TM 1–1520–238–T–1
4–93
4–14 TADS – INTERACTIVE FD/LS CHECK
4–14
Personnel Required:
(2)
References:
TM 1-1270-476-T
TM 9-1230-476-20-1
TM 1-1270-476-20
TM 9-1230-476-20-2
TM 1-5855-265-T
TM 9-1270-476-30
Equipment Conditions:
Ref
Condition
TM 1-1270-476-T
Inspect optics and clean as
required
NOTE
If the AGPU is selected to provide power to the
aircraft, refer to paragraph 3–1. If the APU is
selected to provide power to the aircraft, refer to
paragraph 3–3.
1. Perform SYSTEMS – POWER–UP procedures in
accordance with paragraph 3–1.
2. Preset crew station switch/control settings as follows after
an aircraft power source is on–line.
CAUTION
When icing conditions exist, ensure that
TADS/PNVS gear teeth are free of ice, or
damage may result.
NOTE
If the FD/LS functional check does not locate
the faulty component or continues to indicate
the same component after it has been replaced
and the problem still exists refer to the PNVS
malfunction symptom index (TM 1-5855-265-T).
