支奴干运输直升机操作手册2(59)

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within 6 hours of transmission operation.
When MIL-H-83282 hydraulic fluid is
not available and MIL-H-5606 is
used.
Indicate quantity added.
When rotary wing blade has made
contact with a foreign object or when
the power train has been subjected
to a sudden reduction in RRPM.
Comment
Helicopter is struck by lightning. Comment
When a rotary wing blade has been
struck by lightning.
Comment
When a rotary wing has been flapping
due to high winds.
Comment
TM 1-1520-240-10
C-3/(C-4 blank)
CONDITION 2408-13-1 ENTRY REQUIRED REMARKS
When the rotor blades are pounded
against the droop stops, or have experienced
violent and heavy flapping,
or have been exposed to hurricane
or tornadic winds.
Comment
When a rotorhead is suspected of
excessive oil leakage.
Comment
When internal failure (metal
contamination) of a flight control or
utility hydraulic pump or motor
occurs.
Comment
When two different types of oil are
mixed in the APU.
Comment APU oil shall be changed and the
system flushed within 6 hours of
APU operation.
When the compass is suspected of
being in error.
Comment
After every manual release of the
center cargo hook under the load.
Comment
When a fault indication is displayed
on the MAINTENANCE PANEL.
Comment
When any Chapter 5 limitations
have been exceeded.
Limit or limits exceeded, range, time
above limits, and any additional data
that would aid maintenance personnel.
Whenever the aircraft is refueled
with JP8+100.
2408–13–1 Amount of JP8+100 fuel
recieved in gallons or pounds.
This is an informational entry and may
be removed after three refuelings of
JP8 without the +100 additive.

TM 1-1520-240-10
Index-1
ALPHABETICAL INDEX
Subject Paragraph, Figure, Subject Paragraph, Figure,
Table Number Table Number


Abbreviations . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . B-1
AC Cabin Utility Receptacles . . . . . . . . . . . . . . . . 2-9-14
Accumulator Gage . . . . . . . . . . . . . . . . . . . . . . . . . 6-6-26
Accumulator Precharge Limits . . . . . . . . . . . . . F 2-15-3
AC System . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-11–2
AC Power Supply
(Typical) 712 . . . . . . . . . . . . . . . . . . . . . . . . . F FO-3
AC Power Supply (Typical) 714A . . . . . . . . . F FO-6
Electrical Power Panel . . . . . . . . . . . . . . . . . . F 2-11-2
EXT PWR Caution . . . . . . . . . . . . . . . . . . . . . . . . 2-11-5
External Power Receptacles . . . . . . . . . . . . . F 2-11-1
Generator Control Switches . . . . . . . . . . . . . . . . 2-11-3
GEN OFF Cautions . . . . . . . . . . . . . . . . . . . . . . . 2-11-4
Power Distribution Panels (Typical) 712 . . . . F FO-2
Power Distribution Panels (Typical) 714A . . F FO-5
ADDITIONAL LIMITATIONS
Air-to-Ground Towing . . . . . . . . . . . . . . . . . . . . . 5-9-1
APU Operation . . . . . . . . . . . . . . . . . . . . . . . . . . 5-9-2
Extended Range Fuel System II(ERFSII) 4-80, 5-9-6
Pitot Tube and AFCS Sideslip Port . . . . . . . . . . 5-9-3
Single Point Refueling . . . . . . . . . . . . . . . . . . . . . 5-9-5
Windshield Heat . . . . . . . . . . . . . . . . . . . . . . . . . . 5-9-4
Advanced Flight Control System (AFCS) . . . . . . 2-5-7
Advanced Flight Control System Panel . . . . F 2-5-3
AFCS Control Panel . . . . . . . . . . . . . . . . . . . . . . 2-5-15
AFCS OFF Caution . . . . . . . . . . . . . . . . . . . . . . 2-5-17
Airspeed Hold . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-10
Altitude Hold . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-11
Bank Angle Hold . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-8
Command Select Switch . . . . . . . . . . . . . . . . . . 2-5-18
Controls and Indicators . . . . . . . . . . . . . . . . . . . 2-5-14
Cyclic Trim Indicators . . . . . . . . . . . . . . . . . . . . . 2-5-16
Forward and Aft Cyclic Trim Indicators . . . . . F 2-5-4
Heading Hold . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-9
Heading Select . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-12
Longitudinal Cyclic Trim System . . . . . . . . . . . 2-5-13
Aerobatics Prohibition . . . . . . . . . . . . . . . . . . . . . . . 5-1-29
Aerodynamic Loads . . . . . . . . . . . . . . . . . . . . . . . . 8-3-6
AFS Limitations . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-5-7
AFCS Trim Switch . . . . . . . . . . . . . . . . . . . . . . . . . . 2-5-5
After Landing . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8-2-35
　
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