TM 1-1510-262-10
$ FLAPS -- As required.
% CMWS -- SAFE/ARM as required.
9-15. SINGLE-ENGINE GO-AROUND.
The decision to go around must be made as early as possible. Elevator forces at the start of the go-around are very
high, and a considerable amount of rudder control will also be required at low airspeeds. Trim as required. If rudder
application is insuficient or applied too slowly, directional control cannot be maintained. If control dificulties are
experienced, reduce power on the operating engine. Ensure the aircraft will not touch the ground before retracting
the landing gear. Retract the laps only as safe airspeed permits. Perform single-engine go-around as follows:
1. POWER -- Maximum allowable.
2. LDG GEAR CONTROL handle -- UP.
# FLAPS -- UP.
4. Airspeed -- Vyse.
5. LANDING lights -- OFF.
^ CMWS -- SAFE/ARM as required.
NOTE
With propellers feathered, there is less drag and the aircraft will have a tendency to overshoot the
planned Touchdown point. When landing on rough terrain or unprepared surfaces, the landing
gear will absorb landing energy during touchdown, if extended.
9-16. TWO ENGINES INOPERATIVE -- OFF AIRFIELD LANDING.
Select landing gear up or down as best suits the conditions of the landing site. If gear-up, follow gear-up landing
procedure. If gear-down, make a normal touchdown and use brakes as required.
9-17. LOW OIL PRESSURE.
In the event of a low oil pressure indication, perform procedures as applicable:
1. Oil pressure below 90 PSI and above 60 PSI: Torque -- As required (54% maximum).
2. Oil pressure below 60 PSI: Perform engine shutdown in Flight Procedures, or land as soon as practi-
cable using minimum power to ensure safe arrival.
9-18. #1 OR #2 CHIP DETECTOR WARNING ANNUNCIATOR ILLUMINATED.
If the #1 CHIP DETR or #2 CHIP DETR warning annunciator illuminates, and safe single-engine light can be
maintained:
! Perform engine shutdown in Flight Procedures.
2. Land as soon as practicable.
9-19. PROPELLER FAILURE (OVER 1802 RPM).
If an overspeed condition occurs that cannot be controlled with the propeller lever or by reducing power, perform
the following:
1. POWER lever (affected engine) -- IDLE.
@ PROP lever(affected engine) -- FEATHER.
# MISSION CONTROLswitch -- OFF.
$ CONDITION lever -- As required.
5. TCAS -- Set TA.
^ Engine cleanup -- As required
9-9
Change 2
