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MAULE M-7-260C Скачать руководство пользователя страница 23

MAULE AEROSPACE TECHNOLOGY, INC.

SECTION V

AIRPLANE FLIGHT MANUAL

WEIGHT AND BALANCE

MAULE

M-7-260C

SECTION V

5.1

WEIGHT AND BALANCE:

Serial Number______________________ Registration Number______________________

It is the responsibility of the airplane owner and the pilot to insure that the airplane is

loaded properly. The empty weight, empty weight center of gravity and useful load are listed be-
low for this airplane 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:

Basic Empty Weight (including engine oil)……………………._________Lbs.

Gross Weight………………………………………………………__2500___Lbs.

Useful Load……………………………………………………….._________Lbs.

Empty Center of Gravity…………………………………………._________Inches

Empty Weight Moment………………………………..…………_________ Inch Lbs.

CENTER OF GRAVITY RANGE:

At Weight of

Center of Gravity Range

2500 lbs.

+15.0 to +20.0 inches

1700 lbs.

+12.5 to +20.0 inches

NOTE: Straight line variation between given points

DATUM: Wing leading edge

CERTIFIED BY______________________________DATE____________________

FORM 74

PAGE 17

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Содержание M-7-260C

Страница 1: ...MENT MUST BE KEPT IN THE AIRPLANE AT ALL TIMES FAA APPROVED ______________________________ Manager Aircraft Certification Office Federal Aviation Administration Atlanta Georgia USA DATE ______________...

Страница 2: ..._____________ C 19 2 4 13 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 Cer...

Страница 3: ...FAA Atlanta Georgia Date ______________ H 6 10 24 Corrected Alternate Air Control operating check to read PUSH IN AND LOCK in rear cabin area added loading caution placard for 4 seater Revised Section...

Страница 4: ...S 300XL GPS COMM System Maule Dwg 7207A 01 03 01 3 Inst of Garmin GNS 250XL GPS COMM System Maule Dwg 7209A 01 03 01 3 Inst of Bendix King SLX 135A GPS COMM System Maule Dwg 7219A 01 03 01 5 Inst of S...

Страница 5: ...ts 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...

Страница 6: ...lance 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...

Страница 7: ...MAULE AEROSPACE TECHNOLOGY INC SECTION I AIRPLANE FLIGHT MANUAL GENERAL MAULE M 7 260C PAGE 1...

Страница 8: ...THE 5TH 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 Maneuver...

Страница 9: ...r 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 Ran...

Страница 10: ...g 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 9...

Страница 11: ...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 SAFE LY IN FLIGHT SEE LOADING INSTRUCTIONS IN WEIGHT AND...

Страница 12: ...EA A 100 LBS MAX LOAD AREA B 175 LBS MAX LOAD AREA C 125 LBS Also in rear cabin area when 5th seat is installed CHECK WEIGHT AND BALANCE CAREFULLY WHEN USING 5TH SEAT OR LOADING REAR CARGO BAGGAGE MAX...

Страница 13: ...L ATTACHMENTS 3 Aileron CHECK HINGES CONTROL ATTACHMENTS 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 CHE...

Страница 14: ...ONTROL ATTACHMENT NAV LIGHT 26 Tailwheel CHECK FOR INFLATION ATTACH MENTS REMOVE TIEDOWN 27 Left Elevator CHECK TAB CONTROLS ALL HINGE POINTS 28 Left Stabilizer CHECK ATTACHMENT POINTS STRUT 29 Left F...

Страница 15: ...OR ANOTHER 3 TO 5 SECONDS OVER PRIME CAN BE NOTED BY FUEL COMING FROM DRAIN IN CENTER OF BOTTOM COWL CAUTION IN EVENT OF ENGINE FIRE CONTINUE CRANKING PULL MIXTURE TO FULL LEAN IF ENGINE FAILS TO STAR...

Страница 16: ...S DESIRED FOR T O MAX 24 3 Trim Controls SET FOR TAKEOFF 4 Flight Controls CHECK FOR FREEDOM AND PROPER TRAVEL 5 Mixture Control FULL RICH 6 Propeller Control FULL INCREASE RPM 7 Alternate Air Control...

Страница 17: ...ation Flap Handle Position Flap Position Cruise Handle Full Down 7 Flaps Up First Notch 0 Takeoff Second Notch 24 Landing Third Notch 40 Landing Fourth Notch 48 B RECOMMENDED FLAP SETTINGS Flap settin...

Страница 18: ...hen lock E STALLS Stalls are preceded by mild buffet that can be felt through the rudder pedals The red stall warning light on the instrument panel will illuminate at 4 to 9K 5 to 10 mph above the sta...

Страница 19: ...so observe the following additional limitations 1 Maximum airspeed 109K 125 mph 2 Maximum bank angle 30 3 Maximum yaw angle 10 4 No Smoking permitted 5 Limit flight to VFR conditions 3 5 NOISE LEVEL...

Страница 20: ...itch 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 f...

Страница 21: ...tric Fuel Pump On 6 Ignition Switch Both 7 Master Switch On 4 9 COMPLETE POWER FAILURE DURING FLIGHT 1 Glide Establish 69K 80 mph IAS 2 Attempt engine airstart if warranted 4 10 ENGINE AIRSTART 1 Fuel...

Страница 22: ...rtently enters a spin simultaneously 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 neutral...

Страница 23: ...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 Basic Empty Weight inc...

Страница 24: ...of the tailwheel until the aircraft 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 cen...

Страница 25: ..._______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 empty weight of...

Страница 26: ...MAULE AEROSPACE TECHNOLOGY INC SECTION V AIRPLANE FLIGHT MANUAL WEIGHT AND BALANCE MAULE M 7 260C 07 08 08 FORM 74 PAGE 20...

Страница 27: ...MAULE AEROSPACE TECHNOLOGY INC SECTION V AIRPLANE FLIGHT MANUAL WEIGHT AND BALANCE MAULE M 7 260C CENTER OF GRAVITY ENVELOPE FORM 74 PAGE 21...

Страница 28: ...MAULE AEROSPACE TECHNOLOGY INC SECTION V AIRPLANE FLIGHT MANUAL WEIGHT AND BALANCE MAULE M 7 260C 07 08 08 Rev J dated 7 16 18 FORM 74 PAGE 22...

Страница 29: ...M MOMENTS Previous Aircraft Empty A New Empty Weight ______________________lbs B New Empty Center of Gravity ______________ins C New Empty Weight C G Moment ___________in lbs D New Useful Load _______...

Страница 30: ...most of the manufacturer s recommended inspections It is required that owner s email address name and address optional and Aircraft S N be sent to OwnerAlert mauleairinc com for notification of any M...

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