MAULE AEROSPACE TECHNOLOGY, INC.
4.11 ELECTRICAL FIRE:
1.
Master Switch -
4.12 ENGINE FIRE DURING FLIGHT:
1.
Accomplish ENGINE EMERGENCY SHUT
2.
Make forced landing
4.13 SMOKE AND FUME ELIMINATION:
1.
Cabin Heat Knob
2.
Cabin Air Knob
3.
Upper Air Vents
4.
Pilot's Window -
4.14 STRUCTURAL DAMAGE:
1.
On Takeoff - Abort
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 allow the aircraft to stall.
6.
Make full stop landing using
normal approach speed, whichever is higher.
4.15 RECOVERY FROM INADVERTENT SPINS:
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
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
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during reco
ery.
4.16 ALTERNATOR FAILURE
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
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
reset, reduce the electrical load as much as possible, land as soon as practical and invest
gate the electrical system malfunction before further flight.
FAA APPROVED: 5/4/00
Rev. A dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180AC
OFF
ENGINE FIRE DURING FLIGHT:
Accomplish ENGINE EMERGENCY SHUT DOWN
Make forced landing
SMOKE AND FUME ELIMINATION:
Cabin Heat Knob - IN
Cabin Air Knob - IN
Upper Air Vents - OPEN
- OPEN below 104K (120 mph)
STRUCTURAL DAMAGE:
Abort
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. Do
not allow the aircraft to stall.
Make full stop landing using 4 to 9K (5-10 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,
apply full rudder opposite to the direction of rotation and full nose down elevator with ail
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 to smoothly regain level flight.
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during reco
ALTERNATOR FAILURE:
Alternator output should be monitored by reference to the ammeter located on the right side
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,
push ALT switch OFF then ON. Repeat two times as necessary to reset. If system will not
educe the electrical load as much as possible, land as soon as practical and invest
gate the electrical system malfunction before further flight.
PAGE 16
SECTION IV
EMERGENCY
PROCEDURES
Determine control difficulty airspeed by slowing down while flying straight ahead. Do
above difficulty airspeed or above
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 aile-
rons neutral and reduce power to idle. When the rotation stops, neutralize the rudder and
to smoothly regain level flight.
Wing flaps should be retracted to avoid exceeding the maximum flap speeds during recov-
Alternator output should be monitored by reference to the ammeter located on the right side
ne instrument cluster. Should the ammeter indicate a minus deflection when en-
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
educe the electrical load as much as possible, land as soon as practical and investi-
