Whelen 7112000 User Manual

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

Installation Guide:

Aviation model 7112000

P/N 01-0771120-00

Flasher/Current Source Ass’y

TSO-C30c TYPES I, II & III / TSO-C96a CLASS II APPROVED

MADE IN THE U.S.A.

SPECIFICATIONS:

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

Current Source Input Current:

LED Forward Position Light ........................................... 0.25 AMPS

LED Tail Position Light.................................................... 0.25 AMPS

LED Anti-Collision Light (Peak@.25 Sec.)..................... 4.5 AMPS

LED Anti-Collision Light (Avg.) ...................................... 0.85 AMPS

Flashrate.............................................................................. 45 ±5 Per. Min.

Total Weight ........................................................................ 0.95 lbs.

EQUIPMENT LIMITATIONS:

An approved Anti-Collision / Position Light System consists of at least 2 flasher/current source units, each connected to a LED anti-collision and position light lighthead model 90325( ), one Red and one Green.

CONTINUED AIRWORTHINESS:

The forward position light is designed with 6 LED’s. The rear position light is designed with 3 LED’s. The Anti-Collision light is designed with 36 LED’s. If any bank of LEDs fail, the lighthead module should be checked. If the module checks good, replace the flasher.

Note: The anti-collision light will automatically shut-off after 9-10 flashes if a failure is detected.

INSTALLATION PROCEDURES:

1. Consider areas or locations designated by the aircraft manufacturer. Check that breakers are properly rated.

2. Attach the flasher using the (4) 0.188 dia. mounting holes.

3. Connect the anti-collision inputs and the position light inputs according to the chart shown. Connect the cable from 90325( ) to the flasher position light. Connections to be in accordance with FAA approved methods.

4. Check all avionic systems for interference from the installation

5. A flight check should be performed by a certified pilot

6. Update aircraft records, complete form 337 and obtain FAA field approval for installation, as necessary

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.

Output Connector

MS3470L12-10S A LED1 B +28V C LED2 D LED3 E Anode F G H J K

5.60

Anti Collision Light Anti Collision Light Anti Collision Light Anti Collision Light Rear Position Light Anti Collision Light

LED4

Forward Position Light

Anode

Position Lights

Common

Anti Collision Light

LED5

Anti Collision Light

LED6

2.53

20 GA WHITE WIRE +28V 20 GA BLACK WIRE Ground

4 x Ø0.188

Mounting Holes

2.80

2.55

5.10

WIRE 7.00 ±1.00 LG

2.06

1.812

PIONEERSIN SAFETY SIGNALS

ENGINEERINGCOMPANY, INC.

Anti-Collision Input Connector

MS 3102E10SL-3P A +28V B Ground C SYNC

4.63

Position Lights Input Wires

4.13

3.625

Aviation

For warranty information regarding this product, visit www.whelen.com/warranty

Page 1