MAULE MX-7-180AC Caractéristiques techniques

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 •

Fax:

FAA APPROVED

FOR

AULE MX-7-180AC

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:

(229) 985-2048 or (229) 890-2402 •

www.mauleairinc.com

THIS DOCUMENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES.

__________________________

Manager, Aircraft Certification Office

Federal Aviation Administration

www.mauleairinc.com

MAULE AEROSPACE TECHNOLOGY, INC.

REV.

PAGES

3,5,

11-16

Changed primary airspeed units to knots.

B iiii

Changed page no. in TOC from 34 to 24.

Moved Note from Sec. 2.3 to Sec. 2.1.

Added

JPI EDM

Sec. 2.3.

Corrected Cargo Limitations in areas A, B, C.

Added requirement paragraph to Sec. 6.2.

Changed page no. from 34 to 24.

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

LOG OF REVISIONS

DESCRIPTION

APPROVAL AND DATE

Changed primary airspeed units to knots.

__________________________

Manager, Aircraft Certification Office,

FAA, Atlanta, GA

Date:__________________________

Changed page no. in TOC from 34 to 24.

Moved Note from Sec. 2.3 to Sec. 2.1.

JPI EDM

-900/930. Removed Note from

Corrected Cargo Limitations in areas A, B, C.

Added requirement paragraph to Sec. 6.2.

Changed page no. from 34 to 24.

__________________________

Manager, Southeast Flight Test Se

tion, AIR-

712, FAA

Atlanta, GA

Date:__________________________

Page i

APPROVAL AND DATE

__________________________

Manager, Aircraft Certification Office,

FAA, Atlanta, GA

Date:__________________________

__________________________

Manager, Southeast Flight Test Se

712, FAA

Date:__________________________

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC Page ii

LOG OF SUPPLEMENTS

SUPP.

NO NO. OF

PAGES

DESCRIPTION

APPROVAL

DATE

1 9 Installation of Aqua 2200 Floats - Maule Drawing 9225A. 10/29/02

- 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

2 6 Conversion Charts to facilitate conversions between Metric, Imperial and

U.S. units - required in aircraft when registered in Canada. 06/26/06

- 3 Operation of aircraft when Micro AeroDynamics Vortex Generator System is

installed in accordance with Maule Drawing 9177A.12/16/05

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

Page iii

TABLE OF CONTENTS

ITEM

COVER PAGE

LOG OF REVISIONS……………………………………………………..

LOG OF SUPPLEMENTS……………………………………………..…

TABLE OF CONTENTS………………………………………………..... iii

& iiii

SECTION I

GENERAL

Plan View………………………………………………………….. 1

1.1 Maximum Weight………………………………………….

1.2 Center of Gravity Limits…………………………………. 2

1.3 Maneuvers…………………………………………………

1.4 Fuel Capacity……………………………………………...

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………………………………...

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………………………….

4.6 Takeoff Abort………………………………………………

4.7 Engine Failure After T.O. or Forced Landing…………..

4.8 Partial Power Failure During Flight of After T.0………. 15

4.9 Complete Power Failure During Flight………………….

4.10 Engine Airstart……………………………………………. 15

4.11 Electrical Fire………………………………………………

MAULE AEROSPACE

ITEM

SECTION IV

EMERGENCY PROCEDURES

4.12

Engine Fire During Flight…………………………………

4.13

Smoke and Fume Elimination……………………………

4.14

Structural

4.15

Recovery From Inadvertent Spins………………………

4.16

Alternator Failure………………………………………….

SECTION V

WEIGHT AND BALANCE AND EQUIPMENT LIST

5.1

Weight and Balance Data………………………………..

Required Equipment List ………Provided

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

6.4

Alterations or Repairs to Airplane……………………….

SECTION VII

MANUFACTURER'S DATA

Optional Equipment List

Rev. B dated:

MAULE AEROSPACE

TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

TABLE OF CONTENTS

EMERGENCY PROCEDURES

(Cont’d)

Engine Fire During Flight…………………………………

Smoke and Fume Elimination……………………………

Structural

Damage………………………………………..

Recovery From Inadvertent Spins………………………

Alternator Failure………………………………………….

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

Page iiii

Engine Fire During Flight…………………………………

Smoke and Fume Elimination……………………………

Damage………………………………………..

Recovery From Inadvertent Spins………………………

Alternator Failure………………………………………….

WEIGHT AND BALANCE AND EQUIPMENT LIST

Weight and Balance Data………………………………..

for each Airplane

AIRCRAFT SERVICING, HANDLING AND MAINTENANCE

Introduction…………………………………………………

Airplane Inspection Period……………………………….

Preventive Maintenance that may be Accomplished by

Pilot…………………………………………………………

Alterations or Repairs to Airplane……………………….

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

SECTION I

GENERAL

PAGE 1

MAULE AEROSPACE TECHNOLOGY, INC.

SECTION I

GENERAL: NORMAL CATEGORY OPERATION

1.1 MAXIMUM WEIGHT:

2400 Pounds

1.2

CENTER OF GRAVITY LIMITS:

Straight line variation between points given

Datum: Wing Leading Edge

NOTE:

It is the responsibility of the pilot to assure that the airplane is property loaded. R

fer to the Weight and Balance Data for

and loading graphs.

////////////////////////

////CAUTION////

////////////////////////

CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN

USING THE 5

IS CARRIED IN T

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

this airplane.

////////////////////////

////CAUTION////

////////////////////////

AEROBATICS AND INTENTIONAL SPINS PROHIBITED.

1.4 FUEL CAPACITY:

Usable Fuel: MAIN TANKS

AUXILIARY TANKS

Unusable Fuel: 1.5 Gallons per Main Tank

*Fuel Capacity -

See Instrument Panel Placard for Auxiliary Tank configuration installed in

this aircraft.

////////////////////////

////CAUTION////

////////////////////////

FUEL REMAINING IN TANK WHEN INDICA

CANNOT BE USED SAFELY IN FLIGHT.

FAA APPROVED

DATE:

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

GENERAL: NORMAL CATEGORY OPERATION

2400 Pounds

CENTER OF GRAVITY LIMITS:

+15.9 to +20.5 @ 2400 lbs.

+12.4 to +20.5 @ 1740 lbs. or less

Straight line variation between points given

Datum: Wing Leading Edge

It is the responsibility of the pilot to assure that the airplane is property loaded. R

fer to the Weight and Balance Data for

baggage/cargo loading recommendations

and loading graphs.

CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN

USING THE 5

SEAT, IF INSTALLED, OR WHEN CARGO OR BAGGAGE

IS CARRIED IN T

HE REAR CABIN AREA. ALSO, FLIGHT PLANNING

SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT WITH

FUEL BURN.

Only Normal Category Maneuvers including Stalls, Lazy Eights, Chandelles

and steep turns involving bank angles

not

greater than 60

this airplane.

AEROBATICS AND INTENTIONAL SPINS PROHIBITED.

Usable Fuel: MAIN TANKS

21.5 Gal. Each

AUXILIARY TANKS

15.0 Gal. or 21.0 Gal. each*

Unusable Fuel: 1.5 Gallons per Main Tank

See Instrument Panel Placard for Auxiliary Tank configuration installed in

FUEL REMAINING IN TANK WHEN INDICA

TOR READS EMPTY

CANNOT BE USED SAFELY IN FLIGHT.

PAGE 2

SECTION I

GENERAL

+12.4 to +20.5 @ 1740 lbs. or less

It is the responsibility of the pilot to assure that the airplane is property loaded. R

baggage/cargo loading recommendations

CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN

SEAT, IF INSTALLED, OR WHEN CARGO OR BAGGAGE

HE REAR CABIN AREA. ALSO, FLIGHT PLANNING

SHOULD INCLUDE ALLOWANCE FOR FORWARD C.G. SHIFT WITH

Only Normal Category Maneuvers including Stalls, Lazy Eights, Chandelles

greater than 60

°are approved in

AEROBATICS AND INTENTIONAL SPINS PROHIBITED.

See Instrument Panel Placard for Auxiliary Tank configuration installed in

TOR READS EMPTY

MAULE AEROSPACE TECHNOLOGY, INC.

SECTION II

LIMITATIONS

2.1 AIRSPEED LIMITS

: All airspeeds are Indicated

AIRSPEED INDICATOR MARKINGS:

Red Radial, (V

) -

161K

Yellow Arc, Caution Range

Green Arc, Normal Operating Range

White Arc, Flap Operating Range

EXPLANATION OF AIRSPEED INDICATOR MARKINGS:

Red Radial Line -

Never Exceed Speed (V

speed in smooth air.

Yellow Arc -

Caution Range,

range should be

ments should not be large or abrupt.

Green Arc -

Normal Operating Range,

flaps up, power off stall speed at 2400 lbs. (V

speed (V

White Arc -

Flap

power off minimum stall speed at 2400 lbs. (V

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 ai

speed indicator.

FAA APPROVED: 5/4/00

Rev. A dated:

Rev. B dated:

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

: All airspeeds are Indicated

Airspeeds (IAS).

AIRSPEED INDICATOR MARKINGS:

161K

(185 mph)

Yellow Arc, Caution Range

- 129 - 161K (149 - 185 mph)

Green Arc, Normal Operating Range

- 53 - 129K (61 - 149 mph)

White Arc, Flap Operating Range

- 41 - 85K (47 - 98 mph)

EXPLANATION OF AIRSPEED INDICATOR MARKINGS:

Never Exceed Speed (V

) 161K (185 mph

): Maximum safe ai

speed in smooth air.

Caution Range, 129-161K (149-185 mph

): Operation in this speed

range should be

conducted only in smooth air and control mov

ments should not be large or abrupt.

Normal Operating Range, 53-129K (61-

149 mph

flaps up, power off stall speed at 2400 lbs. (V

speed (V

Flap

Operating Range, 41-85K (47-98 mph

): Extends from full flap,

power off minimum stall speed at 2400 lbs. (V

flaps extended speed (V

DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic

applied (VA) is 109K (125 mph). This airspeed is not marked on the ai

PAGE 3

SECTION II

LIMITATIONS

): Maximum safe ai

): Operation in this speed

conducted only in smooth air and control mov

149 mph

): Extends from

) to design cruise

): Extends from full flap,

) to the Maximum

DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aerodynamic

applied (VA) is 109K (125 mph). This airspeed is not marked on the ai

MAULE AEROSPACE TECHNOLOGY, INC.

2.2 POWER PLANT LIMITS:

Engine:

Engine Limits:

Propeller:

Fuel:

Engine Instrument Markings:

Cylinder Head Temperature:

Oil Temperature:

Oil Pressure:

Fuel Pressure

Tachometer:

FAA APPROVED

DATE:

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

Lycoming O-360-C1F or O-360-C4F

180 hp @ 2700 RPM, Full Throttle Continuous

Sensenich Fixed Pitch 76EM8S5-0-

56 (76”) or

76EM8S8-0-

56 (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

140°F - 245°

Red Radial -

Operating Limit, 245

Green Arc -

Normal Operating Range, 55

to 95 psi

Yellow Arc -

Caution Range, 25 to 55 and

95 to 115 psi

Red Radial -

Minimum Operating Pressure,

25 psi, Maximum Operating

Pressure, 115 psi

Green Arc -

Normal Operating Range, 0.5

to 8 psi

Red Radial -

Minimum, 0.5 psi, Maximum,

8.0 psi

Red Arc -

O-360-C1F

Avoid Continuous Operation

2150 –

2350 RPM

Green Arc -

O-360-C1F

Normal Operating Range,

2350 -

2700 RPM

Green Arc -

O-360-C4F

Normal Operating Range,

2000 -

2700 RPM

Red Radial -

Maximum RPM, 2700 RPM

PAGE 4

SECTION II

LIMITATIONS

180 hp @ 2700 RPM, Full Throttle Continuous

56 (76”) or

56 (76”)

100/100LL Minimum Grade Aviation Gasoline

Normal Operating Range,

Operating Limit, 500

°F

Normal Operating

Range,

Operating Limit, 245

°F

Normal Operating Range, 55

Caution Range, 25 to 55 and

Minimum Operating Pressure,

25 psi, Maximum Operating

Pressure, 115 psi

Normal Operating Range, 0.5

Minimum, 0.5 psi, Maximum,

Avoid Continuous Operation

2350 RPM

Normal Operating Range,

2700 RPM

Normal Operating Range,

2700 RPM

Maximum RPM, 2700 RPM

MAULE AEROSPACE TECHNOLOGY, INC.

2.3 FLIGHT LOAD FACTORS:

2.4 PLACARDS:

The following placards are in the cockpit in clear view of the pilot:

"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE

IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE

MANUAL AND IN THE FORM OF PLACARDS AND MARKINGS.”

"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."

"MANEUVERING SPEED

"THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON

EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.”

"DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF

"FUEL REMAINING IN TANK WHEN INDICATOR READS Z

USED SAFELY IN FLIGHT.

"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF

AIRPLANE FLIGHT MANUAL."

"DEMONSTRATED CROSSWIND

On the instrument panel at the auxiliary tank transfer switches:

PUSH FOR

AUX. QUANT.

NOTE: If JPI EDM-

900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pl

cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are

used as below:

FUEL CAPACITY:

MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS

USABLE EACH.

15 Gal. or 21 Gal. Instrument Panel Placard will show capacity of

craft.

FAA APPROVED: 5/4/00

Rev. A dated:

Rev. B dated:

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE MX-7-180AC

Flaps Fully Retracted: 3.8g Positive to 1.5g Negative

Flaps Extended: 1.9g Positive to 0g Negative

The following placards are in the cockpit in clear view of the pilot:

"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE

IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE

MANUAL AND IN THE FORM OF PLACARDS AND MARKINGS.”

"NO AEROBATIC MANEUVERS INCLUDING SPINS, APPROVED."

"MANEUVERING SPEED

109K (125 MPH) IAS."

"THIS AIRPLANE APPROVED FOR DAY OR NIGHT IFR NON

ICING FLIGHT

EQUIPPED IN ACCORDANCE WITH FAR 91 OR FAR 135.”

"DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF

"FUEL REMAINING IN TANK WHEN INDICATOR READS Z

ERO CANNOT BE

USED SAFELY IN FLIGHT.

"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF

AIRPLANE FLIGHT MANUAL."

"DEMONSTRATED CROSSWIND

13K (15 MPH)."

On the instrument panel at the auxiliary tank transfer switches:

FUEL TRANSFER PUMPS

PUSH FOR

AUX. QUANT.

LEFT RIGHT

900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pl

cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are

FUEL TRANSFER PUMPS

LEFT RIGHT

MAIN TANKS 21.5 GAL. USABLE EACH, AUX. TANKS

GAL.

USABLE EACH.

15 Gal. or 21 Gal. Instrument Panel Placard will show capacity of

the tanks installed in this ai

PAGE 5

SECTION II

LIMITATIONS

Flaps Fully Retracted: 3.8g Positive to 1.5g Negative

"THIS AIRPLANE MUST BE OPERATED AS A NORMAL CATEGORY AIRPLANE

IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE

FLIGHT

ICING FLIGHT

WHEN

"DO NOT TURN OFF ALTERNATOR IN FLIGHT EXCEPT IN CASE OF

EMERGENCY."

ERO CANNOT BE

"SEE LOADING INSTRUCTIONS IN WEIGHT AND BALANCE SECTION OF

PUSH FOR

900/930 units are installed, the PUSH FOR AUX. QUANT. buttons and pl

cards are not installed. However, FUEL TRANSFER PUMPS and LEFT and RIGHT placards are

GAL.

the tanks installed in this ai

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