Whelen 9061391 - Manual

Page 1
®
ENGINEERING COMPANY INC.
2.02
3.31"
7.40
3.50
2.63
20AWG WIRE
MIL-W-22759/43
6.00" ±1.00"
PIN 1
PIN 2
PIN 3
PIN 4
WHT
RED
YEL
BLK
+28V POSITION
+28V ANTI-COLLISION
SYNC
GROUND
CONNECTOR WIRING
51 Winthrop Road
Chester, Connecticut 06412-0684
Phone: (860) 526-9504
Fax: (860) 526-2009
Internet: www.whelen.com
Sales/Service e-mail: [email protected]
Aviation
Installation Guide:
Aviation model 9061391, 9061392
P/N 01-0790613-91, 01-0790613-92
LED Position and Anti-Collision
Light Assembly
©2010 Whelen Engineering Company Inc.
Form No.14455A (060112)
SPECIFICATIONS:
Nominal Operational Voltage:............................... 28 VDC
(Operation from 22-32 VDC)
Input Current:
LED Position Light .....................................................0.23 Amps
LED Anti-Collision Light (Avg.) .................................0.73 Amps
LED Anti-Collision Light ([email protected] Sec.) ..............3.9 Amps
Flashrate.......................................................................45 ±5 / Min.
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.
Certain types of installations may require additional testing.
CONTINUED AIRWORTHINESS:
The forward position light is designed with 4 Green LEDs or 5 Red LEDs.
The tail position light is designed with 2 LEDs. The anti-collision light is
designed with 36 LEDs. If any one LED fails, the unit must be repaired or
replaced. Note: To reduce eye strain, use an optical filter such as dark
glasses or a blue covering dome during LED inspection. 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.
INSTALLATION PROCEDURES:
The following information is to assist you in installing a Whelen light
system. The installation procedure described in the following text will be
confined to a single light installation, but is identical for multiple light
installations.
1. Choose the appropriate Model 90613( ) light assembly.
2. Using the mounting detail information provided, prepare the aircraft
for means to secure the LED light assembly.
3. Connect the inputs according to the chart shown. Connect the
power leads to an appropriately sized breaker. Connections to be in
accordance with FAA approved methods.
4. Remove the lens retainers and carefully remove the lens. Using
appropriate hardware, install the light assembly and insure that all
leads are clear of any obstructions. Secure as required. Secure the
light assembly using vibration resistant threaded fasteners.
5. Carefully reinstall the lens and retainers.
6. Waterproof the lightbase to aircraft. Apply single-part Silicone
(RTV) or equivalent around any open area where water could get
in.
7. Check all avionics systems for interference from this installation.
8. A flight check should be performed by a properly certified pilot.
9. Update aircraft records, complete Form 337 and obtain FAA
field approval for installation, as required.
Note: SYNC is a low power bi-directional control signal. Connecting
to the synchronize signal of any Whelen LED anti-collision
assembly will cause the lights to flash at the same time. If
syncronization is not necessary, the connection may be left open.
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.
TSO-C30c
TYPE I, II & III;
APPROVED
TSO-C96a
CLASS II;
APPROVED