Screw

Save

Replacement Procedure...

1. Insert the LED assembly into the now vacant
lamp socket. The contact is 28VDC. The
chassis is ground.

2. Secure the 70970 LED assembly using the
position light retainer screws from Step 2.
Tighten these screws equally to maximum
torque value of 13 in./lbs.

3. Reinstall the gasket, lens, retainer and
retainer screws in their original location.
Tighten these screws equally to maximum
torque value of 13 in./lbs.

4. Update aircraft records, complete form 337
and obtain FAA field approval for installation.

Aviation

©2005 Whelen Engineering Company Inc.
Form No.13957A (062005)

Note: Screws should be

alternately tightened

until the final torque

value has been

achieved!

70970
LED
Assembly

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