Piper PA-32-301 Saratoga User manual

SARATOGA
MAINTENANCE
MANUAL
CARD
1OF
3
PA-32-301/301T
SARATOGA
PIPER
AIRCRAFT
CORPORATION
(PART
NUMBER
761
721) 1A1

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
INTRODUCTION.
This PIPER AIRCRAFT Maintenance Manual is prepared in accordancewith the GAMA (General
Aviation ManufacturersAssociation)format.This maintenancemanual isdivided
into various
Groups which
enable a broad separation of contents (Chapters) within each group.
The various Chapters are broken down into major systemssuch as ElectricalPower, Flight Controls.
Fuel. Landing Gear. etc. The System/Chapters are arranged more or lessalphabetically rather than by
precedenceor importance.AllSystem/Chapters are assigned
a number, whichbecomes
the first elementofa
standardized numbering system. Thus the element "32" of the number series 32-00-00refers to the
System Chapter on "Landing Gear." All information pertaining to the landing gearwill be coveredin this
System Chapter.
The major System/Chapters are then broken down into Sub-System/Sections. These sections are
identifiedbythe second
elementofthe standardized numberingsystem.
The number"40"ofthe basicnumber
series 32-40-00is forthe "Wheels and Brakes" portion of the landinggear.
The individual units within a Sub-System/
Section may be identified by a third element of the
standardized numberingsystem.
such as 32-40-01.
This number could beassignedbythe manufacturer to fit
the coverage requirementsof the publication.
Example:
CHAPTER SYSTEM SUB-SYSTEMS
LANDING GEAR WHEELS AND BRAKES
INDIVIDUAL UNITS
NOSE WHEEL REMOVAL
This manual doesnot contain hardware callouts for installation. Hardware calloutsare only indicated
wherea special applicationis required. To confirmthe correct hardware used, referto the PA-32-301 301T
Parts Catalog P/N 761720,and FAR 43 for proper utilization.
Introduction
Page- 1
1A2 Issued: January 2, 1980
IA2

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
AEROFICHEEXPLANATION AND REVISIONSTATUS
TheMaintenance
Manual
information incorporated
in thisset
of Aerofiche
cards
hasbeen
arranged
in
accordancewith
thegeneral
specifications
of Aerofiche
adopted
bytheGeneral
Aircraft Manufacturer's
Association.
(GAMA).The
information
compiled
in thisAerofiche
Maintenance
Manual will
be
kept
current
byrevisions
distributed
periodically..
These
revisions
will supersede
allprevious
revisions
and
willbe
complete
Aerofiche
cardreplacements
andshall
supersede
Aerofiche
cards
of thesame
number
in theset.
Conversion
of Aerofiche
alpha numeric
code
numbers:
First number
istheAerofiche
card
number.
Letteristhehorizontal
linereference
percard.
Second
number
isthevertical
linereference
percard.
Example:
2J16=Aerofiche
cardnumber
two of given
set.Grid location
J16.
Toaidin locating
thevarious
chapters
and
related
service
information
desired.
the
following
is
provided:
I. A complete
manual
System
Chapter
Index
Guideisfor all fiche
in thisset.
2. A complete
list of Illustrations
isfor all fiche
in thissetfollowingSystem
Chapter
Index
3. A complete
list of Charts
isfor all fichein this setfollowinglistof Illustrations.
4. A complete
listofparagraph
titles
and
appropriate
Gridlocation
numbers
isgiven
atthe
beginning
of
each
Chapter
relating
to theinformation
within thatChapter.
5. Identification
of Revised
Material:
Revised
textandillustrations
areindicated
byablack
vertical
line
along
the
left-hand
margin
of
the frame.oppositerevised,
added
or deletedmaterial. Revisionlines indicateonly currentrevisions,
with changes and additions to or deletions of existing text and illustrations. Changes in
capitalization. spelling.punctuation. indexing.thephysicallocationofthematerialorcomplete
page
additions are not identified by revision lines.
A reference and record of the material revised is included in each chapter's Table of
Contents Effectivity. Thecodes
used
in theeffectivitycolumnsofeach
chapter
aredefinedas
follows.
TABLE OF CONTENTS EFFECTIVITY CODES
Original Issue: None
First Revision: Revision Identification. (IR Month-Year)
Second Revision: Revision Identification. (2R Month-Year)
All subsequent
revisionswill follow with consecutive
revision numbers
such as3R. 4R. etc..
along with the appropriate month-year.
Added Subject: Revision Identification. (A Month-Year)
DeletedSubject: RevisionIdentification. (D Month-Year)
Introduction
Page -2
1A3 Revised: August
II. 1983
IA3

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE
MANUAL
6. Revisions to Maintenance Manual 761 721 issued January 2, 1980 are as
follows:
Effectivity Publication Date Aerofiche Card Effectivity
ORG800102
PR800521
PR800819
PR810923
PR820219
PR820823
PR830811
PR840809
PR850815
IR860431
IR860730
IR860920
IR870316*
January 2, 1980
May 21, 1980
August 19, 1980
September 23, 1981
February 19, 1982
August 23, 1982
August 11, 1983
August 9, 1984
August 15, 1985
April 30, 1986
July 30, 1986
September 20, 1986
May 12, 1987
1,2 and 3
1, 2and 3
, 2 and 3
, 2 and 3
, 2 and 3
, 2 and 3
, 2 and 3
1, 2 and 3
3
1
1
1
I
The date on Aerofiche cards must not be earlier than the date noted for the respective card effectivity. Consult
the latest Aerofiche card in this series for current Aerofiche card effectivity.
This publication contains material revised as of August 15, 1985
(with four interim revisions effective April 30, 1986,July 30, 1986,
September 20, 1986and March 16, 1987).
*INTERIM CHANGE
Revisions appearin chapter5 of card 1.Thereareno otherchanges
in thismaintenance manual. Please discardyourcurrent
card 1and
replaceit with this revisedone. DO NOT DISCARD CARDS 2or
3.
Introduction
Page -3
Interim Revision: March 16, 1987
1A4

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE
MANUAL
VENDOR PUBLICATIONS.
ENGINE
Overhaul Manual = AVCO LYCOMING - OVERHAUL MAL AL
DIRECT DRIVE ENGINE - P \ 60294--
Axco Lycoming Dixision
Williamsport. Pa. 17701
PartsCatalog = AVCO LYCOMING - P N PC-102
Axco Lvcoming Dixision
Williamsport. Pa. 17701
OperatorsHandbook = AVCO LYCOMING 10-540andTIO-540
SERIES AIRCRAFT ENGINES - P N 60297-10
Avco Lycoming Division
Williamsport. Pa. 17701
PROPELIER:
Overhaul Instructions =HARTZELL COMPACT CONSTANT SPEED
and FEATHERING PROPELLER - P N I -- D
Hartzell PropellerInc.
Piqua.Ohio 45356
MAGNETOS:
Installation. Operation
and Maintenance
Instructions =
AUTO FL.IGHT:
D-2000and D-2200SERIES MAGNETO
IGNITION SYSTEM -P N L-928
Bendix Electrical Components
Dixision
Sidney.NewYork 13838
CENTURY 41 AUTO PILOT
EDO-AIRE Mitchell
P.O. Box 610
Mineral Wells.Texas76067
S
Introduction
Page -4
Revised:
August9. 1984
IA5

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
PIPERPUBLICATIONS.
COMMUNICATIONS:
Removal. Installation
and Maintenance
Instructions = 761502AutoControl III B ServiceManual
761481 AutoFlite II ServiceManual
753771 Pitch Trim ServiceManual
Radio Service and
Maintenance Manual = 761 713 Avionics Wiring Diagram Service Manual
Vol. I and Vol. 11(1979)
REPAIRS:
A.B.S. Thermoplastic
Landing Gear Wheel
and Strut Fairing
Repair Instructions =761 708V A.B.S. Thermoplastic Landing Gear
Wheel and Strut Fairing Repair Instruction Manual
PARTS CATALOG 761720
PA-32-301301T
PERIODIC INSPECTION
REPORT FORM 230 1046
PA-32-301 301T
PROGRAMMED INSPEC-
TION MANUAL= 761747
PA-32-301 301T
Introduction
Page -5
Revised: August 9, 1984
1A6

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
GAMA SYSTEM/CHAPTERINDEX GUIDE
SYST
CHAP
4
5
6
7
8
9
10
II
12
20
21
22
23
24
25
27
28
32
33
34
35
SUB-SYST
SECTION TITLE
AIRWORTHINESS
TIME LIMITS MAINT CHECKS
DIMENSIONS AND AREAS
LIFTING AND SHORING
LEVELING AND WEIGHING
TOWING AND TAXIING
PARKING AND MOORING
REQUIRED PLACARDS
SERVICING - LUBRICATION
STANDARD PRACT - AIRFRAME
ENVIRONMENTAL SYSTEM
ALTOFLIGHT
COMMUNICATIONS
ELECTRICAL POWER
EQUIPMENT/FURNISHINGS
FLIGHT CONTROLS
FUEL
LANDING GEAR
LIGHTS
NAVIGATION & PITOT, STATIC
OXYGEN
AEROFICHE
GRID NO.
1A17
IA20
IBII
IB22
ICI
IC5
IC8
IC11
IC15
ID20
IE8
IG8
IG12
IG19
1122
IJ2
2A18
2B17
2D5
2D17
2E6
Introduction
Page - 6
Revised:
August11, 1983
1A7

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
GAMA SYSTEM/CHAPTER INDEX GUIDE (cont)
SYST
CHAP
37
39
51
52
55
56
57
61
70
71
73
74
77
78
79
80
81
91
95
SUB-SYST
SECTION TITLE
VACUUM
ELECTRICAL
STRUCTURES
DOORS
STABILIZERS
WINDOWS
WINGS
PROPELLERS
STANDARD PRACTICES -ENGINES
POWER PLANT
ENGINE FUEL SYSTEM
IGNITION
ENGINE INDICATING
EXHAUST
OIL SYSTEM
STARTING
TURBINES
CHARTS AND WIRING DIAGRAMS
SPECIAL PURPOSE EQUIPMENT
AEROFICHE
GRID NO.
2F4
2F14
2F17
2G9
2G20
2H5
2H14
212
2115
2118
2J14
2J23
2L5
2L14
2L19
3A18
3B9
3B23
3FI
Introduction
Page- 7
Revised:August
9. 1984
1A8

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF ILLUSTRATIONS
FIGURE NO. SUBJECT GRID NO.
6-1. Three Viewof PA-32-301 1B16
6-2. Three Viewof PA-32-301T 1B17
6-3. Station Reference Lines (PA-32-301) 1B19
6-4. Station Reference Lines(PA-32-301T) 1B20
6-5. AccessPlates and Panels 1B21
7-1. Jacking 1B24
8-1. LevelingAirplane 1C3
8-2. Weighing IC4
11 1-. Placards and Decals 1C13
12-1. Fuel Filter Bowland Screen 1C18
12-2. Servicing Points IC22
12-3. Main Gear Oleo Struts (Cut-Away View) 1D2
12-4. Lubrication Chart (Landing Gear, Main) 1DII
12-5. Lubrication Chart (Landing Gear, Nose) ID12
12-6. Lubrication Chart (Control System) ID13
12-7. Lubrication Chart (Air Conditioning Condenser) ID16
12-8. Lubrication Chart (Cabin Door, BaggageDoor
and Seat) ID17
12-9. Lubrication Chart (Power Plant, Propeller and
Control Pivot Points) 1D18
12-10. LubricationChart (Back-UpExtenderand FuelSelector) ID19
20-1. Torque Wrench Formula 1D23
20-2. Method of Installing Rod End Bearings 1D23
20-3. Cherrylock Rivet Removal 1D24
20-4. Hose Line Markings IE2
20-5. Flareless-TubeFittings IE3
20-6. Maximum DistanceBetweenSupports forFluid Tubing IE4
21-1. Cabin Heater. Defrostersand Fresh Air System
(PA-32-301) IE
14
21-2. Cabin Heater. Defroster and Fresh Air System
(PA-32-301T) 1E15
21-3. Air Conditioning System Installation (Typical) 1E23
21-4. ServiceValves 1F4
21-5. Test Gauge and Manifold Set 1F5
21-6. Manifold Set Operation 1F6
21-7. Leak Test Hookup 1F7
21-8. Evacuation Hookup 1F9
21-9. Charging Stand IFII
21-10. Charging Hookup 1F13
21-11. Compressor and Fabricated Oil Dipstick IF17
21-12. Compressor and Alternator Belt Installation 1F18
21-13. Magnetic Clutch 1F20
21-14. Condenser Air Scoop Installation 1F24
21-15. Expansion Valve 1GI
21-16. Components Installation 1G3
21-17. Air Conditioning WiringSchematic (Early Models) 1G4
21-18. Air Conditioning WiringSchematic (Later Models) IG5
Introduction
Page -8
1A9 Revised:August 11,1983

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LIST OF ILLUSTRATIONS
(cont)
FIGL RE NO. SUBJECT GRID NO
23-1. EmergencyLocator Transmitter Schematic
(Narco) IG15
23-2. ELT.Portable Folding Antenna (Narco) IG16
23-3. ELT Using Fixed Aircraft Antenna (Narco) 1G16
23-4. Avionics Master and EmergencySwitch Circuit IG18
24-1. Exploded Viewof Alternator - Prestolite 1H7
24-2. Lamp-Bank Load 1H7
24-3. Removalof Slip Ring End Bearing IHIO
24-4. Removalof Rectifier IHIO
24-5. Removal of Drive End Head IH 10
24-6. Removalof End Head Bearing IH10
24-7. Testing Rotor for Ground IHI1
24-8. Testing Rotor for Shorts IH11
24-9. Installation of Bearing IH13
24-10. Installation of Rectifier IH13
24-11
.Terminal Assembly- Prestolite IH13
24-12. Slip Ring End BearingAssembly IH14
24-13. Testing Alternator IH14
24-14. Brush Installation IH15
24-15. Internal Wiring Diagram IH15
24-16. Alternator Exploded View- Ford IH19
24-17. Rear ViewTerminal Identification 1H19
24-18. Stator Core and Windings IH20
24-19. RectifierAssembly 1H20
24-20. Internal Relationship of Alternator Components 1H21
24-21. RectifierGround and Positive Diode Test II1
24-22. Stator Ground and Negative Diode Test III
24-23. Field Circuit Open or Ground Test 113
24-24. Alternator Housing Disassembly 114
24-25. Rear Housing Components I15
24-26. Front Housing Disassembly 116
24-27. Front Housing Components 116
24-28. Rotor Continuity Test 118
24-29. Rotor Ground Test 119
24-30. Stator Continuity Test 1110
24-31. Stator Ground Test 1111
Introduction
Page-9
lA10 Revised: August 11, 1983
IAI0