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to determine location of leak.
Expedite landing if tank quantity gauge
indications are amber.
NOTE
1. The minimum fuel quantity for go-around is 230 kg
(500 lb) per wing (with the airplane level), and
assuming a maximum airplane climb attitude of
10° nose up.
2. Do not action FUEL IMBALANCE, L (R) FUEL LO
PRESS or L (R) SCAV EJECTOR caution
messages or L (R) MAIN EJECTOR FAIL status
messages. Disregard fuel imbalance limitations.
(3) Autopilot ......................................................................MONITOR
NOTE
Anticipate out of trim situation when disconnecting
autopilot.
Fuel leak from engine is suspected:
Yes
On low quantity side:
(4) Thrust lever..........................................CONFIRM and IDLE
(5) Thrust lever................................CONFIRM and SHUT OFF
(6) Affected ENG FIRE ....................................................PUSH
(7) In-Flight Engine
Failure/Shutdown..........................................ACCOMPLISH
(See Page ABNORM 1–2)
− END −
ABNORM 9-22
REV 74, Nov 07/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Fuel Leak (Cont’d)
No
Fuel leak from wing tank is suspected:
(4) GRAVITY/XFLOW........................................................... CLOSE
Range is a consideration:
Yes
NOTE
Consider use of asymmetric thrust to use as much fuel as
possible from the leaking tank.
Leak in auxiliary tank is confirmed:
Yes
(5) TAIL TANK TRANSFER,
MANUAL OVRD............................................MANUAL
(6) Auxiliary tank quantity .................................MONITOR
When auxiliary tank quantity has stabilized:
(7) PRI TAIL TANK TRANSFER...................................ON
Ensure auxiliary and tail tank quantities remain
within limits.
− END −
No
Leak in tail tank is confirmed:
Yes
(5) TAIL TANK TRANSFER,
MANUAL OVRD............................................MANUAL
(6) PRI and SEC TAIL TANK
TRANSFER.............................................................ON
Ensure auxiliary and tail tank quantities remain
within limits.
When AUX TANK HEAVY caution message is
displayed:
(7) PRI and SEC TAIL TANK
TRANSFER...........................................................OFF
− END −
No
ABNORM 9-23
REV 74, Nov 07/08
▼
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
Fuel Leak (Cont’d)
Leak in wing tank is confirmed:
Yes
(5) Affected L (R) TO AUX
XFLOW...............................................................OPEN
NOTE
Anticipate increasing lateral trim and control
forces.
When trim or control forces becomes excessive:
(6) L (R) TO AUX XFLOW .....................................CLOSE
(7) Repeat steps (5) and (6), as necessary to conserve
as much fuel as possible from the leaking tank.
(8) Tank quantities ............................................MONITOR
NOTE
Consider use of asymmetric thrust to maintain
fuel imbalance within limits.
No
(5) Tank quantities ............................................................MONITOR
NOTE
Consider use of asymmetric thrust to maintain fuel
imbalance within limits.
Landing with a FUEL IMBALANCE caution message:
Yes
NOTE
Select the longest runway available with minimum
turbulence and crosswind.
Prior to landing:
(6) GPWS/FLAP OVRD
(if installed) ................................................................ OVRD
(7) Landing flaps .................................................................. 20°
(8) Approach speed ...................................................VREF + 14
minimum.
(9) Actual landing distance...................................... INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.55 (55%) 1.50 (50%)
− END −
No
(6) No further action required.
END
ABNORM 9-24
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15 FUEL MALFUNCTIONS
CONTENTS PAGE
• HYD 1 LO PRESS ..................................................ABNORM 10−2
• HYD 2 LO PRESS ..................................................ABNORM 10−3
• HYD 3 LO PRESS ..................................................ABNORM 10−4
• HYD 1 (2) HI TEMP ................................................ABNORM 10−5
• HYD 3 HI TEMP .....................................................ABNORM 10−6
　
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