MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
M-7-235C
2800# Upgross Per STC
SA04077CH
FAA APPROVED
DATE: 11-16-16
9 of 28
2.3 FLIGHT LOAD FACTORS:
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Flaps Extended: 1.9g Positive to 0g Negative
NOTE: DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aero-
dynamic controls can be applied (V
A
) is 109K (125 mph). This airspeed is not
marked on the airspeed indicator.
2.4 PLACARDS:
The following placards are in the cockpit in clear view of the pilot:
THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON-ICING FLIGHT WHEN
EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE USED
SAFELY IN FLIGHT.
DEMONSTRATED CROSSWIND 12K (14 mph)
When equipped with Hartzell –6R (78”) 2 blade propeller:
DO NOT EXCEED 23 INCHES M.P. BELOW 2050 RPM.
At the main fuel tank selector valve on the left kick panel:
FUEL SELECTOR VALVE
LEFT: 21.5 GAL.
OFF
BOTH
RIGHT: 21.5 GAL.
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE
IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE
FLIGHT MANUAL AND IN THE FORM OF PLACARDS AND MARKINGS.
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED.
MANEUVERING SPEED 109K (125 MPH) IAS.
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE
SECTION OF AIRPLANE FLIGHT MANUAL.