TM-1-1520-240-10 Army CH-47D Heilcopter (EIC:RCD) Manual

CHAPTER 1 INTRODUCTION
1-1-15.  Series and Effectivity Codes
CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION
Figure  2-1-1.  Principal Dimensions Diagram
Figure  2-1-2.  Turning Radii
Figure  2-1-3.  Cockpit and Controls
2-1-6.  STEERING CONTROL Panel
2-1-10.  Brakes and Steering Isolation Switch.
Figure  2-1-5.  Center Console With XM-130 Countermeasures (Typical) (Sheet 1 of 2)
Figure  2-1-5. Center Console With AN/ALE-47 Countermeasures (Typical) (Sheet 2 of 2)
Figure  2-1-6.  Canted Console (Typical)
Figure  2-1-7.  Copilot Instrument Panel (Typical) 712
Figure  2-1-8.  Center Instrument Panel (Typical) 712
Figure  2-1-9.  Pilot Instrument Panel (Typical) 712
Figure  2-1-10.  Overhead Switch Panel 712
Figure  2-1-11.  Copilot Instrument Panel 714A
Figure  2-1-12.  Center Instrument Panel 714A
Figure  2-1-13.  Pilot Instrument Panel 714A
Figure  2-1-14.  Overhead Switch Panel 714A
Figure  2-1-15.  Armored Seats
SECTION  II.  EMERGENCY EQUIPMENT
Figure  2-2-1.  Engine Compartment Fire Detection and Extinguishing System (Typical)
2-2-4.  AGENT DISCH Switch
2-2-8.  TROOP WARN Panel
SECTION  III.  ENGINES AND RELATED SYSTEMS
2-3-8.  ENG COND Levers 712
2-3-10.  EMERG ENG TRIM Panel 712
Figure  2-3-2.  Emergency Engine Trim Panel
Figure  2-3-4.  ENGINE START PANEL 712
2-3-24.  Engine CAUTION/ADVISORY Capsules.
2-3-29.  FADEC Description
2-3-32.  FADEC Panel. 714A
Figure  2-3-6.  FADEC Panel 714A
2-3-37.  Starting in Reversionary Mode. 714A
Table  2-3-1. T55-GA-714A DECU BIT Fault Code List/Matrix
T55-GA-714A DECU BIT Fault Code List/Matrix (Continued) - TM-1-1520-240-10_49
T55-GA-714A DECU BIT Fault Code List/Matrix (Continued) - TM-1-1520-240-10_50
T55-GA-714A DECU BIT Fault Code List/Matrix (Continued) - TM-1-1520-240-10_51
T55-GA-714A DECU BIT Fault Code List/Matrix (Continued) - TM-1-1520-240-10_52
2-3-41.  Engine Air Particle Separator (EAPS)
2-3-45.  EAPS Switches
Figure  2-3-9.  EAPS 1 Shown With Bypass Doors Open
Figure  2-3-10.  EAPS Control Boxes
SECTION  IV.  FUEL SYSTEM
2-4-5.  Fuel Valves
2-4-7.  Fuel Quantity Indicator and Selector.
Figure  2-4-5.  Fuel Flow Indicator
2-4-16.  REFUEL VALVE POSN Indicating Lights.
Figure  2-4-6.  Pressure Refueling Station
SECTION  V.  FLIGHT CONTROLS
2-5-2.  THRUST CONT Lever
Figure  2-5-2.  Cyclic Stick Grip
2-5-11.  Altitude Hold
Figure  2-5-3.  Advanced Flight Control System Panel
2-5-18.  Command Select Switch.
SECTION  VI.  HYDRAULIC SYSTEMS
2-6-5.  PWR XFER Switches.
2-6-11.  EMERG   UTIL   PRESS   Controllable   Check Valve.
SECTION  VII.  POWER TRAIN SYSTEM
Figure  2-7-1.  Transmission Main Oil Pressure Indicator and Selector Switch
Figure  2-7-2.  Transmission Main Oil Temperature Switch and Indicator
2-7-12.  Transmission Chip Detectors Fuzz Burn- Off
SECTION  VIII.  ROTOR SYSTEM
SECTION  IX.  UTILITY SYSTEMS
Figure  2-9-2.  Maintenance Panel
2-9-7.  GROUND CONTACT Section.
2-9-14.  AC Cabin Utility Receptacles
SECTION  X.  HEATING, VENTILATION, COOLING, AND ENVIRONMENTAL CONTROL SYSTEMS
2-10-4.  Air Control Handles.
SECTION  XI.  ELECTRICAL POWER SUPPLY AND DISTRIBUTION SYSTEMS
Figure  2-11-2.  Electrical Power Panel
2-11-7.  BATT Switch.
SECTION  XII.  AUXILIARY POWER UNIT
Figure  2-12-2.  Auxiliary Power Unit
SECTION XIII. LIGHTING
2-13-4.  FORM Light Switches
2-13-10.  Overhead Switch Panel Lights.
Figure  2-13-2.  Cockpit Lighting and Control
2-13-13.  PLT and CPLT INST Switches.
2-13-22.  FLOOD SWITCHES
Figure  2-13-3.  Emergency Exit Light
Figure  2-13-4.  Cabin Lighting and Controls
2-13-28.  Forward   Transmission   Oil   Level   Check Lights
SECTION  XIV.  FLIGHT INSTRUMENTS
Figure  2-14-2.  AIMS Altimeter
Figure  2-14-3.  Radar Altimeter (AN/APN-209)
2-14-11.  Normal Operation - Radar Altimeter (AN/ APN-209A)
2-14-13.  Controls   and   Function,   Radar   Altime- ter(AN/APN-209(V)) (AVWS)
2-14-16.  Attitude Indicator
2-14-21.  CHRONOMETER.
Figure  2-14-5.  Master Caution System 712
Table  2-14-1.   Master Caution Panel Capsules 712
2-14-29.  MASTER CAUTION Lights.
Table  2-14-2   Master Caution/Advisory Panel Capsules 714A
Master Caution/Advisory Panel Capsules 714A   (Continued)
SECTION  XV.  SERVICING, PARKING, AND MOORING
2-15-6.  Single-Point Pressure Refueling
m.   APU Start
Figure  2-15-1.  No Step, No Handhold, and Walkway Areas
Figure  2-15-2.  Servicing Diagram (Sheet 1 of 4)
Figure  2-15-2. Servicing Diagram (Sheet 2 of 4)
Figure  2-15-2. Servicing Diagram (Sheet 3 of 4)
Figure  2-15-2. Servicing Diagram (Sheet 4 of 4)
Table  2-15-1. Servicing
Table  2-15-2. Equivalent Oils and Hydraulic Fluids
Table  2-15-3. JP-4 Equivalent Fuel
Table  2-15-4. JP-5 and JP-8 Equivalent Fuel
2-15-9.  ERFS II Refueling
2-15-13.  Engine Oil System.
2-15-15.  Transmission Oil System
2-15-22.  Parking
Figure  2-15-3.  Accumulators Precharge Limits
2-15-24.  Protective Covers
Figure  2-15-4.  Protective Covers
Figure  2-15-5.  EAPS Protective Covers
Figure  2-15-6.  Installation of Helicopter Security Devises (Typical)
CHAPTER 3 AVIONICS
Table  3-1-1.   Communications/Navigation Equipment
SECTION II. COMMUNICATIONS
Figure  3-2-1.  Interphone Stations
Figure  3-2-2.  Interphone Control (C-6533/ARC)
Figure  3-2-3.  Antenna Locations
Table  3-2-1.   Have Quick II Additional Functions Frequency and Use
Figure  3-2-4.  UHF-AM Have Quick II Radio (An/ARC-164)
3-2-11.  Normal Operation UHF-AM Have Quick II Radio
b.  Operate/Verify Modes
3-2-13.  VHF AM/FM Radio Sets (AN/ARC-186)
3-2-14.  Controls and Function, VHF AM/FM Radio Set.
Figure  3-2-5.  VHF AM/FM Radio Set (AN/ARC-186)
3-2-17.  Controls    and    Functions    VHF/FM    Radio Set.
Figure  3-2-6.  VHF/FM Radio Set (AN/ARC-201)
3-2-19.  Controls and Functions
d.  Manual remote keying procedures
3-2-21.  HF Radio Set (AN/ARC-220)
3-2-23.  Display Lines, HF Radio Set (AN/ARC-220).
3-2-24.  Operating Modes/Functions, HF Radio Set (AN/ARC-220)
3-2-24.  Operating Modes/Functions, HF Radio Set (AN/ARC-220) -cont
3-2-24. Operating Modes/Functions, HF Radio Set (AN/ARC-220) -cont - TM-1-1520-240-10_151
3-2-24. Operating Modes/Functions, HF Radio Set (AN/ARC-220) -cont - TM-1-1520-240-10_152
3-2-24. Operating Modes/Functions, HF Radio Set (AN/ARC-220) -cont - TM-1-1520-240-10_153
3-2-26.  Controls, Indicators, Connectors and Func- tion (TSEC/KY-100, Z-AVH)
3-2-27. Display Annunciators/Fields (TSEC/ KY-100, Z-AVH).
3-2-29.  Key Loading Procedures
3-2-31.  Online Mode Selection Menu
3-2-33.  Standard Operation
Figure  3-2-9.  Remote Control Unit TSEC/KY-100 (Z-AVH)
SECTION  III.  NAVIGATION EQUIPMENT
3-3-4.  Normal Operation - VHF Navigation and In- strument Landing System
Figure  3-3-2.  Direction Finder Control
3-3-9.  Controls and Function, Gyromagnetic Com- pass Set (AN/ASN-43)
3-3-11.  Doppler Navigation Set (AN/ASN-128)
Figure  3-3-5.  Doppler Navigation Set Control (AN/ASN-128)
3-3-12.  Controls and Function - Doppler Naviga- tion Set.
3-3-13.  Display and Keyboard Operation.
Table  3-3-2.   Computer-Display Unit Data Displays
3-3-17.  Entering Spheroid and/or Variation.
3-3-19.  Entering Present Position or Destination in LAT/LONG
3-3-24.  Update of Present Position from Land- mark
3-3-28.  Transferring Stored Target Coordinates from One Location to Another.
3-3-34.  Controls and Indicators - Horizontal Situa- tion Indicators
Figure  3-3-6.  Horizontal Situation Indicator and Mode Select Panel
3-3-35.  Horizontal   Situation   Indicator   Mode   Se- lect.
3-3-37.  Controls, Displays and Function. -cont
Figure  3-3-7.  Doppler/GPS Navigation System AN/ANS-128B
3-3-44.  Test Mode
3-3-46.  CDU Operation.
3-3-49.  General Operating Procedures for Entering Data. The panel display consists of four line LCD readout. The top line of the display is reserved for the display of Fly-To- destination number and destination name/International Civil Aeronautic Organization (ICAO) identifier, EPE in meters, mode of GPS and mode of AN/ASN-128B opera- tion and target store number. The remaining lines will display data in accordance with the DISPLAY and MODE switches. When depressing the KYBD key for the first time in an entry procedure, the display freezes, kybd is displayed in the bottom right corner indicating the display is in the keyboard mode and the input field under key- board control blinks. If it is not desired to change the display field under control, the pilot can advance to the next field of the display by depressing the KYBD key again. Depressing ENT key (whether or not new data has been entered) causes the display to blank momentarily and return with the latest computed data. To abort a keyboard operation, move the mode or display switch to another position. NOTE All keys activate upon release after being de- pressed. Keys should be depressed and im- mediately released in one continuous motion. a.  Data Entry. To display a letter, first depress the LTR key corresponding to the position of the desired letter on a key. Then depress the key which contains the desired letter. For example, to enter an L, first depress The LTR RIGHT key, then depress the 4 key. b.  Keyboard Correction Capability. The last charac- ter entered may be cleared by depressing the CLR key. If the CLR key is depressed twice in succession, the field is cleared but remains under control (indicated by blink- ing) and the last valid data entered is displayed. c.  Destination Variation Constraint. The magnetic variation associated with a destination must be entered AFTER the coordinates for that destination are entered. The order of entry for present position is irrelevant. d.  Impossibility of Entering Unacceptable Data. In most cases the computer program will reject unaccept- able data (for example, a MGRS area W1 does not exists and will be rejected). If the operator attempts to insert unacceptable data, the unacceptable data will be dis- played on the panel and then the selected field will blink after ENT key is pressed displaying the last valid data. NOTE The computer cannot prevent insertion of er- roneous data resulting, for example, from hu- man or map errors. e.  Procedure for Displaying Wind Speed and Direc- tion. NOTE In MGRS mode, wind speed is displayed in km/hr; in LAT/LONG mode, wind speed is dis- played in knots. Wind direction is defined as the direction from which the wind originates. (1) Set MODE switch to LAT/LONG (MGRS may also be used). (2) Set DISPLAY switch to WINDUTC/DATA and observe display. (3) The display indicates: SP;XXXKn DIR:XXX_ f.  Procedure for Displaying/Entering UTC and Dis- playing GPS Status. (1) Set MODE switch to LAT/LONG (MGRS may also be used). (2) Set DISPLAY switch to WIND-UTC/DATA and observe the wind speed/direction display. (3) Depress ENT key. Observe that the CDU display indicates year XX, day XXX and indicates hours, minutes, and seconds of UTC time: XX Hours, XX Min- utes, XX Seconds. (4) To enter year, day, and time depress the KYBD key to select the field for input shown as a blinking field, enter the desired data and depress the ENT key. (5) To display GPS status depress the ENT to display selection menu. 1>SEA CURRENT 2>SURFACE WIND 3>GPS STATUS 4>DATA LOAD end (6) To select the GPS STATUS page depress the 3 key.
3-3-50.  Preflight Procedures.
d.  Self-Test
e.  Procedure for Displaying or Selecting GPS M or Y Operating Mode, Doppler, GPS, or Combined Operation, and Displaying Groundspeed and Track
g.  Procedure for Entering/Displaying Present Posi- tion or one of the 100 Possible Destinations in LAT/ LONG
h.  Procedures for Entering Variation and Landing Mode Data.
3-3-51. Flight Procedures
3-3-52.  Fly-To Destination Operation
Figure  3-3-8.  Graphic Definition of Course Terms
d.  Procedure   to   Enter   Route-Sequence   Random Mode
f.  Procedure for Displaying Distance/Bearing/Time Information
Table  3-3-4.   Map Datum Codes
Map Datum Codes - (Continued).
3-3-55.  Normal Operation - GPS Data Loader Recep- tacle.
3-3-60.  Normal Operation GPS Zeroize Switch
SECTION IV. TRANSPONDERS
3-4-2.  Controls and Function, Transponder Control (TR-1285/APX-100) (RT-1558/APX-100) -cont
3-4-3.  Normal Operation Transponder System
Figure  3-4-2.  Remote GPS Data Loader Receptacle/KYK-13 Fill Panel
CHAPTER 4 MISSION EQUIPMENT
Threat symbols
Figure  4-1-1.  Radar Signal Detecting Set Indicator
4-1-3.  Controls and Function, Radar Signal Detect- ing Control
Figure  4-1-3.  Radar Signal Detecting Set (OFP and EID VERSION DISPLAY)
Figure  4-1-4.  Radar Signal Detecting Set Indicator (Self Test Displays)
4-1-6.  Controls and Indicators, Missile Detector Set (AN/ALQ-156)
4-1-8.  Flare Dispenser M-130
4-1-14.  In-Flight Operation
4-1-17.  Countermeasures Dispenser System, AN/ ALE 47.
Figure  4-1-6.  Flare Dispenser System (Sheet 1 of 2)
Figure  4-1-6. ALE 47 Flare Dispenser System (Sheet 2 of 2)
4-1-18.  Controls and Function, Countermeasures Dispenser System (AN/ALE-47)
Figure  4-1-7.  AN/ALE-47 Countermeasures Dispenser System (CMDS)
4-1-24.  Normal Operation
4-1-25.  Flight Operations
4-1-26.  CMDS Messages.
4-1-28.  Controls and Function, Converter Control Unit
Figure  4-1-8.  Heads Up Display AN/AVS-7
4-1-29.  Controls and Function, Pilot/Copilot HUD Control (THRUST CONT LEVER)
Figure  4-1-9.   CH-47D HUD Master Mode Symbology Display (Sheet 2 of 3)
4-1-33.  Starting Procedure
4-1-35.  Displayed System Faults
Figure  4-1-10.  Symbol Generator Test Mode
4-1-37.  Adjustment of Barometric Altitude, Pitch, and Roll.
4-1-40.  Emergency Egress
SECTION II. ARMAMENT
Table  4-2-1.   Armament Subsystem M24 Data
Figure  4-2-1.  Armament Subsystem
Figure  4-2-2.  Machine Gun M60D
3.   After Firing Operation
Figure  4-2-3.  M24 Mount
Figure  4-2-5.  Right Machine Gun Mount Installed
Figure  4-2-7.  Ejection control Bag Installed
Figure  4-2-8.  Ammunition Can Installed
Figure  4-2-9.  Machine Gun Positioned on Pintle Left Side Shown
Figure  4-2-10.  M41 Mount Installed on Ramp
SECTION  III.  CARGO HANDLING SYSTEMS
b. Winch control switches
Figure  4-3-1.  Winching System
Figure  4-3-2.  Winch Capabilities (Sheet 1 of 2)
Figure  4-3-2.   Winch Capabilities (Sheet 2 of 2)
Figure  4-3-3.  Hoist Control Panel
Figure  4-3-7.  Winch/Hoist Control Grip
e. Rigging and operating procedures
Figure  4-3-9.  Hoisting System (Sheet 1 of 2)
(2) Break the shear wire
Figure  4-3-9.   Hoisting System (Sheet 2 of 2)
4-3-4.  Winching Accessories.
4-3-5.  Hoisting System
4-3-9.  Center Cargo Hook Loading Pole.
Figure  4-3-11.  Static Line Retriever System
4-3-11.  Cargo Hook Controls
Figure  4-3-13.  Center Cargo Hook and Cargo Hook Release
Figure  4-3-14.  Forward and Aft Cargo Hooks
4-3-16.  Cargo Hooks Operational Check.
4-3-17.  Normal Operation of Cargo hooks
Figure  4-3-15.  HICHS with 463L Palletized
Figure  4-3-16.  Fixture Configuration
4-3-21.  System Configuration.
Figure  4-3-17.  Internal Cargo Handling System
Figure  4-3-18.  Tiedown Fittings HICHS
SECTION  IV.  EXTENDED RANGE FUEL SYSTEM (ERFS) AND ERFS II
a. Fuel Hoses.
Figure  4-4-1.  ERFS II Fuel Tank
4-4-7.  Fuel Transfer to Helicopter Main Tanks
Figure  4-4-2.  ERFS II Fuel Control Panel
Figure  4-4-3.  ERFS Fuel System Schematic
4-4-9.  FARE Transfer
CHAPTER 5 OPERATING LIMITS AND RESTRICTIONS
SECTION  II.  SYSTEM LIMITS
Figure  5-2-1.  Instrument Markings (Sheet 1 of 5)
Figure  5-2-1 Instrument Markings (Sheet 2 of 5)
Figure  5-2-1 Instrument Markings (Sheet 3 of 5)
Figure  5-2-1 Instrument Markings (Sheet 4 of 5)
Figure  5-2-1 Instrument Markings (Sheet 5 of 5)
SECTION  III.  POWER LIMITS
SECTION  IV.  LOADING LIMITS
SECTION  V.  AIRSPEED LIMITS
Figure  5-5-1.  Airspeed Limitations Inoperative Cruise Guide Indicator
Figure  5-5-2.  Airspeed Limitations Longitudinal Cyclic Trim Retracted
SECTION  VI.  MANEUVERING LIMITS
SECTION  VII.  ENVIRONMENTAL RESTRICTIONS
Table  5-7-1.     Bypass Panel Removal Requirement
Figure  5-7-1.  Rotor Blade Start-Up & Shutdown Limits   Sheet (1 of 2)
Figure  5-7-1.     Rotor Blade Start-Up & Shutdown Limits   Sheet (2 of 2)
SECTION  VIII.  WATER OPERATION LIMITATIONS
Table  5-8-1.     Description of Sea States (Continued)
SECTION  IX.  ADDITIONAL LIMITATIONS
CHAPTER 6 WEIGHT/BALANCE AND LOADING
Figure  6-1-1.  Aircraft Compartment and Loading Diagram
SECTION  II.  WEIGHT AND BALANCE
SECTION III. FUEL/OIL
Figure  6-3-1.  Fuel Moment Chart
SECTION IV. PERSONNEL
6-4-11.  Litter Support Brackets.
Figure  6-4-1.  Personnel Moments
Figure  6-4-2.  Litter Patient Moments
Figure  6-4-3.  Troop Seats and Litters
Figure  6-4-4.  Troop Seat Installation (Sheet 1 of 2)
Figure  6-4-4.   Troop Seat Installation (Sheet 2 of 2)
Figure  6-4-5.  Litter Installation (Sheet 1 of 3)
Figure  6-4-5.   Litter Installation (Sheet 2 of 3)
Figure  6-4-5.   Litter Installation (Sheet 3 of 3)
Table  6-4-1.   Seat and Litter Arrangement Data
SECTION  V.  MISSION EQUIPMENT
Figure  6-5-1.  Mission Equipment Weights and Moments (Sheet 1 of 2)
Figure  6-5-1. Mission Equipment Weights and Moments (Sheet 2 of 2)
SECTION  VI.  CARGO LOADING
6-6-8.  Uniformly Distributed Loads.
Figure  6-6-1.  Cargo Compartment Dimensions
Figure  6-6-2.  Maximum Package Size (Sheet 1 of 3)
Figure  6-6-2.   Maximum Package Size (Sheet 2 of 3)
6-6-18.  Cargo Loading Aids
Figure  6-6-2.   Maximum Package Size (Sheet 3 of 3)
Figure  6-6-3.  Tiedown Fittings
Figure  6-6-4.  Compartment Data
Figure  6-6-5.  Internal Cargo Moments Chart (Sheet 1 of 2)
Figure  6-6-5.   Internal Cargo Moments Chart (Sheet 2 of 2)
Figure  6-6-6.  External Cargo Moments Chart (Sheet 1 of 2)
Figure  6-6-6.   External Cargo Moments Chart (Sheet 2 of 2)
Figure  6-6-7.  Cargo Door and Ramp
Figure  6-6-8.  Ramp Controls
Figure  6-6-9.  Sequence Valve Operation
6-6-31.  Ramp Emergency Control
6-6-35. Cargo Weight.
Figure  6-6-10.  Stowage Locations
Figure  6-6-11.  Cargo Door Cranking
6-6-47.  Securing Cargo.
Figure  6-6-12.  Compartment Loading
Figure  6-6-13.  Station Loading
6-6-55.  463 L Pallet/Extended Range Fuel System (ERFS)
Table  6-6-1.   Extended Range Fuel System (ERFS) Weight and Balance Data
Table  6-6-2.   Extended Range Fuel System II (ERFS II) Weight and Balance Data
Table  6-6-3.   Loading Sequence Configuration
Loading Sequence Configuration (Continued) - TM-1-1520-240-10_335
Loading Sequence Configuration (Continued) - TM-1-1520-240-10_336
Figure  6-6-14.  Loading With Ramp Down (Forklift Loading)
Figure  6-6-15.  Loading With Ramp In Level Position
Figure  6-6-16.  Loading Clearances
SECTION  VII.  LOADING LIMITS
Figure  6-7-1.  C.G. Limits Chart
CHAPTER 7 712 PERFORMANCE DATA
7-1-7.  General Conditions
Figure  7-1-1.  Temperature Conversion Chart
SECTION  II.  EMERGENCY TORQUE AVAILABLE
Figure  7-2-1.  Emergency Torque Available
SECTION  III.  MAXIMUM TORQUE AVAILABLE - TM-1-1520-240-10_347
Figure  7-3-1.  Maximum Torque Available (10 - Minute Operation)
Figure  7-3-2.  Maximum Torque Available (30 - Minute Operation)
SECTION  IV.  CONTINUOUS TORQUE AVAILABLE - TM-1-1520-240-10_350
Figure  7-4-1.  Continuous Torque Available
SECTION V. HOVER - TM-1-1520-240-10_352
Figure  7-5-1.  Hover Chart
Figure  7-5-2.  Hover Ceiling
SECTION VI. TAKEOFF - TM-1-1520-240-10_355
Figure  7-6-1.  Takeoff Chart
SECTION VII. CRUISE - TM-1-1520-240-10_357
Table  7-7-1     EAPS Penalty Table
EAPS Penalty Table (Continued) - TM-1-1520-240-10_359
EAPS Penalty Table (Continued) - TM-1-1520-240-10_360
EAPS Penalty Table (Continued) - TM-1-1520-240-10_361
CRUISE EXAMPLE
Figure 7-7-1 Example Cruise Chart (Sheet 2 of 2)
Figure  7-7-2.  98 and 100% Rotor RPM, 50_C, Sea Level
Figure  7-7-3.  98 and 100% Rotor RPM, 40_C, Sea Level
Figure  7-7-4.  98 and 100% Rotor RPM, 30_C, Sea Level
Figure  7-7-5.  98 and 100% Rotor RPM, 20_C, Sea Level
Figure  7-7-6.  100% Rotor RPM, 10_ and and 0_C, Sea Level
Figure  7-7-7.  100% Rotor RPM, 10_ and 20_C, Sea Level
Figure  7-7-8.  100% Rotor RPM, 30_ and 40_C, Sea Level
Figure  7-7-9.  100% Rotor RPM, 50_C, Sea Level
Figure  7-7-10.  98 and 100% Rotor RPM, 50_C, 2,000 Feet
Figure  7-7-11.  98 and 100% Rotor RPM, 40_C, 2,000 Feet
Figure  7-7-12.  98 and 100% Rotor RPM, 30_C, 2,000 Feet
Figure  7-7-13.  98 and 100% Rotor RPM, 20_C, 2,000 Feet
Figure  7-7-14.  100% Rotor RPM, 10_ and 0_C, 2,000 Feet
Figure  7-7-15.  100% Rotor RPM, 10_ and 20_C, 2,000 Feet
Figure  7-7-16.  100% Rotor RPM, 30_ and 40_C, 2,000 Feet
Figure  7-7-17.  100% Rotor RPM, 50_C, 2,000 Feet
Figure  7-7-18.  98 and 100% Rotor RPM, 50_C, 4,000 Feet
Figure  7-7-19.  98 and 100% Rotor RPM, 40_C, 4,000 Feet
Figure  7-7-20.  98 and 100% Rotor RPM, 30_C, 4,000 Feet
Figure  7-7-21.  98 and 100% Rotor RPM, 20_C, 4,000 Feet
Figure  7-7-22.  100% Rotor RPM, 10_ and 0_C, 4,000 Feet
Figure  7-7-23.  100% Rotor RPM, 10_ and 20_C, 4,000 Feet
Figure  7-7-24.  100% Rotor RPM, 30_ and 40_C, 4,000 Feet
Figure  7-7-25.  100% Rotor RPM, 50_C, 4,000 Feet
Figure  7-7-26. 98 and 100% Rotor RPM, 50_C, 6,000 Feet
Figure  7-7-27. 98 and 100% Rotor RPM, 40_C, 6,000 Feet
Figure  7-7-28. 98 and 100% Rotor RPM, 30_C, 6,000 Feet
Figure  7-7-29. 98 and 100% Rotor RPM, 20_C, 6,000 Feet
Figure  7-7-30. 100% Rotor RPM, 10_and 0_C, 6,000 Feet
Figure  7-7-31. 100% Rotor RPM, 10_ and 20_C, 6,000 Feet
Figure  7-7-32. 100% Rotor RPM, 30_ and 40_C, 6,000 Feet
Figure  7-7-33. 100% Rotor RPM, 50_C, 6,000 Feet
Figure  7-7-34. 98 and 100% RPM, 50_C, 8,000 Feet
Figure  7-7-35. 98 and 100% Rotor RPM, 40_C, 8,000 Feet.
Figure  7-7-36. 98 and 100% Rotor RPM, 30_C, 8,000 Feet
Figure  7-7-37. 98 and 100% Rotor RPM, 20_C, 8,000 Feet
Figure  7-7-38. 100% Rotor RPM, 10_ and 0_C, 8,000 Feet
Figure  7-7-39. 100% Rotor RPM, 10_ and 20_C, 8,000 Feet
Figure  7-7-40. 100% Rotor RPM, 30_ and 40_C, 8,000 Feet
Figure  7-7-41. 100% Rotor RPM, 50_C, 8,000 Feet
Figure  7-7-42. 98 and 100% Rotor RPM, 50_C, 10,000 Feet
Figure  7-7-43. 98 and 100% Rotor RPM, 40_C, 10,000 Feet
Figure  7-7-44. 98 and 100% Rotor RPM, 30_C, 10,000 Feet
Figure  7-7-45. 98 and 100% Rotor RPM, 20_C, 10,000 Feet
Figure  7-7-46. 100% Rotor RPM, 10_ and 0_C, 10,000 Feet
Figure  7-7-47. 100% Rotor RPM, 10_ and 20_C, 10,000 Feet
Figure  7-7-48. 100% Rotor RPM, 30_ and 40_C, 10,000 Feet
Figure  7-7-49. 100% Rotor RPM, 50_C, 10,000 Feet
Figure  7-7-50. 98 and 100% Rotor RPM, 50_C, 12,000 Feet
Figure  7-7-51. 98 and 100% Rotor RPM, 40_C, 12,000 Feet
Figure  7-7-52. 98 and 100% Rotor RPM, 30_C, 12,000 Feet
Figure  7-7-53. 98 and 100% Rotor RPM, 20_C, 12,000 Feet
Figure  7-7-54. 100% Rotor RPM, 10_ and 0_C, 12,000 Feet
Figure  7-7-55. 100% Rotor RPM, 10_ and 20_C, 12,000 Feet
Figure  7-7-56. 100% Rotor RPM, 30_ and 40_C, 12,000 Feet
Figure  7-7-57. 100% Rotor RPM, 50_C, 12,000 Feet
Figure  7-7-58.  98 and 100% Rotor RPM, -50_C, 14,000 Feet
Figure  7-7-59. 98 and 100% Rotor RPM, 40_C, 14,000 Feet
Figure  7-7-60. 98 and 100% Rotor RPM, 30_C, 14,000 Feet
Figure  7-7-61. 98 and 100% Rotor RPM, 20_C, 14,000 Feet
Figure  7-7-62. 100% Rotor RPM, 10_ and 0_C, 14,000 Feet
Figure  7-7-63. 100% Rotor RPM, 10_ and 20_C, 14,000 Feet
Figure  7-7-64. 100% Rotor RPM, 30_ and 40_C, 14,000 Feet
Figure  7-7-65. 100% Rotor RPM, 50_C, 14,000 Feet
Figure  7-7-66. 98 and 100% Rotor RPM, 50_C, 16,000 Feet
Figure  7-7-67. 98 and 100% Rotor RPM, 40_C, 16,000 Feet
Figure  7-7-68. 98 and 100% Rotor RPM, 30_C, 16,000 Feet
Figure  7-7-69. 98 and 100% Rotor RPM, 20_C, 16,000 Feet
Figure  7-7-70. 100% Rotor RPM, 10_ and 0_C, 16,000 Feet
Figure  7-7-71. 100% Rotor RPM, 10_ and 20_C, 16,000 Feet
Figure  7-7-72. 100% Rotor RPM, 30_ and 40_C, 16,000 Feet
Figure  7-7-73. 98 and 100% Rotor RPM, 50_C, 18,000 Feet
Figure  7-7-74. 98 and 100% Rotor RPM, 40_C, 18,000 Feet
Figure  7-7-75. 98 and 100% Rotor RPM, 30_C, 18,000 Feet
Figure  7-7-76. 98 and 100% Rotor RPM, 20_C, 18,000 Feet
Figure  7-7-77. 98 and 100% Rotor RPM, 10_ and 0_C, 18,000 Feet
Figure  7-7-78. 98 and 100% Rotor RPM, 10_ and 20_C, 18,000 Feet
Figure  7-7-79. 98 and 100% Rotor RPM, 50_C, 20,000 Feet
Figure  7-7-80. 98 and 100% Rotor RPM, 40_C, 20,000 Feet
Figure  7-7-81. 98 and 100% Rotor RPM, 30_C, 20,000 Feet
Figure  7-7-82. 98 and 100% Rotor RPM, 20_C, 20,000 Feet
Figure  7-7-83. 100% Rotor RPM, 10_ and 0_C, 20,000 Feet
Figure  7-7-84.  100% Rotor RPM, 10_ and 20_C, 20,000 Feet
SECTION VIII. DRAG - TM-1-1520-240-10_447
Figure  7-8-1. Drag Chart
SECTION  IX.  CLIMB DESCENT - TM-1-1520-240-10_449
Figure  7-9-1.  Climb and Descent Chart
Figure  7-9-2.  Climb Performance (Sheet 1 of 2)
Figure 7-9-2. Climb Performance (Sheet 2 of 2)
SECTION  X.  FUEL FLOW
Figure  7-10-1.  Idle Fuel Flow Chart
Figure  7-10-2.  Idle Fuel Flow Chart
SECTION  XI.  AIRSPEED CALIBRATION - TM-1-1520-240-10_456
Figure  7-11-1.  Airspeed Calibration Chart
CHAPTER 7A    PERFORMANCE DATA
7A-1-7.  General Conditions.
Figure  7A-1-1.  Temperature Conversion Chart
SECTION  II.  CONTINGENCY TORQUE AVAILABLE
Figure  7A-2-1.  Contingency Torque Available
SECTION  III.  MAXIMUM TORQUE AVAILABLE - TM-1-1520-240-10_463
Figure  7A-3-1.  Maximum Torque Available (10 - Minute Operation)
Figure  7A-3-2.  Intermediate Torque Available (30 - Minute Operation)
SECTION  IV.  CONTINUOUS TORQUE AVAILABLE - TM-1-1520-240-10_466
Figure  7A-4-1.  Continuous Torque Available
SECTION V. HOVER - TM-1-1520-240-10_468
Figure  7A-5-1. Hover Chart
Figure  7A-5-2.  Hover Ceiling
SECTION VI. TAKEOFF - TM-1-1520-240-10_471
Figure  7A-6-1.  Takeoff Chart
SECTION VII. CRUISE - TM-1-1520-240-10_473
Table  7A-7-1.     EAPS Penalty Table
EAPS Penalty Table (Continued) - TM-1-1520-240-10_475
EAPS Penalty Table (Continued) - TM-1-1520-240-10_476
EAPS Penalty Table (Continued) - TM-1-1520-240-10_477
Figure  7A-7-1.  Example Cruise Chart (Sheet 1 of 2)
Figure  7A-7-1.     Example Cruise Chart (Sheet 2 of 2)
Figure  7A-7-2.  98 and 100% Rotor RPM, 50_C, Sea Level
Figure  7A-7-3.  98 and 100% Rotor RPM, 40_C, Sea Level
Figure  7A-7-4.  98 and 100% Rotor RPM, 30_C, Sea Level
Figure  7A-7-5.  98 and 100% Rotor RPM, 20_C, Sea Level
Figure  7A-7-6.  100% Rotor RPM, 10_ and 0_C, Sea Level
Figure  7A-7-7.  100% Rotor RPM, 10_ and 20_C, Sea Level
Figure  7A-7-8.  100% Rotor RPM, 30_ and 40_C, Sea Level
Figure  7A-7-9.  100% Rotor RPM, 50_C, Sea Level
Figure  7A-7-10. 98 and 100% Rotor RPM, 50_C, 2,000 Feet
Figure  7A-7-11.  98 and 100% Rotor RPM, 40_C, 2,000 Feet
Figure  7A-7-12.  98 and 100% Rotor RPM, 30_C, 2,000 Feet
Figure  7A-7-13.  98 and 100% Rotor RPM, 20_C, 2,000 Feet
Figure  7A-7-14.  100% Rotor RPM, -10_ and 0_C, 2,000 Feet
Figure  7A-7-15.  100% Rotor RPM, 10_ and 20_C, 2,000 Fee
Figure  7A-7-16.  100% Rotor RPM, 30_ and 40_C, 2,000 Feet
Figure  7A-7-17.  100% Rotor RPM, 50_C, 2,000 Feet
Figure  7A-7-18.  98 and 100% Rotor RPM, 50_C, 4,000 Feet
Figure  7A-7-19.  98 and 100% Rotor RPM, 40_C, 4,000 Feet
Figure  7A-7-20.  98 and 100% Rotor RPM, 30_C, 4,000 Feet
Figure  7A-7-21. 98 and 100% Rotor RPM, 20_C, 4,000 Feet
Figure  7A-7-22.  100% Rotor RPM, 10_ and 0_C, 4,000 Feet
Figure  7A-7-23.  100% Rotor RPM, 10_ and 20_C, 4,000 Feet
Figure  7A-7-24.  100% Rotor RPM,   30_ and 40_C, 4,000 Feet
Figure  7A-7-25.  100% Rotor RPM,   50_C, 4,000 Feet
Figure  7A-7-26.  98 and 100% Rotor RPM,   50_C, 6,000 Feet
Figure  7A-7-27.  98 and 100% Rotor RPM,   40_C, 6,000 Feet
Figure  7A-7-28.  98 and 100% Rotor RPM,   30_C, 6,000 Feet
Figure  7A-7-29.  98 and 100% Rotor RPM,   20_C, 6,000 Feet
Figure  7A-7-30.  100% Rotor RPM,   10_ and 0_C, 6,000 Feet
Figure  7A-7-31.  100% Rotor RPM,   10_ and 20_C, 6,000 Feet
Figure  7A-7-32.  100% Rotor RPM,   30 and 40_C, 6,000 Feet
Figure  7A-7-33.  100% Rotor RPM,   50_C, 6,000 Feet
Figure  7A-7-34.  98 and 100% Rotor RPM,   50_C, 8,000 Feet
Figure  7A-7-35.  98 and 100% Rotor RPM,   40_C, 8,000 Feet
Figure  7A-7-36.  98 and 100% Rotor RPM,   30_C, 8,000 Feet
Figure  7A-7-37.  98 and 100% Rotor RPM,   20_C, 8,000 Feet
Figure  7A-7-38.  100% Rotor RPM,   10_ and 0_C, 8,000 Feet
Figure  7A-7-39.  100% Rotor RPM,   10_ and 20_C, 8,000 Feet
Figure  7A-7-40.  100% Rotor RPM,   30_ and 40_C, 8,000 Feet
Figure  7A-7-41.  100% Rotor RPM,   50_C, 8,000 Feet
Figure  7A-7-42.  98 and 100% Rotor RPM,   50_C, 10,000 Feet
Figure  7A-7-43.  98 and 100% Rotor RPM,   40_C, 10,000 Feet
Figure  7A-7-44.  98 and 100% Rotor RPM,   30_C, 10,000 Feet
Figure  7A-7-45.  98 and 100% Rotor RPM,   20_C, 10,000 Feet
Figure  7A-7-46.  100% Rotor RPM,   10_ and 0_C, 10,000 Feet
Figure  7A-7-47.  100% Rotor RPM,   10_ and 20_C, 10,000 Feet
Figure  7A-7-48.  100% Rotor RPM,   30_ and 40_C, 10,000 Feet
Figure  7A-7-49.  100% Rotor RPM,   50_C, 10,000 Feet
Figure  7A-7-50.  98 and 100% Rotor RPM,   50_C, 12,000 Feet
Figure  7A-7-51.  98 and 100% Rotor RPM,   40_C, 12,000 Feet
Figure  7A-7-52.  98 and 100% Rotor RPM,   30_C, 12,000 Feet
Figure  7A-7-53.  98 and 100% Rotor RPM,   20_C, 12,000 Feet
Figure  7A-7-54.  100% Rotor RPM,   10_ and 0_C, 12,000 Feet
Figure  7A-7-55.  100% Rotor RPM,   10_ and 20_C, 12,000 Feet
Figure  7A-7-56.  100% Rotor RPM,   30_ and 40_C, 12,000 Feet
Figure  7A-7-57.  100% Rotor RPM, 50_C, 12,000 Feet
Figure  7A-7-58.  98 and 100% Rotor RPM,   50_C, 14,000 Feet
Figure  7A-7-59.  98 and 100% Rotor RPM,   40_C, 14,000 Feet
Figure  7A-7-60.  98 and 100% Rotor RPM,   30_C, 14,000 Feet
Figure  7A-7-61. 98 and 100% Rotor RPM,   20_C, 14,000 Feet
Figure  7A-7-62.  100% Rotor RPM,   10_ and 0_C, 14,000 Feet
Figure  7A-7-63.  100% Rotor RPM,   10_ and 20_C, 14,000 Feet
Figure  7A-7-64.  100% Rotor RPM,   30_ and 40_C, 14,000 Feet
Figure  7A-7-65.  100% Rotor RPM,   50_C, 14,000 Feet
Figure  7A-7-66.  98 and 100% Rotor RPM,   50_C, 16,000 Feet
Figure  7A-7-67.  98 and 100% Rotor RPM,   40_C, 16,000 Feet
Figure  7A-7-68.  98 and 100% Rotor RPM,   30_C, 16,000 Feet
Figure  7A-7-69.  98 and 100% Rotor RPM,   20_C, 16,000 Feet
Figure  7A-7-70.  100% Rotor RPM,   10_ and 0_C, 16,000 Feet
Figure  7A-7-71.  100% Rotor RPM,   10_ and 20_C, 16,000 Feet
Figure  7A-7-72.  100% Rotor RPM,   30_ and 40_C, 16,000 Feet
Figure  7A-7-73.  98 and 100% Rotor RPM, 50_C, 18,000 Feet
Figure  7A-7-74. 98 and 100% Rotor RPM, 40_C, 18,000 Feet
Figure  7A-7-75.  98 and 100% Rotor RPM, 30_C, 18,000 Feet
Figure  7A-7-76.  98 and 100% Rotor RPM, 20_C, 18,000 Feet
Figure  7A-7-77.  100% Rotor RPM, 10_ and 0_C, 18,000 Feet
Figure  7A-7-78.  100% Rotor RPM, 10_ and 20_C, 18,000 Feet
Figure  7A-7-79.  98 and 100% Rotor RPM, 50_C, 20,000 Feet
Figure  7A-7-80. 98 and 100% Rotor RPM, 40_C, 20,000 Feet
Figure  7A-7-81.  98 and 100% Rotor RPM, 30_C, 20,000 Feet
Figure  7A-7-82.  98 and 100% Rotor RPM, 20_C, 20,000 Feet
Figure  7A-7-83.  100% Rotor RPM, 10_ and 0_C, 20,000 Feet
SECTION VIII. DRAG - TM-1-1520-240-10_562
TM-1-1520-240-10_563
Figure  7A-8-1.  Drag Chart
SECTION  IX.  CLIMB DESCENT - TM-1-1520-240-10_565
Figure  7A-9-1.  Climb Descent Chart
Figure  7A-9-2.  Climb Performance (Sheet 1 of 2)
Figure 7A-9-2. Climb Performance (Sheet 2 of 2)
SECTION  X. FUEL FLOW
Figure  7A-10-1.  Idle Fuel Flow Chart
Figure  7A-10-2.  Single Engine Fuel Flow Chart
SECTION  XI.  AIRSPEED CALIBRATION - TM-1-1520-240-10_572
Figure  7A-11-1.  Airspeed Calibration Chart
CHAPTER 8 NORMAL PROCEDURES
d.  Normal Procedures.
SECTION  II.  OPERATING PROCEDURES AND MANEUVERS
8-2-8.  Forward Cabin
8-2-9.  Aft Cabin
8-2-12.  Right Cabin.
8-2-15.  Top of Fuselage.
8-2-17.  Before Starting Engines.
8-2-18.  Starting Engines.
20.   Cyclic trim
b.   Reversionary
8-2-19.  Engine Ground Operation.
8-2-20.  Before Taxi.
Figure 8-2-1.  Taxi Director and Blade Watcher Positions
8-2-23.  Hover Check.
8-2-30.  DESCENT
8-2-35.  After Landing
Personnel injury or death
8-2-38.  Before Leaving Helicopter.
SECTION  III.  FLIGHT CHARACTERISTICS
8-3-6.  Aerodynamic Loads
SECTION  IV.  ADVERSE ENVIRONMENTAL CONDITIONS
c.  Stopping.
8-4-17.  Before Leaving Helicopter
8-4-40.  Power Deterioration
8-4-41.  Hovering.
CHAPTER 9 EMERGENCY PROCEDURES
9-1-6.  Engine
Figure 9-1-1.  Emergency Equipment
Figure 9-1-2.  Emergency Entrance and Escape Routes (Sheet 1 of 2)
Figure  9-1-2. Emergency Entrance and Escape Routes (Sheet 2 of 2)
9-1-10.  Dual Engine Failure.
Figure 9-1-3. 712  Single - Engine Service Ceiling
Figure 9-1-4. 712 Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 1 of 3)
Figure 9-1-4. 712 Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 2 of 3)
Figure 9-1-4. 712 Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 3 of 3)
Figure 9-1-5. 714A Single-Engine Service Ceiling
Figure 9-1-6. 714A   Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 1 of 3)
Figure  9-1-6.   714A   Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 2 of 3)
Figure 9-1-6. 714A   Height Velocity Diagram for Safe Landing After Single-Engine Failure (Sheet 3 of 3)
Figure 9-1-7.  Maximum Glide Distance / Minimum Rate of Decent in Autorotation
Figure 9-1-8. Autorotational Approach Corridor for Second Engine Failure
9-1-13.  Single Engine Failure Low Altitude/Low Airspeed and Cruise
9-1-16. 712 Normal Engine Beep Trim System Failure (Low Side or Static)
9-1-25.  Engine   Transmission   Clutch   Failure   to Engage.
9-1-28.  Engine Shutdown with APU or APU Genera- tor Inoperative
9-1-34.  Transmission Low Oil Pressure or High Temperature Indications.
9-1-41.  FIRE
9-1-48.  Smoke and Fume Elimination
9-1-56.  NO. 1 or NO. 2 GEN OFF Caution
9-1-59.  NO.1 and NO. 2 RECT OFF Cautions.
9-1-65.  Emergency Descent
9-1-70.  Ditching Power OFF
Figure 9-1-9.  Ditching Exits
9-1-77.  Vertical Gyro (VGI) Malfunction
SECTION  II.  MISSION EQUIPMENT
9-2-10.  FARE Pump Failure During Ground FARE Refueling Operation
Figure FO-1.  General Arrangement (Sheet 1 of 2)
Figure  FO-1 General Arrangement (Sheet 2 of 2)
Figure FO-2.  Power Distribution Panel (Typical)
Figure FO-3.  AC Power Supply (Typical)
Figure FO-4.  DC Power Supply (Typical)
Figure FO-5.  Power Distribution Panels (Typical) 714A
Figure FO-6.  AC Power Supply (Typical)
Figure FO-7.  DC Power Supply (Typical)
APPENDIX A REFERENCES
APPENDIX B GLOSSARY
ABBREVIATION -cont - TM-1-1520-240-10_641
ABBREVIATION -cont - TM-1-1520-240-10_642
ABBREVIATION -cont - TM-1-1520-240-10_643
ABBREVIATION -cont - TM-1-1520-240-10_644
APPENDIX C CONDITIONAL INSPECTIONS
CONDITIONAL INSPECTIONS -cont - TM-1-1520-240-10_646
CONDITIONAL INSPECTIONS -cont - TM-1-1520-240-10_647
PART 1 ALL PUBLICATIONS (EXCEPT RPSTL AND SC/SM) AND BLANK FORMS - TM-1-1520-240-10_670
PART II REPAIR PARTS AND SPECIAL TOOL LISTS AND SUPPLY CATALOGS/SUPPLY MANUALS - TM-1-1520-240-10_671
PART 1 ALL PUBLICATIONS (EXCEPT RPSTL AND SC/SM) AND BLANK FORMS - TM-1-1520-240-10_672
PART II REPAIR PARTS AND SPECIAL TOOL LISTS AND SUPPLY CATALOGS/SUPPLY MANUALS - TM-1-1520-240-10_673
PART 1 ALL PUBLICATIONS (EXCEPT RPSTL AND SC/SM) AND BLANK FORMS - TM-1-1520-240-10_674
PART II REPAIR PARTS AND SPECIAL TOOL LISTS AND SUPPLY CATALOGS/SUPPLY MANUALS - TM-1-1520-240-10_675

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