Mooney M20V Acclaim Ultra Installation and user guide

M20V
SERVICE AND MAINTENANCE
MANUAL
MOONEY
P/N: MAN185
ISSUED: MARCH 2017
MOONEY INTERNATIONAL CORPORATION
Copyright 2017 - All Rights Reserved
MOONEY INTERNATIONAL CORPORATION - 165 Al Mooney Road, Kerrville, Texas 78028
tel: [phone] www.mooney.com
REVISED: OCTOBER 2017

MOONEY INTERNATIONAL CORPORATION
M20V SERVICE AND MAINTENANCE MANUAL
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WARNING
Manufactured with 1,1,1 Trichlorethane substances which are determined
to harm public health and environment by destroying ozone in the upper atmosphere.
and installed on the Mooney Aircraft Model(s) addressed in this pubication.
This warning applies to placards manufactured at Mooney Aviation Company, Inc. facility
WARNING
Manufactured with 1,1,1 Trichlorethane substances which are determined
to harm public health and environment by destroying ozone in the upper atmosphere.
and installed on the Mooney Aircraft Model(s) addressed in this pubication.
This warning applies to placards manufactured at Mooney Aviation Company, Inc. facility

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SERVICE AND MAINTENANCE MANUAL
LOG OF REVISIONS
The Log of Revisions pages are updated by Mooney International Corporation each time revisions are issued.
The Log of Revisions contains a list of all revisions made to the service and maintenance manual since its
original issue. By comparing the Log of Revisions to the Record of Incorporated Revisions, the user of this
manual can verify that all applicable reversions are included.
Revision Status Date FAA Approved
ORIGINAL ISSUE MARCH 28, 2017
Revision A OCTOBER 4, 2017
Always destroy superceded pages when you insert the revised pages.
Revision/
Date
Affected Pages Description of Revision
INTRODUCTION:
OI ALL Pages Original Issue
Chapter 4 AIRWORTHINESS:
OI ALL Pages Original Issue
Chapter 5 TIME LIMITS:
OI ALL Pages Original Issue
Chapter 6 DIMENSIONS:
OI ALL Pages Original Issue
Chapter 7 LIFTING AND SHORING:
OI ALL Pages Original Issue
Chapter 8 LEVELING AND WEIGHING:
OI ALL Pages Original Issue
Chapter 10 PARKING AND MOORING:
OI ALL Pages Original Issue
Chapter 12 SERVICING:
OI ALL Pages Original Issue
Chapter 21 ENVIRONMENTAL SYSTEMS:
OI ALL Pages Original Issue
Chapter 22 AUTOPILOT SYSTEMS:
OI ALL Pages Original Issue
Chapter 24 ELECTRICAL POWER:
OI ALL Pages Original Issue
Chapter 25 EQUIPMENT AND FURNISHINGS:
OI ALL Pages Original Issue
Chapter 27 FLIGHT CONTROLS:
ACover page Rev A
ALog of Revisions Rev A
AList of Effected
Pages
Rev A
OCT 2017
LOG OF REVISIONS/SERVICE BULLETINS

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ATable of Contents Rev A
APage 17 Rev A - Revised Aileron Allowable deflection up or down
Chapter 28 FUEL:
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Chapter 30 ICE PROTECTION:
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Chapter 32 LANDING GEAR:
OI ALL Pages Original Issue
Chapter 33 LIGHTS:
OI ALL Pages Original Issue
Chapter 34 NAVIGATION:
OI ALL Pages Original Issue
Chapter 35 OXYGEN:
OI ALL Pages Original Issue
Chapter 39 ELECTRICAL PANELS:
OI ALL Pages Original Issue
Chapter 51 STRUCTURES:
OI ALL Pages Original Issue
Chapter 52 DOORS:
OI ALL Pages Original Issue
Chapter 55 STABILIZERS:
OI ALL Pages Original Issue
Chapter 57 WINGS:
OI ALL Pages Original Issue
Chapter 61 PROPELLERS:
OI ALL Pages Original Issue
Chapter 71 POWERPLANT:
OI ALL Pages Original Issue
Chapter 73 ENGINE FUEL SYSTEMS:
OI ALL Pages Original Issue
Chapter 74 IGNITION:
OI ALL Pages Original Issue
Chapter 76 ENGINE CONTROLS:
OI ALL Pages Original Issue
Chapter 77 ENGINE INDICATING:
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Chapter 78 EXHAUST:
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Chapter 79 OIL:
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Chapter 80 STARTING:
OI ALL Pages Original Issue
Chapter 81 TURBOCHARGER:
OI ALL Pages Original Issue
Chapter 91 ELECTRICAL WIRING SCHEMATICS AND HARNESSES:
OI ALL Pages Original Issue
Chapter 95 SPECIAL TOOLS:
OI ALL Pages Original Issue
NOTE:
A list of Effective Pages will appear at the beginning of each chapter.
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SERVICE BULLETIN LOG
Service Bulletins and Service Instructions are issued by the manufacturer and may require a special inspection or
modification to the airplane. At the time of delivery, applicable service bulletins are normally incorporated. When a
subsequent Service Bulletin is issued after the delivery date, Mooney International Corporation will post them on the
www.mooney.com website for owner’s concerning details for compliance. The Service Bulletin number, date, title
and incorporation should be noted in the log provided . The Service Bulletin will be incorporated into the next sched-
uled revision of the maintenance manual.
S.B.
NUMBER
DATE DESCRIPTION OF BULLETIN COMPLETED BY
LOG OF REVISIONS/SERVICE BULLETINS

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BULLETIN
COMPLETED BY
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INTRODUCTION
This manual provides servicing and maintenance infor-
mation for the Mooney Model M20V, Serial Numbers
33- 0001 and ON. Maintenance actions that refer to a
limited number of aircraft will be designated by serial
number of applicable airplanes.
The Part Number’s of replacement or repair parts
should be identified using the Illustrated Parts Catalog
applicable to Model and S/N of aircraft being worked
on. The correct P/N can be ordered through any Au-
thorized Mooney Service Center, visit www.mooney.-
com/Support for a listing. See Section 91 for excep-
tions on Electrical Components.
The format and contents of this manual are prepared in
accordance with GENERAL AVIATION MANUFAC-
TURER’S ASSOCIATION (GAMA) Specification No. 2.
The manual is supplemented with wiring schematics
and Electrical Harnesses for the various model year
airplanes, as necessary. These are located in Chapter
91 of this Service and Maintenance Manual.
-NOTE-
To request additional Technical Publications, or
current revisions to this manual, contact your
Authorized Mooney Service Center or email
[email protected]
MOONEY INTERNATIONAL CORPORATION
165 AL MOONEY ROAD
Kerrville, TX. 78029- 0072
The YELLOW CARD supplied in this manual is
No Longer used for subscription mailing lists.
To be informed of all Revision Status of Technical
Publications, Service Bulletins, Service
Instructions, Special Letters
Email your Contact Information to
[email protected] or [email protected]
The Technical Publications Revision Status of all
Mooney Manuals can be electronically viewed at
www.mooney.com within the Service and Support sec-
tion. To be on the email distribution list for these items
as well as Service Bulletins, Service Instructions and
special letters email [email protected] .
Correspondence concerning maintenance or part
numbers on an airplane should contain the aircraft
model number and serial number. The serial number
appears on the identification placard located on the aft
end, left hand side of the tailcone below the horizontal
stabilizer.
ASSIGNMENT OF SUBJECT MATERIAL
The content of this publication is organized at four lev-
els:
Group
Chapter (System)
Section (Sub- system)
Subject (Unit)
GROUP
These are primary divisions of the manual that enable
broad separation of content, ie., Airframe Systems vs
Powerplant Systems. These groups are identified by
tabs.
CHAPTER (System)
The various groups contain major systems information
such as flight controls, landing gear, etc. The systems
are arranged numerically per GAMA recommended
number assignment, It is suggested, for example that
“Fuel” be identified with the Chapter number “28”. The
sequence of numbers, 28- 00- 00, refers to the General
information of the Fuel Systems.
SECTION (Sub- System)
The major systems of an aircraft are broken down into
sub- systems. These sub- systems are identified by the
second element of the sequence of numbers, ie.,
28- 20- 00. The element - 20- indicates the distribution
portion of the fuel system.
SUBJECT (Unit)
The individual units within a sub- system may be identi-
fied by a third element of the sequence of numbers, ie.,
28- 20- 01. This number is assigned by the manufactur-
er and may or may not be used depending upon the
complexity of the maintenance action recommended.
APPLICATION OF NUMBERING SYSTEM
Mooney International Corporation, Inc. is in the pro-
cess of revising all applicable maintenance technical
publications to GAMA format. When this effort is com-
pleted any publication concerning maintenance of air-
craft will conform to this basic numbering system. Any
person wishing information concerning the Fuel Dis-
tribution System would refer to the pages identified as
28- 20- 00, in any maintenance oriented publication.
These pages will be numbered sequentially within each
system breakdown in the current Mooney series of air-
craft. As Mooney aircraft models become more com-
plex the page numbers may be sequentially numbered
within sub- systems.
The table of contents in the front of each Chapter will
provide a list of systems and/or subjects covered in the
Chapter. For example:
28- 00 General
28- 10 Storage
(Tanks, vents, repair, etc.)
28- 20 Distribution
(Boost pumps, fuel lines, etc.)
28- 40 Indicating
(Sender Units, quantity gauges, etc.)
If there is a reason to distinguish between LEFT
HAND or RIGHT HAND fuel quantity sending units
then the number would be expanded to 28- 40- 01
(Left Hand) and 28- 40- 02 (Right Hand). This con-
cept will apply to any expanded information through-
out the publications.
INTRODUCTION

MOONEY AVIATION COMPANY, INC.
M20V SERVICE AND MAINTENANCE MANUAL
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SUPPLEMENTAL TYPE CERTIFICATE (STC) INFORMATION
Modifications to the Mooney airplane, which are incorporated under a Supplemental Type Certificate (STC), can
affect procedures and inspection as well as part replacement cycles. The STC holder will issue maintenance proce-
dures and appropriate time intervals for areas of the airplane that are affected by the STC. Sometimes the STC
modifications can change operating characteristics, component loads, and component stresses. Since the interface
of the STC modification with the existing structure can result in a number of unknown elements, the standards estab-
lished by Mooney International Corporation may not be valid.
SUPPLEMENTARY PUBLICATIONS
The following list of Manufacturers and/or publications can provide servicing and maintenance information on com-
ponents of the Mooney, Model M20V. Not all avionics equipment Manufacturers or publications are listed due to the
many configurations that can be installed in the aircraft. These can be obtained from the repair stations for a particu-
lar avionics manufacturer
Any publications available from Mooney International Corporation are listed in the Parts Price List and are available
through any Mooney Service Center, refer to www.mooney.com for a complete listing of manual revisions. Most
manufacturer/vendor publications are not available through Mooney International Corporation These should be ob-
tained from the applicable Manufacturer/Vendor.
As publications on various components become available, they will be added to the list below.
VENDOR ADDRESSES - PUBLICATIONS
ENGINE PUBLICATIONS
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Accounts Receivable (Prepaid only).
Overhaul Manual for Continental Motors Aircraft TSIO- 550- G Engine Models, Form M18 Illustrated Parts Catalog
for Continental Motors TSIO- 550- G series aircraft engines, Form X30615A Maintenance & Operators Manual for
Continental Motors TSIO- 550- G aircraft engines, Form OI- 18 Service Bulletins - Specify model of engine for which
maintenance data is desired when ordering Fuel Injection System Parts and Overhaul Manual, Form X30593A Mas-
ter Service Manual Continental Motors Ignition Systems and Components, Form X40000
ACCESSORY PUBLICATIONS
PROPELLER
Hartzell Propellers -
Hartzell Propellers Inc.
One Propeller Place
Piqua, OH 45356 - 2634 U.S.A.
Ph: 937 - 778 - 4200 (general)
Ph: 937 - 778 - 4379 (prod. support)
Product Support Fax: [phone]
Hartzell Propeller Owner’s Manual - 115N
MAGNETO
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.,
for CMI (Bendix), Type S6RSC- 25P Pressurized, Im-
pulse Coupling.
TURBOCHARGER
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.,
for (CMI/Kelly Aerospace), Model TA36
Kelly Aerospace Corporate Office
1400 East South Boulevard
Montgomery, Alabama, U.S.A. 36116
Ph: 334- 286- 8551
Fax: [phone]
ALTERNATOR/STANDBY ALTERNATOR
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.
B & C Specialty Products Inc.
123 East 4th St.
P. O . B o x B
Newton, Kansas USA, 67114- 0894
Telephone [phone]
FAX [phone]
STARTER
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.
Starter Service Manual
INTRODUCTION

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FUEL PUMP (Engine Driven)
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.
IGNITION SYSTEM
Continental Motors
Aircraft Products
P. O . B o x 9 0
Mobile, Alabama, USA, 36601
Attn: Publications Dept.
GARMIN G1000 INTEGRATED AVIONICS SYSTEM
Garmin International, Inc.
1200 E. 151st Street
Olathe, KS 66062
Telephone [phone]
Operation, Maintenance and Troubleshooting Manuals
SPEED BRAKES
Precise Flight, Inc.
63120 Powell Butte Rd.
Bend, OR 97701
Telephone: [phone]
www.preciseflight.com
OXYGEN SYSTEMS
Scott Aviation
Factory Service Department
225 Erie Street
Lancaster, NY 14086
Telephone [phone]
Fax [phone]
Precise Flight, Inc.
63120 Powell Butte Rd.
Bend, OR 97701
Telephone: [phone]
www.preciseflight.com
DE- ICING/ANTI- ICING (TKS)
Aerospace Systems & Technologies, Inc.
2400 Airport Road, Suite 2
Lawrence, KS 66044
Telephone [phone]
Fax [phone]
DE- ICING PROPELLOR
B. F. Goodrich Avionics Systems, Inc.
5353 52nd Street SE
P.O. Box 873
Grand Rapids, MI 49588- 0873
Telephone [phone]
NAVIGATION LIGHTS & STROBES
Whelen Engineering Co.
Route 145, Winthrop Road
Chester, CT 06412- 0684
HEADSETS
Bose Corporation
145 Pennsylvania Avenue
Framingham, MA 01701
DRE Communications Company
1723 Little Orchard Street
San Jose, CA 95125
Telephone [phone]
Telex Aviation
Sales Department
9600 Aldrich Avenue S.
Minneapolis, MN 55420- 9976
EMERGENCY LOCATOR TRANSMITTER (ELT)
ARTEX ME- 406
Artex Aircraft Supplies
P.O. Box 1270
Canby, Oregon 97013
Telephone [phone]
or 1- 800- 547- 8901 (for USA and Canada)
(503) 678- 7930
www.artex.net
AVIONICS
Honeywell/Allied Signal
400 N. Rodgers Road
Olathe, KS 66062
Mid- Continent Instrument Company
9400 East 34th Street North
Wichita, KS 67226
Telephone [phone]
J P. Instruments
P.O. Box 7033
Huntington Beach, CA 92615
Northern Airborne Tech., Ltd.
#14 – 1925 Kirschner Rd.
Kelowna, Canada V1Y 4N7
Telephone [phone]
Fax [phone]
LANDING GEAR COMPONENTS
Eaton Corporation
Aerospace Controls Div.
2338 Alaska Avenue
El Segundo, CA, 90245
AMSAFE INFLATABLE RESTRAINT COM-
PONENTS
AMSAFE AVIATION
1043 N. 47th Ave.
Phoenix, AZ (USA) 85043
Telephone [phone]
www.amsafe.com
INTRODUCTION

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CHAPTER - SECTION - TITLE
INDEX GUIDE
CHAPTER SECTION TITLE
1- 3 RESERVED - MAY BE USED LATER
4AIRWORTHINESS LIMITATIONS
5TIME LIMITS/MAINTENANCE CHECKS
00 GENERAL
10 TIME LIMITS
20 SCHEDULED MAINTENANCE CHECKS
6DIMENSIONS AND AREAS
00 GENERAL
7LIFTING AND SHORING
10 JACKING
8LEVELING AND WEIGHING
00 LEVELING
9TOWING AND TAXIING
00 GROUND HANDLING
10 TOWING
20 WARM- UP AND TAXIING
30 EMERGENCY PROCEDURES
10 PARKING AND MOORING
00 GENERAL
10 PARKING
20 MOORING
11 PLACARDS AND MARKINGS
00 GENERAL
10 MARKINGS
20 PLACARDS - EXTERIOR/INTERIOR
12 SERVICING
00 SERVICING
10 REPLENISHING
20 SCHEDULED SERVICING
20 STANDARD PRACTICES – AIRFRAME
00 GENERAL
21 ENVIRONMENTAL SYSTEMS
00 CABIN VENTILATION SYSTEM
40 HEATING
50 COOLING
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CHAPTER SECTION TITLE
22 AUTOPILOT SYSTEMS (OPTIONAL)
00 GENERAL
10 GARMIN GFC- 700
20 TROUBLESHOOTING
30 AUTOPILOT DISCONNECT SWITCH
40 SYSTEM MONITORING
24 ELECTRICAL POWER
00 GENERAL
30 DC GENERATION
50 ELECTRICAL LOAD DISTRIBUTION
25 EQUIPMENT/FURNISHINGS
00 GENERAL
10 FLIGHT COMPARTMENT
50 CARGO COMPARTMENT
60 EMERGENCY EQUIPMENT
27 FLIGHT CONTROLS
00 GENERAL
10 AILERON SYSTEM
20 RUDDER SYSTEM
30 ELEVATOR SYSTEM
40 STABILIZER TRIM SYSTEM
50 WING FLAP SYSTEM
60 AILERON/RUDDER INTERCONNECT SYSTEM
90 MISCELLANEOUS
28 FUEL
00 GENERAL
10 STORAGE
20 DISTRIBUTION
30 DUMP
40 INDICATING
90 MISCELLANEOUS
30 ICE AND RAIN PROTECTION
00 GENERAL
10 AIRFRAME ICING PROTECTION
30 PITOT AND STATIC
40 WINDSHIELDS
60 PROPELLER
70 SERVICING/CLEANING
INTRODUCTION

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CHAPTER SECTION TITLE
32 LANDING GEAR
00 GENERAL
10 MAIN LANDING GEAR AND DOORS
20 NOSE LANDING GEAR AND DOORS
30 EXTENSION AND RETRACTION
40 WHEELS AND BRAKES
50 STEERING
60 POSITION AND WARNING
80 MISCELLANEOUS
33 LIGHTS
00 GENERAL
10/20 INTERIOR LIGHTS – MAINTENANCE PRACTICES
40 EXTERIOR LIGHTS – MAINTENANCE PRACTICES
34 NAVIGATION
00 GENERAL
10 PITOT & STATIC AIR PRESSURE SYSTEM
30 DIRECTIONAL GYRO COMPASS
90 MISCELLANEOUS INSTRUMENTS
35 OXYGEN
00 GENERAL
37 VACUUM
00 GENERAL
39 ELECTRICAL PANELS AND COMPONENTS
00 GENERAL
10 INSTRUMENT AND CONTROL PANELS
20 ELECTRICAL AND ELECTRONICS EQUIPMENT RACKS
51 STRUCTURES
00 GENERAL
10 STRUCTURAL REPAIR – GENERAL
52 DOORS
00 GENERAL
10 CABIN DOOR – MAINTENANCE PRACTICE
30 BAGGAGE COMPARTMENT DOOR - MAINTENANCE PRACTICE
60 ENTRANCE STEP
INTRODUCTION

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CHAPTER SECTION TITLE
53 FUSELAGE
00 GENERAL
10 MAIN FRAME
20 FIREWALL
30 PLATES/SKIN
40 ATTACH FITTINGS
55 STABILIZERS
00 GENERAL
10 HORIZONTAL STABILIZER
20 ELEVATOR
30 VERTICAL STABILIZER
40 RUDDER
56 WINDOWS
00 GENERAL
10/20 WINDSHIELD & CABIN WINDOWS
50 ACRYLIC DRILLING
57 WINGS
00 GENERAL
10 MAIN FRAME
20 AUXILIARY STRUCTURE
30 PLATES/SKINS
40 ATTACH FITTINGS
50 FLIGHT SURFACES
61 PROPELLERS
00 GENERAL
10 PROPELLER ASSEMBLY
20 CONTROLLING
40 BALANCING PROCEDURES
71 POWERPLANT
00 GENERAL
10 COWLING
20 MOUNTS
30 FIRESEALS
60 AIR INTAKES
72 ENGINE – RECIPROCATING
00 GENERAL
INTRODUCTION

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CHAPTER SECTION TITLE
73 ENGINE FUEL SYSTEM
00 GENERAL
10 DISTRIBUTION
20 CONTROLLING
30 INDICATING
40 FUEL INJECTOR
60 FUEL PUMP
74 IGNITION
00 GENERAL
10 POWER CONTROL
20 ENGINE FIRING ORDER
30 SWITCHING
76 ENGINE CONTROLS
00 GENERAL
10 ENGINE CONTROLS RIGGING
20 MAINTENANCE
77 ENGINE INDICATING
00 GENERAL
10 POWER
20 TEMPERATURE
30 PRESSURE
78 EXHAUST
00 GENERAL
10 INSTALLATION
30 SERVICING
40 REPLACEMENT COMPONENTS
79 OIL
00 GENERAL
20 DISTRIBUTION
30 INDICATING
40 TRANSDUCERS TEST
50 TROUBLESHOOTING
80 STARTING
00 GENERAL
10 CRANKING
INTRODUCTION

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CHAPTER SECTION TITLE
81 TURBINES
00 GENERAL
20 TROUBLESHOOTING
30 SERVICING
40 PERIODIC REPLACEMENT COMPONENTS
91 SCHEMATICS AND HARNESSES
00 GENERAL
20 ELECTRICAL SYSTEM HARDWARE CHARTS
30 SCHEMATICS AND HARNESSES
95 SPECIAL EQUIPMENT
INTRODUCTION

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INTRODUCTION

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CHAPTER 4
AIRWORTHINESS
LIMITATIONS