MAULE MT-7-260 Technical specifications

MAULE
Airplane Serial No._______________________
Registration No._________________________
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:________________________________
DATE:________________________________
2099 Georgia Highway 133 South
(229) 985-
2045
FAA APPROVED
FOR
MAULE
MT-7-260
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
DATE:________________________________
Performance That Counts!
2099 Georgia Highway 133 South
•Moultrie, GA 31788
2045
•Fax: [phone] or [phone] •
www.mauleairinc.
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:________________________________
Aircraft Certification Office
www.mauleairinc.

MAULE AEROSPACE TECHNOLOGY, INC.
REV. TO
PAGES
DESCRIPTION
A 5,6
12
19
Added and revised Placards.
Corrected Crosswind Component.
Corrected omission.
B 4
Vendor part number change.
C 12
Corrected (fully retracted) to read (first notch) in Item F.
D 2
4
13
Corrected unusable fuel to read 2.3 gallons.
Added McCauley Propellers B2D37C224
and B3D32C414-[ ]/[ ]
-
E 3,5,
11-16
Changed primary airspeed units to knots.
F iiii
3
5
6
19
20
22
24
Changed page number from 33
Moved note from Sec. 2.3 to Sec. 2.1
Removed note from Sec. 2.3.
Added JPI EDM-
900/930
Corrected example of Weight & Balance calculation
Corrected Loading Chart
Corrected Structural
Capacity Chart
Changed page number from 33 to 24
to Airplane Inspection Period.
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
LOG OF REVISIONS
DESCRIPTION
APPROVAL AND DATE
Added and revised Placards.
Corrected Crosswind Component.
_________________________
Manager, Aircraft Certificat
Atlanta, Georgia
Date:
_____________________
Vendor part number change.
.
_________________________
Manager, Aircraft Certification Office,
Atlanta, Georgia
Date:_____________________
Corrected (fully retracted) to read (first notch) in Item F.
______
__________________
Manager, Aircraft Certification Office, FAA
Atlanta, Georgia
Date:_____________________
Corrected unusable fuel to read 2.3 gallons.
Added McCauley Propellers B2D37C224
-[ ]/[ ]-90RA-
10.5
-
82NDA-2.
_________________________
Manager, Aircraft Certification Office, FAA
Atlanta, Georgia
Date:_____________________
Changed primary airspeed units to knots.
_________________________
Manager, Aircraft Certification Office, FAA
Atlanta, Georgia
Date:_____________________
Changed page number from 33
to 24 in TOC.
Moved note from Sec. 2.3 to Sec. 2.1
.
Removed note from Sec. 2.3.
900/930
. Corrected cargo limitations.
Corrected example of Weight & Balance calculation
Corrected Loading Chart
Capacity Chart
Changed page number from 33 to 24
.
Added requirement
to Airplane Inspection Period.
_________________________
Manager, Southeast Flight Test
Section, AIR-
712, FAA
Atlanta, GA
Date:_____________________
Page i
APPROVAL AND DATE
_________________________
Manager, Aircraft Certificat
ion Office, FAA
_____________________
_________________________
Manager, Aircraft Certification Office,
FAA
Date:_____________________
__________________
Manager, Aircraft Certification Office, FAA
Date:_____________________
_________________________
Manager, Aircraft Certification Office, FAA
Date:_____________________
_________________________
Manager, Aircraft Certification Office, FAA
Date:_____________________
_________________________
Manager, Southeast Flight Test
712, FAA
Date:_____________________

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
Page ii
LOG OF SUPPLEMENTS
SUPP.
NO. NO. OF PAGES
DESCRIPTION
APPROVAL
DATE
1 21 Installation of Wipline 3000 Amphibious Floats - Maule Drawing 9186A.
(03/12/99) Rev. A 08/19/02
2 8 Installation of Aqua 2400 Floats - Maule Drawing 9135A, Rev. Eor later.
(11/19/99) Rev. A 08/19/02
3 6 English to Metric Conversion Charts - required in aircraft when registered in
Canada. 09/03/99
4 5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST-810-20 (14v) -
Maule Drawing 9197A, Rev. Cor later. (Sea) 07/05/01
5 5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST-810-30 (14v) - Maule
Drawing 9197A, Rev. Cor later. (Sea) 07/05/01
6 4 Inst. of S-TEC System 20 Single Axis Autopilot Model ST-872-20 (28v) -
Maule Drawing 9211A. (Land) 06/25/01
7 5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST-872-30 (28v) - Maule
Drawing 9211A. (Land) 06/25/01
- 5 Inst. of S-TEC System 20 Single Axis Autopilot Model ST-872-20 (28v) -
Maule Drawing 9211A. (Sea) 06/25/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot Model ST-872-30 (28v) - Maule
Drawing 9211A. (Sea) 06/25/01
- 3 Inst. of GARMIN GNS-430
(GPS/NAV/COMM) System - Maule Drawing 7205A. 01/03/01
- 3 Inst. of GARMIN GNC-300XL
(GPS/COMM) System - Maule Drawing 7207A. 01/03/01
- 3 Inst. of GARMIN GNC-250XL
(GPS/COMM) System - Maule Drawing 7209A. 01/03/01
- 3 Installation of Bendix-King KLX-135A (GPS/COMM) System - Maule Drawing
7219A. 01/03/01
- 5 Installation of Apollo MX20 Multi-Function Display - Maule Drawing 7265A. 08/15/02
- 8 Installation of GARMIN GNC-420 (GPS/COMM) System - Maule Drawing
7251A. 06/30/03
- 9 Installation of GARMIN GNS-530 (GPS/NAV/COMM) System - Maule Drawing
7253A. 06/30/03
- 4 Installation 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 MT-7-260
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….……….. 14
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………………………….……… 15
4.13 Smoke and Fume Elimination…………………….……… 16
4.14 Structural Damage………………………………….…….. 16
4.15 Recovery From Inadvertent Spins………………….…… 16
4.16 Alternator Failure…………………………………….……. 16

MAULE AEROSPACE TECHNOLOGY, INC.
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
a Certified Pilot…………………………………………..…
6.4
Alterations or Repairs to Airplane………………………
SECTION VII
MANUFACTURER'S DATA
Optional Equipment List………..Provided for each Airplane
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
Page iiii
TABLE OF CONTENTS
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
Preventive Maintenance that may be
Accomplished by
a Certified Pilot…………………………………………..…
24
Alterations or Repairs to Airplane………………………
.. 24
MANUFACTURER'S DATA
Optional Equipment List………..Provided for each Airplane
Page iiii
WEIGHT AND BALANCE AND EQUIPMENT LIST
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
SECTION I - GENERAL
PAGE 1

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
SECTION I
GENERAL : NORMAL CATEGORY OPERATION
1.1 MAXIMUM WEIGHT: 2500 Pounds
1.2 CENTER OF GRAVITY LIMITS: +15.0 to +20.0 @ 2500 lbs.
+12.0 to +20.0 @ 1700 lbs. or less
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, ESPECIALLY WHEN USING
THE 5
TH
SEAT OR 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 Eights, Chandelles and
steep turns involving bank angles not greater than 60°are approved in this airplane.
////////////////////////
////CAUTION////
//////////////////////// AEROBATICS AND INTENTIONAL SPINS PROHIBITED.
1.4 FUEL CAPACITY: Usable and Unusable Fuel: See Table Below
Usable Fuel: MAIN TANKS - 21.5 Gal. each
OPTIONAL AUXILIARY TANKS - 15.0 Gal. or 21.0 Gal. each*
Unusable Fuel: 2.3 Gallons per Main Tank
*Fuel Capacity - See Instrument Panel Placard for Tank configuration installed
in this aircraft.
////////////////////////
////CAUTION///
////////////////////////
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY CAN-
NOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 4/17/98
Rev. D dated: 4/17/00
PAGE 2

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
) - 158K
(182
Yellow Arc, Caution Range
-
Green Arc, Normal
Operating Range
Whit
e 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
speed range should be conducted only in smooth air and co
trol movements should not be
Green Arc -
Normal Operating Range
from flaps
cruise speed (V
White Arc -
Flap Operating Range
full flap, pow
the Maximum flaps extended speed (V
NOTE:
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic controls
can be applied (VA) is 109K (125 mph). This airspeed is not marked on the airspeed indicator.
FAA APPROVED: 4/17/98
Rev. E dated:
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
: All airspeeds are Indicated Airspeeds (IAS).
AIRSPEED INDICATOR MARKINGS:
(182
mph)
-
128 - 158K (147 - 182 mph)
Operating Range
- 54 - 128K (62 - 147 mph)
e Arc, Flap Operating Range
- 43 - 83K (50 - 95 mph)
EXPLANATION OF AIRSPEED INDICATOR MARKINGS:
Never Exceed Speed (V
NE
) 158K (182
mph): Maximum safe
airspeed in smooth air.
Caution Range
, 128 - 158K (147 - 182
mph): Operation in this
speed range should be conducted only in smooth air and co
trol movements should not be
large or abrupt.
Normal Operating Range
, 54 - 128K (62 - 147
mph): Extends
from flaps
up, power off stall speed at 2500 lbs. (V
S1
) to design
cruise speed (V
C
).
Flap Operating Range
, 43 - 83K (50 - 95
mph): Extends from
full flap, pow
er off minimum stall speed at 2500 lbs. (V
SO
the Maximum flaps extended speed (V
FE
).
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic controls
can be applied (VA) is 109K (125 mph). This airspeed is not marked on the airspeed indicator.
PAGE 3
mph): Maximum safe
mph): Operation in this
speed range should be conducted only in smooth air and co
n-
mph): Extends
) to design
mph): Extends from
SO
) to
DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic controls
can be applied (VA) is 109K (125 mph). This airspeed is not marked on the airspeed indicator.

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
SECTION II - LIMITATIONS
2.2 POWER PLANT LIMITS:
Cylinder Head Temperature: Green Arc - Normal Operating Range,
200°F - 435°F
Red Radial - Operating Limit, 500°F
Oil Temperature: Green Arc - Normal Operating Range,
140°F - 245°F
Red Radial - Operating Limit, 245°F
Oil Pressure: Green Arc - Normal Operating Range,
55 to 95 psi
Yellow Arc - Caution Range, 25 to 55 psi and
95 to 115 psi
Red Radial - Minimum Operating Pressure,
25 psi, Maximum Operating
Pressure, 115 psi
Manifold Pressure: Green Arc - Normal Operating Pressure,
14.5 to 29 ins. of Mercury
Fuel Flow Red Radial - Maximum, 8.9 psi or 26.9 gph
Tachometer: Green Arc - Normal Operating Range,
2000 - 2700 RPM
Red Radial - Maximum RPM, 2700 RPM
* Limited to no dash number (78" diameter) to -2 (76" diameter)
Engine: Lycoming IO-540-V4A5
Engine Limits: 235 hp @ 2700 RPM, Full Throttle Continuous
Propeller: MT-Propeller: MTV-14-B/190-17
Hartzell: HC-C2YR-1BF/F8477D-6
HC-C3YR-1RF/F7693(F)-( )*
McCauley: B2D37C224-[ ]/[ ]-90RA-10.5 or -12
B3D32C414-[ ]/[ ]-82NDA-2 or -4
Fuel: 100/100LL Minimum Grade Aviation Gasoline
Engine Instrument Markings:
FAA APPROVED: 4/17/98
Rev. B dated: 6/23/99
Rev. D dated: 4/17/00 PAGE 4

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II - LIMITATIONS
2.3 FLIGHT LOAD FACTORS:
Flaps Fully Retracted: 3.8g Positive
Flaps Extended: 1.9g Positive to 0g Negative
2.4 PLACARDS:
The following placards are in the cockpit in clear view of the pilot:
DEMONSTRATED CROSSWIND 12K (14 mph)
Located on flap control handle:
FLAPS / PULL ON / 2
ND
NOTCH / TAKEOFF /
On the instrument panel at the
auxiliary tank
FUEL TRANSFER PUMPS
PUSH FOR
AUX. QUANT.
LEFT
NOTE: If JPI EDM-
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:
LEFT RIGHT
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING
NUAL AND IN THE FORM OF PLACARDS AND MARKINGS.
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED.
ROUGH AIR OR
MANEUVERING SPEED 109K (125 MPH) IAS.
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
FLIGHT MANUAL.
THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON
EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS
IN FLIGHT.
FAA APPROVED: 4/17/98
Rev. A dated: 10/26/98
Rev. E dated:
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
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:
DEMONSTRATED CROSSWIND 12K (14 mph)
NOTCH / TAKEOFF /
3
RD
NOTCH / LANDING.
auxiliary tank
transfer switches:
FUEL TRANSFER PUMPS
PUSH FOR
AUX. QUANT.
RIGHT
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and placards are not installed.
FUEL TRANSFER PUMPS and LEFT and RIGHT placards are used as below:
FUEL TRANSFER PUMPS
LEFT RIGHT
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING
LIMITATIONS STATED IN THE FLIGHT M
NUAL AND IN THE FORM OF PLACARDS AND MARKINGS.
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED.
MANEUVERING SPEED 109K (125 MPH) IAS.
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF
AIRPLANE
THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON
-
ICING FLIGHT WHEN
EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS
ZERO CANNOT BE USED SAFELY
PAGE 5
900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and placards are not installed.
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
LIMITATIONS STATED IN THE FLIGHT M
A-
AIRPLANE
ICING FLIGHT WHEN
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
ZERO CANNOT BE USED SAFELY

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II - LIMITATIONS
2.4 PLACARDS: (Cont’d)
FUEL CAPACITY: MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS
USABLE EACH.
*15 Gal. or 21 Gal.
Instrument Panel Placard will show capacity of the tanks installed in this aircraft.
At the main fuel tank selector valve on the left kick panel:
FUEL SELECTOR VALVE
LEFT: 21.5
OFF
RIGHT:
In rear cabin area:
CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A
" 100 LBS.
MAX. LOAD AREA "B" 175
MAX. LOAD AREA "C"
125
CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMU
FAA APPROVED:
DATE: 4/17/98
Rev. A dated: 10/26/98
Rev. F dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
FUEL CAPACITY: MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS
*
USABLE EACH.
Instrument Panel Placard will show capacity of the tanks installed in this aircraft.
At the main fuel tank selector valve on the left kick panel:
FUEL SELECTOR VALVE
LEFT: 21.5
GAL. BOTH
RIGHT:
21.5 GAL.
CARGO OR BAGGAGE LIMITATIONS
" 100 LBS.
MAX. LOAD AREA "B" 175
LBS.
125 LBS.
CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMU
M REAR SEAT LOADING IS 170 LBS.
PAGE 6
GAL.
Instrument Panel Placard will show capacity of the tanks installed in this aircraft.
CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
M REAR SEAT LOADING IS 170 LBS.

MAULE AEROSPACE TECHNOLOGY, INC.
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 & Aux Fuel Tank Drain…….
6.
Left Wing Tip & Nav Light……………………
7.
Auxiliary Fuel Tank.......................................
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:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
Switch………………………………….....
ON
Fuel Gauges……………………………………
CHECK INDICATIONS
Auxiliary Fuel Pumps.....................................
ON, THEN OFF (LISTEN TO VERIFY
OPERATION
All Electrical Switches…………………………
OFF
Switch…………………………………….
OFF
Flaps……………………………………………
FULL DOWN (
3RD 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
Left Wing Top…………………………………
CHECK FOR WRINKLES AS INDIC
TION OF INTERNAL
DAMAGE
Left Wing Main & Aux Fuel Tank Drain…….
DRAIN (2)
Left Wing Tip & Nav Light……………………
CHECK FOR DAMAGE
Auxiliary Fuel Tank.......................................
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)
Top Cowl, Oil Access Door…………………..
CHECK OIL QUANTITY
Propeller…………………………………….....
C
HECK LEADING EDGE FOR
DAMAGE. CHECK SPINNER FOR
SECURITY
Air Inlets………………………………………..
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS
AND COMPONENTS.
PAGE 7
ON, THEN OFF (LISTEN TO VERIFY
3RD 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.
CHECK HINGES & CONTROL
CHECK HINGES & CONTROL
CHECK FOR WRINKLES AS INDIC
A-
DAMAGE
VISUALLY CHECK QUANTITY
CHECK FOR FREEDOM OF
VISUALLY CHECK QUANTITY
CHECK TIRE INFLATION AND BRAKE
DRAIN GASCOLATOR (1)
HECK LEADING EDGE FOR
DAMAGE. CHECK SPINNER FOR
CHECK FOR FOREIGN OBJECTS,
INSPECT VISIBLE CONNECTIONS

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III -
NORMAL PROCEDURES
3.1 PREFLIGHT INSPECTION:
18.
Nose Gear......................................................
19.
Right Landing Gear……………………………
20.
Right Wing & Controls………………………..
21.
Wing Main & Aux Fuel Tank Drain………….
22.
Right Fuselage, Side & Top
23.
Right Side Static Port…………………………
24.
Right Stabilizer………………………………..
25.
Right Elevator………………………………....
26.
Rudder………………………………………....
27. Tail Skid
……………………………………..
28. Left
Elevator……………………………………
29.
Left Stabilizer………………………………….
30. L
eft Fuselage, Side, & Top
31. 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. Prime
………….………………………………
FAA APPROVED
DATE:
SECTION III -
NORMAL PROCEDURES
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
NORMAL PROCEDURES
(Cont'd)
Nose Gear......................................................
CHECK TIRE INFLATION & STRUT E
TENSION
, CLEAN STRUT
Right Landing Gear……………………………
CHECK TIRE
INFLATION & BRAKE LINE
SECURITY
Right Wing & Controls………………………..
INSPECT SAME AS
LEFT WING
Wing Main & Aux Fuel Tank Drain………….
. DRAIN (2)
Right Fuselage, Side & Top
& Bottom……….
INSPECT FOR WRINKLES AS INDIC
TION OF INTERNAL DAMAGE
Right Side Static Port…………………………
CLEAR
Right Stabilizer………………………………..
CHECK
ATTACHMENT POINTS &
FLYING WIRES
Right Elevator………………………………....
CHECK HINGE POINTS
Rudder………………………………………....
CHECK HINGE POINTS, CONTROL
ATTACHMENT & NAV LIGHT
……………………………………..
.... CHECK FOR DAMAGE,
REMOVE
TIEDOWN
Elevator……………………………………
CHECK TAB CONTROLS & ALL HINGE
POINTS
Left Stabilizer………………………………….
CHECK ATTACHMENT POINTS &
STRUT
eft Fuselage, Side, & Top
………….............
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
Port…………………………..
CLEAR
OPERATING CHECK LISTS:
Seat Belts & Shoulder Harnesses…………..
FASTENED
Flaps………………………………………..….
RETRACTED
Circuit Breakers…………………………….....
CHECK
Brakes…………………….….
ON
Fuel Selector Valve……………………………
ON FULLEST TANK, OR BOTH IF SAME
QUANTITY
Throttle…………………………………………
OPEN 1/4 INCH
Propeller Control...........................................
FULL INCREASE RPM
Control………………………………..
FULL
RICH (SEE NOTE NEXT PAGE
FOR HOT START)
Collision Light……………………………
ON
BAT and ALT Switch………………………...
ON
………….………………………………
. AS REQUIRED
USING BOOST PUMP
PAGE 8
NORMAL PROCEDURES
CHECK TIRE INFLATION & STRUT E
X-
, CLEAN STRUT
INFLATION & BRAKE LINE
LEFT WING
INSPECT FOR WRINKLES AS INDIC
A-
TION OF INTERNAL DAMAGE
ATTACHMENT POINTS &
CHECK HINGE POINTS, CONTROL
ATTACHMENT & NAV LIGHT
REMOVE
CHECK TAB CONTROLS & ALL HINGE
CHECK ATTACHMENT POINTS &
CHECK FOR WRINKLES AS
INDICATION OF INTERNAL DAMAGE
ON FULLEST TANK, OR BOTH IF SAME
RICH (SEE NOTE NEXT PAGE
USING BOOST PUMP

MAULE AEROSPACE TECHNOLOGY, INC.
3.2 OPERATING CHECK LISTS:
(Cont'd)
NOTE:
NOTE:
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A START A
TEMPT. 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.
FOR A COLD ENGINE (FIRST SATRT OF THE DAY), PLACE MIXTURE TO FULL RICH.
THROTTLE ¼
" OPEN. PRIME WITH BOOST PUMP FOR 3 TO 5 SECONDS. IF ENGINE
DOES NOT START, PR
NOTED BY FUEL COMING FROM DRAIN I
////////////////////////
////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.
12.
After Starting…………………………………..
////////////////////////
////CAUTION////
////////////////////////
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS, SHUT
DOWN ENGINE.
13.
Alternator………………………………………
14.
Radios & other electrical switches…………..
15.
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 IS UNACCEPTABLE.
5.
Propeller Control………………………………
FAA APPROVED
DATE:
SECTION III -
NORMAL PROCEDURES
9.
Mixture Control………….……………….......
10.
Starter Switch..............................................
11. Mixture
Control............................................
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
(Cont'd)
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A START A
TEMPT. TO CLEAR A FLOODED ENGINE, PULL MIXTURE FULL LEAN AND OPEN
CRANK WITH STARTER. WHEN ENGINE STARTS, PULL THROTTLE TO
IDLE AND EASE MIXTURE TO FULL RICH.
FOR A COLD ENGINE (FIRST SATRT OF THE DAY), PLACE MIXTURE TO FULL RICH.
" OPEN. PRIME WITH BOOST PUMP FOR 3 TO 5 SECONDS. IF ENGINE
DOES NOT START, PR
IME FOR ANOTHER 3 TO 5 SECONDS. OVERPRIME CAN BE
NOTED BY FUEL COMING FROM DRAIN I
N
CENTER OF BOTTOM COWL.
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO FULL
ENGINE FAILS TO START AFTER SEVERAL REVOLUTIONS, AND FIRE
CONTINUES, SECURE IGNITION, BAT. AND ALT. SWITCHES, TURN FUEL VALVE
OFF AND EXIT AIRCRAFT.
After Starting…………………………………..
CHECK OIL PRESSURE
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS, SHUT
Alternator………………………………………
CHECK CHARGING
Radios & 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,
CHECK
ING 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
PAGE 9
NORMAL PROCEDURES
Mixture Control………….……………….......
FULL LEAN
Starter Switch..............................................
TWIST FULL RIGHT TO ENGAGE
Control............................................
FULL RICH WHEN ENGINE STARTS TO
FIRE
FOR A HOT START, DO NOT PRIME. A HOT ENGINE MAY FLOOD ON A START A
T-
TEMPT. TO CLEAR A FLOODED ENGINE, PULL MIXTURE FULL LEAN AND OPEN
CRANK WITH STARTER. WHEN ENGINE STARTS, PULL THROTTLE TO
FOR A COLD ENGINE (FIRST SATRT OF THE DAY), PLACE MIXTURE TO FULL RICH.
" OPEN. PRIME WITH BOOST PUMP FOR 3 TO 5 SECONDS. IF ENGINE
IME FOR ANOTHER 3 TO 5 SECONDS. OVERPRIME CAN BE
CENTER OF BOTTOM COWL.
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO FULL
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
CHECK, IN GREEN ARCS
INCREASE TO 2000 RPM
SWITCH TO RIGHT, LEFT, BOTH,
ING RPM DROPS
A RPM DROP OF MORE THAN 175 RPM OR A DIFFERENCE BETWEEN LEFT AND
RETARD SLOWLY UNTIL MAXIMUM OF
500 RPM DROP IS NOTED.
RETURN TO FULL RPM. REPEAT. SET
FULL INCREASE RPM
.
TWIST FULL RIGHT TO ENGAGE
FULL RICH WHEN ENGINE STARTS TO

MAULE AEROSPACE TECHNOLOGY, INC.
3.2
OPERATING CHECK LISTS:
6. Alternate Air Control....
………………………..
7.
Alternate Air Control......................................
8.
Vacuum Gauge………………………………..
9.
Alternator…………………………………….
10.
Throttle...........................................................
11.
Parking Brake................................................
D. BEFORE TAKEOFF:
1. Fuel
Selector…………………………………..
2.
Flaps……………………………………………
3.
Trim Controls……………………………….....
4.
Flight Controls…………………………………
5. Mixture
Control…………………………….….
6. Propeller Control.......
………......…….………
7.
Alternate 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. Alternate
Air Control………………………..
FAA APPROVED:
DATE:
SECTION III -
NORMAL PROCEDURES
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
OPERATING CHECK LISTS:
(Cont'd)
………………………..
TURN LEFT TO UNLOCK AND PULL
NORMAL RPM DROP WITH ALTERNATE
AIR IS APPROXIMATELY 50 RPM.
Alternate Air Control......................................
PUSH IN AND TURN RIGHT TO LOCK
Vacuum Gauge………………………………..
CHECK IN GREEN
Alternator…………………………………….
…
CHARGING: LIGHT OUT ABOVE 900 RPM
Throttle...........................................................
RETARD TO IDLE
Parking Brake................................................
OFF
Selector…………………………………..
ON FULLEST TANK OR BOTH
Flaps……………………………………………
AS DESIRED FOR T.O. (MAX. 24
Trim Controls……………………………….....
SET FOR TAKEOFF
Flight Controls…………………………………
CHECK FOR FREEDOM
&
TRAVEL
Control…………………………….….
FULL RICH
………......…….………
. FULL INCREASE RPM
Alternate 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.
Parking Brake…………………………….……
OFF
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
Air Control………………………..
... IN AND LOCKED
PAGE 10
NORMAL PROCEDURES
TURN LEFT TO UNLOCK AND PULL
.
NORMAL RPM DROP WITH ALTERNATE
AIR IS APPROXIMATELY 50 RPM.
PUSH IN AND TURN RIGHT TO LOCK
CHARGING: LIGHT OUT ABOVE 900 RPM
ON FULLEST TANK OR BOTH
AS DESIRED FOR T.O. (MAX. 24
°
)
&
PROPER
RECHECK IN NORMAL RANGE
BELTS & HARNESSES SECURED
.
BRIEFED ON OPENING DOORS.
TANK OR BOTH

MAULE AEROSPACE TECHNOLOGY, INC.
3.2
OPERATING CHECK LISTS:
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................................................
3.3
NORMAL FLIGHT OPERATIONS:
A.
NOTE: FLAP SETTINGS:
The following Flap Settings are available:
Flap Configuration
Flap Handle Position
Cruise
Handle Full Down
Flaps Up
First Notch
Takeoff
Second Notch
Landing
Third Notch
B.
RECOMMENDED FLAP SETTINGS:
Flap settings are given in number of notches above the fully
full down (Normal -7°).
NOTE:
The airplane meets CAR 3 takeoff climb requirements at 78K (90 mph) IAS with the
selected in any of the following three positions: (a) Fully Retracted, Handle full
Notch (0°
), and (c) Second Notch (24
Second Notch (24°)
Normal Climb -
First Notch (0
Best Angle of Climb -
Second Notch (24
Cruise - Fully retracted (-7°
/no notches or 0
Landing -
Normally Third Notch (40
FAA APPROVED: 4/17/98
DATE:
SECTION III -
NORMAL PROCEDURES
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
OPERATING CHECK LISTS:
(Cont'd)
....................................
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
Switch.........................................
OFF
Parking Brake................................................
OFF (AS DESIRED)
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°
RECOMMENDED FLAP SETTINGS:
Flap settings are given in number of notches above the fully
retracted position, which is handle
The airplane meets CAR 3 takeoff climb requirements at 78K (90 mph) IAS with the
selected in any of the following three positions: (a) Fully Retracted, Handle full
), and (c) Second Notch (24
°).
First Notch (0
°)
Second Notch (24
°)
/no notches or 0
°/1
ST
notch)
Normally Third Notch (40
°/full flaps) - other positions optional
PAGE 11
NORMAL PROCEDURES
1000 RPM
retracted position, which is handle
The airplane meets CAR 3 takeoff climb requirements at 78K (90 mph) IAS with the
flaps
selected in any of the following three positions: (a) Fully Retracted, Handle full
down (-7°). (b) First

MAULE AEROSPACE TECHNOLOGY, INC.
3.3
NORMAL FLIGHT OPERATIONS:
C. CLIMBING:
Best Rate of Climb -
78K (90 mph) IAS, flaps @ First Notch (0
Best Angle of Climb –
65K (75 mph) IAS with flaps set @ Second Notch (24
////////////////////////
////CAUTION////
////////////////////////
FOR TAKEOFF OR LANDING UNDER GUSTY CROSSWIND
CO
NDITIONS 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.
D. RUDDER TRIM:
NOTE: To assure full effectiveness of the Right Rudder Trim:
Unlock "T" handle (½
turn left), depress right rudder
dle ½ turn right before releasing right rudder pressure. If too much trim, move handle in until trim
is correct and then lock.
E. STALLS:
Stalls are preceded by mild buffet that can be felt through the ru
light on the instrument panel will illuminate at 4 to 9K (5 to 10 mph) above the stall speed. Loss of
altitude prior to recovery from a stall may be as much as 300 feet.
////////////////////////
////CAUTION////
////////////////////////
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
F.
CROSSWIND LANDINGS & TAKEOFFS:
Maximum demons
trated cro
mited to 0°
(fully retracted) with such crosswind
strated for certification of the airplane and is not considered limiting with flaps at 0
FAA APPROVED: 4/17/98
Rev. A dated: 10/26/98
Rev. E dated:
G.
FUEL SYSTEM MANAGEMENT:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
NORMAL FLIGHT OPERATIONS:
(Cont'd.)
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
NDITIONS 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
NOTE: To assure full effectiveness of the Right Rudder Trim:
turn left), depress right rudder
as you pull "T" handle full out. Lock "T" ha
dle ½ turn right before releasing right rudder pressure. If too much trim, move handle in until trim
Stalls are preceded by mild buffet that can be felt through the ru
dder 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 recovery from a stall may be as much as 300 feet.
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
CROSSWIND LANDINGS & TAKEOFFS:
trated cro
sswind component is 12K (14
mph) and flap extension should be l
(fully retracted) with such crosswind
or higher. 12K (14
mph) is the maximum demo
strated for certification of the airplane and is not considered limiting with flaps at 0
PAGE 12
FUEL SYSTEM MANAGEMENT:
65K (75 mph) 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
as you pull "T" handle full out. Lock "T" ha
n-
dle ½ turn right before releasing right rudder pressure. If too much trim, move handle in until trim
dder 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
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
mph) and flap extension should be l
i-
mph) is the maximum demo
n-
strated for certification of the airplane and is not considered limiting with flaps at 0
°.

MAULE AEROSPACE TECHNOLOGY, INC.
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 co
trolled 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 au
iliary tank will force excess fuel overboard, it is recommen
un
til 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
quarter. 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.
3.4 DOOR-
OFF OPERATION:
This aircraft may be operated with either one (not both) of the front doors removed,
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 -
109K (125 mph)
2. Maximum bank angle -
3. Maximum yaw angle -
10
4. No Smoking permitted
5.
Limit flight to VFR conditions
3.5 NOISE LEVEL:
The noise levels obtained during cer
with MT propeller 4 blade
with Hartzell (78") 2blade
with McCauley (78") 2 blade
with Hartzell 3 blade
with McCauley (78") 3 blade
The noise level obtained during certification per
with MT propeller 4 blade
with Hartzell (78") 2blade
with McCauley (78") 2 blade
with Hartzell 3 blade
with McCauley (78") 3 blade
with Hartzell (81") 2 blade
No determination has been made by the Federal Aviation Administration that the noise level of this ai
plane 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 VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
RECOMMENDED THAT IT BE TURNED OFF
FORT BE NOTICED.
FAA APPROVED: 4/17/98
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
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 co
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 au
iliary tank will force excess fuel overboard, it is recommen
ded that the transfer pumps not be activated
til 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
quarter. 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.
OFF OPERATION:
This aircraft may be operated with either one (not both) of the front doors removed,
doors are installed, with the rear passenger door or rear passenger and baggage doors off. When
doing so, observe the following additional limitations:
109K (125 mph)
30°
10
°
Limit flight to VFR conditions
The noise levels obtained during cer
tification per FAR 36, Appendix G was:
74.8 dBA
78.0 dBA
78.8 dBA (79.5"): 80.1 dBA
78.0 dBA
78.0 dBA (80"): 78.2 dBA
The noise level obtained during certification per
ICAO Annex 16 Chapter 10 was:
77.9 dBA
79.7 dBA
80.2 dBA (79.5"): 81.5 dBA
79.7 dBA
79.7 dBA (80"): 79.9 dBA
82.9 dBA
No determination has been made by the Federal Aviation Administration that the noise level of this ai
plane 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
SHOULD PILOT DISCO
FORT BE NOTICED.
PAGE 13
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 co
n-
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 au
x-
ded that the transfer pumps not be activated
til 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
quarter. 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.
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 doors off. When
ICAO Annex 16 Chapter 10 was:
No determination has been made by the Federal Aviation Administration that the noise level of this ai
r-
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
WHEN FLYING IN VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
SHOULD PILOT DISCO
M-

MAULE AEROSPACE TECHNOLOGY, INC.
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
1.
Maintain aircraft control
2.
Analyze the situation and take proper action
3.
Land as soon as conditions permit
4.2
ENGINE EMERGENCY SHUT DOWN:
1. Mixture -
Full lean
2. Fuel Selector -
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
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
4.7
ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING:
1.
Glide
-
Establish 69K (80
2.
Switch Fuel Selector to fullest tank
FAA APPROVED: 4/17/98
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
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. Each aircrew member should remember them.
Maintain aircraft control
Analyze the situation and take proper action
Land as soon as conditions permit
ENGINE EMERGENCY SHUT DOWN:
Full lean
Off
Ignition Switch
- Off
ENGINE FIRE DURING STARTING:
Full lean
Open
Continue 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
Master Switch
- Off
EMERGENCY EXIT ON THE GROUND:
Accomplish ENGINE EMERGENCY SHUT DOWN
Switch
- Off
Leave aircraft by either door or kick out side window panels or baggage door.
(BEFORE LIFT
-OFF)
Closed
As Required
ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING:
Establish 69K (80
mph) IAS with flaps at 0
°
Switch Fuel Selector to fullest tank
Page 14
To assist the pilot when an emergency occurs, three basic rules are established which apply
airborne. Each aircrew member should remember them.
Continue cranking for several revolutions. Attempt to draw fire inside 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.
SECTION IV - EMERGENCY
PROCEDURES
4.7
ENGINE FAILURE AFTER TAKEOFF OR FORCED
3.
Electric Fuel Pump
4.
Mixture Rich, Ignition On
5.
Alternate Air Control
6.
If engine does not restart, accomplish EMERGENCY SHUT DOWN
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 69K (80
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 69K (80
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.
If engine does not start, try flooded engine clearing procedure with throttle wide
open and mixture full lean.
6. If no start, make
forced landing
NOTE: PROP
ELLER WILL NOT WINDMILL BELOW 61K (7
NOTE:
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.
4.11 ELECTRICAL FIRE:
1. Master Switch -
Off
4.12
ENGINE FIRE DURING FLIGHT:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2.
Make forced landing
FAA APPROVED: 4/17/98
Rev. D dated:
SECTION IV -
EMERGENCY
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-260
PROCEDURES
ENGINE FAILURE AFTER TAKEOFF OR FORCED
LANDING: (Cont'd)
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 69K (80
mph) IAS if unable to maintain level flight
Both
Electric Fuel Pump
- On
Both
On
COMPLETE POWER FAILURE DURING FLIGHT:
Establish 69K (80
mph) IAS
Attempt engine airstart if warranted
Both
Electric Fuel Pump
- On
Both (start if propeller is not turning)
If engine does not start, try flooded engine clearing procedure with throttle wide
open and mixture full lean.
forced landing
ELLER WILL NOT WINDMILL BELOW 61K (7
0 MPH).
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.
Off
ENGINE FIRE DURING FLIGHT:
Accomplish ENGINE EMERGENCY SHUT DOWN
Make forced landing
PAGE 15
EMERGENCY
PROCEDURES
If engine does not restart, accomplish EMERGENCY SHUT DOWN
mph) IAS if unable to maintain level flight
If engine does not start, try flooded engine clearing procedure with throttle wide
AT ALTITUDES OVER 8000 FEET, A LEANER MIXTURE MAY BE REQUIRED.