Whelen 9061301 - Manual

Page 1
.25
2.01
3.81"
5.61
1.77
POS. A
POS. B
POS. C
POS. D
POS. E
+28V POSITION
+28V ANTI-COLLISION
+28V INFRARED
GROUND
SYNC
MS27508E10F5P Connector Wiring
®
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: [email protected]
Aviation
Installation Guide:
Aviation model 9061301, 9061302
P/N 01-0790613-01, 01-0790613-02
LED Position, Anti-Collision and
Infrared Light Assembly
©2012 Whelen Engineering Company Inc.
Form No.14444A (053112)
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
LED Infrared Light (Avg.).......................................... 0.09 Amps
LED Infrared Light ([email protected] Sec.) ....................... 0.5 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.
Per FAR 23.1401(d) or 25.1401(d) do not operate the anti-collision
light and the ground recognition light at the same time.
The Ground Recognition Light is a non-TSO function.
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 ground
recognition light is designed with 8 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 necessary.
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