TM 55-1510-221-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
BEFORE LANDING (CONT)
NOTE
During ILS approach, propellers should be
set at 1900 RPM to prevent ILS and glide-
slope needle interference.
4.
Flap switch - APPROACH, below
198 KIAS.
5.
Landing gear control switch - DN,
below 180 KIAS.
6.
Landing lights - As required.
7.
Brake deice - As required.
LANDING
NOTE
Maximum design sink rate below 13,500
pounds gross weight is 600 feet per minute
The maximum design sink rate above 13,
500 pounds gross weight is 500 feet per min-
ute
1. Autopilot and yaw damp - Disen-
gaged
2. Gear down indicator lights (3) -
Check Illuminated.
3. Propeller levers - HIGH RPM.
*4. Brake operation - Check during
landing roll for any tendency to
bleed down, drag after release or
indicate asymmetrical braking
power
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