MAULE MX-7-180 Star Rocket Technical specifications

Airplane Serial No.__________________
Registration No.____________________
THIS DOCUMENT MUST
FAA APPROVED:
DATE
2099 Georgia Highway 133 South
[phone] •
Fax:
FAA APPROVED
FOR
MAULE MX-7-180
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
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
All
Added Flap Control Placard.
Changed company headings to read:
'MAULE AEROSPACE TECHNOLOGY,
B 24
Added Tex Tron
Champ (item 12.D.`) Oil
Teledyne Battery (item 13.E.1)
Added AM-
Assemblies (items 32.C.1. and 33.B.2.) to
Required Equipment List.
Added NOTE re Rear Seat occupants
Shoulder Harness requirement.
C iiii,
23-17
Required Equipment List, pages 23 thru
27, removed and replaced with all recip.
models combined Required Equipment
List.
D All
13
20
10
Updated entire AFM to latest format.
Added Front Door
Corrected Center Seat and Rear Seat
Passenger Stations.
Added "Parking Brake...OFF to 3.2.D.
BEFORE TAKEOFF and E. BEFORE
LANDING.
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
LOG OF REVISIONS
DESCRIPTION
APPROVAL AND DATE
Added Flap Control Placard.
Changed company headings to read:
'MAULE AEROSPACE TECHNOLOGY,
INC.'
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Added Tex Tron
- Avco (item 12.C.1.) and
Champ (item 12.D.`) Oil
Filters and
Teledyne Battery (item 13.E.1)
-
Safe Shoulder Harness
Assemblies (items 32.C.1. and 33.B.2.) to
Required Equipment List.
Added NOTE re Rear Seat occupants
Shoulder Harness requirement.
______________________________
Manager,
Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Required Equipment List, pages 23 thru
27, removed and replaced with all recip.
models combined Required Equipment
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Updated entire AFM to latest format.
Added Front Door
-Off Operation.
Corrected Center Seat and Rear Seat
Passenger Stations.
Added "Parking Brake...OFF to 3.2.D.
BEFORE TAKEOFF and E. BEFORE
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
Page i
APPROVAL AND DATE
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________

MAULE AEROSPACE TECHNOLOGY, INC.
E 2
5
6
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 Limitation Placard from
page 6.
Deleted Fuel Capacity numbers from Fuel
Transfer Pump Switch Placard and added note
for Tank Confi
Added Unusable Fuel weight for new Tank
Configurations.
`
F 6 Added JPI
EDM
G 5
5,7,11
6
9,10
17
19
21
23
25
Corrected baggage & cargo load limits.
Removed asterisks.
Removed
redundant flap handle placard.
Added "PUSH KNOB COMPLETELY AGAINST
INSTRUMENT PANEL" for Parking Brake OFF.
Corrected C.G. Range.
Corrected W.B. Calculation.
Removed antiquated C.G. Envelope chart
Corrected structural capacity chart.
Added Required paragr
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
LOG OF REVISIONS
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 Limitation Placard from
Deleted Fuel Capacity numbers from Fuel
Transfer Pump Switch Placard and added note
for Tank Confi
guration.
Added Unusable Fuel weight for new Tank
Configurations.
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Atlanta, GA
Date:_____________________________
EDM
-900/930
______________________________
Manager, Southeast Flight Test
Section, AIR-
712, FAA
Atlanta, GA
Date:_______________________
Corrected baggage & cargo load limits.
Removed asterisks.
redundant flap handle placard.
Added "PUSH KNOB COMPLETELY AGAINST
INSTRUMENT PANEL" for Parking Brake OFF.
Corrected C.G. Range.
Corrected W.B. Calculation.
Removed antiquated C.G. Envelope chart
.
Corrected structural capacity chart.
Added Required paragr
aph.
______________________________
Manager, Southeast Flight Test
Section, AIR-
712, FAA
Atlanta, GA
Date:_______________________
Page ia
______________________________
Manager, Aircraft Certification Office
Federal Aviation
Administration
Date:_____________________________
______________________________
Manager, Southeast Flight Test
712, FAA
Date:_______________________
______________________________
Manager, Southeast Flight Test
712, FAA
Date:_______________________

Contents
SECTION I..........................................................................................................................................................2
GENERAL: NORMAL CATEGORY OPERATION ........................................................................................2
1.1 MAXIMUM WEIGHT: 2500 Pounds .................................................................................................2
1.2 CENTER OF GRAVITY LIMITS: ........................................................................................................2
1.3 MANEUVERS:....................................................................................................................................2
1.4 FUEL CAPACITY: ..............................................................................................................................2
SECTION II.........................................................................................................................................................3
LIMITATIONS.....................................................................................................................................................3
2.1 AIRSPEED LIMITS:............................................................................................................................3
2.2 POWER PLANT LIMITS.....................................................................................................................4
2.3 FLIGHT LOAD FACTORS..................................................................................................................5
2.4 PLACARDS: .......................................................................................................................................5
SECTION III........................................................................................................................................................7
NORMAL PROCEDURES:.................................................................................................................................7
3.1 PREFLIGHT INSPECTION ................................................................................................................7
3.2 OPERATING CHECK LISTS:.............................................................................................................8
3.3 NORMAL FLIGHT OPERATIONS:...................................................................................................11
3.4 DOOR-OFF OPERATION:...............................................................................................................13
SECTION IV .....................................................................................................................................................14
EMERGENCY PROCEDURES........................................................................................................................14
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: (BEFORE LIFT-OFF) ......................................................................................14
4.7 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING: ....................................................15
4.8 PARTIAL POWER FAILURE DURING FLIGHT OR AFTER TAKEOFF:.........................................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
SECTION V ......................................................................................................................................................17
WEIGHT AND BALANCE.................................................................................................................................17
LOADING CHART............................................................................................................................................20
WEIGHT AND BALANCE ENVELOPE ............................................................................................................22
STRUCTURAL CAPACITY CHART.................................................................................................................23
SECTION VI .....................................................................................................................................................25
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE..........................................................................25
6.1 INTRODUCTION:.............................................................................................................................25
6.2 AIRPLANE INSPECTION PERIOD:.................................................................................................25
6.3 PREVENTIVE MAINTENANCE THAT MAY BE ACCOMPLISHED BY A CERTIFIED PILOT: ......25
6.4 ALTERATIONS OR REPAIRS TO AIRPLANE: ...............................................................................25

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180 Page ii
LOG OF SUPPLEMENTS
SUPP.
NO. NO. OF PAGES
DESCRIPTION
APPROVAL
DATE
1 2 Installation of Century 21 Autopilot - Maule Installation Manual AK932. 08/12/86
- 1 Installation of Aero-Trim Model 400 Electric Aileron Trim System. 09/24/87
2 2 Installation of Century IIB Autopilot - Maule Installation Manual AK513. 09/21/87
4 6 Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14v) - Maule Dwg 9196A. (Land) 04/04/00
5 6 Inst. of S-TEC System 55 Two Axis Autopilot ST-620 (14v) - Maule Dwg 9196A.(Sea) 04/04/00
6 9 Inst. of S-TEC System 50 Two Axis Autopilot ST-418-50 (14v) - Maule Dwg 9193A. 01/05/00
7 9 Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - Dwg 9197A. (Land) 01/21/00
8 9 Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - Dwg 9197A. (Sea) 01/21/00
9 9 Inst. of S-TEC System 50 Two Axis Autopilot ST-609-50 (28v) - Maule Dwg 9200A. 02/14/00
10 9 Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - Dwg 9197A. (Land) 03/20/00
11 9 Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - Dwg 9197A. (Sea) 03/20/00
12 9 Inst. of S-TEC System 20 Single Axis Autopilot ST-820-20 (28v) - Maule Dwg 9201A. 03/20/00
13 7 Inst. of S-TEC System 40 Single Axis Autopilot ST-418-40 (14v) - Maule Dwg 9193A. 10/29/01
14 7 Inst. of S-TEC System 40 Single Axis Autopilot ST-609-40 (28v) - Maule Dwg 9200A. 10/29/01
- 4 Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (28v) - Dwg 9211A. (Land) 06/25/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (28v) - Dwg 9211A. (Land) 06/25/01
- 5 Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (28v) - Dwg 9211A. (Sea) 06/25/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (28v) - Dwg 9211A. (Sea) 06/25/01
- 3 Inst. of GARMIN GNS-430 (GPS/NAV/COMM) System - Maule Dwg 7205A. 01/03/01
- 3 Inst. of GARMIN GNC-300XL (GPS/COMM) System - Maule Dwg 7207A. 01/03/01
- 3 Inst. of GARMIN GNC-250XL (GPS/COMM) System - Maule Dwg 7209A. 01/03/01
- 3 Inst. of Bendix-King KLX-135A (GPS/COMM) System - Maule Dwg 7219A. 01/03/01
- 5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST-873-20 (14/28v) - Maule
Dwg 9212A. (Land) 10/15/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST-873-30 (14/28v) - Maule Dwg
9212A. (Land) 10/15/01
15 9 Installation of Aqua 2200 Floats per Maule Installation Drawing 9225A. 10/29/02
- 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

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

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION I
GENERAL: NORMAL
CATEGORY OPERATION
1.1 MAXIMUM WEIGHT:
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.
C
Main
Aux.
////////////////////////
////CAUTION////
////////////////////////
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 12/18/84
Rev. A dated: 4/25/85
Rev. D dated: 6/10/94
Rev. E dated:
Page 2
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
CATEGORY OPERATION
2500 Pounds
CENTER OF GRAVITY LIMITS:
+16.7 to +20.5 @ 2500 lbs.
+13.6 to +20.5 @ 1600
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.
21.5 15.0 2.3 0.0
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY
CANNOT BE USED SAFELY IN FLIGHT.
SECTION I
GENERAL
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 WITH FUEL BURN.
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:
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
from flaps
cruise speed (V
White Arc -
Flap Operating Range, 41
full flap, pow
the Maximum flaps extended speed (V
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
Rev. D Dated:
Page 3
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
LIMITATIONS
MAULE MX-7-180
All airspeeds are Indicated Airspeeds (IAS).
AIRSPEED INDICATOR MARKINGS:
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 25
00 lbs. (V
cruise speed (V
C
).
Flap Operating Range, 41
- 85K (47 -
98 mph): Extends from
full flap, pow
er off minimum stall speed at 25
00 lbs.
the Maximum flaps extended speed (V
FE
).
SECTION II
LIMITATIONS
) 161K (185 mph): Maximum safe
185 mph): Operation in this
speed range should be conducted only in smooth air and
control movements should not be large or abrupt.
149 mph): Extends
00 lbs. (V
S1
) to design
98 mph): Extends from
00 lbs.
(V
SO
) to

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: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
Page 4
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
POWER PLANT LIMITS
:
Lycoming O-360-C1F
180 hp @ 2700 rpm, Full Throttle Continuous
Hartzell Constant Speed HC-C2YR-
1BF/F7666A (76")
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 in. of Mercury
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 -
Norma
l Operating Range,
2250 - 26
00 RPM
Red Radial -
Maximum RPM, 2700 RPM
Red Arc -
Avoid Continuous Operation,
2000 - 22
50 RPM
SECTION II
LIMITATIONS
180 hp @ 2700 rpm, Full Throttle Continuous
1BF/F7666A (76")
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 in. of Mercury
Normal Operating Range,
Minimum Pressure, 0.5
PSI,
Maximum Pressure, 8.0
PSI
l Operating Range,
00 RPM
Maximum RPM, 2700 RPM
Avoid Continuous Operation,
50 RPM

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

MAULE AEROSPACE TECHNOLOGY, INC.
PLACARDS: (Cont’d)
At the main fuel tank selector
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
installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are used as below:
FUEL CAPACIT
Y: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
(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.
tanks not installed.
FAA APPROVED
DATE: 12/18/85
REV. A Dated: 4/25/85
Rev. D Dated: 6/10/94
Rev. E Dated:
Rev. F Dated: 03/28/2018
Rev G Dated:
Page 6
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
At the main fuel tank selector
valve on the left kick panel:
FUEL SELECTOR VALVE
LEFT: * GAL.
OFF BOTH
RIGHT: * GAL.
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 below:
FUEL TRANSFER PUMPS
LEFT RIGHT
Y: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
*
GAL. 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 auxiliary
SECTION II
LIMITATIONS
placard is located on the instrument panel at the optional auxiliary tank transfer
PUSH FOR
AUX. QUANT.
PUSH FOR AUX. QUANT. buttons and placards are not
installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are used as below:
GAL. USABLE EACH.
*Instrument panel placard will show capacity of the tanks installed in this aircraft. See Table on Page
Auxiliary tank placards will be deleted when auxiliary

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 the fuselage, then around the tail section.
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
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…………………………………….….
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
REV. G Dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
Page 7
PREFLIGHT INSPECTION
:
BAT Switch…………………………………....
ON
Fuel Gauges……………………………….….
CHECK INDICATIONS
Auxiliary Fuel Pumps………………………...
ON, THEN OFF (LISTEN TO VERIFY
OPERATION)
All Electrical Switches…………………….….
OFF
BAT Switch………………………………….…
OFF
Flaps……………………………………….…..
FULL DOWN (4TH NOTCH)
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 &
ATTACHMENTS
Aileron………………………………………….
CHECK HINGES & CONTROL
ATTACHMENTS
Left Wing 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
Auxiliary Fuel Tank (if installed)....................
VISUALLY CHECK QUANTITY
Landing Light…………………………………..
CHECK FOR DAMAGE
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
LINE SECURITY
Bottom left side of Cowl…………………..….
DRAIN GASCOLATOR (1)
Top Cowl, Oil Access Door……………….…
CHECK OIL QUANTITY
Propeller………………………………………..
CHECK LEADING EDGE FOR
DAMAGE.
Inlets…………………………………….….
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
SECTION III
NORMAL
CHECK INDICATIONS
ON, THEN OFF (LISTEN TO VERIFY
FULL DOWN (4TH NOTCH)
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.
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
CHECK FOR FREEDOM OF
VISUALLY CHECK QUANTITY
CHECK TIRE INFLATION
AND BRAKE
DRAIN GASCOLATOR (1)
CHECK OIL QUANTITY
CHECK LEADING EDGE FOR
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS
SECTION III
NORMAL
PROCEDURES

MAULE AEROSPACE TECHNOLOGY, INC.
3.1
PREFLIGHT INSPECTION: (Cont'd)
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.
Propeller Control............................................
5.
Mixture Control...............................................
6. Anti-
Collision Light………………………….....
7.
BAT and ALT Switch......................................
8.
Primer.............................................................
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
Page 8
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
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
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 BOTH IF SAME
QUANTITY
Throttle………………………………………….
OPEN 1/4 INCH
Propeller Control............................................
FULL
INCREASE RPM
Mixture Control...............................................
RICH (SEE NOTE NEXT PAGE FOR
HOT START)
Collision Light………………………….....
ON
BAT and ALT Switch......................................
ON
Primer.............................................................
AS REQUIRED
SECTION III
NORMAL
PROCEDURES
CHECK TIRE INFLATION & BRAKE LINE
INSPECT SAME AS LEFT WING
INSPECT FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
CHECK ATTACHMENT POINTS &
CHECK HINGE POINTS
CHECK HINGE POINTS, CONTROL
ATTACHMENT & NAV LIGHT
CHECK FOR INFLATION,
ATTACHMENTS, REMOVE TIEDOWN
CHECK TAB CONTROLS & ALL HINGE
CHECK ATTACHMENT POINTS &
CHECK FOR WRINKLES AS
INTERNAL DAMAGE
ON FULLEST TANK, OR BOTH IF SAME
INCREASE RPM
RICH (SEE NOTE NEXT PAGE FOR

MAULE AEROSPACE TECHNOLOGY, INC.
3.2
OPERATING CHECK LISTS: (Cont'd)
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
IDLE AND EASE MIXTURE TO FULL RICH.
9.
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.
10. After
Starting……………………………….….
////////////////////////
////CAUTION////
////////////////////////
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS, SHUT
DOWN ENGINE.
11.
Alternator………………………………….…...
12. Radios &
other electrical switches……..……
13.
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
RIGHT OF MORE THAN 50 RPM IS UNACCEPTABLE.
5.
Propeller Control..........................................
6.
Carburetor Air Control
7.
Carburetor Air Control……………………....
8.
Vacuum Gauge………………………….…….
9.
Alternator……………………………………….
10.
Throttle………………………………………….
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
REV. G Dated:
Page 9
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
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 STARTS, PULL
IDLE AND EASE MIXTURE TO FULL RICH.
Starter Switch............................................ TWIST FULL RIGHT TO ENGINE
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 (PUSH KNOB COMPLETELY AGAINST
INSTRUMENT PANEL)
Parking Brake………………………………….
ON, IF DESIRED
Engine Instruments………………………..….
CHECK, IN GREEN
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.
Propeller Control..........................................
RETARD SLOWLY UNTIL MAXIMUM OF
500 RPM DROP IS NOTED. RETURN TO
FULL RPM. REPEAT. SET FULL
INCREASE RPM.
Carburetor Air Control
……………………....
PULL HOT, NORMAL DROP WITH
CARBURETOR AIR HOT IS 150
Carburetor Air Control……………………....
PUSH COLD
Vacuum Gauge………………………….…….
CHECK IN GREEN
Alternator……………………………………….
CHARGING: LIGHT OUT ABOVE
Throttle………………………………………….
RETARD TO IDLE
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 STARTS, PULL
THROTTLE TO
Starter Switch............................................ TWIST FULL RIGHT TO ENGINE
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
CHECK OIL PRESSURE
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS, SHUT
CHECK CHARGING
OFF (PUSH KNOB COMPLETELY AGAINST
INSTRUMENT PANEL)
CHECK, IN GREEN
ARCS
INCREASE TO 2000 RPM
SWITCH TO RIGHT, LEFT, BOTH,
CHECKING RPM DROPS
DIFFERENCE BETWEEN LEFT AND
RETARD SLOWLY UNTIL MAXIMUM OF
500 RPM DROP IS NOTED. RETURN TO
FULL RPM. REPEAT. SET FULL
PULL HOT, NORMAL DROP WITH
CARBURETOR AIR HOT IS 150
±50 RPM
CHECK IN GREEN
CHARGING: LIGHT OUT ABOVE
900 RPM

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.
Propeller Control............................................
7.
Carburetor Air Control .............
8.
Engine Instruments……………..…………….
9.
Radios…………………………….……………
10.
Altimeter………………………….……………
11.
Attitude Indicator………………….…………..
12.
Directional Indicator……………….………….
13.
Seat Belts & Shoulder Harnesses.………….
14.
Doors.............................................................
15.
Passengers....................................................
16. Parking
Brake................................................
E.
BEFORE LANDING:
1.
Seat Belts & Shoulder Harnesses……….….
2.
Fuel Selector Valve……………………….…..
3.
Mixture Control…………………………….….
4.
Propeller Control……………………………...
5.
Flaps……………………………….…………....
6.
Carburetor Air Control
7.
Parking Brake................................................
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: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
REV. G Dated:
Page 10
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MX-7-180
OPERATING CHECK LISTS:
(Cont'd)
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
Control…………….……………….…
FULL RICH
Propeller Control............................................
FULL INCREASE RPM
Carburetor Air Control .............
....…….……..
PUSH COLD
Engine Instruments……………..…………….
RECHECK IN NORMAL RANGE
Radios…………………………….……………
AS DESIRED
Altimeter………………………….……………
SET
Attitude Indicator………………….…………..
CHECK ERECT
Directional Indicator……………….………….
SET
Seat Belts & Shoulder Harnesses.………….
RECHECK FASTENED
Doors.............................................................
CLOSED & LATCHED
Passengers....................................................
BELTS & HARNESSES SECURED.
BRIEFED ON OPENING DOORS.
Brake................................................
OFF
BEFORE LANDING:
Seat Belts & Shoulder Harnesses……….….
FASTENED
Fuel Selector Valve……………………….…..
ON FULLEST TANK OR BOTH
Mixture Control…………………………….….
FULL RICH
Propeller Control……………………………...
FULL INCREASE RPM
Flaps……………………………….…………....
AS REQUIRED
Carburetor Air Control
….…………................ PULL HOT
Parking Brake................................................
OFF
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)
KNOB COMPLETELY AGAINST
INSTRUMENT PANEL)
ON FULLEST TANK OR BOTH
AS DESIRED FOR T.O. (MAX. 24
°)
SET FOR TAKEOFF
CHECK FOR FREEDOM AND
PROPER TRAVEL
FULL INCREASE RPM
RECHECK IN NORMAL RANGE
RECHECK FASTENED
CLOSED & LATCHED
BELTS & HARNESSES SECURED.
BRIEFED ON OPENING DOORS.
ON FULLEST TANK OR BOTH
FULL INCREASE RPM
PERFORM BELOW 1000 RPM
OFF (AS DESIRED)
(FOR OFF, PUSH
KNOB COMPLETELY AGAINST
INSTRUMENT PANEL)

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 LANDING UNDER GUSTY CROSSWIND
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.
FAA APPROVED
DATE: 12/18/84
Rev. A dated: 4/25/85
Rev. D dated:
Rev. G dated:
Page 11
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180
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 optional
94 mph (81.7 knots)
IAS, flaps @ First Notch (0
– 78 mph (67.8 knots)
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.
SECTION III
NORMAL PROCEDURES
Flap settings are given in number of notches above the fully retracted position, which
other positions optional
IAS, flaps @ First Notch (0
°)
IAS with flaps set @ Second Notch (24
°)
FOR TAKEOFF OR 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

MAULE AEROSPACE TECHNOLOGY, INC.
3.3
NORMAL FLIGHT OPERATIONS:
D. RUDDER TRIM:
NOTE: To assure full
Unlock "T" handle (1/2 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
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 prior to rec
feet.
////////////////////////
////CAUTION////
////////////////////////
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
F.
CROSSWIND LANDINGS & TAKEOFFS:
Maximum demonstrated crosswind
should be limited to 0
the maximum demonstrated for certification of the airplane and is not considered
limiting with flaps at 0
G. FUEL SYST
EM 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 switches on the
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 recommended that
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.
transfer pump switch, an increase in the respective main tank fuel gauge indicator, and a
decrease on the respective auxiliary tank indicator.
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
Rev. D Dated:
Page 12
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180
NORMAL FLIGHT OPERATIONS:
(Cont'd)
NOTE: To assure full
effectiveness of the Right Rudder Trim:
Unlock "T" handle (1/2 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 prior to rec
overy 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
°.
EM 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 switches 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 recommended 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.
SECTION III
NORMAL PROCEDURES
Unlock "T" handle (1/2 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
overy from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
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
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
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
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 angle
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 VI
RECOMMENDED THAT IT BE TURNED OFF UNDER THESE
CONDITIONS.
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
Page 13
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III
AIRPLANE FLIGHT MANUAL
NORMAL PROCEDURES
MAULE MX-7-180
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 angle
- 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
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 VI
SIBLE MOISTURE OVERCAST OR HAZE. IT IS
RECOMMENDED THAT IT BE TURNED OFF UNDER THESE
CONDITIONS.
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
airplane is or should be acceptable for operation at, into, or out of any airport.
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
SIBLE 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
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: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
Page 14
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE
MX-7-180
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
EMERGENCY EXIT ON
THE GROUND:
Accomplish ENGINE EMERGENCY SHUT DOWN
OFF
Leave aircraft by either door or kick out side window panels or baggage door.
TAKEOFF ABORT: (BEFORE LIFT
-OFF)
Closed
As Required
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.

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
4.7
ENGINE FAILURE AFTER
1. Glide -
Establish 72K (83 mph) IAS with flaps at 0
2.
Switch Fuel Selector to fullest tank
3.
Electric Fuel Pump
4.
Mixture Rich, Ignition On
5.
Alternate Air Control
6.
If engine does not restart,
7. Wing Flaps -
As Required
8. Master Switch -
Off
4.8
PARTIAL POWER FAILURE DURING FLIGHT OR AFTER TAKEOFF:
1. Mixture - Rich
2.
Alternate Air Control
3. Airspeed -
Glide at 72K (83 mph) IAS if unable to mainta
4. Fuel Selector -
Both
5.
Electric Fuel Pump
6. Ignition Switch -
Both
7. Master Switch -
On
4.9
COMPLETE POWER FAILURE DURING FLIGHT:
1. Glide -
Establish 72K (83 mph) IAS
2.
Attempt engine airstart if warranted
4.10 ENGINE AIRSTART:
1. Fuel Selector -
Both
2.
Electric Fuel Pump
3. Mixture - Rich
4. Ignition Switch -
Both (start if propeller is not turning)
5.
Auxiliary Fuel Tank Pump Switch (when so equipped)
Auxiliary tank has fuel.
6.
If engine does no
and mixture full lean.
7.
If no start, make forced landing
NOTE: PROP
ELLER WILL NOT WINDMILL BELOW 63K (73
NOTE:
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.
4.11 ELECTRICAL FIRE:
1. Master Switch -
Off
FAA APPROVED
DATE: 12/18/84
REV. A Dated: 4/25/85
REV. D Dated:
Page 15
MAULE AEROSPACE TECHNOLOGY, INC.
SECTION IV
AIRPLANE FLIGHT MANUAL
EMERGENCY PROCEDURES
MAULE MX-7-180
ENGINE FAILURE AFTER
TAKEOFF OR FORCED LANDING:
Establish 72K (83 mph) IAS with flaps at 0
°
Switch Fuel Selector to fullest tank
Electric Fuel Pump
- On
Mixture Rich, Ignition On
Alternate Air Control
- Pull On
If engine does not restart,
accomplish EMERGENCY SHUT DOWN
As Required
Off
PARTIAL POWER FAILURE DURING FLIGHT OR AFTER TAKEOFF:
Alternate Air Control
- Pull On
Glide at 72K (83 mph) IAS if unable to mainta
in level flight
Both
Electric Fuel Pump
- On
Both
On
COMPLETE POWER FAILURE DURING FLIGHT:
Establish 72K (83 mph) IAS
Attempt engine airstart if warranted
Both
Electric Fuel Pump
- On
Both (start if propeller is not turning)
Auxiliary Fuel Tank Pump Switch (when so equipped)
–
On for tank feeding engine if
Auxiliary tank has fuel.
If engine does no
t start, try flooded engine clearing procedure with throttle wide open
and mixture full lean.
If no start, make forced landing
ELLER WILL NOT WINDMILL BELOW 63K (73
MPH).
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.
Off
SECTION IV
EMERGENCY PROCEDURES
accomplish EMERGENCY SHUT DOWN
in level flight
On for tank feeding engine if
t start, try flooded engine clearing procedure with throttle wide open
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.