Whelen 9045301 - Manual

Page 1
M
K
L
A
R
J
H
G
N
C
D
F
Anode A
Cathode A1
Cathode A2
Cathode A3
Anode B
Cathode B1
Cathode B2
Cathode B3
Anode
Cathode 1
Cathode 2
Anti-Collision
Anti-Collision
Anti-Collision
Anti-Collision
Anti-Collision
Anti-Collision
Anti-Collision
Anti-Collision
Position
Position
Position
Fault Indicator
D38999 / 20FD15PN Contact
4.86
2.10
.31
.27
.88
3.94
Dust
Cap
Shroud shown
for reference
only.
4 X Ø.164
1.26
.720
.27
.31
2.10
1.43
®
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:
Model(s) 9045301, 9045302
P/N(s): 01-0790453-01, -02
LED Wingtip Anti-Collision /
Position Light Assembly
©2009 Whelen Engineering Company Inc.
Form No.14422 (100110)
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.
EQUIPMENT LIMITATIONS:
An approved forward lighting system consists of at least two
lightheads, one mounted on each wingtip. A separate flasher
assembly, such as model 9045600, is required for each light assembly.
The unit must be mounted parallel to the vertical and horizontal
centerlines of the aircraft to project the patterns properly. This light
assembly must be mounted behind a clear lens.
The maximum length of the interface cable between the light assembly
and the flasher/current source is 20 feet using 20 AWG wire.
Certain types of installations may require additional testing.
SHROUD REQUIREMENT:
If justified by the Aircraft installation and additional FAA testing of
compliance to TSO-C30c and TSO-C96a the shroud may not be
required.
Remove and discard the two, #6 screws that are used to secure the
shroud. Carefully remove the shroud. CAUTION: Do not touch the LED
lens.
CONTINUED AIRWORTHINESS:
The anti-collision light is designed with 36 LEDs. The position light is
designed with 12 red or 10 green LEDs.
If any one bank fails, the flasher module should be checked. If the
module checks good, replace the lighthead. If any one LED fails, the
unit must be repaired or replaced.
Note: The system has an internal diagnostic circuit to detect failures.
After 20-25 seconds if a failure is detected the amber fault light will
illuminate.
INSTALLATION PROCEDURE:
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 90453( ) light assembly.
2. Connect the inputs according to the chart shown. Connections to
be in accordance with FAA approved methods.
3. Remove and discard the two #6 screws holding the shroud to the
unit. Carefully install the shroud as shown in Figure 1.
4. Using appropriate, approved hardware, 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. Check all avionics systems for interference from this installation.
6. A flight check should be performed by a properly certified pilot.
7. Update aircraft records, complete Form 337 and obtain FAA field
approval for installation, as necessary.
MADE IN THE U.S.A.
TSO-C30c
TYPE I & II;
APPROVED
TSO-C96a
CLASS II;
APPROVED (Shroud not shown)