GENERAL INFORMATION AND SCOPE - TM-55-1510-221-CL_6
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS - TM-55-1510-221-CL_7
BEFORE EXTERIOR CHECK - TM-55-1510-221-CL_8
LEFT MAIN LANDING GEAR - TM-55-1510-221-CL_9
INTERIOR CHECK - TM-55-1510-221-CL_10
FIRST ENGINE START (BATTERY START) - TM-55-1510-221-CL_11
SECOND ENGINE START (BATTERY START) - TM-55-1510-221-CL_12
FIRST ENGINE START (GPU START) - TM-55-1510-221-CL_13
BEFORE TAXING
ENGINE RUNUP - TM-55-1510-221-CL_15
LINE UP - TM-55-1510-221-CL_16
CRUISE - TM-55-1510-221-CL_17
DESCENT-ARRIVAL - TM-55-1510-221-CL_18
AFTER LANDING - TM-55-1510-221-CL_19
BEFORE LEAVING AIRCRAFT - TM-55-1510-221-CL_20
13. Aircraft forms
ENGINE MALFUNCTION
ENGINE MALFUNCTION AFTER LIFTOFF (FLIGHT CONTINUED)
ENGINE SHUTDOWN IN FLIGHT - TM-55-1510-221-CL_24
ENGINE RESTART DURING FLIGHT (NOT USING STARTER) - TM-55-1510-221-CL_25
LOW OIL PRESSURE - TM-55-1510-221-CL_26
ENGINE BLEED AIR SYSTEM FAILURE
LOSS OF PRESSURIZATION (ABOVE 10, 000 FEET)
SINGLE-ENGINE GO-AROUND - TM-55-1510-221-CL_29
ENGINE FIRE IN FLIGHT (IDENTIFIED) - TM-55-1510-221-CL_30
SMOKE AND FUME ELIMINATION - TM-55-1510-221-CL_31
FUEL CROSSFEED - TM-55-1510-221-CL_32
EXCESSIVE LOADMETER INDICATION (OVER 100%) - TM-55-1510-221-CL_33
LANDING EMERGENCIES - TM-55-1510-221-CL_34
LANDING WITH NOSE GEAR UNSAFE - TM-55-1510-221-CL_35
CRACKED WINDSHIELD - TM-55-1510-221-CL_36
DITCHING - TM-55-1510-221-CL_37
UNSCHEDULED RUDDER BOOST ACTIVATION
PERFORMANCE CHECKS - TM-55-1510-221-CL_39
EMERGENCY PROCEDURES - TM-55-1510-221-CL_40
OXYGEN SYSTEM - TM-55-1510-221-CL_41
ANNUNCIATOR PANELS TEST
AC/DC POWER
The elevator trim system
PROPELLER MANUAL FEATHERING
AUTOFEATHER - TM-55-1510-221-CL_46
PRIMARY GOVERNORS - TM-55-1510-221-CL_47
PNEUMATIC PRESSURE - TM-55-1510-221-CL_48
DEPARTURE BRIEFING - TM-55-1510-221-CL_49
PPC - REVIEW
COPILOT DUTIES - REVIEW - TM-55-1510-221-CL_51
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS - TM-55-1510-221-CL_7
BEFORE EXTERIOR CHECK - TM-55-1510-221-CL_8
LEFT MAIN LANDING GEAR - TM-55-1510-221-CL_9
INTERIOR CHECK - TM-55-1510-221-CL_10
FIRST ENGINE START (BATTERY START) - TM-55-1510-221-CL_11
SECOND ENGINE START (BATTERY START) - TM-55-1510-221-CL_12
FIRST ENGINE START (GPU START) - TM-55-1510-221-CL_13
BEFORE TAXING
ENGINE RUNUP - TM-55-1510-221-CL_15
LINE UP - TM-55-1510-221-CL_16
CRUISE - TM-55-1510-221-CL_17
DESCENT-ARRIVAL - TM-55-1510-221-CL_18
AFTER LANDING - TM-55-1510-221-CL_19
BEFORE LEAVING AIRCRAFT - TM-55-1510-221-CL_20
13. Aircraft forms
ENGINE MALFUNCTION
ENGINE MALFUNCTION AFTER LIFTOFF (FLIGHT CONTINUED)
ENGINE SHUTDOWN IN FLIGHT - TM-55-1510-221-CL_24
ENGINE RESTART DURING FLIGHT (NOT USING STARTER) - TM-55-1510-221-CL_25
LOW OIL PRESSURE - TM-55-1510-221-CL_26
ENGINE BLEED AIR SYSTEM FAILURE
LOSS OF PRESSURIZATION (ABOVE 10, 000 FEET)
SINGLE-ENGINE GO-AROUND - TM-55-1510-221-CL_29
ENGINE FIRE IN FLIGHT (IDENTIFIED) - TM-55-1510-221-CL_30
SMOKE AND FUME ELIMINATION - TM-55-1510-221-CL_31
FUEL CROSSFEED - TM-55-1510-221-CL_32
EXCESSIVE LOADMETER INDICATION (OVER 100%) - TM-55-1510-221-CL_33
LANDING EMERGENCIES - TM-55-1510-221-CL_34
LANDING WITH NOSE GEAR UNSAFE - TM-55-1510-221-CL_35
CRACKED WINDSHIELD - TM-55-1510-221-CL_36
DITCHING - TM-55-1510-221-CL_37
UNSCHEDULED RUDDER BOOST ACTIVATION
PERFORMANCE CHECKS - TM-55-1510-221-CL_39
EMERGENCY PROCEDURES - TM-55-1510-221-CL_40
OXYGEN SYSTEM - TM-55-1510-221-CL_41
ANNUNCIATOR PANELS TEST
AC/DC POWER
The elevator trim system
PROPELLER MANUAL FEATHERING
AUTOFEATHER - TM-55-1510-221-CL_46
PRIMARY GOVERNORS - TM-55-1510-221-CL_47
PNEUMATIC PRESSURE - TM-55-1510-221-CL_48
DEPARTURE BRIEFING - TM-55-1510-221-CL_49
PPC - REVIEW
COPILOT DUTIES - REVIEW - TM-55-1510-221-CL_51
