MAULE M-7-260 Technische Daten

FAA APPR0VED

AIRPLANE FLIGHT MANUAL

FOR

MAULE

M-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 USA

DATE:______________________________

Performance That Counts!

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

Page i

LOG OF REVISIONS

REV. TO

PAGES

DESCRIPTION APPROVAL AND DATE

5, 6

Added and revised Placards.

Corrected Crosswind Component.

Corrected omission.

__________________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date: ______________

Vendor part number change.

_____________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date: ______________

Corrected (fully retracted) to read (first notch) in

Item F.

_________________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date:_____________________

Added "-D" to Item 5.a.

Corrected Unusable fuel to read 2.3 gallons.

Added McCauley Propellers B2D37C224-[ ]/[ ]-

90RA-10.5 and B3D32C414-[ ]/[ ]-82NDA-2.

_____________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date: ______________

3,5,

11-16

Changed primary airspeed units to knots.

_______________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date: ____________________

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

In 3.3.A FLAP SETTINGS, corrected Landing

flap handle position to read: Fourth Notch for 48°

flap position. In 3.3.B. RECOMMENDED FLAP

SETTINGS, corrected Landing flap setting to

read - Normally Fourth Notch (48°/full flaps).

________________________

Manager, Aircraft Certification

Office, FAA

Atlanta, Georgia

Date: ______________

10,

11,

Described placard notation and removal of aux.

Quantity buttons if JPI EDM-900/930 units are

installed. In rear cabin area revised cargo weight

limitation placard and added loading caution

placard for 4-seater. Added limit placard for

optional swing out windows. Changed FLYING

WIRES to read STRUT in 3.1.23. Added to

Operating Check Lists for Parking Brake when in

OFF position to PUSH KNOB COMPLETELY

AGAINST INSTRUMENT PANEL. Corrected

Alternate Air Control operating check to read:

PUSH IN AND LOCK. Revised Section VI re

Owner Alert System, the availability of data

downloads and Maule Parts Catalog DVD.

_________________________

Manager, Atlanta Aircraft

Certification Office, FAA

Atlanta, GA

Date:__________________

iiii, 24

Changed page number from 33 to 24.

Added note from Sec. 2.3.

Added J.P. Instrument EDM-900/930. Moved

note from Sec. 2.3 to Sec. 2.1.

__________________________

Manager, Southeast Flight Test

Section, AIR-712, FAA

Atlanta, GA

Date:__________________

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-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 Dwg 9135A, Rev. Eor later rev.

(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 ST-810-20 (14v) - Maule Dwg 9197A.

(Sea) 07/05/01

5 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-810-30 (14v) - Maule Dwg 9197A.

(Sea) 07/05/01

- 5 Inst. of S-TEC System 20 Single Axis Autopilot ST-872-20 (28v) - Maule Dwg 9211A.

(Sea) 06/25/01

- 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-872-30 (28v) - Maule Dwg 9211A.

(Sea) 06/25/01

3 Installation of GARMIN GNS-430 (GPS/NAV/COMM) System - Maule Dwg 7205A. 01/03/01

- 3 Inst. of GARMIN GNC-300XL (GPS/COMM) System - Maule Dwg 7207A. 01/03/01

- 3 Inst. of GARMIN GNC-250XL

(GPS/COMM)

System - Maule Dwg 7209A. 01/03/01

- 3 Inst. of Bendix-King KLX-135A

(GPS/COMM)

System - Maule Dwg 7219A. 01/03/01

- 5 Inst. of S-TEC System 20 Single Axis Autopilot ST-873-20 (14/28v) - Maule Dwg

9212A. (Land) 10/15/01

- 5 Inst. of S-TEC System 30 Two Axis Autopilot ST-873-30 (14/28v) - Maule Dwg 9212A.

(Land) 10/15/01

- 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

- 5 Installation of GARMIN SL40 VHF Communications Transceiver - Maule Drawing

7249A. 07/14/08

7 5 Installation of Fli-Lite 3000 Mk IIIA Skis - Maule Dwg 9081A, Rev. For later. 03/11/09

- 9 Inst. of S-TEC System 50 Two Axis Autopilot Model ST-873-50 (14v) - Maule Dwg

9193A, Rev. For later. (Land) 04/19/13

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-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………………………………. 11

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 Shutdown…………………………. 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.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

Page iiii

TABLE OF CONTENTS

ITEM

SECTION V WEIGHT AND BALANCE AND EQUIPMENT LIST

5.1 Weight and Balance Data……………………………… 17

Required Equipment List Provided for each Airplane

SECTION VI AIRCRAFT SERVICING, HANDLING AND MAINTENANCE

6.1 Introduction……………………………………………… 24

6.2 Airplane Inspection Period…………………………….. 24

6.3 Preventive Maintenance that may be Accomplished

by a Certified Pilot………………………………………. 24

6.4 Alterations or Repairs to Airplane…………………….. 24

SECTION VII MANUFACTURER'S DATA

Optional Equipment List

Rev. H dated: 7/16/18

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

SECTION I

GENERAL

PAGE 1

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-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.

+12.5 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 recommen-

dations and loading graphs.

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

////CAUTION////

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

CHECK WEIGHT AND BALANCE CAREFULLY, ESPECIALLY WHEN US-

ING THE 5

SEAT OR WHEN CARGO OR BAGGAGE IS CARRIED IN THE

REAR CABIN AREA. ALSO, FLIGHT PLANNING SHOULD INCLUDE AL-

LOWANCE 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 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 Auxiliary Tank configuration installed in

this aircraft.

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

////CAUTION////

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

FUEL REMAINING IN TANK WHEN INDICATOR READS EMPTY CANNOT

BE USED SAFELY IN FLIGHT

FAA APPROVED

DATE: 417/98

Rev. D dated: PAGE 2

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

SECTION II

LIMITATIONS

2.1 AIRSPEED LIMITS: All airspeeds are Indicated Airspeeds (IAS).

A. AIRSPEED INDICATOR MARKINGS:

Red Radial, (V

) - 158K (182 mph)

Yellow Arc, Caution Range - 128 - 158K (147 - 182 mph)

Green Arc, Normal Operating Range - 54 - 128K (62 - 147 mph)

White Arc, Flap Operating Range - 43 - 83K (50 - 95 mph)

B. EXPLANATION OF AIRSPEED INDICATOR MARKINGS:

Red Radial Line -

Never Exceed Speed (V

) 158K (182 mph): Maximum safe

airspeed in smooth air.

Yellow Arc - Caution Range, 128 - 158K (147 - 182 mph): Operation in this

speed range should be conducted only in smooth air and con-

trol movements should not be large or abrupt.

Green Arc - Normal Operating Range, 54 - 128K (62 - 147 mph): Extends

from flaps up, power off stall speed at 2500 lbs. (V

) to design

cruise speed (V

White Arc - Flap Operating Range, 43 - 83K (50 - 95 mph): Extends from

full flap, power off minimum stall speed at 2500 lbs. (V

) to

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

DATE: 4/17/98

Rev. D dated:

Rev. H dated: 7/16/18 PAGE 3

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE M-7-260

2.2 POWER PLANT LIMITS:

Engine: Lycoming IO-540-V4A5

Engine Limits: 260 hp @ 2700 RPM, Full Throttle Continuous

Propeller: MT-Propeller: MTV-14-B/190-17

Hartzell: HC-C2YR-1BF/F8477D-6

HC-C3YR-1RF/F-7693(F)-( )*

McCauley: B2D37C224-[ ]/[ ]-90RA-10.5 or -12

B3D32C414-[ ]/[ ]-82NDA-2 or -4

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

and 95 to 115 psi

Red Radial - Minimum Operating Pressure,

25 psi, Maximum Operating

Pressure, 115 psi

Manifold Pressure Green Arc - Normal Operating Range,

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)

FAA APPROVED: 4/17/98

Rev. A dated: 6/23/99 PAGE 4

Rev. C dated:

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