Piper Arrow IV Turbo User manual

ARROW IV
MAINTENANCE MANUAL
CARD 1 OF 3
PA-28RT-201 ARROW IV
PA-28RT-201T TURBO ARROW IV
PIPER AIRCRAFT CORPORATION
(PART NUMBER 761 694)
1A1
Courtesy of Bomar Flying Service
www.bomar.biz

INTRODUCTION.
This PIPER AIRCRAFT Maintenance Manual is prepared in accordance with the GAMA (General
Aviation Manufacturers Association) format. This maintenance manual is divided into various Groups which
enable a broad separation of contents (Chapters) within each group.
The various Chapters are broken down into major systems such as Electrical Power, Flight Controls, Fuel,
Landing Gear, etc. The System/Chapters are arranged more or less alphabetically rather than by precedence or
importance. All System/Chapters are assigned a number, which becomes the first element of a standardized
numbering system. Thus the element “32” of the number series 32-00-00 refers to the System/Chapter on
“Landing Gear.” All information pertaining to the landing gear will be covered in this System/Chapter.
The major System/Chapters are then broken down into Sub-System/Sections. These sections are identified
by the second element of the standardized numbering system. The number “40” of the basic number series 32-
40-00 is for the “Wheels and Brakes” portion of the landing gear.
The individual units within a Sub-System/Section may be identified by a third element of the standardized
numbering system, such as 32-40-0l. This number could be assigned by the manufacturer to fit the coverage
requirements of the publication.
Example:
This manual does not contain hardware callouts for installation. Hardware callouts are only indicated
where a special application is required. To confirm the correct hardware used, refer to the PA-28RT-201/201T
Parts Catalog P/N 761 693, and FAR 43 for proper utilization.
Introduction
Page - 1
December 1, 1978
1A2
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL
CHAPTER/SYSTEM
LANDING GEAR
SUB-SYSTEMS
WHEELS AND BRAKES
INDIVIDUAL UNITS
NOSE WHEEL REMOVAL
32-40-01

VENDOR PUBLICATIONS.
ENGINE (LYCOMING):
Overhaul Manual =AVCO LYCOMING - OVERHAUL MANUAL
DIRECT DRIVE ENGINE - P/N 60294-7
Avco Lycoming Division
Williamsport, Pa. 17701
Parts Catalog =AVCO LYCOMING - P/N PC-102
Avco Lycoming Division
Williamsport, Pa. 17701
Operators Handbook =AVCO LYCOMING O-360, HO-360, IO-360,
AIO-360, HIO-360, LIO-360 and TIO-360
SERIES AIRCRAFT ENGINES - P/N 60297-12
Avco Lycoming Division
Williamsport, Pa. 17701
ENGINE (CONTINENTAL):
Overhaul Manual =CONTINENTAL - OVERHAUL MANUAL
Form No. X-30030A
Teledyne Continental Motors
Aircraft Products Division
Mobile, Alabama 36601
Parts Catalog =CONTINENTAL - Form No. X-30031A
Teledyne Continental Motors
Aircraft Products Division
Mobile, Alabama 36601
Operators Handbook = CONTINENTAL - Form No. X-30512
Teledyne Continental Motors
Aircraft Products Division
Mobile, Alabama 36601
PROPELLER:
Overhaul Instructions = HARTZELL COMPACT CONSTANT SPEED
and FEATHERING PROPELLER - P/N 113A
Hartzell Propeller Inc.
Piqua, Ohio 45356
Service Manual =McCAULEY C200 SERIES CONSTANT
SPEED PROPELLERS - P/N 780630
McCauley Accessory Division
3535 McCauley Drive
Vandalia, Ohio 45377
MAGNETOS:
Installation, Operation
and Maintenance
Instructions =D-2000 and D-2200 SERIES MAGNETO
IGNITION SYSTEM - P/N L-928
Bendix Electrical Components Division
Sidney, New York 13838
AUTOPILOT:CENTURY 41 AUTOPILOT, Edo-Aire Mitchell
Box 610, Mineral Wells, Texas 76067
Introduction
Page - 2
Revised: August 17, 1982
1A3
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

PIPER PUBLICATIONS.
ELECTRONICS:
AutoFlight II Service
Manual =Piper P/N 761 481
Pitch Trim Service
Manual =Piper P/N 753 771
AutoControl III B and
Altimatic III B Service
Manual =Piper P/N 753 502
Altimatic III C Service
Manual =Piper P/N 761 602
79 Vero Beach Avionics
Wiring Diagrams
Manual =Piper P/N 761 713
AEROFICHE:
PA-28RT-201/201T
Parts Catalog =Piper P/N 761 693
INSPECTION:
PA-28RT-201/201T
Program Inspection
Manual =Piper P/N 761 736
Inspection Forms =Piper P/N 230 818
Introduction
Page - 3
Added: August 17, 1982
1A4
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

AEROFICHE EXPLANATION AND REVISION STATUS
Maintenance manual information incorporated in this set of Aerofiche cards is arranged in accordance with
the general specifications of Aerofiche adopted by the General Aircraft Manufacturer’s Association. The
information compiled in this Aerofiche maintenance manual will be kept current by revisions distributed
periodically. These revisions supersede all previous revisions and are complete Aerofiche card replacements
and supersede Aerofiche cards of the same number in the set.
Identification of revised material:
Revised text and illustrations are indicated by a black vertical line along the left-hand margin of the frame,
opposite revised, and added material. Revision lines indicate only current revisions with changes and additions
to existing text and illustrations. Changes in capitalization, spelling, punctuation, indexing, the physical
location of the material or complete 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.
The codes used in the effectivity columns of each chapter are defined as follows:
TABLE OF CONTENTS/EFFECTIVITY CODES
Original Issue:None
First Revision: Revision Identification, (1R Month-Year)
Second Revision: Revision Identification, (2R Month-Year)
All subsequent revisions will follow with consecutive revision numbers
such as 3R, 4R, etc., along with the appropriate month-year.
Added Subject: Revision Identification, (A Month-Year)
Introduction
Page - 4
Interim Revision: September 21, 1986
1A5
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

Revisions to Maintenance Manual 761 694 issued December 1, 1978 are as follows:
RevisionsDateAerofiche Card Effectivity
ORG 781201December 1, 19781, 2, and 3
PR790223February 23, 19791, 2, and 3
PR791106November 6, 19791, 2, and 3
PR800818August 18, 19801, 2, and 3
PR810724July 24, 19811, 2, and 3
PR811221December 21, 19811, 2, and 3
PR820817August 17, 19821, 2, and 3
PR830713July 13, 19831, 2, and 3
PR840808August 8, 19841, 2, and 3
IR860730July 30, 1986 (Interim)1
IR860921September 21, 1986 (Interim)1
IR950227February 27, 1995 (Interim)*1, 2, and 3
*INTERIM CHANGE TO MAINTENANCE MANUAL 761-694
Chapters 5, 6, and 27 of Card 1, Chapters 32 and 51 of Card 2, and Chapter 71 of
Card 3 have been revised. There are no other changes included in this interim change
revision. Please discard your current cards 1, 2, and 3, and replace them with the
revised ones.
SERIAL NUMBER INFORMATION
PA-28RT-201, Arrow IV - 1979 - Serial Numbers 28R-7918002 to 28R-7918267 inclusive
PA-28RT-201, Arrow IV - 1980 - Serial Numbers 28R-8018001 to 28R-8018106 inclusive
PA-28RT-201, Arrow IV - 1981 - Serial Numbers 28R-8118001 to 28R-8118082 inclusive
PA-28RT-201, Arrow IV - 1982 - Serial Numbers 28R-8218001 to 28R-8218026 inclusive
PA-28RT-201T, Turbo Arrow IV - 1979 - Serial Numbers 28R-7931002 to 28R-7931310 inclusive
PA-28RT-201T, Turbo Arrow IV - 1980 - Serial Numbers 28R-8031001 to 28R-8031178 inclusive
PA-28RT-201T, Turbo Arrow IV - 1981 - Serial Numbers 28R-8131001 to 28R-8131208 inclusive
PA-28RT-201T, Turbo Arrow IV - 1982 - Serial Numbers 28R-8231001 to 28R-8231080 inclusive
PA-28RT-201T, Turbo Arrow IV - 1983 - Serial Numbers 28R-8331001 to 28R-8331051 inclusive
PA-28RT-201T, Turbo Arrow IV - 1984 - Serial Numbers 28R-8431001 to 28R-8431032 inclusive
PA-28RT-201T, Turbo Arrow IV - 1985 - Serial Numbers 28R-8531001 to 28R-8531015 inclusive
PA-28RT-201T, Turbo Arrow IV - 1986 - Serial Numbers 28R-8631001 and 28R-8631005 inclusive
PA-28RT-201T, Turbo Arrow IV - 1987 - Serial Numbers 28R-8631002 to 28R-8631004 inclusive
Serial Numbers 2831001 to 2831033 inclusive
PA-28RT-201T, Turbo Arrow IV - 1988 - Serial Numbers 2831034 to 2831038 inclusive
Introduction
Page-5
Interim Revision: February 27, 1995
1A6
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE
SYSTSUB-SYSTAEROFICHE
CHAPSECTIONTITLEGRID NO.
4AIRWORTHINESS LIMITATIONS1A18
5TIME LIMITS/MAINT CHECKS1A22
6DIMENSIONS AND AREAS1B16
7LIFTING AND SHORING1C5
8LEVELING AND WEIGHING1C9
9TOWING AND TAXIING1C14
10PARKING AND MOORING1C18
11REQUIRED PLACARDS1C22
12SERVICING1D5
20STANDARD PRACT - AIRFRAME1E14
21ENVIRONMENTAL SYSTEM1E21
22AUTOFLIGHT1H1
23COMMUNICATIONS1H8
24ELECTRICAL POWER1H17
27FLIGHT CONTROLS1J17
28FUEL2A18
29HYDRAULIC POWER2B17
32LANDING GEAR2D4
33LIGHTS2F19
34NAVIGATION & PITOT/STATIC2G7
35OXYGEN SYSTEM2G21
37VACUUM SYSTEM2H17
Introduction
Page - 6
Revised: July 13, 1983
1A7
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

GAMA SYSTEM/CHAPTER INDEX GUIDE (cont)
SYSTSUB-SYSTAEROFICHE
CHAPSECTIONTITLEGRID NO.
39ELECTRICAL/ELECTRONIC PANELS AND
MULTI-PURPOSE PARTS2I2
51STRUCTURES2I6
52DOORS2J1
55STABILIZERS2J10
56WINDOWS2J19
57WINGS2J24
61PROPELLER3A18
70STANDARD PRACTICES - ENGINE3B9
71POWER PLANT3B12
73ENGINE FUEL AND CONTROL3C12
74IGNITION3D7
77ENGINE INDICATING3F16
78EXHAUST3G1
79OIL SYSTEM3G6
80STARTING3G10
81TURBINES3H1
91CHARTS AND WIRING DIAGRAMS3H7
95SPECIAL PURPOSE EQUIPMENT3K1
Introduction
Page - 7
Interim Revision: February 27, 1995
1A8
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS
FIGURE NO.SUBJECTGRID NO.
6-1.Three View of PA-28RT-201T1B22
6-2.Three View of PA-28RT-2011B23
6-3.Station Reference Lines of PA-28RT-201/201T1C1
6-4.Access Plates and Panels1C3
7-1.Jacking Arrangements1C7
8-1.Leveling Longitudinally1C12
8-2.Leveling Laterally1C12
8-3.Weighing Arrangement1C12
11-1.Placards and Decals1C24
12-1.Servicing Points (PA-28RT-201)1D8
12-2.Servicing Points (PA-28RT-201T)1D9
12-3.Fuel Strainer1D10
12-4.Lubrication Chart (Landing Gear, Main)1D24
12-5.Lubrication Chart (Landing Gear, Nose)1E2
12-6.Lubrication Chart (Control System)1E4
12-7.Lubrication Chart (Cabin Door, Baggage Door
and Seat)1E8
12-8.Lubrication Chart (Lycoming Power Plant, Propeller
and Control Pivot Points)1E9
12-9.Lubrication Chart (Continental Power Plant, Propeller
and Control Pivot Points)1E10
12-10.Lubrication Chart (Back-Up Extender)1E11
12-11.Lubrication Chart (Air Conditioning Condenser)1E12
20-1.Torque Wrench Extension1E16
20-2.Method of Installing Rod End Bearings1E17
21-1.Cabin Heater and Defroster (PA-28RT-201)1F7
21-2.Cabin Heater and Defroster (PA-28RT-201T)1F8
21-3.Overhead Vent System and Fresh Air System “Not
Available with Air Conditioning”1F9
21-4.Air Conditioning System Installation1F11
21-5.Service Valves1F16
21-6.Test Gauge and Manifold Set1F16
21-7.Manifold Set Operation1F18
21-8.Leak Test Hookup1F19
21-9.Evacuation Hookup1F21
21-10.Charging Stand1F24
21-11.Charging Hookup1F24
21-12.Top Dead Center Casting Mark (Sankyo Compressor)1G6
21-13.Rotation of Clutch Front Plate (Sankyo Compressor
Oil Check)1G6
21-14.York Compressor and Fabricated Oil Dipstick
(PA-28RT-201)1G7
21-15.Compressor and Alternator Belt Installation
(PA-28RT-201)1G9
21-16.Magnetic Clutch (York Compressor)1G10
Introduction
Page - 8
Revised: July 13, 1983
1A9
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
21-17.Condenser Air Scoop Installation1G14
21-18.Expansion Valve1G15
21-19.Components Installation1G17
21-20.Adjustment of Air Conditioning Throttle Switch
(PA-28RT-201)1G17
21-21.Air Conditioning Wiring Schematic1G19
23-1.ELT Portable Folding Antenna (Narco)1H12
23-2.ELT Using Fixed Aircraft Antenna (Narco)1H12
23-3.ELT Schematics1H16
24-1.Lamp-Bank Load1I8
24-2.Exploded View of Alternator (Chrysler)1I10
24-3.Checking Field Coil Current Draw1I10
24-4.Testing Field Circuit1I10
24-5.Testing Positive Rectifiers With C-3829 Tester1I12
24-6.Testing Negative Rectifiers With C-3829 Tester1I12
24-7.Rectifier End Shield and Stator Assembly1I12
24-8.Testing Positive Rectifiers With Test Lamp1I14
24-9.Testing Negative Rectifiers With Test Lamp1I14
24-10.Rectifier and Heatsink Assembly Removal1I14
24-11.Rectifier End Shield Assembly1I14
24-12.Testing Stator1I16
24-13.Removal of Pulley1I16
24-14.Removal of Bearing1I16
24-15.Removal of Rectifier End Shield Bearing1I16
24-16.Testing Rotor for Ground1I17
24-17.Testing Rotor for Opens or Shorts1I17
24-18.Installation of Grease Retainer1I18
24-19.Installation of Rectifier End Shield Bearing1I18
24-20.Installation of Drive End Shield Bearing1I18
24-21.Installation of Pulley1I18
24-22.Installation of Insulators1I20
24-23.Installation of Positive Rectifier Assembly1I20
24-24.Installation of Capacitor1I20
24-25.Installation of Battery Output Insulator1I20
24-26.Installation of Negative Rectifier Assembly1I21
24-27.Installation of Stator1I21
24-28.Exploded View of Alternator (Prestolite)1I23
24-29.Removal of Slip Ring End Bearing1I24
24-30.Removal of Rectifier1I24
24-31.Removal of Drive End Head1J2
24-32.Removal of End Head Bearing1J2
24-33.Testing Rotor for Ground1J2
24-34.Testing Rotor for Shorts1J2
Introduction
Page - 9
Revised: July 13, 1983
1A10
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
24-35.Installation of Drive End Head1J4
24-36.Installation of Rectifier1J4
24-37.Terminal Assembly (Prestolite)1J4
24-38.Slip Ring End Bearing Assembly1J6
24-39.Testing Alternator1J6
24-40.Brush Installation1J7
24-41.Internal Wiring Diagram1J7
27-1.Rod End Installation Method1K3
27-2.Control Column Assembly1K5
27-3.Aileron Controls (Typical)1K8
27-4.Aileron Rigging1K12
27-5.Bellcrank Rigging Tool1K12
27-6.Aileron Rigging Tool1K13
27-7.Rudder and Steering Pedal Assembly1K15
27-8.Rudder Controls1K17
27-9.Rudder Rigging Tool1K18
27-10.Clamping Rudder Pedals1K18
27-11.Rudder Rigging1K18
27-12.Rudder and Stabilator Travel Adjustments1K22
27-13.Rudder Trim Control1K22
27-14.Stabilator Controls1K24
27-15.Stabilator and Stabilator Trim Travel Adjustments1L1
27-16.Stabilator Rigging Tool1L1
27-17.Methods of Securing Trim Cables1L4
27-18.Stabilator Trim Control1L5
27-19.Flap Controls1L9
27-20.Flap Step Adjustment1L11
27-21.Flap Rigging Tool1L11
27-22.Flap Rigging1L14
28-1.Fuel System Diagram (PA-28RT-201)2A24
28-2.Fuel System Diagram (PA-28RT-201T)2B1
28-3.Engine Primer System Placards (PA-28RT-201T)2B2
28-4.Locking Fuel Cap Assembly2B4
28-5.Fuel Filter Bowl and Screen2B5
28-6.Auxiliary Fuel Pump Variable Resistor2B7
28-7.Tolerances; Union Nut and Tubing Nut2B12
28-8.Fuel Gauge2B14
29-1.Schematic Diagram of Hydraulic System2B20
29-2.Schematic Diagram of Hydraulic System2B21
29-3.Hydraulic System Installation2B22
29-4.Hydraulic System Installation2B23
29-5.Hydraulic Pump/Reservoir, Exploded View2C12
29-6.Test and Adjustment of Hydraulic Pump2C13
29-7.Checking Aligning Brackets of Gear Back-Up Extender
Actuator2C17
29-8.Gear Back-Up Extender Actuator2C18
29-9.Nose Gear Actuating Cylinder2C22
Introduction
Page - 10
Revised: August 8, 1984
1A11
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
29-10.End Gland Locking Device2C24
29-11.Main Gear Actuating Cylinder2D1
32-1.Main Gear Oleo Strut Assembly2D16
32-2.Main Gear Installation2D17
32-3.Main Gear Service Tolerances2D19
32-3a.Aligning Main Gear2E3
32-4.Nose Gear Oleo Strut Assembly2E7
32-5.Nose Gear Installation2E9
32-5a.Nose Gear Service Tolerances2E10
32-6.Nose Gear Adjustment (PA-28RT-201)2E16
32-7.Nose Gear Adjustment (PA-28RT-201T)2E17
32-8.Clamping Rudder Pedals in Neutral Position2E19
32-9.Rudder Pedals at Neutral Angle2E19
32-10.Nose Gear Door Retraction Mechanism(PA-28RT-201)2E20
32-11.Nose Gear Door Retraction Mechanism (PA-28RT-201T)2E21
32-12.Nose Wheel Assembly2E24
32-13.Main Wheel Assembly2F1
32-14.Wheel Brake Assembly (30-55)2F2
32-15.Removal of Anchor Bolt2F4
32-16.Installation of Anchor Bolt2F5
32-17.Brake System Installation2F7
32-18.Brake Master Cylinder (Hand Parking Brake)2F8
32-19.Toe Brake Installation2F9
32-20.Brake Cylinder (17000) (Toe Brake)2F10
32-21.Brake Cylinder (10-30) (Toe Brake)2F11
32-22.Adjustment of Nose Gear Down Limit Switch2F15
32-23.Adjustment of Main Gear Down Limit Switch2F15
32-24.Throttle Warning Switches2F17
33-1.Annunciator Panel2G1
33-2.Strobe Light Connections2G4
34-1.Pitot-Static System Installation2G10
35-1.Fixed Oxygen System2G24
35-2.Portable Oxygen System2H1
35-3.Test Apparatus for Testing Oxygen System2H4
35-4.Oxygen Tubing Installations2H5
35-5.Installation of Swagelok Fittings2H8
51-1.Skin Materials and Thickness2I9
51-1a.Baggage Compartment Inspection Holes Cutout Details2I12
51-2.Surfaces Scratches, Abrasions or Ground-in-Dirt2I16
51-3.Deep Scratches, Shallow Nicks and Small Holes2I17
51-4.Mixing of Epoxy Patching Compound2I17
51-5.Welding Repair Method2I19
51-6.Repairing of Cracks2I19
51-7.Various Repairs2I20
51-8.Repair of Stress Lines2I22
51-9.Repair of Impacted Damage2I22
52-1.Installation of Door Snubber2J7
Introduction
Page - 11
Interim Revision: February 27, 1995
1A12
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
55-1.Stabilator Installation2J13
55-2.Stabilator Balance Configuration2J14
55-3.Vertical Fin Installation2J15
55-4.Rudder Installation2J17
55-5.Rudder Balancing2J18
56-1.Windshield Installation (Typical)2J22
56-2.Side Window Installation, Single Pane (Typical)2J23
57-1.Wing Installation2K3
57-2.Aileron and Flap Installation2K8
57-3.Aileron Balance Configuration2K11
61-1.Propeller Installation (Hartzell)3A21
61-2.Propeller Blade Minor Repair3A23
61-3.Propeller Governor3A24
61-4.Propeller Controls3B2
61-5.Propeller Installation (Hartzell)3B4
61-6.Propeller Blade Minor Repair3B5
61-7.Propeller Governor3B7
71-1.Engine Installation (PA-28RT-201T)3B21
71-2.Engine Cowling Installation (PA-28RT-201T)3B24
71-3.Engine Installation (PA-28RT-201)3C7
71-4.Engine Cowling Installation (PA-28RT-201)3C11
73-1.Schematic Diagram of Fuel Injection System3C15
73-2.Fuel Injector Nozzle Assembly3C17
73-3.Engine Controls3C17
73-4.Idle Speed and Mixture Adjustment Points3C19
73-5.Sectional View of Altitude Compensating Fuel Pump Assembly3C19
73-6.Exhaust Bypass Screw3C21
73-7.Fuel Injector3D1
73-8.Schematic Diagram of RSA Fuel Injector System3D2
73-9.Fuel-Air Bleed Nozzle3D4
73-10.Adjustments of Engine Controls3D4
74-1.Magneto Assembly3D12
74-2.Contact Spring Inspection3D13
74-3.Contact Points3D14
74-4.Impulse Coupling3D15
74-5.Flyweight Clearance of Impulse Coupling3D15
74-6.Rotor Holding Tool Installed3D15
74-7.Timing Kit Installed3D15
74-8.Cast-In Timing Marks3D17
74-9.Fabricated Pointer3D17
74-10.Engine Timing Marks3D17
74-11.Removing Spring From Lead Assembly3D20
Introduction
Page-12
Interim Revision: February 27, 1995
1A13
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
74-12.Assembly Tool3D21
74-13.Assembly Tool Application3D22
74-14.Measuring Lead Assembly Length3D23
74-15.Ferrule Seating Tool3D24
74-16.Measuring Wire From Top of Ferrule3D24
74-17.Needle3D24
74-18.Installing Grommet Over Lead Assemblies3D24
74-19.Lead Assembly Installed in Grommet3E2
74-20.Wire Doubled Over For Installation of Eyelet3E2
74-21.Ignition Schematic3E3
74-22.Removing Frozen Spark Plug3E5
74-23.Contact Points3E9
74-24.Rotor Holding Tool Installed3E10
74-25.Timing Kit Installed3E10
74-26.Aligning Timing Marks3E10
74-27.Checking Flyweight Clearance of Impulse Coupling3E10
74-28.Engine Timing Marks3E13
74-29.Magneto Adjustment Limits3E13
74-30.Magneto Timing Marks3E14
74-31.Removing Spring From Lead Assembly3E15
74-32.Assembly Tool3E16
74-33.Using Assembly Tool3E16
74-34.Measuring Lead Assembly Length3E17
74-35.Cutting Metallic Braid From End of Lead3E17
74-36.Unbraiding Metallic Shielding3E17
74-37.Forming Shielding Around Ferrule3E19
74-38.Ferrule Seating Tool3E19
74-39.Needle3E19
74-40.Measuring Wire From Top of Ferrule3E21
74-41.Installing Grommet Over Lead Assemblies3E21
74-42.Lead Assembly Installed in Grommet3E21
74-43.Wire Doubled Over For Installation of Eyelet3E21
74-44.Removing Spark Plug Frozen to Bushing3E22
74-45.Ignition Switch Wire Positions3F1
78-1.Exhaust System Inspection Points3G4
80-1.Exploded View of Gear Reduction Starting Motor3G15
80-2.Turning Starting Motor Commutator3G17
80-3.Testing Motor Armature for Shorts3G17
80-4.Testing Motor Fields for Grounds3G17
80-5No-Load Test Hook-Up3G19
80-6.Stall-Torque Hook-Up3G19
81-1.Schematic Diagram of Turbocharger System3H4
Introduction
Page - 13
Revised: July 13, 1983
1A14
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF ILLUSTRATIONS (cont)
FIGURE NO.SUBJECTGRID NO.
ELECTRICAL SCHEMATICS
—NOTE—
Refer to Grid 313 for Electrical Schematic Index.
95-1.Tire Balancer Fixture3K4
95-2.Control Surface Balancing Tool3K5
95-3.Ignition Harness Ferrule Seating Tool3K6
95-4.Needle3K6
95-5.Assembly Tool for Ignition Harness Insulating
Sleeve Installation3K6
95-6.Charging Stand3K7
95-7.York Compressor and Fabricated Oil Dipstick
(PA-28RT-201)3K7
95-8.Fabricated Gear Back-Up Extender Actuator
Aligning Tool3K8
95-9.Fabricated Stabilator Rigging Tool3K9
95-10.Fabricated Aileron and Flap Rigging Tool3K10
95-11.Fabricated Aileron Bellcrank Rigging Tool3K11
95-12.Fabricated Rudder Rigging Tool3K11
95-13.Fabricated Tool for Baggage Door Lock3K12
95-14.Retainer Ring Tool3K12
95-15.Orifice Replacement Tool3K13
Introduction
Page-14
Revised: July 13, 1983
1A15
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF CHARTS
CHART NO.SUBJECTGRID NO.
601Leading Particulars and Principal Dimensions1B18
2101Troubleshooting (Air Conditioner)1F1
2102Troubleshooting (Air Conditioning System)1F3
2103Temperature Pressure Chart1F12
2104Aluminum Tubing Torque1F15
2105System Vacuum1F21
2106Compressor Oil Charge (York)1G5
2107Blower System Wire Color Codes1G22
2401Troubleshooting (Alternator)1H21
2402Troubleshooting (Battery)1I2
2403Troubleshooting (Annunciator Panel)1I4
2404Alternator Specifications (Prestolite)1J6
2405Hydrometer Reading and Battery Charge Percent1J8
2701Troubleshooting ( Surface Controls)1J21
2702Cable Tension Vs. Ambient Temperature1K2
2801Troubleshooting Chart (Fuel System)2A22
2802Transmitter/Fuel Gauge Tolerances2B14
2803Fuel Quantity Indicators2B15
2804Fuel Pressure Gauge2B16
2901Hydraulic System Troubleshooting2C1
2902Leading Particulars, Hydraulic System2C10
2903Characteristics, Hydraulic Pump Motor2C15
3201Troubleshooting (Landing Gear)2D10
3202Main Gear Service Tolerances2D20
3203Toe-In—Toe-Out Correction Chart2E4
3204Nose Gear Service Tolerances2E11
3301Troubleshooting (Electrical System)2F23
3401Troubleshooting (Rate of Climb Indicator)2G12
3402Troubleshooting (Altimeter)2G14
3403Troubleshooting (Airspeed Tubes and Indicator)2G15
3404Troubleshooting (Gyro Horizon Indicator)2G16
3405Troubleshooting (Directional Gyro Indicator)2G18
3406Troubleshooting (Magnetic Compass)2G19
3407Troubleshooting (Turn and Bank Indicator)2G20
3501Troubleshooting (Oxygen System)2H1
3502Oxygen System Limits2H9
3503Filling Pressure for Certain Ambient Temperatures2H14
3504Portable Oxygen System Component Limits2H16
3701Troubleshooting (Vacuum System)2H19
5101List of Materials (Thermoplastic Repair)2I15
6101Propeller Specifications3A23
6102Propeller Specifications3B5
Introduction
Page-15
Revised: July 13, 1983
1A16
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

LIST OF CHARTS (cont)
CHART NO.SUBJECTGRID NO.
7101Troubleshooting Chart (Engine)3B14
7102Engine Troubleshooting3C2
7301Metered Fuel Assembly Calibration3C22
7302Limits—Fuel Flow Vs. Brake H.P.3C22
7401Troubleshooting (Magneto)3D10
7402Troubleshooting (Magneto)3E7
7701Troubleshooting (Manifold Pressure Indicator)3F18
7702Troubleshooting (Tachometer)3F19
7703Troubleshooting (Engine Oil Pressure Gauge)3F20
7704Troubleshooting (Oil Temperature Indicators)3F20
7705Troubleshooting (Exhaust Gas Temperature Gauge) (Alcor)3F22
7706Troubleshooting (Cylinder Head Temperature Gauge)3F22
8001Troubleshooting (Starter)3G13
8002Starting Motor Service Test Specifications3G21
9101Flare Fitting Torques3H10
9102Recommended Nut Torques3H11
9103Conversion Tables3H13
9104Decimal/Millimeter Equivalents of Drill Sizes3H19
9105List of Consumable Materials3H20
9106Electrical Wire Coding3I1
9107Electrical Symbols3I2
Introduction
Page- 16
Revised: July 13, 1983
1A17
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

CHAPTER
AIRWORTHINESS
LIMITATIONS
1A18

CHAPTER 4 - AIRWORTHINESS LIMITATIONS
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION GRID
SUBJECT SUBJECT NO. EFFECTIVITY
4-00-00 AIRWORTHINESS LIMITATIONS 1A20
4-00-01 General 1A20
4 - Cont./Effec.
Page - 1
Revised: February 23, 1979
1A19
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL

AIRWORTHINESS LIMITATIONS.
GENERAL.
The airworthiness limitations is FAA approved and specifies inspections and maintenance required under
Part 91.163 of the Federal Aviation Regulations.
The following limitations related to fatigue life of the airplane and its components have been established
with respect to the PA-28RT-201/201T airplane:
1. The safe life of the airframe structure will be released when the information becomes available.
2. The safe life limit of the propeller blades is unlimited.
—NOTE—
Refer to the LIMITATIONS in the Pilot’s Operating Handbook
and FAA Approved Airplane Flight Manual for a detailed
delineation of the flight limitations of the airplane. The
mandatory replacement time and/or inspection intervals of life
limited parts are contained in Chapter 5 of this manual.
—END—
4-00-01
Page 4-01
December 1, 1978
1A20
PIPER AIRCRAFT
PA-28RT-201 / 201T
MAINTENANCE MANUAL