TM-55-1510-220-CL Maintenance Test Flight Manual Army Model RC-12D

GENERAL INFORMATION AND SCOPE - TM-55-1510-220-CL_5
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS.
NORMAL PROCEDURES - TM-55-1510-220-CL_7
EXTERIOR CHECK - TM-55-1510-220-CL_8
CENTER SECTION, RIGHT SIDE
INTERIOR CHECK - TM-55-1510-220-CL_10
FIRST ENGINE START (BATTERY START) - TM-55-1510-220-CL_11
SECOND ENGINE START (BATTERY START) - TM-55-1510-220-CL_12
ABORT START - TM-55-1510-220-CL_13
SECOND ENGINE START (GPU START) - TM-55-1510-220-CL_14
BEFORE TAXIING - TM-55-1510-220-CL_15
BEFORE TAKEOFF - TM-55-1510-220-CL_16
AFTER TAKEOFF - TM-55-1510-220-CL_17
CRUISE - TM-55-1510-220-CL_18
DESCENT - MAX RATE (LANDING CONFIGURATION)
DESCENT-ARRIVAL - TM-55-1510-220-CL_20
BEFORE LANDING - TM-55-1510-220-CL_21
GO-AROUND - TM-55-1510-220-CL_22
ENGINE SHUTDOWN - TM-55-1510-220-CL_23
BEFORE LEAVING AIRCRAFT - TM-55-1510-220-CL_24
EMERGENCY PROCEDURES - TM-55-1510-220-CL_25
Engine Malfunction After Liftoff (Abort)
Engine Malfunction During Flight - TM-55-1510-220-CL_27
Engine Shutdown In Flight - TM-55-1510-220-CL_28
Engine Restart During Flight Using Starter
Engine Restart During Flight (Not Using Starter) - TM-55-1510-220-CL_30
Low Oil Pressure - TM-55-1510-220-CL_31
ICE VANE FAILURE - TM-55-1510-220-CL_32
LOSS OF PRESSURIZATION (ABOVE 10,000 FEET)
SINGLE-ENGINE BEFORE LANDING - TM-55-1510-220-CL_34
PROPELLER FAILURE (OVER 2080 RPM) - TM-55-1510-220-CL_35
FIRE - TM-55-1510-220-CL_36
Wing Fire - TM-55-1510-220-CL_37
FUEL SYSTEM - TM-55-1510-220-CL_38
TM-55-1510-220-CL_39
ELECTRICAL SYSTEM - TM-55-1510-220-CL_40
Circuit Breaker Tripped - TM-55-1510-220-CL_41
EMERGENCY DESCENT - TM-55-1510-220-CL_42
Gear-Up Landing (All Gear Up or Unlocked) - TM-55-1510-220-CL_43
Landing With Nose Gear Unsafe - TM-55-1510-220-CL_44
Landing With One Main Gear Unsafe - TM-55-1510-220-CL_45
CRACKED CABIN WINDOW - TM-55-1510-220-CL_46
FLIGHT CONTROLS MALFUNCTION - TM-55-1510-220-CL_47
BAILOUT - TM-55-1510-220-CL_48
PERFORMANCE CHECKS - TM-55-1510-220-CL_49
FIRE EXTINGUISHER PRESSURE - TM-55-1510-220-CL_50
FUEL PUMPS/CROSSFEED
STALL AND GEAR WARNING SYSTEM - TM-55-1510-220-CL_52
ELECTRIC ELEVATOR TRIM AND AUTOPILOT/FLIGHT DIRECTOR OPERATION
7. AIL HI TORQUE test switch
AUTOPILOT TRIM FAIL SYSTEM - TM-55-1510-220-CL_55
OVERSPEED GOVERNORS - TM-55-1510-220-CL_56
ICE VANES
PNEUMATIC PRESSURE - TM-55-1510-220-CL_58
CREW BRIEFING
DEPARTURE BRIEFING - TM-55-1510-220-CL_60
Approach procedure - Review.
Copilot duties - Review - TM-55-1510-220-CL_62

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