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TARPS ECS Lights Illuminate ............................................................................................1..4..-.2..7.
SENSOR COND Light Illuminated and/or PUMP Phase Circuit Breakers
Popped or APG-71 PM Acronym.. ......................................................................................1..4..-.2...8
Cockpit TemperatureC ontrol Malfunction.. .........................................................................1..4..-.2. 8
Cockpit Overpressurixationo n Deck ...................................................................................1..4..-.2..8
CABIN PRESS Light .........................................................................................................1..4..-.2..8..
WSHLD HOT Light ...........................................................................................................1..4..-.2..8..
OXYGEN SYSTEM FAILURE .........................................................................................1..4..-.2...9
OBOGS Light ....................................................................................................................1..4..-.2..9.. .
B/U OXY LOW Light (Both Cockpits) ................................................................................1..4..-.2. 9
B/U OXY LOW Light (Pilot Only). .....................................................................................1..4..-.3..0
B/IJ OXY LOW Light (RIO Only). ......................................................................................1..4..-.3..0
LAD/CANOPY LIGHT AND/OR LOSS OF CANOPY.. .....................................................1..4..- 30
LAD/CANOPY Light With RIO CANOPY Light/Canopy LOSS.. ..........................................1..4. -30
LAD/CANOPY Light Without RIO CANOPY Light.. ..........................................................1..4..- 31
HYDRAULIC SYSTEM MALFUNCTIONS ......................................................................1..4..-.3. 1
Combined PressureA pproximately 2,400 to 2,600 Psi... ........................................................1..4..- 31
Flight PressureA pproximately 2,400 to 2,600 Psi .................................................................1..4..-.3 1
Combined PressureZ ero... ...................................................................................................1..4..-.3..2.
Flight PressureZ ero ............................................................................................................1..4..-.3..3..
Both Combined and Flight PressureZ ero .............................................................................1..4..-.3. 3
Backup Flight Module Malfunction .....................................................................................1..4..-.3..5
65 ORIGINAL
.\ .\ \ \\ .\
NAVAIR 01.F14AAD-1
14.1
14.1
14.1
,l,
.l,
.l,
.I
.8
.9
Page
No.
Controllability Check . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14-35
Outboard Spoiler Module Malfunction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 14-36
Low Brake Accumulator Pressure. . .. . .. .. . .. . . . .. . .. . .. .. . .. . .. .. . .. . . .. . .. . .. .. .. . .. . .. . .. . .. . . .. . .. . .. . . .. . .. . .. . .. .. . .. . .. . . 14-36
14.12
14.12.1
14.12.2
14.12.3
14.12.4
14.12.5
14.12.6
14.12.7
14.12.8
14.12.9
14.12.10
14.12.11
14.12.12
14.12.13
14.12.14
14.13
14.13.1
14.13.2
14.13.3
FLIGHT CONTROL FAILURES OR MALFUNCTIONS ....................................................1..4. -37
UncommandedR oll and/or Yaw ..........................................................................................1..4..-.3..7
Yaw Channel Failure .........................................................................................................1..4..-.3..7..
Pitch or Roll Channel Failure ...............................................................................................1..4..-.3..7
STAB AUG Transients... ............................................................................................... .............1. 4-38
RudderA uthority Failure.. ...................................................................................................1..4..-.3..8.
Horizontal Tail Authority Failure.. .......................................................................................1..4..-.3..9
Spoiler Malfunction.. ..........................................................................................................1..4..-.3..9..
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F-14D 飞行手册 Flight Manual 2(84)
