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

TRANSFER switch/light ....................................Press in to start applicable pump.
Check the following:
• PRI TAIL TANK
TRANSFER ON light on, or
• SEC TAIL TANK
TRANSFER ON light on.
(3) Fuel tank quantity readouts ................................Monitor to ensure that tail tank fuel
quantity is depleting.
Tail tank quantity is not depleting:
Yes
(4) FUEL, DUMP switch/light ..........................Press in to jettison fuel.
Check DUMP OPEN light on.
NOTE
1. Fuel jettison must only be carried out with flaps set to 0.
2. Jettisoning of fuel in known lightning conditions is
prohibited.
3. Tail tank contents will deplete from full to empty, in
approximately 30 minutes.
− END −
No
(4) No further action required.
END
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−22
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
Z. Loss of Wing Tank Fuel Quantity Indication
Indication: Wing tank fuel quantity indication dashed.
(1) ENGINE CONTROL, ENG
SPEED switches ..................................................Check both selected to ON.
(2) Airplane attitude .................................................... Level Steady heading, wings level.
(3) Engine fuel flow indications .................................. Match left and right fuel flow rates.
(4) APU................................................................Shutdown if not required.
NOTE
APU operation will increase fuel burn from right wing tank, by a rate of
100 to 300 lb/hr.
(5) Airplane trim .........................................................Adjust to achieve hands off flight.
(6) Missing fuel tank quantity ................................Calculate using FMS fuel used page and
displayed quantity indications.
(7) Fuel distribution ..................................................Monitor for wing tank fuel imbalance.
Excessive imbalance exists (more than 25% of available trim required):
Yes
Affected high tank:
(8) FUEL, L (R) TO AUX
XFLOW switch/light ...................................Press in to open crossflow valve.
Check L (R) TO AUX XFLOW
ON light on.
NOTE
Cross flow transfers fuel at a rate of approximately
15 lb/min or higher.
When excessive imbalance has been corrected:
(9) FUEL, affected L (R) TO
AUX XFLOW switch/light.........................Press out to close crossflow valve.
Check L (R) TO AUX XFLOW
ON light out.
NOTE
Increase fuel reserves by 5%.
− END −
No
(8) No further action required.
END
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−23
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
AA. Loss of Tail Tank Fuel Quantity Indication
Indication: Tail tank fuel quantity indication dashed.
(1) FUEL, TAIL TANK TRANSFER,
MANUAL OVRD switch/light .............................Press in to select manual transfer.
Check MANUAL light on.
(2) FUEL, PRI and SEC TAIL TANK
TRANSFER switch/lights...................................Press in to start both pumps.
Check the following:
• PRI TAIL TANK
TRANSFER ON light on,
and
• SEC TAIL TANK
TRANSFER ON light on.
(3) Fuel tank quantity readouts ................................Monitor to ensure that auxiliary tank
quantity does not exceed
7,000 lb.
END
AB. Loss of Totalizer Fuel Quantity Indication
Indication: Totalizer fuel quantity indication dashed.
(1) Fuel tank quantity readouts ................................Monitor sum of each tank vs fuel burn.
END
ABNORMAL PROCEDURES
Fuel
Vol. 1 05−12−24
REV 66, Feb 01/07
CL−604 Operating Manual
PSP 604−6
1. FUEL (CONT'D)
AC. Fuel Leak Procedure
Indication: Fuel leak is evident, suspected or confirmed.
(1) Diversion may be required.
NOTE
If visibility permits, a visual check from the cabin may enable
identification of the leak source.
Leak is confirmed or suspected:
(2) Land immediately at the nearest suitable airport.
CAUTION
Do not delay landing while attempting 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.
　
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