®
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 9020609,9020610
P/N 01-0790206-09, 01-0790206-10
Anti-Collision/LED Position Light Ass’y
TSO-C30c
& TSO-C96a
TYPES I & II
APPROVED
MADE IN THE U.S.A.
SPECIFICATIONS:
Nominal Operational Voltage:........28 VDC
Input Current:..................................0.3 AMP
Total Weight... ... ................ ... ............1.97 lbs.
EQUIPMENT LIMITATIONS:
An approved Anti-Collision / Position System consists
of assembly 90206( ) and strobe power supply
9010104, located on each wi ngtip.
CONTINUED AIRWORTHINESS:
The LED position light i s designed with 5 LED’s. If any
one LED fails, the unit must be repaired or replaced.
Inspect the lens for excessive scratches or pitting.
Replace if necess ary.
INSTALLATION PROCEDURES:
The following info rmation is to assist you in in stalling a
Whelen Anti-Collision / Position light system.
1. Choose the appropriate Model 90206 - ( )
replacement light assembly.
2. The installation procedure described in the
following text will be confined to a single light
installation, but is identical for multiple light
installation.
3. Remove old anti-collision light, locate and record
existing +28 VDC and (-) ground position and
output connector from power supply.
4. Use existing mounting holes and hardware.
5. Connect leads from light assembly in recorded
manner and lead from light to power supply.
6. Breaker
Requirements
Make sure existing system is equipped with an
appropriate sized breaker.
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 sep arate approval for
installation in aircraft. The article may be installed only if
performed under 14 CFR part 43 or the applicable
airworthiness requirements.
7. Install light assembly and insure that all leads are
clear of any obstructions and ty-rap as required.
Secure light assembly, use lock washers and/or
thread lock, on all threaded fasteners.
8. Check all avionics systems for interference from
this installation.
9. A flight check should be performed by a properly
certified pilot.
10. When necessary, waterproof the light assembly to
aircraft. Apply single part silicone (RTV) or
equivalent around any open area where water
could get in.
11. Update aircraft records and complete Form 337.
12. Obtain FAA field approval for installation.
10.63
.51
3.06
1.97
3.75
1.6
22”
APPROX.
FORWARD POSITION LIGHT
BLACK (GROUND)
WHITE (POSITIVE)
9.375
MS 3106F-10SL-3P
3 PIN CONNECTOR
26”
APPROX.
LENS RETAINER
MOUNTING SCREW
(2) PLACES
A - ANODE
B - TRIGGER
C - CATHODE
WINGTIP
SKIN
EXISTING
MTG
PLATE
Aviation
©2006 Whelen Engineering Company Inc.
Form No.14022 (021406)
Page 1
LIGHT ASSY, POS/ANTI COLL - RIGHT (GREEN LED)
LIGHT ASSY, POS/ANTI COLL - LEFT (RED LED)
01-0790206-09
BASEPLATE ASSY, WINGTIP LIGHT
SCREW,6-32 x 3/4 PFHSS (MS51959-32)
STROBE ASSY - WINGTIP LIGHT
01-0790206-10
06-170737-000
14-0050508-32
02-0270603-00
SCREW,6-32 x ½ PPHMS (MS51957-30)
GASKET, LENS
LENS, GLASS (RFI COATED)
RETAINER, MACHINED/POLISHED w/SEAL
7097002 RED LED FWD POSITION LIGHT
7097001 GREEN LED FWD POSITION LIGHT
38-0270590-00
14-0050503-30
68-4170665-34
19-190314-00S
01-0770970-02
01-0770970-01
SCREW,6-32 x 7/8 PPHMS (MS51957-33)
SCREW,10-32 x 3/4 PFHMS
GROMMET EDGING (PANDUIT #GEE62FR-C)
14-0050503-33
14-0050619-67
21-5030903-01
7
11
6
NOTE:
Mounting screws to be tightened evenly
to a maximum of 13 in./lbs. of torque.
*IMPORTANT* Screws should be alternately
tightened until the final torque value has
been achieved.
5
10
4
3
ITEM PART NUMBER DESCRIPTION
QTY QTY
9.93
.750
3.434
1.104 R.
111
1.00 DIA
2
22
(2) HOLES
19.16 R.
7.69 R.
3
4
1
1
1
1
6
5
511
511
7
1
11
121
10
2
3
3
1
1
2
NOTE:
Shield Ground: To be secured
by mounting screw (#7)
9
8
5
2
1
.47 R.
2.00
MIN. OPENING
REQUIRED IN WINGTIP
(LEFT SHOWN)
FLAT
4.140 R.
1.04
2.70
1.14
4.80
7.60
MOUNTING CONFIGURATION
NOTE: ON RIGHT SIDE FORWARD MTG HOLE ON BOTTOM.
14
4
12
REF.
WINGTIP SECTION
8 11
2
# 6-32
(FOR BASE)
(4) MOUNTING HOLES
.625
2.44
MS51959-32 (#4 - qty. 2)
MS51957-33 (#12 - qty. 2)
NOTE:
Grommet Edging (#14) and
Screws:
To be packaged in a plastic
bag and stapled to cable.
.57 R.
Page 2