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disconnected.
(1) Autopilot ...............................................................DISCONNECT
(2) AFCS SEL 1 (2)..............................................................SELECT
operative channel.
(3) FDs and autopilot ......................................................... ENGAGE
and monitor operation. Retrim as required.
FD annunciator flag displayed on both PFDs:
Yes
(4) Flight control panel XFR .........................................SELECT
to operable side.
− END −
No
Sensor failure indicated (red line across affected flight director
mode annunciator):
Yes
(4) Affected mode switch ........................................DESELECT
− END −
No
(4) No further action required.
END
ABNORM 3-5
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
ABNORM 3-6
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUTOMATIC FLIGHT
CONTROL SYSTEM
THIS PAGE INTENTIONALLY LEFT BLANK
CONTENTS PAGE
• APU LCV FAIL .........................................................ABNORM 4−2
• APU OIL PRESS ......................................................ABNORM 4−2
• APU OIL TEMP ........................................................ABNORM 4−3
• APU SOV .................................................................ABNORM 4−3
• APU NEG-G SOV ....................................................ABNORM 4−4
• APU PUMP ..............................................................ABNORM 4−4
ABNORM 4-1
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUXILIARY POWER UNIT
MALFUNCTIONS
APU LCV FAIL
APU LCV FAIL
(1) L 10TH STAGE bleed....................................................CLOSED
(2) 10TH STAGE ISOL ......................................................... CLOSE
(3) L PACK................................................................................. OFF
Above 40,000 feet:
Yes
(4) L COWL ANTI-ICE ......................................................... ON
− END −
No
(4) No further action required.
END
APU OIL PRESS
APU OIL PRESS
........APU automatically shuts down.
APU is supplying bleed air for air-conditioning:
Yes
(1) PACKs.............................................................. TRANSFER
to engine bleeds.
No
(1) APU PWR FUEL .................................................................. OFF
(2) Do not restart APU.
END
ABNORM 4-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUXILIARY POWER UNIT
MALFUNCTIONS
APU OIL TEMP
APU OIL TEMP
........APU automatically shuts down.
APU is supplying bleed air for air-conditioning:
Yes
(1) PACKs.............................................................. TRANSFER
to engine bleeds.
No
(1) APU PWR FUEL .................................................................. OFF
(2) Do not restart APU.
END
APU SOV
APU SOV
APU was shut down due to fire:
Yes
APU is supplying bleed air for air-conditioning:
Yes
(1) PACKs.......................................................TRANSFER
to engine bleeds.
No
(1) APU PWR FUEL........................................................... OFF
(2) Land at the nearest suitable airport.
− END −
No
(1) No further action required. The APU is not available.
END
ABNORM 4-3
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
AUXILIARY POWER UNIT
MALFUNCTIONS
APU NEG-G SOV
APU NEG-G SOV
APU was shut down due to fire:
Yes
(1) L BOOST PUMP........................................................... OFF
Left engine:
(2) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
No
(1) Land at the nearest suitable airport.
END
APU PUMP
APU PUMP
On ground:
Yes
(1) APU ................................................................ SHUTDOWN
− END −
No
In flight:
APU GEN is essential:
Yes
(1) APU indications ...................................................MONITOR
(2) Land at the nearest suitable airport.
CAUTION
APU adapter oil will no longer be
cooled. Adapter oil will overheat
causing APU to auto-shutdown.
− END −
No
(1) APU........................................................................ SHUTDOWN
　
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