MAULE 25115C Airplane Flight Manual Download

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MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE

M-7-235C

2800# Upgross Per STC

SA04077CH

FAA APPROVED
DATE: 11-16-16

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Summary of Contents for 25115C

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: ...L MAULE M 7 235C 2800 Upgross Per STC SA04077CH 2 of 28 LOG OF REVISIONS REV TO PAGES DESCRIPTION APPROVAL AND DATE A 10 12 14 15 16 19 26 Corrected per FAA comments dated 10 27 16 FAA APPROVED ______...

Page 3: ...A APPROVED DATE 11 16 16 3 of 28 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 2013 4...

Page 4: ...17 4 3 ENGINE FIRE DURING STARTING 17 4 4 ENGINE FIRE AFTER STARTING 17 4 5 EMERGENCY EXIT ON THE GROUND 17 4 6 TAKEOFF ABORT BEFORE LIFT OFF 17 4 7 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING 17...

Page 5: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 235C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 5 of 28...

Page 6: ...ndations 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...

Page 7: ...peed 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 flaps up power off stall speed a...

Page 8: ...perating 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 A...

Page 9: ...EN 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 FLIGHT DEMON...

Page 10: ...ards are used as below FUEL TRANSFER PUMPS LEFT RIGHT FUEL CAPACITY MAIN TANKS 21 5 GAL USABLE EACH AUX TANKS 21 0 GAL USABLE EACH On flap control handle FLAPS PULL ON 2ND NOTCH TAKEOFF 4TH NOTCH LAND...

Page 11: ...RNAL 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 R...

Page 12: ...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 RICH SEE NOTE FOR HOT START 6 Anti Collision...

Page 13: ...H COLD 8 Vacuum Gauge CHECK IN GREEN 9 Alternator CHARGING LIGHT OUT ABOVE 900 RPM 10 Throttle RETARD TO IDLE D BEFORE TAKEOFF 1 Fuel Selector ON FULLEST TANK OR BOTH 2 Flaps AS DESIRED FOR T O MAX 24...

Page 14: ...BELOW 1000 RPM 6 Mixture Control FULL LEAN 7 Magneto Switch OFF 8 Anti Collision Light OFF 9 BAT ALT Switch OFF 10 Parking Brake OFF AS DESIRED 3 3 NORMAL FLIGHT OPERATIONS A NOTE FLAP SETTINGS The f...

Page 15: ...M NOTE To assure full effectiveness of the Right Rudder Trim Unlock T handle turn left depress right rudder as you pull T handle full out Lock T handle turn right before releasing right rudder pressur...

Page 16: ...the respective main tank fuel gauge indicator and a decrease on the respective auxil iary tank indicator 3 4 DOOR OFF OPERATION This aircraft may be operated with either one not both of the front doo...

Page 17: ...tch 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 if fi...

Page 18: ...80 mph IAS 2 Attempt 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...

Page 19: ...ers a spin simultaneously apply 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 rudd...

Page 20: ...ane as delivered from the factory If the airplane 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...

Page 21: ...t point center of axle L __________________ Inches b Main Wheel Station D the horizontal distance from the main wheel weight point center of axle to the datum line D __________________ Inches 4 Measur...

Page 22: ...weight of 1549 lbs and empty weight moment of 17 349 inch lbs is loaded with a pilot and front seat passenger fuel and 125 lbs for baggage Item Weight lbs C G Location Moment In lbs Empty Weight incl...

Page 23: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 235C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 23 of 28...

Page 24: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 235C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 24 of 28...

Page 25: ...MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 235C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 25 of 28...

Page 26: ..._ 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 ___________in...

Page 27: ...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 notificatio...

Page 28: ...CHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE M 7 235C 2800 Upgross Per STC SA04077CH FAA APPROVED DATE 11 16 16 28 of 28 SECTION VII MANUFACTURER S DATA 7 1 OPTIONAL AND REQUIRED EQUIPMENT LIST PROVIDED...

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