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MAULE MX-7-180B - Page 18

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MAULE AEROSPACE TECHNOLOGY, INC.
3.3
NORMAL FLIGHT OPERATIONS:
D. RUDDER TRIM:
NOTE: To assure full effectiveness of the Right Rudder Trim:
Unlock "T" handle (1/2 turn left), depress right rudder as you pull "T" handle full out.
Lock "T" handle ½ turn right before releasing right rudder pressure. If too
move handle in until trim is correct and then lock.
E. STALLS:
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above
the stall speed. Loss of altitude prior to recovery from a stall may be as much as 300
feet.
////////////////////////
////CAUTION////
////////////////////////
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
F. CROSSWIND
LANDINGS & TAKEOFFS:
Maximum demons
trated crosswind component is 10K (12
should be limited to 0
the maximum demonstrated for certification of the airplane and is n
limiting with flaps at 0
G.
FUEL SYSTEM MANAGEMENT:
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector
valve on the left kick panel. Auxiliary (outboard) tanks feed their respective main tanks
via
transfer pumps that are controlled by switches on the instrument panel. These
transfer pumps transfer fuel at a rate of 0.4 gallons per minute or approximately 45
minutes for a full auxiliary tank. Since overfilling a main tank from an auxiliary tank wil
force excess fuel overboard, it is recommended that the transfer pumps not be activated
until their respective main tanks are slightly more than one quarter full. If the tank being
transferred to is feeding the engine, however, transfer can be initiated
tank is down to approximately one half. Confirm fuel transfer by illumination of the
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
decrease on the respective auxiliary tank indicator.
FAA APPROVED: 7/12/93
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180B
NORMAL FLIGHT OPERATIONS:
(Cont'd)
NOTE: To assure full effectiveness of the Right Rudder Trim:
move handle in until trim is correct and then lock.
SWITCH IS OFF
LANDINGS & TAKEOFFS:
trated crosswind component is 10K (12
mph) and flap extension
should be limited to 0
° (fully retracted) wi
th such crosswind or higher. 10K (12
the maximum demonstrated for certification of the airplane and is n
ot considered
limiting with flaps at 0
°.
FUEL SYSTEM MANAGEMENT:
decrease on the respective auxiliary tank indicator.
PAGE 12
SECTION III
NORMAL PROCEDURES
Unlock "T" handle (1/2 turn left), depress right rudder as you pull "T" handle full out.
Lock "T" handle ½ turn right before releasing right rudder pressure. If too
much trim,
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above
the stall speed. Loss of altitude prior to recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
mph) and flap extension
th such crosswind or higher. 10K (12
mph) is
ot considered
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector
valve on the left kick panel. Auxiliary (outboard) tanks feed their respective main tanks
transfer pumps that are controlled by switches on the instrument panel. These
transfer pumps transfer fuel at a rate of 0.4 gallons per minute or approximately 45
minutes for a full auxiliary tank. Since overfilling a main tank from an auxiliary tank wil
l
force excess fuel overboard, it is recommended that the transfer pumps not be activated
until their respective main tanks are slightly more than one quarter full. If the tank being
transferred to is feeding the engine, however, transfer can be initiated
when the main
tank is down to approximately one half. Confirm fuel transfer by illumination of the
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a

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