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MAULE AEROSPACE TECHNOLOGY, INC. 

AIRPLANE FLIGHT MANUAL 

MAULE

 

M-7-260C 

2800# Upgross Per STC

 

SA04077CH

 

 

FAA APPROVED 
DATE: 11-16-16 

 

8 of 29 

Rev. A 

 
 

Engine Instrument Markings: 
 

Cylinder Head Temperature: 

Green Arc - 

Normal Operating Range, 
200

°

F - 435

°

 

Red Radial - 

Operating Limit, 500

°

Oil Temperature: 

Green Arc - 

Normal Operating Range, 
140

°

F - 245

°

 

Red Radial - 

Operating Limit, 245

°

Oil Pressure: 

Green Arc - 

Normal Operating Range, 55 
to 95 PSI 

 

Yellow Arc - 

Caution Range, 25 to 55 PSI 
and 95 to 115 PSI 

 

Red Radial - 

Minimum Operating Pressure, 
25 PSI 

 

Red Radial - 

Maximum Operating Pressure, 
115 PSI 

Manifold Pressure 

Green Arc - 

Normal Operating Range,  
14.5 to 29 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 

 

2.3  FLIGHT LOAD FACTORS:  
 

Flaps Fully Retracted: 3.8g Positive to 1.5g Negative 
Flaps Extended: 1.9g Positive to 0g Negative 
 

NOTE:  DESIGN MANEUVERING SPEED: The maximum safe airspeed at which full aero-

dynamic controls can be applied (V

A

) is 109K (125 mph).  This airspeed is not 

marked on the airspeed indicator.  

 

 

2.4  PLACARDS: 

 
 

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

 

Summary of Contents for 30046C

Page 1: ...Performance That Counts 2099 Georgia Highway 133 South Moultrie GA 31788 229 985 2045 Fax 229 985 2048 or 229 890 2402 www mauleairinc com...

Page 2: ...AL MAULE M 7 260C 2800 Upgross Per STC SA04077CH 2 of 29 Rev A LOG OF REVISIONS REV TO PAGES DESCRIPTION APPROVAL AND DATE A 8 14 15 16 19 26 Corrected per FAA comments dated 10 27 16 FAA APPROVED ___...

Page 3: ...PPROVED DATE 11 16 16 3 of 29 Rev A LOG OF SUPPLEMENTS SUPP NO NO OF PAGES DESCRIPTION APPROVAL DATE 1 2 Tow Release Assembly installed in accordance with Maule drawing 3196F Rev G or later 17 Jan 201...

Page 4: ...ING 18 4 4 ENGINE FIRE AFTER STARTING 18 4 5 EMERGENCY EXIT ON THE GROUND 18 4 6 TAKEOFF ABORT BEFORE LIFT OFF 18 4 7 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING 18 4 8 PARTIAL POWER FAILURE DURING...

Page 5: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 260C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 5 of 29 Rev A...

Page 6: ...ations and loading graphs CAUTION CHECK WEIGHT AND BALANCE CAREFULLY ESPECIALLY WHEN USING THE 5TH SEAT IF INSTALLED OR WHEN CARGO OR BAGGAGE IS CAR RIED IN THE REAR CABIN AREA ALSO FLIGHT PLANNING SH...

Page 7: ...K 145 180 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 53 126K 61 145 mph Extends from...

Page 8: ...Radial Minimum Operating Pressure 25 PSI Red Radial 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...

Page 9: ...RIGHT 21 5 GAL On the instrument panel at the auxiliary tank transfer switches FUEL TRANSFER PUMPS PUSH FOR AUX QUANT PUSH FOR AUX QUANT LEFT RIGHT NOTE If JPI EDM 900 930 units are installed the PUS...

Page 10: ...ear cabin area Or also in rear cabin area when 5th seat is not installed On the lower window frame near the latch when optional swing out windows are installed CARGO OR BAGGAGE LIMITATIONS MAX LOAD AR...

Page 11: ...on CHECK HINGES CONTROL AT TACHMENTS 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 Auxi...

Page 12: ...INDICA TION OF INTERNAL DAMAGE 30 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...

Page 13: ...HIN 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 CHEC...

Page 14: ...SH KNOB COMPLETELY AGAINST INSTRUMENT PANEL E BEFORE LANDING 1 Seat Belts Shoulder Harnesses FASTENED 2 Fuel Selector Valve ON FULLEST TANK OR BOTH 3 Mixture Control FULL RICH 4 Propeller Control FULL...

Page 15: ...ull Down 7 b First Notch 0 and c Second Notch 24 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 Normal Takeoff Secon...

Page 16: ...airplane and is not considered limiting with flaps at 0 H 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 Au...

Page 17: ...ade 74 8 dBA with Hartzell 78 2 blade 78 0 dBA with McCauley 78 with Hartzell with McCauley 78 2 blade 3 blade 3 blade 78 8 dBA 78 0 dBA 78 0 dBA 79 5 80 1 dBA 80 78 2 dBA The noise levels obtained du...

Page 18: ...Switch OFF 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 i...

Page 19: ...pt engine airstart if warranted 4 10 ENGINE AIRSTART 1 Fuel Selector BOTH 2 Electric Fuel Pump ON 3 Mixture RICH 4 Ignition Switch BOTH start if propeller is not turning 5 Auxiliary fuel tank pump swi...

Page 20: ...neously ap ply full rudder opposite to the direction of rotation and full nose down elevator with ailerons neutral and reduce power to idle When the rotation stops neutralize the rudder and eleva tor...

Page 21: ...ne has been altered refer to the aircraft log and or aircraft records for this information WEIGHT AND BALANCE DATA SUMMARY AS DELIVERED FROM THE FACTORY Basic Empty Weight including engine oil _______...

Page 22: ...ft is level 3 Measure the following distances a Wheel base L the horizontal distance from the tailwheel weight point center of axle to the main wheel weight point center of axle L __________________ I...

Page 23: ..._______ ___________inches b Moment inch pounds W x C G i e Moment _____________ x ____________ ___________inch lbs EXAMPLE OF WEIGHT AND BALANCE CALCULATION FOR LOADED AIRCRAFT An airplane with an emp...

Page 24: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 260C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 24 of 29 Rev A...

Page 25: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 260C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 25 of 29 Rev A...

Page 26: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 260C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 26 of 29 Rev A...

Page 27: ...____ ITEM S MAKE MODEL WEIGHT ARM MOMENTS Previous Aircraft Empty A New Empty Weight ______________________lbs B New Empty Center of Gravity ______________ins C New Empty Weight C G Moment ___________...

Page 28: ...nd most of the manufacturer s recommended inspections It is required that owner s email address name and address optional and aircraft serial number be sent to OwnerAlert mauleairinc com for notificat...

Page 29: ...OLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 260C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 29 of 29 Rev A SECTION VII MANUFACTURER S DATA 7 1 OPTIONAL AND REQUIRED EQUIPMENT LIST PROVID...

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