Whelen 9036801 User Manual
®
ENGINEERING COMPANY INC.
51 Winthrop Road
Chester, Connecticut 06412-0684
Phone: (860) 526-9504
Fax: (860) 526-2009
Internet: www.whelen.com
Sales/Service e-mail: aviation@whelen.com
Installation Guide:
Aviation model 9036801,9036802
P/N 01-0790368-01, 01-0790368-02
LED Anti-Collision/LED Position Light Ass’y
TSO-C30c
TYPES I , II & III;
APPROVED
TSO-C96a
CLASS I;
APPROVED
MADE IN THE U.S.A.
SPECIFICATIONS:
Nominal Operational Voltage: ....................... 28 VDC
Input Current:
LED Position Light........................................ 0.5 amps
LED Anti-Collision Light (Pulse@0.25 sec) .. 2.8 amps
LED Anti-Collision Light (Average) ............... 0.5 amps
Flashrate: ........................................................ 45± 5 per min.
Total Weight .................................................... 1.1 lbs.
EQUIPMENT LIMITATIONS:
An approved lighting system consists of two lights, one
located on each wingtip. The baseplate must be mounted
parallel to the vertical and horizontal centerlines of the
aircraft to project the patterns properly.
CONTINUED AIRWORTHINESS:
The forward position light is designed with 6 LED’s. The
rear position light is designed with 3 LED’s. The AntiCollision light is designed with 36 LED’s. If any one LED
fails, the unit must be repaired or replaced. Inspect the
lens. Replace if there is excessive scratching, pitting,
discoloration or cracking.
Note: The anti-collision light will automatically shut-off
after 9-10 flashes if a failure is detected.
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.
4. Using #8 flathead screws, install light assembly and
insure that all leads are clear of any obstructions and
ty-rap as required. Secure light assembly, using
vibration resistant threaded fasteners.
5. Reinstall the lens.
6. Check all avionics systems for interference from this
installation.
7. A flight check should be performed by a properly
certified pilot.
8. When necessary, waterproof the light base to
aircraft. Apply single part silicone (RTV) or
equivalent around any open area where water could
get in.
9. Update aircraft records, complete Form 337 and
obtain FAA field approval for installation, as
necessary.
2.64
.40
INSTALLATION PROCEDURES:
The following information is to assist you in installing a
Whelen Anti-Collision / Position light system.
1. Choose the appropriate Model 90368( ) replacement
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 installations.
3. Connect the anti-collision inputs and the position
light inputs according to the chart shown.
Connections to be in accordance with FAA approved
methods.
Aviation
©2008 Whelen Engineering Company Inc.
Form No.14231B (092209)
Page 1
MIL-C-38999 SERIES II
CONNECTOR
1.37
2.75
7.48
2.07
3.67
2
4
7
6
3
1
CONNECTOR PINOUTS
MS27508E10A5P
Ground PIN D
N/C PIN E
Position 28V PIN A
Anti-Collision 28V PIN B
Anti-Collision SYNC. PIN C
7
ASS'Y, GREEN LED FINAL MODEL 9036801
ASS'Y, RED LED FINAL MODEL 9036802
5
ASS'Y, GRN MODULE 90358
ASS'Y, RED MODULE 90358
GASKET, LENS
1.480
.740
.125 RAD.(4)
1.2203.920
6.050
MOUNTING CUTOUT DETAIL
LENS, CLEAR HARD COAT
RETAINER, TAIL
RETAINER, FORWARD
SCREW, 6-32 5/16 PFHMS CSNK
.177 DIA (3)
01-0790368-01
01-0790368-02
ITEM PART NUMBER DESCRIPTION
QTY QTY
01-0290407-40
01-0290407-50
38-0290396-00
68-3990373A30
19-150928-000
11
2
3
5
4
111
1
111
19-150929-000
14-0050508-27
7
6
1
4
1
4
.750
1.500
Page 2
Loading...