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GENERAL INFORMATION AND SCOPE - TM-55-1510-222-CL_4
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS - TM-55-1510-222-CL_5
BEFORE EXTERIOR CHECK - TM-55-1510-222-CL_6
EXTERIOR CHECK - TM-55-1510-222-CL_7
LEFT MAIN LANDING GEAR.
FUSELAGE UNDERSIDE
RIGHT WING CENTER SECTION - TM-55-1510-222-CL_10
RIGHT MAIN LANDING GEAR
FUSELAGE RIGHT SIDE
EMPENNAGE
BEFORE STARTING ENGINES - TM-55-1510-222-CL_14
FIRST ENGINE START (BATTERY START) - TM-55-1510-222-CL_15
ABORT START PROCEDURE - TM-55-1510-222-CL_16
SECOND ENGINE START (GPU START) - TM-55-1510-222-CL_17
BEFORE TAXIING - TM-55-1510-222-CL_18
BEFORE TAKEOFF - TM-55-1510-222-CL_19
AFTER TAKEOFF - TM-55-1510-222-CL_20
BEFORE LANDING - TM-55-1510-222-CL_21
GO-AROUND - TM-55-1510-222-CL_22
BEFORE LEAVING AIRCRAFT - TM-55-1510-222-CL_23
15. Aircraft forms
EMERGENCY PROCEDURES - TM-55-1510-222-CL_25
ENGINE MALFUNCTION DURING FINAL APPROACH - TM-55-1510-222-CL_26
ENGINE RESTART DURING FLIGHT (USING STARTER) - TM-55-1510-222-CL_27
MAXIMUM GLIDE - TM-55-1510-222-CL_28
SINGLE ENGINE BEFORE LANDING
DUCT OVERTEMPERATURE CAUTION ANNUNCIATOR ILLUMINATED
PROPELLER FAILURE (OVER 1802 RPM) - TM-55-1510-222-CL_31
FIRE - TM-55-1510-222-CL_32
WING FIRE - TM-55-1510-222-CL_33
FUEL SYSTEM - TM-55-1510-222-CL_34
ELECTRICAL SYSTEM EMERGENCIES - TM-55-1510-222-CL_35
BATTERY CHARGE ANNUNCIATOR ILLUMINATED - TM-55-1510-222-CL_36
PERFORMANCE CHECKS - TM-55-1510-222-CL_37
STALL AND GEAR WARNING SYSTEM - TM-55-1510-222-CL_38
CABIN/CARGO DOORS - TM-55-1510-222-CL_39
AUTOMATIC FLIGHT CONTROL SYSTEM - TM-55-1510-222-CL_40
2. Autopilot.
3. Electric elevator trim - Check
AUTOFEATHER - TM-55-1510-222-CL_43
RUDDER BOOST - TM-55-1510-222-CL_44
ENGINE ANTI-ICE - TM-55-1510-222-CL_45
PNEUMATIC PRESSURE - TM-55-1510-222-CL_46
DEPARTURE BRIEFING - TM-55-1510-222-CL_47
ARRIVAL BRIEFING - TM-55-1510-222-CL_48
6. Landing performance data