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.
In flight, maintain controllable airspeed
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 al
low 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
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 t
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
of the engine instrument 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
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
DATE: 12/18/93
REV. A Dated: 4/25/85
REV. D Dated:
Page 16
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION IV
MAULE MX-7-180
ENGINE FIRE DURING FLIGHT:
Accomplish ENGINE EMERGENCY SHUT DOWN
SMOKE AND FUME ELIMINATION:
- In
In
- Open
Open (below 104K (120 mph)
In flight, maintain 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.
low 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, simultaneously
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 t
he control wheel as required to smoothly 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
of the engine instrument 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
reset, reduce the electrical load as much as possible, land as soon as practical and
investigate the electrical system malfunction before further flight.
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
inadvertently enters a spin, simultaneously
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
he control wheel as required to smoothly 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
of the engine instrument 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
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