MAULE MT-7-235 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
[phone]
•
FAA APPROVED
FOR
MAULE
MT-7-235
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
•
Fax: [phone] or [phone] •
www.mauleairinc.co
THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.
FAA APPROVED:________________________________
Aircraft Certification Office
www.mauleairinc.co

MAULE AEROSPACE TECHNOLOGY, INC.
REV. TO
PAGES
A 4
Propeller mod. no. B2D37C224
to B2D37C224
B 4
Added Lycoming IO
C 2
5
6
10
20
Deleted Fuel Quantity in Paragraph 1.4 and referred to
Fuel Supply Table. Added Fuel Supply Table.
Relocated the Flap Control Handle
Rear Cabin Cargo Limitations Placard from page 6.
Deleted Fuel Capacity numbers from Fuel Transfer
Pump Switch Placard and added note for Tank Config
ration.
Added "Parking Brake...OFF" to 3.2.D. BEFORE
TAKEOFF.
Added unusable fuel weight
configurations.
D 3, 5,
12-17
Changed primary airspeed units to knots.
E iiii
3
5
6
25
Changed page number from 26 to 25 in TOC.
Moved note from Sec. 2.3 to Sec. 2.1
Removed note from Sec. 2.3.
Added JPI EDM
Changed page number from 26 to 25.
ment to Airplane Inspection Period.
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
LOG OF REVISIONS
Page i
DESCRIPTION
APPROVAL AND DATE
Propeller mod. no. B2D37C224
-C/G-90RA-9 corrected
to B2D37C224
-B/G-90RA-9
_________________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
istration, Atlanta, GA
Date:
_____________________
Added Lycoming IO
-540-W1A5 engine.
_________________________
Manager, Aircraft
Office, Federal Aviation Admi
istration, Atlanta, GA
Date:_____________________
Deleted Fuel Quantity in Paragraph 1.4 and referred to
Fuel Supply Table. Added Fuel Supply Table.
Relocated the Flap Control Handle
Placard and the
Rear Cabin Cargo Limitations Placard from page 6.
Deleted Fuel Capacity numbers from Fuel Transfer
Pump Switch Placard and added note for Tank Config
u-
Added "Parking Brake...OFF" to 3.2.D. BEFORE
Added unusable fuel weight
for new tank
configurations.
______
__________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
istration, Atlanta, GA
Date:_____________________
Changed primary airspeed units to knots.
_________________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
istration, Atlanta, GA
Date:_____________________
Changed page number from 26 to 25 in TOC.
Moved note from Sec. 2.3 to Sec. 2.1
.
Removed note from Sec. 2.3.
Added JPI EDM
-900/930. Corrected cargo limitations.
Changed page number from 26 to 25.
Added require-
ment to Airplane Inspection Period.
_________________________
Manager, Southeast Flight
Test Section, AIR
Atlanta,
GA
Date:_____________________
Page i
APPROVAL AND DATE
_________________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
n-
istration, Atlanta, GA
_____________________
_________________________
Manager, Aircraft
Certification
Office, Federal Aviation Admi
n-
istration, Atlanta, GA
Date:_____________________
__________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
n-
istration, Atlanta, GA
Date:_____________________
_________________________
Manager, Aircraft Certification
Office, Federal Aviation Admi
n-
istration, Atlanta, GA
Date:_____________________
_________________________
Manager, Southeast Flight
Test Section, AIR
-712, FAA
GA
Date:_____________________

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
Page ii
LOG OF SUPPLEMENTS
SUP.
NO.
NO. OF
PAGES
DESCRIPTION
APPROVAL
DATE
1 2 Operation of aircraft with Center Seat moved 3” aft. 12/17/92
2 21
Inst. of Wipline Model 3000 Amphibious Floats - Maule Drawing 9188A. (05/17/99) Rev. A 08/19/02
3 8
Inst. of Aqua Model 2400 Floats - Maule Drawing 9135A, Rev. E or later revision. (11/19/99) Rev. A 08/19/02
4 2
Inst. of Century Flight Systems Century IIB Autopilot - Maule Installation Manual AK513. 03/24/95
5 6 English to Metric Conversion Charts - required in aircraft when registered in Canada. 09/03/99
6 9 Inst. of S-TEC System 50 Two Axis Autopilot ST-418-50 (14v) - 9193A, Rev. Bor later. 01/05/00
7 9 Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - 9197A, Rev. Aor later.
(Land) 01/21/00
8 9 Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - 9197A, Rev. Aor later
(Sea) 01/21/00
9 9 Inst. of S-TEC System 50 Two Axis Autopilot ST-609-50 (28v) - 9200A, Rev. Aor later. 02/14/00
10 6 Inst. of S-TEC System 55 Two Axis Autopilot ST-573 (14v) - 9195A, Rev. Aor later
. (Land) 04/04/00
11 6 Inst. of S-TEC System 55 Two Axis Autopilot ST-573 (14v) - 9195A, Rev. Aor later. (Sea) 04/04/00
12 9 Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - 9197A, Rev. Bor later.
(Land) 03/20/00
13 9 Inst. of S-TEC System 20 Single Axis Autopilot ST-810-20 (14v) - 9197A, Rev. Bor later
. (Sea) 03/20/00
14 8 Inst. of S-TEC System 20 Single Axis Autopilot ST-820-20 (28v) - 9201A, Rev. Aor later. 03/20/00
15 7 Inst. of S-TEC System 40 Single Axis Autopilot ST-418-40 (14v) - 9193A, Rev. Cor later. 10/29/01
16 7 Inst. of S-TEC System 40 Single Axis Autopilot ST-609-40 (28v) - 9200A, Rev. Bor later. 10/29/01
18 4 Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (28v)- Maule Drawing 9211A.
(Land) 06/25/01
19 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (28v) - Maule Drawing 9211A.
(Land) 06/25/01
20 2 Installation of Hartzell HC-C3YR-1RF/F-7693(F)-( ) Propeller - Maule Drawing 5279F. Rev. A 01/28/04
- 5 Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (28v) - Maule Drawing 9211A.
(Sea) 06/25/01
- 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (28v) - Maule Drawing 9211A.
(Sea) 06/25/01
- 3 Installation of GARMIN GNS-430 (GPS/NAV/COMM) System - Maule Drawing 7205A. 01/03/01
- 3 Installation of GARMIN GNC-300XL (GPS/COMM) System - Maule Drawing 7207A. 01/03/01
- 3 Installation 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
21 9 Inst. of S-TEC System 60 Two Axis Autopilot ST-495 (28v) - 9235A, Rev. A. 08/29/03
- 3 Operation of aircraft when
Micro AeroDynamics
Vortex Generator System
is installed in accordance
with Maule Drawing 9177A. 12/16/05
- 2 Installation of McCauley B2D37C224/90RA-4 (86") Prop with Lyc. O-540-J/IO-540-W Engine. 04/03/12

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
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……………………………..…………. 14
3.5 Noise Level………………………………………..……….. 14
3.6 Anti-Collision Light………………………………..……….. 14
SECTION IV EMERGENCY PROCEDURES
4.1 Emergency Basic Rules……………………………….….
15
4.2 Engine Emergency Shut Down……………………….…. 15
4.3 Engine Fire During Starting…………………………….... 15
4.4 Engine Fire After Starting…………………………….…... 15
4.5 Emergency Exit on the Ground………………………….. 15
4.6 Takeoff Abort………………………………………………. 15
4.7 Engine Failure After T.O. or Forced Landing….……….. 16
4.8 Partial Power Failure During Flight of After T.0..………. 16
4.9 Complete Power Failure During Flight………….………. 16
4.10 Engine Airstart……………………………………..………. 16
4.11 Electrical Fire……………………………………….……… 16
4.12 Engine Fire During Flight………………………….……… 16
4.13 Smoke and Fume Elimination…………………….……… 17
4.14 Structural Damage………………………………….…….. 17
4.15 Recovery From Inadvertent Spins………………….…… 17
4.16 Alternator Failure…………………………………….……. 17

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION V
WEIGHT AND BALANCE AND EQUIPMENT LIST
5.1
Weight and Balance Data……………………………
Required Equipment List ………Provided for each
SECTION VI
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
6.1
Introduction…………………………………………………
6.2
Airplane Inspection Period……………………………
6.3
Preventive Maintenance that may be Accomplished by
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-7-235
TABLE OF CONTENTS
WEIGHT AND BALANCE AND EQUIPMENT LIST
Weight and Balance Data……………………………
.
…..
Required Equipment List ………Provided for each
Airplane
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
Introduction…………………………………………………
Airplane Inspection Period……………………………
.
….
Preventive Maintenance that may be Accomplished by
a Certified Pilot…………………………………………..…
Alterations or Repairs to Airplane………………………
MANUFACTURER'S DATA
Optional Equipment List………..Provided for each Airplane
Page iiii
WEIGHT AND BALANCE AND EQUIPMENT LIST
…..
18
Airplane
AIRCRAFT SERVICING, HANDLING AND MAINTENANCE
Introduction…………………………………………………
25
….
25
Preventive Maintenance that may be Accomplished by
a Certified Pilot…………………………………………..…
25
Alterations or Repairs to Airplane………………………
.. 25
Optional Equipment List………..Provided for each Airplane

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION I - GENERAL
PAGE 1

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION I
GENERAL : NORMAL CATEGORY OPERATION
1.1 MAXIMUM WEIGHT: 2500 Pounds
1.2 CENTER OF GRAVITY LIMITS: +15.0 to +20.5 @ 2500 lbs.
+12.0 to +20.5 @ 1800 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
Fuel Capacity - See Instrument Panel Placard for Tank configuration installed
in this aircraft
Tank
Config. Tank Location Usable Fuel (Gal) Unusable Fuel (Gal)
A Main
Aux. 20.0 15.0 1.5 0.0
B Main
Aux. 20.0 21.0 1.5 0.0
C Main
Aux. 21.5 15.0 2.3 0.0
D Main
Aux. 21.5 21.0 2.3 0.0
////////////////////////
////CAUTION////
////////////////////////
FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY CAN-
NOT BE USED SAFELY IN FLIGHT.
FAA APPROVED: 3/20/92
Rev. C dated: 10/28/94
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
) -
1
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 large or abru
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
speed indicator.
FAA APPROVED: 3/20/92
Rev. D dated:
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
: All airspeeds are Indicated Airspeeds (IAS).
AIRSPEED INDICATOR MARKINGS:
1
58K (182 mph)
Yellow Arc, Caution Range
- 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 abru
pt.
Normal Operating Range
, 54 - 128K (62 - 147
mph): Extends
from flaps
up, power off stall speed at 25
00 lbs. (V
cruise speed (V
C
).
Flap Operating Range
, 43 - 83K (50 - 95
mph): Extends from
full flap, pow
er off minimum stall speed at 25
00 lbs. (V
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
PAGE 3
mph): Maximum safe
mph): Operation in this
speed range should be conducted only in smooth air and co
n-
mph): Extends
00 lbs. (V
S1
) to design
mph): Extends from
00 lbs. (V
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 air-

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION II - LIMITATIONS
2.2 POWER PLANT LIMITS:
Engine: Lycoming IO-540-W1A5D or IO-540-W1A5
Engine Limits: 235 hp @ 2400 rpm, Full Throttle Continuous
Propeller: Hartzell: Constant Speed HC-C2YR-1BF/F8468A-6R (78") or
-3R (81")
McCauley: Constant Speed B3D32C414-C/G-82NDA-4 (78") or
-2 (80") or B2D37C224-B/G-90RA-9 (81")
Fuel: 100/100LL Minimum Grade Aviation Gasoline
Engine Instrument Markings:
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 inches of Mercury
Fuel Flow Red Radial - Maximum, 8.9 psi or 26.9 gph
Tachometer: Green Arc - Normal Operating Range,
2050-2400 RPM
Red Radial - Maximum RPM, 2400 RPM
FAA APPROVED: 3/20/92
Rev. A dated: 12/18/92
Rev. B dated: 12/18/92 PAGE 4

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II - LIMITATIONS
2.2 FLIGHT LOAD FACTORS:
////////////////////////
////CAUTION////
////////////////////////
DO NOT EXCEED 23 INCHES M.P.
WITH THE HARTZELL
MITATION WHICH APPLIES TO THIS MODEL PROPELLER.
2.3 FLIGHT LOAD FACTORS:
2.4 PLACARDS:
The following placards are in the cockpit in clear view of the pilot:
Located on
flap control handle:
Rev. C dated: 10/28/94
Rev. D dated:
Rev. E dated:
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
NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED.
MANEUVERING SPEED 109K (125 MPH) IAS.
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AI
PLANE FLIGHT MANUAL.
THIS AIRPLANE APPROVED FOR DAY OR
IN ACCORDANCE WITH FAR 91 OR FAR 135.
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE USED SAFELY IN
FLIGHT.
FLAPS / PULL ON / 2
ND
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
Cont'd.
DO NOT EXCEED 23 INCHES M.P.
BELOW 2050 RPM. WHEN EQUIPPED
WITH THE HARTZELL
-
6R (78") PROP. THIS IS A VIBRATORY STRESS L
MITATION WHICH APPLIES TO THIS MODEL PROPELLER.
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:
flap control handle:
PAGE 5
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 AI
PLANE FLIGHT MANUAL.
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 IN
ND
NOTCH / TAKEOFF / 3
RD
NOTCH / LANDING.
BELOW 2050 RPM. WHEN EQUIPPED
6R (78") PROP. THIS IS A VIBRATORY STRESS L
I-
MITATION WHICH APPLIES TO THIS MODEL PROPELLER.
Flaps Fully Retracted: 3.8g Positive to 1.5g Negative
THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE IN
COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FLIGHT M
A-
SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF AI
R-
ICING FLIGHT WHEN EQUIPPED
DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF EMERGENCY.
FUEL REMAINING IN TANK WHEN INDICATOR READS ZERO CANNOT BE USED SAFELY IN

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION II - LIMITATIONS
2.4 PLACARDS: (Cont’d)
At the main fuel tank selector valve on the
FUEL SELECTOR VALVE
OFF
On the instrument panel at the optional auxiliary tank transfer switches:
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:
FUEL CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
USABLE EACH. (TANK CONFIGURATION ____)
*
Instrument Panel Placard will show capacity of the tanks
Page 2 for capacity of available tank configurations.
In rear cabin area:
CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A
MAX. LOAD AREA "B" 175
MAX. LOAD AREA "C"
"CHECK WEIGHT AND
BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMUM REAR SEAT LOADING IS 170 LBS."
FAA APPROVED:
DATE: 3/20/92
Rev. C dated:
Rev. E dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
At the main fuel tank selector valve on the
left kick panel:
FUEL SELECTOR VALVE
LEFT: * GAL. BOTH
RIGHT: * GAL.
On the instrument panel at the optional auxiliary tank transfer switches:
FUEL TRANSFER PUMPS
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
FUEL CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
USABLE EACH. (TANK CONFIGURATION ____)
Instrument Panel Placard will show capacity of the tanks
installed in this aircraft. See Table on
Page 2 for capacity of available tank configurations.
CARGO OR BAGGAGE LIMITATIONS
MAX. LOAD AREA "A
" 100 LBS.
MAX. LOAD AREA "B" 175
LBS.
MAX. LOAD AREA "C"
125 LBS.
BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING
REAR/CARGO/BAGGAGE. MAXIMUM REAR SEAT LOADING IS 170 LBS."
PAGE 6
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 CAPACITY: MAIN TANKS * GAL. USABLE EACH, AUX. TANKS
*GAL.
installed in this aircraft. See Table on
BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION III
NORMAL PROCEDURES:
3.1 PREFLIGHT INSPECTION:
A. INTERIOR:
1. BAT Switch…………………………………..... ON
2.
Fuel Gauges……………………………………
CHECK INDICATIONS
3.
All Electrical Switches…………………………
OFF
4. BAT Switch……………………………………. OFF
5. Flaps…………………………………………… FULL DOWN (3RD NOTCH)
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……………………… DRAIN (2)
2. Left Flap……………………………………….. CHECK HINGES & CONTROL
ATTACHMENTS
3. Aileron…………………………………………. CHECK HINGES & CONTROL
ATTACHMENTS
4. Left Wing Top………………………………… CHECK FOR WRINKLES AS INDICA-
TION OF INTERNAL DAMAGE
5. Left Wing Main & Aux Fuel Tank Drain……. DRAIN (2)
6. Left Wing Tip & Nav Light…………………… CHECK FOR DAMAGE
7. Auxiliary Fuel Tank....................................... VISUALLY CHECK QUANTITY
8. Landing Light………………………………….. CHECK FOR DAMAGE
9.
Left Wing Tiedown…………………………….
REMOVE
10. Pitot Tube……………………………………… REMOVE COVER
11. Stall Warning Switch…………………………. CHECK FOR FREEDOM OF
MOVEMENT
12. Main Fuel Tank…………………………….…. VISUALLY CHECK QUANTITY
13. Left Landing Gear……………………………. CHECK TIRE INFLATION AND BRAKE
LINE SECURITY
14. Bottom left side of Cowl……………………… DRAIN GASCOLATOR (1)
15. Top Cowl, Oil Access Door………………….. CHECK OIL QUANTITY
16. Propeller……………………………………..... CHECK LEADING EDGE FOR
DAMAGE.
17. Air Inlets……………………………………….. CHECK FOR FOREIGN OBJECTS, IN-
SPECT VISIBLE CONNECTIONS AND
COMPONENTS.
FAA APPROVED
DATE: 3/20/92 PAGE 7

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION III - NORMAL PROCEDURES
3.1 PREFLIGHT INSPECTION: (Cont'd)
18. Nose Gear...................................................... CHECK TIRE INFLATION & STRUT EX-
TENSION, CLEAN STRUT
19. Right Landing Gear…………………………… CHECK TIRE
INFLATION & BRAKE LINE
20. Right Wing & Controls……………………….. INSPECT SAME AS LEFT WING
21.Wing Main & Aux Fuel Tank Drain…………. DRAIN (2)
22. Right Fuselage, Side & Top..............………. INSPECT FOR WRINKLES AS INDICA-
TION OF INTERNAL DAMAGE
23. Right Side Static Port………………………… CLEAR
24. Right Stabilizer……………………………….. CHECK ATTACHMENT POINTS &
STRUT
25. Right Elevator……………………………….... CHECK HINGE POINTS
26. Rudder……………………………………….... CHECK HINGE POINTS, CONTROL AT-
TACHMENT & NAV LIGHT
27. Tail Skid……………………………………...... CHECK FOR DAMAGE, REMOVE TIE-
DOWN
28. Left Elevator…………………………………… CHECK TAB CONTROLS & ALL HINGE
POINTS
29. Left Stabilizer…………………………………. CHECK ATTACHMENT POINTS &
STRUT
30. Left Fuselage, Side, & Top…………............. CHECK FOR WRINKLES AS INDICA-
TION OF INTERNAL DAMAGE
31. Left Side Static Port………………………….. CLEAR
3.2 OPERATING CHECK LISTS:
A. BEFORE STARTING:
1. Seat Belts & Shoulder Harnesses………….. FASTENED
2. Flaps………………………………………..…. RETRACTED
3. Circuit Breakers……………………………..... CHECK
B. STARTING:
1. Parking or Toe Brakes…………………….…. ON
2. Fuel Selector Valve……………………………
ON FULLEST TANK, OR BOTH IF SAME
QUANTITY
3. Throttle………………………………………… OPEN 1/4 INCH
4. Propeller Control........................................... FULL INCREASE RPM
5. Mixture Control……………………………….. FULL RICH (SEE NOTE NEXT PAGE
FOR HOT START)
6. Anti-Collision Light…………………………… ON
7. BAT and ALT Switch………………………... ON
8. Prime………….………………………………. AS REQUIRED USING BOOST PUMP
(SEE NOTE NEXT PAGE)
FAA APPROVED
DATE: 3/20/92 PAGE 8

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
SECTION III - NORMAL PROCEDURES
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 THROTTLE TO IDLE AND EASE MIXTURE TO FULL RICH. FOR
A COLD ENGINE (FIRST SATRT OF THE DAY), PLACE MIXTURE TO FULL
RICH. THROTTLE 1/4" OPEN. PRIME WITH BOOST PUMP FOR 3 TO 5
SECONDS. IF ENGINE DOES NOT START, PRIME FOR ANOTHER 3 TO 5
SECONDS. OVERPRIME CAN BE NOTED BY FUEL COMING FROM DRAIN IN-
CENTER OF BOTTOM COWL.
////////////////////////
////CAUTION////
////////////////////////
IN EVENT OF ENGINE FIRE, CONTINUE CRANKING. PULL MIXTURE TO
FULL LEAN. IF ENGINE FAILS TO START AFTER SEVERAL REVOLU-
TIONS, AND FIRE CONTINUES, SECURE IGNITION, BAT. AND ALT.
SWITCHES, TURN FUEL VALVE OFF AND EXIT AIRCRAFT.
12. After Starting…………………………………..
CHECK OIL PRESSURE
////////////////////////
////CAUTION////
////////////////////////
IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS,
SHUT DOWN ENGINE.
13. Alternator………………………………………
CHECK CHARGING
14. Radios & other electrical switches………….. AS REQUIRED
15. Parking Brake………………………………… OFF
C. ENGINE CHECK:
1. Parking Brake…………………………………. ON, IF DESIRED
2.
Engine Instruments……………………………
CHECK, IN GREEN ARCS
3. Throttle………………………………………… INCREASE TO 2000 RPM
4. Magnetos……………………………………… SWITCH TO RIGHT, LEFT, BOTH,
CHECKING RPM DROPS
////////////////////////
////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………………………………
RETARD SLOWLY UNTIL MAXIMUM
OF 500 RPM DROP IS NOTED. RE-
TURN TO FULL INCREASE RPM.
REPEAT. SET FULL INCREASE RPM.
FAA APPROVED
DATE: 3/20/92 PAGE 9
9. Mixture Control………….………………....... FULL LEAN
10. Starter Switch.............................................. TWIST FULL RIGHT TO ENGAGE
11. Mixture Control............................................
FULL RICH WHEN ENGINE STARTS TO
FIRE

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III -
NORMAL PROCEDURES
3.2
OPERATING CHECK LISTS:
6.
Alternate Air Control....
NOTE: NORMAL RPM DROP WITH ALTERNATE AIR IS APPOXIMATELY 50 RPM.
7.
Alternate Air Control......................................
8.
Vacuum Gauge………………………………..
9.
Alternator…………………………………….
10.
Throttle...........................................................
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: 3/20/92
Rev. C dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
NORMAL PROCEDURES
OPERATING CHECK LISTS:
(Cont'd)
Alternate Air Control....
………………………..
TURN LEFT TO UNLOCK AND PULL
NOTE: NORMAL RPM DROP WITH ALTERNATE AIR IS APPOXIMATELY 50 RPM.
Alternate Air Control......................................
PUSH IN AND TURN
Vacuum Gauge………………………………..
CHECK IN GREEN
Alternator…………………………………….
…
CHARGING: LIGHT OUT ABOVE 900 RPM
Throttle...........................................................
RETARD TO IDLE
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
Propeller Control.......
………......…….……….
FULL INCREASE RPM
Alternate Air Control......................................
PUSH IN AND LOCK
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
TURN LEFT TO UNLOCK AND PULL
NOTE: NORMAL RPM DROP WITH ALTERNATE AIR IS APPOXIMATELY 50 RPM.
PUSH IN AND TURN
RIGHT TO LOCK
CHECK IN GREEN
CHARGING: LIGHT OUT ABOVE 900 RPM
RETARD TO IDLE
ON FULLEST TANK OR BOTH
AS DESIRED FOR T.O. (MAX. 24
°
)
SET FOR TAKEOFF
CHECK FOR FREEDOM
& PROPER
FULL INCREASE RPM
PUSH IN AND LOCK
RECHECK IN NORMAL RANGE
RECHECK FASTENED
& LATCHED
BELTS & HARNESSES SECURED
.
BRIEFED ON OPENING DOORS.
TANK OR BOTH
FULL INCREASE RPM

MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
PAGE 10
SECTION III - NORMAL PROCEDURES
3.2 OPERATING CHECK LISTS: (Cont'd)
F. ENGINE SHUT DOWN:
1 Parking Brakes.............................................. ON, IF DESIRED
2. Radios……………………………………..…… OFF
3. All other electrical switches………………..... AS DESIRED
4. Flaps…………………………………………… AS DESIRED
5. Magneto Grounding Check........................... PERFORM BELOW 1000 RPM
6. Mixture Control.............................................. FULL LEAN
7. Magneto Switch............................................. OFF
8. Anti-Collision Light......................................... OFF
9. BAT & ALT Switch......................................... OFF
FAA APPROVED:
DATE: 3/20/92 PAGE 11

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III -
NORMAL PROCEDURES
3.3
NORMAL FLIGHT OPERATIONS:
A. NOTE: FLAP
SETTINGS:
The following Flap Settings are available:
Flap Configuration
Cruise
Flaps Up
Takeoff
Landing
B.
RECOMMENDED FLAP SETTINGS:
Flap settings are given in number of notches above the fully retracted position, which
is handle full down (Normal
NOTE:
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 Notch (0
Second Notch (24°)
Normal Climb -
First Notch (0
Best Angle of Climb
-
Cruise -
Fully retracted (
Landing -
Normally Third Notch (40
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: 3/20/92
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
NORMAL PROCEDURES
NORMAL FLIGHT OPERATIONS:
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 full down (Normal
-7°).
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
). (b) First Notch (0
°), and (c) Second Notch (24°).
First Notch (0
°)
-
Second Notch (24°)
Fully retracted (
-7°/no notches or 0°/first notch)
Normally Third Notch (40
°/full flaps) -
other positions optional
78K (90 mph) IAS, flaps @ First Notch (0°)
– 65K (75 mph)
IAS with flaps set @ Second Notch (24
FOR TAKEOFF OR LANDING UNDER GUSTY CROSSWIND
CONDITIONS FLAP SETTING OF 0
°
(one notch) IS RECOMMENDED.
OPTIONAL.
USE CLIMB AIRSPEED BELOW 78K (90 MPH) ONLY AS NECESSARY
AND CHECK CYLINDER HEAD TEMPERATURE FREQUENTLY WHEN
SO.
PAGE 12
Flap settings are given in number of notches above the fully retracted position, which
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
other positions optional
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.
SECTION III -
NORMAL PROCEDURES
D. RUDDER TRIM:
NOTE: To assure full effectiveness of the Right Rudder Trim:
Unlock "T" handle (
½
"T" handle ½ turn right before releasing right rudder
handle in until trim is correct and then lock.
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
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
should be limited to 0
the maximum demonstrated for certification of the airplan
with flaps at 0°.
G.
FUEL SYSTEM MANAGEMENT:
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector valve
on the left kick panel. Auxiliary (outboard) tanks feed their respective main t
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
ommended 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, ho
ever, transfer can be
initiated when the main tank is down to approximately one quarter. Co
firm 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.
FAA APPROVED: 3/20/92
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
NORMAL PROCEDURES
NOTE: To assure full effectiveness of the Right Rudder Trim:
½
turn left), depress right rudder as you pull "T" handle full out. Lock
"T" handle ½ turn right before releasing right rudder
pressure. If too much trim, move
handle in until trim is correct and then lock.
Stalls are preceded by mild buffet that can be felt through the rudder pedals. The red
stall warning light on the instrument panel will illuminate at 4 to 9K (5
the stall speed. Loss of altitude prior to recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
SWITCH IS OFF
CROSSWIND LANDINGS & TAKEOFFS:
trated cro
sswind component is 12K (14
mph) and flap extension
should be limited to 0
°(fully retracted) with such crosswind
or higher. 12K (14
the maximum demonstrated for certification of the airplan
e and is not considered limiting
FUEL SYSTEM MANAGEMENT:
Fuel is fed to the engine from the main (inboard) tanks and is controlled by the selector valve
on the left kick panel. Auxiliary (outboard) tanks feed their respective main t
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 re
ommended 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, ho
initiated when the main tank is down to approximately one quarter. Co
firm fuel transfer by illumination of the transfer pump switch, an increase in the respective main
tank fuel gauge indicator, and a decrease on the respective auxiliary tank indicator.
PAGE 13
turn left), depress right rudder as you pull "T" handle full out. Lock
pressure. If too much trim, move
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 recovery from a stall may be as much as 300
THE STALL WARNING LIGHT IS INOPERATIVE WHEN THE BATTERY
mph) and flap extension
or higher. 12K (14
mph) is
e and is not considered limiting
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 t
anks 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.
tank will force excess fuel overboard, it is re
c-
ommended 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, ho
w-
initiated when the main tank is down to approximately one quarter. Co
n-
firm 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.

MAULE AEROSPACE TECHNOLOGY, INC.
SECTION III -
NORMAL PROCEDURES
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 levels obtained during cer
with Hartzell -6R
(78")
with Hartzell -3R
(81")
with McCauley -4
(78")
with McCauley -2
(80")
with McCauley -9
(81")
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,
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
TIONS.
FAA APPROVED: 3/20/92
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
NORMAL PROCEDURES
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 levels obtained during cer
tification per FAR 36, were:
(78")
2blade 67.6 dBA
(81")
2 blade 71.3 dBA
(78")
3 blade 68.0 dBA
(80")
3 blade 73.6 dBA
(81")
2 blade 73.3 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.
COLLISION LIGHT:
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
WHEN FLYING IN VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
RECOMMENDED THAT
IT BE TURNED OFF UNDER THESE COND
PAGE 14
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
No determination has been made by the Federal Aviation Administration that the noise level
or out of any airport.
COLLISION LIGHT MAY CAUSE ADVERSE EFFECT ON PILOT
WHEN FLYING IN VISIBLE MOISTURE OVERCAST OR HAZE. IT IS
IT BE TURNED OFF UNDER THESE COND
I-

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 airborne. Each aircrew member should remember them.
1.
Maintain aircraft control
2.
Analyze the situation and
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 EMERGENCY SHUT DOWN if fire continues.
4.4
ENGINE FIRE AFTER STARTING:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2.
Master Switch
4.5
EMERGENCY EXIT ON THE GROUND:
1.
Accomplish ENGINE EMERGENCY SHUT DOWN
2.
Master Switch
3.
Leave aircraft by either door or kick out side window panels or baggage door.
4.6 TAKEOFF ABORT:
(BEFORE LIFT
1. Throttle -
Closed
2. Brakes -
As Required
4.7
ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING:
1.
Glide
-
Establish 69K (80
2.
Switch Fuel Selector to fullest tank
FAA APPROVED: 3/20/92
Rev. D dated:
MAULE AEROSPACE TECHNOLOGY, INC.
AIRPLANE FLIGHT MANUAL
MAULE MT-7-235
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
Master 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 15
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.
Continue 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.