MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
M-7-260C
SECTION II
LIMITATIONS
2.3
FLIGHT LOAD FACTORS:
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Flaps Extended: 1.9g Positive to 0g Negative
2.4
PLACARDS:
The following placards are in the cockpit in clear view of the pilot:
"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN COM-
PLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE
FLIGHT MANUAL
AND IN THE FORM OF PLACARDS AND MARKINGS.”
"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."
"ROUGH AIR OR MANEUVERING SPEED 109K (125 MPH) I.A.S."
"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 SAFE-
LY IN FLIGHT.
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AIRPLANE
FLIGHT MANUAL."
"DEMONSTRATED CROSSWIND 12K (14 MPH)"
On the instrument panel at the auxiliary tank transfer switches:
FUEL TRANSFER PUMPS
PUSH FOR
PUSH FOR
AUX. QUANT. AUX. QUANT.
LEFT
RIGHT
NOTE: If JPI EDM-900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and placards
are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are used as
below:
FUEL TRANSFER PUMPS
LEFT RIGHT
FUEL CAPACITY:
MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS * GAL.
USABLE EACH.
* 15 Gal. or 21 Gal. Instrument Panel Placard will show capacity of the tanks installed in this aircraft.
FAA APPROVED: 10/19/98
Rev. F dated:
PAGE 5
Rev. I dated:
Rev. J dated: 7/16/18
