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Страница 1: ...MOONEY OPERATORS MANUAL MODEL M 2 O C SERIAL NUMBERS 20 1 1 4 7 ON DECEMBER 1974 ISSUE MOONEY AIRCRAFT CORPORATION K E R R V I L L E T E X A S 78028 m M A N U A L N U M B E R 7 4 2 0 C O G...

Страница 2: ......

Страница 3: ...12 2 74 2 15 0 12 2 74 2 16 12 2 74 2 17 12 2 74 2 18 12 2 74 SECTION Ill Page Date 3 1 12 2 74 3 2 12 2 74 3 4 12 2 74 3 5 12 2 74 3 6 12 2 74 3 7 12 2 74 3 8 12 2 74 3 9 12 2 74 3 10 12 2 74 3 11 12...

Страница 4: ...L O G OF PAGES CONT SECTION V F A A APPROVED Page Dafe SECTION V I Page Date SECTION V I I Page Date...

Страница 5: ...GENERAL DESCRIPTION SECTION SYSTEMS OPERATIONS SECTION NORMAL PROCEDURES SECTION LIMITATIONS SECTION EMERGENCY PROCEDURES SECTION PERFORMANCE SECTION SERVICING 4 SECTION...

Страница 6: ...MITATIONS AND MUST I IE CARRIED I N THE AIRCRAFT AT ALL TIMES A l l i l o r m a t i o n incl illustrations in this manual a r e based on the latest procluct information available at the time of 1 ut l...

Страница 7: ...on re quest provide and execute such instruments a s may be reasonably required to evidence such assignment Mooneyfs obligztion under this warranty is limited to repairing or replacing at Mooney s op...

Страница 8: ...N L I E U OF ANY OTHER P ARRANTIES EXPRESSED OR III P L I E D I N FACT OR BY LAW INCLUDING ANY I I I P L I E D WARRANTY OF MERCHANTABILITY OR F I T N E S S FOR A PARTICULAR PURPOSE AND I S I N L I E...

Страница 9: ...DESCRIPTION DESIGN FEATURES AIRFRAME 1 2 POWERPLANT 1 2 FLIGHT CONTROLS 1 3 LANDING GEAR 1 3 SPECIFICATIONS OUTLINE POWERPLANT 1 3 PROPELLER 1 4 LANDING GEAR 1 4 FUEL OIL 1 5 WEIGHT LOADING 1 5 BAGGAG...

Страница 10: ...area For pitch trim control the empennage pivots on the aft fuselage A torque tube driven jack screw bolted to the r e a r tail con bulkhead sets the stabilizer angle The forward opening cabin door p...

Страница 11: ...C allows you the pilot to devote more time to navigation traffic sur veillance and communications LANDING GEAR The tricycle landing gear allows maximum taxi vision and ground maneuvering Hydraulic dis...

Страница 12: ...lla S4LN 200 S e r i e PROPELLER TYPE Constant speed hydraulically controlled propeller with a single acting governor Model Hartzell H C C Y K 1B 7666 A 2 Diameter 74 IN Blade Angle 30 IN STA Low 130...

Страница 13: ...l Capacity 6 QTS MIN for flight 8 QTS WEIGHT LOADING Gross Weight 2575 LBS Approximate Einpty Weight with standard equipment 1525 LBS Useful Load 1050 LBS Wing Loading Gross Weight 15 1 PSF Power Load...

Страница 14: ...FIGURE 1 1 DIMENSIONED THREE VIEW 1 6...

Страница 15: ...L 2 9 TRIM CONTROLS 2 10 WING FLAP CONTROLS 2 10 LANDING GEAR ELECTRIC GEAR RETRACTION SYSTEM 2 11 EMERGENCY GEAR EXTENSION SYSTEM 2 12 BRAKE STEERING SYSTEMS 2 12 ELECTRICAL POWER ALTERNATOR BATTERY...

Страница 16: ...nt operating technique This Sys tems Operations section describes location function and operation of systems controls and equipment It i s ad visable for you the pilot to familiarize yourself with all...

Страница 17: ...lever to its maximum aft travel position closes the idle cutoff valve shutting down the engine Precise mixture settings may be esta blished by observing the optional EGT gage while adjusting the mixtu...

Страница 18: ...aust Gas 43 Temperature Gage 44 Circuit Breaker Panel 45 Tachometer 46 Cigar Lighter 47 Not Used 48 Carburetor Heat Control 49 Flap Contr01 Switch Mixture Control Quadrant Friction Control Parking Bra...

Страница 19: ...n key clockwise through R L and BOTH to the START MAG position and then pushing for ward on the key and receptacle engages the starter Re leasing the key when the engine starts allows the switch to re...

Страница 20: ...rflow ventilation OIL SYSTEM The engine has a full pressure wet sump oil system with an 8 quart capacity The automatic bypass control valve routes oil flow around the oil cooler when operating tem per...

Страница 21: ...flight panel directly in front of the pilot s seat Optional gyro instruments may be installed in the standard T grouping with the attitude gyro at top center and the directional gyro immediately below...

Страница 22: ...nel A stall warning horn mounted in the cabin head liner and triggered by a sensing vane on the left wing leading edge will sound when airspeed drops t o near stall speed The sound becomes steady a s...

Страница 23: ...the air craft i s trimmed properly However without the installation of a magnetic heading lock P C will not maintain an absolute preselected heading The system is a pneumatically operated two axis au...

Страница 24: ...he aircraft P C must be monitored for proper functioning TRIM CONTROLS For pitch trim control the entire empennage pivots on the tail cone attachment points to increase or decrease the horizontal stab...

Страница 25: ...a red IN TRANSIT light and a warning horn provide visual and audible gear position signals The green light GEAR DN shows continuously when the gear i s fully extended Both lights a r e out when the ge...

Страница 26: ...parking brake control on the console sets the brakes f a x parking Pushing the parking brake control forward releases the brakes It is inadvisable to set the parking brake when the brakes a r e overh...

Страница 27: ...s steadily when voltage regulator output exceeds voltage limits It flashes when the voltage is low CIRCUIT BREAKERS Push to reset push pull or rocker switch circuit breakers protect all of the electr...

Страница 28: ...1 11 OT OW INSTl lJh1EN1 S I C TITIGGEIT 8 TUIIN COOI rl VACUUhl WAftNING INSTRUMENT LTS LEFT INSTRUMENT LTS RIGlfT FUEL BOOS I PUMP PITOT HEAT STRODE 1 IC HT ROTATING BLACON OPT RADIO MASTFII NAV I O...

Страница 29: ...sh pull circuit breaker furnishes an emergency break in the alternator field excitation circuit in the event of alternator or voltage regulator malfunction If the regulator output voltage exceeds limi...

Страница 30: ...lsity CABIN LIGHTING An ad ust lble eyetx111 dome light illuminates the c aI it ancl also serves n s a bacliup i o lightfor illuminating the instrume t anel its OV OFF DIM switch i s slight ly forward...

Страница 31: ...beled CABlN VENT and setting the cabin heat control turns on cabin heat To lower cabin temperature the cabin heat control i s pushed toward the OFF j osition Conlpletely closing the cabin heat control...

Страница 32: ...k to the desired position Safety belts if worn properly keep occupants firmly in their seats in rough air and during maneuvers These belts a r e mechanically simple nuct conlfortal le to wear They a r...

Страница 33: ...Flooded Engine Clearing 3 8 Cold Weather Starting 3 9 Hand Cranking 3 9 WARMUP TAXILNG 3 9 BEFORE TAKEOFF CHECK 3 11 FLIGHT OPERATIONS TAKEOFF a 3 12 C L m B 3 13 CRUISE 3 15 STALLS 3 17 SPINS 3 18 PO...

Страница 34: ...making exceptions when cir cumstances require a deviation in operating procedure GROUND OPERATIONS PREFLIGHT In addition to completing the preflight check visually in spect all of the airwaft exterior...

Страница 35: ...n Switch OFF Master Switch ON to check outside lights then OFF Fuel Selector Drain Selector handle on R pull ring and hold for five seconcls Repeat pr ocedure with selector handle on L 2 Instrument St...

Страница 36: ...d Tiedown REMOVE Left Main Gear Shock Discs and Tire CHECK Fuel Tank Sump Drain SAMPLE Pitot System Drain CHECK Tank Vent UNOBSTRUCTED Fuel Selector Drain Valve C LOSED Windshields C LEAN Left Side En...

Страница 37: ...aft close and latch the door Be sure all baggage i s secure and that all necessary charts computers and other loose items a r e aboard and securely stowed s o that they will not be thrown about the ca...

Страница 38: ...to direct the propel ler blast to an open area before running up the engine To prevent prcpeller damage keep engine RPM low when operating on loose gravel The engine will require some priming for smo...

Страница 39: ...nd depel 3 on the forward speed of i f tincraft to maintain j3 percooling Particular egre i s necessary therefore hen operating the engine o i l the ground To help prei s overheating always I C the ai...

Страница 40: ...system is functioning prop erly Heated carburetor a i r does not pass through the air filter consequently dust dirt and foreign substances can be drawn into the engine to cause accelerated cylinder a...

Страница 41: ...nded WARMUP TAXIING Allow the engine to warmup at 1000 to 1200 RPM normally taxiing will sufficiently warm the engine The engine i s warm enough for takeoff when it will develop full RPM and when the...

Страница 42: ...fore runup head the aircraft into the wind and center the nose wheel It i s always a good practice to stop the airplane with the nose wheel centered since running up the engine or starting to taxi wit...

Страница 43: ...ion 4 Directional Gyro SET to magnetic compass 5 Flight Instruments CHECK 6 Engine Instruments CHECK 7 Clock SET and wind as needed 8 Stabilizer Trim SET for TAKEOFF 9 Propeller CYCLE and CHECK at 170...

Страница 44: ...ine roughness or loss of power may result from over richness In such a case ad just mixture control only enough to obtain smooth operation not for economy Observe instruments for temperature rise FLIG...

Страница 45: ...nd to correct for drift Retract the landing gear only when safely airborne and in good control Retract the flaps when the aircraft has cleared all obstacles and has gained an indicated air speed of ab...

Страница 46: ...f ice in the induc tion system will be reflected by a drop in manifold pressure When an unaccountable loss of manifold pressure i s noted apply full carburetor heat and open the throttle to the limit...

Страница 47: ...ircraft not equipped with an EGT gage Leaning a bove 75 percent power may cause detonation and engine damage unless exhaust gas temperature is maintained 200 F below peak EGT on the rich side Monitor...

Страница 48: ...and starts to decrease Then enrich the mixture by pushing the control lever forward until t h e temperature drops 25 F one mark on the gage froin peak temperature For best power maximum airspeed below...

Страница 49: ...The stall characteristics of the airplane a r e conventional and rapid recovery from a stall i s affected by releasing elevator back pressure and applying power Power off stall speeds at various bank...

Страница 50: ...conventional with release of elevator back pressure and the addition of power Holding the aircraft in a stall with the control wheel fully aft may result in a roll to one side or the other unless prec...

Страница 51: ...one additional turn after antispin controls a r e fully applied WARNING Up t o 2000 feet of altitude may be lost in a one turn spin and recovery therefore stalls at low altitude a r e extremely critic...

Страница 52: ...n margin of safety i s designed to provide adequate controllability when recovery from a stall is tlelayecl The one tiu n margin of safety 1 s col arclized if tlie airplane is not recovered when the l...

Страница 53: ...one hour then switch to the other tank and note the time Use all the fuel from the second tank The relnain illg fuel endurance in the first tank can be calculatecl from the time it took to deplete th...

Страница 54: ...lean niixtur e LETDOWN Plan your letdown well in advance of estimated landing time Generally a power on descent i s most desirable A gradual rate of descent at cruising speed perlnits power settings s...

Страница 55: ...ANDING CHECK 1 Seat Belts FASTENED 2 Fuel Selector Handle SET for fuller tank 3 Electric Fuel Pump ON 5 Carburetor Heat FULL ON 6 Airspeed REDUCE to 120 MPH 104 Knots 7 Propeller FULL INCREASE 8 Landi...

Страница 56: ...evail or when landing crosswind approach at a higher airspeed Slowly relax back pressure and gently lower the nose wheel to the run way after main gear contact so the nose gear steering system can be...

Страница 57: ...kid the main wheels a s doing s o will reduce braking effectiveness and damage the tires AFTER LANDING 1 Electrical Fuel Pump OFF 2 Carburetor Heat OFF 3 Wing Flaps RETRACT 4 Stabilizer Trim TAKEOFF 5...

Страница 58: ...O O N E V PERATORS MANUAL 10 Master Switch OFF yo 11 Control Wheel LOCK with seat belt 12 Overhead Air Scoop CLOSED 13 Wheel Chocks and Tiedown As required...

Страница 59: ...S M0014EY MODEL 1 1 12 0 C RANGEF MOONEY A I R C R A F T COPPORATION SERIAL NO REGISTRATION NO This Manual Must Be Kept Onboard The Airplane At All Times C H I E F E N G I N E E R I N G FIANUFACTURING...

Страница 60: ...FAA APPROVED MOONEY M2OC LOG OF REVISIONS LETTER PAGE DATE APPROVED...

Страница 61: ...Extended Speed 120 MPH 104 Knots CAS Max Flap Operating Speed 125 MPH 109 Knots CAS AIRSPEED INSTRUMENT MARKINGS Radial Red Line 200 MPH 174 Knots CAS Denotes never exceed speed which i s the maxi mum...

Страница 62: ...Red Line Rated 2700 RPM Green Arc Narrow Itateci operating range 2300 2700 IiPlll Green Arc Wide Recommended oper ting range 2300 2500 IIPM IZecl Arc Wide No continuous operation in this range 2000 2...

Страница 63: ...AND MARKINGS Vacuum Warning Lights HI Light 5 00 IN Hg LO Light 4 25 IN Hg Illumination of a HI or LO vacuum annunciator light indicates that the vacuum system has n alfunctionecl The following equipm...

Страница 64: ...st be operated a s a normal category airplane Acrobatic maneuvers including spins a r e unauthorized NOTE Maneuvers involving approach to stal ling angle or full application of elevator rud der or ail...

Страница 65: ...c direction indicator mag compass Tachomete r Manifold pressure gage Oil pressure gage Oil temperature gage Cylinder head temperature gage Fuel quantity gage for each tank Fuel pressure gage Landing g...

Страница 66: ...equipment appropriate to the ground facil ities to be used NOTE Caution should be exercised when in stalled communications equipment interrupts the navigation signal during transmissions OPERATING PR...

Страница 67: ...t then steady tone warns of approaching stall A horn emitting an intermittent tone warns of a re tracted landing gear when power i s reduced below 12 IN Hg manifold pressure All warning devices a r e...

Страница 68: ...oading schedule WARNING See Weight Balance Record for loading schedule The front seat positions can adversely affect CG limi tations at the most rearward loading Allowable bag gage weight may be dicta...

Страница 69: ...FAA APPROVED SECTION V EMERGENCY OPERATION AND PROCEDURES MOONEY IvlODEL M 2 0 C RANGER MOONEY A I R C R A F T CORPORATION...

Страница 70: ......

Страница 71: ...tend the landing gear 1 Pull landing gear actuator circuit breaker to OFF position 2 Place gear switch in DOWN position 3 Push handci ank engage lever forward to engage drive mechanism 4 Crank handcra...

Страница 72: ...ually restore an overloaded circuit If after allow ing the circuit breaker to cool pressing the button a second time does not reactivate the circuit the alternator circuit breaker must remain open and...

Страница 73: ...SECTION VI PERFORMANCE TAKEOFF DISTANCE 6 3 LANDINGDISTANCE 6 4 CLIMBPERFORMANCE 6 5 AIRSPEED CORRECTIONS 6 6 STALLSPEEDS 6 6 ALTITUDE CONVERSION 6 7 CRUISE RANGE 6 8...

Страница 74: ...ge pi loting techniques Note that the cruise performance data pages 6 8 thru 6 14 makes no allowance for wind and nav igation errors All performance charts and graphs are based on operation with no wi...

Страница 75: ...DISTANCE OVER 50 FOOT OBSTACLE 5000 TAKEOFF CONDITIONS WING FLAPS TAKEOFF POSITION HARD SURFACE RUNWAY POWER 2700 RPM MAX MANIFOLD PRESSURE ZERO WEND 41 0 900 740 660 540 1560 1280 1340 1000 960 715 2...

Страница 76: ...LANDING DISTANCE OVER 50 FOOT OBSTACLE WING FLAPS FULL DOWN APPROACH IAS 80 MPH 69 KTS GLIDE RANGE...

Страница 77: ...CLIMB PERFORMANCE 1 GEAR UP 3 FULL RICH MIXTURE...

Страница 78: ...i i l i c t s Airspeed inclic tursmay Ilnve e r r o r s u p to 2 5 MPII 2 2 Knots S T A L L S P E E D S POWER OFF GEAR DOWN GEAR DOWN 1 KNOTS 49 53 60 78 CONDITIONS 1 GROSS WEIGHT 3 IAS IN MPH KTS 2 P...

Страница 79: ...ALTITUDE CONVERSION TAS CAS X Example If ambient temperature is 80 F and pressure altitude is 4000 feet standard altitude is 6000 feet and the factor I is 1 093 TEMPERATURE...

Страница 80: ...of usable fuel standard atmosphere and no wind Talte off weight i s 2575 pounds or 2200pounds 2 The data is taken from flight tests at full rich mixture setting above 75 percent rated power and at a...

Страница 81: ...CRUISE RANGE AT SEA LEVEL 59 F...

Страница 82: ...CRUISE RANGE AT 2500 FT 50 F...

Страница 83: ...CRUISE RANGE AT 5000 FT 41 F...

Страница 84: ...CRUISE RANGE AT 7 500 FT 32 F...

Страница 85: ...CRUISE RANGE AT 10 000 FT 23 F...

Страница 86: ......

Страница 87: ...NG GROUND HANDLING TOWING 7 3 TIEDOWN 7 3 C SERVICING REFUELING 7 4 ENGINE LUBRICATION 7 6 GEAR TIRE SERVICE 7 8 BATTERY SERVICE 7 8 MAINTENANCE PROPELLERCARE 7 9 EXTERIOR CARE 7 9 INTERIOR CARE 7 10...

Страница 88: ...inspection by an ap propriately rated mechanic i s required if the aircraft is flown for hire YAA Regulations also state that the owner or operator of an aircraft i s primarily responsible for main ta...

Страница 89: ...e 7 1 shows the tow bar attached to the nose gear for manual ground maneuvering When using the tow bar never ex ceed the maximum nose gear turning angle indicated on the nose wheel turn indicator Towi...

Страница 90: ...irplane facing the wind 2 Fasten the co pilot seat belt through the flight control wheel 3 Fasten strong ground anchored chain or rope to the in stalled wing tiedown eyebolts and place wheel chocks fo...

Страница 91: ...first flight of the day and after each refueling to check for water or sediment contamination WARNING Allow five minutes after refueling for water and sediment to settle in the tanli and fuel selector...

Страница 92: ...ontrol for about five seconds Re peat the procedure for the right tank being sure that the fuel drain control lu ob is returned to the closed position and that the drain valve i s not leaking ENGINE L...

Страница 93: ...ob served 1 Change the oil againafter not more than five hours of 2 Check all oil screens for evidence of sludge or plugging Change the oil every 10 hours if sludge conditions pre vail Change the oil...

Страница 94: ...nts free of mud and ice to avert retraction interference and binding The gear warning horn may be checked in flight by retard ing the throttle with the gear up The gear horn should sound with a regula...

Страница 95: ...ller blades a r e subjected a makes their careful inspection and maintenance vitally im portant Check the blades for nicks cracks or indications of other damage before each flight Nicks tend to cause...

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