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 (½
Lock "T" handle ½ turn right before releasing right rudder pressure. If too much trim,
move handle in until trim is
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 prio
feet.
////////////////////////
////CAUTION////
////////////////////////
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
F. CROSSWIND LANDINGS & TAKEOFFS:
Maximum demonstrated
should be limited to 0
the maximum demonstrated for certification of the airplane and is not considered
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 switche
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 will
force excess fuel overboard, it is recommen
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
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
decrease on the respective auxiliary tank indicator.
FAA APPROVED: 6/3/93
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE
MX-7-180A
NORMAL FLIGHT OPERATIONS:
(Cont'd)
full effectiveness of the Right Rudder Trim:
½ 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,
move handle in until trim is correct and then lock.
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
SWITCH IS OFF
CROSSWIND LANDINGS & TAKEOFFS:
Maximum demonstrated crosswind component is 13K (15 mph) and flap extension
should be limited to 0
°
(fully retracted) with such crosswind or higher. 13K (15 mph) is
the maximum demonstrated for certification of the airplane and is not considered
limiting with flaps at 0
°
.
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 will
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
decrease on the respective auxiliary tank indicator.
PAGE 12
SECTION III
NORMAL PROCEDURES
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
r to recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
crosswind component is 13K (15 mph) and flap extension
(fully retracted) with such crosswind or higher. 13K (15 mph) is
the maximum demonstrated for certification of the airplane and is not 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
s 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 will
ded 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
one half. Confirm fuel transfer by illumination of the
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
