Whelen 9048200 User Manual

®
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: aviation@whelen.com
Installation Guide:
Aviation model 9048200
P/N 01-0790482-00 LED Tail Position /
Ground Recognition /
Anti-Collision Light Assembly
TSO-C30c TYPE III; APPROVED
TSO-C96a CLASS II; APPROVED
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 9­10 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. 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 LED lens surface with either fingers or sharp objects. This could soil and/or
Aviation
damage the lens and affect the optical performance of the LEDs.
©2010 Whelen Engineering Company Inc. Form No.14329A (091411)
MADE IN THE U.S.A.
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.
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 obstrtuctions, and secure as required.
oriented as shown on Page 2.
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. Update aircraft records, complete Form 337 and obtain FAA field approval for installation, as required.
1.40
Insure that the gasket drain holes are
3.60
Glenair 801-010-02M7-10PA
1
LED1
2
V+ LED2
3
LED3
4
V+
5
LED4
6
Anode
7
Cathode
8
Anode
9
Cathode
10
(Mating Connector 801-008-16M7-10SA)
6-32
Grounding
Stud
.41
1.51
Drain
Hole
ITEM PART NUMBER DESCRIPTION
1
QTY
01-0790482-00
ASS'Y, TAIL/AC MODEL 9048200
14-026116-04P
1
4
19-171306-000
2
2
2
3
1
4
1
5
3
6
1
7
1
68-3990484A30
38-0271320-00
14-040116-060
01-0290521-00
06-171345-100
SCREW, 2-56 X 1/4 PFHMS SS
RETAINER
LENS, HARDCOATED
GASKET, LENS
SCREW, 4-40 X 3/8 PFHMS
ASS'Y, LIGHTHEAD MODEL 9048200
BASE PLATE, MOUNTING MODEL 9048200
2
3
4
5
MOUNTING DETAIL
6
C
.600
L
.800
7
2.000
Ø 0.200
82° Counter-sink (typ)
Ø 0.750
.300
1.80
.65
Mounting Holes
3 x 0.177 for
8-32 Flat Head
Page 2
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