TM 55-1510-220-MTF
PROCEDURE
TROUBLESHOOTING
REFERENCE
NOTE
During approach, propellers should be set to 1900 RPM to
prevent glideslope interference (ILS approach), provide better
power response during approach, and minimize attitude
change when advancing propeller levers for landing.
4.
Flaps - APPROACH (below 202 KIAS).
5.
Gear - DN.
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 minute.
1.
Autopilot and yaw damp - Disengaged.
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
assymmetrical braking power.
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