®
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
TSO-C96a
APPROVED
Installation Guide
Model 90044 - ( )
Flashing Anti-Collision Light Assembly
MADE IN THE U.S.A.
OPERATING INSTRUCTIONS:
Operational Voltage: . . . . . . . . .28 VDC
Average Input Current: . . . . . . .Master 3.2 Amps
EQUIPMENT LIMITATIONS: An approved anti-collision sys tem
consists of two lights, one located on the t op of the vertical fin,
and one located on the underside of the fuselage.
INSTALLATION PROCEDURES: The following information is to
assist you in installing a Whelen flashing anti-collision light
system.
1. Choose the appropriate Model 90044- ( ) replacement light
assembly which is most applicable to your aircraft.
2. The installation procedure described in the following text will
be confined to a sing le light installation, but is identical for
multiple light installation if required .
3. Remove old anti-co lli sion light, locate and save existing +28
VDC lead and (-) ground leads. Clean and prep lead ends
as required.
4. Use existing mounting holes and hardware.
NOTE: If a special mounting ad ap te r plat e is required, contact:
Whelen Aviation Division for requirements.
5. Connect the existing +28 VDC lead to the white/blue lead on
the input cable assembly (supplied with light assembly).
Then connect the ex isting ground lead to the white wi re on
the input cable assembly. If a shield wire exists on the
aircraft, connect it to the shield wire assembly. If no shield
wire exists on the aircraft, trim the shield wire on the cable
assembly flush with the cable jacket. Bo th leads must be
connected by an FAA approved connect ion.
6. Make sure the existing system is equipped with an
appropriate sized breaker.
7. Install light assembly and i nsure that all leads are clear of
Aviation
any obstructions and ty-rap as required. Secure light
©1998 Whelen Engineering Company Inc.
Form No.13224C (062706)
Master/Slave 6.5 Amps
Page 1
assembly, use lock washers and/or thread lo ck on
all threaded fasteners.
8. Check all avionics systems for interference from
this installation.
9. A flight check should be per formed by a properly
certified pilot.
10. When necessary, waterproof the flasher base
assembly to aircraft. Apply single part silicone
(RTV) or equivalent around any open area where
water could get in.
11. Update aircraft record s, complete Form 337 and
obtain FAA field approval for installation.
*OUTPUT
Receptacle MS 3102R10SL-3S mates
with MS 3106F10SL-3P or equivalent.
POS. A, SW. GND.
POS. B, POWER OUT
POS. C, N/C.
INPUT, 28 VDC.
Receptacle MS 3102R10SL-4P mates
with MS 3106F10SL-4S or equivalent.
POS. A, (+) 28 VDC.
POS. B, (-) GROUND.
2.38"
2.70"
.93"
1.00"
.50"
4.40"
2.70"
2.82"
9.87"
2.38"
1.88"
*Only used if
slave is used.
MODEL 90044 REPLACEMENT PARTS
1
2
45
7 8
11 12
ITEM
1
#10-32 X 1/2" PHILLIPS FHMS 14-0050619-65 ALL
RETAINER / 2 HOLE 19-170560-002 -17 thru -20,-35,-41,-53
2
RETAINER / 3 HOLE 19-170560-001 -01 thru -04,-09,-10,-13,-15,-33,-34,-37,-39,-44,-54 thru -58
3
LENS / RED 68-4270569-52 -01,-09,-13,-17,-33,-35,-37,-55,-57
4
5
LENS / WHITE 68-4270569-32 -02,-10,-18,-34,-44,-58
LENS / RED WITH HOLE 68-4270569-53 -03,-15,-19,-39,-41
6
7
LENS / WHITE WITH HOLE 68-4270569-33 -09,-20,-44,-53
LENS / RED WITH 2 HOLES 68-4270569-57
8
9
LENS / MASKED ONLY 68-4250690-33 -53
10
3
6
9
10
LAMP / 28 VOLT / 150 WATT 34-0226010-91 ALL
GASKET / LENS 38-0270584-00 ALL UPPER MT.
11
12
GASKET / LENS / FUEL RESISTANT
ELECTRONIC / 5 HOLE / ALTERNATE / 2.25 LBS. 02-0370601-00 -33,-34
13
ELECTRONIC / 5 HOLE / ALTERNATE 02-0370591-00 -01,-02,-03,-04,-38,-40
14
ELECTRONIC / 5 HOLE / SYNC 02-0370593-00 -09,-10
15
ELECTRONIC / 5 HOLE / ALTERNATE 02-0370634-00 -37,-39,-44
16
ELECTRONIC / 5 HOLE / BOTTOM MOUNT CONN.
17
ELECTRONIC / 5 HOLE / SINGLE CONN.
18
19
GASKET / 5 HOLE
ELECTRONIC / 5 HOLE / SLAVE 02-0370594-00 -13,-15
20
21
ELECTRONIC / 5 HOLE / PIGTAIL
ELECTRONIC / 8 HOLE / ALTERNATE 02-0370595-00 -17,-18,-19,-20,-53
22
ELECTRONIC / 8 HOLE / ALTERNATE / 2.50 LBS.
23
GASKET / 8 HOLE 38-0270585-00 -17,-18,-20,-33,-34,-53
24
GASKET / 8 HOLE 38-0270585-01 -19
25
26
INPUT CABLE 46-0750490-00 -33,-34,-41
INPUT CABLE 46-0770602-00 ALL MASTER UNITS EXCEPT -33-34-41
27
INPUT CABLE 64-0770857-00
28
MOUNTING PLATE / 16 HOLE GULFSTREAM II 06-170618-000 A.R.
29
ELECTRONIC / 9 HOLE / ALTERNATE 02-0370655-00 -41
30
GASKET / 9 HOLE 38-0270656-00 -41
31
DESCRIPTION USED ON FINAL
-( )
PART NUMBER
-54,-56
38-0270584-01 ALL LOWER MT.
02-0370766-00 -54
02-0370767-00 -55,-56
38-0270586-00 -1 thru -04,-09,-10,-13,-15,-16,-33,-34,-37,-39,-44,-54 thru -58
02-0370853-00 -57,-58
02-0370610-00 -35
-57,-58
26 27
28
16
13
14
15
(-37 -39 & -44 5 HOLE MASTER)
20
19
(5 HOLE SLAVE)
29
17
(BOTTOM MOUNTED CONNECTOR)
21
(PIGTAIL)
18
(SINGLE CONNECTION, LOWER LOCATION)
22
23
(8 HOLE MASTER)
30
25
24
WHT/BLUE +28V OR +14V
WHT GROUND
BRAID SHIELD
Page 2
16 HOLE
MOUNTING PLATE
31
(9 HOLE MASTER)