Piper SARATOGA II HP PA-32R-301 User manual

SARATOGA SP
SARATOGA II HP
MAINTENANCE MANUAL
PA-32R-301 SARATOGA SP
PA-32R-301 SARATOGA II HP
PA-32R-301T SARATOGA SP
Card 1 of 4
™
THIS HANDBOOK INCLUDES THE MAINTENANCE INFORMATION REQUIRED TO BE AVAILABLE BY FAR PART 23.
PART NUMBER 761 719
1A1
Courtesy of Bomar Flying Service
www.bomar.biz

Published by
Technical Publications
Piper Aircraft Corporation
2926 Piper Drive
Vero Beach, Florida 32960
U.S.A.
1A2

LIST OF EFFECTIVE REVISIONS
Revisions to this Maintenance Manual 761 719 issued Scptembcr 7, 1979 are as follows:
Log of Revisions
Effectivity Date Aerofiche Card Effectivity
PR80014 January 14, 1980 1, 2 and 3
PR800820 August 20, 1980 1, 2 and 3
PR810220 February 20, 1981 1, 2 and 3
PR810923 Septembcr 23, 1981 1, 2 and 3
PR820913 Septembcr 13, 1982 1, 2 and 3
PR821230 December 30, 1982 1, 2 and 3
PR830715 July 15, 1983 1, 2 and 3
PR840810 August 10, 1984 1, 2 and 3
PR850815 August 15, 1985 3
IR860430 April 30, 1986 (Interim) 1
IR860730 July 30, 1986 (Interim) 1
IR860920 September 20, 1986 (Interim)* 1
Revisions to this Maintenance Manual 761 719, reissued July 1, 1993, are as follows:
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Effective Revisions
Page 1
Reissued: July 1, 1993
1A3

LIST OF EFFECTIVE REVISIONS
Log of Revisions
Effectivity Date Aerofiche Card Effectivity
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Effective Revisions
Page 2
Reissued: July 1, 1993
1A4

INTRODUCTION
TABLE OF CONTENTS/EFFECTIVITY
CHAPTER
SECTION SUBJECT GRID NO. EFFECTIVITY
INTRODUCTION 1A6 July 1, 1993
General 1A6 July 1, 1993
Assignment of Subject Material 1A7 July 1, 1993
Application 1A7 July 1, 1993
Effectivity 1A7 July 1, 1993
Aerofiche 1A8 July 1, 1993
Identifying Revised Material 1A8 July 1, 1993
Serial Number Explanation 1A8 July 1, 1993
System/Chapter Index Guide 1A9 July 1, 1993
Warnings, Cautions and Notes 1A14 July 1, 1993
Supplementary Publications 1A14 July 1, 1993
Vendor Publications 1A15 July 1, 1993
Wire Codes 1A19 July 1, 1993
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction Contents
Page 1
Reissued: July 1, 1993
1A5

INTRODUCTION
A. General
The Piper PA-32R-301 / 301T Saratoga Maintenance Manual is prepared in accordance with the
General Aviation Manufacturers Association (GAMA) Specification No. 2, with respect to the
arrangement and content of the System/Chapters within the designated chapter-numbering system.
– NOTE –
Piper Aircraft Corporation expressly reserves the right to
supersede, cancel and/or declare obsolete any part, part numbers,
kits or publication that may be referenced in this manual with-
out prior notice.
– WARNING –
USE ONLY GENUINE PIPER AIRCRAFT PARTS OR
PIPER AIRCRAFT APPROVED PARTS OBTAINED FROM
PIPER APPROVED SOURCES, IN CONNECTION WITH
THE MAINTENANCE AND REPAIR OF PIPER AIR-
PLANES.
Genuine PIPER parts are produced and inspected under rigorous procedures to insure airworthiness
and suitability for use in PIPER airplane applications. Parts purchased from sources other than PIPER,
even though identical in appearance, may not have had the required tests and inspections performed,
may be different in fabrication techniques and materials, and may be dangerous when installed in an
airplane.
Reworked, salvaged or those parts obtained from non-PIPER approved sources, which the service
history is unknown or cannot be authenticated, may have been subjected to unacceptable stresses or
temperatures or have other hidden damage, not discernible through routine visual or usual nondestructive
testing . This may render the part, component or structural assembly, even though originally manufactured
by PIPER AIRCRAFT unsuitable and unsafe for airplane use.
PIPER AIRCRAFT expressly disclaims any responsibility for malfunctions, failures, damage or injury
caused by use of non-PIPER approved parts.
Any question concerning the care of your airplane, be sure to include the airplane serial number in any
correspondence.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 1
Reissued: July 1, 1993
1A6

INTRODUCTION (cont.)
B. Assignment of Subject Material
The content of this publication is organized at three levels. The three levels are:
1. System/Chapter - The various groups are broken down into major systems such as Environmental
Systems, Electrical Power, Landing Gear, etc. The systems are arranged more or less alphabeti-
cally rather than by precedence or importance. They are assigned a number, which becomes the
first element of the standardized numbering system. Thus, the element “28” of the number 28-40-
01 refers to the chapter “Fuel”. Everything concerning the fuel system will be covered in this
chapter.
2. Sub-System/Section - The major systems/chapters of an airplane are broken down into subsys-
tems. These sub-systems are identified by the second element of the standard numbering system.
The element “40” of the number 28-40-01 concerns itself with the indicating section of the fuel
system.
3. Unit/Subject - The individual units within a sub-system/section may be identified by the third ele-
ment of the standard numbering system. The element “01” of the number 28-40-01 is a subject
designator. This element is assigned at the option of the manufacturer and may or may not be
used.
C. Application
Any publication conforming to the GAMA format will use the same basic numbering system. A per-
son wishing information concerning the indication portion of the fuel system, would refer to the
System/Chapter Tab 28-Fuel. The table of contents in the front of this chapter will provide a list of
sub-systems covered in this chapter. For example, the fuel system chapter with a full index would
contain:
28-00 General
28-10 Storage (Tanks, cells, necks, caps, etc.)
28-20 Distribution (Fuel lines, pumps, valves, controls, etc.)
28-30 Dump (If in-flight dumping system is installed)
28-40 Indicating (Quantity, temperature, pressure, etc.)
Refer to the table of contents for a complete breakdown and list of the System/Chapters. The material
is arranged in ascending numerical sequence.
D. Effectivity
The Log of Revisions following the title page of the manual is a record of the revisions that have been
issued for the manual.
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 2
Reissued: July 1, 1993
1A7

INTRODUCTION (cont.)
E. Aerofiche
The General Aviation Manufacturers Association (GAMA) have developed specifications for micro-
fiche reproduction of aircraft publications. The information compiled in this Aerofiche Maintenance
Manual will be kept current by revisions distributed periodically. These revisions will supersede all
previous revisions and will be complete Aerofiche card replacements and shall supersede Aerofiche
cards of the same number in the set.
Conversion of Aerofiche alpha/numeric code numbers:
Example: 2J16 = Aerofiche card number two of a given set and grid location J16.
First number “2” is the Aerofiche card number.
Letter “J” is the horizontal line reference per card.
Second number “16” is the vertical line reference per card.
F. Identifying Revised Material
A revision to a page is defined as any change to the printed matter that existed previously. Revisions,
additions and deletions shall be identified by a vertical black line along the left-hand margin of the
page opposite only that portion of the printed matter that was changed.
A black line in the left-hand margin opposite the chapter/section/subject, page number and date, will
indicate that the text was unchanged but the material was relocated to a different page.
G. Serial Number Explanation
PA-32R-301 Saratoga SP - 1980
Serial Numbers 32R-8013001 thru 32R-8013139
PA-32R-301 Saratoga SP - 1981
Serial Numbers 32R-8113001 thru 32R-8113123
PA-32R-301 Saratogo SP-1982
Serial Numbers 32R-8213001 thru 32R-8213060
PA-32R-301 Saratoga SP- 1993
Serial Numbers 32R-8313001 thru 32R-8313030
PA-32R-301 Saratoga SP-1984
Serial Numbers 32R-8413001 thru 32R-8413024
PA-32R-301 Saratoga SP-1985
Serial Numbers 32R-8513001 thru 32R-8513016
PA-32R-301 Saratoga SP-1986
Serial Numbers 32R-8613001 thru 32R-8613005 and 3213001 thru 3213002
PA-32R-301 Saratoga SP-1987
Serial Numbers 3213003 thru 3213008
PA-32R-301 Saratoga SP-1988
Serial Numbers 3213009 thru 3213019
PA-32R-301 Saratoga SP-1989
Serial Numbers 3213020 thru 3213033 and 3213035
PA-32R-301 Saratoga SP-1990
Serial Numbers 3213034, 3213036, and 3213037
PA-32R-301 Saratoga SP-1992
Serial Numbers 3213038, 3213041
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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INTRODUCTION (cont.)
G. Serial Number Explanation (cont.)
PA-32R-301 Saratoga II HP-1994
Serial Numbers 3213042 and up
PA-32R-301T Turbo Saratoga SP - 1980
Serial Numbers 32R-8029001 thru 32R-8029110 and 32R-8029121
PA-32R-301T Turbo Saratoga SP - 1981
Serial Numbers 32R-8129001 thru 32R-8129114
PA-32R-301T Turbo Saratoga SP - 1982
Serial Numbers 32R-8229001 to 32R-8229068
PA-32R-301T Turbo Saratoga SP - 1993
Serial Numbers 32R-8329001 TO 32R-8329040
PA-32R-301T Turbo Saratoga SP - 1984
Serial Numbers 32R-8429001 thru 32R-8429027
PA-32R-301T Turbo Saratoga SP - 1985
Serial Numbers 32R-8529001 thru 32R-8529020
PA-32R-301T Turbo Saratoga SP - 1986
Serial Numbers 32R-8629001 thru 32R-8629005 and 3229001 thru 3229002
PA-32R-301T Turbo Saratoga SP - 1987
Serial Numbers 32R-8629006 and 32290003
H. System/Chapter Index Guide
The following System/Chapter, Subsystem Section Index Guide is prepared in accordance with
GAMA Specification No. 2 for use with Maintenance Manuals. The following chapters are not applic-
able to this Maintenance Manual: 31, 36, 38, 49, 53, 54, 60, 72, 75, and 83.
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
INTRODUCTION
4 AIRWORTHINESS LIMITATIONS
00 – 1C3 General
5 TIME LIMITS/MAINTENANCE
CHECKS
00 – 1C6 General
10 – 1C7 Time Limits
20 – 1C8 Scheduled Maintenance
50 – 1D2 Unscheduled Maintenance Checks
6 DIMENSIONS AND AREAS
00 – 1D8 General
7 LIFTING AND SHORING
10 – 1D23 Jacking
8 LEVELING AND WEIGHING
10 – 1E3 Weighing and Balancing
20 – 1E4 Leveling
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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INTRODUCTION (cont.)
H. System/Chapter Index Guide (cont.)
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
9 TOWING AND TAXIING
10 – 1E7 Towing
20 – 1E8 Taxiing
10 PARKING AND MOORING
10 – 1E11 Parking
20 – 1E12 Mooring
11 REQUIRED PLACARDS
20 – 1E15 Exterior Placards and Markings
30 – 1E19 Interior Placards and Markings
12 SERVICING
00 – 1F4 General
10 – 1F7 Replenishing
20 – 1G1 Scheduled Servicing
20 STANDARD PRACTICES - AIRFRAME
00 – 1G19 General
21 ENVIRONMENTAL SYSTEMS
00 – 1H8 General
40 – 1H10 Heating
50 – 1H14 Cooling
22 AUTO FLIGHT
00 – 1J9 General
23 COMMUNICATIONS
00 – 1J14 General
20 – 1J16 Emergency Locator Transmitter
24 ELECTRICAL POWER
00 – 1K1 General
30 – 1K3 DC Generation
40 – 1L19 External Power
50 – 1L21 Electrical Load Distribution
25 EQUIPMENT/FURNISHINGS
10 – 2A15 Flight Compartment
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 5
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1A10

INTRODUCTION (cont.)
H. System/Chapter Index Guide (cont.)
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
27 FLIGHT CONTROLS
00 – 2A23 General
10 – 2B7 Aileron and Tab
20 – 2B18 Rudder and Tab
30 – 2C5 Elevator and Tab
50 – 2C21 Flaps
28 FUEL
00 – 2D14 General
10 – 2D20 Storage
20 – 2E10 Distribution
40 – 2E14 Indicating
29 HYDRAULIC POWER
00 – 2E21 General
10 – 2F19 Main
30 ICE AND RAIN PROTECTION
00 – 2G19 General
10 – 2H1 Airfoil
30 – 2H17 Pitot and Static
40 – 2H19 Windows, Windshields and Doors
60 – 2H21 Propellers/Rotors
80 – 2H23 Detection
32 LANDING GEAR
00 – 3A18 General
10 – 3B4 Main Gear and Doors
20 – 3B22 Nose Gear and Doors
30 – 3C16 Extension and Retraction
40 – 3C22 Wheels and Brakes
60 – 3D18 Position and Warning
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 6
Reissued: July 1, 1993
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INTRODUCTION (cont.)
H. System/Chapter Index Guide (cont.)
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
33 LIGHTS
00 – 3E2 General Compartment
10 – 3E6 Flight Compartment
40 – 3E8 Exterior
34 NAVIGATION AND PITOT/STATIC
00 – 3E14 General
10 – 3E18 Flight Instrtuments Pitot/Static
20 – 3E22 Attitude & Direction
40 – 3F2 Independent Position Determining
35 OXYGEN
00 – 3F10 General
10 – 3F12 Crew – Passenger
37 VACUUM
00 – 3G8 General
10 – 3G12 Distribution
20 – 3G16 Indicating
39 ELECTRICAL / ELECTRONIC
PANELS & MULTIPURPOSE
PARTS
40 – 3G20 Multipurpose Electrical Parts
51 STRUCTURES
00 – 3G24 General
52 DOORS
00 – 3H16 General
10 – 3H18 Passenger/Crew
30 – 3I2 Cargo
55 STABILIZERS
10 – 3I6 Horizontal Stabilizers
30 – 3I12 Vertical Stabilizer
40 – 3I14 Rudder
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 7
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INTRODUCTION (cont.)
H. System/Chapter Index Guide (cont.)
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
56 WINDOWS
10 – 3I18 Flight Compartment
20 – 3I20 Cabin
57 WINGS
00 – 3J2 General
20 – 3J4 Auxiliary Structure
40 – 3J6 Attach Fittings
50 – 3J12 Flight Surfaces
61 PROPELLERS
10 – 3J20 Propeller Assembly
20 – 3K6 Controlling
70 STANDARD PRACTICES - ENGINE
00 – 3K12 General
71 POWER PLANT
00 – 3K16 General
10 – 3L6 Cowling
73 ENGINE FUEL SYSTEMS
10 – 4A15 Distribution
20 – 4A20 Controlling
74 IGNITION
00 – 4B3 General
10 – 4B5 Electrical Power Supply
20 – 4B22 Distribution
30 – 4C7 Switching
77 ENGINE INDICATING
00 – 4C13 General
10 – 4C13 Power
20 – 4C16 Temperature
78 EXHAUST
00 – 4C23 General
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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INTRODUCTION (cont.)
H. System/Chapter Index Guide (cont.)
SYSTEM/ SUB-SYSTEM/ TITLE
CHAPTER SECTION – GRID NUMBER
79 OIL
20 – 4D7 Distribution
30 – 4D7 Indicating
80 STARTING
00 – 4D11 General
10 – 4D15 Cranking
81 TURBINES
20 – 4E1 Turbo-Supercharger
91 CHARTS & WIRING DIAGRAMS
00 – 4E16 General
10 – 4F19 Electrical Schematics
95 SPECIAL PURPOSE EQUIPMENT
00 – 4J8 Special Purpose Equipment
I. Warnings, Cautions and Notes
These adjuncts to the text shall be used to highlight or emphasize important points when necessary.
Warnings call attention to use of materials, processes, methods, procedures or limits which must be
followed precisely to avoid injury or death to persons. Cautions call attention to methods and proce-
dures which must be followed to avoid damage to equipment. Notes call attention to methods which
make the job easier. Warning and caution shall be located directly above and notes directly beneath
the text and be in line with the paragraphs to which they apply.
J. Supplementary Publications
The following is a list of publications providing servicing, overhaul and parts information on various
components on the PA-46-310P/350P airplane, which you may use to supplement the maintenance
manual.
Piper Publications:
(1) Parts Catalog - P/N 761 782
(2) Progressive Inspection Manual (50 hour) - P/N 761 788
(3) Periodic Inspection Report Form - P/N 230 1085
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 9
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1A14

INTRODUCTION (cont.)
K. Vendor Publications
The following is a list of the vendor publications, used in conjunction with the servicing, overhaul and
parts information on various components.
– WARNING –
WHEN SERVICING OR INSPECTING VENDOR EQUIPMENT
INSTALLED IN PIPER AIRCRAFT, IT IS THE USER’S
RESPONSIBILITY TO REFER TO THE APPLICABLE
VENDOR PUBLICATION.
1. AIR CONDITIONING COMPRESSOR:
Vendor Address: York Industries
1750 Toronita Street
York, Pennsylvania 17402
[phone]
2 ALTERNATOR
Vendor Address: The Prestolite Co. / Division of Eltra Corp.
P. O. Box 280, Mortaon and Backus Streets
Bay City, Michigan 48706
3 ALTERNATOR
Vendor Address: Ford Motor Company
Ford Electrical and Electronics
6 Parkland Blvd., Suite 450
Dearborn, Michigan 48126
[phone]
4 ALTERNATOR
Vendor Address: Electro Systems
Airport Complex
P. O. Box 273
Fort Deposit, Alabama 06032
[phone]
5. AUTOFLIGHT:
Vendor Address: Century Flight Systems
P. O. Box 610
Mineral Wells, Texas 76067
6. AUTOFLIGHT:
Vendor Address: Bendix/King Radio Corporation
400 N. Rogers Road
Olathe, Kansas 66062
[phone]
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 10
Reissued: July 1, 1993
1A15

INTRODUCTION (cont.)
K. Vendor Publications (cont.)
7. BRAKES:
Vendor Address: Parker Hannifin Corp.
Aircraft Wheel and Brake Division
1160 Center Road
Avon, Ohio 44011
[phone]
8. DEICER SYSTEMS:
Vendor Address: B.F. Goodrich
Transportation Products Division
500 S. Main Street
Akron, Ohio 44318
[phone]
9. EMERGENCY LOCATOR TRANSMITTER:
Vendor Address: Narco Avionics Division
455 Pennsylvania Ave.
Ft. Washington, Pennsylvania 19034
[phone]
10. ENGINE:
Maintenance Manual: TEXTRON LYCOMING
Vendor Address: Textron Lycoming/ Subsidiary of Textron Inc.
652 Oliver Street, Williamsport, Pennsylvania 17701
11. ELECTRIC FUEL PUMP,
Vendor Address: Parker Hannifin Corp.
Airborne Division
P.O. Box 4032, 711 Taylor Street
Elyria, Ohio 44036
[phone], 777-9500
12. ELECTRIC FUEL PUMP,
Vendor Address: Weldon Pumps
340 Golden Oak Parkway
P. O. Box 46479
Oakwood Village, Ohio 44146
[phone]
13. FUEL CELLS
Vender Address Engineered Fabrics Corporation
669 Goodyear Street
Rockmart, GA 30153
[phone]
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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1A16

INTRODUCTION (cont.)
K. Vendor Publications (cont.)
14. GEAR LOCKING ACTUATORS, NOSE
GEAR DOOR ACTUATOR, HYDRAULIC PUMP
AND ALL HYDRAULIC COMPONENTS:
Vendor Address: Parker Hannifin Corp.
1160 Center Road
Avon, Ohio 44011
[phone]HI-LOK FASTENERS AND TOOLS:
Vendor Address: Hi-Shear Corporation
2600 Skypark Drive
Torrance, California 90509
[phone]
15. MAGNETOS:
Vendor Address: Teledyne Continetal Motors
Bendix Magneto Division
P. O. Box 90
Mobile, Alabama 36601
[phone]
16. MAGNETOS:
Vendor Address: Slick Electro Inc.
530 Blackhawk Park Ave.
Rockford, Illinois 61101
[phone]
17. NAVIGATION/STROBE LIGHTS
STANDBY/MAP LIGHTS:
Vendor Address: Whelen Engineering Co. Inc.
Deep River, Conneticut
[phone]
18. OXYGEN SYSTEM:
Vendor Address: Scott Aviation
2225 Erie Street
Lancaster, New York 14086
[phone]
19. PROPELLER AND
PROPELLER GOVERNOR:
Overhaul Instructions:
Vendor Address: Hartzell Propeller Inc.
350 Washington Ave.
Piqua, Ohio 45356
[phone]
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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INTRODUCTION (cont.)
K. Vendor Publications (cont.)
20. RADAR, WEATHERSCOUT:
Vendor Address: Sperry Flight Systems/ Avionics Division
8500 Balboa Blvd.
P.O. Box 9028
Van Nuys, California 91409
[phone]
21. TURBOCHARGER, SAFETY AND
OUTFLOW VALVE, CONTROLLER VALVE:
Vendor Address: Garrett
AiResearch Industrial Division
3201 Lomita Blvd.
Torrance, California 90505
22. VACUUM PUMP, VACUUM REGULATORS
DEICER PUMP:
Vendor Address: Parker Hannifin Corp.
1160 Center Road
Avon, Ohio 44011
[phone]
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
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1A18

INTRODUCTION (cont.)
L. Wire Codes
Schematic Wire Codes
Figure 1
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 14
Reissued: July 1, 1993
1A19
P7A22
CIRCUIT
IDENTIFICATION
WIRE
NUMBER
WIRE
GAUGE
WIRE
SEGMENT LETTER
CIRCUIT
IDENTIFICATION CIRCUIT
A AutoPilot
AC Vent / Air Conditioning
C Control Surface
CL Cigar Lighter
CP Cabin Pressurization
D Pitot, Stall Warning Heat and Propeller Heat
E Engine Instrument
F Flight Instrument
G Landing Gear
GB Vent / Defogger
J Ignition
K Starter
L Lighting
M Hourmeter
OX Oxygen System
P Power
Q Fuel and Oil
RP Radio Power
RC Avionics Cooling
S Stall Warning
W Warning
HARNESS CONNECTOR NUMBERS AND LOCATION
E100 Series - Left Wing
E200 Series - Right Wing
E300 Series - Pressurized Fuselage
E400 Series - Engine and Baggage Compartment
E500 Series - Tail Cone

INTRODUCTION (cont.)
M. Wire Symbols
Schematic Wire Symbols
Figure 2 (Sheet 1 of 2)
PIPER AIRCRAFT
PA-32R-301/301T
MAINTENANCE MANUAL
Introduction
Page 15
Reissued: July 1, 1993
1A20
AIRCRAFT LOCATION SYMBOLS
FUSELAGE STATION WATER LINE BUTT LINE
FS WL BL
ADJUSTABILITY
GENERAL GENERAL MULTICELL
BATTERIES
-+
BUS
SHIELDED
TWISTED
PAIR
COAXIAL
CABLE
SHIELDED
SINGLE
CONDUCTOR
TWISTED
TRIPLE
CABLES AND CONDUCTORS
TWISTED
PAIR
OR
GROUPING OF LEADS
CIRCUIT BREAKERS
CB
BASIC
PUSH
BREAKER
PUSH-PULL
BREAKER
CAPACITOR
GENERAL
SWITCH
BREAKER
CONNECTORS
CURRENT LIMITER
RECEPTACLE PLUG MATED PLUG
& RECEPTACLE
GROUND TO
CHASSIS
(WITH TERMINAL)
GROUND OR
CIRCUIT
RETURN
GROUNDS
FUSE
- A
DIODES
GENERAL ZENER,
UNIDIRECTIONAL
ZENER,
BIDIRECTIONAL
T
P
SHIELDED TWO
CONDUCTOR
W / GROUND
A
B
HORN HEATED ELEMENT SQUIB ELECTRIC
IGNITER A*
INDICATOR LIGHT
(* LETTER DENOTES
COLOR - ASTERISK
IS NOT PART OF SYMBOL)
INCANDESCENT
LAMP
LAMPS
FLUORESCENT
LAMP
MOTOR METER
* LETTER DENOTES THE
TYPE OF METER
i.e. A = AMMETER
M
A
POLARITY
+-
POSITIVE NEGATIVE
POTENTIOMETER
RHEOSTAT
RESISTOR
RELAY COIL
SPLICE
PERMANENT
DISCONNECT
COILS
GENERAL ADJUSTABLE
TRANSISTORS
PNP TYPE NPN TYPE
THERMAL ELEMENT
(TRANSDUCER)
GENERAL
GENERAL
NON SATURATING
TRANSFORMERS
SINGLE PHASE
(3) WINDING
W/CORE
TRANSDUCER
TERMINAL BOARD
1
2
3
4
OR
VARIABLE
RESISTOR