Whelen Engineering Company WAT 9048200 Installation Manual

Phone: (860) 526-9504
Internet: www.flyWAT.com
Sales/Service e-mail: info@flyWAT.com
TSO-C30c TSO-C96a
TYPE III CLASS II
APPROVED APPROVED
WARNING: This product can expose you to chemicals including Methylene Chloride which is known to the State of California to cause cancer, and
Bisphenol A, which is known to the State of California to cause birth defects or other reproductive harm. For more information go to
www.P65Warnings.ca.gov.
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.
Certain types of installations may require additional testing.
AIRWORTHINESS LIMITATIONS: The Airworthiness
section is FAA approved and specifies inspections and other
maintenance required under §43.16 and §91.403 of the Federal
Aviation Regulations, unless an alternative program has been
approved.
No airworthiness limitations are associated with the installation of the
LED tail position/ground recognition/anti-collision light.
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. Note: To reduce eye
strain, use an optical filter (such as dark glasses or blue covering dome)
during LED inspection.
If any one LED fails, the unit must be repaired or replaced. Inspect the
lens, replace if there is excessive scratching, pitting, discoloration or
cracking. For additional lens maintenance detail see SAE ARP5637.
Note: The anti-collision light will automatically shut-off after 9-10
flashes if a failure is detected.
PERIODIC INSPECTIONS: An annual inspection shall be performed
unless the OEM specifies a shorter interval.
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. Remove 4 (2-56) screws to remove retainers. Carefully remove
lens. Remove 3 (4-40) screws to remove mounting plate.
CAUTION! Do not touch the LEDs with either fingers or sharp
©2010 Whelen Aerospace Technologies
Form No. 14329B (042919)
The conditions and tests required for TSO approval of this article are minimum performance standards.
Those installing this article either on or within a specific type or class of aircraft must determine that
the aircraft installation conditions are within the TSO standards which include any accepted integrated
non-TSO functions. TSO articles and any accepted integrated non-TSO function(s) must have separate
approval for installation in an aircraft. The article may be installed only according to 14 CFR part 43 or
the applicable airworthiness requirements.
Limitations
Page 1
Installation Guide/ICA:
Aviation model 9048200
LED Tail Position / Ground Recognition /
Anti-Collision Light Assembly
objects. This could soil and/or damage the LEDs and
affect the optical performance of the light.
4. Install the mounting baseplate by securing to the aircraft
using appropriate, approved hardware (refer to page 2).
Attach the light assembly using three screws. Insure
that all leads are clear of any obstructions, and secure
as required
5. Reinstall lens, confirm proper gasket fit and secure
using retainers and screws.
6. When necessary, waterproof the lightbase to aircraft.
Apply single-part Silicone (RTV) or equivalent around
any open area where water could get in. Do not cover
the drain holes.
7. Check all avionics systems for interference from this
installation.
8. A flight check should be performed by a properly
certified pilot.
9. If re quire d, upda te a ircra ft re cords utilizing FAA Fie ld
Approva l (Form 337) or e quiva le nt.
1.40
3.60
Glenair 801-010-02M7-10PA
1 LED1
2 V+
3 LED2
4 LED3
5 V+
6 LED4
7 Anode
8 Cathode
9 Anode
10 Cathode
(Mating Connector 801-008-16M7-10SA)
P/N 01-0790482-00
1.51
6-32
Grounding
Stud
.41
Drain
Hole
Anti-Collision Light
Anti-Collision Light
Anti-Collision Light
Anti-Collision Light
Anti-Collision Light
Anti-Collision Light
Rear Position Light
Rear Position Light
Ground Recognition Light
Ground Recognition Light