Whelen 9048201 Manuel d'utilisateur télécharger pdf

Page 1

LED1

V+

LED2

LED3

V+

LED4

Anode

Cathode

Anode

Cathode

(Mating Connector 801-008-16M7-10SA)

Anti-Collision Light

Rear Position Light

Ground Recognition Light

Glenair 801-010-02M7-10PA

1.56

1.40

3.60

Drain

Hole

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: aviatio[email protected]om

Aviation

Installation Guide:

Aviation model 9048201

P/N 01-0790482-01

LED Tail Position /

Ground Recognition /

Anti-Collision Light Assembly

Form No.14330A (091411)

SPECIFICATIONS:

Nominal Operational Voltage: ...............................28 VDC

Input Current (with 7123403 Flasher):

LED Tail Position Light: ............................................0.25 Amps

LED Anti-Collision Light (Average):..........................0.53 Amps

LED Anti-Collision Light (Peak@0.25 sec.):.............2.8 Amps

LED Ground Recognition Light (Average):...............0.13 Amps

LED Ground Recognition Light (Peak@0.25 sec.):..0.7 Amps

Flashrate ..................................................................45± 5 per min.

EQUIPMENT LIMITATIONS:

An approved lighting system consists of three lights, one

located on the tail and 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. The light assembly must be connected to flasher

assembly, model 7123403.

The ground recognition light is a non-TSO function.

Certain types of installations may require additional testing.

CONTINUED AIRWORTHINESS:

The tail position light is designed with 4 LEDs. The anti-collision

light is designed with 28 LEDs. The ground recognition light is

designed with 4 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 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:

1. Using the mounting detail information on page 2 prepare

the aircraft for means to secure the LED light assembly.

Remove any existing mounting adapters.

2. Connect the light inputs according to the chart shown.

Connections to be in accordance with FAA approved

methods

3. Install the light assembly by securing to the aircraft

using appropriate, approved hardware. Refer to page 2.

Insure that all leads are clear of any obstructions, and

secure as required.

Insure that the gasket drain holes

are oriented as shown on Page 2.

4. When necessary, waterproof the light base to aircraft.

Apply single part silicone (RTV) or equivalent around

any open area where water could get in. Do not cover

the drain holes.

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 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.

MADE IN THE U.S.A.

TSO-C30c

TYPE III;

APPROVED

TSO-C96a

CLASS II;

APPROVED

1 2

Résumé du contenu

Page 1 - Aviation

Page 112345678910LED1V+LED2LED3V+LED4AnodeCathodeAnodeCathode(Mating Connector 801-008-16M7-10SA)Anti-Collision LightAnti-Collision LightAnti-Collisio

Page 2 - ITEM PART NUMBER DESCRIPTION

Page 212234567894131ITEM PART NUMBER DESCRIPTIONASS'Y, TAIL/AC MODEL 9048201RETAINERSCREW, 2-56 X 1/4 P82FHMS SSLENS, HARDCOATEDGASKET, LENSSCREW

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Whelen 9048201 Manuel d'utilisateur

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