tm 1-1520-240-10 technical manual operator's manual for army ch ...

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Figure 7A-7-71. 100% Rotor RPM, 10 and 20C, 16,000 Feet TM 1-1520-240-10 7A-7-77
TM 1-1520-240-10 7A-7-78 Figure 7A-7-72. 100% Rotor RPM, 30 and 40C, 16,000 Feet
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TECHNICAL MANUAL OPERATOR’S MANUA
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TM 1-1520-240-10 b Change 1 WARNING
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URGENT TM 1-1520-240-10 CHANGE HEAD
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*Zero in this column indicates an o
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TM 1-1520-240-10 TECHNICAL MANUAL H
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TM 1-1520-240-10 Chapter/Section Pa
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TM 1-1520-240-10 1-1-13. Aircraft D
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TM 1-1520-240-10 2-1-2 Figure 2-1-1
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TM 1-1520-240-10 2-1-4 Figure 2-1-3
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TM 1-1520-240-10 2-1-10. Brakes and
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TM 1-1520-240-10 2-1-8 Figure 2-1-5
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TM 1-1520-240-10 2-1-10 Figure 2-1-
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TM 1-1520-240-10 2-1-12 Figure 2-1-
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TM 1-1520-240-10 2-1-14 Figure 2-1-
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TM 1-1520-240-10 2-1-16 Figure 2-1-
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TM 1-1520-240-10 2-1-18 Figure 2-1-
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TM 1-1520-240-10 2-2-2 Fwd Valve Fw
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TM 1-1520-240-10 2-2-8. TROOP WARN
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TM 1-1520-240-10 The power turbine
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TM 1-1520-240-10 Figure 2-3-2. Emer
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TM 1-1520-240-10 and NO. 2 OIL TEMP
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TM 1-1520-240-10 d. RRPM droop comp
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TM 1-1520-240-10 2-3-10 Figure 2-3-
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TM 1-1520-240-10 Table 2-3-1. T55-G
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TM 1-1520-240-10 2-3-14 Table 2-3-1
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TM 1-1520-240-10 Table 2-3-1. T55-G
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TM 1-1520-240-10 2-3-18 Figure 2-3-
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2-4-1. Fuel Supply System. The fuel
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2-4-6. Manual Defueling Valve. A ma
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2-4-6). The switches are used to te
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2-5-1. Flight Control System. The h
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Figure 2-5-2. Cyclic Stick Grip 2-5
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(1) HDG Switch. The HDG (heading) s
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2-6-1. Hydraulic Power Supply Syste
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us through the RAMP PWR switch and
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TM 1-1520-240-10 No. 2 engine trans
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TM 1-1520-240-10 2-7-12. Transmissi
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2-9-1. Anti Icing Systems. Anti ici
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through the HYDRAULICS MAINT PNL LT
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TM 1-1520-240-10 SECTION X. HEATING
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TM 1-1520-240-10 SECTION XI. ELECTR
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2-11-7. BATT Switch. NOTE The follo
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TM 1-1520-240-10 2-12-2 Figure 2-12
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TM 1-1520-240-10 a. Electroluminesc
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TM 1-1520-240-10 2-13-4 Figure 2-13
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TM 1-1520-240-10 bulkhead. The six
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TM 1-1520-240-10 2-13-8 Figure 2-13
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2-14-1. General. The following para
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When the helicopter descends below
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2-14-13. Controls and Function, Rad
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2-14-21. CHRONOMETER. Two digital c
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Table 2-14-1. Master Caution Panel
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2-14-30. CAUTION LT Panel. The CAUT
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SECTION XV. SERVICING, PARKING, AND
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k. Remove ground cables from the he
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Figure 2-15-2. Servicing Diagram (S
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Figure 2-15-2. Servicing Diagram (S
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TM 1-1520-240-10 Table 2-15-1. Serv
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Table 2-15-3. JP-4 Equivalent Fuel
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2-15-7. Gravity Refueling. Perform
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2-15-15. Transmission Oil System. S
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FLIGHT CONTROL, UTILITY, POWER STEE
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Figure 2-15-4. Protective Covers TM
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Figure 2-15-6. Installation of Heli
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TM 1-1520-240-10 3-1-2 Table 3-1-1.
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TM 1-1520-240-10 3-2-2 Figure 3-2-1
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TM 1-1520-240-10 3-2-6. Word-of-Day
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TM 1-1520-240-10 3-2-9. Conferencin
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TM 1-1520-240-10 SET. 3-2-8 (2) Cha
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TM 1-1520-240-10 3-2-10 NOTE The an
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TM 1-1520-240-10 c. Frequency Range
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TM 1-1520-240-10 3-2-19. Controls a
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TM 1-1520-240-10 3-2-21. HF Radio S
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TM 1-1520-240-10 3-2-24. Operating
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TM 1-1520-240-10 CONTROLS/ FUNCTION
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TM 1-1520-240-10 CONTROLS/ INDICATO
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TM 1-1520-240-10 (6) Push the INIT
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TM 1-1520-240-10 NOTE To exit and s
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TM 1-1520-240-10 3-3-8. Gyromagneti
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TM 1-1520-240-10 3-3-6 Figure 3-3-5
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TM 1-1520-240-10 LEFT DISPLAY RIGHT
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TM 1-1520-240-10 e. FLY-TO DEST thu
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TM 1-1520-240-10 from the No. 2 (No
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TM 1-1520-240-10 3-3-35. Horizontal
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TM 1-1520-240-10 tered in any of th
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TM 1-1520-240-10 (7) Observe the CD
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TM 1-1520-240-10 LEFT DISPLAY RIGHT
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TM 1-1520-240-10 3-3-26 NOTE To acc
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TM 1-1520-240-10 (3) Position updat
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TM 1-1520-240-10 (4) To select the
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TM 1-1520-240-10 NOTE In this mode,
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TM 1-1520-240-10 Table 3-3-4. Map D
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3-4-1. Transponder System (AN/APX-1
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3-4-3. Normal Operation — Transpo
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4-1-1. Radar Signal Detecting, AN/A
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4-1-2. CONTROLS AND FUNCTION, RADAR
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4-1-3). Check OFP and EID numbers a
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4-1-6. Controls and Indicators, Mis
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CONTROLS/ FUNCTION INDICATOR ARM In
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Figure 4-1-6. Flare Dispenser Syste
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4-1-18. Controls and Function, Coun
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4-1-24. Normal Operation. WARNING K
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4-1-26. CMDS Messages. Below is a l
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Figure 4-1-8. Heads Up Display AN/A
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No. Symbol Source Range/Description
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CAUTION Keep the protective caps on
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8. MODE 1-4/DCLT switch — DCLT (1
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4-2-1. Armament Subsystems The arma
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Figure 4-2-1. Armament Subsystem TM
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single cartridges or short bursts c
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Figure 4-2-5. Right Machine Gun Mou
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Figure 4-2-8. Ammunition Can — In
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Figure 4-2-10. M41 Mount — Instal
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TM 1-1520-240-10 (3) Cable cutter s
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TM 1-1520-240-10 4-3-4 Figure 4-3-2
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TM 1-1520-240-10 4-3-6 Figure 4-3-3
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TM 1-1520-240-10 (3) Hoist master s
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TM 1-1520-240-10 (2) Break the shea
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TM 1-1520-240-10 Figure 4-3-10. Hoi
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TM 1-1520-240-10 The hook assembly
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TM 1-1520-240-10 Figure 4-3-12. Cen
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TM 1-1520-240-10 4-3-18 CAUTION The
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TM 1-1520-240-10 HOOK OPEN caution
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TM 1-1520-240-10 4-3-22 Figure 4-3-
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TM 1-1520-240-10 4-3-24 Figure 4-3-
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TM 1-1520-240-10 SECTION IV. EXTEND
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Figure 4-4-1. ERFS II Fuel Tank TM
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Figure 4-4-2. ERFS II Fuel Control
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4-4-9. FARE Transfer. CAUTION Some
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5-2-1. Instrument Markings. 5-2-2.
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400 810 890 781 940 890 O C C C C C
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Figure 5-2-1 Instrument Markings (S
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5-3-1. Engine Rating and Power Leve
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5-5-1. Airspeed Operating Limits. A
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Figure 5-5-2. Airspeed Limitations
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5-7-1. Engine Inlet Screen Limitati
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Figure 5-7-1. Rotor Blade Start-Up
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TM 1-1520-240-10 5-7-5/(5-7-6 blank
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TM 1-1520-240-10 SEA STATE 5-8-2 Ta
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6-1-1. Purpose. This chapter contai
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6-2-1. DD Form 365-3 Chart C — Ba
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TM 1-1520-240-10 6-3-2 Figure 6-3-1
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TM 1-1520-240-10 6-4-11. Litter Sup
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TM 1-1520-240-10 6-4-4 Figure 6-4-2
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TM 1-1520-240-10 6-4-6 Figure 6-4-4
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TM 1-1520-240-10 6-4-8 Figure 6-4-5
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TM 1-1520-240-10 6-4-10 Figure 6-4-
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6-5-1. Mission Equipment. CH-47D mi
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Figure 6-5-1. Mission Equipment Wei
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TM 1-1520-240-10 6-6-8. Uniformly D
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TM 1-1520-240-10 6-6-10. Concentrat
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TM 1-1520-240-10 face of the floor.
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TM 1-1520-240-10 6-6-8 Figure 6-6-3
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TM 1-1520-240-10 6-6-10 Figure 6-6-
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TM 1-1520-240-10 6-6-12 Figure 6-6-
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TM 1-1520-240-10 6-6-21. Winch. Ref
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TM 1-1520-240-10 6-6-16 CAUTION Do
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TM 1-1520-240-10 6-6-35. Cargo Weig
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TM 1-1520-240-10 Figure 6-6-11. Car
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TM 1-1520-240-10 6-6-22 Figure 6-6-
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TM 1-1520-240-10 6-6-24 CAUTION Exc
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TM 1-1520-240-10 6-6-26 Table 6-6-2
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TM 1-1520-240-10 6-6-28 Table 6-6-3
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TM 1-1520-240-10 6-6-30 Figure 6-6-
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TM 1-1520-240-10 6-6-32 Figure 6-6-
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TM 1-1520-240-10 6-7-2 Figure 6-7-1
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TM 1-1520-240-10 b. Calculated Data
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7-2-1. Emergency Torque Available.
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SECTION III. MAXIMUM TORQUE AVAILAB
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Figure 7-3-2. Maximum Torque Availa
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TM 1-1520-240-10 7-4-2 Figure 7-4-1
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TM 1-1520-240-10 7-5-2 Figure 7-5-1
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7-6-1. Description. The takeoff cha
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7-7-1. Description. The cruise char
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Pressure OAT Altitude (ft) (C) Tabl
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Figure 7-7-1 Example Cruise Chart (
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Figure 7-7-3. 98 and 100% Rotor RPM
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Figure 7-7-5. 98 and 100% Rotor RPM
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Figure 7-7-7. 100% Rotor RPM, 10 an
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Figure 7-7-9. 100% Rotor RPM, 50C,
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Figure 7-7-11. 98 and 100% Rotor RP
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Figure 7-7-15. 100% Rotor RPM, 10 a
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Figure 7-7-83. 100% Rotor RPM, -10
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7-8-1. Description. The drag chart
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7-9-1. Description. a. Climb and de
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Figure 7-9-2. Climb Performance (Sh
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7-10-1. Description. The idle fuel
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Figure 7-10-2. Idle Fuel Flow Chart
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TM 1-1520-240-10 7-11-2 Figure 7-11
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TM 1-1520-240-10 c. Estimated Data.
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SECTION II. CONTINGENCY TORQUE AVAI
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SECTION III. MAXIMUM TORQUE AVAILAB
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Figure 7A-3-2. Intermediate Torque
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TM 1-1520-240-10 7A-4-2 Figure 7A-4
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TM 1-1520-240-10 7A-5-2 Figure 7A-5
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7A-6-1. Description. The takeoff ch
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7A-7-1. Description. The cruise cha
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Figure 7A-7-1. Example Cruise Chart
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Figure 7A-7-3. 98 and 100% Rotor RP
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Figure 7A-7-5. 98 and 100% Rotor RP
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Figure 7A-7-7. 100% Rotor RPM, 10 a
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Figure 7A-7-9. 100% Rotor RPM, 50C,
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Figure 7A-7-11. 98 and 100% Rotor R
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Figure 7A-7-15. 100% Rotor RPM, 10
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Figure 7A-25. Figure 7A-7-17. 100%
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Page 528 and 529: Figure 7A-7-21. 98 and 100% Rotor R
Page 530 and 531: Figure 7A-7-23. 100% Rotor RPM, 10
Page 532 and 533: Figure 7A-7-25. 100% Rotor RPM, 50C
Page 534 and 535: Figure 7A-36. Figure 7A-7-27. 98 an
Page 544 and 545: Figure 7A-46. Figure 7A-7-37. 98 an
Page 584 and 585: Figure 7A-7-77. 100% Rotor RPM, -10
Page 590 and 591: Figure 7A-7-83. 100% Rotor RPM, -10
Page 592 and 593: 7A-8-1. Description. The drag chart
Page 594 and 595: 7A-9-1. Description. a. Climb and d
Page 596 and 597: Figure 7A-9-2. Climb Performance (S
Page 598 and 599: 7A-10-1. Description. The idle fuel
Page 600: Figure 7A-10-2. Single Engine Fuel
Page 603 and 604: TM 1-1520-240-10 7A-11-2 Figure 7A-
Page 605 and 606: TM 1-1520-240-10 d. Normal Procedur
Page 607 and 608: TM 1-1520-240-10 8-2-2 * 6. Forward
Page 609 and 610: TM 1-1520-240-10 8-2-4 18. 714A P3
Page 611 and 612: TM 1-1520-240-10 8-2-6 15. Upper bo
Page 613 and 614: TM 1-1520-240-10 8-2-8 * 20. Cyclic
Page 615 and 616: TM 1-1520-240-10 8-2-10 * 38. GEN 1
Page 617 and 618: TM 1-1520-240-10 8-2-12 Figure 8-2-
Page 619 and 620: TM 1-1520-240-10 Takeoff over water
Page 621 and 622: TM 1-1520-240-10 8-2-16 14. PWR XFE
Page 624 and 625: 8-3-1. General. The flight characte
Page 626 and 627: SECTION IV. ADVERSE ENVIRONMENTAL C
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8-4-17. Before Leaving Helicopter.
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operating in these conditions, shou
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TM 1-1520-240-10 nals will be used
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TM 1-1520-240-10 9-1-4 EMERGENCY EX
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TM 1-1520-240-10 9-1-10. Dual Engin
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TM 1-1520-240-10 Figure 9-1-4. 712
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TM 1-1520-240-10 Figure 9-1-4. 712
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TM 1-1520-240-10 Figure 9-1-6. 714A
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TM 1-1520-240-10 Figure 9-1-6. 714A
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TM 1-1520-240-10 9-1-16 Figure 9-1-
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TM 1-1520-240-10 2. ENG COND lever
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TM 1-1520-240-10 9-1-28. Engine Shu
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TM 1-1520-240-10 9-1-40. 714A Torqu
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TM 1-1520-240-10 9-1-54. FUEL LOW a
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TM 1-1520-240-10 9-1-65. Emergency
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TM 1-1520-240-10 9-1-73. Flight Con
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9-2-1. ARMAMENT 9-2-2. Armament Sub
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Figure FO-1. General Arrangement (S
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DC ALE 47 DCDU 5 10 NO.1 SEQ NO.2 S
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Figure FO-4. DC Power Supply (Typic
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EAPS 1 FAN EAPS 2 FAN Figure FO-6.
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APPENDIX A REFERENCES TM 1-1520-240
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TM 1-1520-240-10 ABBREVIATION TERM
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TM 1-1520-240-10 ABBREVIATION TERM
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TM 1-1520-240-10 APPENDIX C CONDITI
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CONDITION 2408-13-1 ENTRY REQUIRED
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TM 1-1520-240-10 Subject Paragraph,
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By Order of the Secretary of the Ar
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RECOMMENDED CHANGES TO PUBLICATIONS
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Page 711 and 712:
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The Metric System and Equivalents L
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