Whelen 90206 User Manual

Page 1
®
ENGINEERING COMPANY INC.
Route 145, Winthrop Road, Chester, Connecticut 06412 Phone: (860) 526-9504 Fax: (860) 526-2009 Internet: www.whelen.com Sales/Service e-mail: aviation@whelen.com
Installation Guide
Aviation model 90206 - ( )
Anti-Collision / Position Light Assembly
FAA / TSO C30c TYPE 1,2 & 3
and
FAA / TSO - C96a
MADE IN THE U.S.A.
APPROVED
Model 90206 - ( )
Anti-Collision / Position
Light Assembly
SPECIFICATIONS (Position Light):
Nominal Operational Voltage:...... 28 VDC
Average Input Current: ................. 1 AMP
Lamp for all Units:.........................28VDC, 26 Watt s Max.
EQUIPMENT LIMITATIONS:
An approved Anti-Collision / Position System consists of two assemblies, one located on each wingtip.
INSTALLATION PROCEDURES:
The following information is to assist you in installing a Whelen Anti-Collision / Position light system.
1. Choose the appropriate M od el 9 020 6 - ( ) re pla ce me nt light assembly.
2. The installation procedure described in the following text will be confined to a single light installation, but is identical for multiple light ins t allation.
3. Remove old anti-collision light, locate and record existing +28 VDC and (-) ground position and output connector from power supply.
4. Use existing mounting holes and hardware.
5. Connect leads from light assembly in recorded manner and l ead from light to power supply.
6. Breaker Make sure existing system is equipped with an appropriate sized breaker.
7. Install light as sembl y and in sure tha t all lead s are cle ar of any obstructions and ty-rap as required. Secure light assembly, use lock washers and/or thread lock, on all threaded fasteners.
Requirements
8. Check all avionics systems for interference from this installation.
9. A flight check should be performed by a properly certified pilot.
10. When necessary, waterproof the light assembly to aircraft. Apply single part silicone (RTV) or equivalent around any open area where water could get in.
11 . Update aircraft records and complete Form 337.
12. Obtain FAA fiel d approval for installation.
10.63
3.06
3.75
.51
1.97
22"
APPROX.
26"
APPROX.
9.375
22"
APPROX.
WINGTIP SKIN
EXISTING
MTG PLATE
Aviation
©1998 Whelen Engineering Company Inc. Form No.13390B (052206)
Page 1
Page 2
DATE
10/2/97
10/2/97
DESCRIPTION
ADD GROM CHG GASK
CHG RET P/N'S
19119
18083
B
A
REV ECN
11/4/98
3/27/98
ADD TSOAPPROVALS
LONGER MTG SCREWS
20054
20963
D
C
CH.SPEC FOR CONDUCTED & RADIATED
5/22/00
EMISSIONS& SUSCEPTABILITY
23213
E
31
5/20/02
10/31/05
5/18/06
ROUTE 145
CHESTER, CT06412-0684
TELEPHONE (860)526-9504
RETAINERMTG SCREWS
CHANGEDTO RFI COATED LENS
ADDEDTORQUE SPEC TO LENS
SEESHEET 3 OF 3
DEL-01 & -02 ASSY
DELTORQUE SPEC
25626
31872
32692
F
G
H
GROMMET EDGING (PANDUIT #GEE62FR-C)
BAG, PLASTIC - 2 1/2 X 5"
SCREW, #6-32 X 7/8 PPHSS (MS51957-33)
RETAINER, LENS - POSITION LIGHT
RETAINER, GLASS LENS - POLISHED W/SEAL
1/8 x 1/2 FOAM PAD
LENS, POSITION LIGHT - GREEN
LENS, POSITION LIGHT - RED
LAMP - W1290-28
GASKET,LENS - POSITION LIGHT
LENS, GLASS (RFI COATED)
STROBE ASSY - WINGTIPLIGHT
GASKET,LENS
SCREW, 6-32 X 1/2 PPHMS (MS51957-30)
BASEPLATEASSY, WINGTIP LIGHT
LABEL, MFG. - MODEL 90206
SCREW, 6-32 X 3/4 PFHSS (MS51959-32)
LABEL, MFG. - MODEL 90206
LABEL, MFG. - MODEL 90206
LABEL, MFG. - MODEL 90206
LABEL, MADE IN USA
R
ENGINEERING COMPANYINC.
LIGHT ASSY, POS/ANTI-COLL - RIGHT (POL. RET)
LIGHT ASSY, POS/ANTI-COLL - LEFT (POL. RET)
OFSHEET
2/7/97
-
ISSUE
H
2/7/97
REV
DATE RELEASEDATE
LIGHT ASSEMBLY
NONE
90206
POSITION/ANTI-COLLISION
SCALE
DWGNO.
VGC
JAN
GPS
JAN
CH.
APP.
ENG.
DR.
2.00
.47 R.
SPECIFICATIONS:
MIN. OPENING
1.00 DIA (2) HOLES
19.16 R.
9.93
FLAT
.750
7.69 R.
4.140 R.
3.434
1.104 R.
.625
(FOR BASE)
# 6-32
(4) MOUNTING HOLES
REQUIRED IN WINGTIP
7.60
4.80
2.70
1.04
1.14
.57 R.
2.44
1. FORWARDPOSITION LIGHT VOLTAGE......27.5V ±0.5V
(LEFT SHOWN)
MOUNTING CONFIGURATION
AVIATIONRED, GREEN, AND WHITE.
2. UNIT COMPLIES WITH COLOR REQUIREMENTS OF FARPART 25.1397(a).
NOTE: ON RIGHT SIDE FORWARDMTG HOLE ON BOTTOM.
POWER SUPPLYOF 22 JOULES MINIMUM, 30 JOULES MAXIMUM.
3. UNIT COMPLIES WITH FARPART 25.1401 REQUIREMENTS USING AN APPROVED
INACCORDANCE WITH RTCA/DO-160 C:
HUMIDITY - SECT.6, CATEGORY C
VIBRATION- SECT. 8, ROBUST (8.6)
TEMPERATURE/ALTITUDE- SECT. 4, CATEGORYD2
4. UNIT COMPLIES WITHTHE FOLLOWING ENVIRONMENTAL TEST REQUIREMENTS
SANDAND DUST - SECTION 12, CATEGORY D
POWER INPUT - SECTION 16, CATEGORYB
MAGNETIC FIELDS INDUCED INTO EQ. - SECTION 19, CAT.B, PAR. 19.3.1
EXPLOSION - SECT.9, CATEGORY A
SALTSPRAY - SECT. 14, CATEGORYS
FLUIDS SUSCEPTABILITY- SECT. 11, SPRAYTEST (11.4.1)
WATERPROOFNESS- SECT. 10, CATEGORYS
VOLTAGESPIKE - SECT. 17, CATEGORYB, PAR. 17.4
SPIKES INDUCED INTO INTERCONN. CABLES - SECT.19, CAT. B, PAR.19.3.4
AUDIO FREQENCY CONDUCTED SUSCEPT.- SECT. 18, CAT.B, PAR. 18.3.1
03-0610017-00
14-0050619-67 SCREW, #10-32 X 3/4 PFHMS
14-0050503-33
21-5030903-01
1231
1122
11-270587-001
211920
22
11
RADIATED& CONDUCTED EMISSIONS - SECTION 21, CATEGORY B, PAR. 21.3 & 21.4
RADIATED& CONDUCTED SUSCEPTABILITY - SECT. 20, CAT.U, PAR. 20.4 & 20.5
5. WEIGHTS: -03,-04 W/GLASS LENS - 1.9 lbs.
6. FAA- TSO-C30c AND TSO-C96a APPROVED.
19-190314-00S
68-4230020-50
38-0125020-00
68-4230020-40
34-0428020-65
38-0230021-00
17
14
15
18
16
--11
111113511
111
11
E
38-0270590-00
14-0050503-30
68-4170665-34
06-170737-000
02-0270603-00
14-0050508-32
22
11531
1
10-0530852-02
10-0530853-02
10-0530851-02
4
3
5678910111213
-
-
1
1
-
-
10-0530819-02
10-0320776-00
1
2
-­1
1
13
11
10
21
PARTNUMBER DESCRIPTION
01-0790206-03
01-0790206-04
*
*
QUANTITY ITEM
THISDRAWING IS PROPRIETARY TO THE WHELEN ENG. CO. INC.,ANY
REPRODUCTION,DISCLOSURE OR USE OF THIS DRAWING WITHOUT
WRITTENAUTHORIZATION FROM WHELEN ENG. CO. INC. IS PROHIBITED
MATERIAL
CAGECODE 10402
.XXX=±.005
.XX=±.02
WHELENENG. CO. INC.
1997
C
TOLERANCE:UNLESS OTHERWISE SPECIFIED
ANGLES±1/2°
FINISH
20
9
LENS RETAINER
MOUNTING SCREW
(2) PLACES
WINGTIP SKIN
EXISTING MTG PLATE
SHIELD GROUND: TO BE SECURED
NOTE:
8
BY MOUNTING SCREW (ITEM 10)
10
APPLY GROMMET EDGING MATERIAL TO HOLE.
7
19
10.63
9.375
.51
1.6
B - TRIGGER
A - ANODE
C - CATHODE
3 PIN CONNECTOR
MS 3106F-10SL-3P
3.06
1.97
FORWARD POSITION LIGHT
3.75
BLACK (GROUND)
WHITE (POSITIVE
22"
APPROX.
26"
APPROX.
NOTE:
GROMMET EDGING (ITEM 22) AND
SCREWS:
MS51957-33 (ITEM 20 - QTY 2)
MS51959-32 (ITEM 7 - QTY 2)
(ITEM 23) AND STAPLEDTO CABLE
TO BE PACKAGEDIN A PLASTIC BAG
Page 2
6
18
17
5
16
4
3
15
2
14
1
7
22
23
7
20
REF.
WINGTIP SECTION
Page 3
DATE
10/2/97
10/2/97
DESCRIPTION
ADD GROM CHG GASK
19119
18083 CHG RETP/N'S
B
A
REV ECN
3/27/98
BAG HARDWARE
20054
C
11/4/98
ADDED TSOAPPROVALS
20963
D
CH.SPEC FOR CONDUCTED & RADIATED
5/22/00
EMISSIONS& SUSCEPTABILITY
CHANGEDTO RFI COATED LENS
23213
E
.47 R.
ADDEDTORQUE SPEC TO LENS
5/20/02
RETAINERMTG SCREWS
25626
F
10/31/05
SEESHEET 3 OF 3
31872
G
DEL-05 & -06
5/18/06
DELTORQUE SPECS
32692
H
2.00
SPECIFICATIONS:
32
OFSHEET
2/7/97
-
ISSUE
H
2/7/97
REV
DATE RELEASEDATE
DESCRIPTIONPARTNUMBER
ROUTE 145
R
CHESTER, CT06412-0684
TELEPHONE (860)526-9504
LIGHT ASSEMBLY
NONE
90206
POSITION/ANTI-COLLISION
SCALE
1/8 x 1/2 FOAM PAD
RETAINER,GLASS LENS - POLISHED W/SEAL
LENS, POSITION LIGHT - RED
RETAINER,LENS - POSITION LIGHT
GASKET,LENS - POSITION LIGHT
LAMP - W1290-28
LENS, POSITION LIGHT - GREEN
SCREW, #10-32 X 3/4" PFHMS
BAG, PLASTIC - 2 1/2 X 5"
GROMMET EDGING (PANDUIT#GEE62FR-C)
SCREW, 6-32 X 7/8 PPHMS (MS51957-33)
38-0125020-00
19-190314-00S
68-4230020-50
11-270587-001
38-0230021-00
34-0428020-65
68-4230020-40
14-0050619-67
14-0050503-33
03-0610017-00
21-5030903-01
27
28
2911
INACCORDANCE WITH RTCA/DO-160 C:
TAILLIGHT VOLTAGE.............................27.5V ±0.5V
AVIATIONRED, GREEN, AND WHITE.
1. FORWARDPOSITION LIGHT VOLTAGE......27.5V ±0.5V
2. UNIT COMPLIES WITH COLOR REQUIREMENTS OF FARPART 25.1397(a).
3. UNIT COMPLIES WITH FARPART 25.1401 REQUIREMENTS USING AN APPROVED
POWER SUPPLYOF 22 JOULES MINIMUM, 30 JOULES MAXIMUM.
4. UNIT COMPLIES WITHTHE FOLLOWING ENVIRONMENTAL TEST REQUIREMENTS
WATERPROOFNESS- SECT. 10, CATEGORYS
FLUIDS SUSCEPTABILITY- SECT. 11, SPRAYTEST (11.4.1)
EXPLOSION - SECT.9, CATEGORY A
VIBRATION- SECT. 8, ROBUST (8.6)
HUMIDITY - SECT.6, CATEGORY C
TEMPERATURE/ALTITUDE- SECT. 4, CATEGORYD2
RADIATED& CONDUCTED EMISSIONS - SECTION 21, CATEGORY B, PAR. 21.3 & 21.4
RADIATED& CONDUCTED SUSCEPTABILITY - SECT. 20, CAT.U, PAR. 20.4 & 20.5
SPIKES INDUCED INTO INTERCONN. CABLES - SECT.19, CAT. B, PAR.19.3.4
VOLTAGESPIKE - SECT. 17, CATEGORYB, PAR. 17.4
SALTSPRAY - SECT. 14, CATEGORYS
MAGNETIC FIELDS INDUCED INTO EQ. - SECTION 19, CAT.B, PAR. 19.3.1
POWER INPUT - SECTION 16, CATEGORYB
SANDAND DUST - SECTION 12, CATEGORY D
AUDIO FREQENCY CONDUCTED SUSCEPT.- SECT. 18, CAT.B, PAR. 18.3.1
5. WEIGHTS: -03,-04 W/GLASS LENS - 1.9 lbs.
6. FAA- TSO-C30c AND TSO-C96a APPROVED.
22
11
24
26
25
1
1
33
22
-
111
11
-
21
201923
18
11
111
LENS, GLASS (RFI COATED)
SCREW, 6-32 X 1/2 PPHMS (MS51957-30)
GASKET,LENS
68-4170665-34
14-0050503-30
38-0270590-00
16
15
17
11
77
11
NUT,2-56 SELF-LOCK (MS21042-02)
LAMP,ESG HALOGEN 28V
13-0050517-02
34-0428070-64
70-0350567-00 SHIELD, TAILLIGHT
14
13
121110
11
11
11
LAMPHOLDER ASSY,TAIL LIGHT
SCREW, 2-56 X 5/8 PPHM (MS51957-8)
FLATWASHER,#4 BRASS
02-0250546-00
14-0050531-08
16-0400910-03
98765
1
11
11
1
BASEPLATEASSY, W/TAILLIGHT
STROBE ASSY,WINGTIP LIGHT
SCREW, 6-32 X 3/4 PFHMS (MS51959-32)
06-170737-001
14-0050508-32
02-0270603-00
11
1
2
2
1
LABEL, MFG. - MODEL 90206 (W/TAIL.)
LABEL, MFG. - MODEL 90206 (W/TAIL.)
LABEL, MFG. - MODEL 90206 (W/TAIL.)
10-0530846-02
10-0530855-02
10-0530854-02
3
4
1
-
1
--
-
LABEL, MADE IN USA
LABEL, MFG. - MODEL 90206 (W/TAIL.)
10-0320776-00
10-0530845-02
2
1
1
--
1
LIGHTASSY, POS-TAIL/ANTI-COLL - RIGHT(POL.RET)
LIGHTASSY, POS-TAIL/ANTI-COLL - LEFT(POL.RET)
01-0790206-08
01-0790206-07
ITEMQUANTITY
*
*
ENGINEERING COMPANYINC.
E
THISDRAWING IS PROPRIETARY TO THE WHELEN ENG. CO. INC.,ANY
REPRODUCTION,DISCLOSURE OR USE OF THIS DRAWING WITHOUT
WRITTENAUTHORIZATION FROM WHELEN ENG. CO. INC. IS PROHIBITED
MATERIAL
DWGNO.
VGC
JAN
GPS
JAN
CH.
APP.
ENG.
DR.
CAGECODE 10402
.XXX=±.010
.XX=±.02
WHELENENG. CO. INC.
1997
C
TOLERANCE:UNLESS OTHERWISE SPECIFIED
ANGLES±1/2°
FINISH
1.00 DIA (2) HOLES
19.16 R.
FLAT
9.93
.750
7.69 R.
4.140 R.
3.434
1.104 R.
(FOR BASE)
# 6-32
(4) MOUNTING HOLES
10.63
9.375
.51
3.06
REQUIRED IN WINGTIP
MIN. OPENING
14
15
16
AND MOUNTING SURFACE
BY MOUNTING SCREW (ITEM 15)
SHIELD GROUND: TO BE SECURED
13
12
11
10
9
8
7
(LEFT SHOWN)
7.60
6.95
4.80
2.70
1.04
PLACE BETWEEN LAMPHOLDER
1.14
MOUNTING CONFIGURATION
WINGTIP SKIN
NOTE: ON RIGHT SIDE FORWARD MTG HOLE ON BOTTOM.
EXISTING MTG PLATE
.625
.57 R.
2.44
LENS RETAINER
MOUNTING SCREW
(2) PLACES
NOTE:
APPLY GROMMET EDGING MATERIAL TO HOLE
NOTE:
22"
APPROX.
17
6
26"
APPROX.
5
1.97
22"
APPROX.
4
3
2
3.75
1
27
19
26
15
25
24
23
22
21
20
1.6
B - TRIGGER
A - ANODE
C - CATHODE
3 PIN CONNECTOR
MS 3106F-10SL-3P
FORWARD POS. LIGHT
BLACK (GROUND)
WHITE (POSITIVE)
TAIL POS. LIGHT
BLUE (BOTH)
NO POLARITY
NOTE:
GROMMET EDGING (ITEM 28) AND
SCREWS:
MS51959-32 (ITEM 7 - QTY 2)
MS51957-33 (ITEM 26 - QTY 2)
TO BE PACKAGEDIN A PLASTIC BAG
28
29
(ITEM 29) AND STAPLEDTO CABLE
Page 3
7
7
26
REF.
WINGTIP SECTION
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