MAULE MX-7-180 - Flight Load Factors; Placards

MAULE AEROSPACE TECHNOLOGY, INC.
2.3 FLIGHT LOAD FACTORS:
NOTE:
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic
controls can be applied (V
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
AND IN THE
FORM OF PLACARDS AND MARKINGS.
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVE
MANEUVERING SPEED: 109K (125
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SEC
FLIGHT MANUAL.
THIS AIRPLANE
APPROVED FOR DAY OR NIGHT IFR NON
EQUIPPED IN ACC
ORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIG
FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
USED SAFELY IN FLIGHT.
Located on flap control handle:
FLAPS / PULL ON / 2
ND
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
DATE: 12/18/84
Rev. A dated: 4/25/85
Rev. D dated: 6/10/94
Rev. D dated:
Rev. G dated:
Page 5
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II
AIRPLANE FLIGHT MANUAL
LIMITATIONS
MAULE MX-7-180
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
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
FORM OF PLACARDS AND MARKINGS.
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVE
D.
MANEUVERING SPEED: 109K (125
MPH) I.A.S.
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SEC
TION OF AIRPLANE
APPROVED FOR DAY OR NIGHT IFR NON
-
ICING FLIGHT WHEN
ORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIG
HT 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.
CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A" 100
LBS.
MAX. LOAD AREA "B" 175
LBS.
MAX. LOAD AREA "C" 125
LBS.
Cabin Area when optional 5th seat is inst
alled:
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
SECTION II
LIMITATIONS
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic
marked on the airspeed
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FLIGHT
MANUAL
TION OF AIRPLANE
ICING FLIGHT WHEN
HT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
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