Whelen 7090000 Manuel d'utilisateur télécharger pdf

Page 1

Teflon Tube 18GA

(Pressure Venting)

4.04±.06

MFG Label

3.66

(+)28VDC White 18GA

Teflon Wire 18”LG

(-)Ground Black 18GA

Teflon Wire 18”LG

(+)14VDC Red 18GA

Teflon Wire 18”LG

ENGINEERING COMPANY INC.

Route 145, Winthrop Road,

Chester, Connecticut 06412

Phone: (860) 526-9504

Fax: (860) 526-2009

Internet: www.whelen.com

Sales/Service e-mail: aviation@whelen.com

Aviation

Installation Guide:

Model 70900( )-series

Model 7090000

7090001

P/N:01-0770900-00

01-0770900-01

LED Flashing Anti-Collision

Light Assembly

Form No.13826D (111505)

OPERATING INSTRUCTIONS:

Operational Voltage: . . . . . . . . . . . 14 / 28 VDC nominal

Average Input Current:. . . . . . . . . 0.85 / 0.425 Amps

Peak Input Current:. . . . . . . . . . . . 4.5 / 2.25 Amps @ .25 Seconds

The Model 70900 series LED anti-collision light assembly meets the

requirements of FAR 91.205(c)(3).

CONTINUED AIRWORTHINESS: The 70900 series LED anti-collision light

assembly is designed with 10 vertical columns consisting of 3 LEDs each.

Should any one LED or any vertical column fail, the unit must be repaired or

replaced.

INSTALLATION PROCEDURES: The following information is to assist in

the installation of a Whelen LED Flashing 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 Anti-collision Light assembly.

3. 14 / 28 VDC (+) and (-) ground leads equipped with an appropriate

sized breaker to be supplied to the LED Flashing Anti-collision Light

Assembly System. Both leads must be connected by an approved FAA

connection. Insure that the wire leads and the pressure venting tube

are all clear of any obstructions and ty-wrap as required. The pressure

venting tube may be trimmed to minimum length of 1” from base.

4. Install the light assembly by first removing the lens. Insert the

appropriate hardware through the counter-bored holes, secure the

assembly and re-install the lens screws with 5-7 in./lbs. of torque.

5. Check all avionics systems for interference from this installation.

6. A flight check should be performed by a properly certified pilot.

7. All inverted (bottom) mounted units shall require waterproofing of the

mounting hardware. An application of single-part silicone (RTV) or

equivalent applied over top of the mounting hardware, after installation,

is recommended. Reference page 2 for an illustration. Inverted and/or

standard mounted units, when necessary, may require waterproofing

around any open area where water could get in. Specifically, the lens to

the flasher base assembly, and the flasher base assembly to the

aircraft. Note: It is permissable to drill a 1/8” hole in the center of the

lens for bottom mount units.

8. Update aircraft records, complete Form 337 and obtain FAA field

approval for installation.

TSO-C96a CLASS III

APPROVED

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.

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Résumé du contenu

Page 1 - Aviation

Page 1Teflon Tube 18GA(Pressure Venting)or4.04±.06MFG Label3.66(+)28VDC White 18GATeflon Wire 18”LG(-)Ground Black 18GATeflon Wire 18”LG(+)14VDC Red 1

Page 2 - 1.00” Clearance for wires

Page 2LensP/N: 68-4990257-30ScrewP/N: 14-062216-05MLED ModuleP/N : 01-0270918-00(28V): 01-0270918-02(14V)GasketP/N: 38-0250843-00Model70900007090001Pa

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Whelen 7090000 Manuel d'utilisateur

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