曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Description
Vol. 2 19−10−31
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
EICAS MESSAGES
Message Meaning Aural Warning (If Any)
ENGINE Left or right N1 or N2 or ITT above exceedance level.
WARNING
(Triple Chime)
L ENG OIL PRESS
Oil pressure in the respective engine is less than 25 psi. “ENGINE OIL”
R ENG OIL PRESS
L ENG START SOV The respective start shutoff valve is not closed with that
engine running.
WARNING
R ENG START SOV (Triple Chime)
APR INOP Either the APR has failed or it is not armed (APR to arm and N1 > 79% and both
eng speed switches on).
APR CMD SET APR has been inadvertently activated on both engines.
L ENG MISCOMP The engine comparator has sensed a discrepancy in the respective engine
R ENG MISCOMP parameters (N1, ITT or N2).
L FUEL FILTER
Respective fuel filter is in impending bypass mode.
R FUEL FILTER
L FUEL LO PRESS
Insufficient pressure at the respective engine pump inlet.
R FUEL LO PRESS
L REV UNLOCKED
Reverser moved away from fully stowed position without a deploy command.
R REV UNLOCKED
L REV UNSAFE
Unarmed thrust reverser received a deploy command.
R REV UNSAFE
APR ARM Aircraft in takeoff configuration, dynamic test OK.
APR TEST 1 OK
APR TEST 2 OK The respective APR circuit has passed the self-test.
APR TEST 3 OK
L ENG SOV CLSD Fuel shutoff valve is closed after activation of the respective ENG FIRE PUSH
R ENG SOV CLSD switch/light.
IGNITION A ’A’ igniters are activated, ’B’ igniters off.
IGNITION A/B Both ’A’ and B’ igniters are activated.
IGNITION B ’B’ igniters are activated, ’A’ igniters off.
L REV ARMED
The respective thrust reverser is armed.
R REV ARMED
DCU 1 APR FAIL
DCU 2 APR FAIL The respective DCU has failed its APR test.
DCU 3 APR FAIL
L ENG ECU FAIL
The respective engine ECU failed to respond to an APR test.
R ENG ECU FAIL
POWER PLANT
Description
Vol. 2 19−10−32
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
POWER SUPPLY AND CIRCUIT BREAKER SUMMARY
SYSTEM SUB−SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION NOTES
Power Plant
Ignition System
ENG IGN A
AC ESS 3 C7
DC BATT 1
L7
ENG IGN B
L8
BATT BUS 5 A1
Starter System
ENG START L
DC BATT 1
L10
ENG START R L9
Oil Pressure
Indications
L OIL PRESS
TRANS L6
R OIL PRESS
TRANS DC ESS 4 B6
OIL BYPASS
IND DC APU
BATT
DIRECT
5
B3
ENG OIL
POWER B4
Vibration Monitor ENG VIB MON AC BUS 1 1 C7
Thrust Reversers
THRUST REV
AUTO STOW 1
DC ESS 4
A4
THRUST REV
AUTO STOW 2 A5
THRUST REV 1 A6
THRUST REV 2 A7
Pneumatics
Supply
Bleed Leak Test
and Control
B/LEAK TEST B12
B/LEAK L DET
AC ESS 3
B1
B/LEAK R DET B2
10th Stage
10 ST B/AIR
ISOL
DC ESS 4
B11
10 ST B/AIR
SOV L C11
10 ST B/AIR
SOV R DC BUS 2 2 F11
14th Stage
14 ST B/AIR
ISOL SOV
DC BUS 1 1
F13
14 ST B/AIR
SOV L F12
14 ST B/AIR
SOV R DC BUS 2 2 F12
POWER PLANT
Summary
Vol. 2 19−20−1
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
POWER PLANT
Summary
Vol. 2 19−20−2
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6

　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：龐巴迪挑戰(zhàn)者604操作手冊 Operating Manual 4(96)