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Page 22

MAULE AEROSPACE TECHNOLOGY, INC.

AIRPLANE FLIGHT MANUAL

MAULE

MX-7-180

SECTION V
WEIGHT AND
BALANCE

WEIGHT AND BALANCE ENVELOPE

FORM 50

Содержание MX-7-180 Star Rocket

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

Страница 2: ...33 B 2 to Required Equipment List Added NOTE re Rear Seat occupants Shoulder Harness requirement ______________________________ Manager Aircraft Certification Office Federal Aviation Atlanta GA Date...

Страница 3: ...e Placard and the Rear Cabin Cargo Limitation Placard from Deleted Fuel Capacity numbers from Fuel Transfer Pump Switch Placard and added note for Tank Configuration Added Unusable Fuel weight for new...

Страница 4: ...4 4 5 EMERGENCY EXIT ON THE GROUND 14 4 6 TAKEOFF ABORT BEFORE LIFT OFF 14 4 7 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING 15 4 8 PARTIAL POWER FAILURE DURING FLIGHT OR AFTER TAKEOFF 15 4 9 COMPLET...

Страница 5: ...ilot ST 418 40 14v Maule Dwg 9193A 10 29 01 14 7 Inst of S TEC System 40 Single Axis Autopilot ST 609 40 28v Maule Dwg 9200A 10 29 01 4 Inst of S TEC System 20 Single Axis Autopilot ST 872 20 28v Dwg...

Страница 6: ...Page 1 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 SECTION I GENERAL...

Страница 7: ...een points given Datum Wing Leading Edge 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 recommendat...

Страница 8: ...MX 7 180 All airspeeds are Indicated Airspeeds IAS AIRSPEED INDICATOR MARKINGS EXPLANATION OF AIRSPEED INDICATOR MARKINGS Never Exceed Speed VNE 161K 185 mph Maximum safe airspeed in smooth air Cauti...

Страница 9: ...w Arc Caution Range 25 to 55 PSI and 95 to 115 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...

Страница 10: ...fe airspeed at which full aerodynamic controls can be applied VA is 109K 125 mph This airspeed is not marked on the airspeed The following placards are in the cockpit in clear view of the pilot THIS A...

Страница 11: ...BOTH RIGHT GAL placard is located on the instrument panel at the optional auxiliary tank transfer FUEL TRANSFER PUMPS PUSH FOR AUX QUANT PUSH FOR AUX QUANT LEFT RIGHT 900 930 units are installed the...

Страница 12: ...HINGES ATTACHMENTS Aileron CHECK HINGES CONTROL ATTACHMENTS Left Wing Top CHECK FOR WRINKLES AS INDICATION OF INTERNAL DAMAGE Left Wing Main Fuel Tank Drain Left Wing Aux Fuel Tank Drain if installed...

Страница 13: ...ION OF INTERNAL DAMAGE Right Side Static Port CLEAR Stabilizer CHECK ATTACHMENT POINTS STRUT Right Elevator CHECK HINGE POINTS Rudder CHECK HINGE POINTS CONTROL ATTACHMENT NAV LIGHT Tailwheel CHECK FO...

Страница 14: ...ION BAT AND ALT SWITCHES TURN FUEL VALVE OFF AND EXIT AIRCRAFT Starting CHECK OIL PRESSURE IF OIL PRESSURE DOES NOT EXCEED 25 PSI WITHIN 30 SECONDS SHUT DOWN ENGINE Alternator CHECK CHARGING other ele...

Страница 15: ...FULL RICH Propeller Control FULL INCREASE RPM Carburetor Air Control PUSH COLD Engine Instruments RECHECK IN NORMAL RANGE Radios AS DESIRED Altimeter SET Attitude Indicator CHECK ERECT Directional Ind...

Страница 16: ...GS The following Flap Settings are available Flap Handle Position Flap Position Handle Full Down 7 First Notch 0 Second Notch 24 Third Notch 40 Fourth Notch 48 RECOMMENDED FLAP SETTINGS Flap settings...

Страница 17: ...BATTERY SWITCH IS OFF CROSSWIND LANDINGS TAKEOFFS Maximum demonstrated crosswind component is 13K 15 mph and flap extension should be limited to 0 fully retracted with such crosswind or higher 13K 15...

Страница 18: ...emoved both front doors are installed with the rear passenger door or rear passenger and baggage doors off When doing so observe the following additional limitations Maximum airspeed 109K 125 mph Maxi...

Страница 19: ...4 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 EMERGENCY PROCEDURES EMERGENCY BASIC RULES To assist the pilot when an emergency occurs three basic rules are established which a...

Страница 20: ...4 25 85 REV D Dated Page 15 MAULE AEROSPACE TECHNOLOGY INC SECTION IV AIRPLANE FLIGHT MANUAL EMERGENCY PROCEDURES MAULE MX 7 180 ENGINE FAILURE AFTER TAKEOFF OR FORCED LANDING Establish 72K 83 mph IA...

Страница 21: ...appropriate controlling agency if appropriate Determine control difficulty airspeed by slowing down while flying straight ahead low the aircraft to stall Make full stop landing using 4 to 9K 5 to 10 m...

Страница 22: ...plane is loaded properly The empty weight empty weight center of gravity and useful load are listed below for this airplane as delivered from the factory If the airplane has been altered refer to the...

Страница 23: ...e tailwheel elevated to place the airplane in approximately the flight attitude Place a level on the leveling mark and leveling lug on the bottom of the right wing near the root Adjust the height of t...

Страница 24: ...______________lbs The corresponding empty weight center of gravity is ______________inches Calculations for determining weight C G and moment Center of Gravity inches L x T D W i e C G _____________ _...

Страница 25: ...Page 20 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 LOADING CHART SECTION V WEIGHT AND BALANCE FORM 50...

Страница 26: ...ROSPACE TECHNOLOGY INC THIS PAGE INTENTIONALLY FORM 50 Rev G dated Page 21 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 THIS PAGE INTENTIONALLY LEFT BLANK SECTION V WEIGHT AND...

Страница 27: ...Page 22 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 SECTION V WEIGHT AND BALANCE WEIGHT AND BALANCE ENVELOPE FORM 50...

Страница 28: ...RPLANE FLIGHT MANUAL MAULE STRUCTURAL CAPACITY CHART FORM 50 Rev G dated Page 23 MAULE AEROSPACE TECHNOLOGY INC AIRPLANE FLIGHT MANUAL MAULE MX 7 180 SECTION V WEIGHT AND BALANCE STRUCTURAL CAPACITY C...

Страница 29: ...EIGHT 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 lbs D New Useful Load...

Страница 30: ...e owner operator is responsible for Airworthiness Directives AD s that may be issued from time to time Reference should be made to FAR 91 and FAR 43 requirements ncy or personnel to accomplish the req...

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