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时间:2010-04-23 13:55来源:蓝天飞行翻译 作者:admin
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DCU 2 INOP 2 IRS 2 ON BATT <0025> 12 YD 1 INOP 11
DCU 3 INOP <0019> 2 IRS 2 OVERTEMP <0025> 12 YD 2 INOP 11
I. Inhibits
During take-off and landing, the DCUs will process inhibit logic to minimize spurious or
distracting messages.
During take--off, the caution messages are inhibited when:
S The left and right engine N1 is greater than 79% with weight--on--wheels.
The caution message inhibit is removed when:
S Left and right engine N1 is less than 67.6%, or
S Radio altitude is greater than 400 ft AGL with the landing gear extended, or
S 30 seconds after ground to air transition.
During landing, the caution messages are inhibited when:
S Radio altitude is less than 400 ft AGL with the landing gear extended.
The caution message inhibit is removed:
S 30 seconds after air to ground transition.
Vol. 1 02--20--19
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual
CSP A--013
MASTER
The following caution messages and their corresponding switchlights (if applicable) are
not inhibited during tale--off and/or landing.
AIRCRAFT SYSTEM CAUTION MESSAGE (Not Inhibited)
Power Plant APR INOP
L (R) REV UNLOCKED
L (R) REV UNSAFE
Automatic Flight Control System AP TRIM LWD (RWD) (ND) (NU)
AP PITCH TRIM
YAW DAMPER
Fire Protection APU BTL LO
ENG BTL 1 (2) LO
Flight Controls FLAPS FAIL
FLT SPLR DEPLOY
FLT SPLRS
L (R) FLT SPLR
IB (OB) GND SPLR
GLD NOT ARMED
GLD UNSAFE
GND SPLR DEPLOY
L (R) SPOILERON
SPOILERONS
SPOILERONS ROLL
STAB TRIM
Fuel L (R) FUEL LO PRESS
Hydraulic Power HYD 1 (2) (3) LO PRESS
Instruments EFIS COMP MON
Landing Gear A/SKID INBD (OUTBD)
IB/OB BRAKE PRESS
STEERING INOP
WOW INPUT (OUTPUT)
Miscellaneous SMOKE TOILET
J. Inhibits <0039>
During the initial take-off, final take-off and landing phases, the DCU’s will process
inhibit logic to minimize intermittent or distracting warning or caution messages.
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND Vol. 1 02--20--20
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual MASTER
CSP A--013
(1) Initial Take-off Phase
The initial take-off inhibits are enabled when:
S Left and right engine N1 is greater than 79%,
S Weight-on-wheels, and
S Airspeed is less than 100 knots.
The initial take-off inhibit is removed when:
S Left and right engine N1 is less than 67.6%, or
S Aircraft is in the final take-off phase.
(2) Final Take-off Phase
The final take-off inhibits are enabled when:
S Left and right engine N1 is greater than 79%, and
S Airspeed transitions to greater than 100 knots.
The final take-off inhibit is removed when:
S Left and right engine N1 is less than 67.6%, or
S Radio altitude is greater than 400 ft AGL, or
S 30 seconds after ground to air transition.
(3) Landing Phase
Landing phase inhibits are enabled when:
S Radio altitude transitions to less than 400 ft AGL, and
S Landing gear down and locked.
The landing phase inhibit is removed when:
S 30 seconds after air to ground transition or
S Radio altitude is less than 400 ft AGL for 3 seconds.
Vol. 1 02--20--21
REV 56, Jan 31/03
AURAL/VISUAL INDICATING AND
RECORDING
Engine Indication and Crew Alerting System
Flight Crew Operating Manual
CSP A--013
MASTER
K. Warnings That Are Not Inhibited <0039>
The following warning messages, their corresponding switchlights and aurals are not
inhibited during initial take-off and/or landing:
Aircraft System Warning Message
(NOT Inhibited)
Aural
(NOT Inhibited)
Air--Conditioning and
Pressurization
L (R) 10TH DUCT BLEED AIR DUCT
Aural/Visual Warning System CONFIG AILERON
CONFIG AP
CONFIG FLAPS
CONFIG RUDDER
CONFIG SPLRS
CONFIG STAB
PARKING BRAKE
CONFIG TRIM
CONFIG AUTOPILOT
CONFIG FLAPS
CONFIG TRIM
CONFIG SPOILERS
CONFIG STAB
CONFIG BRAKES
Automatic Flight Control
System
Autopilot Cavalry Charge
Altitude C--Chord
Auxiliary Power Unit APU OVERTEMP APU
Fire Protection APU FIRE
L (R) ENG FIRE
SMOKE CARGO
SMOKE TOILET <0037>
Firebell
Firebell
SMOKE
SMOKE
Flight Controls Stall Warbler
Overspeed Clacker
Trim Clacker
Ice and Rain Protection 14TH DUCT
ANTI--ICE DUCT
WING OVERHEAT
BLEED AIR DUCT
(anti--ice duct inhibited)
 
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