Whelen 9052001 User Manual

®
ENGINEERING COMPANY INC.
3.74
MFG LABEL
(28VDC) 18AWG 12” ±1.0”
(14VDC) 20AWG 6.0"±1.0"
WHITE (+) 28VDC
18AWG 12” ±1.0”
RED (+)14VDC
20AWG 6" ±1.0"
2.60
NOTE: RED LEDs TO THE FRONT
MADE IN THE U.S.A.
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:
Model 90520( )-series
Model(s) 9052001, 9052051
P/N:01-0790520-01,
01-0790520-51
LED Flashing Split Anti-Collision
Light Assembly
Aviation
TSO-C96a CLASS III APPROVED
OPERATING INSTRUCTIONS:
Operational Voltage: . . . . . . . . . . . 28 VDC nominal
Average Input Current:. . . . . . . . . 0.67 Amps
Pulse Input Current: . . . . . . . . . . . 3.0 Amps @ .3 Seconds
The Model 90520 series LED Flashing Split Anti-collision Light Assembly meets the requirements of FAR 91.205(c)(3).
CONTINUED AIRWORTHINESS: The 90520 series LED Flashing Split Anti-collision Light Assembly is designed with 4 vertical columns consisting of 4 red LEDs each and 4 vertical columns consisting of 3 white LEDs each. Should any one LED or any vertical column fail, the unit must be repaired or replaced. Inspect the lens and replace if there is excessive scratching, discoloration or cracking.
INSTALLATION PROCEDURES: The following information is to assist in the installation of a Whelen LED Flashing Split Anti-collision Light System.
1. The installation procedure described in the following text will be confined to a single light installation, but is identical for multiple light installations.
2. Using the “suggested mounting hole pattern” prepare the aircraft for means to secure the LED Flashing Split Anti-collision Light Assembly. Remove any existing mounting adapters.
3. 28 VDC (+) and (-) ground leads equipped with an appropriate sized breaker to be supplied to the LED Flashing Split Anti­collision Light Assembly System. Both leads must be connected by an approved FAA connection. Insure that the wire leads are clear of any obstructions and ty-wrap as required.
4. Install the light assembly by first removing the lens. Remove the adapter plate. Attach the adapter plate to the aircraft mounting holes. Refer to page 2. Reinstall the light assembly and lens.
5. All inverted (bottom) mounted units shall require waterproofing of the flasher base assembly to the aircraft. Note: Drill a 1/8” hole in the center of the lens for bottom mount units.
6. Check all avionics systems for interference from this installation.
7. A flight check should be performed by a properly certified pilot.
8. Update aircraft records, complete Form 337 and obtain FAA field approval for installation, as required.
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.
©2009 Whelen Engineering Company Inc. Form No.14290A (012712)
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ITEM PART NUMBER DESCRIPTION
MODEL 9052001 (IRIDITE / 28V)
ADAPTER PLATE, 8-HOLE
MODEL 9052051 (IRIDITE / 14V)
ASSY, 28V LED ANTI COLLISION LIGHT 90520
ASSY, 14V LED ANTI COLLISION LIGHT 90520
GASKET, LENS
LENS, CLEAR LED ANTI-COLLISION HARDCOAT
RETAINER, LENS IRIDITE
WASHER, #4 LOCK-SPRING MS35338-135
WASHER, #6 LOCK-SPRING MS35338-136
SCREW, 6-32 X 1/2 PPHMS SS MS51957-123
SCREW, 4-40 X 5/16 PPHMS MS51957-14
01-0790520-01
07-771051-100
01-0790520-51
01-0290522-00
01-0290522-50
38-0250885-00
68-4971082A30
19-171047-100
16-0050506135
16-0050506136
14-0050503123
14-0050505-14
QTY QTY
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213
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4 x #6-32 MTG holes equally spaced on a 1.625 bolt circle
4 x #6-32 MTG holes equally spaced on a 1.250 bolt circle
#6-32 Flat Head
100° Countersink
(typ)
Front
9052001 9052051 MOUNTING HOLE PATTERN
1.00”
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