Mooney M20TN S type Pilot Operating Handbook Download

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MOONEY

M20TN - MODEL TYPE-S

SECTION III

EMERGENCY PROCEDURES

3 -- 19

AIRPLANE FLIGHT MANUAL

ORIGINAL ISSUE -- 04-02-2008

The following systems on the non-essential bus will be unpowered:

Com 2

Nav 2 / GPS 2

All lighting on the Overhead Panel

Fuel Pumps

Autopilot

Electric Trim

Landing Gear Motor and Indicators

Defrost Blower

WX Stormscope

ADF/DME/DATA LINK

TRAFFIC ALERT

SKYWATCH

5. TERMINATE FLIGHT AS SOON AS PRACTICABLE.

On approach, the pilot may engage the “BAT” circuit breaker to reestablish power to all sys-

tems if necessary.

If using battery power only and the primary battery has been depleted (minimum of 18 VDC),

the pilot may select the alternate battery using the main battery selection switch. There will

be no change in available equipment when changing battery sources. All equipment pow-

ered previously will remain powered

AVIONICS EMERGENCIES

PFD OR MFD DISPLAY FAILURE

DISPLAY BACKUP button on audio panel

PUSH

. . . . .

AHRS FAILURE

NOTE:

Failure of the Attitude and Heading Reference System (AHRS) is indicated by a

removal of the sky/ground presentation and a red X and a yellow “AHRS FAIL-

URE” shown on the PFD. The digital heading presentation will be replaced with a

yellow “HDG” and the compass rose digits will be removed. The course pointer

will indicate straight up and course may be set using the digital window.

Use Standby Attitude Indicator and Magnetic compass.

Course Set using digital window

3. LAND AS SOON AS PRACTICABLE.

AIR DATA COMPUTER (ADC) FAILURE

NOTE:

Complete loss of the Air Data Computer is indicated by a red X and yellow text

over the airspeed, altimeter, vertical speed, TAS and OAT displays. Some FMS

functions, such as true airspeed and wind calculations, will also be lost.

Use Standby Airspeed Indicator and Altimeter

2. LAND AS SOON AS PRACTICABLE

at a suitable airport

Summary of Contents for M20TN S type

Page 1: ...901 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road Kerrville Texas 78028 tel 830 896 6000 www mooney com ORIGINAL ISSUE 04 02 2008 Copyright 2015 All Rights Reserved AND FAA APPROVED AIRPLANE FLIGHT MANUAL MODEL TYPE S REVISION C 02 10 2015 ...

Page 2: ...M20TN PILOT S OPERATING HANDBOOK P N POH 003901 MOONEY INTERNATIONAL CORPORATION and FAA APPROVED AIRPLANE FLIGHT MANUAL MODEL TYPE S ...

Page 3: ...THIS AIRCRAFT IS CERTIFIED TO USE 100LL BLUE OR 100 130 GREEN AVIATION GASOLINE ONLY IT IS THE PILOT S RESPONSIBILITY TO INSURE THAT THE PROPER FUEL IS USED AT EACH REFUELING CAUTION ...

Page 4: ......

Page 5: ...AA APPROVED FOR Michele M Owsley Manager Airplane Certification Office FEDERAL AVIATION ADMINISTRATION 2601 Meacham Boulevard Fort Worth Texas 76137 0150 DATE 04 02 2008 FAA APPROVED in Normal Category based on CAR PART 3 applicable portions of FAR PART 23 and when applicable components are installed in accordance with Mooney Drawing 110080 applicable to Model M20TN TYPE S S N listed above only Th...

Page 6: ...MOONEY M20TN BLANK ...

Page 7: ...o use the manual as a reference Your cooperation in reporting presenta tion and content recommendations is solicited REVISING THE MANUAL The i pages of this manual contain a List of Effective Pages containing a complete current listing of all pages i e Original or Revised Also in the lower right corner of the outlined portion is a box which denotes the manual number and issue or revision of the ma...

Page 8: ...MOONEY M20TN MODEL TYPE S INTRODUCTION BLANK ...

Page 9: ...15 ix 02 12 2015 x 02 12 2015 xi 02 12 2015 xii 02 12 2015 1 1 02 12 2015 1 2 ORIGINAL ISSUE 1 3 ORIGINAL ISSUE 1 4 11 21 2014 1 5 11 21 2014 1 6 ORIGINAL ISSUE 1 7 ORIGINAL ISSUE 1 8 ORIGINAL ISSUE 1 9 ORIGINAL ISSUE 1 10 ORIGINAL ISSUE 1 11 ORIGINAL ISSUE 1 12 ORIGINAL ISSUE 1 13 ORIGINAL ISSUE 1 14 ORIGINAL ISSUE 2 1 02 12 2015 2 2 ORIGINAL ISSUE 2 3 ORIGINAL ISSUE 2 4 02 12 2015 2 5 02 12 2015...

Page 10: ...AL ISSUE 3 22 ORIGINAL ISSUE 3 23 ORIGINAL ISSUE 3 24 ORIGINAL ISSUE 4 1 11 21 2014 4 2 ORIGINAL ISSUE 4 3 ORIGINAL ISSUE 4 4 ORIGINAL ISSUE 4 5 ORIGINAL ISSUE 4 6 11 21 2014 4 7 ORIGINAL ISSUE 4 8 ORIGINAL ISSUE 4 9 11 21 2014 4 10 ORIGINAL ISSUE 4 11 ORIGINAL ISSUE 4 12 ORIGINAL ISSUE 4 13 ORIGINAL ISSUE 4 14 ORIGINAL ISSUE 4 15 ORIGINAL ISSUE 4 16 ORIGINAL ISSUE 4 17 ORIGINAL ISSUE 4 18 ORIGINA...

Page 11: ...5 36 ORIGINAL ISSUE 5 37 ORIGINAL ISSUE 5 38 ORIGINAL ISSUE 5 39 ORIGINAL ISSUE 5 40 ORIGINAL ISSUE 5 41 ORIGINAL ISSUE 5 42 ORIGINAL ISSUE 5 43 ORIGINAL ISSUE 5 44 ORIGINAL ISSUE 5 45 ORIGINAL ISSUE 5 46 ORIGINAL ISSUE 5 47 ORIGINAL ISSUE 5 48 ORIGINAL ISSUE 5 49 ORIGINAL ISSUE 5 50 ORIGINAL ISSUE 5 51 ORIGINAL ISSUE 5 52 ORIGINAL ISSUE 5 53 ORIGINAL ISSUE 5 54 11 21 2014 5 55 ORIGINAL ISSUE 5 56...

Page 12: ...17 ORIGINAL ISSUE 6 18 ORIGINAL ISSUE 6 19 ORIGINAL ISSUE 6 20 ORIGINAL ISSUE 6 21 ORIGINAL ISSUE 6 22 ORIGINAL ISSUE 6 23 ORIGINAL ISSUE 6 24 ORIGINAL ISSUE 6 25 ORIGINAL ISSUE 6 26 ORIGINAL ISSUE 6 27 ORIGINAL ISSUE 6 28 11 21 2014 6 29 ORIGINAL ISSUE 6 30 11 21 2014 6 31 02 12 2015 6 32 ORIGINAL ISSUE 7 1 11 21 2014 7 2 11 21 2014 7 3 ORIGINAL ISSUE 7 4 11 21 2014 7 5 ORIGINAL ISSUE 7 6 11 21 2...

Page 13: ...RIGINAL ISSUE 7 38 ORIGINAL ISSUE 8 1 11 21 2014 8 2 ORIGINAL ISSUE 8 3 11 21 2014 8 4 ORIGINAL ISSUE 8 5 ORIGINAL ISSUE 8 6 11 21 2014 8 7 ORIGINAL ISSUE 8 8 ORIGINAL ISSUE 8 9 11 21 2014 8 10 11 21 2014 8 11 ORIGINAL ISSUE 8 12 ORIGINAL ISSUE 9 1 ORIGINAL ISSUE 9 2 ORIGINAL ISSUE 9 3 ORIGINAL ISSUE 9 4 ORIGINAL ISSUE Plus applicable supplements inserted 10 1 ORIGINAL ISSUE 10 2 ORIGINAL ISSUE 10...

Page 14: ...MOONEY INTRODUCTION M20TN MODEL TYPE S vi POH AFM POH 003901 This POH AFM effective with S N 31 0090 thru 31 TBA ORIGINAL ISSUE 04 02 2008 BLANK Revision C 02 12 2015 ...

Page 15: ...008 vii LOG OF REVISIONS REVISION LETTER REVISED PAGES FAA APPROVED DATE ORIGINAL ISSUE ALL 04 02 2008 A Supplement Heater Mod 12 05 2008 B see Narrative Discussion of Revisions Page viii 11 21 2014 C see Narrative Discussion of Revisions Page viii 02 12 2015 Revision C 02 12 2015 ...

Page 16: ... Hours to 2200 Hours B 2 5 Revised Airspeed Indicator Markings B 1 5 2 6 Added Serial Numbers and Engine Designation letter B 2 15 Added Vne 194 Placard to Limitations Section B 2 11 7 6 Revised G1000 software number revision letter B 2 19 2 20 Labelled effectivity B 3 9 3 10 Added Airspeed and Braking B 4 6 Added Master Switch OFF B 4 9 Revised CAUTION for Extreme Cold Weather Engine Starts B 5 1...

Page 17: ...3901 ORIGINAL ISSUE 04 02 2008 ix Rev Level Page Number Comment B 7 34 Revised Figure 7 12 Removed Altitude numbers from M20K B 7 34 Added Note Precise Flight Oxygen System Optional B 7 34 7 35 7 36 Revised to show Avox Oxygen System Revision B 11 21 2015 ...

Page 18: ...ve Discussion of Revisions and how to obtain revisions to this manual C 2 1 6 1 Revised Table of Contents C 2 4 Revised VNE 196 194 to VNE 196 195 Revised VNO 175 175 to VNO 175 174 Revised VLE 166 164 to VLE 166 165 C 2 5 Revised Red White Barber Pole to 195 KIAS is the Maxim um speed for all operations Revised Red Radial to 195 KIAS is the Maximum speed for all operations C 2 15 Added Vne 194 Re...

Page 19: ...04 02 2008 TABLE OF CONTENTS TITLE SECTION GENERAL I LIMITATIONS II EMERGENCY PROCEDURES III NORMAL PROCEDURES IV PERFORMANCE V WEIGHT BALANCE VI AIRPLANE SYSTEM DESCRIPTIONS VII HANDLING SERVICE MAINTENANCE VIII SUPPLEMENTAL DATA IX SAFETY OPERATIONAL TIPS X ...

Page 20: ...MOONEY M20TN MODEL TYPE S INTRODUCTION xii ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 21: ... 7 CABIN ENTRY DIMENSIONS 1 7 BAGGAGE SPACE ENTRY DIMENSIONS 1 7 SPECIFIC LOADINGS 1 7 IDENTIFICATION PLATE 1 8 GARMIN G1000 1 8 SYMBOLS ABBREVIATIONS TERMINOLOGY 1 9 GENERAL AIRSPEED TERMINOLOGY SYMBOLS 1 9 ENGINE POWER TERMINOLOGY 1 9 AIRPLANE PERFORMANCE FLIGHT PLANNING TERMINOLOGY 1 10 ENGINE CONTROLS INSTRUMENTS TERMINOLOGY 1 10 METEOROLOGICAL TERMINOLOGY 1 10 WEIGHT BALANCE TERMINOLOGY 1 11 ...

Page 22: ...MOONEY M20TN MODEL TYPE S SECTION I GENERAL 1 2 ORIGINAL ISSUE 04 02 2008 AIRPLANE FLIGHT MANUAL BLANK ...

Page 23: ...20TN MODEL TYPE S SECTION I GENERAL 1 3 ORIGINAL ISSUE 04 02 2008 AIRPLANE FLIGHT MANUAL 1112 5 cm 279 4 cm 76 193 04 cm 201 9 cm 6 7 1 2 9 2 358 1 cm 11 9 259 1 cm 8 6 36 6 812 8 cm 26 8 FIGURE 1 1 THREE VIEW ...

Page 24: ...f the terminology used in this Operators Manual This Pilot s Operating Handbook is not designed as a substitute for adequate and competent flight instruction knowledge of current airworthiness directives applicable federal air regula tions or advisory circulars It is not intended to be a guide for basic flight instruction or a training manual and should not be used for operational purposes unless ...

Page 25: ...Liters Bore 5 25 In 13 3 cm Stroke 4 25 In 10 8 cm Compression Ratio 7 5 1 Fuel System Type Fuel Injection Make Continental Motors Inc Fuel Aviation Gasoline 100 octane 100LL Accessories Magnetos Bendix S6RSC 25P pressurized Ignition Harness Shielded Braided Spark Plugs AC 273 or equivalent 18 m m Oil Cooler Continental Motors Inc Full Flow Alternator 28 Volt DC 100 AMPS Starter 24 volt DC Interco...

Page 26: ...966 shall be used during the first 25 hours of flight operations However if the engine is flown less than once a week a straight mineral oil with corrosion preventative MIL C 6529 for the first 25 hours is recommended Oil Specification or Oil Grade After 25 Engine Hours Teledyne Continental Motors Specifica tion MHS 24 An ashless dispersant oil shall be used after 25 hours Oil Grades Recommended f...

Page 27: ...r Storage Area 10 Lbs 4 5 Kg Cargo Rear Seats Folded Down 340 Lbs 154 2 Kg STANDARD AIRPLANE WEIGHTS Basic Empty Weight See Page 1 11 Useful Load Varies with installed equipment See SECTION VI for specific airplane weight CABIN AND ENTRY DIMENSIONS Cabin Width Maximum 43 5 In 110 5 cm Cabin Length Maximum 126 In 315 cm Cabin Height Maximum 44 5 In 113 cm Entry Width Minimum 29 0 In 73 4 cm Entry H...

Page 28: ...election of radios for transmitting and listening intercom functions and marker beacon functions The primary function of the VHF Communication portion of the G1000 is to enable external radio communication The primary function of the VOR ILS Receiver portion of the equipment is to receive and demodulate VOR localizer and Glide Slope signals The primary function of the GPS portion of the system is ...

Page 29: ...d or retracted Vne NEVER EXCEED SPEED The speed limit that may not be exceeded at any time Vno MAXIMUM STRUCTURAL CRUISING SPEED The speed that should not be exceeded except in smooth air and then only with caution Vs STALLING SPEED The minimum steady flight speed at which the air plane is controllable Vso STALLING SPEED The minimum steady flight speed at which the air plane is controllable in the...

Page 30: ...evolutions per minute RPM Propeller Governor The device that regulates RPM of the engine propeller by increasing or decreasing the propeller pitch through a pitch change mechanism in the propeller hub METEOROLOGICAL TERMINOLOGY AGL Above ground level Density Altitude Altitude as determined by pressure altitude and existing ambient tempera ture In standard atmosphere ISA density and pressure altitu...

Page 31: ...Chord Maximum Weight The maximum authorized weight of the aircraft and its contents as listed in the aircraft specifications Maximum Landing Weight The maximum authorized weight of the aircraft and its contents when a normal landing is to be made Moment The product of the weight of an item multiplied by its arm Moment divided by a constant is used to simplify balance calculations by reducing the n...

Page 32: ...alents 1 square inch 6 4516 sq centimeters 1 square foot 929 sq centimeters 1 square yard 0 836 sq meter VOLUME OR CAPACITY U S Customary Unit Metric Equivalents 1 cubic inch 16 39 cubic centimeters 1 cubic foot 0 028 cubic meter 1 cubic yard 0 765 cubic meter U S Customary Metric Equivalents Liquid Measure 1 fluid ounce 29 573 milliliters 1 pint 0 473 liter 1 quart 0 946 liter 1 gallon 3 785 lite...

Page 33: ... 27 75 940 28 75 974 9 75 1007 30 70 1040 27 80 941 28 80 975 29 80 1009 30 75 1041 27 85 943 28 85 977 29 85 1011 30 80 1043 27 90 945 28 90 979 29 90 1013 30 85 1045 27 95 946 28 95 980 29 92 1013 30 90 1046 28 00 948 29 00 982 29 95 1014 30 95 1048 28 05 950 29 05 984 30 00 1016 31 00 1050 28 10 952 29 10 985 30 05 1018 31 05 1051 28 15 953 29 15 987 30 10 1019 31 10 1053 28 20 955 29 20 989 30...

Page 34: ...follows is of critical importance and concerns procedures and techniques which could cause or result in personal injury or death if not carefully followed CAUTION The use of the Caution symbol means information which follows is of significant importance and concerns procedures and techniques which could cause or re sult in damage to the airplane and or its equipment if not carefully followed NOTE ...

Page 35: ...LANT INSTRUMENT MARKINGS 2 7 FUEL LIMITATIONS 2 8 WEIGHT LIMITS 2 8 CENTER OF GRAVITY LIMITS GEAR DOWN 2 8 MANEUVER LIMITS 2 9 FLIGHT LOAD FACTOR LIMITS 2 9 FLIGHT CREW 2 9 OPERATING LIMITATIONS 2 9 KINDS OF OPERATION LIMITS 2 9 KINDS OF OPERATION EQUIPMENT LIST 2 10 TYPES OF OPERATION 2 11 GENERAL 2 11 G1000 SYSTEM 2 11 ADVISORY MESSAGES 2 13 DECALS PLACARDS 2 14 CABIN INTERIOR 2 14 CABIN INTERIO...

Page 36: ...MOONEY M20TN MODEL TYPE S SECTION II LIMITATIONS 2 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 37: ...ator Markings chart Figure 2 2 are based on Airspeed Calibration data shown in SECTION V with the normal static source If the alternate static source is being used ample margins should be observed to allow for the air speed calibration variations between the normal and alternate static sources as shown in SECTION V Your Mooney is certificated under FAA Type Certificate No 2A3 as a Mooney M20TN NOI...

Page 38: ...1012 104 103 2430 1102 109 108 3300 1497 127 126 3368 1528 128 127 Do not make full or abrupt control move ment above this speed VFE Maximum Flap Ex tended Speed 111 110 Do not exceed this speed with flaps in full down position VLE Maximum Landing Gear Extended Speed 166 165 Maximum speed at which the aircraft can be safely flown with the landing gear extended VLO EXT Max Speed for Gear Extension ...

Page 39: ...ating range with flaps fully extended Green band 66 KIAS 174 KIAS Normal operating range Yellow band 174 KIAS 195 KIAS Caution range smooth air only Red White barber pole 195 KIAS and greater 195 KIAS is the maximum speed for all operations STANDBY AIRSPEED INDICATOR MARKINGS MARKING IAS SIGNIFICANCE White band 59 KIAS 110 KIAS Operating range with flaps fully extended Green band 66 KIAS 174 KIAS ...

Page 40: ...rature Takeoff 100o F 38o C Recommended Cruising Oil Temperature 170o F 220o F 76 7o C 104 4o C Maximum Manifold Pressure 33 5 Inches of Hg Oil Pressure Normal Operating 30 100 PSI Minimum IDLE ONLY 10 PSI Maximum Allowable Cold Oil 100 PSI Oil Grades Recommended for Various Average Air Temperature Ranges Below 40o F 4o C SAE 30 10W30 15W50 or 20W50 Above 40o F 4o C SAE 50 15W50 or 20W50 Fuel Grad...

Page 41: ...display will change to the color of the prohibited range and will begin flashing as well INDICATION Red arc bar Lower prohibited range Yellow arc bar Caution range Green arc bar Normal operating range Yellow arc bar Caution range Red arc bar Upper prohibited range Engine RPM 2200 2500 2500 Manifold Press In Hg 15 33 5 33 5 Oil Temp oF 100 240 240 Oil Press PSI 10 Idle 10 30 30 100 100 Cold Cyl Hea...

Page 42: ...deteriorating effects within the fuel system Under cer tain conditions of temperature and humidity water can be present in fuel in suffi cient quantities to create ice formations within the fuel system To prevent this add Anhydrous ISOPROPYL Alcohol to the fuel supply in quantities not to exceed 3 of total fuel volume per tank WEIGHT LIMITS Maximum Weight Takeoff 3368 lb 1528 Kg Maximum Weight Lan...

Page 43: ...oxygen in accordance with FAR 23 1441 2 Operate in accordance with FAR 91 211 and 3 Equipped with avionics in accordance with FAR 91 or FAR 135 ALTERNATOR OPERATING LIMITATIONS IS 94 AMPS Above 30 5 inHg of manifold pressure only full rich mixture is permitted At altitudes above 22 000 feet power settings above 2300 RPM must be operated at 1675o F TIT or richer Above 12 000 ft the minimum manifold...

Page 44: ...GEAR POSITION INDICATOR 2 2 2 2 SEAT BELT SHOULDER HARNESS FOR EACH OCCUPANT 3 1 1 1 1 OXYGEN MASK FOR EACH OCCUPANT 4 1 1 1 1 POSITION LIGHTS 3 3 STROBE LIGHTS ANTI COLLISION 3 3 GYRO HORIZON 1 1 LANDING LIGHT 5 1 1 INSTRUMENT LIGHTS INTERNAL or GLARESHIELD 1 1 BATTERIES 2 2 2 2 FUEL BOOST PUMP 1 1 1 1 PILOT S OPERATING HANDBOOK AIRPLANE FLIGHT MANUAL 1 1 1 1 PITOT HEATED 5 1 1 ELT 1 1 1 1 ALTERN...

Page 45: ...2 14 00 GEA1 GIA1 006 B0193 02 2 04 GEA1 GIA2 006 B0193 02 2 04 GIA1 006 B0190 13 2 08 GIA2 006 B0190 13 2 08 GMA1 GIA1 006 B0203 10 2 11 GMA1 GIA2 006 B0203 10 2 11 GMU1 006 B0224 00 2 01 GMU1 FPGA 006 C0048 00 2 00 GPS1 006 B0093 XX 3 01 GPS2 006 B0093 XX 3 01 GRS1 GIA1 006 B0223 02 2 03 GRS1 GIA2 006 B0223 02 2 03 GRS1 FPGA 006 B0049 00 2 00 GTX GIA1 006 B0172 XX 4 02 GTX GIA2 006 B0172 XX 4 02...

Page 46: ...between the top of descent and the way point where the VNAV path terminates in terminal or enroute operations 5 If not previously defined the following default settings must be made in the SYSTEMSETUP menu of the G1000 prior to operation refer to Pilot s Guide for procedure if necessary a DIS SPD n m k t sets navigation units to nautical miles and knots b ALT VS f t fpm sets altitude units to feet...

Page 47: ...TITUDE FAIL Display system is not receiving attitude ref erence information from the AHRS accom panied by the removal of sky ground pre sentation and a red X over the attitude area AIRSPEED FAIL Display system is not receiving airspeed in put from the air data computer accompa nied by a red X through the airspeed dis play ALTITUDE FAIL Display system is not receiving airspeed in put from the air d...

Page 48: ...LIGHTNING DETECTION EQUIPMENT NOT TO BE USED FOR THUNDERSTORM AREA PENETRATION 150056 X 1004 Y 150056 X 1012 Y 150056 X 1010 Y 150056 X 1007 Y 150056 X 1008 Y 150056 X 3017 Y OPTIONAL PULL FOR ALTERNATE STATIC SOURCE L A N D I N G G E A R GEAR NOT EXTENDED GEAR UP 106 KIAS PUSH GEAR SAFETY GEAR DOWN 140 KIAS GEAR EXTD 165 KIAS BYPASS MIC 150056 X 1009 Y 150056 X 3038 150085 038 OPTIONAL 150056 303...

Page 49: ...HEN OPERATING THIS AIRPLANE IN THE NORMAL CATEGORY THIS AIRPLANE IS CERTIFIED FOR DAY AND NIGHT VFR IFR OPERATION WHEN THE REQUIRED EQUIPMENT IS INSTALLED AND OPERATIONAL FLIGHT INTO KNOWN ICING CONDITIONS IS PROHIBITED NO AEROBATIC MANEUVERS INCLUDING SPINS ARE APPROVED OTHER OPERATING LIMITATIONS WHICH MUST BE COMPLIED WITH WHEN OPERATING THIS AIRPLANE IN THIS CATEGORY ARE CONTAINED IN THE AIRPL...

Page 50: ...IN 3 ACTUATE HANDLE TO CLOSE 1 STORE HANDLE 2 INSERT LOCK PIN 3 INSTALL COVER 4 CLOSE AND LATCH DOOR USING OUTSIDE HANDLE 5 LOCK DOOR 150056 X 1045 Y ABOVE INSIDE BAGGAGE DOOR HANDLE OXY OH OPTIONAL AROUND EACH OXYGEN OUTLET ON OVERHEAD PANEL LIGHT SWITCH 150056 X 1043 Y BAGGAGE DOOR FRAME GEAR DOWN 150056 X 1015 Y FLOORBOARD BETWEEN SEATS FUEL DRAIN PULL OPEN 150056 X 1036 Y FLOORBOARD FWD OF CO ...

Page 51: ...LE 150056 X 1044 Y BAGGAGE COMPARTMENT ON HAT RACK SHELF WARNING DO NOT EXCEED 120 LBS SEE AIRCRAFT LOADING SCHEDULE DATA FOR BAGGAGE COMPARTMENT ALLOWABLE 150056 X 1046 Y TOP OF BAGGAGE 54 4 Kg IN THIS COMPARTMENT DOOR JAMB PUSH TO RELEASE 150056 X 1040 Y BETWEEN SEATS ON EMERGENCY GEAR RELEASE EXTENSION HANDLE ON RADIO PANEL ADJACENT TO ELT SWITCH CAUTION ABSENCE OF ELT LIGHT DURING FIRST 3 SECO...

Page 52: ...orporation M20TN IPC or call Mooney Service Parts Dept MAINTAIN LEVEL HERE 150056 X 2016 Y HYDRAULIC OIL RESERVOIR 28 VOLTS ONLY 150056 X 2023 Y BACKSIDE OF AUX PWR RECEPTACLE DOOR USE AVIATORS OXYGEN ONLY SEE PILOT S OPERATING HANDBOOK FOR FILLING PRESSURES 150056 X 2018 Y INSIDE OXYGEN FILLER DOOR ENGINE OIL OIL INSTALLED IN THIS ENGINE IS NEXT OIL CHANGE DUE AT HRS USE GREASE PENCIL TACH TIME 1...

Page 53: ...Y UNDERSIDE OF WINGS 2 PLCS AFT OF L H COWL FLAP 1 PLC 150056 X 2019 Y HORIZ STAB L E RUDDER T E BOTH SIDES 150056 X 2014 Y UNDER TAILCONE AFT OF WING T E 150056 X 2011 Y UNDER LEFT WING L E NEAR FUSELAGE 150056 X 2013 Y UNDER WING NEAR SUMP DRAINS 150056 X 2010 Y UNDER FUSELAGE RT SIDE AFT OF NOSE WHEEL WELL TIRE PRESSURE 42 PSI 2 95 Kg cm 2 ON MAIN LANDING GEAR DOOR 150056 X 2005 Y TIRE PRESSURE...

Page 54: ...LANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE 04 02 2008 150056 2007 TOP LEFT RIGHT WINGS AT FUEL FILLERS TOP LEFT RIGHT WINGS AT FUEL FILLERS 150056 X 4002 Y 150056 X 2025 Y UNDER WING NEAR SUMP DRAINS Effective with S N 31 0080 and ON Revision B 11 21 2014 ...

Page 55: ...IMARY ENGINE INDUCTION AIR SYSTEM BLOCKAGE 3 10 TURBOCHARGER FAILURE 3 11 TURBOCHARGER OVERBOOST 3 12 ENGINE ROUGHNESS 3 12 HIGH CYLINDER HEAD TEMPERATURE 3 12 HIGH OIL TEMPERATURE 3 12 LOSS OF OIL PRESSURE 3 13 ENGINE DRIVEN FUEL PUMP FAILURE 3 13 FUEL VAPOR SUPPRESSION FLUCTUATING FUEL FLOW 3 13 FIRES 3 14 ENGINE FIRE ON GROUND DURING STARTUP 3 14 ENGINE FIRE IN FLIGHT 3 14 ELECTRICAL FIRE IN FL...

Page 56: ...FAILURE OF LANDING GEAR TO RETRACT 3 21 GEAR FAILS TO RETRACT GEAR WARNING VOICE ALERT SOUNDING 3 21 WHEN READY TO EXTEND LANDING GEAR 3 21 GEAR FAILS TO RETRACT GEAR WARNING VOICE ALERT DOES NOT SOUND 3 21 WHEN READY TO EXTEND LANDING GEAR AT NEXT LANDING 3 21 OXYGEN 3 21 ALTERNATE STATIC SOURCE 3 21 UNLATCHED DOORS IN FLIGHT 3 22 CABIN DOOR 3 22 BAGGAGE DOOR 3 22 ICING 3 22 INADVERTENT ICING ENC...

Page 57: ...ion of your airplane As it is not possible to have a procedure for all types of emergencies that may occur it is the pilot s responsibility to use sound judgement based on experience and knowledge of the aircraft to determine the best course of action Therefore it is considered mandatory that the pilot read the entire manual especially this section before flight When applicable emergency procedure...

Page 58: ...0 0 KIAS MANEUVERING SPEED 3368 lb 1528 kg 127 KIAS 3300 lb 1497 kg 126 KIAS 2430 lb 1102 kg 108 KIAS 2232 lb 1012 kg 103 KIAS PRECAUTIONARY LANDING WITH ENGINE POWER Flaps DOWN 75 KIAS PRECAUTIONARY LANDING ABOVE 3200 LBS Flaps DOWN 80 KIAS EMERGENCY DESCENT GEAR UP Smooth Air 194 KIAS Turbulent Air 3368 lb 1528 kg 127 KIAS 3300 lb 1497 kg 126 KIAS 2430 lb 1102 kg 108 KIAS 2232 lb 1012 kg 103 KIA...

Page 59: ...RAKE AMBER light indicates Speed Brakes are activated ALT AIR AMBER light indicates alternate induction air door is open PITOT HEAT BLUE light indicates power is applied to heater Some Foreign A C AMBER light indicates power is NOT applied to heater ALT VOLTS Flashing RED light indicates alternator output low Refer to ALTERNATOR OUTPUT LOW ALT VOLTS Steady RED light indicates over voltage and Alt ...

Page 60: ...hat the pilot initiate the missed ap proach upon receipt of this message from the G1000 Navigation guidance will continue for 5 minutes allowing the pilot to initiate the missed approach while maintaining course guidance on the final approach course Then the system will flag and no longer provide course guidance with approach sensitivity Missed approach course guidance may still be available with ...

Page 61: ...edures are important During the descent and approach to landing phases of the flight DO NOT set the mixture too rich as prescribed in the normal landing procedures and avoid closing the throttle completely If a balked landing is nec essary coordinate the simultaneous application of throttle and mixture ENGINE POWER LOSS IN FLIGHT Above 400 Feet AGL Airspeed 85 KIAS Flaps UP 80 KIAS Flaps DOWN Fuel...

Page 62: ...otors specifications the Model TSIO 550 series engine is NOT APPROVED for continuous negative or zero g operation and operation in that environment is prohibited Depending on the loading and amount of time encountered more than normally encountered in gusts the engine may quit due to low oil pressure Upon return to positive loading the engine will normally restart on its own but may require some l...

Page 63: ...ible over rich conditions S Very low power settings at high altitude and rich mixture S Very low power settings with the fuel boost on and rich mixture S Severe induction system blockage leakage or turbo failure and rich mixture Possible over lean conditions S Advancing the throttle or prop from a lean condition before richening S HIGH Fuel boost switched off from a lean condition before richening...

Page 64: ... OFF LOW Boost Pump Verify OFF Braking AS REQUIRED TO STOP AIRCRAFT NOTE If fire is not extinguished attempt to increase airflow over engine by increasing glide speed Proceed with FORCED LANDING EMERGENCY DO NOT attempt an engine restart If necessary use fire extinguisher to keep fire out of cabin area POWER LOSS PRIMARY ENGINE INDUCTION AIR SYSTEM BLOCKAGE Blockage of the primary engine induction...

Page 65: ...kg 89 0 KIAS 2900 lb 1315 kg 84 5 KIAS 2600 lb 1179 kg 80 0 KIAS Alternate Air Manually OPEN LOW Boost Pump ON Throttle SET TO HALF OPEN Propeller FULL FORWARD Mixture PULL TO CUTOFF THEN GRADUALLY RICHEN UNTIL ENGINE STARTS Magneto Starter Switch Verify on BOTH After engine re start Throttle ADJUST as required Propeller ADJUST as required Mixture RELEAN as required for power setting Refer to powe...

Page 66: ...E as required to keep manifold pressure within limits ENGINE ROUGHNESS Engine instruments CHECK Fuel Selector OTHER TANK Mixture READJUST for smooth operation Magneto Starter Switch Select R or L or BOTH If roughness disappears on single magneto monitor power and continue on selected magneto WARNING The engine may quit completely when one magneto is switched off if the other magneto is faulty If t...

Page 67: ...te with HIGH BOOST pump ON Operation of engine with a failed engine driven fuel pump and auxiliary fuel pump HIGH BOOST ON will require smooth operation of engine controls and corresponding mixture change when throttle is repositioned or engine speed is changed When retarding throttle or reducing engine speed adjust mixture to prevent engine power loss from an overrich condition Enrich mixture whe...

Page 68: ... Extinguisher ENGINE FIRE IN FLIGHT Fuel Selector Valve OFF Throttle CLOSED Mixture IDLE CUT OFF Magneto Starter Switch OFF Cabin Ventilation Heating Controls CLOSED ELECTRICAL FIRE IN FLIGHT Smoke in Cabin If electrical power is essential for the flight attempt to isolate the faulty circuit Cabin Ventilation OPEN Heating Controls CLOSED Circuit Breakers CHECK to identify faulty circuit if possibl...

Page 69: ...er minute can be obtained in two different configurations 1 With landing gear and flaps retracted an airspeed of 194 KIAS will be required for maximum rate of descent 2 With the landing gear extended and flaps retracted an airspeed of 164 KIAS will also give approximately the same rate of descent At 164 KIAS and the gear extended the angle of descent will be greater thus resulting in less horizont...

Page 70: ...SPEED Weight 3368 1528 3200 1452 2900 1315 2600 1179 IAS Kts 91 5 89 0 84 5 80 0 LBS Kg M GLIDE 0 10 20 30 40 50 60 70 80 90 100 110 GROUND DISTANCE KILOMETERS 22000 24000 NOTE Greater glide distances can be attained by moving the propeller control FULL AFT LOW RPM FORCED LANDING EMERGENCY GEAR RETRACTED OR EXTENDED Emergency Locator Transmitter ARMED Seat Belts Shoulder Harnesses SECURE Cabin Doo...

Page 71: ... to determine continued airwor thiness requirements post flight ALTERNATOR OVERVOLTAGE Alternator warning light illuminated steady and Alternator Field circuit breaker tripped Alternator Field Circuit Breaker RESET If circuit breaker will not reset the following procedures are required 1 Reduce electrical load as required to maintain essential systems 2 Continue flight and LAND when PRACTICABLE to...

Page 72: ...ill remain powered and functional 3 If the RED ALT VOLTS annunciator remains flashing then CAUTION If the RED ALT VOLTS annunciation remains flashing then the standby alterna tor has failed and only main battery power remains 4 Reduce the electrical load by pulling the BAT circuit breaker This load sheds the non es sential bus The following systems remain powered by the essential bus CAUTION If th...

Page 73: ...ment pow ered previously will remain powered AVIONICS EMERGENCIES PFD OR MFD DISPLAY FAILURE 1 DISPLAY BACKUP button on audio panel PUSH AHRS FAILURE NOTE Failure of the Attitude and Heading Reference System AHRS is indicated by a removal of the sky ground presentation and a red X and a yellow AHRS FAIL URE shown on the PFD The digital heading presentation will be replaced with a yellow HDG and th...

Page 74: ...es contained in this AFMS 2 If a display indicates an abnormal condition but no annunciator is present use other system information such as engine displays fuel quantity and flow to determine if the condition ex ists If it cannot be determined that the condition does not exist treat the situation as if the condition exists Refer to the POH AFM Emergency or Abnormal procedures or the proce dures co...

Page 75: ...n floor Verify LATCHED in proper position GEAR ACTUATOR C B RESET Gear should retract if C B was tripped FLIGHT CONTINUE if desired WHEN READY TO EXTEND LANDING GEAR AT NEXT LANDING AIRSPEED Below 140 KIAS GEAR SWITCH DOWN Position If gear will not extend electrically at this time refer to FAILURE OF LANDING GEAR TO EX TEND ELECTRICALLY previous page OXYGEN In the event of oxygen loss above 12 500...

Page 76: ...e position depending upon speed of aircraft There will be considerable wind noise loose objects in the vicinity of the open door may exit the aircraft There is no way to shut and latch door from the inside Aircraft flight characteristics will not be affected fly aircraft in normal manner LAND AS SOON AS POSSIBLE and secure baggage door Baggage Door latching mechanism VERIFY MECHANISM PROPERLY ENGA...

Page 77: ...e and climb performance and higher stall speeds Plan for higher approach speeds requiring higher power settings and longer landing rolls CAUTION Stall warning system may be inoperative NOTE The defroster may not clear ice from windshield If necessary open pilot s storm window for visibility in landing approach and touchdown With ice accumulations of 1 inch or less use no more than 10o wing flaps f...

Page 78: ...ucive to spin entry Low speed flight near stall should be approached with caution and exces sive flight control movements in this flight regime should be avoided Should an unintentional stall occur the aircraft should not be allowed to progress into a deep stall Fast but smooth stall recovery will minimize the risk of progressing into a spin If an unusual post stall attitude develops and results i...

Page 79: ...E START 4 9 EXTREME COLD WEATHER ENGINE START 4 9 AFTER ENGINE START 4 9 BEFORE TAXI 4 10 TAXI 4 10 MINOR SPARK PLUG FOULING 4 11 BEFORE TAKEOFF 4 12 TAKEOFF 4 13 CLIMB 4 14 CLIMB CRUISE 4 14 CLIMB BEST RATE Vy 4 14 CLIMB BEST RATE Vx 4 14 CRUISE 4 14 FUEL TANK SELECTION 4 15 OXYGEN SYSTEM 4 15 DESCENT 4 16 NORMAL DESCENT GEAR UP 4 16 NORMAL DESCENT GEAR DOWN 4 16 APPROACH FOR LANDING 4 17 GO AROU...

Page 80: ...MOONEY M20TN MODEL TYPE S SECTION IV NORMAL PROCEDURES 4 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 81: ...s determined by the operating and design features of the airplane are presented These procedures are provided to present a source of reference and review and to supply infor mation on procedures which are the same for all aircraft Pilots should familiarize themselves with the procedures given in this section in order to become proficient in the normal operations of the airplane Normal procedures a...

Page 82: ...akeoff Speed At 50 Ft 75 KIAS ENROUTE CLIMB GEAR and FLAPS UP Best Rate of Climb 104 KIAS Best Angle of Climb 85 KIAS LANDING APPROACH 3200 lbs Normal Approach Flaps 10 degrees 80 KIAS Normal Approach Flaps 33 degrees 75 KIAS Short Field Approach Flaps 33 degrees 70 KIAS BALKED LANDING 3200 lbs Maximum Power Flaps 10 degrees 85 KIAS MAXIMUM RECOMMENDED TURBULENT AIR PENETRATION SPEED 3368 lbs 1528...

Page 83: ...eter after each selection Leave on Battery with highest voltage Internal External Lights CHECK operation Check for ammeter fluctuations as each light is checked Pitot Heat Switch ON Check Pitot Heat annunciator light illuminated BLUE Fuel Quantity Gauges CHECK QTY Master Switch OFF Pilot Window OPEN Fuel Selector It is recommended that wing tank sumps be drained prior to draining gascolator Rt Tan...

Page 84: ...ne Cabin Fresh Air Vent Dorsal Fin UNOBSTRUCTED Tailcone Empennage Access Panel SECURED Instrument Static Pressure Port UNOBSTRUCTED Avionics Battery 1 Access Panel SECURED Auxiliary Power Plug Access Door SECURED Static System Drain PUSH Plunger UP Hold 3 5 Seconds General Skin Condition INSPECT 5 Left Wing General Skin Condition INSPECT Remove ice snow or frost Wing Flap attach points INSPECT Ai...

Page 85: ...nal movement Prop De Ice Boots if installed INSPECT condition Induction Air Inlet Filter UNOBSTRUCTED Nose Gear Shock Discs Tire Doors INSPECT Wheel Chock REMOVE 8 Right Cowl Area Right Side Engine Cowl Fasteners SECURED Cooling Air Inlet Verify UNOBSTRUCTED Windshield CLEAN Cabin Air Inlet UNOBSTRUCTED 9 Right Wing Fuel Tank Sump Drain DRAIN Use sampler cup to VERIFY fuel is free of water sedimen...

Page 86: ...F Cabin Heat Push OFF Cabin Vent As Desired Fuel Selector Fullest Tank Landing Gear Switch Down Position Red Emergency Gear Extension Handle Down and Latched Internal Lights OFF Passenger Briefing Completed Refer to SECTION IX Supplemental Data for other Optional Equipment Procedures and Checks WARNING IFR flight should not be initiated if the operation of the standby alternator and emergency bus ...

Page 87: ...esult in engine damage or malfunction HOT ENGINE START Before Starting Check List COMPLETED Mixture IDLE CUT OFF Propeller FULL FWD High RPM Throttle Control SET TO CLOSED Fuel Boost Pump HIGH for 5 SEC or LOW for 25 SEC THEN SET TO OFF Engine Start follow NORMAL procedures FLOODED ENGINE START Before Starting Check List COMPLETED Mixture IDLE CUTOFF Throttle Control 1 2 OPEN Ignition Switch TURN ...

Page 88: ...ly exists without first removing the existing arrival or departure procedure Failing to observe this limitation can cause erroneous course deviation indications loss of GPS navigation information and other display anomalies NOTE If display anomalies are noted after editing the flight plan perform either a direct to or activate leg operation as appropriate on the flight plan to ensure correct fligh...

Page 89: ...F A drop in excess of 150 RPM may indicate a faulty magneto or fouled spark plugs WARNING Continuous overboost operation may damage the engine and require engine in spection MINOR SPARK PLUG FOULING Minor spark plug fouling may be cleared by Brakes HOLD MANUALLY Throttle SET TO 2200 RPM Mixture ADJUST FOR MAXIMUM PERFORMANCE Move Towards Idle Cutoff Until RPM Peaks Hold For 10 Seconds Return To Fu...

Page 90: ...agneto Switch BOTH EGTs should drop Propeller CHECK OPERATION Cycle from high to low RPM two to three times Engine Instruments CHECK Annunciator TEST Throttle SET TO IDLE Standby Alternator Preflight Check Will Not Show A Charge Until Approximately 2000 rpm Alt Field Switch OFF Verify red ALT VOLTS light illuminates Stdby Alt Emerg Bus switch ON Verify amber Emerg Bus light illuminates Pull BATT C...

Page 91: ...e RELEASE TAKEOFF Proper engine operation should be checked early in the takeoff roll Any significant indication of rough or sluggish engine response is reason to discontinue takeoff When takeoff must be made over a gravel surface it is important that the throttle be applied SLOWLY This will allow the air craftto startrolling beforehigh RPMisdeveloped and gravelor loosematerialwillbe blownback fro...

Page 92: ...LL Propeller 2500 RPM Mixture FULL RICH 1350 F to 1450 TIT LOW Boost Pump ON for vapor suppression above 12 000 ft or if TIT is rising above 1450 F NOTE Leaning may be required during CLIMB depending on atmospheric conditions CRUISE Airspeed ACCELERATE to cruise airspeed Throttle SELECT setting Propeller SELECT setting Mixture LEAN AS REQUIRED observe limits see CAUTION below 50 F Rich of Peak for...

Page 93: ...hrottle control and then decrease RPM with the propeller control When engine temperatures have stabi lized lean mixture to desired TIT FUEL TANK SELECTION LOW Boost Pump ON Fuel Selector OPPOSITE TANK LOW Boost Pump OFF OXYGEN SYSTEM OPTIONAL EQUIPMENT WARNING Greasy lipsticks and waxed mustaches have been known to ignite spontaneously inside oxygen masks Passengers should be suitably advised prio...

Page 94: ...start the engine at any altitude by leaning the mixture NOTE Avoid extended descents at low manifold pressure setting as engine can cool excessively and may not accelerate satisfactorily when power is re applied NORMAL DESCENT GEAR UP Seats Seat Belts Shoulder Harness ADJUST AND SECURE Wing Flaps UP Landing Gear UP Power Settings AS REQUIRED Mixture MOVE TO RICHER SETTING AS REQUIRED LOW Boost Pum...

Page 95: ...mize control wheel forces when entering landing configuration timely nose up trimming is recommended to counteract nose down pitching moment caused by reduction of power and or extension of flaps Elevator Trim AS DESIRED Rudder Trim AS DESIRED Parking Brake VERIFY OFF NOTE The parking brake should be rechecked to preclude partially applied brakes dur ing touchdown GO AROUND BALKED LANDING CAUTION ...

Page 96: ...f landing gear switch is placed in the UP position TAXI AFTER LANDING Throttle AS REQUIRED Fuel Boost Pump Switches OFF Wing Flaps RETRACT Elevator Trim TAKEOFF SETTING Avionics Radios AS REQUIRED Interior Exterior Lights AS DESIRED SHUTDOWN Parking Brake SET Throttle IDLE 900 RPM Interior Exterior Lights OFF Pitot Heat OFF Magneto Starter Switch GROUNDING CHECK Mixture IDLE Cut OFF Alternator Fie...

Page 97: ...TATIC SYS POWER ON 33 GR DWN 5 11 AIRSPEED CALIBRATION PRIMARY STATIC SYS POWER OFF 33 GR DWN 5 12 AIRSPEED CALIBRATION ALTERNATE STATIC SYSTEM 5 13 ALTIMETER CORRECTION PRIMARY STATIC SYSTEM 5 14 ALTIMETER CORRECTION ALTERNATE STATIC SYSTEM 5 15 STALL SPEED VS ANGLE OF BANK 5 16 TAKEOFF GROUND ROLL 5 17 OVER 50 OBSTACLE 5 18 CLIMB RATE AT Vy 5 19 CLIMB RATE AT 120 KIAS CRUISE CLIMB 5 20 TIME FUEL...

Page 98: ...ple are those where such an example of use would be repetitive To obtain effect of altitude and OAT on aircraft performance 1 Set altimeter to 29 92 and read pressure altitude 2 Using the OAT grid for the applicable chart read the corresponding effect of OAT on perfor mance CAUTION Be sure to return to local altimeter setting in calculating aircraft elevation above sea level OPERATIONAL PROCEDURES...

Page 99: ...mixture control toward lean while observing TIT indicator and maintaining TIT limits If manifold pressure changes while leaning readjust throttle and continue leaning until peak TIT is attained Note peak TIT and slow ly lean mixture until TIT indication is 50 F LEAN OF PEAK Re adjust throttle or RPM as re quired CAUTION Above 30 5 inHg of manifold pressure only full rich mixture is permitted At al...

Page 100: ...ture Example 160 KIAS ISA 20ºC 25000 correction 2 5 0 04 2 5 2 6 KTAS REMOVABLE STEP The cruise speed tables herein were established with the aircraft step removed Aircraft equipped with a removable step may have it removed or installed by a mechanic If the step is installed decrease the true airspeed at normal cruise power setting by approximately 1 KTAS LANDING GEAR DOORS When snow and ice are l...

Page 101: ...S SECTION V PERFORMANCE 5 5 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TEMPERATURE CONVERSION 160 60 130 70 140 150 o o CELSIUS FAHRENHEIT 120 110 50 40 30 20 10 0 10 20 30 40 50 60 70 80 90 100 40 30 20 10 0 10 20 30 40 ...

Page 102: ...45 40 35 30 25 20 15 10 5 0 5 10 15 20 0 5 10 15 20 25 30 35 40 45 50 55 60 10 20 30 40 50 60 70 80 90 100 110 120 130 140 150 160 170 180 o o o o o o o o o o o o o o o o o o 0o EXAMPLE WIND SPEED 18 KNOTS ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH 35 HEADWIND COMPONENT 16 4 KNOTS CROSSWIND COMPONENT 11 2 KNOTS o CROSSWIND COMPONENT IN KNOTS CROSSWIND COMPONENT CHART HEADWIND COMPONENT IN KNOTS ...

Page 103: ...Clean Configuration Air Speed Calibration 60 65 70 75 85 90 95 100 105 110 115 KIAS KCAS 120 125 60 65 70 76 86 91 96 101 106 111 116 121 126 80 81 130 135 140 145 150 155 160 165 170 175 180 KIAS KCAS 185 190 131 136 141 146 152 157 162 167 172 177 182 187 192 195 197 200 200 EXAMPLE GIVEN IAS 129 KNOTS FIND CAS 130 KNOTS 0 3 0 4 0 4 0 5 0 7 0 7 0 8 0 9 0 9 1 0 1 1 1 1 1 2 0 6 1 3 1 4 1 4 1 5 1 6...

Page 104: ... Clean Configuration Air Speed Calibration 60 65 70 75 85 90 95 100 105 110 115 KIAS KCAS 120 125 60 65 70 75 85 90 96 101 106 111 116 121 126 80 80 130 135 140 145 150 155 160 165 170 175 180 KIAS KCAS 185 190 131 136 141 146 151 156 162 167 172 177 182 187 192 195 197 200 200 EXAMPLE GIVEN IAS 129 KNOTS FIND CAS 130 KNOTS 0 0 0 1 0 2 0 2 0 4 0 5 0 5 0 6 0 7 0 8 0 8 0 9 1 0 0 3 1 1 1 1 1 2 1 3 1 ...

Page 105: ... 85 90 95 100 105 110 115 KIAS KCAS 120 60 65 70 75 85 90 95 100 105 111 116 121 80 80 0 1 0 0 0 0 0 1 0 2 0 3 0 3 0 4 0 5 0 5 0 6 0 7 0 2 ERROR Primary Static System Power On 10 Flap Gear Down 50 50 55 55 0 2 NOTE The minus sign indicates subtraction of the given numbers from KIAS to obtain the corrected airspeed EXAMPLE GIVEN IAS 80 KNOTS FIND CAS 80 KNOTS SPEED FOR SAFELY LOWERING FLAPS KNOTS I...

Page 106: ...5 85 90 95 100 105 110 115 KIAS KCAS 120 61 66 71 75 85 90 95 100 105 110 115 120 80 80 0 6 0 6 0 5 0 4 0 3 0 2 0 2 0 1 0 1 0 0 0 1 0 1 0 4 ERROR Primary Static System Power Off 10 Flap Gear Down 50 50 55 56 0 7 NOTE The minus sign indicates subtraction of the given numbers from KIAS to obtain the corrected airspeed EXAMPLE GIVEN IAS 80 KNOTS FIND CAS 80 KNOTS SPEED FOR SAFELY LOWERING FLAPS KNOTS...

Page 107: ...tic System Power On 33 Flap Gear Down 60 70 80 90 100 110 120 60 70 80 90 100 110 120 50 50 KNOTS INDICATED AIRSPEED KIAS KNOTS CALIBRATED AIRSPEED KCAS 60 65 70 75 85 90 95 100 105 110 115 KIAS KCAS 120 59 64 69 74 83 88 93 98 103 108 113 118 80 78 1 4 1 4 1 5 1 5 1 6 1 6 1 6 1 6 1 7 1 7 1 7 1 8 1 5 ERROR 55 54 1 4 NOTE The minus sign indicates subtraction of the given numbers from KIAS to obtain...

Page 108: ...10 120 50 50 KNOTS INDICATED AIRSPEED KIAS KNOTS CALIBRATED AIRSPEED KCAS 60 65 70 75 85 90 95 100 105 110 115 KIAS KCAS 120 60 65 70 75 85 90 95 99 104 109 114 119 80 80 0 2 0 3 0 3 0 4 0 4 0 5 0 5 0 5 0 6 0 6 0 6 0 7 0 4 ERROR 55 55 0 2 NOTE The minus sign indicates subtraction of the given numbers from KIAS to obtain the corrected airspeed Air Speed Calibration With Flap Seals Primary Static Sy...

Page 109: ...00 KIAS GEAR FLAPS DN 330 KIAS 50 3 0 0 0 1 0 60 1 5 1 2 2 0 70 0 0 2 2 3 2 80 1 8 3 2 4 5 90 2 8 4 0 6 0 100 3 0 4 7 7 4 110 3 0 5 4 8 8 120 3 0 130 3 6 140 4 5 150 5 1 160 5 6 170 6 1 180 6 5 190 7 2 200 7 9 NOTE The minus sign indicates subtraction of the given numbers from KIAS to obtain the corrected airspeed CONDITIONS Power ON Storm Window Vents CLOSED Heater Defroster ON or OFF ...

Page 110: ... 3 1 12 4 1 20 70 3 0 9 4 0 14 7 1 24 80 4 1 11 7 2 17 11 3 29 90 6 2 13 9 4 20 16 6 34 100 8 4 15 13 6 23 21 10 39 110 10 5 17 16 8 27 27 14 45 120 12 20 34 130 15 24 41 140 18 29 49 150 22 35 58 160 25 40 68 170 29 47 78 180 33 53 90 190 38 60 102 200 42 68 115 NOTE The minus sign indicates subtraction of the given numbers from the indicated pressure altitude to obtain correct altitude assuming ...

Page 111: ...0 0 10 60 8 6 11 12 9 16 18 14 24 70 0 14 20 0 20 29 0 31 45 80 13 23 32 19 34 47 29 51 72 90 23 32 48 33 47 71 50 72 108 100 27 42 66 39 62 97 68 94 148 110 30 53 87 43 78 127 66 119 194 120 32 48 72 130 53 77 118 140 57 84 127 150 69 102 155 160 82 128 182 170 95 139 211 180 107 158 248 190 126 185 282 200 146 215 327 NOTE The minus sign indicates subtraction of the given numbers from the indica...

Page 112: ...E WEIGHT LANDING GEAR FLAPS ANGLE OF BANK STALL SPEED OCCUR DURING STALLS AT MAXIMUM WEIGHT UP TO 500 FEET ALTITUDE LOSS MAY NOTE DOWN 10 45 FLAPS 10 FLAPS 10 FLAPS 10 3368 LBS 1528 KGS 3000 LBS 1361 KGS 2700 LBS 1225 KGS 3000 LBS 1361 KGS 74 5 KCAS 74 4 KIAS 66 9 66 8 71 9 71 7 79 6 79 3 94 6 94 1 66 4 66 4 71 4 71 3 79 0 78 8 93 9 93 6 60 2 60 5 64 7 65 0 71 6 71 9 85 1 85 6 63 1 63 1 67 8 67 7 ...

Page 113: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 17 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TAKEOFF DISTANCE GROUND ROLL ...

Page 114: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 18 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TAKEOFF DISTANCE OVER 50 15m OBSTACLE ...

Page 115: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 19 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 RATE OF CLIMB AT Vy ...

Page 116: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 20 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 RATE OF CLIMB at 120 KIAS CRUISE CLIMB ...

Page 117: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 21 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TIME FUEL DISTANCE to CLIMB at Vy Revision B 11 21 2014 ...

Page 118: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 22 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TIME FUEL DISTANCE to CLIMB at 120 KIAS ...

Page 119: ...3 12 5 20 9 19 9 18 0 15 6 20 2 18 0 16 2 14 4 17 7 15 9 14 1 12 3 12 6 20 9 19 9 18 0 15 6 20 2 17 9 16 2 14 5 17 7 15 9 14 1 12 4 12 7 0 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 22000 20 9 19 9 18 0 15 7 20 1 17 9 16 2 14 5 17 7 15 9 14 2 12 6 12 8 20 9 19 9 18 0 15 7 20 1 17 9 16 2 14 6 17 6 15 9 14 2 12 7 12 8 24000 25000 Note 1 At altitudes above 22 000 feet power settings abov...

Page 120: ... 6 14 1 12 5 15 5 13 9 12 2 10 6 10 9 18 1 17 2 15 6 13 5 17 5 15 6 14 0 12 5 15 5 13 8 12 3 10 6 11 0 18 1 17 2 15 6 13 5 17 5 15 6 14 0 12 5 15 4 13 8 12 3 10 7 11 1 0 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 22000 18 1 17 2 15 6 13 5 17 5 15 6 14 0 12 6 15 4 13 8 12 3 10 9 11 1 18 1 17 2 15 6 13 5 17 5 15 6 14 1 12 7 15 4 13 8 12 4 11 0 11 2 24000 25000 Note 1 At altitudes above ...

Page 121: ...ich of Peak TIT Propeller Speed 2400 RPM Manifold Pressure 30 5 in HG Cruise Weight 3100 LB Outside Air Temp 16 C Altimeter Set to 29 92 True Airspeed 220 KTAS Configuration Clean Fuel Flow 20 3 GPH Some low power settings may not be attainable due to low cylinder or oil temperatures depending on ambient conditions ISA 30 65 C 0 34 C 30 4 C OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS...

Page 122: ...0 28 0 221 19 2 222 17 9 220 16 6 2300 25 0 212 17 2 213 16 1 211 14 9 2300 22 0 202 15 3 202 14 3 199 13 2 2300 19 0 191 13 5 190 12 6 187 11 7 2200 21 0 193 13 8 193 12 9 190 11 9 ISA 30 59 C 0 28 C 30 2 C 22000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 230 22 6 232 21 1 231 19 6 2500 29 0 226 21 6 228 20 1 226 18 6 2500 26 0 218 19 5 219 18 2 2...

Page 123: ... 28 0 214 19 2 214 17 9 212 16 6 2300 25 0 204 17 2 205 16 1 203 14 9 2300 22 0 195 15 3 194 14 3 192 13 2 2300 19 0 183 13 3 183 12 5 180 11 5 2200 21 0 186 13 6 185 12 7 182 11 7 ISA 30 51 C 0 20 C 30 10 C 18000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 223 22 6 223 21 2 222 19 6 2500 29 0 219 21 6 219 20 2 218 18 7 2500 26 0 210 19 6 211 18 3 2...

Page 124: ...0 28 0 205 19 2 205 18 0 203 16 6 2300 25 0 196 17 2 196 16 1 194 14 9 2300 22 0 186 15 3 186 14 3 184 13 2 2300 19 0 175 13 2 175 12 4 172 11 5 2200 21 0 177 13 5 177 12 6 174 11 7 ISA 30 43 C 0 12 C 30 18 C 14000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 214 22 7 214 21 2 213 19 7 2500 29 0 210 21 7 210 20 3 209 18 8 2500 26 0 202 19 7 202 18 4 ...

Page 125: ...00 28 0 196 19 2 196 18 0 195 16 6 2300 25 0 188 17 3 188 16 2 186 15 0 2300 22 0 178 15 3 178 14 3 175 13 2 2300 19 0 167 13 2 166 12 3 164 11 4 2200 21 0 169 13 5 169 12 6 166 11 7 ISA 30 35 C 0 4 C 30 26 C 10000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 205 22 8 205 21 4 204 19 8 2500 29 0 201 21 9 202 20 5 200 19 0 2500 26 0 193 19 9 193 18 6 ...

Page 126: ...00 28 0 187 19 2 187 18 0 186 16 7 2300 25 0 179 17 3 178 16 2 177 15 0 2300 22 0 169 15 2 168 14 2 166 13 2 2300 19 0 157 13 0 156 12 2 154 11 3 2200 21 0 161 13 6 161 12 7 158 11 8 ISA 30 27 C 0 3 C 30 33 C 6000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 196 23 0 196 21 5 194 19 9 2500 29 0 192 22 0 192 20 6 190 19 1 2500 26 0 184 20 1 184 18 8 1...

Page 127: ...300 28 0 178 19 3 178 18 1 176 16 7 2300 25 0 169 17 2 169 16 1 167 14 9 2300 22 0 158 15 0 157 14 1 155 13 0 2300 19 0 145 12 7 145 11 9 142 11 0 2200 21 0 152 13 6 151 12 7 149 11 8 ISA 30 19 C 0 11 C 30 41 C 2000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 186 23 1 186 21 6 184 20 0 2500 29 0 182 22 2 182 20 7 180 19 2 2500 26 0 173 20 2 173 18 9...

Page 128: ...S GPH KTAS GPH 2500 30 5 235 19 4 236 18 3 234 17 0 2500 29 0 231 18 4 232 17 4 229 16 2 2500 26 0 222 16 7 222 15 7 219 14 6 2500 22 0 208 14 6 208 13 7 204 12 7 2400 30 5 232 18 8 233 17 7 230 16 5 2400 27 0 222 16 7 223 15 7 220 14 7 2400 24 0 213 15 1 213 14 2 209 13 2 2400 21 0 203 13 6 202 12 8 197 11 9 2300 28 0 221 16 5 221 15 6 218 14 5 2300 25 0 212 14 9 212 14 0 208 13 0 2300 22 0 201 1...

Page 129: ...0 28 0 216 16 6 216 15 6 213 14 5 2300 25 0 207 14 9 206 14 0 203 13 0 2300 22 0 196 13 2 195 12 4 191 11 6 2300 19 0 184 11 6 182 10 9 177 10 1 2200 21 0 187 11 9 186 11 2 181 10 4 ISA 30 51 C 0 20 C 30 10 C 22000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 226 19 3 227 18 2 224 17 0 2500 29 0 222 18 4 222 17 4 220 16 2 2500 26 0 213 16 7 213 15 8 ...

Page 130: ...00 28 0 209 16 6 209 15 6 206 14 6 2300 25 0 199 14 9 199 14 0 196 13 0 2300 22 0 188 13 2 187 12 4 184 11 5 2300 19 0 176 11 4 175 10 7 170 10 0 2200 21 0 179 11 8 178 11 1 174 10 3 ISA 30 51 C 0 20 C 30 10 C 18000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 218 19 3 218 18 2 216 17 0 2500 29 0 214 18 5 214 17 4 212 16 3 2500 26 0 205 16 8 205 15 8...

Page 131: ...300 28 0 200 16 6 200 15 6 198 14 6 2300 25 0 191 14 9 191 14 0 188 13 1 2300 22 0 181 13 2 180 12 4 176 11 5 2300 19 0 169 11 4 167 10 7 163 9 9 2200 21 0 172 11 7 170 11 0 166 10 2 ISA 30 43 C 0 12 C 30 18 C 14000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 210 19 3 210 18 2 207 17 1 2500 29 0 206 18 5 205 17 5 203 16 3 2500 26 0 197 16 9 196 15 9...

Page 132: ...2300 28 0 192 16 6 192 15 6 189 14 6 2300 25 0 183 14 9 182 14 1 179 13 1 2300 22 0 173 13 2 172 12 4 168 11 5 2300 19 0 160 11 3 158 10 6 154 9 9 2200 21 0 164 11 7 163 11 0 159 10 2 ISA 30 35 C 0 4 C 30 26 C 10000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 201 19 4 201 18 4 199 17 2 2500 29 0 197 18 7 197 17 6 194 16 5 2500 26 0 188 17 0 188 16 1...

Page 133: ...2300 28 0 183 16 6 183 15 7 180 14 6 2300 25 0 174 14 9 173 14 1 171 13 1 2300 22 0 163 13 1 162 12 3 159 11 5 2300 19 0 150 11 2 148 10 5 144 9 7 2200 21 0 156 11 7 154 11 0 151 10 3 ISA 30 27 C 0 3 C 30 33 C 6000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 192 19 6 191 18 5 189 17 3 2500 29 0 188 18 8 187 17 8 185 16 6 2500 26 0 179 17 2 178 16 2 ...

Page 134: ... 2300 28 0 174 16 7 173 15 7 171 14 7 2300 25 0 164 14 9 163 14 0 160 13 1 2300 22 0 152 13 0 151 12 2 148 11 3 2300 19 0 138 10 8 136 10 2 131 9 5 2200 21 0 146 11 8 145 11 0 141 10 3 ISA 30 19 C 0 11 C 30 41 C 2000 Ft Pressure Altitude OAT 54 81 F 0 27 F 54 27 F RPM MAP KTAS GPH KTAS GPH KTAS GPH 2500 30 5 182 19 7 181 18 6 179 17 4 2500 29 0 178 19 0 177 17 9 174 16 7 2500 26 0 168 17 4 168 16 ...

Page 135: ...g to power setting in Section V cruise tables Figure range reduction and subtract from range figure time reduction and subtract from time For 10 gal less 79 gal useable 217 kts 20 1 gph x 10 gal 108 nmi New zero wind range 704 nmi 108 nmi 596 nmi Final time estimate 3 43 hrs 108 nmi 217 kts 2 93 hours Conservatively estimate wind enroute e g maximum headwind minmum tailwind subtract headwind x tim...

Page 136: ...9 3 36 743 3 41 24000 33 685 3 20 702 3 25 717 3 29 730 3 34 742 3 38 25000 35 688 3 20 704 3 25 718 3 29 731 3 33 741 3 37 Mixture Best Economy Cruise MAP 30 5 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 669 3 70 691 3 82 714 3 96 738 4 11 763 4 29 4000 7 700 3 71 722 3 82 744 3 94 767 4 08 791 4 23 8000 1 72...

Page 137: ... 3 51 769 3 57 24000 33 710 3 34 727 3 39 743 3 44 757 3 49 768 3 53 25000 35 713 3 35 730 3 39 744 3 43 757 3 48 767 3 51 Mixture Best Economy Cruise MAP 29 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 684 3 87 707 4 00 730 4 15 754 4 31 779 4 49 4000 7 718 3 88 740 4 00 763 4 13 786 4 27 810 4 43 8000 1 747 3...

Page 138: ... 3 85 820 3 91 24000 33 761 3 66 779 3 71 795 3 76 808 3 81 819 3 85 25000 35 764 3 65 781 3 70 796 3 75 809 3 79 818 3 83 Mixture Best Economy Cruise MAP 26 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 721 4 31 745 4 46 769 4 62 794 4 80 820 5 00 4000 7 760 4 31 783 4 44 807 4 59 830 4 75 855 4 92 8000 1 794 4...

Page 139: ... 4 38 895 4 45 24000 33 832 4 14 851 4 20 866 4 26 879 4 31 889 4 36 25000 35 834 4 13 851 4 18 865 4 22 877 4 27 885 4 31 Mixture Best Economy Cruise MAP 22 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 788 5 17 813 5 34 838 5 53 863 5 75 888 6 00 4000 7 835 5 14 860 5 30 885 5 47 910 5 66 935 5 88 8000 1 873 5...

Page 140: ...7 3 47 761 3 53 24000 33 703 3 30 719 3 35 735 3 40 749 3 45 760 3 49 25000 35 705 3 31 721 3 35 736 3 39 749 3 43 759 3 47 Mixture Best Economy Cruise MAP 30 5 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 696 3 90 719 4 03 742 4 17 767 4 33 793 4 52 4000 7 725 3 90 748 4 02 770 4 14 794 4 29 818 4 45 8000 1 75...

Page 141: ... 3 86 824 3 92 24000 33 762 3 67 781 3 72 796 3 77 810 3 82 820 3 87 25000 35 766 3 66 782 3 71 796 3 75 809 3 79 818 3 83 Mixture Best Economy Cruise MAP 27 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 748 4 49 773 4 64 797 4 81 823 5 00 850 5 21 4000 7 778 4 41 802 4 55 826 4 69 850 4 86 875 5 04 8000 1 803 4...

Page 142: ... 4 25 878 4 31 24000 33 817 4 02 835 4 08 850 4 13 863 4 18 873 4 23 25000 35 817 4 00 835 4 05 849 4 10 861 4 14 869 4 18 Mixture Best Economy Cruise MAP 24 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 812 5 23 838 5 41 864 5 61 890 5 83 917 6 07 4000 7 835 5 03 860 5 18 885 5 35 910 5 54 936 5 75 8000 1 860 4...

Page 143: ...78 24000 33 872 4 43 890 4 49 905 4 55 918 4 60 926 4 65 25000 35 870 4 39 887 4 44 901 4 49 912 4 54 919 4 58 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 891 6 35 917 6 56 943 6 80 968 7 06 990 7 36 4000 7 913 5 91 939 6 09 965 6 29 990 6 51 1015 6 76 8000 1 930 5 63 954 5 7...

Page 144: ... 3 90 829 3 97 24000 33 770 3 72 788 3 77 804 3 82 818 3 87 829 3 91 25000 35 773 3 72 791 3 76 806 3 81 818 3 85 827 3 89 Mixture Best Economy Cruise MAP 28 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 760 4 52 784 4 67 810 4 84 836 5 02 863 5 24 4000 7 790 4 48 813 4 61 838 4 76 863 4 92 889 5 11 8000 1 816 4...

Page 145: ... 4 31 889 4 38 24000 33 828 4 09 846 4 15 861 4 20 874 4 25 884 4 30 25000 35 830 4 08 846 4 13 861 4 18 872 4 22 880 4 26 Mixture Best Economy Cruise MAP 25 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 816 5 19 842 5 36 869 5 56 896 5 77 924 6 02 4000 7 847 5 06 872 5 22 898 5 39 924 5 57 950 5 78 8000 1 874 4...

Page 146: ...24000 33 888 4 53 906 4 59 921 4 65 933 4 70 941 4 75 25000 35 887 4 50 904 4 55 919 4 60 929 4 65 936 4 69 Mixture Best Economy Cruise MAP 22 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 895 6 17 922 6 37 948 6 60 975 6 86 1001 7 15 4000 7 920 5 89 946 6 07 973 6 27 999 6 49 1026 6 73 8000 1 948 5 72 974 5 88 ...

Page 147: ...000 33 953 5 06 970 5 13 984 5 19 995 5 25 1001 5 30 25000 35 948 5 00 964 5 06 977 5 11 986 5 16 990 5 20 Mixture Best Economy Cruise MAP 19 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 987 7 69 1012 7 95 1036 8 24 1058 8 56 1077 8 91 4000 7 1016 7 12 1043 7 34 1069 7 58 1093 7 84 1115 8 14 8000 1 1042 6 79 10...

Page 148: ...00 33 948 4 99 966 5 06 981 5 12 992 5 18 998 5 23 25000 35 947 4 95 964 5 01 978 5 07 987 5 11 991 5 15 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2200 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 957 6 85 985 7 08 1012 7 34 1040 7 63 1065 7 95 4000 7 989 6 61 1016 6 81 1044 7 03 1071 7 28 1097 7 55 8000 1 1027 6 50 1053 6...

Page 149: ... 24000 33 992 5 34 1010 5 40 1023 5 47 1033 5 53 1038 5 58 25000 35 992 5 30 1008 5 36 1020 5 42 1027 5 47 1029 5 51 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2100 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 987 7 12 1015 7 36 1044 7 62 1073 7 92 1101 8 25 4000 7 1031 7 01 1059 7 22 1087 7 45 1114 7 71 1140 8 00 8000 1 10...

Page 150: ...setting in Section V cruise tables Figure range reduction and subtract from range figure time reduction and subtract from time For 10 gal less 90 gal useable 217 kts 20 1 gph x 10 gal 108 nmi New zero wind range 817 nmi 108 nmi 709 nmi Final time estimate 4 09 hrs 108 nmi 217 kts 3 59 hours Conservatively estimate wind enroute e g maximum headwind minmum tailwind subtract headwind x time from rang...

Page 151: ...50 3 88 869 3 95 24000 33 796 3 66 817 3 73 835 3 79 853 3 85 869 3 92 25000 35 799 3 67 820 3 73 838 3 79 855 3 84 869 3 90 Mixture Best Economy Cruise MAP 30 5 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 771 4 26 796 4 40 822 4 55 848 4 73 876 4 92 4000 7 808 4 27 832 4 40 857 4 53 883 4 69 910 4 86 8000 1 8...

Page 152: ...4 05 899 4 13 24000 33 825 3 83 846 3 90 866 3 96 884 4 03 900 4 10 25000 35 829 3 84 850 3 90 868 3 96 885 4 02 899 4 08 Mixture Best Economy Cruise MAP 29 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 788 4 46 813 4 60 839 4 76 866 4 95 893 5 15 4000 7 827 4 47 852 4 60 878 4 74 904 4 91 932 5 09 8000 1 861 4 ...

Page 153: ...3 24000 33 883 4 20 906 4 27 926 4 34 944 4 41 959 4 48 25000 35 887 4 19 909 4 26 928 4 32 945 4 39 959 4 45 Mixture Best Economy Cruise MAP 26 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 828 4 95 855 5 11 883 5 30 911 5 50 940 5 73 4000 7 874 4 95 900 5 10 927 5 26 954 5 45 981 5 65 8000 1 914 4 96 940 5 09 ...

Page 154: ...0 33 964 4 77 987 4 84 1007 4 92 1025 5 00 1039 5 07 25000 35 966 4 75 988 4 82 1007 4 89 1023 4 96 1036 5 02 Mixture Best Economy Cruise MAP 22 inHG Cruise RPM 2500 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 902 5 91 930 6 11 958 6 33 986 6 57 1014 6 85 4000 7 956 5 89 985 6 07 1014 6 26 1042 6 48 1070 6 73 8000 1 1002 5 86 1029...

Page 155: ...71 4 01 890 4 09 24000 33 816 3 79 836 3 85 856 3 92 875 3 98 891 4 05 25000 35 820 3 79 839 3 85 859 3 91 876 3 97 890 4 03 Mixture Best Economy Cruise MAP 30 5 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 801 4 49 826 4 63 853 4 80 880 4 98 909 5 18 4000 7 835 4 49 861 4 62 887 4 76 913 4 93 941 5 11 8000 1 8...

Page 156: ...24000 33 884 4 21 908 4 28 927 4 35 945 4 42 960 4 49 25000 35 889 4 20 909 4 27 928 4 33 945 4 39 959 4 46 Mixture Best Economy Cruise MAP 27 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 859 5 15 886 5 32 914 5 51 942 5 73 973 5 96 4000 7 894 5 07 921 5 22 948 5 38 976 5 57 1005 5 78 8000 1 924 5 01 950 5 14 9...

Page 157: ... 33 947 4 62 969 4 70 989 4 77 1007 4 85 1022 4 92 25000 35 948 4 60 970 4 67 989 4 74 1006 4 80 1019 4 87 Mixture Best Economy Cruise MAP 24 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 930 5 99 958 6 19 988 6 41 1017 6 66 1047 6 94 4000 7 958 5 77 986 5 94 1014 6 13 1043 6 34 1072 6 58 8000 1 988 5 61 1016 5 ...

Page 158: ...4000 33 1010 5 10 1032 5 18 1052 5 26 1069 5 34 1083 5 42 25000 35 1008 5 05 1029 5 13 1048 5 20 1064 5 27 1076 5 34 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2400 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 1017 7 24 1047 7 49 1076 7 75 1103 8 05 1128 8 39 4000 7 1044 6 76 1074 6 97 1103 7 19 1132 7 45 1160 7 73 8000 1 1...

Page 159: ...4000 33 893 4 27 916 4 34 936 4 41 955 4 48 970 4 55 25000 35 897 4 27 919 4 33 939 4 40 956 4 46 970 4 52 Mixture Best Economy Cruise MAP 28 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 872 5 18 899 5 35 928 5 54 957 5 75 988 5 99 4000 7 907 5 14 934 5 29 962 5 46 990 5 65 1020 5 86 8000 1 939 5 10 965 5 23 99...

Page 160: ... 33 960 4 70 982 4 78 1002 4 85 1019 4 93 1034 5 01 25000 35 962 4 69 983 4 76 1002 4 83 1018 4 90 1031 4 96 Mixture Best Economy Cruise MAP 25 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 934 5 94 964 6 14 993 6 35 1024 6 60 1056 6 87 4000 7 971 5 80 1000 5 98 1029 6 17 1058 6 38 1088 6 62 8000 1 1004 5 71 103...

Page 161: ... 24000 33 1028 5 21 1051 5 30 1071 5 38 1088 5 46 1101 5 54 25000 35 1028 5 18 1050 5 25 1069 5 33 1084 5 40 1096 5 47 Mixture Best Economy Cruise MAP 22 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 1022 7 04 1052 7 28 1082 7 53 1112 7 82 1140 8 15 4000 7 1052 6 74 1082 6 94 1112 7 17 1143 7 42 1173 7 70 8000 1...

Page 162: ...6 40 24000 33 1102 5 84 1124 5 93 1143 6 02 1159 6 11 1170 6 19 25000 35 1097 5 76 1119 5 85 1136 5 93 1150 6 01 1159 6 08 Mixture Best Economy Cruise MAP 19 inHG Cruise RPM 2300 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 1124 8 76 1152 9 05 1179 9 37 1204 9 73 1225 10 14 4000 7 1160 8 13 1191 8 38 1220 8 65 1247 8 95 1272 9 29 8...

Page 163: ...6 28 24000 33 1098 5 75 1120 5 84 1139 5 93 1155 6 02 1166 6 11 25000 35 1097 5 71 1119 5 79 1137 5 87 1151 5 95 1160 6 03 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2200 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 1091 7 82 1122 8 08 1153 8 36 1184 8 68 1212 9 05 4000 7 1129 7 55 1161 7 78 1192 8 03 1223 8 31 1253 8 63 80...

Page 164: ... 6 72 24000 33 1148 6 15 1171 6 25 1189 6 34 1203 6 44 1212 6 53 25000 35 1149 6 12 1169 6 20 1186 6 29 1198 6 37 1205 6 45 Mixture Best Economy Cruise MAP 21 inHG Cruise RPM 2100 Press Alt Ft STD OAT C ISA 30 C NMI HRS ISA 15 C NMI HRS ISA 0 C NMI HRS ISA 15 C NMI HRS ISA 30 C NMI HRS 0 15 1124 8 12 1157 8 38 1189 8 68 1222 9 02 1253 9 39 4000 7 1177 8 00 1209 8 24 1241 8 51 1271 8 81 1302 9 14 8...

Page 165: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 69 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TIME FUEL DISTANCE to DESCEND Maintain 500 fpm Rate of Descent ...

Page 166: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 70 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TIME FUEL DISTANCE to DESCEND Maintain 1000 fpm Rate of Descent ...

Page 167: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 71 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 LANDING GROUND ROLL ...

Page 168: ...MOONEY M20TN MODEL TYPE S SECTION V PERFORMANCE 5 72 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 LANDING OVER 50 15m OBSTACLE ...

Page 169: ...TY MOMENT ENVELOPE 6 10 CENTER OF GRAVITY LIMITS ENVELOPE 6 11 FIXED BALLAST 6 12 EQUIPMENT LIST 6 12 NOTE The empty weight center of gravity and equipment list for the airplane as delivered section is valid for use with the airplane identified below when approved by Mooney International Corporation MOONEY M20TN MODEL TYPE S AIRCRAFT SERIAL NO AIRCRAFT REGISTRATION NO from Mooney International Cor...

Page 170: ...MOONEY M20TN MODEL TYPE S SECTION VI WEIGHT AND BALANCE 6 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 171: ...provides the empty weight and center of gravity data for the computation of individual loadings The empty weight and C G gear extended as delivered from the factory is tabulated on page 6 6 when this manual is supplied with the aircraft from the factory FAA regulations also require that any change in the original equipment affecting the empty weightand center ofgravitybe recorded in the AircraftLo...

Page 172: ...l boost pump until tank is empty REPEAT STEPS C AND D TO DRAIN OTHER TANK e Replace 3 0 gallons 11 4 liters fuel into each tank unusable fuel Use 5 82lb gal 69 Kg liter for 100LL fuel f Replace filler caps 3 Fill oil tank to capacity 8 qts 4 Position front seats in full forward position 5 Position flaps in full up position 6 Position a 2000 pound 907 2 Kg capacity scale under each of the three whe...

Page 173: ...rained of fuel has not been drained LBS Kg Weight Nose WN In cm mm Distance Between Main Nose Wheel Axle Centers LM N Total Weight of Aircraft WT CG Forward of Main Wheels LM a CG Forward of Main Wheels b CG Aft of Datum Station 0 13 In 33 0 cm 330 mm Distance from Center Nose Gear Trunnion to Center of Main Wheel Axles Horizontal LM R Distance from Nose Gear Trun nion to Datum Result of Computati...

Page 174: ...FROM AIRCRAFT LOG BOOK AIRPLANE MODEL SERIAL NO FAA REG NO DATE DESCRIPTON WEIGHT CHANGE ADDED REMOVED RUNNING EMPTY WEIGHT WT LBS Kg ARM INCHES CM MM MOMENT 1000 USEFUL LOAD BASIC EMPTY WEIGHT AS INCLUDES Mult Inches by 25 4 for mm Mult Inches by 2 54 for cm Mult Pounds by 4536 for Kg WT LBS Kg WT LBS Kg INCHES CM MM ARM ARM INCHES CM MM DELIVERED WT QTS LITERS OF MODIFICATION ...

Page 175: ...eat position Repeat procedure for co pilot and enter these weights and moment 1000 values in the proper sub columns in the Problem Form on page 6 8 9 Step 3 Proceed as in Step 2 to account for the passengers in seats 3 and 4 Enter the weight and value of moment 1000 in the proper columns Step 4 Again proceed as in Step 2 to account for the amount of fuel carried and enter the weight and moment 100...

Page 176: ... Rack Max 10 Lbs 4 54 Kg Sta 126 0 320 CM CONTINUE PROBLEM FORM ON NEXT PAGE 1009 2225 164 7 363 77 1 170 77 1 170 77 1 170 114 6 99 46 7 64 6 63 7 25 6 29 14 3 12 41 20 59 17 87 aft pos 2nd pos page 6 5 includes Full Oil 8 Qts 7 57 Li 1 875 Lbs Qt 80 Kg Li Sta 20 19 51 3 cm Oil sump assumed FULL for all flights Max Usable 386 1 Li 266 4 Kg Sta 49 23 125 cm Obtain the moment 1000 value for each se...

Page 177: ...84 3 186 1452 3200 190 2 165 0 9 53 8 27 180 6 156 7 of A C Max Weight A C will have to burn off 168 Lbs fuel before normal landing is accomplished loading is acceptable CAUTION DO NOT LAND A C WHEN OVER 3200 LBS EXCEPT IN AN EMERGENCY SITUATION CAUTION Pilot is responsible for cargo loaded in rear seat area with seat backs folded down Cargo Center of Gravity location varies with total weight load...

Page 178: ... A C WEIGHT Kg LBS LOAD AIRCRAFT MOMENT 1000 Kg MM 1528 1500 1452 1400 1300 1200 1100 1000 907 3368 3300 3200 3100 3000 2900 2800 2700 2600 2500 2400 2300 2200 2100 2000 LOADED AIRCRAFT WEIGHT 70 90 110 130 150 170 190 LOAD AIRCRAFT MOMENT 1000 POUND INCHES 2430 145 2 254 9 171 7 A C LOADED WITHIN THIS RANGE AREA ARE ABOVE NORMAL APPROVED LANDING WEIGHT FUEL MUST BE BURNED OFF PRIOR TO NORMAL LAND...

Page 179: ...0 2200 2400 2500 2600 2700 2100 2300 2800 2900 3000 3100 3200 3300 3368 1000 1100 1200 1300 1400 1500 1452 1528 41 42 43 44 45 46 47 48 49 50 51 A C WEIGHT 1050 1100 1150 1200 1250 1300 AIRCRAFT CG LOCATION L INCHES AFT OF DATUM STA 0 0 FORWARD LIMIT AFT LIMIT 2430 C G MRCG LIM LOADED AIRCRAFT WEIGHT 3368 lbs AIRCRAFT CG LOCATION L MM AFT OF DATUM STA 0 0 C G 3300 ...

Page 180: ... of this manual for the Mooney M20TN Only those items having an X in the Mark If Installed column and dated were installed at Mooney International Corporation at the time of manufacture If additional equipment is to be installed it must be done in accordance with the reference draw ing or a separate FAA approval NOTE Positive arms are distances aft of the airplane datum Negative arms are dis tance...

Page 181: ...SUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm A FIXED BALLAST WEIGHT 501 INSTL DESCRIPTION REF DRAWING NO DAY YEAR WEIGHT 503 INSTL WEIGHT 505 INSTL 1A 2A 3A 350203 350203 350203 2 81 6 08 8 94 6 2 13 4 19 7 532 1 209 50 532 1 209 50 532 1 209 50 MRSTN EQ A ...

Page 182: ...49 3 549 5 159 16 23 29 MRSTN EQ B1 STARTER ALTERNATOR EXHAUST INDUCT SYST ALT AIR ENG MT FULL OIL PROP GOV X Refer to Section I II for engine propeller configuration PROPELLER CONSTANT SPEED HARTZELL PHC J3YF 1RF F7498 W SPINNER 680038 34 02 75 0 125 7 49 5 2A PROPELLER CONSTANT SPEED HARTZELL PHC J3YF 1RF F7693DF 2 W SPINNER 680038 36 29 80 0 125 7 49 5 2C PROPELLER CONSTANT SPEED HARTZELL PHC J...

Page 183: ...CTION VI WEIGHT AND BALANCE 6 15 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm B POWERPLANT ACCESSORIES CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ B2 ...

Page 184: ...UX EQUIP 12v FUEL PUMP ELECTRIC BOOST STALL WARNING INDICATOR GEAR WARNING INDICATOR WING TIP STROBE LIGHT INSTL TAIL STROBE LIGHT INSTL LANDING TAXI LIGHTS 2 SETS ACTUATOR FLAPS 1C 2C 3C 4C 5C 6C 7C 8C 9C 10C 11C REFER TO APPLICABLE A C ELECTRICAL SCHEMATIC FOR COMPONENT INFORMATION 13 4 29 55 370 8 146 0 27 6 EA 41 28 16 25 52 1 15 106 3 41 85 08 17 49 53 19 5 86 1 9 38 1 15 0 45 1 0 127 0 50 0 ...

Page 185: ... INCHES cm C ELECTRICAL SYSTEM CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ C2 E L T AMERI KING AK 450 V REG VOLT REG 12C 13C 14C 15C 16C 17C 18C 19C 20C 810436 1 41 3 1 429 0 168 9 1 36 3 0 40 15 75 X ACTUATOR LANDING GEAR 5 08 11 2 99 06 39 0 X REFER TO APPLICABLE A C ELECTRICAL SCHEMATIC FOR COMPONENT INFORMATION E L T ARTEX ME406 1 85 4 07 378 84 149 15 810509 ...

Page 186: ...G 6 00 X 6 TYPE III 2 NOSE WHEEL ASSEMBLY 1 1D 2D 3D 4D 5D 6D 7D 520029 520029 540000 540000 1 92 4 24 153 74 60 53 8 2 18 0 162 51 63 98 1 36 3 0 33 8 13 3 2 4 5 3 33 8 13 3 X X X 8D TIRE NOSE 6 PLY RATING 5 00 X 5 TYPE III 1 MAIN WHEEL BRAKE DISC ASSYS 2 WHEEL ASSEMBLY 2 1 81 4 0 21 08 8 3 MASTER CYLINDER BRAKE 2 27 6 3 68 1 45 VALVE PARKING BRAKE 2 67 5 88 168 48 66 53 DUAL PUCK BRAKE CYL ASSY ...

Page 187: ...SECTION VI WEIGHT AND BALANCE 6 19 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm D WHEELS TIRES BRAKES CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ D2 ...

Page 188: ... EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm E INSTRUMENTS DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ E1 1E 4E 5E 6E 7E 8E 9E 83 1 84 41 91 16 5 X 10E INDICATOR TURN SLIP TURN COORD 49 1 07 36 0 14 17 ALTIMETER 32 70 47 75 18 8 INDICATOR AIRSPEED 11E X 2E 3E 12E 820358 820358 820358 ...

Page 189: ... INSTALLED WT LBS Kg ARM INCHES cm E INSTRUMENTS CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ E2 ALTERNATE STATIC AIR SOURCE 13E 16E 17E 18E 19E 20E 21E 14 0 31 44 99 18 5 X 22E ANNUNCIATOR PANEL MAGNETIC COMPASS 1 03 2 3 17 5 ELECT ARTIFICIAL HORIZON 3 IN 23E 820358 58 1 3 44 45 17 5 23 0 5 60 6 23 87 X X X 14E 15E 24E 820230 820360 820336 ...

Page 190: ...AND BALANCE 6 22 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm F MISCELLANEOUS SYSTEMS DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ F1 1F 4F 5F 6F 7F 8F 9F 10F 11F 2F 3F 12F ...

Page 191: ... CABIN ACCOMODATIONS DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ G1 RESTRAINT ASSY FWD 2 AMSAFE V23 SYSTEM 2 1G 4G 5G 6G 7G 8G 9G 2 27 5 0 106 7 42 0 3 91 8 61 FW 137 92 54 3 4 78 10 53 10G SUN VISORS 2 RESTRAINT ASSY REAR 2 130250 32 1 0 83 8 33 0 2 27 5 0 194 3 76 48 X X 2G 3G 140345 140345 140318 140318 11G 12G AMSAFE V23 SYSTEM 4 AFT 145 03 57 1 FW 137 92 54 3 AFT 156 72 61 7 ...

Page 192: ... Kg ARM INCHES cm H AVIONICS AUTOPILOTS DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ H1 GARMIN ADF KN 63 DME GARMIN GFC700 AUTOPILOT 1H 4H 5H 6H 7H 8H 9H 3 44 7 59 332 41 130 87 1 36 3 00 321 82 126 70 7 60 16 75 286 56 112 82 10H GARMIN G1000 GARMIN GDL 69 69A 11H 950300 38 08 83 95 208 28 82 00 1 28 2 93 350 01 137 80 X X 2H 3H 12H 950300 950300 950300 830153 ...

Page 193: ... LBS Kg ARM INCHES cm H AVIONICS AUTOPILOTS CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ H2 S TEC AUTO PILOT SYSTEM 55X W O AIR CONDITIONING 13H 16H 17H 18H 19H 7 39 16 29 179 17 70 54 7 39 16 29 186 03 73 24 20H W AIR CONDITIONING 2 81 6 20 334 47 131 68 S TEC ELECTRIC TRIM 0 60 1 31 67 51 26 58 REIFF ENGINE HEATER 21H 14H 15H 22H 830084 950303 830084 ...

Page 194: ...LANCE 6 26 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm H AVIONICS AUTOPILOTS CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ H3 23H 26H 27H 28H 29H 30H 31H 32H 33H 24H 25H 34H ...

Page 195: ...T MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm H AVIONICS AUTOPILOTS CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ H4 BOSE INTERFACE 35H 38H 39H 40H 41H 42H 43H X 44H 45H 36H 37H 810150 LOCATION WILL VARY NEGLIGIBLE ...

Page 196: ...TOWED 1I 4I 5I 6I 7I 8I 9I 09 1 332 7 131 0 04 05 332 7 131 0 04 16 332 7 131 0 27 1 0 332 7 131 0 X X X X 10I CARGO RESTRAINT BELTS 2 STOWED TOW BAR FOLDING STOWED JACK POINTS 2 STOWED 03 3 332 7 131 0 PITOT COVER STOWED 84 1 5 332 7 131 0 POH AFM NO 35 5 332 7 131 0 ENGINE OPERATOR S MANUAL CMI 11I 010037 1 03 2 6 273 1 107 5 07 1 332 7 131 0 X X X X X 2I 3I 12I ENGINE LOG BOOK 07 2 332 7 131 0 ...

Page 197: ... 38 1 15 0 1 48 3 27 332 7 131 0 X 10J AUX POWER RECEPTACLE INSTL ARM REST INSTL PILOT S SEAT LUMBAR SUPPORT INSTL 2 3 43 7 57 AUX POWER CABLE ADAPTER 1 38 3 05 38 1 15 0 DUAL BRAKE PEDAL INSTL STATIC DISCHARGE INSTL STATIC WICKS 11J 140295 95 2 1 87 6 34 5 99 2 18 88 9 35 0 X 2J 3J NORMALLY STOWED IN BAGGAGE COMPARTMENT BETWEEN ST 110 130 STEP ASSY INSTL 880042 950270 950253 950256 1 25 2 75 274 ...

Page 198: ...03 20 80 0 1 57 3 47 114 3 45 0 21J ANTI COLLISION BEACON FLASHING RED 39 87 24 1 9 5 DEFROSTER BLOWER NO CHANGE NO CHANGE 3 PASSENGER REAR BENCH SEAT 16 8 36 5 202 3 79 6 TKS AIRFRAME WINGS ONLY NO FLUID 22J 950272 48 1 06 215 9 85 0 274 3 108 0 13J 14J 23J TKS A F WINGS PROP KNOWN ICE NO FLUID 640315 140305 690007 690007 18 1 39 8 203 5 80 1 950301 140313 140323 140313 140323 TKS FLUID TANKS FUL...

Page 199: ... 28 56 347 98 137 0 33J OXYGEN SYSTEM 77 1 CU FT Avox Scott 51 GALLON CAPACITY USABLE FUEL TANKS 2 30 0 66 1 151 5 59 7 AIR CONDITIONER MINUS WTS 4 1 9 0 180 3 71 0 SPEEDBRAKE 2000 34J 210217 125 04 49 23 25J 26J 35J OXYGEN SYSTEM 115 7 CU FT Avox Scottt 770000 950286 870029 20 2 44 55 347 9 137 0 810447 870029 WX500 STORMSCOPE 374 45 3 34 1 52 50 GALLON CAPACITY USABLE FUEL TANKS 2 210217 125 04 ...

Page 200: ...LANCE 6 32 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm J OPTIONAL EQUIPMENT CONT DESCRIPTION REF DRAWING NO DAY YEAR MRSTN EQ J4 36J 39J 40J 41J 42J 43J 44J 45J 46J 37J 38J 47J ...

Page 201: ... 13 GROUND CONTROL 7 15 NOSE GEAR STEERING 7 15 TAXIING AND GROUND HANDLING 7 15 LANDING GEAR 7 15 CONSTRUCTION 7 15 RETRACTION SYSTEM 7 15 WHEEL BRAKES 7 16 EMERGENCY EXTENSION SYSTEM 7 16 WARNING SYSTEM 7 16 CABIN 7 16 BAGGAGE COMPARTMENT 7 16 CARGO RESTRAINT 7 17 SEATS 7 18 SEAT BELTS SAFETY HARNESS 7 18 DOORS WINDOWS EXITS 7 18 CABIN DOOR 7 18 PILOT S WINDOW 7 18 EMERGENCY EXITS 7 18 ENGINE 7 ...

Page 202: ...25 FUEL SYSTEM 7 26 ELECTRICAL SYSTEM 7 26 ALTERNATOR BATTERY 7 26 ESSENTIAL BUS 7 27 NON ESSENTIAL BUS 7 27 EQUIPMENT LOCATION 7 27 SCHEMATIC 7 28 CIRCUIT BREAKER PANEL 7 29 ACCESSORIES 7 30 ANNUNCIATOR PANEL 7 30 LIGHTING SYSTEM 7 30 INSTRUMENT PLACARD LIGHTS 7 30 MAP LIGHT 7 31 CABIN LIGHTING 7 31 EXTERIOR LIGHTING 7 31 CABIN ENVIRONMENT 7 32 HEATING VENTILATION SYSTEMS 7 32 PITOT PRESSURE STAT...

Page 203: ...pennage consists of the vertical and horizontal stabilizer assembly and the rudder and elevator surfaces The entire empennage pivots around attaching points on the aft fuselage to provide pitch attitude trim The tricycle landing gear allows maximum vision and ground maneuvering Hydraulic disc brakes and a steerable nose wheel aid in directional control during taxiing and ground opera tions The lan...

Page 204: ... electrically actuated with a split toggle switch on the control wheel for autopilot equipped aircraft The pitch trim may be manually actuated by a wheel located on the floor be tween the pilot and co pilot seat Trim actuation turns a ball screw that increases or decreases the pitch angle of the entire empennage The elevator trim position indicator located on the MFD depicts the position up down o...

Page 205: ...ency volume and squelch knob S Communications frequency set knobs S Communications frequency transfer button S Altimeter setting knob baro QNH set S Course knob S Map range knob and cursor control S FMS control buttons and knob S PFD softkey buttons including master warning caution acknowledgement S Altitude reference set knob S Heading bug control S Navigation frequency transfer button S Navigati...

Page 206: ...ntinuous uplink capabilities at any alti tude throughout North America Also available with the GDL 69A is XM s digital audio entertain ment which provides 130 plus channels of music news talk sports and information For detailed operating instructions see Garmin G 1000 Cockpit Reference Guide for the Mooney M20TN The TSO d KN 63 if installed is a complete 100 watt 200 channel remote DME system Dis ...

Page 207: ...ISSUE 04 02 2008 1 2 3 4 5 6 56 8 9 10 11 12 13 14 15 1617 1819 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 41 42 47 48 50 49 51 45 46 43 44 LOCATED ABOVE LOCATED IN LOCATED BEHIND GAU 10 XX MFD 55 GLARESHIELD HEADLINER 53 54 52 FIGURE 7 1 FLIGHT PANEL 31 0001 THRU 31 TBD Revision B 11 21 2014 ...

Page 208: ...turn coordinator displays variation in roll and yaw to the pilot by means of a damped miniature aircraft silhouette display this provides the pilot with es sential information to execute a proper turn 5 ANNUNCIATOR PANEL See description elsewhere in this SECTION 6 MAGNETIC COMPASS Magnetic compass dial is graduated in five degree increments and is encased in liquid filled glass and metal case It i...

Page 209: ...s wing tip and tail strobe lights ON Should a short occur the combination switch circuit breaker will automatically trip to the OFF position 17 NAVIGATION LIGHT NAV LITE SWITCH CIRCUIT BREAKER Navigation light combination switch circuit breaker turns wing tip and tail navigation lights ON Should a short occur the combination switch circuit breaker will automatically trip to the OFF position The gl...

Page 210: ...ncy Never run the boost pump without fuel in the system CAUTION Pushing HIGH BOOST pump switch ON when engine driven pump is operating proper ly will cause engine to quit due to excessive rich fuel mixture 25 BOOST PUMP SWITCH LOW BOOST The Low Fuel boost pump switch operates the fuel boost pump on low power to provide a means of suppressing fuel vapor from fuel system during hot day and high alti...

Page 211: ...E OFF flaps 10o Move switch to full down position to select FULL DOWN flaps 33o When flap switch is moved UP to either TAKEOFF position or FULL UP posi tion the flaps will retract to the selected position CAUTION Positioning Flap Switch to the UP position retracts the flaps completely 32 ALTERNATE STATIC SOURCE VALVE Pull alternate static source valve full aft to change source of static air for th...

Page 212: ... gear is NOT in the down position 41 PANEL LIGHT SWITCH AND DIMMER Turning panel light switch knob clockwise turns instrument lights located in glareshield ON Con tinued turning clockwise increases light intensity 42 CIRCUIT BREAKER PANEL See details elsewhere in this Section 43 44 CO PILOT S HEADSET JACKS 45 46 PILOT S HEADSET JACKS See description elsewhere in this section 47 EMERGENCY LOCATOR T...

Page 213: ...QUIPMENT SWITCHES MAP LIGHT SWITCH RHEOSTAT MIKE SWITCH ELECTRIC TRIM SWITCH if installed OPTIONAL AUTO PILOT SWITCHES are located in the pilot s control wheel 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 FIGURE 7 2 ANNUNCIATOR SWITCH PANEL ANNUNCIATOR SWITCH PANEL ANNUNCIATOR 1 PRESS TO TEST SWITCH Press RED press to test switch 3 5 sec with Master Switch ON to illuminate light bulbs some annunci...

Page 214: ... engine is drawn from inside cowling rather than through the induction air intake The normal induction air system MUST be checked for proper operation prior to next flight NOTE Induction of alternate air warm air will result in loss of power 9 PROP DE ICE Illuminates BLUE when Propeller De Ice has been selected ON 10 PITOT HEAT Illuminates BLUE when pilot has selected PITOT HEAT rocker switch ON S...

Page 215: ...TION Landinggear legsare constructedofchrome molybdenumtubular steel heat treated forgreat er strength and wear resistance Main gear leg attaching points pivot in bearing surfaces on for ward and stub spars The nose gear mounts on cabin tubular steel frame Rubber discs in all gear leg assemblies absorb shock of taxiing and landing RETRACTION SYSTEM Landing gear is electrically retracted and extend...

Page 216: ... DOWN and RED for GEAR UNSAFE and 2 VOICE ALERT activated when landing gear is not down and locked and throttle is approxi mately 1 4 inch from idle position The green light shows continuously when landing gear is fully extended The red light shows when ever landing gear is in transit or not locked down but is OFF when landing gear is fully retracted A visual gear position indicator located on flo...

Page 217: ...vis pins are to be inserted into holes provided in web of front seat rails The cargo belts attach to these rings and to standard seat belt harness to retain cargo Refer to Figure 7 3 for typical restraint CAUTION Proper loading and retention of cargo is mandatory See Loading Computation Graph SECTION VI SEAT BELT STD SEAT BELT REEL SINGLE POINT ADJUSTMENT FIGURE 7 4 INERTIAL REEL HARNESS RETENTION...

Page 218: ...s possible Rear seat occupants should take care to conform with this procedure in adjusting chest strap and inboard belt length This diagonal configuration places body center of gravity inside the triangle formed by chest strap and lap belt The lap belt should be adjusted comfortably tight As a result the body is restricted from rolling out toward the unrestricted shoulder or open side of the harn...

Page 219: ... viewed from the cockpit ENGINE CONTROLS The engine controls are centrally located between the pilot and co pilot on the engine control console The BLACK throttle knob regulates manifold pressure push the knob forward to in crease the setting pull the knob aft to decrease the setting The propeller control with its crowned BLUE knob controls engine RPM through the propeller governor Push the knob f...

Page 220: ...ne aviation gasoline Operational proce dures for adverse environmental conditions can be found in engine maintenance and operator s manual OIL SYSTEM The engine has a full pressure wet sump oil system with an 8 quart 7 57 liters capacity A con ventional dipstick is provided for determining oil quantity The oil system is depicted in Figure 7 5 The propeller governor boosts engine oil pressure for o...

Page 221: ...ber bushings in the drive gear turns the coupling drive lugs counter weighted latch pawls inside the coupling cover engage pins on the magneto case and hold back the latch plate until forced inward by the coupling cover When the latch plate is released the coupling spring spins the magneto shaft through its neutral position and the breaker opens to produce a high voltage surge in the secondary coi...

Page 222: ...N ENGINE INTERCOOLER LH INTERCOOLER RH FRONT OF AIRCRAFT LH TURBO RH TURBO AIR INLET LOWER COWL PLENUM UPPER COWL PLENUM FIGURE 7 6 AIR INDUCTION SYSTEM SCHEMATIC A secondary or alternate air source for combustion air is provided It has a door which normally remains closed and is held by a magnetic catch If the air filter or induction air inlet is restricted beyond a minimum allowable inlet pressu...

Page 223: ... used as reference for manual leaning Use the TIT gauge for this purpose The continuous flow system permits the use of a typical rotary vane pump with integral relief valve With this system there is no need for an intricate mechanism for timing fuel injection to the engine The fuel injector pump is equipped with a separator where vapor is separated by a swirl ing augmenter system from the liquid f...

Page 224: ...ed Warning bar indicates 1750 degrees Fahrenheit The TIT gauge is used as the primary source to lean fuel mixture PROPELLER HARTZELL THREE BLADE PHC J3YF 1RF F7498 or PHC J3YF 1RF F7498 B The B denotes a booted prop for TKS The propeller is a three blade 76 inch 193 cm diameter constant speed unit that features aluminum blades in an aluminum hub The spinner is fabricated from aluminum alloy A more...

Page 225: ...AIN LEFT FUEL TANK SELECTOR VALVE FIREWALL INDICATOR FUEL FLOW FUEL FLOW TRANSDUCER FUEL METERING UNIT FUEL PUMP ENGINE DRIVEN GASCOLATOR DRAIN ELECTRIC FUEL PUMP FILLER CAP VENT RIGHT FUEL QUANTITY LEFT FUEL QUANTITY INBOARD OUTLET RIGHT FUEL TANK DRAIN VALVE FILLER CAP SCREEN ASSY INDICATOR INDICATOR ASSY TRANSMITTER TRANSMITTER OUTBOARD TRANSMITTER VALVE VALVE VALVE INBOARD TRANSMITTER M20TN7 7...

Page 226: ...for proper use of the HIGH BOOST setting CAUTION Pushing HIGH BOOST pump switch ON when engine driven pump is operating proper ly will cause engine to quit due to excessive rich fuel mixture The BOOST PUMP Low Boost switch operates the fuel boost pump on low power to provide a means of suppressing fuel vapor from fuel system during hot day and high altitude conditions Low boost may also be used as...

Page 227: ...nd power Essential systems consisting of S G1000 system which is comprised of the PFD MFD AHRS ADC Com1 Nav1 GPS1 transponder audio panel and Engine Instruments S An independent standby attitude indicator artificial horizon S Aux Overhead Equipment Aux Panel Equipment and Ice Protection Activating the EMER BUS switch bypasses the master switch and electrically feeds the standby attitude indicator ...

Page 228: ...2 GPS2 TURN COORDINATOR NO 2 GIA 63 INTEGRATED AVIONICS GOODRICH WX 500 STORMSCOPE DIMMER CONTROL STEC SYSTEM 55X AFCS DIM SW BACKUP AIRSPEED BACKUP ALTITUDE ELEC STANDBY GYRO INSTRUMENT LIGHTING BACKUP HEADING WET COMPASS LIGHT 2A STBY 7 5A GLRSHLD 5A ADC 5A AHRS 5A ENGINE 5A MFD 5A PFD NO 1 GDU10 XX PFD NO 2 GDU10 XX MFD GEA71 ENGINE AIRFRAME GRS77 AHRS GDC74 AIR DATA GLARE SHIELD NO 1 GIA63 INT...

Page 229: ...ADC ENGINE INST CDU FAN AV FAN FLAP ACT MFD STBY GYRO ICE PROTECT SYS STBY BUS BAT TURN COORD SPEED BRAKE RUDDER TRIM ACT A C COM1 NAV1 GPS1 RADIO XPONDR COM2 NAV2 GPS2 HEAD SET1 HEAD SET2 ADF RADAR ALTIM DME WX TRAFFIC ALERT DATA LINK MUSIC IN E S S E N T I A L E S S E N T I A L FIGURE 7 9 CIRCUIT BREAKER PANEL TYPICAL CIRCUIT BREAKER PANEL See FIGURES 7 9 Illustration depicts typical C B panel m...

Page 230: ...function NOTE The circuit breakers installed in the panel may vary depending on installed equip ment ACCESSORIES Standard electrical accessories include the starter the electric fuel pump and the stall warning horn Electrical accessories include the navigation lights anti collision strobe lights instrument panel lighting and cabin courtesy lights Make sure the lighting and Emergency Bus switch as ...

Page 231: ...xcluding front seat passenger Front seat passenger s light switch is located forward of cabin door hinge on side panel CAUTION The Cabin Light rocker switches are connected directly to the battery Leaving the POWER LITES switch on indefinitely when the engine is shutdown will run down the batteries EXTERIOR LIGHTING Conventional navigation and high intensity strobe lights are installed on the wing...

Page 232: ...s provided for each cockpit seat on the cabin walls at knee height just forward of the front seats These valves are supplied directly by outside ram air Twist vent to adjust flow Tilt vent to direct flow CABIN VENT The CABIN VENT handle on the center console opens a valve that will mix fresh outside air with the cabin heat or defrost system Pull CABIN VENT knob to open When cabin heat is on interm...

Page 233: ...tion system and distributes this over the windshield interior surface any time the CABIN HEAT and or CABIN VENT valves are opened Pulling the DEFROST control full AFT decreases flow to the cabin turns the defroster blower ON and forces maximum air to flow through the defrost ducts PITOT PRESSURE STATIC SYSTEM A pitot tube mounted on lower surface of the left wing picks up ram air for air speed ind...

Page 234: ...een the pilot s and co pilot s seat for the convenience of all occupants Oxygen flows from the outlets only when a mask hose is connected Four partial re breathing type masks are provided each with vinyl plastic hoses and flow indicators The three passenger masks are of the disposable type The pilot s mask is a per manent type with a built in microphone for ease of radio communication while using ...

Page 235: ...tional disturbances Also the habitual and excessive use of tobacco or alcohol will usually necessitate the use of oxygen at less than 10 000 feet 1850 1800 1600 1400 1200 1000 800 600 400 200 YELLOW RED 30 000 27 500 25 000 22 000 20 000 17 500 15 000 12 500 10 000 FEET 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 GAUGE PRESSURE PSI 1 0 1 2 1 6 2 4 3 3 4 4 PLAN TO DESCEND BELOW 14 000 FT ALTITUDE DESC...

Page 236: ...FT CAPACITY FIGURE 7 13 AVOX OXYGEN DURATION CHART 77 1 CU FT The Avox oxygen system duration chart Fig 7 12 or Fig 7 13 should be used in determining the usable duration in hours of the oxygen supply in the airplane for the chosen cruising alti tude The following procedure outlines the method of finding the duration from the chart 1 Note the available oxygen pressure shown on the pressure gauge 2...

Page 237: ...ible from the battery access door on the right side of the tailcone The emergency locator transmitter meets the requirements of FAR 91 52 and is automatically activated by a longitudinal force of 5 to 7 g s The ELT transmits a distress signal on both 121 5 MHz and 243 0 MHz for a period of from 48 hoursin lowtemperature areasand up to 100 hoursin high temperature areas The unitoperates on a self c...

Page 238: ...turns to armed the switch is in the ARMED position NOTE If for any reason a test transmission is necessary the operator must first obtain permission from a local FAA or FCC representative or other applicable Authority or in accordance with current regulations Test transmission should be kept to a minimal duration Testing of ELT should be conducted only during the first five 5 minutes after any hou...

Page 239: ...ON 8 3 GROUND HANDLING 8 4 TOWING 8 4 TIEDOWN 8 4 JACKING 8 4 SERVICING 8 5 REFUELING 8 5 FUEL ADDITIVES 8 5 ENGINE LUBRICATION 8 6 INDUCTION AIR FILTER 8 6 GEAR AND TIRES 8 8 BATTERIES 8 8 HYDRAULIC BRAKE RESERVOIR SYSTEM 8 9 MAINTENANCE 8 9 ENGINE PERFORMANCE CHECKS 8 9 PROPELLER CARE 8 9 EXTERIOR CARE 8 9 INTERIOR CARE 8 10 AIRPLANE FILE 8 10 Revision B 11 21 2014 ...

Page 240: ...MOONEY M20TN MODEL TYPE S SECTION VIII HANDLING SERVICE AND MAINTENANCE 8 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 241: ...perform or supervise Reference should be made to FAR Part 43 for information regarding preventive maintenance which may be performed by a U S licensed pilot Itiswise to followa planned schedule oflubrication andpreventive maintenancebased onclima tic and flying conditions encountered in your locality Keep in touch with your Authorized Mooney Service Center and take advantage of his knowl edge and ...

Page 242: ...d outside Re movable wing tie down eye bolts supplied with the loose equipment screw into wing recep tacles marked HOIST POINT just outboard of each main gear Replace these eye bolts with jack point fixtures when it is necessary to lift the aircraft with jacks The tail tie down point is part of the tail skid To Tie Down Aircraft 1 Park the airplane facing the wind 2 Fasten the co pilot seat belt t...

Page 243: ...ing action of refueling process WARNING Allow five minutes after refueling for water and sediment to settle in tank and fuel drain valve before taking fuel samples or draining gascolator Tank sump drains are near each wing root forward of the wheel wells A small plastic cup is sup plied as loose equipment for obtaining fuel samples To collect a fuel sample insert cup actuator prong into sump drain...

Page 244: ...starter alter nator engine driven fuel and oil pumps oil cooler and propeller governor should be inspected for oil leaks and security Your Mooney Service Center will change engine oil in addition to performing allother service and inspection procedures needed when you bring your airplane in for its 50 hour 100 hour or annual inspections CAUTION Excessive oil sludge buildup indicates that the oil s...

Page 245: ...in color Begin re oiling the dry filter by applying a bead or line of red oil along the top only of each pleat of the filter The oil will soak into the length of each pleat It may be necessary to apply oil on filter material that has not received oil from the wicking action The entire filter medium must be covered with red oil DONOTOVEROIL Ifoildripsfromthefilter ithasbeenover oiled Allow the filt...

Page 246: ...at 42 PSI and the nose tire at 49 PSI for maximum service life Proper inflation will mini mize tire wear and impact damage Visually inspect tires during pre flight for cracks ruptures and worn spots Avoid taxi speeds that require heavy braking or fast turns Keep the gear and exposed gear retraction system components free of mud and ice to prevent retraction interfer ence and binding It is recommen...

Page 247: ...ion and maintenance vitally important Check blades for nicks cracks or indications of other damage before each flight Nicks tend to cause high stress concentrations in the blades which if ignored may result in cracks It is very important that all nicks and scratches be repaired prior to flight It is not unusual for propeller blades to have some end play or fore and aft movement as a result of manu...

Page 248: ...nels and headliner to remove as much surface dust and dirt as possible Spot clean Neather Leather with mild soap and water For stubborn stains use mild solvent such as FantastikR 409R Other type cleaners are not recommended at this time CAUTION Never use benzene carbon tetrachloride acetone or gasoline for cleaning Plexi glass or interior panels Carefully follow the manufacturer s instructions whe...

Page 249: ...SUE 04 02 2008 3 To be made available upon request a Airplane Log Book b Engine Log Book Since the regulations of other nations may require other documents and data owners of air planes not registered in the United States should check with their own aviation officials to deter mine their individual requirements ...

Page 250: ...MOONEY M20TN MODEL TYPE S SECTION VIII HANDLING SERVICE AND MAINTENANCE 8 12 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 251: ...YPE S SECTION IX SUPPLEMENTAL DATA 9 1 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 TABLE OF CONTENTS TITLE SECTION INTRODUCTION 9 3 THE SUPPLEMENTS INSERTED INTO THIS SECTION ARE FAA APPROVED SUPPLEMENT INSERTED DATE ...

Page 252: ...MOONEY M20TN MODEL TYPE S SECTION IX SUPPLEMENTAL DATA 9 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 SUPPLEMENT INSERTED DATE ...

Page 253: ...dures Emergency Procedures and effects on performance for certain optional equipment installed in the airplane are con tained in this section Commonly installed items of optional equipment whose function and operation do not require detailed instructions are described by Section VII The supplements are Approved by the FAA prior to incorporation into the Airplane Flight Manual ...

Page 254: ...MOONEY M20TN MODEL TYPE S SECTION IX SUPPLEMENTAL DATA 9 4 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 255: ... 10 6 INSPECTIONS MAINTENANCE 10 6 SPECIAL CONDITIONS CAUTIONARY NOTICE 10 6 WALK AROUND INSPECTIONS 10 7 COCKPIT CHECKS 10 7 FLIGHT OPERATIONS 10 7 GENERAL 10 7 TURBULENT WEATHER 10 7 FLIGHT IN TURBULENT AIR 10 8 MOUNTAIN FLYING 10 8 VFR LOW CEILINGS 10 8 VFR AT NIGHT 10 8 VERTIGO DISORIENTATION 10 9 STALLS SPINS AND SLOW FLIGHT 10 9 STANDARD PROCEDURE SPIN RECOVERY 10 10 VORTICES WAKE TURBULENCE...

Page 256: ...MOONEY M20TN MODEL TYPE S SECTION X SAFETY INFORMATION 10 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 04 02 2008 BLANK ...

Page 257: ...misplaced If any are missing replacements should be ob tained from any Authorized Mooney Service Center as soon as possible For your added protection and safety we have added this special section to the Pilot s Operating Handbook to refresh your knowledge of a number of safety subjects You should review these subjects periodically Topics in this section are mostly excerpts from FAA Documents and o...

Page 258: ... loading and C G are within limits 8 Be sure articles and baggage are secured 9 Check freedom of all controls 10 Maintain appropriate airspeed in take off climb descent and landing 11 Avoid other aircraft wake turbulence 12 Switch fuel tanks before engine starvation occurs 13 Practice engine out emergency landing gear extension and other emergency procedures at safe altitude preferably with a chec...

Page 259: ... action Fuel requirements Flight rules Maintenance preventative maintenance alterations inspections and maintenance records These are only some of the topics covered It is the owner s and pilot s responsibility to be thor oughly familiar with all items in FAR Part 91 and to follow them FEDERAL AVIATION REGULATIONS PART 39 AIRWORTHINESS DIRECTIVES This document specifies that no person may operate ...

Page 260: ...ffect of temperature and pressure altitude must be taken into account in determining performance if not accounted for on the charts Appli cable FAA manuals must be aboard the airplane at all times including the weight and balance forms and equipment lists The airplane must be loaded so as not to exceed the weight and the weight and balance loading center of gravity c g limitations Also that at lea...

Page 261: ...gauges Altimeter setting checked FLIGHT OPERATIONS GENERAL The pilot should be thoroughly familiar with all information published by the manufacturer con cerning the airplane The pilot is required by FAA to operate in accordance with the FAR s and the FAA Approved Airplane Flight Manual and or placards installed TURBULENT WEATHER A complete weather briefing prior to beginning a flight is the start...

Page 262: ...ar the lee slopes If the wind velocity at the level of the ridge exceeds 50 knots a strong mountain wave is probable with strong up and down drafts and severe or extreme turbulence The worst turbulence will be en countered in and below the rotor zone which is usually 8 to 10 miles down wind from the ridge This zone is characterized by the presence of roll clouds if sufficient moisture is present a...

Page 263: ...e in excess of 6 000 feet above ground level Spins may be dangerous and should be avoided In fact most airplanes are placarded against inten tional spins Spins are preceded by stalls A prompt and decisive stall recovery protects against inadvertent spins All airplanes are required to have flight characteristics that give adequate ad vance warning of an impending stall or they must be equipped with...

Page 264: ...and may extend several miles behind the airplane Plan to fly slightly above or to the up wind side of the other airplane s flight path Because of the wide variety of conditions that can be encountered there is no set rule to follow to avoid wake turbulence in all situations However the Aeronautical Information Manual goes into considerable detail for a number of wake turbulence avoidance procedure...

Page 265: ...ll manifest itself A major early symp tom of hypoxia is an increased sense of well being referred to as euphoria This progresses to slow reactions impaired thinking ability unusual fatigue and dull headache feeling Symptomsare slowbutprogressive insidiousin onset and aremostmarkedataltitudesstarting above 10 000 feet Night vision however can be impaired starting at altitudes lower than 10 000 feet...

Page 266: ...sed prior to take off for your system to rid itself of this excess gas you may experience the bends at altitudes even under 10 000 feet where most light planes fly ADDITIONAL INFORMATION In addition to the coverage of subjects in this section the National Transportation Safety Board and the FAA periodically issue general aviation pamphlets concerning aviation safety and in greater detail These can...

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