background image

 

MAULE AEROSPACE TECHNOLOGY, INC. 

AIRPLANE FLIGHT MANUAL 

MAULE

 

M-7-235C 

2800# Upgross Per STC

 

SA04077CH

 

 

FAA APPROVED 
DATE: 11-16-16 

 

19 of 28 

 

 
 

4. 

Pilot's Window - OPEN (below 104K (120 mph) 

 

4.14 STRUCTURAL DAMAGE: 

 

1. 

On Takeoff - Abort 

2. 

In flight, maintain controllable airspeed 

3. 

Climb to safe stall recovery altitude 

4. 

Notify appropriate controlling agency, if appropriate. 

5. 

Determine control difficulty airspeed by slowing down while flying straight ahead.  
Do not allow the aircraft to stall. 

6. 

Make full stop landing using 4 to 9K (5-10 mph) above difficulty airspeed or above 
normal approach speed, whichever is higher. 

 

4.15 RECOVERY FROM INADVERTENT SPINS: 

 

Intentional spins are prohibited.  If the aircraft inadvertently enters 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 rudder and eleva-
tor, and ease back on the control wheel as required to smoothly regain level flight.  Wing 
flaps should be retracted to avoid exceeding the maximum flap speeds during recovery. 

 

4.16 ALTERNATOR FAILURE:  

 

Alternator output should be monitored by reference to the ammeter located on the right side 
of the engine instrument cluster.  Should the ammeter indicate a minus deflection when en-
gine RPM is above 900 and/or red "ALTERNATOR OFF WARNING" light is illuminated, 
push ALT switch OFF then ON.  Repeat two times as necessary to reset.  If system will not 
reset, reduce the electrical load as much as possible, land as soon as practical and investi-
gate the electrical system malfunction before further flight. 

Содержание 25115C

Страница 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...

Страница 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 ______...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Отзывы: