Whelen 7114800 User Manual

ENGINEERINGCOMPANY,INC.

MS3470L16-8P

1.80

4.56

.080

.75

3.50

5.00

1.20

1.63

5XØ.156

THRU

3.830

1.915

4.270

2.500

WING

CHESTER,CONNECTICUT 06412-0684

BY:

MODEL 7114800

INPUT

OUTPUT

ENGINEERINGCOMPANY,INC.

TAIL

CHESTER,CONNECTICUT06412-0684

BY:

MODEL 7114801

INPUT

OUTPUT

MS3470L18-11S

7114801 Shown

for reference only

ANTI-COLL ANTI-COLL ANTI-COLL POSITION POSITION GROUND REF. GROUND REF. NO CONNECTION

ANTI-COLL ANTI-COLL ANTI-COLL POSITION POSITION NO CONNECTION NO CONNECTION NO CONNECTION

ANTI-COLL ANTI-COLL ANTI-COLL ANTI-COLL ANTI-COLL POSITION 1 POSITION 1 POSITION 2 POSITION 2 GROUND REF. GROUND REF.

ANTI-COLL ANTI-COLL ANTI-COLL ANTI-COLL ANTI-COLL ANTI-COLL POSITION POSITION NO CONNECTION NO CONNECTION NO CONNECTION

28V GND SYNC. S8V GND 28V GND

28V GND SYNC. S8V GND

ANODE CATH. 1 CATH. 2 CATH. 3 CATH. 4 ANODE CATH. ANODE CATH. 28V GND

ANODE CATH. 1 CATH. 2 CATH. 3 CATH. 4 CATH. 5 ANODE CATH.

A B C D E F G H

A B C F G D E J K H L

G A B C D E H J F K L

J1 SIGNAL J1 SIGNAL

Model 7114800 Model 7114801

J2 SIGNAL J2 SIGNAL

CONTACT CONTACT

ENGINEERING COMPANY INC.

MADE IN THE U.S.A.

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(s) 7114800, 7114801

P/N: 01-0771148-00

01-0771148-01

Flasher/Current Source Ass’y

SPECIFICATIONS:

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

Current Source Input Current:

LED Forward Position Light ...................................... 0.35 AMPS (each)

LED Tail Navigation Light .......................................... 0.25 AMPS

LED Wing Anti-Collision Light (Pulse@.25 Sec.)..... 4.0 AMPS

LED Wing Anti-Collision Light (Avg.) ....................... 0.75 AMPS

LED Tail Anti-Collision Light (Pulse@.25 Sec.) ....... 3.8 AMPS

LED Tail Anti-Collision Light (Avg.).......................... 0.71 AMPS

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

Total Weight ................................................................... 0.75 lbs.

Aviation

EQUIPMENT LIMITATIONS:

An approved forward anti-collision/position light system consists of at least 2 flasher/current source units, each connected to a LED anticollision lighthead, model 71184( ), and an LED position lighthead, models 7118201 (green) and 7118202 (red).

An approved tail anti-collision/navigation light system consists of at least one flasher/current source unit, connected to an LED anticollision and tail navigation lighthead, model 90354( ).

Certain types of installations may require additional testing.

CONTINUED AIRWORTHINESS:

The forward position light is designed with 6 LED’s. The forward anticollision light is designed with 24 LED’s. The tail navigation light is designed with 4 LED’s. The tail Anti-Collision light is designed with 30 LED’s. If any bank of LEDs fail, the lighthead module should be checked. If the module checks good, replace the flasher.

NOTE: To reduce eye strain use an optical filter such as dark glasses or a blue covering dome during LED inspection.

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

2. Attach the flasher using the (5) 0.156 dia. mounting holes.

3. Connect the anti-collision light inputs, position light inputs, and

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

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

manufacturer. Check that breakers are properly rated.

navigation light inputs according to the charts shown. Connect the cable harnesses from 7118201/7118202, and 71184( ) to 7114800 and connect the cable harnesses from 9035401 to

7114801. Connections to be in accordance with FAA approved methods.

approval for installation, as necessary

Page 1

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.