4.11 Electrical Fire; Engine Fire During Flight; Smoke And Fume Elimination; Damage - MAULE MX-7-180AC Airplane Flight Manual

4.11 ELECTRICAL FIRE:

1. Master Switch -

4.12 ENGINE FIRE DURING FLIGHT:

ENGINE FIRE DURING FLIGHT:
1. Accomplish ENGINE EMERGENCY SHUT Accomplish ENGINE EMERGENCY SHUT DOWN
2. Make forced landing Make forced landing

4.13 SMOKE AND FUME ELIMINATION:

SMOKE AND FUME ELIMINATION:
1. Cabin Heat Knob Cabin Heat Knob - IN
2. Cabin Air Knob - IN Cabin Air Knob
3. Upper Air Vents - OPEN Upper Air Vents
4. Pilot's Window -
4.14 STRUCTURAL DAMAGE: STRUCTURAL DAMAGE:
1. On Takeoff - Abort
2. In flight, maintain controllable airspeed
3. Climb to safe stall recovery altitude Climb to safe stall recovery altitude
4. Notify appropriate controlling agency, if appropriate. Notify appropriate controlling agency, if appropriate.
5. Determine control difficulty airspeed by slowing down while flying straight ahead. Do Determine control difficulty airspeed by slowing down while flying straight ahead. Do Determine control difficulty airspeed by slowing down while flying straight ahead. Do
not allow the aircraft to stall. not allow the aircraft to stall.
6. Make full stop landing using Make full stop landing using 4 to 9K (5-10 mph) above difficulty airspeed or above
normal approach speed, whichever is higher. normal approach speed, whichever is higher.

4.15 RECOVERY FROM INADVERTENT SPINS:

RECOVERY FROM INADVERTENT SPINS:
Intentional spins are prohibited. If the aircraft inadvertently enters a spin, Intentional spins are prohibited. If the aircraft inadvertently enters a spin, simultaneously Intentional spins are prohibited. If the aircraft inadvertently enters a spin,
apply full rudder opposite to the direction of rotation and full nose down elevator with ail apply full rudder opposite to the direction of rotation and full nose down elevator with ail apply full rudder opposite to the direction of rotation and full nose down elevator with aile-
rons neutral and reduce power to idle. When the rotation stops, neutralize the rudder and rons neutral and reduce power to idle. When the rotation stops, neutralize the rudder and rons neutral and reduce power to idle. When the rotation stops, neutralize the rudder and
elevator, and ease back on the control wheel as required elevator, and ease back on the control wheel as required to smoothly regain level flight.
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during recov- Wing flaps should be retracted to avoid exceeding the maximum flap speeds during reco Wing flaps should be retracted to avoid exceeding the maximum flap speeds during reco
ery.

4.16 ALTERNATOR FAILURE

ALTERNATOR FAILURE:
Alternator output should be monitored by reference to the ammeter located on the right side Alternator output should be monitored by reference to the ammeter located on the right side 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 e ne instrument cluster. Should the ammeter indicate a minus deflection when en- ne instrument cluster. Should the ammeter indicate a minus deflection when e
gine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated, gine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated, gine 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 push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not 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 invest educe the electrical load as much as possible, land as soon as practical and invest educe the electrical load as much as possible, land as soon as practical and investi-
gate the electrical system malfunction before further flight. gate the electrical system malfunction before further flight.
FAA APPROVED: 5/4/00
Rev. A dated:
MAULE AEROSPACE TECHNOLOGY, INC. MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MX-7-180AC
MAULE
OFF
- OPEN below 104K (120 mph)
Abort
maintain controllable airspeed
above difficulty airspeed or above
to smoothly regain level flight.
PAGE 16
SECTION IV
EMERGENCY
PROCEDURES