Learjet 36A - Fuel Crossflow (Wing-Ta-Wing Fuel Transfer)

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FUEL MANAGEMENT (CONT)
FUEL CROSSFLOW (WING-TO-WING FUEL TRANSFER)
'CAUTION I~
Do not crossflow with jet pump inoperative. Engine
starvation may occur due to
fuel being pumped through
open cross flow valve into opposite wing.
1. CROSSFLOW Switch - OPEN.
2. STANDBY PUMP Switch (heavy wing) - ON.
3. STANDBY PUMP Switch (light wing) - Off.
4. CROSSFLOW Switch - CLOSE after fuel balance is obtained.
5.
STANDBY PUMP Switches - Off.
6. If the preceding procedure fails to balance fuel, unequal power set-
tings may
be used to balance fuel load.
2-62
FAA APPROVED 4-30-76
REISSUED 2-25-81. CHANGE 12