Whelen Engineering Company WAT OR5001V Installation And Service Manual page 56

MODEL A600 PG/PR SERIES INSTALLATION
A600 PG/PR series wing tip anti-collision, forward position and tail
position lights, all in one compact unit. Tail position light eliminates
the need for a tail mounted position light. Available in 14 or 28 VDC
and in a radio-shielded version. The forward position lamp is 26
watts and the taillight lamp is 25 watts.
Model A600 PG/PR Specifications
Model Part
Mount
Numbers Number
A600PG1 01-0790006-00 Position Green
A600PG2 01-0790006-01 Position Green
A600PR1 01-0790006-02 Position Red
A600PR2 01-0790006-03 Position Red
Position Green,
A600PGD1 01-0790006-04
Radio-shielded
Position Green,
A600PGD2 01-0790006-05
Radio-shielded
Position Red,
A600PRD1 01-0790006-06
Radio-shielded
Position Red,
A600PRD2 01-0790006-07
Radio-shielded
Operation
Wingtip anti-collision, forward position, and tail position lights,
all in one compact unit. Tail position light eliminates the need for
a tail mounted position light. Available in 14 or 28 volts, and in a
radio-shielded version. The forward position lamp is 26 watts and
the taillight lamp is 25 watts.
Installation
The A600 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 convergence of the two wingtip tail position must occur within 1200 feet
directly behind the aircraft to comply with field of coverage requirements. The
baseplate must be mounted parallel to the vertical & horizontal centerlines of the
aircraft to project the patterns properly.
Mounting
1. If necessary, fabricate the mounting pattern using dimensions found in
Figure 40a.
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 two (6-32 x .312) retainer mounting screws 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 (see Figure 48a).
1.00"
(25mm)
.50"
(13mm)
.88"
(22mm)
Wiring
1. The strobe connector should plug into the Whelen Aerospace interconnect-
ing cable, or a Whelen Aerospace strobe power supply.
56
Document #05131 Rev. E
LENS /
Approvals
Color
Green
Red
FAA TSO-C30b
/ FAA/PMA
Green
Red
.140" (4mm) DIA. (3)
MOUNTING HOLES
FOR #6-32 SCREWS
1.75"
(44mm)
Nav Light Input Current Strobe Input
/ Operational Voltage Current
4.0 amps @ 14 VDC
2.0 amps @ 28 VDC
4.0 amps @ 14 VDC
2.0 amps @ 28 VDC
Dependant on
strobe
power supply
4.0 amps @ 14 VDC
used
2.0 amps @ 28 VDC
4.0 amps @ 14 VDC
2.0 amps @ 28 VDC
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:
RED - +14 or +28 volts (depending on aircraft voltage)
BLACK - ( - ) Ground
3. The tail position light has no polarity, as noted by both wires being BLUE.
Connect one BLUE wire to +14 or +28 volts (depending on aircraft voltage).
Connect the other BLUE wire to ground (see Figure 48b).
Dimensions
1.83"
(mm)
2.46"
(62mm)
110°
1.08"
(27mm)
1.79"
(45mm)
1.35"
(34mm)
DIA.
Exposed Height /
Weight
Length / Width
2.4" (61mm /
0.8 lbs. (363gm) 5.63" (143mm) /
1.7" (43mm)
5.63"
(143mm)
1.66"
(42mm)
70°
.15" (4mm)
TAIL LIGHT WIRES(BLUE)
NO POLARITY
POS 3 - WHITE(TRIGGER)
POS 2 - BLACK(CATHODE)
POS 1 - RED(ANODE)
RED (+14 or +28VDC)
BLACK (-) GROUND
18 AWG TEFLON
LEAD LENGTH 6.00"±1.00"