曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
ENG 1 CHIP DETR Metal chips in No. 1 engine or engine transmission oil.
XMSN OIL HOT Transmission oil temperature is more than 140C.
XMSN CHIP DETR Metal chips in the oil of the forward, combining, or aft transmission or the aft thrust bearing.
ENG 2 CHIP DETR Metal chip in the No. 2 engine or engine transmission oil.
ENG 1 XMSN HOT No. 1 engine transmission oil temperature is above about 190C.
XMSN OIL PRESS Transmission main oil pressure is less than 20 psi, or less than 10 psi in the aft rotor
shaft.
ENG 2 XMSN HOT No. 2 engine transmission oil temperature is above about 190C.
L FUEL LVL Left main fuel tank has approximately 20 percent of fuel remaining.
XMSN AUX OIL
PRESS
Less than 20 psi auxilliary oil pressure in the forward, or aft transmission or less than 10
psi in the combining transmission.
R FUEL LVL Right main fuel tank has approximately 20 percent of fuel remaining.
L FUEL PRESS Left fuel pressure is below 10 spi.
HTR HOT Temperature within heater is greater than 177C.
R FUEL PRESS Right fuel pressure is below 10 psi.
RECT 1 Transformer-rectifier has failed or the generator output is interrupted.
BATT SYS MALF Battery or battery charging system has failed or the battery has exceeded the safe operating
temperature.
TM 1-1520-240-10
2-14-12
Table 2-14-2 Master Caution/Advisory Panel Capsules 714A (Continued)
WORD SEGMENT EXPLANATION
PWR STEER Steering control has been disabled due to system malfunction or steering limits have
been exceeded.
RECT 2 Transformer-rectifier has failed or the generator output is interrupted.
GEN 1 No. 1 generator is inoperative or the generator switch is at OFF.
GEN 2 No. 2 generator is inoperative or the generator switch is at OFF.
HYD 1 No. 1 flight control hydraulic system pressure us below 1,800 psi.
CD JAM Counter measures jammer failed.
UTIL HYD SYS Utility hydraulic system pressure is below 1,800 psi.
HYD 2 No. 2 flight control hydraulic system pressure is below 1,800 psi.
AFCS 1 The No. 1 AFCS is off, failed, or DASH is reprogramming.
CM INOP Counter measures inoperative.
DUAL HOOK FAULT The forward and/or aft hook circuit has an electrical fault and the hook(s) shall not be released
electrically.
AFCS 2 The No. 2 AFCS is off, failed, or DASH is reprogramming.
APU ON The APU is up to speed and can be used.
EXT PWR The light comes on whenever external popwer is conencted to the bus.
FWD HOOK OPEN The forward cargo hook has been opened either electrically or manually.
PARK BRK ON Parking brake is on.
MID HOOK OPEN The midcargo hook has been opened, either hydraulically, pneumatically, or manually.
AFT HOOK OPEN The aft cargo hook has been opened either electrically or manually.
TM 1-1520-240-10
2-15-1
SECTION XV. SERVICING, PARKING, AND MOORING
2-15-1. General.
This section contains instructions on servicing, parking,
and mooring the helicopter. These instructions include
only those tasks which a flight crew may be expected to
perform when away from a military maintenance support
activity. Diagrams and tables are provided depicting servicing
points, materials and walkways.
2-15-2. Servicing.
Safe walkway areas, no step areas, and no hand holds
are depicted in Figure 2-15-1. Servicing points are depicted
in Figure 2-15-2. Table 2-15-1 lists the approved
materials, specifications and capabilities. Table 2-15-2
lists commercial equivalents for oils.
2-15-3. Fuel Types.
The following describe the various types of fuel.
a. Army Standard Fuels. JP-8 is the Army-designated
primary fuels adopted for worldwide use.
b. Alternate Fuels. These are JP-4 and equivalent
commercial fuels which can be used continuously without
power reduction when Army standard fuel is not available.
Power setting adjustments and increased maintenance
may be required when an alternate fuel is used.
c. Emergency Fuels. 100LL (Low Lead) AVGAS
(aviation gasoline) is authorized for use as an emergency
fuel with operation not to exceed 6 hours cumulative
time.
2-15-4. Use of Fuel.
Consult TB 55-9150-200-24 for use of fuel and substitute
data as applicable for turbine engine aircraft (Refer to
tables 2-15-2, 2-15-3 and 2-15-4.)
a. There is no special limitation on the use of Army
standard or alternate fuel. Certain limitations are imposed
when emergency fuels are used. For record purposes,
fuel mixtures shall be identified as to the major
component of the mixture.
b. The use of JP8+100 additive is not authorized for
use. However in the event of an inadvertent JP8+100
refueling (ground or aviation), the following procedures
will apply;
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
支奴干运输直升机操作手册1(62)
