MAULE AEROSPACE TECHNOLOGY, INC.
4.12
ENGINE FIRE DURING FLIGHT:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2.
4.13
SMOKE AND FUME ELIMINATION:
1.
2. Cabin Air Knob
3.
4. Pilot's Window
4.14
1. On Takeoff -
2.
3.
Climb to safe stall recovery altitude
4.
Notify appropriate controlling agency, if appropriate.
5.
Determine control difficulty airspeed by slowing down while flying straight ahead.
Do not allow the aircraft to stall.
6.
Make full stop landing using 4 to 9K (5 to 10 mph) above difficulty airspeed or
above normal approach speed, whichever is higher.
4.15
RECOVERY FROM INADVERTENT SPINS:
Intentional spins are prohibited. If the aircraft inadvertently enters a spin, simult
apply full rudder opposite to the direction of rotation and full nose down elevator with
ailerons neutral and reduce power to idle. When the rotation stops, neutralize the rudder
and elevator, and ease back on the control wheel as required to smo
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during
recovery.
4.16
Alternator output should be monitored by reference to the ammeter located on the right side
of the engine in
strument cluster. Should the ammeter indicate a minus deflection when
engine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated,
push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not
reset, reduce
the electrical load as much as possible, land as soon as practical and
investigate the electrical system malfunction before further flight.
FAA APPROVED: 6/3/93
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
MAULE MX-7-180A
ENGINE FIRE DURING FLIGHT:
Accomplish ENGINE EMERGENCY SHUT DOWN
SMOKE AND FUME ELIMINATION:
- In
In
- Open
Open (below 104K (120 mph)
controllable airspeed
Climb to safe stall recovery altitude
Notify appropriate controlling agency, if appropriate.
Determine control difficulty airspeed by slowing down while flying straight ahead.
Do not allow the aircraft to stall.
Make full stop landing using 4 to 9K (5 to 10 mph) above difficulty airspeed or
above normal approach speed, whichever is higher.
RECOVERY FROM INADVERTENT SPINS:
Intentional spins are prohibited. If the aircraft inadvertently enters a spin, simult
apply full rudder opposite to the direction of rotation and full nose down elevator with
ailerons neutral and reduce power to idle. When the rotation stops, neutralize the rudder
and elevator, and ease back on the control wheel as required to smo
othly regain level flight.
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during
:
Alternator output should be monitored by reference to the ammeter located on the right side
strument cluster. Should the ammeter indicate a minus deflection when
engine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated,
push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not
the electrical load as much as possible, land as soon as practical and
investigate the electrical system malfunction before further flight.
PAGE 16
Determine control difficulty airspeed by slowing down while flying straight ahead.
Make full stop landing using 4 to 9K (5 to 10 mph) above difficulty airspeed or
Intentional spins are prohibited. If the aircraft inadvertently enters a spin, simult
aneously
apply full rudder opposite to the direction of rotation and full nose down elevator with
ailerons neutral and reduce power to idle. When the rotation stops, neutralize the rudder
othly regain level flight.
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during
Alternator output should be monitored by reference to the ammeter located on the right side
strument cluster. Should the ammeter indicate a minus deflection when
engine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated,
push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not
the electrical load as much as possible, land as soon as practical and
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