MAULE AEROSPACE
2.3 FLIGHT LOAD FACTORS:
NOTE: DESIGN MANEUVERING SPEED: The
aerodynamic controls can be applied (V
marked on the airspeed indicator.
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
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
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AIRPLANE
FLIGHT MANUAL."
"THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON
EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.”
"DO NOT TURN OFF ALTERNATOR IN FLIGHT E
"FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
USED SAFELY IN FLIGHT.
Located on flap control handle:
"FLAPS / PULL ON / 2
ND
3rd notch/landing for s/n's 22003C,
complied with
In rear cabin area:
"CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A" 100
MAX. LOAD AREA "B" 175
MAX. LOAD AREA "C" 125
Also in Rear Cabin Area when optional 5th seat is inst
"CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMUM REAR SEAT LOADING IS 170 LBS. WHEN REAR SEAT IS
INSTALLED."
FAA APPROVED: 7/12/93
Rev. A dated: 10/28/94
Rev. B dated: 5/11/95
Rev. D dated:
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II
AIRPLANE FLIGHT MANUAL
LIMITATIONS
MAULE
MX-7-180B
FLIGHT LOAD FACTORS:
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Flaps Extended: 1.9g Positive to 0g Negative
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full
aerodynamic controls can be applied (V
A
) is 109K (125 mph). This airspeed is not
marked on the airspeed indicator.
The following placards are in the cockpit in clear view of the pilot:
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) I.A.S."
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AIRPLANE
"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.
Located on flap control handle:
ND
NOTCH / TAKEOFF / 4
TH
NOTCH / LANDING." *
3rd notch/landing for s/n's 22003C, 22006C & 22007C unless Maule Mod Kit #11
"CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A" 100 LBS.
MAX. LOAD AREA "B" 175 LBS.
MAX. LOAD AREA "C" 125 LBS.
Also in Rear Cabin Area when optional 5th seat is installed:
"CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMUM REAR SEAT LOADING IS 170 LBS. WHEN REAR SEAT IS
PAGE 5
SECTION II
LIMITATIONS
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Flaps Extended: 1.9g Positive to 0g Negative
maximum safe airspeed at which full
) is 109K (125 mph). This airspeed is not
MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FLIGHT MANUAL
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AIRPLANE
ICING FLIGHT WHEN
XCEPT IN CASE OF EMERGENCY."
"FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
22006C & 22007C unless Maule Mod Kit #11
"CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMUM REAR SEAT LOADING IS 170 LBS. WHEN REAR SEAT IS
