MAULE AEROSPACE TECHNOLOGY, INC.
2.3
FLIGHT LOAD FACTORS:
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
MANUAL AND IN THE FORM OF PLACARDS AND MARKINGS.”
"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."
"MANEUVERING SPEED
"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 EXCEPT IN CASE OF
"FUEL REMAINING IN TANK WHEN INDICATOR READS Z
USED SAFELY IN FLIGHT.
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
AIRPLANE FLIGHT MANUAL."
"DEMONSTRATED CROSSWIND
On the instrument panel at the auxiliary tank transfer switches:
PUSH FOR
AUX. QUANT.
NOTE: If JPI EDM-900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pl
cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are
used as below:
FUEL CAPACITY: MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS
USABLE EACH.
*15 Gal. or 21 Gal. Instrument Panel Placard will show capacity of
craft.
FAA APPROVED: 5/4/00
Rev. A dated:
Rev. B dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180AC
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Flaps Extended: 1.9g Positive to 0g Negative
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
MANUAL AND IN THE FORM OF PLACARDS AND MARKINGS.”
"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."
"MANEUVERING SPEED 109K (125 MPH) IAS."
"THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON-ICING FLIGHT
EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.”
"DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF
"FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
USED SAFELY IN FLIGHT.
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
AIRPLANE FLIGHT MANUAL."
"DEMONSTRATED CROSSWIND 13K (15 MPH)."
On the instrument panel at the auxiliary tank transfer switches:
FUEL TRANSFER PUMPS
PUSH FOR
PUSH FOR
AUX. QUANT. AUX. QUANT.
LEFT
RIGHT
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pl
cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are
FUEL TRANSFER PUMPS
LEFT RIGHT
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 ai
PAGE 5
SECTION II
LIMITATIONS
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE
IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE
FLIGHT
ICING FLIGHT
WHEN
"DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF
EMERGENCY."
ERO CANNOT BE
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
PUSH FOR
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pla-
cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are
GAL.
the tanks installed in this air-
