Page 1 PILOT’S OPERATING HANDBOOK AND FAA APPROVED AIRPLANE FLIGHT MANUAL M20V P/N: POH- 003920 ORIGINAL ISSUE - 03-16-2017 Revision A - 08-18-2017 Copyright 2017 - All Rights Reserved MOONEY INTERNATIONAL CORPORATION 165 Al Mooney Road, Kerrville, Texas 78028 tel: 830-896-6000 www.mooney.com...
Page 2 CAUTION 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.
Page 4 This handbook meets GAMA Specification No. 1, SPECIFICATION FOR PILOT’S OPERATING HAND- BOOK, issued February 15, 1975, revised October 18, 1996; Revision No. 2. CopyrightE 2017 All Rights Reserved Mooney International Corporation - 165 Al Mooney Rd - Kerrville, Texas 78028 ORIGINAL ISSUE - 03-16-2017...
Page 5 MOONEY M20V BLANK...
Page 6 PROFITABLE EVER. - NOTICE - This manual is provided as an operating guide for the Mooney Model M20V. It is important that you, regardless of your previous experience, carefully read the handbook from cover to cover and review it frequently. THIS AFM MUST BE CARRIED IN THE AIRCRAFT AT ALL TIMES.
Page 7 INTRODUCTION MOONEY M20V ACCLAIM ULTRA BLANK...
Page 8: Poh/Afm Poh
MOONEY INTRODUCTION M20V ACCLAIM ULTRA LIST OF EFFECTIVE PAGES ORIGINAL ISSUE ............
Page 9 INTRODUCTION MOONEY M20V ACCLAIM ULTRA 3- 3 .............
Page 10 MOONEY INTRODUCTION M20V ACCLAIM ULTRA 5- 11 ............
Page 11 INTRODUCTION MOONEY M20V ACCLAIM ULTRA 5- 67 ............
Page 12 MOONEY INTRODUCTION M20V ACCLAIM ULTRA 7- 21 ............
Page 13 INTRODUCTION MOONEY M20V ACCLAIM ULTRA BLANK POH/AFM POH- 003920 ORIGINAL ISSUE - 03-16-2017 This POH/AFM effective with S/N 33-0001 AND ON...
Page 14 MOONEY INTRODUCTION M20V ACCLAIM ULTRA LOG OF REVISIONS REVISION REVISED DATE LETTER PAGES APPROVED ORIGINAL 3-16-2017 ISSUE See Narrative Discussion of Revision A 08-18-2017 Revisions Page viii ORIGINAL ISSUE - 03-16-2017 POH/AFM POH- 003920 Revision A: 08-18-2017...
Page 15 M20V ACCLAIM ULTRA NARRATIVE DISCUSSION OF REVISIONS Page Level Number Comment Original Issue: Release of M20V Acclaim Ultra Title page Corrected spelling of “Registration” Title page, Revised page numbers of effected pages i, ii, iii, vii, viii Removed “Hartzell” from Governor line...
Page 16 MOONEY INTRODUCTION M20V ACCLAIM ULTRA TABLE OF CONTENTS TITLE ..............
Page 17 INTRODUCTION MOONEY M20V ACCLAIM ULTRA BLANK ORIGINAL ISSUE - 03-16-2017...
Page 18: Table Of Contents
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL TABLE OF CONTENTS TITLE ..............
Page 19 SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA BLANK ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 1 - 2...
Page 20: Three View
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL 26’- 8” (812.8 cm) 8’- 6” 76” (259.1 cm) (193.04 cm) 6’- 7 1/2” (201.9 cm) 36’- 6” (1112.5 cm) 11’- 9” (358.1 cm) 9’- 2” (279.4 cm) FIGURE 1- 1 THREE VIEW...
Page 21: Introduction
This Operators Manual conforms to GAMA Specification No. 1 and includes both Manufacturer’s material and FAA APPROVED material required to be furnished to the pilot by the applicable Federal Aviation Regulations. Section IX contains supplemental data supplied by Mooney Inter- national Corporation.
Page 22: Descriptive Data
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL DESCRIPTIVE DATA ENGINE Number of Engines ............. . .
Page 23: Propeller
SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA PROPELLER Hartzell Number ............... . .
Page 24: Landing Gear
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL LANDING GEAR TYPE: Electrically operated, fully retractable tricycle gear with rubber shock discs. The main wheels have hydraulically operated disc brakes. The nose wheel is fully steerable 11 left to 13 right of center.
Page 25: Identification Plate
SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA IDENTIFICATION PLATE All correspondence regarding your airplane should include the Serial Number as depicted on the identification plate. The identification plate is located on the left hand side, aft end of the tailcone, below the horizontal stabilizer leading edge.
Page 26: Symbols, Abbreviations & Terminology
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL SYMBOLS, ABBREVIATIONS & TERMINOLOGY GENERAL AIR SPEED TERMINOLOGY & SYMBOLS GROUND SPEED - Speed of an airplane relative to the ground. KCAS KNOTS CALIBRATED AIR SPEED - The indicated speed of an aircraft, corrected for position and instrument error.
Page 27: Airplane Performance & Flight Planning Terminology
SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA AIRPLANE PERFORMANCE AND FLIGHT PLANNING TERMINOLOGY Demonstrated The velocity of the crosswind component for which adequate control of the Crosswind airplane during take off and landing test was actually demonstrated during Velocity certification. The value shown is not considered to be limiting.
Page 28: Weight & Balance Terminology
MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL WEIGHT AND BALANCE TERMINOLOGY The horizontal distance from the reference datum to the center of gravity (C.G.) of an item. Basic The actual weight of the airplane and includes all operating equipment (in-...
Page 29: Measurement Conversion Tables
SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA MEASUREMENT CONVERSION TABLES On the following pages are conversion tables and charts to and from U.S. weights and measures to metric and imperial equivalents. The conversion tables are included to help pilots who live in countries other than the United States or pilots from the United States who are traveling to or within other countries.
Page 30 MOONEY SECTION I M20V ACCLAIM ULTRA GENERAL WEIGHT U. S. Customary Unit ......... . .
Page 31: Use Of The Terms Warning, Caution And Note
SECTION I MOONEY GENERAL M20V ACCLAIM ULTRA USE OF THE TERMS WARNING, CAUTION AND NOTE The following conventions will be used for the terms Warning, Caution and Note: -WARNING- The use of a Warning symbol means that information which follows is of critical impor- tance and concerns procedures and techniques which could cause or result in personal injury or death if not carefully followed.
Page 32 MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS TABLE OF CONTENTS TITLE ..............
Page 33 SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 2 - 2...
Page 34: Introduction
The certificated noise level per 14 CFR Part 36, Appendix G, Amendment 36-28 of the Federal Aviation Regulations for the Mooney M20V, with the Hartzell 3 blade propeller installed at 3368 lbs (1528 Kg.) maximum weight is 78.0 dB(A). No determination has been made by the Federal Aviation Administration that the noise levels of this airplane are or should be acceptable or unac- ceptable for operation at, into, or out of, any airport.
Page 35: Airspeed Limitations
SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA AIRSPEED LIMITATIONS Airspeed limitations and their operational significance are shown in Figure 2-1. This calibration assumes zero instrument error. V/SPEED KCAS/KIAS REMARKS Never Exceed 196/195 Do not exceed this Speed speed in any op- eration.
Page 36: Airspeed Markings
MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS AIRSPEED MARKINGS Airspeed indicator markings, their color code and operational significance are shown in Figure 2- 2. G- 1000 AIRSPEED INDICATOR & STANDBY MARKINGS MARKING IAS / STANDBY SIGNIFICANCE Low speed awareness - Red band 20 KIAS –...
Page 37: Power Plant Limitations
SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA POWER PLANT LIMITATIONS Number of Engines ............. . .
Page 38: Power Plant Instrument Markings
MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS POWER PLANT INSTRUMENT MARKINGS Power plant instrument markings and their color code significance are shown in the table below. -NOTE- When an indication lies in the caution range, the legend for that display will change to the color of the caution range.
Page 39: Fuel Limitations
SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA FUEL LIMITATIONS -WARNING- Takeoff maneuvers when the selected fuel tank contains less than 12 gallons (45.4 liters) of fuel have not been demonstrated. -NOTE- Each fuel quantity gauge is calibrated to read zero only in coordinated level flight when remaining quantity of fuel can no longer be safely used.
Page 40: Flight Load Factor Limits
MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS -NOTE- Up to 500 foot altitude loss may occur during stalls at maximum weight. FLIGHT LOAD FACTOR LIMITS Maximum Positive Load Factor Flaps Up ..............
Page 41: Types Of Operation
SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA KINDS OF OPERATION EQUIPMENT LIST SYSTEM or COMPONENT NIGHT NIGHT AIRSPEED INDICATOR ALTIMETER, SENSITIVE MAGNETIC DIRECTION INDICATOR PRIMARY FLIGHT DISPLAY MULTI- FUNCTION DISPLAY AUDIO PANEL AIR DATA COMPUTER ATTITUDE AND HEADING REFERENCE SYSTEM LANDING GEAR POSITION INDICATOR SEAT BELT &...
Page 42: General
MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS GENERAL OXYGEN SYSTEM: (Refer to Supplemental Information Section IX) G1000 System: 1. The GARMIN G1000 Cockpit Reference Guide for the M20V Series aircraft, P/N 190-02285-00, Revision A or later FAA approved revision must be immediately available to the flight crew.
Page 43 SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA 3. IFR enroute, oceanic and terminal navigation predicated upon the G1000 GPS Receiver is prohibited unless the pilot verifies the currency of the database or verifies each selected way- point for accuracy by reference to current approved data.
Page 44: Advisory Messages
MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS ADVISORY MESSAGES The G1000 Cockpit Reference Guide and the G1000 Pilot’s Guide contain detailed descriptions of the annunciator system and all advisory messages. These messages appear on the PFD for flight crew awareness.
Page 45: Decals, Placards And Panels
Decals & Placards - The following placards are relevant to proper operation of the airplane and must be installed inside the cabin at the locations specified. When ordering replacement Decals and Placards, refer to the Mooney International Corporation M20V IPC or call Mooney Service Parts Dept.
Page 46 MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS BELOW REAR SEAT 150110-A3040W (OPTIONAL) (CLEAR W/WHITE TEXT) FLOORBOARD BETWEEN SEATS 150110-N1015 UNDERSIDE OF GREEN & CLEAR PLEXIGLASS FLOORBOARD ABOVE FUEL CHECK VALVE 150110-A2032R (CLEAR W/RED TEXT) ON MAGNETIC COMPASS 150110-F1016 DO NOT EXCEED 10 LBS (4.5Kg) IN THIS COMPARTMENT...
Page 47 SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA WARNING: DO NOT EXCEED 170 LBS. FWD END OF REAR SEAT BOTTOM (77.1 Kg) ON THIS SEAT BACK STRUCTURE SEE AIRCRAFT LOADING SCHEDULE DATA 150110-A1041W FOR BAGGAGE COMPARTMENT ALLOWABLE (CLEAR W/WHITE TEXT) FLOORBOARD...
Page 48 Panels - The following “Electroluminescent Panels” with 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 Parts Catalog when ordering. FAA APPROVED...
Page 49 SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA FAA APPROVED AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 2 - 18...
Page 50: Fuselage Interior
The following placards are relevant to proper operation of the airplane and must be installed in- side the fuselage at the locations specified. When ordering replacement Decals and Placards, refer to the Mooney International Corporation M20V IPC or call Mooney Service Parts Dept. BACKSIDE OF...
Page 51 The following placards are relevant to proper operation of the airplane and must be installed on the exterior of the aircraft at the locations specified. When ordering replacement Decals and Placards, refer to the Mooney International Corporation M20V IPC or call Mooney Service Parts Dept.
Page 52 MOONEY SECTION II M20V ACCLAIM ULTRA LIMITATIONS UNDER WING NEAR SUMP DRAINS 150110-A2025B (CLEAR W/BLACK TEXT) 150110- A2025W (CLEAR W/WHITE TEXT) LEFT/RIGHT WINGS AT FUEL FILLERS 150110-B2007B (FULL COLOR PLACARD) LEFT/RIGHT WINGS AT FUEL FILLERS 150110-B2008B (WHITE W/BLACK INK) FAA APPROVED...
Page 53 SECTION II MOONEY LIMITATIONS M20V ACCLAIM ULTRA BLANK FAA APPROVED AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 2 - 22...
Page 54 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES TABLE OF CONTENTS TITLE ..............
Page 55 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA TABLE OF CONTENTS (cont’d) ERRONEOUS OR LOSS OF WARNING/CAUTION ANNUNCIATORS ... . . 3- 26 LANDING GEAR .............
Page 56 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES INTRODUCTION This section provides the recommended procedures to follow during adverse flight conditions. The information is presented to enable you to form, in advance, a definite plan of action for coping with the most probable emergency situations which could occur in the operation of your airplane.
Page 57: Airspeeds For Emergency Operations
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA AIRSPEEDS FOR EMERGENCY OPERATIONS CONDITION RECOMMENDED SPEED ENGINE FAILURE AFTER TAKEOFF Wing Flaps UP ....... .
Page 58: Emergency Procedures
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D ANNUNCIATION ANNUNCIATION ANNUNCIATION ACTION ACTION FUNCTION COLOR TRIGGER WHEN ON WHEN OFF SPEEDBRAKE WHITE WHITE SPEED BRAKE DIS- STEADY WHITE OFF WHEN PLAYED ON G1000.
Page 59 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D GEAR UNSAFE - MASTER WARNING GEAR DOWN - ALERT & ANNUNCIATION GEAR UNSAFE - ALERT & GEAR UNSAFE - ALERT & ANNUNCIATION ANNUNCIATION “IN TRANSITION”...
Page 60 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D ALTERNATE AIR - ALERT ALTERNATE AIR & ANNUNCIATION MASTER CAUTION PITOT HEAT FAIL PITOT HEAT FAIL MASTER CAUTION ALERT & ANNUNCIATION PROP DE-ICE FAIL...
Page 61 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D ALTERNATOR FAIL ALTERNATOR FAIL ALERT & ANNUNCIATION MASTER WARNING DOOR OPEN DOOR OPEN - MASTER WARNING ALERT & ANNUNCIATION EMERGENCY BUS EMERGENCY BUS ALERT & ANNUNCIATION...
Page 62 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D HIGH BOOST PUMP HIGH BOOST PUMP ALERT & ANNUNCIATION MASTER CAUTION LOW BOOST PUMP - ALERT START POWER - ALERT & ANNUNCIATION & ANNUNCIATION LOW FUEL WARNING - LEFT &...
Page 63 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D LOW FUEL CAUTION LOW FUEL WARNING - LH & RH LEFT GAUGE CAS & ALERT LOW FUEL CAUTION - LEFT LOW FUEL CAUTION CAS & ALERT...
Page 64 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES GARMIN G1000 ANNUNCIATIONS AND WARNING LIGHTS - CONT’D SYSTEM CONFIG ERROR LRU REPLACEMENT MESSAGE TCAS FAIL / DATA PATH FAIL TRAFFIC FAIL AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 3 - 11...
Page 65 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA If GARMIN G1000 GPS navigation information is not available or invalid, utilize remaining op- erational navigation equipment as required. If the “POSN ERROR” annunciation is displayed the system will flag and no longer provide GPS based navigational guidance.
Page 66: Engine
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES ENGINE ENGINE POWER LOSS - DURING TAKE-OFF ROLL Throttle ............. .
Page 67: Engine Power Loss, Sustained Negative "G" Loading
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA -WARNING- At altitudes above 18,000 ft., an overrich mixture may result if the turbocharger fails and the engine may stop firing. -NOTE- Excessive engine cooling may be experienced during long descents resulting in low engine oil and cylinder head temperatures.
Page 68: After Engine Restart
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES AFTER ENGINE RESTART HIGH Boost Pump ..........
Page 69: Emergency Landing With Throttle Stuck At Idle Power
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA EMERGENCY LANDING WITH THROTTLE STUCK AT IDLE POWER GLIDE Airspeed ....BEST GLIDE SPEED (See MAXIMUM GLIDE DISTANCE Chart) 3368 lb./1528 kg...
Page 70: Turbocharger Failure
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES The following check list should be used if a partial power loss due to primary induction air sys- tem blockage is experienced: Alternate Air ........
Page 71: Turbocharger Overboost
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA An interruption in fuel flow or manifold pressure to the engine will result in turbocharger “run- down”. At high altitude, merely restoring fuel flow may not cause the engine to restart, because without turbocharger boost, the mixture will be excessively rich.
Page 72: Loss Of Oil Pressure
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES LOSS OF OIL PRESSURE Oil temperature ........
Page 73: Fires
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA FIRES -NOTE- If necessary, use fire extinguisher to keep fire out of cabin area. ENGINE FIRE - DURING START ON GROUND Magneto/Starter Switch ....
Page 74: Emergency Descent Procedure
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES If power must be re-established to navigation equipment to continue flight: If the faulty compo- nent can be determined, pull the associated circuit breaker if not tripped already. Do not close the open breaker to re- establish power to the failed circuit.
Page 75: Forced Landing Emergency
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA MAXIMUM GLIDE DISTANCE MODEL M20V 24000 22000 20000 18000 16000 ASSOCIATED CONDITIONS 14000 Landing Gear Retracted Wing Flaps Zero Degrees Propeller Windmilling 12000 Wind Zero Wind 10000 8000 BEST GLIDE SPEED Weight...
Page 76: Overweight Landing Procedure
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES OVERWEIGHT LANDING PROCEDURES In the event it is necessary to land with weight exceeding 3200 Lbs. (1452 Kg.) (max. landing weight) the following procedure is recommended in addition to normal APPROACH FOR LAND-...
Page 77: Alternator Failure
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA ALTERNATOR FAILURE If the Main Alternator fails, indicated by the Master Warning “ALT VOLTS” flashing: Perform the Standby Alternator Emergency Checklist (repeated below) 1. Push the “Stdby Alt/Emergency Bus” switch ON. (This activates the emergency bus circuitry &...
Page 78: Avionics Emergencies
MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES 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...
Page 79: Erroneous Or Loss Of Engine And Fuel Displays
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA ERRONEOUS OR LOSS OF ENGINE AND FUEL DISPLAYS -NOTE- Loss of an engine parameter is indicated by a red X through the data field. Erro- neous information may be identified by indications which do not agree with other system information.
Page 80 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES FAILURE OF LANDING GEAR TO RETRACT AIRSPEED ............
Page 81 SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA -NOTE- When using Alternate Static Source, pilot’s window and air vents MUST BE KEPT CLOSED. Alternate Static Source ........... .
Page 82 MOONEY SECTION III M20V ACCLAIM ULTRA EMERGENCY PROCEDURES Move propeller control to maximum RPM to minimize ice build- up on propeller blades. If ice builds up or sheds unevenly on propeller, vibration will occur. If excessive vibration is noted, mo- mentarily reduce engine speed with propeller control to bottom of GREEN ARC (Lowest RPM), then rapidly move control FULL FORWARD.
Page 83: Other Emergencies
SECTION III MOONEY EMERGENCY PROCEDURES M20V ACCLAIM ULTRA EMERGENCY EXIT OF AIRCRAFT CABIN DOORS LH/RH PULL latch handle UP. PUSH OPEN door and exit aircraft. BAGGAGE COMPARTMENT DOOR (Auxiliary Exit) Release (Pull UP) rear seat back latches on spar. Fold rear seat backs forward, CLIMB OVER.
Page 84 MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES TABLE OF CONTENTS TITLE ..............
Page 85 SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA BLANK ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 4 - 2...
Page 86: Introduction
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES INTRODUCTION This section describes the recommended procedures for the conduct of normal operations for the airplane. All of the required (FAA or ICAO regulations) procedures and those necessary for operation of the airplane as determined by the operating and design features of the airplane are presented.
Page 87: Speeds For Normal Operation
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA SPEEDS FOR NORMAL OPERATION Unless otherwise noted, the following speeds are based on a weight of 3368 pounds and may be used for any lesser weight. However, to achieve the performance specified in...
Page 88: Pre-Flight Inspection
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES PRE- FLIGHT INSPECTION 1. Cockpit POH/Documentation ............
Page 89 SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA Verify adequate oxygen supply for trip, (if use of oxygen is anticipated), refer to oxygen duration chart, found in the POH/AFM Supplement Section IX Also check that face masks and hoses are accessible and in good condition * If TKS system is installed, pitot heat annunciation will illuminate AMBER when Pitot Heat has failed.
Page 90 MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES ............
Page 91: Before Starting Check
MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA Avionics/Battery #1 Access Panel .........
Page 92: Engine Start
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES ENGINE START -CAUTION- When either battery voltage is low, inspection should be conducted to determine condition of battery and/or reason for battery being low. Replacement or servicing of batteries is essential and charging for at least one hour should be done before engine is started.
Page 93: Extreme Cold Weather Engine Start
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA EXTREME COLD WEATHER ENGINE START Refer to Continental Motors Engine Operating Manual OI- 18 Section 7.5.1 for extreme cold weather starting procedures. -CAUTION- For engine operation at outside air temperatures below - 25C (- 13F), the engine and engine oil should be preheated to at least - 25C (- 13F) before the engine is...
Page 94 MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES -CAUTION- With Rudder Trim in the full right position the aircraft will tend to steer to the right during taxi. Parking Brake ............
Page 95: Standby Alternator Preflight Check
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA BEFORE TAKEOFF Taxi Checklist ............
Page 96: Takeoff
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES 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- craft to start rolling before high RPM is developed, and gravel or loose material will be blown back from the propeller area instead of being pulled into it.
Page 97: Climb (Cruise)
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA CLIMB -NOTE- If applicable, use noise abatement procedures as required. See Section V, for rate of climb graph. CLIMB (CRUISE) Airspeed ..............
Page 98: Fuel Tank Selection
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES -CAUTION- 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 1675F TIT or richer. -CAUTION- When changing power, the sequence control usage is important.
Page 99: Normal Descent - Gear Down
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA NORMAL DESCENT - GEAR DOWN Seats, Seat Belts/Shoulder Harness ......
Page 100: Go Around (Balked Landing)
MOONEY SECTION IV M20V ACCLAIM ULTRA NORMAL PROCEDURES GO AROUND (BALKED LANDING) -CAUTION- To minimize control wheel forces during GO-AROUND, timely nose-down trimming is recommended to counteract nose up pitching moment as power is increased and/or flaps are retracted. Power .
Page 101: Securing Aircraft
SECTION IV MOONEY NORMAL PROCEDURES M20V ACCLAIM ULTRA SECURING AIRCRAFT Magneto/Starter Switch ........
Page 102 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE TABLE OF CONTENTS TITLE ..............
Page 103: Introduction
However, the performance on the charts can be duplicated by following the stated procedures in a properly maintained MOONEY M20V. Examples are given to show how each chart is used. The only charts with no example are those where such an example of use would be repetitive.
Page 104: Best Economy
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE Best Economy − Best Economy mixture is desirable for maximizing range and minimizing fuel cost. Best Economy is operated 50F lean of peak TIT. The engine may be leaned up to 100F lean of peak however the fuel economy generally doesn’t improve beyond 50F lean of peak.
Page 105: Removable Steps
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA TRUE AIRSPEED INDICATION True airspeed indication is included on the instrument panel as an aid to the pilot. This true air- speed indication is based on the conversion of indicated airspeed (KIAS) with zero instrument error not calibrated airspeed (KCAS).
Page 106: Temperature Conversion
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE TEMPERATURE CONVERSION −10 −20 −10 −20 −30 −30 −40 −40 FAHRENHEIT CELSIUS ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 5...
Page 107: Crosswind Component Chart
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA CROSSWIND COMPONENT CHART DEMONSTRATED CROSS WIND IS 18 KNOTS (THIS IS NOT A LIMITATION) CROSSWIND COMPONENT CHART EXAMPLE: WIND SPEED 18 KNOTS ANGLE BETWEEN WIND DIRECTION AND FLIGHT PATH 16.4 KNOTS HEADWIND COMPONENT 11.2 KNOTS...
Page 108 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE AIRSPEED CALIBRATION − PRIMARY STATIC SYSTEM POWER ON, CLEAN CONFIGURATION Air Speed Calibration Primary Static System − Power On, Clean Configuration EXAMPLE GIVEN : IAS 129 KNOTS FIND: CAS 130 KNOTS KNOTS INDICATED AIRSPEED (KIAS)
Page 109 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRSPEED CALIBRATION − PRIMARY STATIC SYSTEM POWER OFF, CLEAN CONFIGURATION Air Speed Calibration Primary Static System − Power Off, Clean Configuration EXAMPLE GIVEN : IAS 129 KNOTS FIND: CAS 130 KNOTS KNOTS INDICATED AIRSPEED (KIAS)
Page 110 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE AIRSPEED CALIBRATION − PRIMARY STATIC SYSTEM POWER ON, 10 FLAP, GEAR DOWN Air Speed Calibration Primary Static System - Power On, 105 Flap, Gear Down SPEED FOR SAFELY LOWERING FLAPS KNOTS INDICATED AIRSPEED (KIAS)
Page 111 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRSPEED CALIBRATION − PRIMARY STATIC SYSTEM POWER OFF, 10 FLAP, GEAR DOWN Air Speed Calibration Primary Static System - Power Off, 105 Flap, Gear Down SPEED FOR SAFELY LOWERING FLAPS KNOTS INDICATED AIRSPEED (KIAS)
Page 112 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE AIRSPEED CALIBRATION − PRIMARY STATIC SYSTEM POWER ON, 33 FLAP, GEAR DOWN Air Speed Calibration − With Flap Seals Primary Static System - Power On, 335 Flap, Gear Down KIAS KCAS ERROR KNOTS INDICATED AIRSPEED (KIAS) −1.4...
Page 113 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRSPEED CALIBRATION WITH FLAP SEALS− PRIMARY STATIC SYSTEM POWER OFF, 33 FLAP, GEAR DOWN Air Speed Calibration − With Flap Seals Primary Static System - Power Off, 335 Flap, Gear Down KIAS KCAS...
Page 114: Airspeed Calibration - Alternate Static System
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE AIRSPEED CALIBRATION − ALTERNATE STATIC SYSTEM GEAR & GEAR & GEAR & FLAPS DN FLAPS DN KIAS FLAPS UP KIAS KIAS KIAS −1.0 −1.2 −2.0 −2.2 −3.2 −1.8 −3.2 −4.5 −2.8 −4.0 −6.0 −3.0...
Page 115: Altimeter Correction - Primary Static System
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA ALTIMETER CORRECTION − PRIMARY STATIC SYSTEM −−− SEA LEVEL 12,500 FT. 25,000 FT. Gear & Gear Gear Gear & Gear Gear Gear & Gear Gear KIAS Flaps Dn/10 DN/33 Flaps Dn/10 DN/33 Flaps...
Page 116: Altimeter Correction - Alternate Static System
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ALTIMETER CORRECTION − ALTERNATE STATIC SYSTEM −−− SEA LEVEL 12,500 FT. 25,000 FT. Gear & Gear Gear Gear & Gear Gear Gear & Gear Gear KIAS Flaps Dn/10 DN/33 Flaps Dn/10 DN/33 Flaps...
Page 117: Stall Speed Vs Angle Of Bank
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA STALL SPEED VS. ANGLE OF BANK ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 16...
Page 118 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE TAKEOFF DISTANCE − GROUND ROLL ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 17...
Page 119 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA TAKEOFF DISTANCE − OVER 50’ (15m) OBSTACLE ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 18...
Page 120 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE RATE OF CLIMB AT Vy ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 19...
Page 121 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA RATE OF CLIMB at 120 KIAS (CRUISE CLIMB) ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 20...
Page 122: Time - Fuel - Distance (To Climb At Vy)
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE TIME - FUEL - DISTANCE (to CLIMB at Vy) ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 21...
Page 123: Time - Fuel - Distance (To Climb At 120 Kias)
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA TIME - FUEL - DISTANCE (to CLIMB at 120 KIAS) ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 22...
Page 124 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE CRUISE POWER SETTINGS & FUEL FLOWS − BEST POWER ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 23...
Page 125 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA CRUISE POWER SETTINGS & FUEL FLOWS − BEST ECONOMY ORIGINAL ISSUE − 03-16-2017 AIRPLANE FLIGHT MANUAL 5 − 24...
Page 126: Best Power
MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) Conditions: Example: Mixture: Pressure Altitude: 16000 ft Best Power (50 F Rich of Peak TIT) Propeller Speed: 2400 RPM Manifold Pressure: 30.5 in HG...
Page 127 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 22000 Ft. Pressure Altitude DISA: −30 (−59)5C (−28)5C (2)5C (OAT) −54 (−73)5F (−19)5F (35)5F KTAS KTAS KTAS 2500 30.5 22.6 21.1 19.5 2500 29.0 21.5...
Page 128 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 18000 Ft. Pressure Altitude −30 (−51)5C (−20)5C (10)5C DISA: (OAT) −54 (−59)5F (−5)5F (49)5F KTAS KTAS KTAS 2500 30.5 22.6 21.2 19.6 2500 29.0 21.6...
Page 129 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 14000 Ft. Pressure Altitude DISA: −30 (−43)5C (−12)5C (18)5C (OAT) −54 (−45)5F (9)5F (63)5F KTAS KTAS KTAS 2500 30.5 22.7 21.2 19.6 2500 29.0 21.7...
Page 130 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 10000 Ft. Pressure Altitude DISA: −30 (−35)5C (−4)5C (26)5C (OAT) −54 (−31)5F (23)5F (77)5F KTAS KTAS KTAS 2500 30.5 22.8 21.3 19.7 2500 29.0 21.8...
Page 131 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 6000 Ft. Pressure Altitude −30 (−27)5C (3)5C (33)5C DISA: (OAT) −54 (−16)5F (33)5F (92)5F KTAS KTAS KTAS 2500 30.5 22.9 21.4 19.9 2500 29.0 22.0...
Page 132 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST POWER) 2000 Ft. Pressure Altitude −30 (−19)5C (11)5C (41)5C DISA: (OAT) −54 (−2)5F (52)5F (106)5F KTAS KTAS KTAS 2500 30.5 23.0 21.6 20.0 2500 29.0 22.1...
Page 133: Best Economy
SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) Conditions: Example: Mixture: Pressure Altitude: 12000 ft Best Economy (50 F Lean of Peak TIT) Propeller Speed: 2300 RPM Manifold Pressure: 28.0 in HG...
Page 134 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 22000 Ft. Pressure Altitude −30 (−51)5C (−20)5C (10)5C DISA: (OAT) −54 (−73)5F (−19)5F (35)5F KTAS KTAS KTAS 2500 30.5 19.4 18.2 17.0 2500 29.0 18.4...
Page 135 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 18000 Ft. Pressure Altitude −30 (−51)5C (−20)5C (10)5C DISA: (OAT) −54 (−59)5F (−5)5F (49)5F KTAS KTAS KTAS 2500 30.5 19.3 18.2 17.0 2500 29.0 18.4...
Page 136 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 14000 Ft. Pressure Altitude −30 (−43)5C (−12)5C (18)5C DISA: (OAT) −54 (−45)5F (9)5F (63)5F KTAS KTAS KTAS 2500 30.5 19.3 18.2 17.0 2500 29.0 18.5...
Page 137 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 10000 Ft. Pressure Altitude −30 (−35)5C (−4)5C (26)5C DISA: (OAT) −54 (−31)5F (23)5F (77)5F KTAS KTAS KTAS 2500 30.5 19.4 18.3 17.1 2500 29.0 18.6...
Page 138 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 6000 Ft. Pressure Altitude DISA: −30 (−27)5C (3)5C (33)5C (OAT) −54 (−16)5F (38)5F (92)5F KTAS KTAS KTAS 2500 30.5 19.5 18.4 17.2 2500 29.0 18.7...
Page 139 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA SPEED and POWER SETTINGS vs ALTITUDE − (BEST ECONOMY) 2000 Ft. Pressure Altitude −30 (−19)5C (11)5C (41)5C DISA: (OAT) −54 (−2)5F (52)5F (106)5F KTAS KTAS KTAS 2500 30.5 19.6 18.6 17.4 2500 29.0 18.9...
Page 140 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 39...
Page 141 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 40...
Page 142 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 41...
Page 143 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 42...
Page 144 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 43...
Page 145 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 44...
Page 146 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 45...
Page 147 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 46...
Page 148 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 47...
Page 149 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 48...
Page 150 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 49...
Page 151 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 50...
Page 152 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 51...
Page 153 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 52...
Page 154 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 53...
Page 155 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 54...
Page 156 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 55...
Page 157 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 56...
Page 158 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 57...
Page 159 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 58...
Page 160 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 59...
Page 161 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 60...
Page 162 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 61...
Page 163 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 62...
Page 164 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 63...
Page 165 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 64...
Page 166 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 65...
Page 167 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 66...
Page 168 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 67...
Page 169 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 5 - 68...
Page 170 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE TIME - FUEL - DISTANCE to DESCEND (Maintain 500 fpm Rate of Descent) ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 69...
Page 171 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA TIME - FUEL - DISTANCE to DESCEND (Maintain 1000 fpm Rate of Descent) ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 70...
Page 172 MOONEY SECTION V M20V ACCLAIM ULTRA PERFORMANCE LANDING - GROUND ROLL ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 71...
Page 173 SECTION V MOONEY PERFORMANCE M20V ACCLAIM ULTRA LANDING - OVER 50’ (15m) OBSTACLE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 5 - 72...
Page 174 The empty weight, center of gravity and equipment list for the airplane as delivered from Mooney International Corporation is contained in this section. The use of this section is valid for use with the airplane identified below when approved by Mooney International Corporation.
Page 175 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 2...
Page 176: Introduction
A comprehensive list of all Mooney equipment available for this airplane is included in this section. Only those items checked (X) were installed at Mooney and are included in the empty weight- and- balance data.
Page 177: Airplane Weighing Procedure
SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE WEIGHING PROCEDURE LEVELING Place a spirit level on the leveling screws above the tailcone left access door when leveling the aircraft longitudinally. Level the aircraft by increasing or decreasing air pressure in the nose wheel tire.
Page 178: Weight & Balance Chart
MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE M20V - WEIGHT & BALANCE CHART REF.POINT REFERENCE LEVEL REF. (NOSE GEAR DATUM(STA.0) (LEVELING SCREWS) TRUNNION STA. - 13) Lc/g MEASUREMENTS Lm/r Lm/n INCHES/CM INCHES/CM SCALE POSITION AND SYMBOL SCALE READING...
Page 179 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 6...
Page 180: Pilots Loading Guide
MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE PILOT’S LOADING GUIDE LOADING CALCULATION PROCEDURE Proper loading of the aircraft is essential for maximum flight performance and safety. This section will assist you in determining whether the aircraft loading schedule is within the approved weight and center- of- gravity limits.
Page 181: Problem Form
SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA PROBLEM FORM YOUR SAMPLE PROBLEM PROBLEM ITEM WEIGHT MOMENT WEIGHT MOMENT (Kg) (Kg- cm lb- in (Kg) (Kg- cm lb- in /1000) /1000 /1000) /1000 A/C Basic Empty Wt. (W.) (from...
Page 182 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE PROBLEM FORM (CONT) YOUR SAMPLE PROBLEM PROBLEM ITEM WEIGHT MOMENT WEIGHT MOMENT (Kg) (Kg- cm lb- in (Kg) (Kg- cm lb- in /1000) /1000 /1000) /1000 Loaded A/C Weight (Takeoff at (1528) (191.1)
Page 183: Center Of Gravity Moment Envelope
SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA CENTER OF GRAVITY MOMENT ENVELOPE 1100 1300 1500 1700 1900 A/C WEIGHT 1000 1200 1400 1600 1800 2000 (Kg) LBS. LOAD AIRCRAFT MOMENT/1000- Kg- MM (1528) 3368 254.9 (1500) 171.7 3300 145.2...
Page 184: Center Of Gravity Limits Envelope
MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE M20V - CENTER OF GRAVITY LIMITS ENVELOPE A/C WEIGHT 1050 1150 1200 1250 1300 1100 (Kg) Lbs. AIRCRAFT CG LOCATION (L ) MM AFT OF DATUM (STA. 0.0) (1528) 3368 (1500)
Page 185: Fixed Ballast
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.
Page 186 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 13...
Page 187 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 14...
Page 188 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 15...
Page 189 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 16...
Page 190 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 17...
Page 191 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 18...
Page 192 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 19...
Page 193 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 20...
Page 194 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 21...
Page 195 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 22...
Page 196 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 23...
Page 197 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 Revision A: 08-18-2017 6 - 24...
Page 198 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 25...
Page 199 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 26...
Page 200 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 6 - 27...
Page 201 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 28...
Page 202 MOONEY SECTION VI M20V ACCLAIM ULTRA WEIGHT AND BALANCE ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL Revision A: 08-18-2017 6 - 29...
Page 203 SECTION VI MOONEY WEIGHT AND BALANCE M20V ACCLAIM ULTRA AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 6 - 30...
Page 204 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION TABLE OF CONTENTS TITLE ..............
Page 205 MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA EXHAUST SYSTEM ............
Page 206: Introduction
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION INTRODUCTION Acquiring a working knowledge of the aircraft’s controls and equipment is one of your important first steps in developing a fully efficient operating technique. This Airplane and Systems Section describes location, function, and operation of systems’...
Page 207: Rudder System
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA RUDDER SYSTEM The rudder attaches to the aft, vertical fin spar at four hinge points. Push- pull tubes and bellcranks link the rudder to the rudder pedals. RUDDER TRIM SYSTEM The M20V is equipped with an electric rudder trim system which allows the pilot to trim out much of the rudder force required for take off, climb, cruise and descent.
Page 208: Instrument Panel
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION INSTRUMENT PANEL The instrument panel has been designed to incorporate the G1000 Integrated Cockpit. All Com- munications, Navigation, Engine Instruments, and System annunciations have been integrated into a custom design package specifically for the M20V series aircraft.
Page 209 The traffic information is displayed on the PFD and MFD via HSDB, refer to the Pilot’s Guide and the Garmin G1000 Cockpit Reference Guide for the Mooney M20V. Refer to the GARMIN G1000 Cockpit Reference Guide for the M20V MODEL aircraft, GARMIN P/N 190-02285-00, Rev.
Page 210 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION FIGURE 7- 1 FLIGHT PANEL (33-0001 THRU 33- TBD) ORIGINAL ISSUE - 03-16-2017 AIRPLANE FLIGHT MANUAL 7 - 7...
Page 211: Flight Panel & Instruments
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA FLIGHT PANEL & INSTRUMENTS SWITCHES & CONTROLS -NOTE- The illustration depicts a standard panel configuration. The location of instru- ments, switches, and avionics may be relocated in each aircraft, dependant upon the optional equipment selected by the customer and available panel space.
Page 212 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION 9. MASTER POWER SWITCH Master switch operates battery relay which controls battery power (selected battery) to main buss. This switch cuts ALL ship power OFF, except cabin overhead lights and baggage com- partment light.
Page 213 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA 21. ICE LIGHT SWITCH (if Equipped) Lighting to alert the pilot of ice formation on surfaces of an aircraft. 22. READING LIGHTS SWITCH Momentary switch operates 4 overhead lamps in 3 modes. Reading Light Switch UP posi- tion, only the Pilot reading light is activated.
Page 214 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION 30. PROPELLER CONTROL Push propeller control forward to increase engine RPM; pull control aft to decrease engine RPM. Control is a vernier type and fine adjustments of RPM can be obtained by turning knob clockwise to increase RPM and counter clockwise to decrease RPM.
Page 215 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA 43. 476 KEYPAD UNIT The GCU 476 refers to the Garmin Flight Management System (FMS) Controller used in a Garmin Integrated Flight Deck. The GCU 476 Line Replaceable Unit (LRU) provides alphanumeric, softkey, and flight plan- ning function keys used to interface with a Garmin Integrated Flight Deck.
Page 216: Annunciations Or Alerts
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION FIGURE 7- 2 ANNUNCIATIONS ANNUNCIATIONS AND ALERTS ANNUNCIATIONS or ALERTS GEAR SAFETY INDICATOR (GEAR DOWN - GEAR UNSAFE) A GEAR DOWN annunciation “GREEN”, a GEAR UNSAFE annunciation “RED”, and a gear warning VOICE ALERT provide visual and audible gear position signals.
Page 217 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA ALTERNATE AIR Illuminates AMBER when the alternate air door is opened, either manually or automatically. In this situation, induction air for the engine is drawn from inside cowling rather than through the induction air intake.
Page 218: Ground Control
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION GROUND CONTROL NOSE GEAR STEERING Nose gear steering system consists of a steering horn on the nose gear leg linked to the rudder pedals by push- pull tubes. Rudder pedal action steers the nose wheel. Gear retraction relieves the rudder control system of its nose wheel steering and centers wheel to permit retraction into the nose wheel well.
Page 219: Emergency Extension System
MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA ing both toe pedals and pulling parking brake control, on console, sets the brakes. Push parking brake control forward to release brakes. It is not advisable to set parking brake when brakes are overheated, after heavy braking or when outside temperatures are unusually high.
Page 220: Cargo Restraint
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION FIGURE 7- 3 CARGO RETENTION (TYPICAL) CARGO RESTRAINT Cargo tie down rings/clevis 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.
Page 221: Seats
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA SEATS The front seats are individually mounted and may be adjusted fore and aft to fit individual comfort preferences. The front seat back may be adjusted by turning left side hand crank (knob) until seat back is in desired position.
Page 222: Engine
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION To verify re-engagement of latching mechanism; open outside handle fully, close inside handle to engage pin into cam slide of latch mechanism; insert latch pin into shaft hole to hold Red Han- dle down.
Page 223: Engine Operation And Care
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA Engine operating instruments are displayed in the Garmin GDU 10(XX) Multi- Function Display. Colored bars on instrument faces mark operating ranges. Proper interpretation of engine instru- ment readings is essential for selecting optimum control settings and for maintaining maximum cruise fuel economy.
Page 224: Lubrication System
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION PROPELLER CRANKSHAFT BEARNGS PROP CRANKSHAFT GOVERNOR CAMSHAFT PISTON & CONNECTING TAPPET VALVE ASSY TEMP SUCTION CNTRL TUBE VALVE COOLER STARTER SHAFT IDLER GEAR GEAR TURBOCHARGER PUMP TURBOCHARGER WASTEGATE CHECK CONTROLLER...
Page 225 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA coupling spring spins the magneto shaft through its neutral position and the breaker opens to produce a high voltage surge in the secondary coil. The spring action permits the latch plate, magnet and breaker to be delayed through a lag angle of 30 degrees of drive gear rotation during the engine cranking period.
Page 226: Air Induction System
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION AIR INDUCTION SYSTEM The primary engine air induction system draws air from the upper cowling plenum through the engine cooling inlets. The air passes through a filter and is split to provide air to the left and right turbo.
Page 227: Icing Protection
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA ICING PROTECTION Continued operation of the induction system in the event of intake air being obstructed is provid- ed by activation of the alternate air system. The alternate air is automatically or manually con- trolled.
Page 228 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION ENGINE STARTING SYSTEM Engine starting is provided by a 24 volt starter. The starter engages the drive shaft with a spring clutch. Avoid manually turning the propeller backwards as it may damage the clutch. A starter engaged warning annunciation (START POWER) is incorporated in the annunciator panel.
Page 229 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA FIGURE 7- 7 FUEL SYSTEM SCHEMATIC AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 7 - 26...
Page 230: Fuel System
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION FUEL SYSTEM Fuel is carried in two integrally sealed sections of the forward, inboard area of wing. Total usable fuel capacity is 89 U.S. gallons (336.9 liters). There are sump drains at the lowest point in each tank for taking fuel samples to check for sediment contamination or condensed water accumula- tion.
Page 231 MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA Amp standby alternator, actuated by the pilot using a manual switch in the cockpit labeled EMER BUS, powers Essential systems as presented on the fascia of the Circuit Breaker Panel. If the Primary and Standby charging systems fail, the ship’s battery(s) provide the system with electri-...
Page 232 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION SCHEMATIC (See FIGURE 7- 8) The voltage regulator adjusts alternator output to current load while maintaining a constant volt- age level. It also prevents Overvoltage and Field Short conditions from damaging the electrical system.
Page 233 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA FIGURE 7- 9 CIRCUIT BREAKER PANEL (TYPICAL) 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 is clearly marked to show which circuit it protects.
Page 234 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION Push- pull circuit breakers automatically break the electrical current flow if the system or unit re- ceives current overload to prevent damage to electrical wiring. Figure 7- 9 illustrates a typical main circuit breaker panel with its push- pull circuit breakers.
Page 235 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA MAP LIGHT Map lights are installed on the bottom of the pilot and co- pilot’s wheel. The intensity of the map light may be adjusted with the MAP LITE knob located (while facing the wheel) on the right aft side of the pilot’s and co- pilot’s control wheel.
Page 236 MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION CABIN ENVIRONMENT FIGURE 7- 10 CABIN AIR FLOW CABIN ENVIRONMENT HEATING & VENTILATION SYSTEMS Multiple controls are available to provide fresh air and/or heated fresh air according to individual preferences.
Page 237: Stall Warning System
SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA CABIN HEAT - Sonic nozzles extract high temperature bleed air immediately downstream from the turbo compressor. A silencer quiets the bleed air flow. The nozzles are most effective at high altitude and higher power settings because they rely on the compressor pressure ratio &...
Page 238: Vacuum System
MOONEY SECTION VII M20V ACCLAIM ULTRA AIRPLANE AND SYSTEM DESCRIPTION OXYGEN SYSTEM If Oxygen is Required or Preferred, Refer to Supplemental Information in Section IX VACUUM SYSTEM The M20V aircraft is all electric. There is no Vacuum System in the standard aircraft.
Page 239 SECTION VII MOONEY AIRPLANE AND SYSTEM DESCRIPTION M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 7 - 36...
Page 240 MOONEY SECTION VIII M20V ACCLAIM ULTRA HANDLING, SERVICE AND MAINTENANCE TABLE OF CONTENTS TITLE ..............
Page 241 SECTION VIII MOONEY HANDLING, SERVICE AND MAINTENANCE M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 8 - 2...
Page 242: Introduction
It is wise to follow a planned schedule of lubrication and preventive maintenance based on clima- 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 experience. He knows your airplane and how to maintain it. Should an extraordinary or...
Page 243: Ground Handling
SECTION VIII MOONEY HANDLING, SERVICE AND MAINTENANCE M20V ACCLAIM ULTRA GROUND HANDLING TOWING For maneuvering the aircraft in close quarters, in the hangar, or on the ramp, use the manual tow bar furnished with the aircraft loose equipment. The tow bar attaches to the nose gear crossbar.
Page 244: Servicing
MOONEY SECTION VIII M20V ACCLAIM ULTRA HANDLING, SERVICE AND MAINTENANCE -CAUTION- Do not raise the aircraft on jacks out of doors when wind velocity is over 8 KTS. When lowering aircraft on jacks, bleed off pressure on all jacks simultaneously and evenly to keep aircraft level as it is lowered.
Page 245: Engine Lubrication
Your Authorized Mooney Service Center will change engine oil in addition to performing all other service and inspection procedures needed when you bring your airplane in for its 50-hour;...
Page 246 MOONEY SECTION VIII M20V ACCLAIM ULTRA HANDLING, SERVICE AND MAINTENANCE Challenger Aviation Products Re- charging instructions must be followed carefully for maximum air filter life. Air filter must be recharged every 100 hours or 12 months or sooner if operated in extreme dusty conditions. Air filter assembly must be replaced after 25 cleanings or sooner if any deterioration or damage is found during pre- flight, post flight or any other aircraft inspections.
Page 247: Gear And Tires
SECTION VIII MOONEY HANDLING, SERVICE AND MAINTENANCE M20V ACCLAIM ULTRA To clean the dry-type induction air filter: 1. Remove engine cowling. 2. Remove filter element. 3. Direct a jet of air from inside of filter out (opposite normal airflow). Cover entire filter area with air jet.
Page 248: Hydraulic Brake Reservoir System
Pre-flight inspection of the propeller blades should include, in addition to the foregoing, an occa- sional wiping with an cloth soaked in kerosene. NEVER USE AN ALKALINE CLEANER ON THE BLADES. Your Mooney Service Center will answer any questions you may have concerning blade repair and inspection. EXTERIOR CARE As with any paint applied to a metal surface, an initial curing period is necessary for developing the desired qualities of durability and appearance.
Page 249: Interior Care
The original weight and balance data and Equipment List are contained in SECTION VI of this manual. This manual is supplied with each new airplane pur- chased from Mooney International Corporation. It is recommended that copies of SECTION VI be made and stored in a safe place.
Page 250 MOONEY SECTION IX M20V ACCLAIM ULTRA SUPPLEMENTAL DATA TABLE OF CONTENTS TITLE ..............
Page 251 SECTION IX MOONEY SUPPLEMENTAL DATA M20V ACCLAIM ULTRA SUPPLEMENT INSERTED DATE AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 9 - 2...
Page 252 MOONEY SECTION IX M20V ACCLAIM ULTRA SUPPLEMENTAL DATA INTRODUCTION FAA approved data pertaining to Limitations, Normal Procedures, 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...
Page 253 SECTION IX MOONEY SUPPLEMENTAL DATA M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 9 - 4...
Page 254 MOONEY SECTION X M20V ACCLAIM ULTRA SAFETY INFORMATION TABLE OF CONTENTS TITLE ..............
Page 255 SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA BLANK AIRPLANE FLIGHT MANUAL ORIGINAL ISSUE - 03-16-2017 10 - 2...
Page 256: Introduction
They are not limited to any particular make or model airplane and do not replace instructions for particular types of airplanes. Your Mooney aircraft was designed and built to provide you with many years of safe and efficient transportation. By maintaining it properly and flying it prudently, you should realize its full poten- tial.
Page 257: General
SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA GENERAL Flying is one of the safest modes of travel. Remarkable safety records are being established each year. As a pilot you are responsible to yourself, your relatives, to those who travel with you, to other pilots and to ground personnel to fly wisely and safely.
Page 258: General Sources Of Information
MOONEY SECTION X M20V ACCLAIM ULTRA SAFETY INFORMATION GENERAL SOURCES OF INFORMATION There is a wealth of information available to the pilot created for the sole purpose of making your flying easier, faster, and safer. Take advantage of this knowledge and be prepared for an emer- gency in the remote event that one should occur.
Page 259: Advisory Information
SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA We urge all pilots to be thoroughly familiar with and use the information in this manual. ADVISORY INFORMATION Airmen can subscribe to services to obtain FAA NOTAMS and Airman Advisories, and these are also available at FAA Flight Service Stations.
Page 260: Walk Around Inspections
MOONEY SECTION X M20V ACCLAIM ULTRA SAFETY INFORMATION tive films and sealants help to keep corrosive agents from contacting metallic surfaces. Corro- sion inspections should be made most frequently under high-corrosion-risk operating conditions, such as in regions of heavy airborne salt concentrations (e.g., near the sea) and high-humidity areas (e.g., tropical regions).
Page 261: Flight In Turbulent Air
SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA FLIGHT IN TURBULENT AIR Even though flight in severe turbulence is to be avoided, flight in turbulent air may be encoun- tered under certain conditions. Flying through turbulent air presents two basic problems, to both of which the answer is PROPER AIRSPEED.
Page 262: Vertigo-Disorientation
MOONEY SECTION X M20V ACCLAIM ULTRA SAFETY INFORMATION VERTIGO - DISORIENTATION Disorientation can occur in a variety of ways. During flight, inner ear balancing mechanisms are subjected to varied forces not normally experienced on the ground. This combined with loss of outside visual reference can cause vertigo.
Page 263: Standard Procedure - Spin Recovery
SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA STANDARD PROCEDURE FOR SPIN RECOVERY In the event of an inadvertent spin, the following recovery procedure should be used: Throttle ............
Page 264: Medical Facts For Pilots
MOONEY SECTION X M20V ACCLAIM ULTRA SAFETY INFORMATION MEDICAL FACTS FOR PILOTS GENERAL Modern industry’s record in providing reliable equipment is very good. When the pilot enters the airplane, he becomes an integral part of the man-machine system. He is just as essential to a successful flight as the control surfaces.
Page 265: Drugs
SECTION X MOONEY SAFETY INFORMATION M20V ACCLAIM ULTRA DRUGS Self-medication or taking medicine in any form when you are flying can be extremely hazardous. Even simple home or over-the-counter remedies drugs such as aspirin, antihistamines, cold tab- lets, cough mixtures, laxatives, tranquilizers, and appetite suppressors, may seriously impair the judgment and coordination needed while flying.

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