曝光臺(tái) 注意防騙 網(wǎng)曝天貓店富美金盛家居專(zhuān)營(yíng)店坑蒙拐騙欺詐消費(fèi)者

Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
A detected failure may hinder auto start.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
9-8
TM 1-1520-248-10
TABLE 9-6. (CDS4) ADVISORY MESSAGES AND ACTIONS REQUIRED (Cont)
ADVISORY
ONE YAW CHANNEL OFF
P(Y) CODE INVALID
PITOT HEAT ON
RHE FAIL
RIGHT COOLANT LOW
RIGHT LAUNCHER FAIL
RMS FAIL
TACAN FAIL
TACAN INVALID
TACFIRE AUTH TABLE LOW
TACFIRE MSG CHKALL
TACFIRE MSG CHKFIRE
TACFIRE MSG MAYDAY
TACFIRE MSG NO
TACFIRE QUEUE FULL
TIMER (timer name)
UHF FAIL
VDU FAIL
VHF FAIL
VTR FAIL
VTR TAPE FULL
WEDGE CONSTANT ZERO
WPN NOT ACTIONED
WPN NOT ARMED
ACTION
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
Information/system status.
5. LAND AS SOON AS PRACTICABLE.
e. The term FADEC MANUAL OPERATION is
defined as manually controlling the RPM with the
collective and throttle as necessary as follows:
If engine RPM cannot be maintained within limits:
6. LAND AS SOON AS POSSIBLE.
9-4. AFTER EMERGENCY ACTION.
appropriate emergency actions have been taken, and
the helicopter is on the ground, an entry shall be made
in the Remarks section of DA Form 2408-13-1 and
2408-13-1 E describing the malfunction. Ground and
flight operations shall be discontinued until corrective
action has been taken.
Information/system status.
Information/system status.
Information/system status.
RPM within limits.
4. Throttle and collective - Adjust to maintain
After a malfunction of equipment has occurred,
3. Collective - Adjust to maintain RPM within
limits.
2. AUTO/MAN switch - MAN (when appropriate
for the situation, if not already in MAN).
1. Throttle - Reduce.
9-9
TM 1-1520-248-10
9-5. EMERGENCY EQUIPMENT.
A fire extinguisher is mounted on left side of center
post behind the CPG seat. A first aid kit is mounted on
the right side of the center post behind the pilot seat
(fig. 9-1).
9-6. EMERGENCY EXITS.
Emergency exits are shown in fig, 9-1. Emergency exit
release handles are yellow. To exit the aircraft in the
event of an emergency, first attempt to open doors, If
doors will not open, use emergency jettison handles. If
doors will not jettison, break Plexiglass to exit the
aircraft.
9-7. ENGINE MALFUNCTION - PARTIAL OR
COMPLETE POWER LOSS.
WARNING
Do not respond to the RPM audio and/or
display on MFD and/or MPD without first
confirming engine failure by observing
one or more of the other indications.
Normal indications signify that the
engine is functioning properly and that
there is a malfunction in the engine or
rotor sensing system(s).
a. Indications. The indications of an engine
malfunction, either a partial power loss or complete
power loss, are a left yaw (caused by the reduction in
torque applied to the main rotor), a drop in engine RPM
(NG) and (NP), a drop in rotor RPM (NR), LOW RPM
ROTOR warning message on MFD, low RPM audio,
ENGINE OUT warning message on MFD, engine out
audio alarm, and a change in engine noise.
b. Flight Characteristics. The characteristics and
reactions in this helicopter without power are similar to
those during a normal powered descent. Full control
can be maintained with the helicopter in autorotational
descent. Main rotor RPM decays rapidly unless
collective is lowered immediately; deceleration attitude
　
中國(guó)航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：OPERATOR’S MANUAL FOR ARMY OH-58D HELICOPTER 2(86)