MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
NORMAL PROCEDURES:
3.1
PREFLIGHT INSPECTION:
A. INTERIOR:
1. BAT Switch…………………………………...
2. Fuel Gauges…………………………………
3. Auxiliary Fuel Pumps………………………
4. All Electrical Switches………………………
5. BAT Switch……………………………………
6. Flaps…………………………………………
EXTERIOR: Begin at the left front door, proceed around the left wing to the nose area,
then around the right wing and back to the fuselage, then around the tail
section.
1. Fuel drains behind step……………………
2. Left Flap………………………………………
3. Aileron…………………………………………
4. Left Wing Top………………………………
5. Left Wing Main & Aux Fuel Tank Drain……
6. Left Wing Tip & Nav Light…………………
7. Auxiliary Fuel Tank.....................................
8. Landing Light…………………………………
9. Left Wing Tiedown…………………………
10. Pitot Tube……………………………
11. Stall Warning Switch………………………
12. Main Fuel Tank…………………………….…
13. Left Landing Gear……………………………
14. Bottom left side of Cowl……………………
15. Top Cowl, Oil Access Door…………………
16. Propeller……………………………………...
17. Air Inlets……………………………………….
FAA APPROVED
DATE: 8/26/96
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180C
NORMAL PROCEDURES:
PREFLIGHT INSPECTION:
BAT Switch…………………………………..... ON
Fuel Gauges…………………………………… CHECK INDICATIONS
Auxiliary Fuel Pumps………………………… ON, THEN OFF (LISTEN TO VERIFY
OPERATION)
All Electrical Switches………………………… OFF
BAT Switch……………………………………. OFF
Flaps…………………………………………… FULL DOWN (4TH NOTCH)
Begin at the left front door, proceed around the left wing to the nose area,
then around the right wing and back to the fuselage, then around the tail
Fuel drains behind step……………………… DRAIN (2)
Left Flap……………………………………….. CHECK HINGES & CONTROL
ATTACHMENTS
Aileron…………………………………………. CHECK HINGES & CONTROL
ATTACHMENTS
Left Wing Top………………………………… CHECK FOR WRINKLES AS INDIC
TION OF INTERNAL DAMAGE
Left Wing Main & Aux Fuel Tank Drain……. DRAIN (2)
Wing Tip & Nav Light…………………… CHECK FOR DAMAGE
Auxiliary Fuel Tank....................................... VISUALLY CHECK QUANTITY
Landing Light………………………………….. CHECK FOR DAMAGE
Left Wing Tiedown……………………………. REMOVE
Pitot Tube……………………………………… REMOVE COVER
Stall Warning Switch…………………………. CHECK FOR FREEDOM OF MOV
MENT
Main Fuel Tank…………………………….…. VISUALLY CHECK QUANTITY
Left Landing Gear……………………………. CHECK TIRE INFLATION AND
BRAKE LINE SECURITY
left side of Cowl……………………… DRAIN GASCOLATOR (1)
Top Cowl, Oil Access Door………………….. CHECK OIL QUANTITY
Propeller……………………………………..... CHECK LEADING EDGE FOR
DAMAGE. CHECK SPINNER FOR
SECURITY
Air Inlets……………………………………….. CHECK FOR FOREIGN OBJ
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
PAGE 7
SECTION III
NORMAL
PROCEDURES
CHECK INDICATIONS
ON, THEN OFF (LISTEN TO VERIFY
FULL DOWN (4TH NOTCH)
Begin at the left front door, proceed around the left wing to the nose area,
then around the right wing and back to the fuselage, then around the tail
CHECK HINGES & CONTROL
CHECK HINGES & CONTROL
CHECK FOR WRINKLES AS INDICA-
TION OF INTERNAL DAMAGE
CHECK FOR DAMAGE
VISUALLY CHECK QUANTITY
CHECK FOR DAMAGE
REMOVE COVER
CHECK FOR FREEDOM OF MOVE-
VISUALLY CHECK QUANTITY
CHECK TIRE INFLATION AND
BRAKE LINE SECURITY
DRAIN GASCOLATOR (1)
CHECK OIL QUANTITY
CHECK LEADING EDGE FOR
CHECK SPINNER FOR
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
