GENERAL INFORMATION AND SCOPE
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS - TM-1-1520-240-CL_3
BEFORE EXTERIOR CHECK
AFT CABIN
RIGHT CABIN - TM-1-1520-240-CL_6
TOP OF FUSELAGE - TM-1-1520-240-CL_7
WALK AROUND CHECK AND SECURITY BRIEF
STARTING ENGINES - TM-1-1520-240-CL_9
STARTING ENGINES -cont
ENGINE GROUND OPERATION
BEFORE HOVER
BEFORE LANDING - TM-1-1520-240-CL_13
ENGINE SHUTDOWN -cont
BEFORE LEAVING HELICOPTER - TM-1-1520-240-CL_15
ENGINE DUAL ENGINE FAILURE
Normal Engine Beep Trim System Failure (High Side) or N2 Governor Failure
Engine Fluctuations without FADEC 1/2 Light
Engine Shutdown Complete Electrical Failure
ROTOR, TRANSMISSION, AND DRIVE SYSTEMS
LEFT or RIGHT
FIRE
Engine or Fuselage Fire Flight
FUEL SYSTEM
ELECTRICAL SYSTEM
Electrical power is restored (from either generator)
HYDRAULIC
LANDING AND DITCHING
FLIGHT CONTROLS
MISSION EQUIPMENT
HOIST
FARE Pump Failure During Ground FARE Refueling Operation
DETAILED PROCEDURES
HYDRAULIC COMPARTMENTS CHECKS
OVERHEAD SWITCHES AND CONTROL PANELS
APU START
FLIGHT CONTROL TRAVEL AND HYDRAULICS (FOR THUR FLIGHTS PERFORM STEPS 2 THUR 5 IN BOTH)
ENGINE START (EITHER ENGINE)
FUEL PUMP AND XFEED CHECK
FADEC Reversionary system
KIT1C is not installed or keyed
Engine Fire Extinguisher Bottles Pressures
Figure P-1. Flight Control, Utility System, Power Steering, and Signal Accumulators Precharge Limits
Figure P-2. APU Start Accumulator Precharge Limits
Figure FO-1. Steady Windspeed - Knots (Chart A)
Figure FO-2. Steady Windspeed - Knots (Chart B)
REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS - TM-1-1520-240-CL_3
BEFORE EXTERIOR CHECK
AFT CABIN
RIGHT CABIN - TM-1-1520-240-CL_6
TOP OF FUSELAGE - TM-1-1520-240-CL_7
WALK AROUND CHECK AND SECURITY BRIEF
STARTING ENGINES - TM-1-1520-240-CL_9
STARTING ENGINES -cont
ENGINE GROUND OPERATION
BEFORE HOVER
BEFORE LANDING - TM-1-1520-240-CL_13
ENGINE SHUTDOWN -cont
BEFORE LEAVING HELICOPTER - TM-1-1520-240-CL_15
ENGINE DUAL ENGINE FAILURE
Normal Engine Beep Trim System Failure (High Side) or N2 Governor Failure
Engine Fluctuations without FADEC 1/2 Light
Engine Shutdown Complete Electrical Failure
ROTOR, TRANSMISSION, AND DRIVE SYSTEMS
LEFT or RIGHT
FIRE
Engine or Fuselage Fire Flight
FUEL SYSTEM
ELECTRICAL SYSTEM
Electrical power is restored (from either generator)
HYDRAULIC
LANDING AND DITCHING
FLIGHT CONTROLS
MISSION EQUIPMENT
HOIST
FARE Pump Failure During Ground FARE Refueling Operation
DETAILED PROCEDURES
HYDRAULIC COMPARTMENTS CHECKS
OVERHEAD SWITCHES AND CONTROL PANELS
APU START
FLIGHT CONTROL TRAVEL AND HYDRAULICS (FOR THUR FLIGHTS PERFORM STEPS 2 THUR 5 IN BOTH)
ENGINE START (EITHER ENGINE)
FUEL PUMP AND XFEED CHECK
FADEC Reversionary system
KIT1C is not installed or keyed
Engine Fire Extinguisher Bottles Pressures
Figure P-1. Flight Control, Utility System, Power Steering, and Signal Accumulators Precharge Limits
Figure P-2. APU Start Accumulator Precharge Limits
Figure FO-1. Steady Windspeed - Knots (Chart A)
Figure FO-2. Steady Windspeed - Knots (Chart B)
