MAULE MX-7-180A Technical specifications

Airplane Serial No.__________________
Registration No.____________________
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:
DATE
2099 Georgia Highway 133 South
[phone] •
FAA APPROVED
FOR
MAULE MX-7-180A
Airplane Serial No.__________________
Registration No.____________________
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:
_______________________________________
Manager, Aircraft Certification Office
Federal Aviation Administration
Atlanta, Georgia USA
DATE
:
Performance That Counts!
2099 Georgia Highway 133 South
•Moultrie, GA 31788 •
Fax: [phone] or [phone] •
www.mauleairinc.com
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
_______________________________________
Manager, Aircraft Certification Office
Federal Aviation Administration
www.mauleairinc.com

MAULE AEROSPACE TECHNOLOGY, INC.
REV. TO
PAGES
A 2
5
6
10
19
Deleted Fuel Quantity in Paragraph 1.4
and referred to Fuel Supply Table. Added
Fuel Supply Table. Added to CAUTION
Note under Paragraph 1.2.
Relocated the Flap Control Handle
Placard and the Rear Cabin Cargo
Limitations Placard from page 6.
Deleted Fuel Capacity numbers from Fuel
Transfer P
ump Switch Placard and added
note for Tank Configuration.
Added "Parking Brake...OFF" to 3.2.D
BEFORE TAKEOFF.
Added Unusable Fuel weight for new
Tank Configurations.
B 5, 7, 11 Added 48°
Setting. (
20001C-
20026C, 20028C, 20029C,
20031C-
20035C unless Mod Kit No. 11
c/w.)
C 2. 17,
22, 21
Revised C.G. Range. Delete page 21.
(Page 21 reinstated in new Weight and
Balance Data)
D 3, 5,
11-13,
15-16
Changed primary airspeed units to knots.
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
LOG OF REVISIONS
DESCRIPTION
APPROVAL AND DATE
Deleted Fuel Quantity in Paragraph 1.4
and referred to Fuel Supply Table. Added
Fuel Supply Table. Added to CAUTION
Note under Paragraph 1.2.
Relocated the Flap Control Handle
Placard and the Rear Cabin Cargo
Limitations Placard from page 6.
Deleted Fuel Capacity numbers from Fuel
ump Switch Placard and added
note for Tank Configuration.
Added "Parking Brake...OFF" to 3.2.D
BEFORE TAKEOFF.
Added Unusable Fuel weight for new
Tank Configurations.
______________________________
Manager, Aircraft Certification
Federal Aviation
Atlanta, GA
Date:_____________________________
Setting. (
48°n/a to s/n's
20026C, 20028C, 20029C,
20035C unless Mod Kit No. 11
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Revised C.G. Range. Delete page 21.
(Page 21 reinstated in new Weight and
Balance Data)
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Changed primary airspeed units to knots.
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Page i
APPROVAL AND DATE
______________________________
Manager, Aircraft Certification
Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________

E 2
20
Removed cautionary note when using 5th
seat, (this Model is 4
Revised Rear
and the optional Rear Passenger Seat
location.
F iiii
3
5
6
24
Changed page number from 25 to 24.
Moved Note from Sec. 2.3 to Sec. 2.1
Removed Note from Sec. 2.3
Added JPI EDM
Changed page number from 25 to 24.
Added required note in Airplane
Inspection Period section.
Removed cautionary note when using 5th
seat, (this Model is 4
-place)
Revised Rear
Passenger Seat location
and the optional Rear Passenger Seat
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Changed page number from 25 to 24.
Moved Note from Sec. 2.3 to Sec. 2.1
Removed Note from Sec. 2.3
Added JPI EDM
-900/930.
Changed page number from 25 to 24.
Added required note in Airplane
Inspection Period section.
______________________________
Man
ager, Southeast Flight Test
Section, AIR
-
Atlanta, GA
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
ager, Southeast Flight Test
-
712, FAA
Date:_____________________________

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A Page ii
LOG OF SUPPLEMENTS
SUPP.
NO. NO. OF PAGES
DESCRIPTION
APPROVAL
DATE
- 9 Installation of Aqua 2200 Floats per STC No. SA253CH. 03/25/98
1 6 English to Metric Conversion Charts - required in aircraft when registered in
Canada. 09/03/99
2 Installation of Sensenich 76EM8S8-0-56 Propeller - Maule Drawing 5538B. 02/11/00
3 9 Installation of S-TEC System 30 Two Axis Autopilot Model ST-810-30 (14v) -
Maule Drawing 9197A, Rev. Aor later. (Land) 01/21/00
4 9 Installation of S-TEC System 30 Two Axis Autopilot Model ST-810-30 (14v) -
Maule Drawing 9197A, Rev. Aor later. (Sea) 01/21/00
5 9 Installation of S-TEC System 50 Two Axis Autopilot Model ST-609-50 (28v) -
Maule Drawing 9200A, Rev. Aor later. 02/14/00
6 6 Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) -
Maule Drawing 9196A, Rev. Aor later. (Land) 04/04/00
7 6 Installation of S-TEC System 55 Two Axis Autopilot Model ST-620 (14v) -
Maule Drawing 9196A, Rev. Aor later. (Sea) 04/04/00
8 9 Installation of S-TEC System 20 Single Axis Autopilot Model ST-810-20 (14v) -
Maule Drawing 9197A, Rev. Bor later. (Land) 03/20/00
9 9 Installation of S-TEC System 20 Single Axis Autopilot Model ST-810-20 (14v) -
Maule Drawing 9197A, Rev. Bor later. (Sea) 03/20/00
10 9 Installation of S-TEC System 20 Single Axis Autopilot Model ST-820-20 (28v) -
Maule Drawing 9201A, Rev. Aor later. 03/20/00
11 7 Inst. of S-TEC System 40 Single Axis Autopilot Model ST-418-40 (14v) - Maule
Dwg 9193A, Rev. Cor later. 10/29/01
12 7 Inst. of S-TEC System 40 Single Axis Autopilot Model ST-609-40 (28v) -
Maule
Dwg 9200A, Rev. Bor later. 10/29/01
- 4 Installation of S-TEC System 20 Single Axis Autopilot Model ST-872-20 (28v) -
Maule Drawing 9211A. (Land) 06/25/01
- 5 Installation of S-TEC System 30 Two Axis Autopilot Model ST-872-30 (28v) -
Maule Drawing 9211A. (Land) 06/25/01
- 5 Installation of S-TEC System 20 Single Axis Autopilot Model ST-872-20 (28v) -
Maule Drawing 9211A. (Sea) 06/25/01
- 5 Installation of S-TEC System 30 Two Axis Autopilot Model ST-872-30 (28v) -
Maule Drawing 9211A. (Sea) 06/25/01
- 8 Installation of S-TEC System 50 Two Axis Autopilot Model ST-418-50 (14v) -
Maule Drawing 9193A, Rev. Dor later. (Land) 12/05/01
- 5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST-873-20 (14/28v) -
Maule Drawing 9212A. (Land) 10/15/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST-873-30 (14/28v) -
Maule
Drawing 9212A. (Land) 10/15/01
- 5 Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A. 08/15/02
- 8 Inst. of GARMIN GNC-420
(GPS/COMM) System - Maule Drawing 7251A. 06/30/03
- 9 Inst. of GARMIN GNS-530
(GPS/NAV/COMM) System - Maule Drawing 7253A. 06/30/03
- 4 Inst. of GARMIN GTX-330 Mode S Transponder Traffic Information System
(TIS) - Maule Drawing 7255A. 06/30/03
- 3 Operation of aircraft when Micro AeroDynamics Vortex Generator System is
installed in accordance with Maule Drawing 9177A. 12/16/05

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A Page iii
TABLE OF CONTENTS
ITEM
COVER PAGE
LOG OF REVISIONS……………………………….…………………….. i
LOG OF SUPPLEMENTS………………………….…………………..… ii
TABLE OF CONTENTS…………………………….…………………..... iii & iiii
SECTION I GENERAL
Plan View……………………………………………..……………..
1
1.1
Maximum Weight……………………………..…………….
2
1.2 Center of Gravity Limits………………………..…………. 2
1.3
Maneuvers………………………………………..…………
2
1.4 Fuel
Capacity……………………………………..………...
2
SECTION II LIMITATIONS
2.1 Airspeed Limits……………………………..………………
3
2.2 Power Plant Limits…………………………..…………….. 4
2.3 Flight Load Factors…………………………..……………. 5
2.4 Placards………………………………………..…………… 5
SECTION III NORMAL PROCEDURES
3.1 Preflight Inspection…………………………..…………….
7
3.2 Operating Check Lists………………………..…………… 8
3.3
Normal Flight Operations……………………..…………...
12
3.4 Door-Off Operation……………………………..…………. 13
3.5 Noise Level………………………………………..……….. 13
3.6 Anti-Collision Light………………………………..……….. 13
SECTION IV EMERGENCY PROCEDURES
4.1 Emergency Basic Rules……………………………….….
14
4.2 Engine Emergency Shut Down……………………….…. 14
4.3 Engine Fire During Starting…………………………….... 14
4.4 Engine Fire After Starting…………………………….…... 14
4.5 Emergency Exit on the Ground………………………….. 14
4.6 Takeoff Abort………………………………………………. 14
4.7 Engine Failure After T.O. or Forced Landing….……….. 15
4.8 Partial Power Failure During Flight of After T.0..………. 15
4.9 Complete Power Failure During Flight………….………. 15
4.10 Engine Airstart……………………………………..………. 15
4.11 Electrical Fire……………………………………….……… 15
4.12 Engine Fire During Flight………………………….……… 16
4.13 Smoke and Fume Elimination…………………….……… 16
4.14 Structural Damage………………………………….…….. 16
4.15 Recovery From Inadvertent Spins………………….…… 16
4.16 Alternator Failure…………………………………….……. 16

TABLE OF CONTENTS
SECTION V
WEIGHT AND BALANCE AND EQUIPMENT LIST
5.1
Weight and Balance Data…………………………….…..
Required Equipment List ………Provided for each Airplane
SECTION VI
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
6.1
Introduction…………………………………………………
6.2
Airplane Inspection Period…………………………….….
6.3
Preventive Maintenance that may be Accomplished
a Certified Pilot…………………………………………..…
6.4
Alterations or Repairs to Airplane………………………..
SECTION VII
MANUFACTURER'S DATA
Optional Equipment List………..Provided for each Airplane
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
WEIGHT AND BALANCE AND EQUIPMENT LIST
Weight and Balance Data…………………………….…..
Required Equipment List ………Provided for each Airplane
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
Introduction…………………………………………………
Airplane Inspection Period…………………………….….
Preventive Maintenance that may be Accomplished
by
a Certified Pilot…………………………………………..…
Alterations or Repairs to Airplane………………………..
MANUFACTURER'S DATA
Optional Equipment List………..Provided for each Airplane
Page iiii
MAULE AEROSPACE TECHNOLOGY, INC.
WEIGHT AND BALANCE AND EQUIPMENT LIST
Weight and Balance Data…………………………….…..
17
Required Equipment List ………Provided for each Airplane
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
Introduction…………………………………………………
24
Airplane Inspection Period…………………………….….
24
by
a Certified Pilot…………………………………………..…
24
Alterations or Repairs to Airplane………………………..
24
Optional Equipment List………..Provided for each Airplane

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
SECTION I
GENERAL
Page 1

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION I
GENERAL:
NORMAL CATEGORY OPERATION
1.1 MAXIMUM WEIGHT:
2400 Pounds
1.2
CENTER OF GRAVITY LIMITS:
Straight line variation between points given
Datum: Wing Leading Edge
NOTE:
It is the responsibility of the pilot to assure that the airplane is property loaded. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
graphs.
////////////////////////
////CAUTION////
////////////////////////
CHECK WEIGHT AND BALANCE CAREFULLY WHEN CARGO OR
BAGGAGE IS CARRIED IN THE REAR CABIN AREA. ALSO, FLIGHT
PLANNING SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT
WITH FUEL BURN.
1.3 MANEUVERS:
Only Normal Category Maneuvers including Stalls, Lazy Ei
and steep turns involving bank angles
this airplane.
////////////////////////
////CAUTION////
////////////////////////
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
1.4 FUEL CAPACITY:
Usable Fuel and Unusable Fuel: See Table Below
Fuel Capacity -
See Instrument Panel Placard for Auxiliary T
Tank
Configuration
Tank
Location
A
Main
Aux.
B
Main
Aux.
C
Main
Aux.
D
Main
Aux.
////////////////////////
////CAUTION////
////////////////////////
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 6/3/93
Rev. A dated: 10/28/94
Rev. C dated: 5/28/99
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
NORMAL CATEGORY OPERATION
2400 Pounds
CENTER OF GRAVITY LIMITS:
+15.9 to +20.5 @ 2400 lbs.
+12.4 to +20.5 @ 1740 lbs. or less
Straight line variation between points given
Datum: Wing Leading Edge
It is the responsibility of the pilot to assure that the airplane is property loaded. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
CHECK WEIGHT AND BALANCE CAREFULLY WHEN CARGO OR
BAGGAGE IS CARRIED IN THE REAR CABIN AREA. ALSO, FLIGHT
PLANNING SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT
WITH FUEL BURN.
Only Normal Category Maneuvers including Stalls, Lazy Ei
and steep turns involving bank angles
not
greater than 60
this airplane.
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
Usable Fuel and Unusable Fuel: See Table Below
See Instrument Panel Placard for Auxiliary T
ank configuration installed in
Tank
Location
Usable Fuel (Gal) Unusable Fuel (Gal)
Main
Aux.
20.0 15.0 1.5 0.0
Main
Aux.
20.0 21.0 1.5 0.0
Main
Aux.
21.5 15.0 2.3 0.0
Main
Aux.
21.5 21.0 2.3 0.0
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
PAGE 2
SECTION I
GENERAL
+12.4 to +20.5 @ 1740 lbs. or less
It is the responsibility of the pilot to assure that the airplane is property loaded. Refer to
the Weight and Balance Data for baggage/cargo loading recommendations and loading
CHECK WEIGHT AND BALANCE CAREFULLY WHEN CARGO OR
BAGGAGE IS CARRIED IN THE REAR CABIN AREA. ALSO, FLIGHT
PLANNING SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT
Only Normal Category Maneuvers including Stalls, Lazy Ei
ghts, Chandelles
greater than 60
°are approved in
AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
ank configuration installed in
this aircraft.
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II
LIMITATIONS
2.1 AIRSPEED LIMITS:
All airspeeds are Indicated Airspeeds (IAS).
A.
AIRSPEED INDICATOR MARKINGS:
Red Radial, (V
NE
) -
161K (185 mph)
Yellow Arc, Caution Range
Green Arc, Normal Operating Range
White Arc,
Flap Operating Range
B.
EXPLANATION OF AIRSPEED INDICATOR MARKINGS:
Red Radial Line -
Never Exceed Speed (V
airspeed in smooth air.
Yellow Arc -
Caution Range, 129
speed range should be conducted only in smooth air and
control movements should not be large or abrupt.
Green Arc -
Normal Operating Range, 53
from flaps up, power off stall speed at 2400 lbs. (V
cruise speed (V
White Arc -
Flap Operating Range, 41
full flap, power off minimum stall speed at 2400 lbs. (V
the Maximum flaps extended speed (V
NOTE:
DESIGN MANEUVERING SPEED: The maximum safe
aerodynamic controls can be applied (V
marked on the airspeed indicator.
FAA APPROVED: 6/3/93
Rev. D dated:
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II
AIRPLANE FLIGHT MANUAL
LIMITATIONS
MAULE MX-7-180A
All airspeeds are Indicated Airspeeds (IAS).
AIRSPEED INDICATOR MARKINGS:
161K (185 mph)
Yellow Arc, Caution Range
- 129 - 161K (149 - 185 mph)
Green Arc, Normal Operating Range
- 53 - 129K (61 - 149 mph)
Flap Operating Range
- 41 - 85K (47 - 98 mph)
EXPLANATION OF AIRSPEED INDICATOR MARKINGS:
Never Exceed Speed (V
NE
) 161K (185 mph): Maximum safe
airspeed in smooth air.
Caution Range, 129
- 161K (149 - 185 mph):
Operation in this
speed range should be conducted only in smooth air and
control movements should not be large or abrupt.
Normal Operating Range, 53
- 129K (61 -
149 mph): Extends
from flaps up, power off stall speed at 2400 lbs. (V
cruise speed (V
C
).
Flap Operating Range, 41
- 85K (47 -
98 mph): Extends from
full flap, power off minimum stall speed at 2400 lbs. (V
the Maximum flaps extended speed (V
FE
).
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.
PAGE 3
SECTION II
LIMITATIONS
) 161K (185 mph): Maximum safe
Operation in this
speed range should be conducted only in smooth air and
control movements should not be large or abrupt.
149 mph): Extends
from flaps up, power off stall speed at 2400 lbs. (V
S1
) to design
98 mph): Extends from
full flap, power off minimum stall speed at 2400 lbs. (V
SO
) to
airspeed at which full
) is 109K (125 mph). This airspeed is not

MAULE AEROSPACE TECHNOLOGY, INC.
2.2 POWER PLANT LIMITS:
Engine:
Engine Limits:
Propeller:
Fuel:
Engine Instrument Markings:
Cylinder Head Temperature:
Oil Temperature:
Oil Pressure:
Manifold Pressure
Fuel Pressure
Tachometer:
FAA APPROVED
DATE:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
Lycoming O-360-C1F or 0-360-C4F
180 hp @ 2700 rpm, Full Throttle Continuous
Sensenich Fixed Pitch 76EM8S5-0-
56 (76" Dia.)
100/100LL Minimum Grade Aviation Gasoline
Engine Instrument Markings:
Cylinder Head Temperature:
Green Arc -
Normal Operating Range,
200°F - 435
°
Red Radial -
Operating Limit, 500
Oil Temperature:
Green Arc -
Normal Operating Range,
140°F - 245
°
Red Radial -
Operating Limit, 245
Oil Pressure:
Green Arc -
Normal Operating Range,
55 to 95 PSI
Yellow Arc -
Caution Range, 25 to 55 PSI
and 95 to 115
Red Radial -
Minimum Operating Pressure,
25 PSI
Red Radial -
Maximum Operating Pressure,
115 PSI
Manifold Pressure
Green Arc -
Normal Operating Range,
14.5 to 29 ins. of Mercury
Fuel Pressure
Green Arc -
Normal Operating Range,
0.5 to 8 PSI
Red Radial -
Minimum Pressure, 0.5
Red Radial -
Maximum Pressure, 8.0
Green Arc -
Normal Operating Range,
(0-360-
C1F) 2350
Green Arc -
Normal Operating Range,
(0-360-
C4F) 2000
Red Radial -
Maximum RPM, 2700 RPM
Red Arc -
Avoid Continuous Operation,
(0-360-
C1F) 2150
PAGE 4
SECTION II
LIMITATIONS
180 hp @ 2700 rpm, Full Throttle Continuous
56 (76" Dia.)
100/100LL Minimum Grade Aviation Gasoline
Normal Operating Range,
°
F
Operating Limit, 500
°F
Normal Operating Range,
°
F
Operating Limit, 245
°F
Normal Operating Range,
Caution Range, 25 to 55 PSI
and 95 to 115
PSI
Minimum Operating Pressure,
Maximum Operating Pressure,
Normal Operating Range,
14.5 to 29 ins. of Mercury
Normal Operating Range,
Minimum Pressure, 0.5
PSI,
Maximum Pressure, 8.0
PSI
Normal Operating Range,
C1F) 2350
- 2700 RPM
Normal Operating Range,
C4F) 2000
- 2700 RPM
Maximum RPM, 2700 RPM
Avoid Continuous Operation,
C1F) 2150
- 2350 RPM

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 FLIGHT
M
ANUAL 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
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:
"FLAPS / PULL ON / 2
In rear cabin area:
"CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A" 1
MAX. LOAD AREA "B" 175
MAX. LOAD AREA
"C" 125
* 3
RD
NOTCH/LANDING for s/n 20001C
Mod Kit No. 11 is complied with.
FAA APPROVED: 6/3/93
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-7-180A
FLIGHT LOAD FACTORS:
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 FLIGHT
ANUAL 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 FLIGHT MANUAL."
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
"FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE
USED SAFELY IN FLIGHT.
Located on flap control handle:
"FLAPS / PULL ON / 2
ND
NOTCH / TAKEOFF / 4
TH
NOTCH / LANDING." *
"CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A" 1
00 LBS.
MAX. LOAD AREA "B" 175
LBS.
"C" 125
LBS.
NOTCH/LANDING for s/n 20001C
-20026C, 200028C, 20029C, 20031C-
20035C unless Maule
Mod Kit No. 11 is complied with.
PAGE 5
SECTION II
LIMITATIONS
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
Extended: 1.9g Positive to 0g Negative
"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE
IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FLIGHT
"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."
"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
ICING FLIGHT
WHEN 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
NOTCH / LANDING." *
20035C unless Maule

MAULE AEROSPACE TECHNOLOGY, INC.
2.4 PLACARDS: (Cont’d)
At the main fuel tank selector valve on the left kick panel:
OFF
The following placard is located on the instrument panel at the optional auxiliary tank transfer
switches, when installed:
PUSH FOR
AUX. QUANT.
NOTE: If JPI EDM-
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and placards
are not installed. However, FUEL TRANSFER PUMPS
below:
FUEL CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
USABLE EACH. (TANK CONFIGURATION ____)
*Instrument panel placard will show capacity of the tanks installed in this aircraft. See Table on Page
2 for capacity of available tank configurations. Auxiliary tank placards will be deleted when auxiliar
tanks not installed.
FAA APPROVED
DATE: 6/3/9 PAGE 6
Rev. A dated:
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
At the main fuel tank selector valve on the left kick panel:
FUEL SELECTOR VALVE
LEFT: * GAL.
OFF
BOTH
RIGHT: * GAL.
The following placard is located on the instrument panel at the optional auxiliary tank transfer
FUEL TRANSFER PUMPS
PUSH FOR
AUX. QUANT.
PUSH FOR
AUX. QUANT.
LEFT RIGHT
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
FUEL TRANSFER PUMPS
LEFT RIGHT
FUEL CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
USABLE EACH. (TANK CONFIGURATION ____)
*Instrument panel placard will show capacity of the tanks installed in this aircraft. See Table on Page
2 for capacity of available tank configurations. Auxiliary tank placards will be deleted when auxiliar
DATE: 6/3/9 PAGE 6
SECTION II
LIMITATIONS
The following placard is located on the instrument panel at the optional auxiliary tank transfer
PUSH FOR
AUX. QUANT.
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and placards
and LEFT and RIGHT placards are used as
FUEL CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
*GAL.
*Instrument panel placard will show capacity of the tanks installed in this aircraft. See Table on Page
2 for capacity of available tank configurations. Auxiliary tank placards will be deleted when auxiliar
y

SECTION III
NORMAL PROCEDURES:
3.1
PREFLIGHT INSPECTION:
A. INTERIOR:
1.
BAT Switch…………………………………....
2.
Fuel Gauges……………………………….….
3.
Auxiliary Fuel Pumps………………………...
4. All
Electrical Switches…………………….….
5.
BAT Switch………………………………….…
6.
Flaps……………………………………….…..
EXTERIOR:
Begin at the left front door, proceed around the left wing to the nose area, then
around the right wing and back to
1.
Fuel drains behind step……………………....
2.
Left Flap………………………………………..
3.
Aileron………………………………………….
4. Left Wing
Top………………………………….
5.
Left Wing Main Fuel Tank Drain….…
Left Wing Aux Fuel Tank Drain (if installed).
6.
Left Wing Tip & Nav Light…………………....
7. Auxiliary Fuel
Tank (if installed)....................
8.
Landing Light…………………………………..
9.
Left Wing Tiedown…………………………….
10.
Pitot Tube………………………………..…….
11.
Stall Warning Switch…………………..……..
12.
Main Fuel Tank………………………….….…
13.
Left Landing Gear………………………….…
14.
Bottom left side of Cowl…………………..….
15. Top Cowl,
Oil Access Door……………….…
16.
Propeller………………………………………..
17.
Air Inlets…………………………………….….
*(3rd NOTCH) for s/n's 20001C-
20026C,
FAA APPROVED: 6/3/93
Rev. B dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES:
PREFLIGHT INSPECTION:
BAT Switch…………………………………....
ON
Fuel Gauges……………………………….….
CHECK INDICATIONS
Auxiliary Fuel Pumps………………………...
ON, THEN OFF (LISTEN TO VERIFY
OPERATION)
Electrical Switches…………………….….
OFF
BAT Switch………………………………….…
OFF
Flaps……………………………………….…..
FULL DOWN (4TH NOTCH)*
Begin at the left front door, proceed around the left wing to the nose area, then
around the right wing and back to
the fuselage, then around the tail section.
Fuel drains behind step……………………....
DRAIN (2)
Left Flap………………………………………..
CHECK HINGES & CONTROL
ATTACHMENTS
Aileron………………………………………….
CHECK HINGES & CONTROL
ATTACHMENTS
Top………………………………….
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
Left Wing Main Fuel Tank Drain….…
Left Wing Aux Fuel Tank Drain (if installed).
DRAIN (1)
DRAIN (1)
Left Wing Tip & Nav Light…………………....
CHECK FOR DAMAGE
Tank (if installed)....................
VISUALLY CHECK QUANTITY
Landing Light…………………………………..
CHECK FOR DAMAGE
Left Wing Tiedown…………………………….
REMOVE
Pitot Tube………………………………..…….
REMOVE COVER
Stall Warning Switch…………………..……..
CHECK FOR
FREEDOM OF
MOVEMENT
Main Fuel Tank………………………….….…
VISUALLY CHECK QUANTITY
Left Landing Gear………………………….…
CHECK TIRE INFLATION AND
BRAKE LINE SECURITY
Bottom left side of Cowl…………………..….
DRAIN GASCOLATOR (1)
Oil Access Door……………….…
CHECK OIL QUANTITY
Propeller………………………………………..
CHECK LEADING EDGE FOR
DAMAGE.
Air Inlets…………………………………….….
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
20026C,
20028C, 20029C, 20031C-
20035C unless Mod Kit No. 11 c/w
PAGE 7
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
SECTION III
NORMAL
CHECK INDICATIONS
ON, THEN OFF (LISTEN TO VERIFY
FULL DOWN (4TH NOTCH)*
Begin at the left front door, proceed around the left wing to the nose area, then
the fuselage, then around the tail section.
CHECK HINGES & CONTROL
CHECK HINGES & CONTROL
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
CHECK FOR DAMAGE
VISUALLY CHECK QUANTITY
CHECK FOR DAMAGE
REMOVE COVER
FREEDOM OF
VISUALLY CHECK QUANTITY
CHECK TIRE INFLATION AND
BRAKE LINE SECURITY
DRAIN GASCOLATOR (1)
CHECK OIL QUANTITY
CHECK LEADING EDGE FOR
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
20035C unless Mod Kit No. 11 c/w
.
SECTION III
NORMAL
PROCEDURES

MAULE AEROSPACE TECHNOLOGY, INC.
3.1
PREFLIGHT INSPECTION:
18.
Right Landing Gear……………………….….
19.
Right Wing & Controls…………………….….
20.
Wing Main Fuel Tank Drain……….…
Wing Aux Fuel Tank Drain (if installed).........
21.
Right Fuselage, Side, Top & Bottom……….
22.
Right Side Static Port………………………...
23.
Right Stabilizer…………………………….….
24.
Right Elevator………………………………....
25.
Rudder………………………………………....
26.
Tailwheel……………………………………....
27.
Left Elevator…………………………………...
28.
Left Stabilizer……………………………….…
29.
Left Fuselage, Side, Top & Bottom………...
30.
Left Side Static Port……………………….….
3.2
OPERATING CHECK LISTS:
A.
BEFORE STARTING:
1.
Seat Belts & Shoulder Harnesses…………..
2.
Flaps……………………………………………
3.
Circuit Breakers………………………………..
B. STARTING:
1.
Parking or Toe Brakes……………………..…
2.
Fuel Selector Valve…………………………...
3.
Throttle………………………………………….
4.
Mixture Control...............................................
5. Anti-
Collision Light………………………….....
6. BAT and ALT
Switch......................................
7.
Primer.............................................................
FAA APPROVED
DATE:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
PREFLIGHT INSPECTION:
(Cont'd)
Right Landing Gear……………………….….
CHECK TIRE INFLATION & BRAKE
LINE SECURITY
Right Wing & Controls…………………….….
INSPECT SAME AS LEFT WING
Wing Main Fuel Tank Drain……….…
...........
Wing Aux Fuel Tank Drain (if installed).........
DRAIN (1)
DRAIN (1)
Right Fuselage, Side, Top & Bottom……….
INSPECT FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
Right Side Static Port………………………...
CLEAR
Right Stabilizer…………………………….….
CHECK ATTACHMENT POINTS &
STRUT
Right Elevator………………………………....
CHECK
HINGE POINTS
Rudder………………………………………....
CHECK HINGE POINTS, CONTROL
ATTACHMENT & NAV LIGHT
Tailwheel……………………………………....
CHECK FOR INFLATION,
ATTACHMENTS, REMOVE TIEDOWN
Left Elevator…………………………………...
CHECK TAB CONTROLS & ALL
HINGE POINTS
Left Stabilizer……………………………….…
CHECK ATTACHMENT POINTS &
STRUT
Left Fuselage, Side, Top & Bottom………...
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
Left Side Static Port……………………….….
CLEAR
OPERATING CHECK LISTS:
BEFORE STARTING:
Seat Belts & Shoulder Harnesses…………..
FASTENED
Flaps……………………………………………
RETRACTED
Circuit Breakers………………………………..
CHECK
Parking or Toe Brakes……………………..…
ON
Fuel Selector Valve…………………………...
ON FULLEST TANK, OR
SAME QUANTITY
Throttle………………………………………….
OPEN 1/4 INCH
Mixture Control...............................................
RICH (SEE NOTE NEXT PAGE FOR
HOT START)
Collision Light………………………….....
ON
Switch......................................
ON
Primer.............................................................
AS REQUIRED
PAGE 8
SECTION III
NORMAL
PROCEDURES
CHECK TIRE INFLATION & BRAKE
INSPECT SAME AS LEFT WING
INSPECT FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
CHECK ATTACHMENT POINTS &
HINGE POINTS
CHECK HINGE POINTS, CONTROL
ATTACHMENT & NAV LIGHT
CHECK FOR INFLATION,
ATTACHMENTS, REMOVE TIEDOWN
CHECK TAB CONTROLS & ALL
CHECK ATTACHMENT POINTS &
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
ON FULLEST TANK, OR
BOTH IF
SAME QUANTITY
RICH (SEE NOTE NEXT PAGE FOR

MAULE AEROSPACE TECHNOLOGY, INC.
3.2
OPERATING CHECK LISTS:
NOTE:
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A
START ATTEMPT. TO CLEAR A FLOODED ENGINE, PULL MIXTURE FULL
LEAN AND OPEN THROTTLE, CRANK WITH STARTER. WHEN ENGINE
STARTS,
PULL THROTTLE TO IDLE AND EASE MIXTURE TO FULL RICH.
8.
Starter Switch............................................ TWIST FULL RIGHT TO ENGINE
////////////////////////
////CAUTION////
////////////////////////
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO
FULL LEAN. IF ENGINE FAILS TO START AFTER SEVERAL
REVOLUTIONS, AND FIRE CONTINUES, SECURE IGNITION, BAT. AND
ALT. SWITCHES, TURN FUEL VALVE OFF AND EXIT AIRCRAFT.
9. After
Starting……………………………….….
////////////////////////
////CAUTION////
////////////////////////
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS,
SHUT DOWN ENGINE.
10.
Alternator………………………………….…...
11. Radios &
other electrical switches……..……
12.
Parking Brake………………………………
C. ENGINE CHECK:
1.
Parking Brake………………………………….
2.
Engine Instruments………………………..….
3.
Throttle………………………………………....
4.
Magnetos…………………………………..…..
////////////////////////
////CAUTION////
////////////////////////
A RPM DROP OF MORE THAN 175 RPM OR A DIFFERENCE BETWEEN
LEFT AND RIGHT OF MORE THAN 50 RPM
5.
Carburetor Air Control
6.
Carburetor Air Control……………………....
7.
Vacuum Gauge………………………….…….
8.
Alternator……………………………………….
9.
Throttle………………………………………….
FAA APPROVED
DATE: PAGE 9
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
OPERATING CHECK LISTS:
(Cont'd)
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A
START ATTEMPT. TO CLEAR A FLOODED ENGINE, PULL MIXTURE FULL
LEAN AND OPEN THROTTLE, CRANK WITH STARTER. WHEN ENGINE
PULL THROTTLE TO IDLE AND EASE MIXTURE TO FULL RICH.
Starter Switch............................................ TWIST FULL RIGHT TO ENGINE
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO
FULL LEAN. IF ENGINE FAILS TO START AFTER SEVERAL
REVOLUTIONS, AND FIRE CONTINUES, SECURE IGNITION, BAT. AND
ALT. SWITCHES, TURN FUEL VALVE OFF AND EXIT AIRCRAFT.
Starting……………………………….….
CHECK OIL PRESSURE
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS,
SHUT DOWN ENGINE.
Alternator………………………………….…...
CHECK CHARGING
other electrical switches……..……
AS REQUIRED
Parking Brake………………………………
.... OFF
Parking Brake………………………………….
ON, IF DESIRED
Engine Instruments………………………..….
CHECK, IN GREEN ARCS
Throttle………………………………………....
INCREASE
TO 2000 RPM
Magnetos…………………………………..…..
SWITCH TO RIGHT, LEFT, BOTH,
CHECKING RPM DROPS
A RPM DROP OF MORE THAN 175 RPM OR A DIFFERENCE BETWEEN
LEFT AND RIGHT OF MORE THAN 50 RPM
IS UNACCEPTABLE.
Carburetor Air Control
……………………....
PULL HOT, NORMAL DROP WITH
CARBURETOR AIR HOT IS 150
RPM
Carburetor Air Control……………………....
PUSH COLD
Vacuum Gauge………………………….…….
CHECK IN GREEN
Alternator……………………………………….
CHARGING: LIGHT OUT ABOVE 900
RPM
Throttle………………………………………….
RETARD TO IDLE
DATE: PAGE 9
SECTION III
NORMAL
PROCEDURES
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A
START ATTEMPT. TO CLEAR A FLOODED ENGINE, PULL MIXTURE FULL
LEAN AND OPEN THROTTLE, CRANK WITH STARTER. WHEN ENGINE
PULL THROTTLE TO IDLE AND EASE MIXTURE TO FULL RICH.
Starter Switch............................................ TWIST FULL RIGHT TO ENGINE
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO
FULL LEAN. IF ENGINE FAILS TO START AFTER SEVERAL
REVOLUTIONS, AND FIRE CONTINUES, SECURE IGNITION, BAT. AND
ALT. SWITCHES, TURN FUEL VALVE OFF AND EXIT AIRCRAFT.
CHECK OIL PRESSURE
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS,
CHECK CHARGING
CHECK, IN GREEN ARCS
TO 2000 RPM
SWITCH TO RIGHT, LEFT, BOTH,
CHECKING RPM DROPS
A RPM DROP OF MORE THAN 175 RPM OR A DIFFERENCE BETWEEN
IS UNACCEPTABLE.
PULL HOT, NORMAL DROP WITH
CARBURETOR AIR HOT IS 150
±50
CHECK IN GREEN
CHARGING: LIGHT OUT ABOVE 900
RETARD TO IDLE

MAULE AEROSPACE TECHNOLOGY, INC.
3.2
OPERATING CHECK LISTS:
D. BEFORE TAKEOFF:
1.
Fuel Selector………………………………..…
2.
Flaps…………………….……………………..
3.
Trim Controls…………….…………………....
4.
Flight Controls…………….…………………..
5.
Mixture Control…………….……………….…
6.
Carburetor Air Control
7.
Engine Instruments……………..…………….
8.
Radios…………………………….……………
9.
Altimeter………………………….……………
10.
Attitude Indicator………………….…………..
11. Directional
Indicator……………….………….
12.
Seat Belts & Shoulder Harnesses.………….
13.
Doors.............................................................
14.
Passengers....................................................
15.
Parking Brake................................................
E.
BEFORE LANDING:
1.
Seat Belts & Shoulder Harnesses……….….
2.
Fuel Selector Valve……………………….…..
3.
Mixture Control…………………………….….
4.
Flaps……………………………….…………....
5.
Carburetor Air Control (
F.
ENGINE SHUT DOWN:
1.
Parking Brakes………………………..…..…..
2.
Radios………………………………….…..….
3.
All other electrical switches…………..……...
4.
Flaps……………………………………..……..
5.
Magneto Grounding Check……………..……
6.
Mixture Control…………………………………
7.
Magneto Switch…………………………….…
8. Anti-
Collision Light………………..…………..
9.
BAT & ALT Switch…………………..………..
10.
Parking Brake………………………
FAA APPROVED
DATE: 6/3/93
Rev. A dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180A
OPERATING CHECK LISTS:
(Cont'd)
Fuel Selector………………………………..…
ON FULLEST TANK OR BOTH
Flaps…………………….……………………..
AS DESIRED FOR T.O. (MAX. 24
Trim Controls…………….…………………....
SET FOR TAKEOFF
Flight Controls…………….…………………..
CHECK FOR FREEDOM AND
PROPER TRAVEL
Mixture Control…………….……………….…
FULL RICH
Carburetor Air Control
.............
....…….……..
PUSH COLD
Engine Instruments……………..…………….
RECHECK IN NORMAL RANGE
Radios…………………………….……………
AS DESIRED
Altimeter………………………….……………
SET
Attitude Indicator………………….…………..
CHECK ERECT
Indicator……………….………….
SET
Seat Belts & Shoulder Harnesses.………….
RECHECK FASTENED
Doors.............................................................
CLOSED & LATCHED
Passengers....................................................
BELTS &
HARNESSES SECURED.
BRIEFED ON OPENING DOORS.
Parking Brake................................................
OFF
BEFORE LANDING:
Seat Belts & Shoulder Harnesses……….….
FASTENED
Fuel Selector Valve……………………….…..
ON FULLEST TANK OR BOTH
Mixture Control…………………………….….
FULL RICH
Flaps……………………………….…………....
AS REQUIRED
Carburetor Air Control (
O-540)….………….. PULL HOT
ENGINE SHUT DOWN:
Parking Brakes………………………..…..…..
ON, IF DESIRED
Radios………………………………….…..….
OFF
All other electrical switches…………..……...
AS DESIRED
Flaps……………………………………..……..
AS DESIRED
Magneto Grounding Check……………..……
PERFORM BELOW 1000 RPM
Mixture Control…………………………………
FULL LEAN
Magneto Switch…………………………….…
OFF
Collision Light………………..…………..
OFF
BAT & ALT Switch…………………..………..
OFF
Parking Brake………………………
..………..
OFF (AS DESIRED)
PAGE 10
ON FULLEST TANK OR BOTH
AS DESIRED FOR T.O. (MAX. 24
°)
SET FOR TAKEOFF
CHECK FOR FREEDOM AND
PROPER TRAVEL
RECHECK IN NORMAL RANGE
RECHECK FASTENED
CLOSED & LATCHED
HARNESSES SECURED.
BRIEFED ON OPENING DOORS.
ON FULLEST TANK OR BOTH
PERFORM BELOW 1000 RPM
OFF (AS DESIRED)

MAULE AEROSPACE TECHNOLOGY, INC.
3.3
NORMAL FLIGHT OPERATIONS:
A.
NOTE: FLAP SETTINGS:
The following Flap Settings are available:
Flap Configuration
Cruise
Flaps Up
Takeoff
Landing
Landing
B.
RECOMMENDED FLAP SETTINGS:
Flap settings are given in number of notches above the fully retracted position, which
is handle full down (Normal
Normal Takeoff -
Second Notch (24
Normal Climb -
First Notch (0
Best Angle of Climb
-
Cruise -
Fully retracted (
Landing -
Normally Fourth Notch (48
C. CLIMBING:
Best Rate of Climb -
Best Angle of Climb
–
////////////////////////
////CAUTION////
////////////////////////
FOR TAKEOFF OR
CONDITIONS FLAP SETTING OF 0
-7°
OPTIONAL.
////////////////////////
////CAUTION////
////////////////////////
USE CLIMB AIRSPEED BELOW 78K (90 MPH) ONLY AS NECESSARY
AND CHECK CYLINDER HEAD TEMPERATURE FREQUENTLY WHEN
DOING
SO.
* 40°
flap position limit for s/n 20001C
Mod Kit No. 11 is complied with.
FAA APPROVED: 6/3/93
Rev. B dated: 5/11/95
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180A
NORMAL FLIGHT OPERATIONS:
NOTE: FLAP SETTINGS:
The following Flap Settings are available:
Flap Handle Position Flap Position
Handle Full Down -7°
First Notch 0°
Second Notch 24°
Third Notch 40°
Fourth Notch 48°*
RECOMMENDED FLAP SETTINGS:
Flap settings are given in number of notches above the fully retracted position, which
is handle full down (Normal
-7°).
Second Notch (24
°)
First Notch (0
°)
-
Second Notch (24°)
Fully retracted (
-7°/no notches or 0°/first notch)
Normally Fourth Notch (48
°/full flaps) * - other positions o
ptional
78K (90 mph) IAS, flaps @ First Notch (0°)
–
65K (75 mph) IAS with flaps set @ Second Notch (24
FOR TAKEOFF OR
LANDING UNDER GUSTY CROSSWIND
CONDITIONS FLAP SETTING OF 0
°
(one notch) IS RECOMMENDED.
OPTIONAL.
USE CLIMB AIRSPEED BELOW 78K (90 MPH) ONLY AS NECESSARY
AND CHECK CYLINDER HEAD TEMPERATURE FREQUENTLY WHEN
SO.
flap position limit for s/n 20001C
- 20026C, 200028C, 20029C, 20031C -
20035C unless Maule
Mod Kit No. 11 is complied with.
PAGE 11
SECTION
III
NORMAL PROCEDURES
Flap settings are given in number of notches above the fully retracted position, which
ptional
65K (75 mph) IAS with flaps set @ Second Notch (24
°)
LANDING UNDER GUSTY CROSSWIND
(one notch) IS RECOMMENDED.
USE CLIMB AIRSPEED BELOW 78K (90 MPH) ONLY AS NECESSARY
AND CHECK CYLINDER HEAD TEMPERATURE FREQUENTLY WHEN
20035C unless Maule

MAULE AEROSPACE TECHNOLOGY, INC.
3.3
NORMAL FLIGHT OPERATIONS:
D. RUDDER TRIM:
NOTE: To assure
full effectiveness of the Right Rudder Trim:
Unlock "T" handle (
½
Lock "T" handle ½ turn right before releasing right rudder pressure. If too much trim,
move handle in until trim is
E. STALLS:
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above
the stall speed. Loss of altitude prio
feet.
////////////////////////
////CAUTION////
////////////////////////
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
F.
CROSSWIND LANDINGS & TAKEOFFS:
Maximum demonstrated
should be limited to 0
the maximum demonstrated for certification of the airplane and is not considered
limiting with flaps at 0
G.
FUEL SYSTEM MANAGEMENT:
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector
valve on the left kick panel. Auxiliary (outboard) tanks feed their respective main tanks
via transfer pumps that are controlled by switche
transfer pumps transfer fuel at a rate of 0.4 gallons per minute or approximately 45
minutes for a full auxiliary tank. Since overfilling a main tank from an auxiliary tank will
force excess fuel overboard, it is recommen
until their respective main tanks are slightly more than one quarter full. If the tank being
transferred to is feeding the engine, however, transfer can be initiated when the main
tank is down to approximately
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
decrease on the respective auxiliary tank indicator.
FAA APPROVED: 6/3/93
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180A
NORMAL FLIGHT OPERATIONS:
(Cont'd)
full effectiveness of the Right Rudder Trim:
½
turn left), depress right rudder as you pull "T" handle full out.
Lock "T" handle ½ turn right before releasing right rudder pressure. If too much trim,
move handle in until trim is
correct and then lock.
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above
the stall speed. Loss of altitude prio
r to recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
CROSSWIND LANDINGS & TAKEOFFS:
Maximum demonstrated
crosswind component is 13K (15 mph) and flap extension
should be limited to 0
°
(fully retracted) with such crosswind or higher. 13K (15 mph) is
the maximum demonstrated for certification of the airplane and is not considered
limiting with flaps at 0
°.
FUEL SYSTEM MANAGEMENT:
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector
valve on the left kick panel. Auxiliary (outboard) tanks feed their respective main tanks
via transfer pumps that are controlled by switche
s on the instrument panel. These
transfer pumps transfer fuel at a rate of 0.4 gallons per minute or approximately 45
minutes for a full auxiliary tank. Since overfilling a main tank from an auxiliary tank will
force excess fuel overboard, it is recommen
ded that the transfer pumps not be activated
until their respective main tanks are slightly more than one quarter full. If the tank being
transferred to is feeding the engine, however, transfer can be initiated when the main
tank is down to approximately
one half. Confirm fuel transfer by illumination of the
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
decrease on the respective auxiliary tank indicator.
PAGE 12
SECTION III
NORMAL PROCEDURES
turn left), depress right rudder as you pull "T" handle full out.
Lock "T" handle ½ turn right before releasing right rudder pressure. If too much trim,
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above
r to recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
crosswind component is 13K (15 mph) and flap extension
(fully retracted) with such crosswind or higher. 13K (15 mph) is
the maximum demonstrated for certification of the airplane and is not considered
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector
valve on the left kick panel. Auxiliary (outboard) tanks feed their respective main tanks
s on the instrument panel. These
transfer pumps transfer fuel at a rate of 0.4 gallons per minute or approximately 45
minutes for a full auxiliary tank. Since overfilling a main tank from an auxiliary tank will
ded that the transfer pumps not be activated
until their respective main tanks are slightly more than one quarter full. If the tank being
transferred to is feeding the engine, however, transfer can be initiated when the main
one half. Confirm fuel transfer by illumination of the
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a

MAULE AEROSPACE TECHNOLOGY, INC.
3.4 DOOR-
OFF OPERATION:
This aircraft may be operated with either one (not both) of the front doors removed,
both front doors are installed, with the rear passenger door or rear passenger and baggage
doors off. When doing so, observe the following additional limitations:
1.
Maximum airspeed
2.
Maximum bank angle
3.
Maximum yaw angl
4.
No Smoking permitted
5.
Limit flight to VFR conditions
3.5 NOISE LEVEL:
The noise level obtained during certification per FAR 36 was 76.2 dBA.
No determination has been made by the Federal Aviation Administration that the noise level
of
this airplane is or should be acceptable for operation at, into, or out of any airport.
3.6 ANTI-
COLLISION LIGHT:
/////////////////////////
////WARNING////
/////////////////////////
ANTI-
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
WHEN FLYING IN
RECOMMENDED THAT IT BE TURNED OFF UNDER THESE
CONDITIONS.
FAA APPROVED: 6/3/93
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180A
OFF OPERATION:
This aircraft may be operated with either one (not both) of the front doors removed,
both front doors are installed, with the rear passenger door or rear passenger and baggage
doors off. When doing so, observe the following additional limitations:
Maximum airspeed
- 109K (125 mph)
Maximum bank angle
- 30°
Maximum yaw angl
e - 10°
No Smoking permitted
Limit flight to VFR conditions
The noise level obtained during certification per FAR 36 was 76.2 dBA.
No determination has been made by the Federal Aviation Administration that the noise level
this airplane is or should be acceptable for operation at, into, or out of any airport.
COLLISION LIGHT:
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
WHEN FLYING IN
VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
RECOMMENDED THAT IT BE TURNED OFF UNDER THESE
CONDITIONS.
PAGE 13
SECTION III
NORMAL PROCEDURES
This aircraft may be operated with either one (not both) of the front doors removed,
or when
both front doors are installed, with the rear passenger door or rear passenger and baggage
The noise level obtained during certification per FAR 36 was 76.2 dBA.
No determination has been made by the Federal Aviation Administration that the noise level
this airplane is or should be acceptable for operation at, into, or out of any airport.
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
RECOMMENDED THAT IT BE TURNED OFF UNDER THESE

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
SECTION IV
EMERGENCY PROCEDURES
4.1
EMERGENCY BASIC RULES:
To assist the pilot when an emergency occurs, three basic rules are established which apply to
most emergencies occurring while airborne. They should be remembered by each crew
member.
1.
Maintain aircraft control
2.
Analyze the situation and take prop
3.
Land as soon as conditions permit
4.2
ENGINE EMERGENCY SHUT DOWN:
1. Mixture -
Full lean
2. Fuel Selector -
OFF
3. Ignition Switch
-
4.3
ENGINE FIRE DURING STARTING:
1. Mixture -
Full lean
2. Throttle - Open
3. Continue
cranking for several revolutions. Attempt to draw fire inside engine.
4.
Accomplish ENGINE EMERGENCY SHUT DOWN if fire continues.
4.4
ENGINE FIRE AFTER STARTING:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2. Master Switch -
4.5 EMERGENCY EXIT ON
THE GROUND:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2. Master Switch -
3.
Leave aircraft by either door or kick out side window panels or baggage door.
4.6 TAKEOFF ABORT:
(BEFORE LIFT
1. Throttle -
Closed
2. Brakes -
As Required
FAA APPROVED
DATE: PAGE 14
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180A
EMERGENCY PROCEDURES
EMERGENCY BASIC RULES:
To assist the pilot when an emergency occurs, three basic rules are established which apply to
most emergencies occurring while airborne. They should be remembered by each crew
Maintain aircraft control
Analyze the situation and take prop
er action
Land as soon as conditions permit
ENGINE EMERGENCY SHUT DOWN:
Full lean
OFF
-
OFF
ENGINE FIRE DURING STARTING:
Full lean
cranking for several revolutions. Attempt to draw fire inside engine.
Accomplish ENGINE EMERGENCY SHUT DOWN if fire continues.
ENGINE FIRE AFTER STARTING:
Accomplish ENGINE EMERGENCY SHUT DOWN
OFF
THE GROUND:
Accomplish ENGINE EMERGENCY SHUT DOWN
OFF
Leave aircraft by either door or kick out side window panels or baggage door.
(BEFORE LIFT
-OFF)
Closed
As Required
DATE: PAGE 14
SECTION IV
EMERGENCY
PROCEDURES
To assist the pilot when an emergency occurs, three basic rules are established which apply to
most emergencies occurring while airborne. They should be remembered by each crew
cranking for several revolutions. Attempt to draw fire inside engine.
Accomplish ENGINE EMERGENCY SHUT DOWN if fire continues.
Leave aircraft by either door or kick out side window panels or baggage door.