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MOONEY

M20V ACCLAIM ULTRA

SECTION III

EMERGENCY PROCEDURES

3 - 1

AIRPLANE FLIGHT MANUAL

ORIGINAL ISSUE - 03-16-2017

TABLE OF CONTENTS

TITLE

SECTION

. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .

INTRODUCTION

3- 3

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AIRSPEEDS FOR EMERGENCY OPERATIONS

3- 4

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GARMIN G1000 ANNUNCIATOR PANEL WARNING LIGHTS

3- 4

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ENGINE

3- 13

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ENGINE POWER LOSS - DURING TAKEOFF ROLL

3- 13

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ENGINE POWER LOSS - IMMEDIATELY AFTER LIFTOFF (Below 400 Ft AGL)

3- 13

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ENGINE POWER LOSS - DURING FLIGHT (ABOVE 400 FEET AGL)

3- 13

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ENGINE POWER LOSS, SUSTAINED NEGATIVE ”g” LOADING

3- 14

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AFTER ENGINE RE- START

3- 15

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EMERGENCY LANDING WITHOUT ENGINE POWER

3- 15

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EMERGENCY LANDING WITH THROTTLE STUCK AT IDLE POWER

3- 16

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PRECAUTIONARY LANDING WITH ENGINE POWER

3- 16

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POWER LOSS - PRIMARY ENGINE INDUCTION AIR SYSTEM BLOCKAGE

3- 16

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TURBOCHARGER FAILURE

3- 17

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TURBOCHARGER OVERBOOST

3- 18

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ENGINE ROUGHNESS

3- 18

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HIGH CYLINDER HEAD TEMPERATURE

3- 18

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HIGH OIL TEMPERATURE

3- 18

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LOSS OF OIL PRESSURE

3- 19

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ENGINE DRIVEN FUEL PUMP FAILURE

3- 19

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FUEL VAPOR SUPPRESSION (FLUCTUATING FUEL FLOW)

3- 19

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FIRES

3- 20

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ENGINE FIRE ON GROUND DURING STARTUP

3- 20

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ENGINE FIRE IN- FLIGHT

3- 20

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ELECTRICAL FIRE - IN FLIGHT (SMOKE IN CABIN)

3- 20

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EMERGENCY DESCENT PROCEDURE

3- 21

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GLIDE

3- 22

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FORCED LANDING EMERGENCY

3- 22

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GEAR RETRACTED OR EXTENDED

3- 22

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OVERWEIGHT LANDING PROCEDURE

3- 23

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SYSTEMS EMERGENCIES

3- 23

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PROPELLER OVERSPEED

3- 23

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ALTERNATOR OVERVOLTAGE

3- 23

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ALTERNATOR OUTPUT LOW

3- 23

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ALTERNATOR FAILURE

3- 24

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AVIONICS EMERGENCIES

3- 25

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PFD OR MFD DISPLAY FAILURE

3- 25

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AHRS FAILURE

3- 25

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AIR DATA COMPUTER (ADC) FAILURE

3- 25

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ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS

3- 26

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Revision A: 08-18-2017

Summary of Contents for M20V Acclaim Ultra

Page 1: ...920 MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road Kerrville Texas 78028 tel 830 896 6000 www mooney com ORIGINAL ISSUE 03 16 2017 Copyright 2017 All Rights Reserved AND FAA APPROVED AIRPLANE FLI...

Page 2: ...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 3: ......

Page 4: ...RATION NUMBER FAA APPROVED Jim Grigg Manager Aircraft Certification Office FEDERAL AVIATION ADMINISTRATION 10101 Hillwood Parkway Fort Worth Texas 76177 DATE 03 16 2017 FAA APPROVED in Normal Category...

Page 5: ...MOONEY M20V BLANK...

Page 6: ...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...

Page 7: ...MOONEY M20V ACCLAIM ULTRA INTRODUCTION BLANK...

Page 8: ...ISSUE 1 3 ORIGINAL ISSUE 1 4 ORIGINAL ISSUE 1 5 ORIGINAL ISSUE 1 6 08 18 2017 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...

Page 9: ...24 08 18 2017 3 25 08 18 2017 3 26 08 18 2017 3 27 08 18 2017 3 28 08 18 2017 3 29 08 18 2017 3 30 08 18 2017 4 1 ORIGINAL ISSUE 4 2 ORIGINAL ISSUE 4 3 ORIGINAL ISSUE 4 4 ORIGINAL ISSUE 4 5 ORIGINAL I...

Page 10: ...L ISSUE 5 31 ORIGINAL ISSUE 5 32 ORIGINAL ISSUE 5 33 ORIGINAL ISSUE 5 34 ORIGINAL ISSUE 5 35 ORIGINAL ISSUE 5 36 ORIGINAL ISSUE 5 37 ORIGINAL ISSUE 5 38 ORIGINAL ISSUE 5 39 ORIGINAL ISSUE 5 40 ORIGINA...

Page 11: ...NAL ISSUE 6 15 ORIGINAL ISSUE 6 16 ORIGINAL ISSUE 6 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 08 18...

Page 12: ...7 35 ORIGINAL ISSUE 7 36 ORIGINAL ISSUE 8 1 ORIGINAL ISSUE 8 2 ORIGINAL ISSUE 8 3 ORIGINAL ISSUE 8 4 ORIGINAL ISSUE 8 5 ORIGINAL ISSUE 8 6 ORIGINAL ISSUE 8 7 ORIGINAL ISSUE 8 8 ORIGINAL ISSUE 8 9 ORIG...

Page 13: ...MOONEY INTRODUCTION M20V ACCLAIM ULTRA vi POH AFM POH 003920 This POH AFM effective with S N 33 0001 AND ON ORIGINAL ISSUE 03 16 2017 BLANK...

Page 14: ...N POH AFM POH 003920 ORIGINAL ISSUE 03 16 2017 vii LOG OF REVISIONS REVISION LETTER REVISED PAGES FAA APPROVED DATE ORIGINAL ISSUE ALL 3 16 2017 Revision A See Narrative Discussion of Revisions Page v...

Page 15: ...number A 3 4 Added LOW MAN PRESS Annunciation A 3 5 Revised ACTION WHEN ON spelled out names A 3 6 thru 3 11 7 13 Revised and Added Alert Annunciation Images A 3 5 thru 3 30 Page numbering has change...

Page 16: ...6 2017 ix 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 MAINT...

Page 17: ...MOONEY M20V ACCLAIM ULTRA INTRODUCTION ORIGINAL ISSUE 03 16 2017 x BLANK...

Page 18: ...NTRY DIMENSIONS 1 7 BAGGAGE SPACE ENTRY DIMENSIONS 1 7 SPECIFIC LOADINGS 1 7 IDENTIFICATION PLATE 1 8 OXYGEN SYSTEM 1 8 GARMIN G1000 1 8 SYMBOLS ABBREVIATIONS TERMINOLOGY 1 9 GENERAL AIRSPEED TERMINOL...

Page 19: ...MOONEY M20V ACCLAIM ULTRA SECTION I GENERAL 1 2 ORIGINAL ISSUE 03 16 2017 AIRPLANE FLIGHT MANUAL BLANK...

Page 20: ...0V ACCLAIM ULTRA SECTION I GENERAL 1 3 ORIGINAL ISSUE 03 16 2017 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 TH...

Page 21: ...s definitions of 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 airwor...

Page 22: ...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 25...

Page 23: ...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...

Page 24: ...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 speci...

Page 25: ...e audio panel is used for selection 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 ena...

Page 26: ...tended 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 the...

Page 27: ...volutions 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...

Page 28: ...hord 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...

Page 29: ...lents 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...

Page 30: ...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...

Page 31: ...s of critical impor tance and concerns procedures and techniques which could cause or result in personal injury or death if not carefully followed WARNING The use of the Caution symbol means informati...

Page 32: ...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...

Page 33: ...MOONEY M20V ACCLAIM ULTRA SECTION II LIMITATIONS 2 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 34: ...served to allow for the air speed calibration variations between the normal and alternate static sources as shown in SECTION V When the alternate static system source is first opened there will be an...

Page 35: ...g 2232 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 spee...

Page 36: ...band 20 KIAS 59 KIAS Low speed awareness stall is imminent Yellow band 59 KIAS 66 KIAS Lower limit of white band approaching stall White band 66 KIAS 110 KIAS Operating range with flaps in all extend...

Page 37: ...eoff 100 F 38 C Recommended Cruising Oil Temperature 170 F 220 F 76 7 C 104 4 C Maximum Manifold Pressure 33 5 Inches of Hg Oil Pressure Normal Operating 30 100 PSI Minimum IDLE ONLY 10 PSI Maximum Al...

Page 38: ...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...

Page 39: ...condi tions of temperature and humidity water can be present in fuel in sufficient quanti ties to create ice formations within the fuel system To prevent this add Anhydrous ISOPROPYL Alcohol to the fu...

Page 40: ...ld 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 pressure is...

Page 41: ...AL 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 ALTERNATE STATIC SOURCE 5 1 1 1 Equipment must...

Page 42: ...lan to ensure correct flight plan sequencing and guidance 2 The GARMIN G1000 must utilize the following or later FAA approved software versions The database version should be 0401 35 or later FAA appr...

Page 43: ...must be op erational e VNAV information may be utilized for advisory information only Use of VNAV information for Instrument Approach Procedures does not guarantee step down fix altitude protection o...

Page 44: ...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 Displ...

Page 45: ...TNING DETECTION EQUIPMENT NOT TO BE USED FOR THUNDERSTORM AREA PENETRATION OPTIONAL ON INSTRUMENT PANEL ON INSTRUMENT PANEL ENGRAVED ON INSTRUMENT PANEL CONTROL YOKE OPTIONAL WHEN ORDERING DECALS PLAC...

Page 46: ...N THIS COMPARTMENT USE FOR STOWAGE OF LIGHT SOFT ARTICLES ONLY SEE AIRCRAFT LOADING SCHEDULE DATA FOR BAGGAGE COMPARTMENT ALLOWABLE BAGGAGE COMPARTMENT ON HAT RACK SHELF WARNING DO NOT EXCEED 120 LBS...

Page 47: ...RACTING LOCK PIN 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 ABOVE INSIDE BAGGAGE DOOR HANDLE FUEL DRAIN PULL OPE...

Page 48: ...h backlit reverse engraved nomen clature relevant to proper operation of the airplane Replacement panels are available through any Authorized Mooney Service Center also refer to the M20V Illustrated P...

Page 49: ...FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE 03 16 2017 RH DETAIL SHOWN LOWER INSTRUMENT ELECTROLUMINESCENT PANEL 150111 13 W TKS OPTION SHOWN 150111 15 W AIR CONDITION OPTION LH DETAIL RH DETAIL 150111...

Page 50: ...ney Service Parts Dept MAINTAIN LEVEL HERE HYDRAULIC OIL RESERVOIR 28 VOLTS ONLY BACKSIDE OF AUX PWR RECEPTACLE DOOR USE AVIATORS OXYGEN ONLY SEE PILOT S OPERATING HANDBOOK FOR FILLING PRESSURES INSID...

Page 51: ...GEAR LEG ASSEMBLY WARNING DO NOT EXCEED TOWING LIMITS ON NOSE LANDING GEAR SPINDLE ASSEMBLY 150110 B2012 WHITE CUTOUT ON WING EACH SPEEDBRAKE LOCATION OPTIONAL Electronically Acutated DO NOT MANUALLY...

Page 52: ...E FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TOP LEFT RIGHT WINGS AT FUEL FILLERS TOP LEFT RIGHT WINGS AT FUEL FILLERS UNDER WING NEAR SUMP DRAINS 150110 A2025B CLEAR W BLACK TEXT 150110 B2007B 150110 B2...

Page 53: ...MOONEY M20V ACCLAIM ULTRA SECTION II LIMITATIONS 2 22 AIRPLANE FLIGHT MANUAL FAA APPROVED ORIGINAL ISSUE 03 16 2017 BLANK...

Page 54: ...ENGINE INDUCTION AIR SYSTEM BLOCKAGE 3 16 TURBOCHARGER FAILURE 3 17 TURBOCHARGER OVERBOOST 3 18 ENGINE ROUGHNESS 3 18 HIGH CYLINDER HEAD TEMPERATURE 3 18 HIGH OIL TEMPERATURE 3 18 LOSS OF OIL PRESSURE...

Page 55: ...GEAR TO RETRACT 3 27 GEAR FAILS TO RETRACT GEAR WARNING VOICE ALERT SOUNDING 3 27 WHEN READY TO EXTEND LANDING GEAR 3 27 GEAR FAILS TO RETRACT GEAR WARNING VOICE ALERT DOES NOT SOUND 3 27 WHEN READY T...

Page 56: ...on 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 t...

Page 57: ...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 KIAS EMERGENCY DESCENT GEAR DOWN Smooth Air 165 KIAS Turbulent Air 3368 lb 1528 kg 127...

Page 58: ...at system has failed STEADY AMBER PITOT HEAT FAIL OFF WHEN PITOT HEAT SWITCH IS SELECTED OFF ALTERNATOR FAIL RED RED ALTERNTR FAIL when Al ternator output goes to zero or when Field shorts NOTE Volt m...

Page 59: ...ISSUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D GEAR DOWN ALERT ANNUNCIATION GEAR UNSAFE MASTER WARNING GEAR UNSAFE ALERT ANNUNCIATION GEAR UNSAFE ALERT ANNUNCIATION IN TRANSITIO...

Page 60: ...NAL ISSUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D ALTERNATE AIR ALERT ANNUNCIATION PROP DE ICE FAIL MASTER CAUTION PROP DE ICE FAIL ALERT ANNUNCIATION PITOT HEAT FAIL MASTER CA...

Page 61: ...L ORIGINAL ISSUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D ALTERNATOR FAIL MASTER WARNING ALTERNATOR FAIL ALERT ANNUNCIATION DOOR OPEN ALERT ANNUNCIATION DOOR OPEN MASTER WARNING...

Page 62: ...SUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D START POWER ALERT ANNUNCIATION LOW BOOST PUMP ALERT ANNUNCIATION HIGH BOOST PUMP ALERT ANNUNCIATION HIGH BOOST PUMP MASTER CAUTION L...

Page 63: ...HT MANUAL ORIGINAL ISSUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D LOW FUEL CAUTION LEFT GAUGE LOW FUEL WARNING LH RH CAS ALERT LOW FUEL CAUTION LEFT CAS ALERT LOW FUEL CAUTION R...

Page 64: ...II EMERGENCY PROCEDURES 3 11 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS CONT D LRU REPLACEMENT MESSAGE SYSTEM CONFIG ERROR TCAS FAIL DATA PATH FAIL...

Page 65: ...d approach upon receipt of this message from the G1000 Navigation guidance will continue for 5 minutes al lowing the pilot to initiate the missed approach while maintaining course guidance on the fina...

Page 66: ...portant 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 ba...

Page 67: ...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...

Page 68: ...r 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 fail...

Page 69: ...eto Switch OFF LOW Boost Pump Verify OFF Braking AS REQUIRED TO STOP AIRCRAFT If necessary use fire extinguisher to keep fire out of cabin area POWER LOSS PRIMARY ENGINE INDUCTION AIR SYSTEM BLOCKAGE...

Page 70: ...lly 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...

Page 71: ...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 roughn...

Page 72: ...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 wh...

Page 73: ...ch 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 H...

Page 74: ...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...

Page 75: ...368 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 attain...

Page 76: ...continued airwor thiness requirements post flight ALTERNATOR OVERVOLTAGE Alternator warning light illuminated Red steady and Alternator Field circuit breaker tripped Alternator Field Circuit Breaker R...

Page 77: ...in powered and functional 3 If the RED ALT VOLTS annunciator remains flashing then If the RED ALT VOLTS annunciation remains flashing then the standby alternator has failed and only main battery power...

Page 78: ...l equipment 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 Re...

Page 79: ...is 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 I...

Page 80: ...XT 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 EXTEND ELECTRICALLY previous page OXYGEN In the event...

Page 81: ...nciation will display and it may come unlatched in flight This may occur during or after take off The door may open to its full open position and then take an intermediate position depending upon spee...

Page 82: ...inch or more on the airframe be prepared for a significant increase in aircraft weight and drag This will result in significantly reduced cruise and climb performance and higher stall speeds Plan for...

Page 83: ...o 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 aircr...

Page 84: ...ER ENGINE START 4 10 BEFORE TAXI 4 10 Standby Alternator Preflight Check 4 10 Oxygen System 4 10 Standby Alternator Checks Complete 4 10 TAXI 4 10 MINOR SPARK PLUG FOULING 4 11 BEFORE TAKEOFF 4 12 TAK...

Page 85: ...MOONEY M20V ACCLAIM ULTRA SECTION IV NORMAL PROCEDURES 4 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 86: ...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...

Page 87: ...keoff 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...

Page 88: ...tmeter 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...

Page 89: ...E CAP NOTE The optional visual fuel quantity gauge is to be used for partial refueling purpos es only DO NOT use for preflight quantity check Tiedown Rope Chain REMOVE Wheel Chock REMOVE Left Main Lan...

Page 90: ...sual fuel quantity gauge is to be used for partial refueling purpos es only DO NOT use for preflight quantity check Tiedown Rope Chain REMOVE Fuel Tank Vent UNOBSTRUCTED Landing Taxi Lights INSPECT Le...

Page 91: ...or Field Switch OFF Fuel Boost Pump Switches OFF Circuit Breakers Check All In Rocker Switches OFF Alternate Static Source Push OFF Throttle Closed Propeller Full Forward High RPM Mixture Idle Cut OFF...

Page 92: ...batteries for at least one hour at 3 4 amps before starting engine Only No 1 battery left side of tailcone is connected to the Auxiliary Power plug NORMAL ENGINE START Before Starting Check List COMP...

Page 93: ...ht is OFF and the system is charging Position and Anti collision Lights SET AS REQUIRED Radios and Required Avionics SET AS REQUIRED BEFORE TAXI Engine Start Checklist Completed Elevator Trim Switch O...

Page 94: ...isregard the importance of pre takeoff magneto checks When operating on a single ignition some RPM drop should always occur Normal indications are 25 to 75 RPM and a slight engine roughness as each ma...

Page 95: ...on battery ammeter Verify red ALT VOLTS light extinguishes Reset BATT Circuit Breaker Stdby Alt Emerg Bus switch OFF Verify red ALT VOLTS light illuminates Alt Field Switch ON Verify red ALT VOLTS lig...

Page 96: ...rom the propeller area instead of being pulled into it TAKEOFF NORMAL Mixture FULL RICH Power ADVANCE SLOWLY TO FULL RPM 2500 RPM Watch manifold pressure adjust throttle as required to avoid overboost...

Page 97: ...e 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 C...

Page 98: ...e 12 000 ft the minimum manifold pressure is 15 in Hg and the minimum RPM is 2 200 Do not pull the throttle back to idle without leaning mixture appropriately above 12 000 ft The lack of manifold pres...

Page 99: ...ng REF SECTION VI It will require a minimum of one hour of flight before a permissible land ing weight is attained when takeoffs are made at maximum gross weight If landing at a weight exceeding maxim...

Page 100: ...NG NORMAL Approach for Landing Check list COMPLETED Approach Airspeed As specified in SECTION V Landing Distance Touchdown MAIN WHEELS FIRST aligned w runway Landing Roll LOWER nose wheel gently Brake...

Page 101: ...ey removed Master Switch VERIFY OFF Electrical Switches VERIFY OFF Interior Light Switches VERIFY OFF Emergency Bus Switch VERIFY OFF Parking Brake RELEASE Install wheel chocks Extended Parking Contro...

Page 102: ...ALIBRATION PRIMARY STATIC 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 ST...

Page 103: ...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...

Page 104: ...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 mi...

Page 105: ...Example 160 KIAS ISA 20 C 25000 correction 2 5 0 04 2 5 2 6 KTAS REMOVABLE STEPS The cruise speed tables herein were established with the aircraft step removed Aircraft equipped with a removable step...

Page 106: ...SECTION V PERFORMANCE 5 5 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 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...

Page 107: ...5 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 K...

Page 108: ...lean 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...

Page 109: ...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 KCA...

Page 110: ...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 105 Flap Gear Down 50 50...

Page 111: ...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 105 Flap Gear Down 50 5...

Page 112: ...ic System Power On 335 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...

Page 113: ...0 120 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...

Page 114: ...0 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...

Page 115: ...5 60 2 0 7 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...

Page 116: ...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 i...

Page 117: ...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 K...

Page 118: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 17 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TAKEOFF DISTANCE GROUND ROLL...

Page 119: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 18 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TAKEOFF DISTANCE OVER 50 15m OBSTACLE...

Page 120: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 19 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 RATE OF CLIMB AT Vy...

Page 121: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 20 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 RATE OF CLIMB at 120 KIAS CRUISE CLIMB...

Page 122: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 21 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TIME FUEL DISTANCE to CLIMB at Vy...

Page 123: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 22 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TIME FUEL DISTANCE to CLIMB at 120 KIAS...

Page 124: ...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...

Page 125: ...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 18...

Page 126: ...f 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 l...

Page 127: ...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 DISA 30 59 5C 0 28 5C 3...

Page 128: ...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 DISA 30 51 5C 0 20 5C 30...

Page 129: ...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 DISA 30 43 5C 0 12 5C 30...

Page 130: ...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 DISA 30 35 5C 0 4 5C 3...

Page 131: ...8 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 DISA 30 27 5C 0 3 5C...

Page 132: ...8 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 DISA 30 19 5C 0 11 5C...

Page 133: ...KTAS 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...

Page 134: ...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 DISA 30 51 5C 0 20 5C 3...

Page 135: ...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 DISA 30 51 5C 0 20 5C...

Page 136: ...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 DISA 30 43 5C 0 12 5C 3...

Page 137: ...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 DISA 30 35 5C 0 4 5C...

Page 138: ...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 DISA 30 27 5C 0 3 5C...

Page 139: ...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 DISA 30 19 5C 0 11 5...

Page 140: ...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 nm...

Page 141: ...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 OA...

Page 142: ...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...

Page 143: ...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...

Page 144: ...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...

Page 145: ...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 OA...

Page 146: ...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...

Page 147: ...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...

Page 148: ...8 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 NM...

Page 149: ...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...

Page 150: ...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...

Page 151: ...4000 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 H...

Page 152: ...00 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 HR...

Page 153: ...0 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...

Page 154: ...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 3...

Page 155: ...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 90 gal useable 217 kts 20 1 gph x 10 gal 108 nm...

Page 156: ...0 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 O...

Page 157: ...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...

Page 158: ...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...

Page 159: ...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...

Page 160: ...1 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 O...

Page 161: ...4000 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 H...

Page 162: ...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 HR...

Page 163: ...000 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 3...

Page 164: ...000 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 HR...

Page 165: ...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...

Page 166: ...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...

Page 167: ...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...

Page 168: ...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...

Page 169: ...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...

Page 170: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 69 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TIME FUEL DISTANCE to DESCEND Maintain 500 fpm Rate of Descent...

Page 171: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 70 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TIME FUEL DISTANCE to DESCEND Maintain 1000 fpm Rate of Descent...

Page 172: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 71 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 LANDING GROUND ROLL...

Page 173: ...MOONEY M20V ACCLAIM ULTRA SECTION V PERFORMANCE 5 72 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 LANDING OVER 50 15m OBSTACLE...

Page 174: ...OMENT 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 va...

Page 175: ...MOONEY M20V ACCLAIM ULTRA SECTION VI WEIGHT AND BALANCE 6 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 176: ...Corporation 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...

Page 177: ...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...

Page 178: ...ined 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...

Page 179: ...ROM 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 INCL...

Page 180: ...seat 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 pa...

Page 181: ...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 8 52 7 40 7 25 6 29 14 3 12 41 20 59 17 87 aft pos 2nd pos page 6...

Page 182: ...528 3368 84 3 186 1452 3200 191 1 165 8 9 53 8 27 181 5 157 53 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...

Page 183: ...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 11...

Page 184: ...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 LOCA...

Page 185: ...of this manual for the Mooney M20V 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 eq...

Page 186: ...AL ISSUE 03 16 2017 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 3...

Page 187: ...50 G INCLUDES DESCRIPTION REF DRAWING NO DAY YEAR 1B 3B 600292 249 3 549 5 159 16 23 29 STARTER ALTERNATOR EXHAUST INDUCT SYST ALT AIR ENG MT FULL OIL PROP GOV X Refer to Section I II for engine prope...

Page 188: ...NE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm B POWERPLANT ACCESSORIES CONT DESCRIPTION REF DRAWING NO DAY YEAR 0 60 1 31 67 51 26 58...

Page 189: ...P 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 1...

Page 190: ...g ARM INCHES cm C ELECTRICAL SYSTEM CONT DESCRIPTION REF DRAWING NO DAY YEAR 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...

Page 191: ...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...

Page 192: ...LTRA SECTION VI WEIGHT AND BALANCE 6 19 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm D WHEELS TIRES BRAKES CONT DESCRIPTION RE...

Page 193: ...MARK IF INSTALLED WT LBS Kg ARM INCHES cm E INSTRUMENTS DESCRIPTION REF DRAWING NO DAY YEAR 1E 4E 5E 6E 7E 8E 9E 83 1 84 41 91 16 5 10E INDICATOR TURN SLIP TURN COORD 49 1 07 36 0 14 17 ALTIMETER 32 7...

Page 194: ...HT AND BALANCE 6 21 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm E INSTRUMENTS CONT DESCRIPTION REF DRAWING NO DAY YEAR 13E 16...

Page 195: ...IGHT AND BALANCE 6 22 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm F MISCELLANEOUS SYSTEMS DESCRIPTION REF DRAWING NO DAY YEAR...

Page 196: ...LBS Kg ARM INCHES cm G CABIN ACCOMODATIONS DESCRIPTION REF DRAWING NO DAY YEAR 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...

Page 197: ...IONICS AUTOPILOTS DESCRIPTION REF DRAWING NO DAY YEAR 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 82 17 23 288 04 113 40 X 10H G...

Page 198: ...HT AND BALANCE 6 25 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm H AVIONICS AUTOPILOTS CONT DESCRIPTION REF DRAWING NO DAY YEA...

Page 199: ...2 STOWED 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...

Page 200: ...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...

Page 201: ...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 21...

Page 202: ...PMENT CONT DESCRIPTION REF DRAWING NO DAY YEAR 24J 27J 28J 29J 30J 31J 32J 147 42 33J 30 0 66 1 151 5 59 7 AIR CONDITIONER MINUS WTS 4 1 9 0 180 3 71 0 SPEEDBRAKE 2000 34J 25J 26J 770000 950286 810447...

Page 203: ...ND BALANCE 6 30 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 EQUIPMENT LIST MO ITEM ITEM MARK IF INSTALLED WT LBS Kg ARM INCHES cm J OPTIONAL EQUIPMENT CONT DESCRIPTION REF DRAWING NO DAY YEAR 36J...

Page 204: ...3 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 15 EMERGENCY EXTENSION SYSTEM 7 16 WARNING SYST...

Page 205: ...UEL SYSTEM 7 27 ELECTRICAL SYSTEM 7 27 ALTERNATOR BATTERY 7 27 ESSENTIAL BUS 7 28 NON ESSENTIAL BUS 7 28 EQUIPMENT LOCATION 7 28 SCHEMATIC 7 29 CIRCUIT BREAKER PANEL 7 30 ACCESSORIES 7 31 ANNUNCIATION...

Page 206: ...namics The empennage 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...

Page 207: ...a bobweight located forward of the con trol column help create desirable stability characteristics A factory set fixed trim tab spans the length of the elevator Counterweights balance the elevators P...

Page 208: ...nown as GCU 476 KEYPAD UNIT this provides alphanumeric softkey and flight planning function keys used to interface with a Garmin Integrated Flight Deck The GCU 476 also provides heading course and alt...

Page 209: ...e and status but remains a supplemental display of autopilot operating modes The GDL 69 Series are SiriusXM Satellite Radio data link receivers The SiriusXM Satellite Ra dio antenna receives the Siriu...

Page 210: ...MOONEY M20V ACCLAIM ULTRA SECTION VII AIRPLANE AND SYSTEM DESCRIPTION 7 7 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 FIGURE 7 1 FLIGHT PANEL 33 0001 THRU 33 TBD...

Page 211: ...ltitude Airspeed and Slip Information ATTITUDE Indicator portion of the display will always appear on the top display The Atti tude Indicator consists of seven parts Horizon Line Sky blue Ground brown...

Page 212: ...nual means of electrically by passing the Air speed Safety Switch In the event the landing gear switch is placed in gear up position a properly operating Airspeed Safety Switch prevents gear from bein...

Page 213: ...y also be used as an engine starting aid Continuous operation of the low boost is permitted Never run the boost pump without fuel in the system Pushing LOW BOOST pump switch ON when engine is operatin...

Page 214: ...lternate static source valve full aft to change source of static air for the altimeter air speed and vertical speed indicator from outside of aircraft to cabin interior Air speed and al timeter readin...

Page 215: ...VALVE NOT SHOWN Fuel selector valve located on floorboard is a three position valve which allows pilot to select either left or right fuel tank Turning valve OFF shuts off ALL fuel to engine At full t...

Page 216: ...indicates a failure of one of the SpeedBrake cartridges The SpeedBrake switch should be depressed OFF The system may be checked a second time for proper operation but after the second attempt the Spee...

Page 217: ...but Pitot Heat system has failed PITOT HEAT will illuminate AMBER only when there is any type of electrical failure in the pitot heat system It will not illuminate when switch is OFF and will not illu...

Page 218: ...absorb shock of taxiing and landing RETRACTION SYSTEM Landing gear is electrically retracted and extended The landing gear switch operates a landing gear actuator relay Pull wheel shaped knob out and...

Page 219: ...usly when landing gear is fully extended The red annunciation 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 indic...

Page 220: ...is 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 restra...

Page 221: ...h 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 b...

Page 222: ...n the induc tion system provides protection from too much pressure by actuating at 35 in Hg of manifold pressure The engine operates with three standard engine controls The propeller turns clockwise a...

Page 223: ...and reduced service life Efficient engine operation demands care ful attention to cleanliness of air fuel oil and maintaining operating temperatures within required limits Servicing of the engine sho...

Page 224: ...tor to a C shaped standpipe mounted in the left wheel well area The air oil separator condenses some of the oil vapor and returns the oil back to the crankcase Proper maintenance of this system is req...

Page 225: ...during the engine cranking period Two lobes on the breaker cam produce two sparks per revolution of the drive shaft After engine is running counter weights hold the latch pawls away from the stop pins...

Page 226: ...CAN 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...

Page 227: ...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 f...

Page 228: ...es Fahrenheit A red 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 F74...

Page 229: ...DRAIN 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 QUANTIT...

Page 230: ...properly will cause engine to quit due to excessive rich fuel mixture CAUTION The BOOST PUMP Low Boost switch operates the fuel boost pump on low power to provide a means of suppressing fuel vapor fr...

Page 231: ...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 A...

Page 232: ...NTROL GARMIN GFC700 AFCS DIM SW BACKUP AIRSPEED ALTITUDE 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...

Page 233: ...CAL CIRCUIT BREAKER PANEL See FIGURES 7 9 Illustration depicts typical C B panel may vary from your aircraft The circuit breaker panel is located on the right side of the instrument panel Each breaker...

Page 234: ...E 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 ho...

Page 235: ...on both cabin and baggage doors When one of the cabin or baggage doors are opened the baggage light will illuminate for approximately 1 5 min utes and then distinguish until door has been shut and reo...

Page 236: ...d valve is 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...

Page 237: ...ir distribution 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...

Page 238: ...battery is drained to depletion or until the switch is manually reset ARM position is selected when the transmitter is installed at the factory and switch should re main in that position whenever uni...

Page 239: ...MOONEY M20V ACCLAIM ULTRA SECTION VII AIRPLANE AND SYSTEM DESCRIPTION 7 36 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 240: ...ION 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...

Page 241: ...MOONEY M20V ACCLAIM ULTRA SECTION VIII HANDLING SERVICE AND MAINTENANCE 8 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 242: ...rform or supervise Reference should be made to CFR Part 43 and 91 for information regarding preventive maintenance which may be performed by a U S licensed pilot It is wise to follow a planned schedul...

Page 243: ...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 fi...

Page 244: ...ed that fuel samples be taken prior to each flight Fuel samples taken immediately after refueling may not show water or sediment due to mixing action of refueling process Allow five minutes after refu...

Page 245: ...iscarded oil for evidence of metal particles Thereafter the oil and oil filter must be changed at every 50 hours of time in service At the first oil change the engine and related accessories including...

Page 246: ...E ANY OTHER DRY ING METHOD 6 Remove the bottle from the Re charger Kit P N CP 99 5050 containing oil red in color Begin re oiling the dry filter by applying a bead or line of red oil along the top onl...

Page 247: ...inflated 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 wor...

Page 248: ...ich 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...

Page 249: ...e manufacturer s instructions when using commercial cleaning and finishing compounds CAUTION Foam type shampoos may be used for routine cleaning of carpets To minimize carpet wetting keep foam type cl...

Page 250: ...LTRA SECTION IX SUPPLEMENTAL DATA 9 1 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 TABLE OF CONTENTS TITLE SECTION INTRODUCTION 9 3 THE SUPPLEMENTS INSERTED INTO THIS SECTION ARE FAA APPROVED SUPP...

Page 251: ...MOONEY M20V ACCLAIM ULTRA SECTION IX SUPPLEMENTAL DATA 9 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 SUPPLEMENT INSERTED DATE...

Page 252: ...ures 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 functi...

Page 253: ...MOONEY M20V ACCLAIM ULTRA SECTION IX SUPPLEMENTAL DATA 9 4 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 254: ...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 TURBUL...

Page 255: ...MOONEY M20V ACCLAIM ULTRA SECTION X SAFETY INFORMATION 10 2 AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE 03 16 2017 BLANK...

Page 256: ...splaced 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...

Page 257: ...ing 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...

Page 258: ...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 respo...

Page 259: ...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...

Page 260: ...d by 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 require...

Page 261: ...and near 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 tu...

Page 262: ...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 decis...

Page 263: ...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 th...

Page 264: ...est 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 f...

Page 265: ...s not elapsed 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...

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