13048 - Whelen Engineering

®
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
Wingtip Power Supply Replacement for
Cessna Citation 550, Serial #128 and above,
S550 and 560 serial #0001-0256 without
SB560-3308 applied, with 90159 Series
Wingtip Strobe Light Assembly.
90101 Series Strobe Light Power Supply
Installation . . .
1. On both wings of the aircraft, remove the
wingtip access panel by unscrewing the
mounting screws.
2. Remove existing strobe light power supply
from the wing-tip access cut-out by removing
the four mounting screws. Disconnect cables
from power supply.
3. Install the two supplied mounting brackets
(“A” and “B”) with lips on top of existing
brackets, located inside wing-tip access cutout,
and secure with the four mounting
screws.
IMPORTANT NOTE: When brackets are
installed, insure that the upward slope is
facing outboard of the wing.
4. Connect the Whelen Strobe Light Power
Supply to the connectors of the existing
cables and install the power supply onto “A”
and “B” mounting brackets with the
connectors facing outboard. Secure the
power supply with the four #8-32 MS51957-
46mounting screws (supplied) to the “A” and
“B” mounting brackets.
5. Replace the wingtip access panel over the
wingtip cut-out, and secure with the mounting
screws.
EXISTING
BRACKET
MOUNTING BRACKET
LIPS ON TOP OF EXISTING
BRACKETS
MOUNTING BRACKET LIPS
ON TOP OF EXISTING
BRACKETS
EXISTING
BRACKET
VIEW A-A
MOUNT. BRACKETS “A” & “B” TO SLOPE UPWARD FACING OUTBOARD OF AIRCRAFT WING
OUTBOARD
EXISTING BRACKET
MOUNTING BRACKET “B”
INBOARD
MOUNTING BRACKET “A”
Aviation
MOUNTING BRACKETS “A”
AND “B” ARE TO SLOPE
UPWARD FACING OUTBOARD
OF AIRCRAFT WING
OUTBOARD
EXISTING MOUNTING SCREWS (QTY. 4) TO SECURE
MOUNTING BRACKETS TO EXISTING BRACKETS
EXISTING
BRACKET
BRACKET LIP
NOTE: ACCESS CUT-OUT SHOWN IN
ISOMETRIC DRAWINGS AS SEEN FROM
BELOW THE AIRCRAFT’S WING
BRACKET LIP
MOUNTING BRACKET “B”
PN / 11-170576-000
MOUNTING BRACKET “A”
PN / 11-170575-000
©1997 Whelen Engineering Company Inc.
Form No.13048C (052102)
Page 1

Strobe Light Power Supply Installation Instructions (Whelen 90101 Series)
ACCESS
CUT-OUT
MOUNTING
BRACKET “B”
AIRCRAFT
SKIN
OUTBOARD
MOUNTING
BRACKET “A”
WHELEN STROBE
LIGHT POWER SUPPLY
OUTBOARD
Four, #8-32 (MS51957-46)
mounting screws to secure
strobe light power supply
to mounting brackets “A” & “B”
CONNECTORS ON STROBE
LIGHT POWER SUPPLY
MUST FACE OUTWARD
WHELEN STROBE
LIGHT POWER SUPPLY
WARNING! THE STROBE LIGHT POWER SUPPLY
IS A HIGH VOLTAGE DEVICE. DO NOT REMOVE
STROBE TUBES OR DISMANTLE THE STROBE
LIGHT HEAD ASSEMBLIES WHILE IN OPERATION.
IMPORTANT NOTE: CONNECT
CABLES TO STROBE LIGHT
POWER SUPPLY BEFORE
INSERTING INSIDE ACCESS
CUT-OUT AND SECURE TO
MOUNTING BRACKETS.
WAIT 10 MINUTES AFTER TURNING OFF POWER
BEFORE STARTING WORK ON ANY TROUBLE
SHOOTING.
OUTBOARD
WHELEN STROBE
LIGHT POWER SUPPLY
Form No.13048C
Page 2

WHITE WIRE POSITIVE,
(+ 28 VDC)
BLACK WIRE NEGATIVE,
(-) GROUND
TO POWER SUPPLY
WINGTIP SECTION
WHELEN 90159 SERIES WINGTIP
STROBE LIGHT ASSEMBLY
WARNING! THE STROBE LIGHT POWER SUPPLY IS A HIGH VOLTAGE
DEVICE DO NOT REMOVE STROBE TUBES OR DISMANTLE THE
STROBE LIGHT HEAD ASSEMBLIES WHILE IN OPERATION.
WAIT 10 MINUTES AFTER TURNING OFF POWER BEFORE STARTING
WORK ON ANY TROUBLE SHOOTING.
BASE PLATE MOUNTING SCREWS (4)
#10-32 X ¾ INCH, PHILLIPS PAN HEAD
(MS51958-65)
LENS GASKET
LENS
Wingtip Anti-collision/
Position Strobe Light Replacement
for Cessna 550 and 560 Series . . .
BASE PLATE
ASSEMBLY
1. Remove existing wingtip assembly.
2. Clean all excess adhesive from opening and mounting surface.
3. Fill lower hole, if any, with hardware included seperately.
4. Position doubler plate inside wing behind opening.
5. The position light wires should be fed through doubler plate.
6. Observe polarity of existing position light wires, and connect to the wires of
the Whelen light assembly, using DME-20 or equivilant.
LENS RETAINER
LENS RETAINER MOUNTING
SCREWS (2), #10-32 X1INCH,
PHILLIPS FLAT HEAD
(MS51960-70)
NOTE: AT INSTALLATION,
MOUNTING SCREWS SHOULD BE
TIGHTENED EVENLY TO A
MAXIMUM OF 13 IN./LBS. OF
TORQUE.
NOTE: CONNECTION METHOD TO BE CERTIFIED FAA TYPE.
7. Remove lens retainer, lens and gasket from base plate assembly.
8. Using the two lens retainer mounting screws, temporarily attach the base
assembly to the doubler plate to align into position for step 9.
IMPORTANT! SCREWS SHOULD
BE ALTERNATELY TIGHTENED
UNTIL THE FINAL TORQUE VALUE
HAS BEEN ACHIEVED.
9. Permanently align and attach base plate assembly to doubler plate using the
four base plate mounting screws.
10. Remove the two lens retainer screws.
11. Following the procedure provided for the mounting hardware, securely attach
gasket, lens and lens retainer to base plate assembly, using the two lens
retainer screws. NOTE: Gasket should be aligned properly.
13. Connect strobe power cable to strobe light power supply.
Form No.13048C
Page 3

.187 DIA.
(4) MOUNTING HOLES
.25
4.13
3.625 MTG.
1
3.12
OUTPUT INPUT
A=ANODE
B=TRIGGER
C=CATHODE
A=POWER
B=GROUND-
C=SYNC.
3.21
.080
MS3102R10SL-3S CONN.(REF) MS3102R10SL-3P CONN.(REF)
OR EQUIVALENT
OR EQUIVALENT
WIRING
WIRING
A=ANODE
B=TRIGGER
C=CATHODE
A=POWER(+)
B=GROUND(-)
C=SYNC.
.25
.95
2
INSTALL CAP
AFTER FINAL
TEST
5.60
5.100 MTG.
3
5.00
1.36 TYP.
4
REV ECN DESCRIPTION DATE
F
8339 ADDED -02 & -03 UNITS 11/2/92
G 8386 DELETED RIVETS
11/17/92
H 8464 ADDED NOTES
12/10/92
J 9254 ADDED SHEET #4
6/15/93
K 10100 CHGD SPECS 1/25/94
L 10210 REV'D DWG & SPECS 2/17/94
M 10714 ROTATE MS CONNECTORS 6/6/94
N 11300 ADDED -05 ASSEMBLY 10/28/94
P 11776 ADDED -06 ASSEMBLY 2/2/95
R
REVISED RADIATED SUSCEPT. NOTE
14469
5/22/96
T 15283 ADDED -07 ASSEMBLY 10/24/96
U 16256 REV'D RADIATED SUSCEPT. NOTE REV'D RADIATED EMISSIONS NOTE 3/4/97
17398 ADDED -01 ASSEMBLY
7/8/97
W
GENERAL NOTES:
1. SPECIFICATIONS:
INPUT VOLTAGE.........14 VDC or 28 VDC (TYP)
INPUT CURRENT........4 AMPS or 2 AMPS
FLASHRATE................45±5 BURSTS PER MIN.
JOULES......................16,6,6,6
WEIGHT......................1.7 lbs.
34 JOULES WITHIN 405ms.
ENERGY.....................22 JOULES WITHIN 200ms.
(AVG)
2. THIS POWER SUPPLY (P/N 01-0790101-04) USED WITH STROBE LIGHT
PART NUMBERS 01-0790159-( ) MEETS THE MINIMUM REQUIREMENTS
STATED IN FAR PART 23 & PART 25 FOR ANTI-COLLISION LIGHT SYSTEMS.
ENVIRONMENTAL TEST REQUIREMENTS IN ACCORDANCE WITH RTCA/DO-160C:
3. THE 01-0790101-04 POWER SUPPLY COMPLIES WITH THE FOLLOWING
U
R
TEMPERATURE/ALTITUDE - SECT. 4, CAT. D2
VIBRATION - SECT. 8, ROBUST (8.6)
WATERPROOFNESS - SECT. 10, CAT. S
FLUIDS SUSCEPTABILITY - SECT. 11, SPRAY TEST (11.4.1)
SAND & DUST - SECT. 12, CAT. D
SALT SPRAY - SECT. 14, CAT. S
POWER INPUT - SECT. 16, CAT B
VOLTAGE SPIKE - SECT. 17, CAT. B, PAR. 17.4
AUDIO FREQUENCY CONDUCTED SUSPECT. - SECT. 18, CAT. B, PAR. 18.3.1
MAGNETIC FIELDS INDUCED INTO EQ. - SECT. 19, CAT. B, PAR. 19.3.1
SPIKES INDUCED INTO INTERCONN. CABLES - SECT. 19, CAT. B, PAR 19.3.4
RADIATED AND CONDUCTED SUSCEPTABILITY - SECT. 20, CAT. U, PAR 20.4, 20.5
RADIATED AND CONDUCTED EMISSIONS - SECT. 21, CAT. B, PAR. 21.3, 21.4
4. FAA - STC, TSO - C96a APPROVED
1 4 01-0267530-00
POWER SUPPLY, HTS-CF-MS - MOD YAL14/28Q4516-1VA
1 3
10-0530592-02
MFG. LABEL
2 2 22-0430469-00 CAP PLUG
1 1 10-0330445-00 INPUT OUTPUT LABEL
01-0790101-04
POWER SUPPLY, STROBE LIGHT (HTS-CF-MS)
QTY. ITEM
PART NUMBER
DESCRIPTION
1994
WHELEN ENG. CO.
TOLERANCE:
UNLESS OTHERWISE SPECIFIED
ANGLES ±1/2ANGLES °
THIS DRAWING IS PROPRIETARY TO THE WHELEN ENGINEERING
COMPANY ANY REPRODUCTION, DISCLOSURE OR USE OF THIS
DRAWING WITHOUT WRITTEN AUTHORIZATION FROM WHELEN
ENGINEERING COMPANY IS PROHIBITED.
CUSTOMER CONTRACT NO. CALC. WT.
PIONEERS IN SAFETY SIGNALS
ENGINEERING COMPANY
ROUTE 145
CHESTER, CT 06412-0684
TELEPHONE (203) 526-9504
MATERIAL
.XX = ±.03
.XXX = ±.020
DR. DATE
JPA 2/18/94
1.7 lbs. HTS - 90101 SERIES
POWER SUPPLY ASSY.
FINISH
CH.
DATE
SCALE
REL. DATE
GPS
10/28/94 NONE
2/18/94
ENG.
DATE
CAGE CODE DWG NO.
REV SHEET OF
VGC
2/21/94
APP.
DATE
VGC
10402
2 5
10/28/94
90101 W
C
#
R
Form No.13048C
Page 4

.62
3.06
3.65
(GLASS LENS)
3.50
(PLASTIC LENS)
WINGTIP SECTION
REF.
1.89
22"
APPROX.
26"
APPROX.
11 21 12
11.03
9.375
LENS RETAINER MOUNTING SCREW
(2) PLACES
CLEARANCE HOLES FOR #10
(2)PLACES
.49
1.6
MS 3106F-10SL-3P
3 PIN CONNECTOR
A - ANODE
B - TRIGGER
C - CATHODE
2.38
.85 R.
BLACK (GROUND)
WHITE (POSITIVE)
SHIELD GROUND: TO BE SECURED
BY MOUNTING SCREW (ITEM 4)
1
3
4
5
6
7
8
4 13 14 15 16 17 18
8
19
9.375
3.45
8.12
19.11 R.
7.65 R.
MOUNTING CONFIGURATION
9 20 22 10 2
NOTE:
MOUNTING SCREWS TO
BE TIGHTENED EVENLY
TO A MAXIMUM OF
13 IN./LBS. OF TORQUE.
IMPORTANT...
SCREWS SHOULD BE
ALTERNATELY TIGHTENED
UNTIL THE FINAL TORQUE
VALUE HAS BEEN
ACHIEVED.
REV ECN DESCRIPTION DATE
REV ECN DESCRIPTION DATE
.62 R.
U
V
MIN. OPENING
REQUIRED IN WINGTIP
20986
25628
NOTES:
ADD "STC", DELETED "PMA"
ADDED TORQUE SPEC TO LENS
RETAINER MTG SCREWS
11/12/98
5/20/02
A
B 8902 REV STROBE ASSY 1/19/93
C
D 9149 REMOVE GASKET 5/17/93
E
F 9526 ADD SHEET 2 8/27/93
G
8615
9019
9213
9881
REV'D SCREWS TO #6
CHG P/N OF IT 5
ADD SHIELD GRD
UPDATE DWG
1/19/93
4/6/93
6/3/93
12/2/93
H 10025 CHG 70603 TITLE 1/13/94
11057 SEE SHEET 2
9/7/94
ADDED FAA NOTE
K 11312
11/1/94
CHANGED P/N ITEM 5
ADDED NEW ASSEMBLYS
L 13203
-05 THRU -08
10/16/95
CH. HDWARE, ADDED GASKET
M 13401
ADDED WEIGHTS 11/21/95
N 13609
P 14305
R
14470
T 16349
CHANGED MOUNTING HARDWARE
2/5/96
DELETED GASKET FOR GLASS LENS 4/24/96
USE ITEM 7 GASKET
REVISED RADIATED SUSCEPT. NOTE
REV'D RADIATED SUSCEPT. NOTE
REV'D RADIATED EMISSIONS NOTE
ADDED ASSY'S -09 & -10
ADDED ITEM # 22
5/22/96
3/13/97
1. SPECIFICATIONS:
POSITION LIGHT VOLTAGE......27.5V +/-0.5V
FLASHTUBE.............................XENON
2. UNIT COMPLIES WITH COLOR REQUIREMENTS OF FAR PART 25.1397(a).
AVIATION RED, GREEN, AND WHITE.
3. UNIT COMPLIES WITH FAR PART 25.1401 REQUIREMENTS USING AN APPROVED
POWER SUPPLY OF 22 JOULES MINIMUM, 30 JOULES MAXIMUM.
4. UNIT COMPLIES WITH THE FOLLOWING ENVIRONMENTAL TEST REQUIREMENTS
IN ACCORDANCE WITH RTCA/DO-160 C:
TEMPERATURE/ALTITUDE: SECT. 4, CATEGORY D2
HUMIDITY: SECT. 6, CATEGORY C
VIBRATION: SECT. 8, ROBUST (8.6)
EXPLOSION: SECT. 9, CATEGORY A
WATERPROOFNESS: SECT. 10, CATEGORY S
FLUIDS SUSCEPTABILITY: SECT. 11, SPRAY TEST (11.4.1)
SAND AND DUST: SECTION 12, CATEGORY D
SALT SPRAY: SECT. 14, CATEGORY S
POWER INPUT: SECTION 16, CATEGORY B
VOLTAGE SPIKE: SECT. 17, CATEGORY B, PAR. 17.4
AUDIO FREQENCY CONDUCTED SUSCEPTABILITY: SECT. 18, CAT. B, PAR. 18.3.1
MAGNETIC FIELDS INDUCED INTO EQ.: SECTION 19, CAT. B, PAR. 19.3.1
SPIKES INDUCED INTO INTERCONN. CABLES: SECT. 19, CAT. B, PAR. 19.3.4
RADIATED AND CONDUCTED SUSCEPTABILITY: SECTION 20, CATEGORY U, PAR. 20.4, 20.5
R RADIATED AND CONDUCTED EMISSIONS: SECTION 21, CATEGORY B, PAR. 21.3, 21.4
5. FAA - STC, TSO-C30c AND TSO-C96a APPROVED.
6. WEIGHTS: -05 & -06 W/GLASS LENS - 1.9 lbs.
-01 & -02 W/PLASTIC LENS - 1.3 lbs.
1 1 - - - - 22 68-4170665-34 LENS, GLASS EMI COATED
1 1
1 21 10-0530693-02 LABEL, MFG.
1 1
20
68-4170665-30 LENS, GLASS
2 2
2 2 19 14-0050619-69
#10-32 X 1" PHILLIPS FHMS
18
11-270587-001 RETAINER, LENS - POSITION LIGHT
1 1 17 38-0125020-00
1/8 x 1/2 FOAM PAD
- 1
16 68-4230020-50
LENS, POSITION LIGHT - RED
1 -
15
68-4230020-40 LENS, POSITION LIGHT - GREEN
1 1
1 14
34A0428020-65 LAMP - W1290-28
1 1
1 13
38-0230021-00 GASKET, LENS - POSITION LIGHT
1 1
1 12 10-0320776-00
LABEL, MADE IN USA
- -
1 11 10-0530572-02
LABEL, MFG. -01 & -02 ASSYS.
- - 1 1 10 19-190154-001 RETAINER, PLASTIC LENS
1 9
68-4170581-3A
LENS, PLASTIC
4 4
14-0050503-30
SCREW, 6-32 X 1/2 PPHMS (MS51957-30)
1 1
38-0270590-00
GASKET, LENS
1 1
14-0050503-32
SCREW, 6-32 X 3/4 PPHSS (MS51957-32)
1 1
1 5 02-0270603-00
STROBE ASSY - WINGTIP LIGHT
4 4
4 4 14-0050620-65
#10-32 X 3/4" PPHMS
1 1
1 3 06-170600-000
BASEPLATE ASSY, WINGTIP LIGHT
1 1
19-190187-001 RETAINER, GLASS LENS
1 1
07-790157-001
DOUBLER PLATE
* 01-0790159-10 RIGHT LIGHT ASSY. POS./ANTI-COLL. (EMI GLASS)
01-0790159-09 LEFT LIGHT ASSY. POS./ANTI-COLL. (EMI GLASS)
01-0790159-06 RIGHT LIGHT ASSY. POS./ANTI-COLL. (GLASS LENS)
01-0790159-05 LEFT LIGHT ASSY. POS./ANTI-COLL. (GLASS LENS)
01-0790159-02
RIGHT LIGHT ASSY. POS./ANTI-COLL. (PLASTIC LENS)
01-0790159-01
LEFT LIGHT ASSY. POS./ANTI-COLL. (PLASTIC LENS)
QUANTITY ITEM PART NUMBER DESCRIPTION
THIS DRAWING IS PROPRIETARY TO THE WHELEN ENG. CO. INC., ANY
REPRODUCTION, DISCLOSURE OR USE OF THIS DRAWING WITHOUT
WRITTEN AUTHORIZATION FROM WHELEN ENG. CO. INC. IS PROHIBITED
ENGINEERING COMPANY INC.
ROUTE 145
CHESTER, CT 06412-0684
TELEPHONE (860) 526-9504
MATERIAL
FINISH
POSITION/ANTI-COLLISION
WINGTIP LIGHT
TOLERANCE: UNLESS OTHERWISE SPECIFIED
ANGLES ± 1/2°
.XX=±.02
.XXX=±.002
C 1994 WHELEN ENG. CO. INC. CAGE CODE 10402
DR.
CH.
ENG.
APP.
JAN
GPS
JAN
VGC
SCALE
DATE
11/30/92
90159 V
NONE
RELEASE DATE
11/1/94
1 2
DWG NO. REV ISSUE SHEET OF
-
2
1
1
1
-
-
4
1
4
1
1
1
T
-
2
1
1
1
-
-
4
1
4
1
1
1
*
1
1
-
1
1
1
-
-
1
1
*
1
1
1
1
-
1
1
-
-
1
1
*
-
-
1
-
1
1
1
1
1
1
4
1
1
1
4
1
-
1
*
-
-
1
1
-
4
1
1
-
1
*
8
7
6
2
1
J
R
Form No.13048C
Page 5

.62
3.06
3.50
(PLASTIC LENS)
22"
APPROX.
26"
APPROX.
11.03
9.375
22"
APPROX.
2.38
.85 R.
19.11 R.
MIN. OPENING
REQUIRED IN WINGTIP
7.65 R.
MOUNTING CONFIGURATION
25
26
13
.62 R.
11057 CHG TAIL LIGHT SHIELD
9/7/94
ADDED FAA NOTE
K 11312
CHANGED P/N ITEM 3
11/1/94
ADDED NEW ASSEMBLYS
L 13203
-05 THRU -08 10/16/95
CHANGED HARDWARE, ADDED GASKET
13401
ADDED WEIGHTS
11/21/95
DEL GASKET FOR GLASS LENS
P 14302
USE ITEM 10 GASKET
4/24/96
NOTES:
R 14470 REVISED RADIATED SUSCEPT. NOTE 5/22/96
REVISED RADIATED SUSCEPT. NOTE
1. SPECIFICATIONS:
T
REVISED RADIATED EMISSIONS NOTE
16349
3/13/97
ADDED ASSY'S -11 AND -12
POSITION LIGHT VOLTAGE......27.5V 0.5V
ADDED ITEM #30
FLASHTUBE.............................XENON
2. UNIT COMPLIES WITH COLOR REQUIREMENTS OF FAR PART 25.1397(a).
AVIATION RED, GREEN, AND WHITE.
3. UNIT COMPLIES WITH FAR PART 25.1401 REQUIREMENTS USING AN APPROVED
POWER SUPPLY OF 22 JOULES MINIMUM, 30 JOULES MAXIMUM.
4. UNIT COMPLIES WITH THE FOLLOWING ENVIRONMENTAL TEST REQUIREMENTS
IN ACCORDANCE WITH RTCA/DO-160 C:
TEMPERATURE/ALTITUDE: SECT. 4, CATEGORY D2
HUMIDITY: SECT. 6, CATEGORY C
VIBRATION: SECT. 8, ROBUST (8.6)
EXPLOSION: SECT. 9, CATEGORY A
WATERPROOFNESS: SECT. 10, CATEGORY S
FLUIDS SUSCEPTABILITY: SECT. 11, SPRAY TEST (11.4.1)
SAND AND DUST: SECTION 12, CATEGORY D
SALT SPRAY: SECT. 14, CATEGORY S
POWER INPUT: SECTION 16, CATEGORY B
VOLTAGE SPIKE: SECT. 17, CATEGORY B, PAR. 17.4
AUDIO FREQENCY CONDUCTED SUSCEPTABILITY: SECT. 18, CAT. B, PAR. 18.3.1
MAGNETIC FIELDS INDUCED INTO EQ.: SECTION 19, CAT. B, PAR. 19.3.1
SPIKES INDUCED INTO INTERCONN. CABLES: SECT. 19, CAT. B, PAR. 19.3.4
RADIATED AND CONDUCTED SUSCEPTABILITY: SECTION 20, CATEGORY U, PAR. 20.4, 20.5
RADIATED AND CONDUCTED EMISSIONS: SECTION 21, CATEGORY B, PAR. 21.3, 21.4
5. FAA - STC, TSO-C30c AND TSO-C96a APPROVED.
J
1 2 7
3.65
(GLASS LENS)
WINGTIP SECTION
REF.
1.89
14
29
15
8
9.375
CLEARANCE HOLES FOR #10
(2)PLACES
3.45
LENS RETAINER MOUNTING SCREW
(2) PLACES
.49 8.12
1.6
MS 3106F-10SL-3P
3 PIN CONNECTOR
A - ANODE
B - TRIGGER
C - CATHODE
BLACK (GROUND)
WHITE (POSITIVE)
SHIELD GROUND: TO BE SECURED
BY MOUNTING SCREW (ITEM 8)
NOTE:
PLACE BETWEEN LAMPHOLDER
AND MOUNTING SURFACE
3 4 5
6
23
8
24
9
10
11
27
30
12
28
NOTE:
MOUNTING SCREWS TO
BE TIGHTENED EVENLY
TO A MAXIMUM OF
13 IN./LBS. OF TORQUE.
16
17
18 20
21
19
9
22
IMPORTANT...
SCREWS SHOULD BE
ALTERNATELY TIGHTENED
UNTIL THE FINAL TORQUE
VALUE HAS BEEN
ACHIEVED.
REV ECN DESCRIPTION DATE
REV ECN DESCRIPTION DATE
20986
25628
ADD "STC", DELETED "PMA" 11/12/98 F 9526 ADD SHEET 2 (W\TAILIGHT) 8/27/93
ADDED TORQUE SPEC TO LENS
RETAINER MTG SCREWS
5/20/02
9881 UPDATE DWG
12/2/93
H 10025 ADD TAIL LIGHT SHIELD 1/13/94
N 13609 CHANGED MOUNTING HARDWARE 2/5/96
6. WEIGHTS: -07 & -08 W/GLASS LENS - 2.0 lbs.
-03 & -04 W/PLASTIC LENS - 1.4 lbs.
1 1 - - - - 30 68-4170665-34 LENS, GLASS EMI COATED
1 1
- - 29 1 10-0530694-02 LABEL, MFG.
1 1
28 19-190187-001
RETAINER, GLASS LENS
- -
- - 27 68-4170665-30
LENS, GLASS
1 1
1 1 26 70-0350567-00 SHIELD, TAIL LIGHT - WINGTIP
1 1
1 1
25 21-11091202-0
GROMMET
2 2
2 2 24 14-0050503-27 SCREW, 6-32 X 5/16 PPHSS
1 1
1 1
23 16-0400910-03
FLATWASHER, #4 BRASS
22
14-0050503-32
SCREW, 6-32 X 3/4 PPHSS (MS51957-32)
1 1
1 21 11-270587-001
RETAINER, LENS - POSITION LIGHT
1 1
1 1 20 38-0125020-00 1/8 x 1/2 FOAM PAD
1 19 68-4230020-50
LENS, POSITION LIGHT - RED
18
68-4230020-40
LENS, POSITION LIGHT - GREEN
17
34A0428020-65
LAMP - W1290-28
16
38-0230021-00
GASKET, LENS - POSITION LIGHT
15
10-0320776-00 LABEL, MADE IN USA
14
10-0530692-02 LABEL, MFG.
2 2
13
14-0050619-69 #10-32 X 1" PHILLIPS FHMS
- -
12 19-190154-001
RETAINER, PLASTIC LENS
11
68-4170581-3A LENS, PLASTIC
1 1
10
38-0270590-00 GASKET, LENS
14-0050503-30
SCREW, 6-32 X 1/2 PPHSS (MS51957-30)
4 4
14-0050620-65
#10-32 X 3/4" PPHMS
1 1
1 1
34-0428070-64
LAMP, ESG HALOGEN 28V
1 1
14-0050531-08
SCREW, 2-56 X 5/8 PPHM (MS51957-08)
1 1
1 1
02-0250546-00
LAMPHOLDER ASSY, TAIL LIGHT (WINGTIP)
1 1
13-0050517-02
NUT, 2-56 SELF-LOCKING (MS21042-02)
02-0270603-00 STROBE ASSY, WINGTIP LIGHT
06-170600-001 BASEPLATE ASSY, WINGTIP LIGHT
07-790177-001 DOUBLER PLATE
01-0790159-12
RIGHT LIGHT ASSY. POS./ANTI-COLL/TAIL (EMI GLASS)
01-0790159-11
LEFT LIGHT ASSY. POS./ANTI-COLL/TAIL (EMI GLASS)
01-0790159-08
RIGHT LIGHT ASSY. POS./ANTI-COLL/TAIL (GLASS LENS)
01-0790159-07
LEFT LIGHT ASSY. POS./ANTI-COLL/TAIL (GLASS LENS)
01-0790159-04 RIGHT LIGHT ASSY. POS./ANTI-COLL/TAIL (PLASTIC LENS)
01-0790159-03
LEFT LIGHT ASSY. POS./ANTI-COLL/TAIL (PLASTIC LENS)
QUANTITY ITEM PART NUMBER DESCRIPTION
THIS DRAWING IS PROPRIETARY TO THE WHELEN ENG. CO. INC., ANY
REPRODUCTION, DISCLOSURE OR USE OF THIS DRAWING WITHOUT
WRITTEN AUTHORIZATION FROM WHELEN ENG. CO. INC. IS PROHIBITED
ENGINEERING COMPANY INC.
ROUTE 145
CHESTER, CT 06412-0684
TELEPHONE (860) 526-9504
MATERIAL
FINISH
POSITION/ANTI-COLLISION
WINGTIP LIGHT
TOLERANCE: UNLESS OTHERWISE SPECIFIED
ANGLES ± 1/2°
.XX=±.02
.XXX=±.002
C 1993 WHELEN ENG. CO. INC. CAGE CODE 10402
DR.
JNELSON
CH. GPS
ENG.
JNELSON
APP. VGC
SCALE
DATE
7/29/93
90159 V
NONE
RELEASE DATE
11/1/94
2 2
DWG NO. REV ISSUE SHEET OF
1
1
2
1
1
-
1
1
1
1
-
2
-
-
1
4
4
1
1
1
1
1
*
1
1
2
1
1
1
-
1
1
1
-
2
-
-
1
4
4
1
1
1
1
1
*
T
R
1
1
1
1
1
-
1
1
1
1
-
-
4
1
1
1
1
1
*
1
1
1
1
1
1
1
-
1
1
1
-
-
4
1
1
1
1
1
*
-
1
1
-
1
1
1
1
1
2
1
1
1
4
4
1
1
1
1
1
*
U
V
-
1
-
1
1
1
1
2
1
1
1
4
4
1
1
1
1
1
*
9
8
7
6
5
4
3
2
1
G
M
R
Form No.13048C
Page 6