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MODEL A650PG/PR SERIES WINGTIP STROBE
ANTI-COLLISION/POSITION LIGHT ASSEMBLY
A650 PG/PR Series wingtip with Anti-Collision & Forward Position lights
can be used to convert non-Whelen Aerospace Position lights into a
Position/Anti-Collision light system. The small size allows for mounting
into a wing tip enclosure. Available in 14 or 28 VDC and in a radio
shielded version. The forward position lamp is 26 watts.
Model A650PG/PR Specifications
Model
Part
Numbers
Number
A650PG1
01-0770054-00
A650PG2
01-0770054-01
A650PR1
01-0770054-02
A650PR2
01-0770054-03
A650PGD1
01-0770054-04
A650PGD2
01-0770054-05
A650PRD1
01-0770054-06
A650PRD2
01-0770054-07
A650PGDM
01-0770054-14
Radio Shielded (Molex)
A650PRDM
01-0770054-15
Installation
The A650 Series must be properly mounted to comply with FAR Part 91.205(c-
2) & (c-3). The light assembly must be mounted so that the light distribution
pattern is not obstructed by any parts of the aircraft. A limited amount of
obstruction is permitted (Ref. FAR Part 23.1401 for anti-collision lights, and
PAR 23.1387 for position lights).
The baseplate must be mounted parallel to the vertical and horizontal
centerlines of the aircraft to project the patterns properly. These
assemblies are interchangeable with the Grimes model A1285 position
light.
Mounting
1. If necessary, fabricate the mounting pattern using dimensions found in
Figure 16b (Note: A 1" diameter hole is needed for the connector to pass
through).
2. Make the necessary wiring connections using 18 gauge wire for the posi-
tion lights, and Whelen Aerospace 16 gauge 3/c cable for the strobe lights.
All connections must use FAA approved techniques.
3. Remove the (6-32 x .312) retainer mounting screw and retainer.
4. Attach the base assembly to the wingtip using (3) #6-32 counter-sunk
screws (unit may be sealed around periphery with RTV or equivalent).
5. Re-attach lens retainer.
Wiring
1. The strobe connector should plug into the Whelen Aerospace 16 gauge
inter-connecting cable, or a Whelen Aerospace strobe power supply.
Observe the following strobe color coding:
PIN 1 - RED (Anode)
PIN 2 - BLACK (Cathode)
PIN 3 - WHITE (Trigger)
Caution:
When pins 1 & 2 or pins 2 & 3 are reversed, the system will appear
to operate normally, however this condition will cause pre-mature flash tube
failure.
2. Connect the forward position light wires as follows, using 18 gauge
approved aviation wire or cable:
RED - +14 or +28 volts (depending on aircraft voltage)
BLACK - ( - ) Ground
44
Document #05131 Rev. E
Lens
Mount
Color
Position Green
Position Green
Standard Assembly
Position Red
Position Red
Position Green
Position Green
Radio Shielded
Position Red
Position Red
Position Green
Position Red
Nav Light
Approvals
Input Current /
Operational Voltage
2.0 Amps @ 14 VDC
1.0 Amps @ 28 VDC
2.0 Amps @ 14 VDC
1.0 Amps @ 28 VDC
2.0 Amps @ 14 VDC
FAA/PMA
1.0 Amps @ 28 VDC
2.0 Amps @ 14 VDC
1.0 Amps @ 28 VDC
1.0 Amps @ 28 VDC
Dimensions
1.75"
(19mm)
2.47"
(63mm)
1.08"
(27mm)
1.79"
(45mm)
Mounting Diagram
.50"
(13mm)
1.00"
(25mm)
"
.140 DIA. (3) MTG. HOLES
Peak Input
Weight
Current
Dependant on
strobe power
0.6 lbs.
supply used
3.84"
(98mm)
1.66"
(42mm)
.15"
(4mm)
1.35"
(34mm)
Pin 1 = RED (Anode)
Pin 2 = BLACK (Cathode)
Pin 3 = WHITE (Trigger)
RED - (+14/28 VDC)
BLACK - (-)GROUND
BOTTOM VIEW
.85"
(22mm)
.88"
1.75"
(22mm)
(44mm)
"
.280 DIA X 100° DIMPLE
(OPP. SIDE)
Length /
Width /
Height
3.84" L x
1.7" W x
2.4" H
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