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

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF ILLUSTRATIONS
(cont)
FIGURE NO. SUBJECT GRID NO.
24-32. DiodeTesting 1112
24-33. Front Housing
Assembly 1113
24-34. Rear Housing Bearingand Brush
Assembly
Installation 1114
24-35. RearHousing
Components 1115
24-36. Housing
Assembly 1115
24-37. AlternatorInstallation
-Ford 1116
25-1. Seat
BackLock 1124
27-1. RodEnd Installation
Method IJ12
27-2. Control Column
Assembly 1J14
27-3. Aileron Controls 1J16
27-4. Aileron Rigging IJ0
27-5. Bellcrank
Rigging
Tool IJ20
27-6. Aileron Rigging
Tool IJ'I
27-7. Aileron Rudder
Interconnect IJ23
27-8. Rudder
Controls IK2
27-9. Rudder
Rigging
Tool IK4
27-10. Rudder
Tra\el Adjustments IK4
27-11. Rudder
Rigging IK4
27-12. Clamping
Rudder
Pedals IK4
27-13. Rudder
Trim Control IK5
27-14. Rudder
Steering
Pedal
Assembly IK -
27-15. StabilatorControls IK9
27-16. StabilatorRigging IK 1
27-17. StabilatorTravelAdjustments K15
27-18. Methods
of Securing
Trim Cables K15
27-19. StabilatorTrim Controls IK I'
27-20. Wrapping
Trim Barrels IK20
27-21. StabilatorRigging
Tool K
20
27-22. Manually
Operated
FlapSystem K22
27-23. Flap Step
Adjustment IK24
27-24. Electrically
Operated
FlapSystem IL2
27-25. Flap Rigging
Tool IL4
28-1. FuelSystem
(PA-32-301) 2A2
28-2. FuelSystem
(PA-32-301T) 2A23
28-3. -Fuel
CellInstallation 2B3
284. Installation
of Locking
Fuel
Cap 2Bl I
'2-5. FuelFilter 2B12
28-6. Fuel
Gauge 2B16
32-1. MainGear
OleoStrut Assembly 2B24
32-2. MainGearInstallation 2C2
32-3. Nose
Gear
Oleo
Strut Assembly 2C4
Introduction
Page
-10
1All Revised:
August
9, 1984
1A11

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF ILLUSTRATIONS
(cont)
FIGURE NO. SUBJECT GRID NO.
32-4. Nose Gear Installation 2C8
32-5. Clamping Rudder Pedals in Neutral Position 2C10
32-6. Rudder Pedals at Neutral Angle 2C10
32-7. Main WheelAssembly 2C11
32-8. Nose WheelAssembly 2C13
32-9. Brake Assembly 2C15
32-10. Removaland Installation of Anchor Bolts 2C16
32-11. Brake Disc MinimumThickness 2C16
32-12. Brake System Installation 2C17
32-13. Brake Master Cylinder(Hand Parking Brake) 2C18
32-14. Toe Brake Installation 2C20
32-15. Brake Cylinder (10-30)(Toe Brake) 2C21
32-16. Brake Cylinder (17000)(Toe Brake) 2C21
32-17. Landing Gear Fairing Installation 2D1
33-1. Strobe Light Connections 2D13
34-1. Pitot-Static System Installation 2D20
35-1. Fixed Oxygen System Installation 2E11
35-2. Test Apparatus for TestingOxygen System 2E11
35-3. Oxygen Tubing Installation 2E13
35-4. Installation of Swagelock Fittings 2E16
35-5. Oxygen Cylinderand Regulator Assembly 2E19
35-6. Oxygen System RechargeValve Installation 2E19
35-7. Oxygen Pressure Gauge Installation 2E21
35-8. Oxygen Installation (Portable) 2F2
51-1. Skin Material and Thickness 2F21
51-2. Surface Scratches. Abrasions or Ground-in-Dirt 2G1
51-3. Deep Scratches. Shallow Nicksand Small Holes 2G2
51-4. Mixing of Epoxy Patching Compound 2G2
51-5. Welding Repair Method 2G3
51-6. Repairing of Cracks 2G3
51-7. Various Repairs 2G4
51-8. Repair of Stress Lines 2G6
51-9. Repair of Impacted Damage 2G6
52-1. Snubber Installation 2G14
55-1. Empennage Group 2G23
55-2. Stabilator Balancing 2H1
55-3. Rudder Balancing 2H3
56-1. Windshield Installation (Typical) 2H8
Introduction
Page- 11
1A12 Revised: August 11. 1983

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF ILLUSTRATIONS
(cont)
FIGURE NO. SUBJECT GRID NO.
56-2. Side Window Installation. Single Pane (Typical) 2H9
57-1. Wing Installation 2H17
57-2. Aileron and Flap Installation 2H21
57-3. Aileron Balance Configuration 2H24
61-1. Typical Nicksand Removal Method 214
61-2. Propeller Installation (PA-32-301) 215
61-3. Three Blade Propeller Installation (PA-32-301) 216
61-4. Propeller Installation (PA-32-301T) 217
61-5. Three BladePropeller Installation (PA-32-301T) 218
61-6. Propeller Governor 2113
71-1. Engine Installation (PA-32-301) 2J3
71-2. Engine Mount Installation (PA-32-301T)
(Dvnafocal) 2J4
71-3. Engine Mount Installation(PA-32-301T)
(Lord Mounts) 2J5
73-1. Fuel Injector 2J18
73-2. Schematic Diagram of RSA Fuel Injection System 2J19
73-3. Fuel-Air BleedNozzle 2J21
73-4. Adjustment of EngineControls 2J21
74-1. Height of Spring in Distributor BlockTower 2K4
74-2. Contact Points 2K4
74-3. Engine Timing Marks 2K6
74-4. Timing LightConnected to Magneto 2K6
74-5. Timing Marks on Magneto Rotor 2K7
74-6. Painted Tooth Centered in Timing Window 2K8
74-7. Timing Mark on Rotor Aligned with Pointer 2K8
74-8. Timing Light Connected to Magento and Breakers 2K10
74-9. Cam End Viewof Magneto 2K11
74-10. Removing Impulse Coupling 2K13
74-11. Checking Flyweightto Stop Pin Clearance 2K13
74-12. Stop Pin Installation Dimension 2K13
74-13. Checking FlyweightAxial Wearwith Drill Shank 2K14
74-14. Checking Flyweight Radial Wearwith Gauge 2K14
74-15. Points of Coupling Body Wear 2K15
74-16. Acceptableand Deformed Coupling Springs 2K15
74-17. Checking Impulse Coupling for Magnetization 2K17
74-18. Orientation of Spring in Coupling Body 2K17
74-19. Lifting Inner End of Spring 2K17
74-20. Checking Harness Lead Continuity 2K19
74-21. Checking Harness Lead Insulation Resistance 2K19
74-22. Modified Pliers 2K19
74-23. RemovingSpring From Lead Assembly 2K19
74-24. AssemblyTool 2K21
74-25. Using AssemblyTool 2K21
74-26. Ferrule Postioned Under Braid 2K22
74-27. Ferrule Seating Tool 2K22
74-28. Position of 11-8627
Kit and Contact Spring at
Start of Installation 2K23
Introduction
Page- 12
1A13 Revised:
August 11, 1983

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF ILLUSTRATIONS(cont)
FIGURE NO. SUBJECT GRID NO.
74-29. Position of 11-8627Kit and Contact Spring
After Installation 2K23
74-30. LubricatingSleeve 2K23
74-31. Lubricating Ferrule Shoulder 2K23
74-32. RemovingSpark Plug Frozen to Bushing 2LI
74-33. IgnitionSwitch Wire Positions 2L3
78-1. Exhaust System Inspection Points 2L17
80-1. Exploded Viewof Gear Reduction Starting Motor 3A23
80-2. Turning Starting Motor Commutator 3B1
80-3. Testing Motor Armature for Shorts 3B1
80-4. Testing Motor Fields for Grounds 3B1
80-5. No-Load Test Hook-Up 3B3
80-6. Stall-Torque Hook-Up 3B3
81-1. Turbocharger Installation 3B18
95-1. Tire Balancer Fixture 3F3
95-2. OrificeReplacement Tool 3F4
95-3. Fabricated Tool for BaggageDoor Lock 3F5
95-4. Retainer Ring Tool 3F5
95-5. Fabricated Aileron BellcrankRigging Tool 3F6
95-6. Fabricated Rudder RiggingTool 3F6
95-7. Fabricated Aileron and Flap RiggingTool 3F7
95-8. Fabricated Stabilator RiggingTool 3F8
95-9. Control Surface BalancingTool 3F9
Refer to Card 3, GridNo. 3D11for ElectricalSchematicIndex.
Introduction
Page- 13
1A14 Revised:August9. 1984
1A14

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
LISTOF CHARTS
CHART NO. SUBJECT GRID NO.
601 Leading Particulars and Principal Dimensions 1B13
1201 Thread Lubricants 1D8
1202 Type of Lubricants 1D9
2001 Hose Clamp Tightening (Initial Installation) E4
2101 BlowerSystem WireColor Codes 1E12
2102 Troubleshooting (Air Conditioner) 1E17
2103 Troubleshooting (Air Conditioning System) 1E19
2104 Temperature Pressure IFI
2105 Aluminum Tubing Torque 1F3
2106 System Vacuum Chart 1F9
2107 Compressor Oil Charge 1F16
2401 Troubleshooting (Alternator) 1G23
2402 Troubleshooting (Battery) 1H4
2403 Alternator Specifications (Prestolite) IH16
2404 Alternator BeltTension (Prestolite) 1H
17
2405 Hydrometer Reading and Battery Charge Percent 1118
2406 Electrical System Component Loads 1121
2701 Troubleshooting (Surface Controls) IJ6
2702 Cable Tension Vs.Ambient Temperature IJ11
2801 Troubleshooting Chart (Fuel System) 2A20
2802 Fuel Cell Repair Equipment Lists 2B6
2803 Sender, Fuel Quantity Gauge Tolerances 2B16
3201 Troubleshooting Chart (Landing Gear) 2B21
3202 Nose Gear Alignment Tolerances 2C10
3301 ElectricalSystem Troubleshooting 2D7
3401 Troubleshooting (Rate of Climb Indicator) 2D21
3402 Troubleshooting (Altimeter) 2D23
3403 Troubleshooting (Airspeed Tubes and Indicator) 2D24
3404 Troubleshooting (Gyro Horizon Indicator) 2E1
3405 Troubleshooting (Directional Gyro Indicator) 2E3
3406 Troubleshooting (Magnetic Compass) 2E4
3407 Troubleshooting (Turn and Bank Indicator) 2E5
3501 Troubleshooting (OxygenSystem) 2E9
3502 OxygenSystem Component Limits (Fixed) 2E17
3503 Filling Pressures for Certain Ambient Temperatures 2E23
3504 OxygenSystem Component Limits(Portable) 2FI
3701 Troubleshooting (Vacuum System) 2F6
5101 List of Materials (Thermoplastic Repair) 2F24
6101 Propeller Specifications(PA-32-301) 219
6102 Propeller Specifications(PA-32-301T) 219
7101 EngineTroubleshooting Chart 2121
7401 Troubleshooting (Magneto) 2K2
7402 Coupling Torques 2K24
Introduction
Page- 14
1A15 Revised:
August 11,1983
1A15

PIPER AIRCRAFT
PA-32-301/301 T
MAINTENANCE MANUAL
LISTOF CHARTS(cont)
CHART NO. SUBJECT GRID NO.
7701
7702
7703
7704
7705
7706
8001
8002
8101
9101
9102
9103
9104
9105
9106
9107
Troubleshooting (Manifold Pressure Indicator)
Troubleshooting (Tachometer)
Troubleshooting (Engine Oil Pressure Gauge)
Troubleshooting (Oil Temperature Indicators)
Troubleshooting (Exhaust Gas Temperature
Gauge) (Alcor)
Troubleshooting (Cylinder Head Temperature Gauge)
Troubleshooting (Starter)
Starting Motor Specifications
Troubleshooting (Turbocharger)
Tube and Hose Assembly Torque
Recommended Nut Torques
Decimal Conversions
Conversion Charts
List of Consumable Materials
Electrical Wire Coding
Electrical Symbols
2L7
2L8
2L9
2L9
2L II
2L12
3A21
3B5
3B12
3C2
3C4
3C6
3C7
3C13
3D2
3D3
Introduction
Page 15
Revised:
August
9, 1984
1A16

CHAPTER
AIRWORTHINESS
LIMITATIONS
1A17

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
CHAPTER 4-AIRWORTHINESS LIMITATIONS
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION
SUBJECT GRID
NO.
SUBJECT EFFECTIVITY
4-00-00
4-01-00 AIRWORTHINESS LIMITATIONS
General IA19
IA 19
4 - Cont./Effec.
Page -1
Revised: August 11. 1983
1A18

PIPER AIRCRAFT
PA-32-301/301T
MAINTENANCE MANUAL
AIRWORTHINESS LIMITATIONS.
GENERAL.
The airworthiness limitations are FAA approved and specify inspectionsand maintenancerequired
under Part 91.163
of the FederalAviation Regulations.
The following limitations relatedto fatiguelife of theairplaneandits components
have
been
establihed
with respectto the PA-32-301 301T airplane:
1. The safelife of the airframe structure will be released
when the information becomes
available
2. The safelife limit of the propeller blades
is unlimited.
-NOTE-
Refer to the LIMITATIONS in the Pilot's OperatingHandbook
and FAA Approved Airplane Flight Manual for a detailed
delineation
of the
flight limitationsoftheairplane.
The
mandatory
replacement
timeandor inspectionintervals
of lifelimitedparts are
contained in Chapter5 of this manual.
-END -
4-01-00
Page 4-01
Revised:
August11.
1983
1A19

CHAPTER
TIME LIMITS/MAINT CHECKS
1A20