Piper Parts Catalog

Piper PA-23 Apache · Checklist

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Overview

This document is a Parts Catalog for the Piper PA-23-150 and PA-23-160 Apache models. It provides detailed information on replacement parts, including part numbers, descriptions, and serial number applicability. The catalog is organized into sections that cover various components of the aircraft, making it easier for maintenance personnel and owners to identify and order the correct parts. The document emphasizes that it should not be used for rigging and installation purposes, and it includes a comprehensive table of contents for navigation.

This catalog is for the Piper PA-23-150 and PA-23-160 Apache models.
It includes detailed part numbers and descriptions for replacement parts.
Serial number ranges for parts applicability are provided.
Ordering instructions specify the need for model and serial number.
A standard paint chart for the aircraft is included.

Document

Source

Originally published by www.aeroelectric.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: Checklist
Year: 1998
Pages: 358
File size: 17 MB
Publisher: www.aeroelectric.com

How rare is it?

7Piper PA-23 Apache registered worldwide · 0 active

Common. Rarer than 8% of the aircraft models we track.

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Pilot's Operating Handbook / AFM
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Type Certificate (TCDS)

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PIPER PA-23-160 Apache

In this document

Introduction

The Parts Catalog is designed for the Piper PA-23-150 and PA-23-160 Apache models, providing identification of replacement parts. It is divided into major sections, each containing illustrations and part listings. The catalog should be studied before use to understand its arrangement.

How to Identify a Part

To identify a part, refer to the figures and the table of contents to locate the section. Find the part in the illustration and note the index number for complete descriptions in the parts listing.

How to Order Parts

When ordering parts, specify the model and serial number of the aircraft, along with the part number, name, type, and quantity required. Orders should be placed through authorized distributors.

Serial Number Information

The catalog includes serial number ranges for the PA-23 Apache models, detailing which parts apply to specific serial numbers from 23-1 to 23-2012.

Standard Paint Chart

The catalog lists exterior and interior paint colors available for the PA-23 Apache, including specific color names and the type of paint used.

Safety notes

The catalog should not be used for rigging and installation purposes.

Full document text

AIRPLANE PARTS CATALOG PA-23-150 APACHE PA-23-160 APACHE CARD 1 OF 2 PIPER AIRCRAFT CORPORATION a PART NUMBER: 752 421 INTERIM REVISION: SEPTEMBER 1998 1A1 Courtesy of Bomar Flying Service www.bomar.biz PIPER PARTS CATALOG AEROFICHE EXPLANATION AND REVISION STATUS The Parts Catalog infomtion Incorporatedin this set of Aerofiche cards has been arranged in accordance with the general specifica- tions of Aerofiche adopted by the General Aircraft Manufacturefs Association. Conversion of Aerofiche alphalnumeric code numbers: First number is the Aerofiche card identifier. Letter is the horizontal line reference per card. Second number is the vertical line reference per card. Example: 2J16 = Aerofiche card number two of given set, Grid location J16. To aid in locating the various sections and related informationdesired, the following is provided: A complete Catalog Table of Contents is given at Grid 1A8 of Aerofiche card number 1 of this set. Each additional card in this set will have a Table of Contents for all sections on that particular card. This table will start at Grid A3. REVISIONS The information compiled in this Aerofiche Parts Catalog 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. Current Revisionsto this PA-23-150 and PA-23-160 Parts Catalog issued April 2, 1973 are as follows: 752 421 (ORG730402)............................................................................Dated April 1973 752 421 (PR770506) ............................................................................Dated May 1977 752 421 (PR830211)..................................................................Dated February 1983 752 421 (lR980904) ......................................................................a t September 1998 NOTE: Refer to the last card of the Piper - Parts Price List - Aerofiche for a check list of current revision dates and card effectivities for this parts catalog. Interim Revislon: September 1998 PIPER PARTS CATALOG INTRODUCTION This illustrated P a t s Catalog is designed to provide simple but positive identification of replacement parts forthe Piper Model PA-23- 150 "Apache" and PA-23- 160 "Apache", manufactured by the Piper Aircraft Corporation of Lock Haven, Pennsylvania. NOTE: UNDER NO CIRCUMSTANCES SHALL THIS CATALOG BE USED FOR RIGGING AND INSTALLATION PURPOSES. It is suggested that this catalog be thoroughly studied to determine its arrangement prior to its utilization. 1. The catalog is divided into eleven (11) major sections described as follows: a. Section I to X inclusive contains all replacement parts for the complete airplane. Each section is subdivided and each division iccludes an illustration and a parts listing. b. Section XI is the Miscellaneous Group. This group includes a listing of the Optional Equipment Kits, Repair Kits and Special Tools. 2. The following is a brief explanation of the columns in the pans listing: a. The "FIGURE AND INDEX" column indicates the illustration figure number and its part index number. Example: (2-11, the 2 is the figure number and the 1 is the index number. The figure number appears only at the topof each parts listing page or at the beginning of each new parts listing. b. The "PART NUMBER" column contains the identifying number of the replacement part and this number must be shown on all Parts Orders. c. The "CODE" column is for the purpose of indicating special uses of the pan. An explanation of the letter code used is shown below each listing. d. The "NOMENCLATURE'' column indicates the part name. This name must be shown on all Parts Orders. e. The "NO. REQ." (Number Required) column represents the total quantity of parts used per aircraft per figure when the part is not indented and the quantity of parts used per assembly when the part is indented. ThB symbol "AR" listed in this column means "As Required". f. The "SERIAL NUMBERS AFFECTED" column indicates the part application by airplane serial numbers. Indentation Example: Indentations of listings in the "Nomenclature column" indicate "assemblies" and "components" or "parts", in order of their indentations. Figure and Index Number TI PIr t Numbar is listing is EXAMPLE Code I NOMENCLATURE DOOR ASSEMBLY - Baggage compartment FRAME ASSEMBLY - Baggage compartment door HINGE ASSEMBLY - Baggage door CUP - Baggage door spring iterpreted as follows: ' No. SERIAL NUMBERS AFFECTED If the DOOR ASSEMBLY (not indented) is ordered, it will include the three items listed under that item. If the FRAME ASSEMBLY (indented one space) is ordered, it will include the two items listed under the subassembly. If you want only a HINGE ASSEMBLY or CLIP, you order only that item. 3. The "ATTACHING PARTS" such as nuts, bolts, screws, etc., that are available as commercial hardware items, are not generally supplied by the Piper Aircraft Corporation. The catalog lists, for your convenience, those attaching parts required for main assemblies and installations. The identifying number for these parts appears after the pan name. 4. All items of Optional Equipment are contained in the parts list in their proper sequence and sections. These items were not marked optional. since they are fully identified by their descriptions. REVISED: FEBRUARY 1983 PA-23- 150 PA-23- 160 P I P E R A I R C R A F T C O R P O R A T I O N HOW TO IDENTIFY A PART I F YOU KNOW WHAT I T LOOKS LIKE AND KNOW WHERE I T IS LOCATED 1. Refer t o Figure 1 and Figure 1A t o determine the section number i n which the part is used. 2. Refer t o the Table of Contentsand locate the section. Note the figure numbers that illustrate the various subgroups of this main section. a. Select the figure title you think might contain the part you wish t o identify and turn t o the grid (page) specified.

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3. Find the part on the illustration and note the index number. NOTE: I f you don't find the part on this illustration, try another figure i n this goup. 4. Refer t o the "Figure and Index Number" in the Parts Listing for complete description of the part. HOW TO ORDER PARTS I n ordering parts for your Piper Airplanes, 0 b S e r ~the following instructions which will aid in your getting the right parts required without delay. a. Place your order with the distributor or dealer for your territory, since parts are available only through our distributor organization. b. Always specify the model and serial number of your airplane. c. Always specify part number, name, type and quantity required. d. Specify the method of shipment, freight, expms, parcel post, air express, air freight or air parcel post. Where the nature of the shipment requires it or when no instructions are given, we reserve the right to ship the most suitable way. GENERAL INFORMATION A l l orders are checked and rechecked before leaving our Shipping Department. A packing slip is enclosed with the shipment and claims for errors or shortages must be made within three days after receipt of orders. b. Returned Goods No material should be returned t o us without first securing our written permission. Material sent in without notice will be held at the owner's risk for thirty (30)days and will then be disposed of as we sea fit. Transportation charges m u d be PREPPlD on returned goods or the shipment will be refused. c. Transmrtation Liebilities The Piper Aircraft Corporation cannot be held liable for damages to parts in transit from the factory. I f a shipment is received in a damaged condition, have the delivery man or Transportation Company make a notation of the damage and file your claim with the Carrier. In case of consealed d a m e , do not attempt to remove the part from the shipping container or endeavor t o repair the damage, but call the Carrier and have his Claim Agent inspect the damage before filing your claim with the Carrier. REVISED: MAY 1977 PIPER PARTS CATALOG PA-23- 150 AND PA-23-160 SERIAL NUMBER INFORMATION The following information should be kept in mind when ordering from this Catalog: a. The serial numbers of the aircraft covered by this Parts Catalog are as follows: (1) Serial numbers of the 1954-1955 PA-23 "Apache" Models are 23-1 to 23-375 inclusive. (2) Serial numbers of the 1956 PA-23 "Apache" Models are 23-376 to 23-746 inclusive. (3) Serial numbers of the 1957 PA-23 "Apache" Models are 23-747 to 23-1067 inclusive, 23-1069 to 23-1 163 inclusive. (4) Serial numbers of the 1958 PA-23 "Apache" Models ere 23-1068, 23-1164 to 23- 1396, 23-1398 to 23- 1501 inclusive. (5) Serial numbers of the 1959 PA-23 "Apache" Models are 23-1397. 23-1502 to 23-1767, 23-1769 to 23- 1870 inclusive. (6) Serial numbers of the PA-23 Apache Model G are 23-1768, 23-1871 to 23-2012 inclusive. (7) Serial numbers of the PA-23 Apache Model H are 23-2013 and up. REVISED: FEBRUARY 1983 PA-23-150 PA- 23- 160 PIPER PARTS CATALOG STANDARD PAINT CHART EXTERIOR POLYURETHANE ENAMEL (Dupont Imron) Baja Yellow Juneau White Ocala Orange Madrid Red Bahama Blue Avocado Las Vegas Gold Dakota Black Denver Brown Matador Red Royal Blue Hickory Brown Silver Lime Green Sage Green Flrethom Buckskin Dark Blue Platinum Gray Sandalwood Tan Dark Claret Burnished Gold Light Blue Dark Saddle Dark Green Saffron Light Sandalwood Light Platlnum Catalyst (Activator) Reducer Retarder Accelerator POLYURETHANE PRIMER (Dupont Imron) Wash Primer Wash Primer Thinner Acid Thinner MFG. NO. PIPER PART NUMBER QUART GALLON INTERIOR w:SEE SERVICE SPARES LETTER 407 FOR AVAILABILITY OF COLOR PAINT FOR THERMOPLASTIC INTERIOR PANELS. Interim Revision: September 1998 P I P E R A I R C R A F T C O R P O R A T I O N WIN6 STATIONS FUSELAGE STATIONS REVISED: MAY 1977 DO NOT USE FOR WEIGHT AND BALANCE INFORMATION P IPER A IRCRAFT C O R P O R A T I O N TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER 1 Exploded View of Complete Airplane ................. .............. 1A12 1A Exploded View of Complete Airplane ................................ 1A13 SECTION I WING GROUP 2 Wing Installation ............................................ 1A14 3 Wing and Wing Tip Construction ......... .......................... 1A19 4 Aileron Assembly and Flap Assembly ................................ 1B1 5 Wing and Wing Tip Skins ....................................... 1B4 SECTION II FUSELAGE GROUP 6 Complete Fuselage ........................................... 1 B8 7 FuselageForward Section ..... .............. ................... 1B11 8 FuselageCenter Section (PA-23-150-160 S/N 23-1 to 23-1870 incl.) .............. 1B16 9 FuselageCenter Section (PA-23-150-160 S/N 23-1871 and up) ................. 1B19 10 FuselageAft Section ......................................... 1B23 11 FuselageFrame Assembly ...................................... 1C2 12 Instrument Panel Installation (PA-23-150-160 S/N 23-1 to 23-1501 incl.) ........... 1C6 13 Instrument Panel Installation (PA-23-150-160 S/N 23-1502 and up) .............. 1C10 14 Control PedestalInstallation ..................................... 1C16 15 Floorboard and Cockpit Finishing Installation (PA-23-150-160 S/N 23-1 to 23-1163 incl.) ............................................. 1C21 16 Floorboard and Cockpit Finishing Installation (PA-23-150-160 S/N 23-1164 to 23-1870 incl.) ...................................... 3...... 1D3 17 Floorboard and Cockpit Finishing Installation (PA-23-150-160 S/N 23-1871 and up) .... 1D8 18 Window Curtains Installation (PA-23-150-160 S/N 23-1 to 23-1870 incl.) ........... 1D14 19 Window Curtains Installation (PA-23-150-160 S/N 23-1871 and up) .............. 1D16 20 FuselageEnclosure Installation (PA-23-150-160 S/N 23-1 to 23-1870 incl.) .......... 1D18 21 FuselageEnclosure Installation (PA-23-150-160 S/N 23-1871 and up) . ..... ...... . 1D21 22 BaggageDoor Assembly and Cabin Door .............................. 1E1 23 Seats Installation (PA-23-150-160 S/N 23-1 to 23-1163 incl.) .................. 1E8 24 Seats Installation (PA-23-150-160 S/N 23-1164 and up) . ..................... 1Ell 25 Reclining Seats, Center Seats, Fifth seatand Headrest ...................... 1E16 26 Vacuum Pump Installation ..................................................... 1E22 27 Dual Vacuum Pump Installation .................................. . 1F1 28 MiscellaneousAir and Fluid Lines Installation ........................... 1F7 29 Heater System Installation (PA.23-150-160-S/N 23-1 to 23-375 incl.) ............. 1F11 30 Heater Assembly (PA-23-150-160S/N 23-1 to 23-170incl.) ................... 1F14 31 Heater Assembly (PA-23-150-160S/N 23-171 and up) ............... ....... 1F16 32 Heater Installation (PA-23-150-160 S/N 23-376and up) . ............ ............. 1F19 33 Ventilating System (PA-23-150-160 S/N 23-1 to 23-1870 incl.) ................. 1G1 34 Ventilating System (PA-23-150-160 S/N 23-1871 and up) . ............... ...... . 1G4 35 Oxygen System Installation ..... .... ........................................... 1G7 SECTION III CHASSIS GROUP 36 Nose Gear Installation ......................................... 1G9 36A Nose Wheel Assembly ............. ..... ............... .................. 1G14 REVISED: FEBRUARY 1983 1 AO PA-23-150 I 1A8_ PA-23-160 P I P E R A I R C R A F T C O R P O R A T I O N FIGURE NUMBER TABLE OF CONTENTS FIGURE TITLE SECTION Ill CHASSIS GROUP (ant.) GRID NUMBER Main Gear Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1G16 Gear Strut Arremblies . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . l G 2 l Brake System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H I Cleveland Brake Arrsmbly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H6 Main Wheel Auembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H8 SECTION I V T A I L SURFACES GROUP Tall Surfacer I n d l a t i o n . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H10 Fin Aormbly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H14 Stabilizer Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H16 Elevator Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H19 RuddwAorembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1H22 SECTION V POWER PLANT GROUP P o w r P l a t Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 111 Engine Bafflts Imtaliation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 116 . . . . . . . . . . . . . . . . . Exhaust Collectors (PA-23-150-180 SIN 23-1 to 23-1 151 incl.) 119 . . . . . . . . . . . . . . . . . . . . Exhaust Collecton (PA-23-160160 SIN 23-1152 and up) 1111 Namlle lmtallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1114 Propeller . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1118 SECTION VI FUEL SYSTEM GROUP Fuel System Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1120 Fuel Cell Instailstion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 1J1 . . Auxiliary Fuel Sysmm Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .' 1J4 Fuel System Contrd Box . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 158 SECT1ON VI I ELECTRICAL SYSTEM GROUP Fuselage Elactrial lnrtdlation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Wing Electrical Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Instrument Panel Electrical Installation Taxi Light lnstallatlon . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Dual Generator Innallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rotating Beacon lnmllation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . External P o w Supply . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Electric Pitot Tube lnstallation Piper Automatic Locator (ELT) Inrtelhation (Gerrett M f g . Ltd.) . . . . . . . . . . . . . . . . Piper Automatic Locator (ELT) Installation (Narco Avionics) ............................ REVISED: FEBRUARY 1983 P I . P E R A I R C R A F T C O R P O R A T I O N FIGURE NUMBER TABLE OF CONTENTS FIGURE TITLE SECTION V l l l HYDRAULIC SYSTEM GROUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Hydraulic System Installation . . . . . . . . . . . . . . . . . . . . . . . . . Landing Gear AntIRetmction Valve lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Hydraulic Pawer Pak Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Hydraulic Powerpak Components . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . E m e r ~ n c yGear Extender Installation SECTION I X CONTROL SYSTEM GROUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Engine Controls lnrtallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Elevator Controls lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Aileron Controls Inrtallatim . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Auto Control I Installetion . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AltiMatic Pilot I Installation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AutoControl ll lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . AltiMatic Pilot II lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Rudder Control lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Tail Trim Mechanism Installation Tail Trim Mechanism Installation (Used on Special English Apache Only) . . . . . . . . . . . SECTION X RADIO GROUP . . . . . . . . . . . . . . . . . . . . . . . . . . . . Leer Radio Instellation ADF-12 and ADF-14 Narco Radio Installation .Simplexer and Omnigetor . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . L T R A B Radio lnstallation . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Radio Junction Boxes . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . Redio In*ellation Drawing SECTION XI MISCELLANEOUS GROUP . . . . . . . . . . . . . . . . . . . . . Optional Equipment Kits. Repair Kits and Special Tods Deals. Stencils and Medallions . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . NUMERICAL INDEX GRID NUMBER REVISED: FEBRUARY 1983 1 All INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T C O R P O R A T I O N MISCELLANEOUS XI FUSELAGE HYDRAULIC SYSTEM Figure 1. Exploded View of Complete Airplane REVISED: MAY 1977 P I P E R A I R C R A F T C O R P O R A T I O N CONTROLS IX POWER PLANT CHASSIS 111 Figure 1A. Exploded View of Complete Airplane REVISED: MAY 1977 P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 2 . Wing lnsmllaion WING INSTALLATION SECTION I Wing Group When ordering, always specify Port Number, Description and Serial Number of Aircraft Figure a n d Index Number 2- -1 -2 -3 -4 - 5 - 6 -7 - 8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 -26 -27 -28 -29 -30 -31 -32 -33 ISSUED: APRIL 1973 Part Number 17901 18268 17422-01 17422-00 17422-45 17422-44 17422-61 17422-62 17477-00 17477-02 17476-00 17476-02 400156 406 683 401 270 404887 17681-00 19303-00 19459-02 19459-03 400 440 401 269 407 564 404 887 17475-02 17475-04 17475-03 17475-05 401 393 401 394 401394 401 395 407 567 404 890 17694-04 17694-02 17694-03 401 332 407 565 406 682 17480-00 401363 401 364 401 364 407566 406 683 18380-02 18380-03 18380-04 SERIAL NUMBERS AFFECTED 23-1 to 23-1 151 inclusive 23-1 to 23-1151 inclusive 23-1152andup 23-1152 and up 23- 1152 and up 23-1152andup 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23- 1152 to 23-1329 inclusive 23- 1330 and up 23- 1330 and up 23- 1 to 23-1151 inclusive 23-1152andup 23-1 to 23-1151 inclusive 23-1152andup 23-1 to 23-1151 inclusive 23- 1152 and up 23-1 to 23-1151 inclusive 23-1152 and up 23-1 to 23-1151 inclusive 23-1152 and up 23-1 to 23-1151 inclusive 23-1152 and up z? XI 0" 1 1 1 1 1 1 1 1 1 1 8 8 4 4 1 1 1 1 6 6 6 6 1 1 1 1 16 16 16 16 32 32 2 1 1 2 2 2 4 2 2 2 4 4 A R A R A R IZ n % m A A B B NOMENCLATURE DRAWING - Wing Installation DRAWING - Wing Fairing ~nstallation' PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing STRAP - Spar attachment lower rear STRAP - Spar attachment lower front STRAP - Front spar attachment upper r e a r STRAP - Front spar attachment upper front BOLT - (AN5-11) NUT - Elastic stop (#42Eo54) BOLT - (AN3-11A) NUT - Elastic stop (MS20365-1032C) PLATE - Front spar attachment, r e a r PLATE - Front spar attachment, rear PLATE - Front spar attachment, rear (. 187) PLATE - Front spar attachment, r e a r (. 125) BOLT - (AN3-6A) BOLT - (AN3-1OA) WASHER - (AN960-10) NUT - Elastic stop (MS20365- 1032C) PLATE - Front spar attachment, bottom PLATE - Front spar attachment, bottom PLATE - Front spar attachment, top PLATE - Front spar attachment, top BOLT - (AN6-1U) BOLT - (AN- 13A) BOLT - (AN6-13A) BOLT - (AN6-14A) WASHER - (AN960-616) NUT - Elastic stop (MS20365-624C) BLOCK - Front spar spacer, rear, top BLOCK - Front spar spacer, front left, top BLOCK - Front spar spacer, front right, top BOLT - (AN4-34A) WASHER - (AN960-416) NUT - Elastic stop (142E048) BLOCK - Front spar side attachment spacer BOLT - (AN5-24A) BOLT - (AN5-25A) BOLT - (AN5-25A) WASHER - (AN960-516) NUT - Elastic stop (#42E054) SHIM - ( .020) SHIM - ( ,032) SHIM - ( .064) A - Used when 150 H.P. engines a r e installed. B - Used when 160 H.P. engines a r e installed. SECTION I Wing Group WING INSTALLATION Figure I I NOMENCLATURE Number 2-34 -35 -36 -37 -38 -39 -40 -41 -42 -43 -44 -45 -46 -47 -48 -49 -50 -51 -52 -53 -54 -55 -56 -57 -58 -59 -60 -61 -62 -63 -64 -65 -66 -67 BOLT - Rear spar attachment (AN176-10A) WASHER - Rear s p a r attachment (AN960-616) NUT - Elastic stop (MS20365-624C) FAIRING ASSEMBLY - Right wing root, upper FAIRING ASSEMBLY - Left wing root, upper EXTRUSION - Rubber FAIRING ASSEMBLY - Right wing root, front FAIRING ASSEMBLY - Left wing root, front FAIRING ASSEMBLY - Right wing root, front FAIRING ASSEMBLY - Left wing root, front EXTRUSION - Rubber FAIRING ASSEMBLY - Right wing root, lower FAIRING ASSEMBLY - Left wing root, lower EXTRUSION - Rubber PLATE - Wing, front spar bolt cover PLATE - Right wing root, r e a r fairing PLATE - Left wing root, r e a r fairing FAIRING ASSEMBLY - Right wing root, r e a r FAIRING ASSEMBLY - Left wing root, r e a r RING - T i e down SCREW - (A N509- 10R- 15) AILERON ASSEMBLY - Right wing AILERON ASSEMBLY - Left wing BALANCE ASSEMBLY - Right aileron BALANCE ASSEMBLY - Left aileron HINGE - Right aileron, center HINGE - Left aileron, center HINGE - Right aileron, inboard HINGE - Left aileron, inboard TAB - Aileron trim SHIM - Aileron hinge BUSHING - Aileron center hinge BOLT - (AN4- IOA) BOLT - (AM-13A) NUT - Elastic stop (#42E0483 FLAP ASSEMBLY - Right wing FLAP ASSEMBLY - Left wing HINGE - Right flap, outboard HINGE - Left flap, outboard HINGE - Right flap, center HINGE - Left flap. center HINGE - Right flap, inboard HINGE - Left flap, inboard STOP - Wing flap BUSHING - Flap outboard hinge WASHER - Flap inboard and center hinge BOLT - (AN4-13A) 1 WASHER - (AN960-416) NUT - Elastic stop (#42E048) 402 350 407 567 404 890 18166-01 18166-00 19795-00 18164-01 18164-00 19360-01 19360-00 19795-00 18165-01 18165-00 19795-00 18176-00 18129-00 18128-00 18131-00 18130-00 18457-00 410 044 17100-01 17100-00 17126-09 17126-08 17097-01 17097-00 17095-01 17095-00 18379-00 17202-00 80012-94 401310 400 008 406 682 17104-01 17104-40 17103-01 17103-00 17102-01 17102-00 17101-01 17101-00 17120-00 14175-46 80122-68 400 008 407 565 406 682 ISSUED: APRIL 1973 When ordering, olwoys specify Part Number, Description and Serial Number of Aircraft WING INSTA LLATION SECTION I Wing Group When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23-1164andup 23-1164 and up Z 0 cprn P 1 1 1 1 4 5 8 2 2 2 2 1 1 Figure and Index Number 2-68 -69 -70 -71 -72 -73 -74 -75 Part Number 17531-00 17531-01 17531-40 17531-41 81172-70 415 449 17125-00 401 365 406 683 17529-04 19361-01 19361-00 P m B B C C A A NOMENCLATURE TIP ASSEMBLY - Left wing TIP ASSEMBLY - Right wing TIP ASSEMBLY - Left wing TIP ASSEMBLY - Right wing LUG - Wing tip attachmg SCREW - T r u s s head machine (#8-32 x 1/2 L) BLOCK - Aileron balance BOLT - (AM-26A) NUT - Elastic stop (#423054) PIN - Wing tip hinge FAIRING ASSEMBLY - Right FAIRING ASSEMBLY - Left A - Used on 23- 1 to 23- 1163 inclusive when Kit 754 175 is installed. B - If Kit 754 493 i s used, o r d e r part number 17531-40 left o r 17531-41 n g h t . C - Used only if Kit 754 493 has been installed. INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 3. Wing and Wing Tip Construction WlNG AND WlNG TIP CONSTRUCTION SECTION I Wing Group I I I PIPER PARTS CATALOG Flgure 1 I I and Index I Number Number II NOMENCLATURE DRAWING - Wing Panel DRAWING - Wing Tip BRACKET - Aileron hinge BEARING BRACKET - Aileron and flap hinge BEARING BRACKET - Flap hlnge, center BEARING BRACKET - Flap hinge inboard, right BRACKET - Flap hinge inboard, left BEARING HINGE - Wing tip HINGE -Wing tip attachment PIN -Wing tip hinge RIB ASSEMBLY - Wing trailing edge, right RIB ASSEMBLY - Wing trailing edge, left STRlP ASSEMBLY - Wing tip attachment tip, rear STRIP ASSEMBLY - Wing tip attachment top, center STRlP ASSEMBLY -Wing tip attachment, front STRlP ASSEMBLY - Wing tip attachment bottom center, right STRlP ASSEMBLY - Wing tip attachment bottom center, left RIB - Wing tip front, right RIB - Wing tip front, left RIB - Wing tip rear, right RIB - Wing tip rear, left SPAR - Wing tip front, right SPAR - Wing tlp front, left RIB -Wing tip center, right RIB - Wing tip center, left SPAR - Wing tip rear, right SPAR - Wing tip rear, left BULKHEAD - Rear spar, right. Sta. 146 and 191 BULKHEAD - Rear spar, left, Sta. 146 and 191 BULKHEAD - Rear spar, right, Sta. 157,168 and 180 BULKHEAD - Rear spar, left, Sta. 157,168 and 180 BULKHEAD - Rear spar, right, Sta. 102,118 and 136 BULKHEAD - Rear spar, left, Sta. 102,118 and 136 BULKHEAD ASSEMBLY - Rear spar, right, Sta. 127 BULKHEAD ASSEMBLY - Rear spar, left, Sta. 127 BULKHEAD - Rear spar, right, Sta. 110 BULKHEAD - Rear spar, left, Sta. 110 BULKHEAD - Rear spar, right, Sta. 95 BULKHEAD - Rear spar, left, Sta. 95 BULKHEAD - Rear spar, right. Sta. 87, outboard of torque rib BULKHEAD - Rear spar, left, Sta. 87, outboard of toque rib BULKHEAD - Rear spar, right, Sta. 56, outboard of torque rib BULKHEAD - Rear spar, left, Sta. 56, outboard of torque rib When ordering, always specify Part Number, Description, and Serial Number of Aircraft No. Req. 2 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 3 3 3 3 1 1 1 1 1 1 2 2 2 2 Interim Revision: September 1998 1A20 SERIAL NUMBERS AFFECTED 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive SECTION I Wing Group WING AND WING TIP CONSTRUCTION When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23-1152 and up 23-1152 and up 2 3 - l a n d u p 2 3 - l a n d u p 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up 23-1 to 23-1151 inclusive 23-1 to 23- 1151 inclusive 23- 1152 and up 23-1152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23- 1152 and up 23- 1152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23- 1152 and up 23- 1152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152andup 23-1152 and up 23- 1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up 23-1 to 23-1151 inclusive 23- 1 to 23- 1151 inclusive 23- 1152 and up 23- 1152 and up 23-1 to 23- 1151 inclusive 23-1 to 23-1151 inclusive 23- 1152 and up 23-1152 and up Z 0 mP 9 2 2 1 1 1 1 1 1 1 1 1 1 2 2 2 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 Figure and index Number 3-28 -29 -30 -31 -32 -33 -34 -35 -36 -37 -38 -39 -40 -41 -42 -43 -43a -44 -45 -46 -47 Part Number 19283-10 19283-07 17329-30 17329-02 17329-30 17329-02 19283-05 19283-06 17329-20 17329- 11 19283- 13 19283-14 17329-22 17329-10 19283-03 19283-02 17329-15 17329-14 17329-31 17329-32 751 228 149 063 18369-01 18369-00 18370-07 18370-06 18370-09 18370-08 18370-05 18370-04 19664-06 19664-02 19664-04 19664-08 19664-07 19664-03 19664-09 19664-05 18368-01 18368-00 19309-01 19309-00 17133-04 17133-05 19282-04 19282-05 17133-03 17 133-02 19282-03 19282-02 17130-03 17130-02 19285-01 19285-00 6 $ NOMENCLATURE BULKHEAD - Rear spar, right, Sta . 56, outboard of torque rlb BULKHEAD - Rear spar, left, Sta. 56, outboard of torque rib BULKHEAD - Rear spar, right, Sta. 80 BULKHEAD - Rear spar. left, Sta. 80 BULKHEAD - Rear spar, right, Sta. 49 BULKHEAD - Rear spar, left, Sta. 49 BULKHEAD - Rear spar, right, Sta . 49 BULKHEAD - Rear spar, left. Sta . 49 BULKHEAD - Rear spar, right, torque rib BULKHEAD - Rear spar. left, torquerib BULKHEAD - Rear spar, right, torque rib BULKHEAD - Rear spar, left, torque rib BULKHEAD - Rear spar, right, Sta . 34 and 42 BULKHEAD - Rear spar, left. Sta. 34 and 42 BULKHEAD - Rear spar, right, Sta. 34 and 42 BULKHEAD - Rear spar, left, Sta. 34 and 42 BULKHEAD - Rear spar, right, Sta. 27 BULKHEAD - Rear spar, left, Sta. 27 BULKHEAD - Rear spar. right. Sta. 27 BULKHEAD - Rear spar, left, Sta. 27 ANGLE - Stringer section (6' section) ANGLE - Extrusion (6' section) RIB ASSEMBLY - Wing, right, Sta. 191 RIB ASSEMBLY - Wing. left. Sta. 191 RIB ASSEMBLY - Wing. r@t, Sta. 146 RIB ASSEMBLY - Wing, left, Sta. 146 RIB ASSEMBLY - Wing, right. Sta. 168 RIB ASSEMBLY - Wing. left. Sta. 168 RIB ASSEMBLY - Wing, right, Sta . 127 RIB ASSEMBLY - Wing, left, Sta. 127 RIB ASSEMBLY - Wing. Sta . 110. top. right RIB ASSEMBLY - Wing, Sta. 110. top, left RIB ASSEMBLY - Wing. Sta. 95, top. right RIB ASSEMBLY - Wing, Sta. 95, top, left RIB ASSEMBLY - Wing, Sta. 10, bottom, right RIB ASSEMBLY - Wing. Sta. 10, bottom, left RIB ASSEMBLY - Wing, Sta. 95, bottom, right RIB ASSEMBLY - Wing. Sta . 95. bottom. left RIB ASSEMBLY - Wing, right, Sta. 80 RIB ASSEMBLY - Wing, left, Sta . 80 RIB ASSEMBLY - Wing, right, Sta . 80 RIB ASSEMBLY - Wing, left, Sta . 80 RIB ASSEMBLY - Wing, outboard torque, right RIB ASSEMBLY - Wing, outboard torque, left RIB ASSEMBLY - Wing, outboard torque, right RIB ASSEMBLY - Wing, outboard torque, left RIB ASSEMBLY - Wing, inboard torque, right RIB ASSEMBLY - Wing, inboard torque, left RIB ASSEMBLY - Wing, inboard torque, right RIB ASSEMBLY - Wing, inboard torque, left RIB ASSEMBLY - Wing, right, Sta. 56 RIB ASSEMBLY - Wing, left, Sta. 56 RIB ASSEMBLY - Wing, right, Sta. 56 RIB ASSEMBLY - Wing, left, Sta. 56 WING AND WING TIP CONSTRUCTION SECTION I Wing Group Figure and lndex Numbel -3 -48 Part Number NOMENCLATURE RIB ASSEMBLY - Wing, right, Sta . 42 and 49 RIB ASSEMBLY - Wing, left, Sta. 42 and 49 RIB ASSEMBLY - Wing, right, Sta. 42 and 49 RIB ASSEMBLY - Wing, left, Sta. 42 and 49 RIB ASSEMBLY - Wing, right, Sta. 34 RIB ASSEMBLY - Wing, left, Sta. 34 RIB ASSEMBLY - Wing, right. Sta. 34 RIB ASSEMBLY - Wing, left, Sta. 34 RIB ASSEMBLY - Wing butt, right RIB ASSEMBLY - Wing butt, left RIB ASSEMBLY - Wing butt, right RIB ASSEMBLY - Wing butt, left SPAR ASSEMBLY - Wing rear, right SPAR ASSEMBLY - Wing r e a r , left SPAR ASSEMBLY - Wing r e a r , right SPAR ASSEMBLY - Wing r e a r , left PLATE - Rear spar, left front, right r e a r PLATE - Rear spar, left rear, right front CHANNEL - Rear s p a r tip, left CHANNEL - Rear s p a r tip, right BUSHING SPAR ASSEMBLY - Wing front, right SPAR ASSEMBLY - Wing from, left SPAR ASSEMBLY - Wing front, right SPAR ASSEMBLY - Wing front, left PLATE - Front s p a r end CHANNEL - Outboard, LH CHANNEL - Outboard, RH BRACKET - Hydraulic llne support, right BRACKET - Hydraulic line support, left BRACKET - Fuel valve shutoff, rigfit BRACKET - Fuel valve shutoff, left BRACKET - Fuel valve shutoff, right BRACKET - Fuel valve shutoff, left RIB ASSEMBLY - Wing nose, right, Sta. 180 and 191 RIB ASSEMBLY - Wing nose, left. Sta. 180 and 191 RIB - Wing nose, right, Sta. 191 RIB - Wing nose, left, Sta. 191 RIB - Wing nose, right, Sta. 180 RIB - Wing nose, left, Sta. 180 RIB ASSEMBLY - Wing nose, right, Sta. 157 and 168 RIB - Wing nose, right, Sta. 157 and 168 RIB ASSEMBLY - Wing nose, left, Sta. 157 and 168 RIB - Wing nose, left, Sta. 157 and 168 RIB ASSEMBLY - Wing nose, right. Sta. 1% RIB ASSEMBLY - Wing nose, left, Sta. 146 RIB ASSEMBLY - Wing nose, right, Sta. 136 RIB - Wing nose, right, Sta. 136 RIB ASSEMBLY - Wing nose, left, Sta. 136 RIB - Wing nose, left, Sta. 136 RIB ASSEMBLY - Wing nose, right, Sta. 127 RIB ASSEMBLY - Wing nose, left. Sta. 127 A - Must use shim 18942-02 and angle 19469-00 for installation. B - Must use shim 19302-00 for installation. SERIAL NUMBERS 1 m 1 AFFECTED I 23-1 to 23- 1151 inclusive 23-1 to 23-1151 inclusive 23-1 152 and up 23-1 152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1 152 and up 23 - 1 to 23 - 1151 inclusive 23-1 to 23-1151 inclusive 23 - 1152 and up 23 -1 152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up 23-1 to 23-115 1 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up 23-1 to 23-1870 inclusive 23-1 to 23- 1870 inclusive 23-1871 and up 23-1871 and up 23-1 to 23-2000 inclusive 23-1 to 23-2000 inclusive 23-2001 and up 23-2001 and up 23-2001 and up 23 -2001 and up 23-1 to 23 -2000 inclusive 23-2001 and up 23-1 to 23-2000 inclusive 23-2001 and up 23-1 to 23 -2000 inclusive 23 -2001 and up 23-1 to 23-2000 inclusive 23-2001 and up When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SECTION I Wing Group WING AND WING TIP COWTRUCTION When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 Z ? 8" 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 2 2 2 2 2 2 2 1 1 1 1 1 1 1 1 1 1 NOMENCLATURE RIB ASSEMBLY - Wing nose, right. Sta. 118 RIB ASSEMBLY - Wing nose, left. Sta. 118 RIB ASSEMBLY - Wing nose. right, Sta. 110 RIB ASSEMBLY - Wing nose. left, Sta. 110 RIB ASSEMBLY - Wing nose, right, Sta. 102 RIB ASSEMBLY - Wing nose, left, Sta. 102 RIB ASSEMBLY - Wing nose, right. Sta . 95 RIB ASSEMBLY - Wing nose. left, Sta . 95 RIB ASSEMBLY - Wing nose. right. Sta. 87 RIB ASSEMBLY - Wing nose, left, Sta . 87 RIB ASSEMBLY - Wing nose, right, Sta. 80 RIB ASSEMBLY - Wing nose. left. Sta . 80 RIB ASSEMBLY - Wing nose. right. Sta. 56 RIB ASSEMBLY - Wing nose. left, Sta. 56 RIB ASSEMBLY - Wing nose. right. Sta . 49 RIB ASSEMBLY - Wing nose, left, Sta. 49 RLB ASSEMBLY - Wing nose, right, Sta . ,42 RIB ASSEMBLY - Wing nose. left. Sta. 42 RIB ASSEMBLY - Wing nose, right, Sta. 34 RIB ASSEMBLY - Wing nose. left, Sta. 34 RIB ASSEMBLY - Wing nose. left. Sta . 27 RIB ASSEMBLY - Wing nose, right, Sta. 27 RIB ASSEMBLY - Wing nose, right, Sta. 27 RIB ASSEMBLY - Wing nose, left, Sta. 27 BULKHEAD - Nose rib, right BULKHEAD - Nose rib, left BULKHEAD - Nose rib, outboard, right BULKHEAD - Nose rib, outboard, left PLATE - Wing r i b cover BRACKET ASSEMBLY - Aileron bellcrank, right BRACKET ASSEMBLY - Aileron bellcrank, right BRACKET ASSEMBLY - Aileron bellcrank, left BRACKET ASSEMBLY - Aileron bellcrank, left BRACKET - Aileron cable pulley CHANNEL - Torque r i b reinforcement inboard, right CHANNEL - Torque r i b reinforcement inboard, left CHANNEL - Torque rib reinforcement outboard, right CHANNEL - Torque rib reinforcement outboard, left CONDUIT - Wire harness (1") CONDUIT - Wire harness (1-1/4") BOLT - "U" PLATE - Wheel well attachment, right hand PLATE - Wheel well attachment, left hand PLATE - Cover SHIM CHANNEL - Access hole reinforcement, right CHANNEL - Access hole reinforcement, right CHANNEL - Access hole reinforcement, left CHANNEL - Access hole reinforcement, left FITTING - Landing gear reinforcement, right FITTING - Landing gear reinforcement, right FITTING - Landing gear reinforcement, left FI'ITING - Landing gear reinforcement, left PLATE - Filler, right PLATE - Filler, left Figure and Index Number 3-63 -64 -65 -66 -67 -68 -69 -70 -71 -72 -73 -74 -75 -76 -77 -78 -79 -80 -81 -82 -83 -84 -85 -86 -87 -88 SERIAL NUMBERS AFFECTED 23- 1 to 23-1151 inclusive 23- 1 to 23- 1151.inclusive 23-1152 and up 23- 1152 and up 23-1 to 23-2000 inclusive 23- 200 1 and up 23- 1 to 23-2000 inclusive 23-2001 and up 23- 1 to 23- 109 inclusive 23-1 to 23-109 inclusive 23- 110 and up 23- 1 to 23-109 inslusive 23-110andup 23-1 to 23-109 inclusive 23- 110 and up 23- 1 to 23- 109 inclusive 23- 110 and up 23-1 to 23-109 inclusive Port Number 17186-01 17186-00 17184-03 17184-02 17187-07 17187-06 17188-07 17188-08 17189-09 17189-08 17192-01 17192-00 17190-01 17190-00 17187-03 17187-02 17188-03 17188-02 17189-03 17189-02 19450-02 19450-03 17191-07 17191-06 17328-01 17328-00 17382-01 17382-00 17193-00 17428-01 17428-03 17428-00 17428-02 17459-00 17143-03 17143-02 17143-04 17143-05 17752-00 17752-02 18329-02 18358-01 18358-00 SK574-2 SK574-3 18573-01 SK574-5 18573-00 SK574-4 18572-01 SK574-7 18572-00 SK574-6 18571-01 18571-00 6 % WING AND WING TIP CONSTRUCTION SECTION I Wing Group ISSUED: APRIL 1973 When ordering, always specify Part Number, Description and Serial Number of Aircraft P I P E R A I R C R A F T C O R P O R A T I O N - a R E V I S E D : F E B R U A R Y 1983 Figure 4. Flap Assembly and Aileron Assembly FLAP ASSEMBLY AND AILERON ASSEMBLY SECTION I Wing Group Figure and Index Number 4- 1 - 2 -3 -4 - 5 -5a -5b -6 -7 -8 - 9 -10 -1 1 -1 2 -12a -13 -14 -15 -16 -17 -18 -19 - 20 -21 -22 -22a -23 -24 -25 -26 -27 -28 -29 -30 -31 l-7- PIPER PARTS CATALOG Part Number 17104-01 17 104-40 17104-02 17104-37 17104-22 17104-23 17104-26 17104-27 17104-47 17 104-46 17104-24 17104-25 17104-49 17104-52 17104-48 17104-05 17104-04 17104-07 17104-06 17104-05 17104-04 17104-04 17104-05 17104-42 17104-43 31002-00 31002-01 17270-00 17104-10 17104-09 17104-12 17104-11 18387-00 17104-10 17104-09 16234-00 17104-41 17104-08 17101-00 17101-01 17120-00 17104-16 33555-00 33555-01 17102-00 17102-01 17 103-00 17103-01 17100-00 17100-01 17100-18 17100-12 17100-11 17100-16 17100-17 17100-17 17100-16 18379-00 17100-08 When ordering, always specify Part Number, Description and Serial Number of Aircraft Code REVISED: FEBRUARY 1983 1B2 NOMENCLATURE FLAP ASSEMBLY - Right wing FLAP ASSEMBLY - Left wing SPAR ASSEMBLY - Left flap SPAR ASSEMBLY - Right flap SKlN - Leading edge left flap, outboard 'SKIN - Leading edge right flap, outboard SKlN - Leading edge left flap, inboard SKlN - Leading edge right flap, inboard SKlN ASSEMBLY - Left flap, top * SKlN ASSEMBLY - Right flap, top * STRIP - Beaded 'PLATE - Reinforcement, right flap, top skin SKlN ASSEMBLY - Left flap, bottom SKlN ASSEMBLY - Right flap. bottom, outboard * SKlN ASSEMBLY - Right flap, bottom, inboard BULKHEAD - Left flap BULKHEAD - Right flap ' BULKHEAD - Left flap BULKHEAD - Right flap BULKHEAD - Left flap BULKHEAD - Right flap BULKHEAD - Left flap BULKHEAD - Right flap RIB - Left flap RIB - Right flap REINFORCEMENT - Flap outboard rib, left + REINFORCEMENT - Flap outboard rib, right ' PLATE RIB - Left flap RIB - Right flap RIB - Left flap RIB - Right flap + BRACKET - Right flap RIB - Left flap RIB - Right flap CHANNEL - Left flap RIB - Left flap RIB - Right flap 'HINGE - Flap inboard, left + HINGE - Flap inboard, right STOP 'CHANNEL - Flap hinge reinforcement ' CHANNEL - Flap hinge reinforcement, left CHANNEL - Flap hinge reinforcement, right HINGE - Flap center, left HINGE - Flap center, right HINGE - Flap outboard, left HINGE - Flap outboard, right AILERON ASSEMBLY - Left wing AILERON ASSEMBLY - Right wing SPAR ASSEMBLY - Aileron * SKIN - Leading edge, left SKlN - Leading edge, right ' SKIN ASSEMBLY - Left, top SKIN ASSEMBLY - Right, top SKIN ASSEMBLY - Left, bottom + SKlN ASSEMBLY - Right. bottom TAB - Aileron trim ' RIB - Aileron, outboard FLAP ASSEMBLY AND AILERON ASSEMBLY SECTION I Wing Group When ordering, always specify Port Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 Figure and Index Number 4-32 -33 -34 -35 -36 -37 -38 -39 -40 -41 -42 P a r t Number 17100-20 17100-19 17100-04 17100-05 17100-05 17 100-04 17100-14 17100-21 17100-13 17095-00 17095-01 17097-00 17097-01 17126-08 17126-09 17202-00 17270-00 8 m z? ?0 1 1 9 9 1 1 2 1 1 1 1 1 1 1 1 1 1 NOMENCLATURE RIB ASSEMBLY - Leading edge, outboard. left RIB ASSEMBLY - Leading edge, outboard, right RIB - Leading edge RLB - Leading edge RIB - Leading edge, left RIB - Leading edge, right RIB - Aileron center PLATE ASSEMBLY - Aileron hinge, reinforcement, center RIB - Aileron inboard HINGE - Aileron inboard, left HINGE - Aileron inboard, right HINGE - Aileron center, left HINGE - Aileron center, right BALANCE ASSEMBLY - Aileron, left BALANCE ASSEMBLY - Aileron, right SHIM PLATE SERIAL NUMBERS AFFECTED P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 5. Wing and Wing T p Skin SECTION I Wing Group WING AND WING TIP SKIN When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23-1 to 23-1151 inclusive 23-1152 and up 23-1 to 23-2000 inclusive 23-2001 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up 23-1 to 23-1151 inclusive 23-1152 and up 23-1 to 23-1151 inclusive 23-1 to 23-1151 inclusive 23-1152 and up 23-1152 and up Figure and Index Number 5- -1 -2 -3 -4 -5 -6 -7 -7a -8 -8a -9 -10 1 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 Part Number 17422 17901 17422-08 17422-06 17422-04 17422-48 17337-00 17336-02 17335-02 17422-11 17422-34 17315-00 19973-00 17422-13 17422-12 17317-00 17422-15 17422-14 17422-03 17422-02 17422-47 17422-46 17317-00 17316-00 17318-03 17318-03 17383-01 17383-00 17361-03 17361-02 17361-05 17361-04 17362-01 17362-00 17362-03 17362-02 17422-09 17422-38 17422-07 17422-05 17336-03 17335-03 17365-00 n g ca A B C C NOMENCLATURE DRAWING - Wing Panel DRAWING - Wing Installation SKIN - Wing top, outboard SKIN - Wing top, center SKIN - Wing top, inboard SKIN - Wing top, inboard PLATE ASSEMBLY - Fuel cell access hole cover GUSSET - Wing top, r e a r GUSSET - Wing top, front SKIN - Right wing leading edge, outboard SKIN - Left wing leading edge, outboard PLATE - Aileron bellcrank access hole reinforcement PLATE - Aileron bellcrank access hole reinforcement SKIN - Right wing leading edge, center SKIN - Left wing leading edge, center PLATE - Access hole reinforcement SKIN - Right wing leading edge, inboard center SKIN - Left wing leading edge, inboard center SKIN - Right wing leading edge, inboard SKIN - Left wing leading edge, inboard SKIN - Right wing leading edge, inboard SKIN - Left wing leading edge, inboard PLATE - Access hole reinforcement PLATE - Aileron bellcrank access hole cover PLATE - Access hole cover PLATE - Access hole cover FAIRING - False spar, right FAIRING - False spar, left SPAR - False, right wing outboard SPAR - False, left wing outboard SPAR - False, right wing center SPAR - False, Ieft wing center SPAR - False, right wing inboard SPAR - False, left wing inboard SPAR - False, right wing inboard SPAR - False, left wing inboard SKIN - Wing, bottom, outboard, right SKIN - Wing, bottom, outboard, left SKIN - Wing, bottom, center SKIN - Wing, bottom, inboard GUSSET - Wing bottom, r e a r GUSSET - Wing bottom, front PAD - Jack A - Use 18624-07 if auxiliary fuel cells a r e installed. B - Use 18624-12 if auxiliary fuel cells a r e installed. C - Use 18624-08 if auxiliary fuel cells a r e rnstalled. z P ?P 2 2 1 1 2 2 4 1 1 2 2 1 1 2 1 1 1 1 1 1 2 2 2 4 1 1 1 1 1 1 1 1 1 1 1 1 2 2 2 4 2 WING AND WING TIP SKIN Figure and lndex Numbel SECTION I Wing Group - -- SKIN ASSEMBLY - Left wing tip, lower SKlN ASSEMBLY - Right wing tip, lower SKIN ASSEMBLY - Left wing tip, lower SKIN ASSEMBLY - Right wing tip. lower SKIN - Right wing tip, upper SKIN - Left wing tip, upper COVER ASSEMBLY - Wing tip access opening ANGLE - Nacelle attaching, right wing, outboard, top ANGLE - Nacelle attaching, left wing, outboard, top ANGLE - Nacelle attaching, right wing, inboard, top ANGLE - Nacelle attaching, left wing, inboard, top ANGLE - Nacelle attachmg, right wing, outboard, bottom, r e a r ANGLE - Nacelle attaching, left wing, outboard, bottom, rear ANCLE - Nacelle attaching, right wing, outboard. bottom, front ANGLE - Nacelle attaching, left wing, outboard, bottom, front ANGLE - Nacelle attaching, right wing, inboard, bottom A m L E - Nacelle attaching, left wing, b a r d , bottom A NGLE - Nacelle attachurg, left wing, outboard, nose ANGLE - Nacelle attaching, right wing, outboard, nose ANGLE - Nacelle attaching, left wing, inboard, nose ANGLE - Nacelle attaching, right wing, inboard, nose NUT - Shell (#3600-62BC) CLIP ASSEMBLY - Engine nacelle attachment CHANNEL SECTION - Wing tip skin reinforcement (6' section) REINFORCEMENT - Aileron balance weight opening, LH REINFORCEMENT - Aileron balance weight opening, RH SEAL - Aileron balance weight opening , SUPPORT - Aileron balance weight opening seal A - If Kit 754 493 has been installed, order wing s u n 17531-36left o r 17531-37right. B - Used only if Kit 754 493 has been installed. When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 1 87 INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T & - C O R P O R A T I O N - REVISED: MAY 1977 Figure 6. Complete Fuselage COMPLETE FUSELAGE SECTION I1 Fuselage Group When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: FEBRUARY 1983 SERIAL NUMBERS. AFFECTED 23- 1 to 23-1870 inclusive 23-1871 and up 23- 1 to 23- 1870 inclusive 23- 1871 and up 23- 1 to 23- 1870 inclusive 23-1 to 23-1163 inclusive 23-11&andup Z P A 8 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 2 1 1 1 1 2 20 1 1 1 1 1 3 3 1 Figure and Index Number 6 - - 1 -2 -3 -4 -5 -5a -6 -7 - 8 -9 -10 -11 -12 -13 -14 -15 - 16 -17 -18 -19 -20 -21 -22 -23 -24 -25 Part Number 18228 19718 19757 16921-00 16921-01 16922-00 16922-01 19758-00 19759-00 81342-72 18514-00 17413-03 453644 99479-02 17494-00 19326-00 18230-00 18231-00 17387-00 189625 19734-00 400 009 407 565 406 682 454 879 17667-00 17885-00 17885-08 17885-10 17885-09 494 057 487 579 17919-00 B m A A A A A A V NOMENCLATURE DRAWING - Complete Fuselage Assembly DRAWING - Complete Fuselage Assembly DRAWING - Plates Installation - Ice Shield PLATE - Ice shield, lower, left PLATE - Ice shield, lower, right PLATE - Ice shield. upper, left PLATE - Ice shield, upper, right PLATE - Ice shield, right, center PLATE - Ice shield, left, center WASHER - Cabin assist handle HANDLE - Cabin assist HANDLE - Cabin assist BUMPER - Rubber GAUGE - Air temperature FAIRING - Fuselage nose FAIRING - Fuselage nose SUPPORT ASSEMBLY - Fuselage sldn BRACKET ASSEMBLY - Fuselage skin support PAD ASSEMBLY - Fuselage skin support GROMMET - Engine control support STEP ASSEMBLY - Fuselage BOLT - (AM-14A) WASHER - (A N960-416) NUT - Elastic stop (#42E048) LETTERS - "PIPER" CLIP - Tubular, t i n n e w a n (C2205-032-24) SKID ASSEMBLY - Fuselage tail CONE ASSEMBLY - Fuselage tail FAIRING - Elevator torque tube, top FAIRING ASSEMBLY - Elevator torque tube, bottom CONE - Fuselage tail WASHER - Split (82600-SW2) STUD - (2600-5) CLIP - Fuselage tail fairing A - Optional equipment. V - These parts must be ordered from Service Spares Department. Piper Aircraft Corporation. Vero Beach. Florida. INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 7. Fuselaw Forward Section SECTION U Fuselage Group FUSELAGE FORWARD SECTION Figure and lndex Number 7- - 1 -2 - 3 -4 - 5 - 6 -7 - 8 -9 - 10 - 11 - 12 - 13 - 14 - 15 - 16 - 17 - 18 - 19 - 20 -21 -22 -23 -24 -25 Part Number 17474 17360 19447 19750 16828 17262-00 17216-00 17244-00 17214-00 17247-00 17245-00 17248-00 17252-00 751 228 80122-69 80122-70 80122-71 17438-00 17226-00 17386-00 17387-00 18280-00 17386-00 17387-00 17425-00 19504-00 16866-00 30187-00 16885-00 19860-00 19860-03 17360-04 17360-21 19447-12 19553-04 17360-11 17360-22 19553-02 17360-10 17350-08 19515-00 17357-00 19535-00 19535-01 NOMENCLATURE DRAWING - Fuselage Assembly DRAWING - Fuselage Forward Section DRAWING - Fuselage Forward Section DRAWING - Fuselage Assembly DRAWING - Shelves Installation ANGLE - Baggage compartment door frame, upper rear corner A N L E - Baggage compartment door frame, r e a r ANGLE - Baggage compartment door frame, lower rear corner FAIRING - Baggage compartment door frame, lower ANGLE - Baggage compartment door frame, lower front corner ANGLE - Baggage compartment door frame, front ANGLE - Baggage compartment door frame, upper front corner ANGLE - Baggage compartment door frame, top ANGLE - Stringer section (6' section) WASHER - Shim (.032) WASHER - Shim (.0&) WASHER - Shim (.125) BRACE - Fuselage skin BRACKET ASSEMBLY - Elevator control tube SUPPORT - Fuselage skin PAD ASSEMBLY - Fuselage skin support BRACKET ASSEMBLY - Fuselage skin support SUPPORT - Fuselage skin PAD ASSEMBLY - Fuselage skin support PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument TOP ASSEMBLY - Forward section TOP ASSEMBLY - Forward section TOP ASSEMBLY - Forward section TOP ASSEMBLY - Forward section SKIN - Rear top SKIN - Rear top SKIN - Rear top SKIN - Center top assembly STRINGER STRINGER BULKHEAD ASSEMBLY - Top, Sta. 55 BULKHEAD ASSEMBLY - Top, Sta. 55, LH BULKHEAD ASSEMBLY - Top. Sta. 55, RH A - Used when Collins Radio Installation i s not installed. B - Used when Collins R a d o Installation i s installed. SERIAL NUMBERS AFFECTED 23-1 to 23-1870 inclusive 23-1 to 23-1390 inclusive 23-1391 and up 23-1871 to 23-1967 inclusive 23-1 to 23-1870 inclusive 23-1 to 23-1870 inclusive a23-1 to 23-1870 inclusive 23-1 to 23-1501 inclusive 23-1502 to 23-1870 inclusive 23-1871 to 23-1907 inclusive 23-1908 and up 23-1871 to 23-1907 inclusive 23-1908 to 23-1976 inclusive 23-1977 and up 23-1 to 23-375 inclusive 23-376 to 23-1390 inclusive 23-1391 to 23-1501 inclusive 23-1502 and up 23-1 to 23-375 inclusive 23-376 to 23-1501 inclusive 23-1502 and up 23-1 to 23-1501 inclusive 23-1502 and up 23-1 to 23-1501 inclusive 23-1502 and up 23-1502 and up When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 FUSELAGE FORWARD SECTION SECTION I1 Fuselage G r m p Figure and lndex Number 7-26 - 27 -28 -29 - 30 -31 -32 -33 - 34 - 35 -36 - 37 - 38 - 39 -39a -39b -3% - 39d -39e -3% -3% -40 -41 -42 -43 -44 -45 -45a -46 -47 -48 - 4 9 - 50 -51 -52 ISSUED: APRIL 1973 NOMENCLATURE WLKHEAD ASSEMBLY BULKHEAD - Upper BULKHEAD - Upper BRACKET - Fuselage bulkhead CHANNEL - Fuselage bulkhead, upper right CHANNEL - Fuselage bulkhead, upper left CHANNEL - Fuselage bulkhead, right CHANNEL - Fuselage bulkhead, left CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, right CHANNEL - Fuselage f o m a r d section, right RECEPrACLE - (#2600-212- 12D) ANGLE - Fuselage f o m a r d section, right ANGLE - Fuselage forward section, left ANGLE - Fuselage forward section, right ANCLE - Fuselage forward section, left PANEL ASSEMBLY - Left front side PANEL ASSEMBLY - Left front side PANEL ASSEMBLY - Left front side PANEL ASSEMBLY - Left front side PLATE ASSEMBLY - Access, powerpak filler line PLATE ASSEMBLY - Access, powerpak filler line STUD - Slotted head (#2600- 1) LOCKWASHER - (#2600 LW) PLATE ASSEMBLY - Access, brake fluid reservoir PLATE ASSEMBLY - Access, brake fluid reservoir STUD - Slotted head (#2600- 1) LOCKWASHER - (#2600 LW) RECEFTACLE - Stud (P212-12D) SECTION ASSEMBLY - Fuselage nose SECTION ASSEMBLY - Fuselage nose SECTION ASSEMBLY - Fuselage nose SKIN - Nose, left side SKIN - Nose, right side SKIN - Nose, front top SKIN - Nose, front bottom CHANNEL - Fuselage bulkhead PLATE ASSEMBLY - Landing light compartment back FAIRING - Fuselage nose FAIRING - Fuselage mse WLKHEAD ASSEMBLY - Top, Sta . 6 BULKHEAD ASSEMBLY - Bottom. Sta. 6 PANEL ASSEMBLY - Right front side PANEL ASSEMBLY - Right front side STUD - (2600-2) WASHER - (2600-SW2) PANEL ASSEMBLY - Right rear, side PANEL ASSEMBLY - Right rear, side PANEL ASSEMBLY - Right rear, side PANEL ASSEMBLY - Right rear, side A - This assembly includes the heater a i r intake box. cold a i r intake box (See Figure 17) and landing light installation (See Figure 31). 23- 1 to 23- 1870 inclusive 23-1871 and up z ? n (P P 23-1 to 23-1390 inclusive 23-1391 and up 23- 1 to 23- 1390 inclusive 23- 1391 and up SERIAL NUMBERS AFFECTED 23- 1 to 23- 1182 inclusive 23- 1183 to 23-1390 inclusive 23- 1391 to 23- 1870 inclusive 23- 1871 and up 23- 1 to 23- 1390 inclusive 23-1391 and up 23-1391 and up 23- 1391 and up 23- 1 to 23- 1390 inclusive 23-1391 and up 23- 1391 and up 23- 1391 and up 23- 1391 and up 23- 1 to 23-746 inclusive 23-747 to 23-1163 inclusive 23- 1164 and up 23- 1 to 23- 1163 inclusive 23-1164 and up 23- 1 to 23- 1163 inclusive 23- 1164 and up 23- 1 to 23- 1390 inclusive 23-1391 and up 23-1 to 23-1182 inclusive 23- 1183 to 23- 1390 inclusive 23-1391 to 23-1870 inclusive 23-1871 and up When ordering, always specify Part Number, Description and Serial Number of Aircraft SECTION I1 Fuselage Group Figure I I FUSELAGE FORWARD SECTION NOMENCLATURE and Index Number PANEL - Fuselage access, left PANEL - Fuselage access, left r e a r PANEL - Fuselage access, right front ANGLE BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward section SKIN - Left forward SKIN - Left forward SKIN - Right forward SKIN - Right forward SKIN - Left r e a r SKIN - Left r e a r SKIN - Right r e a r SKIN - Right r e a r BULKHEAD ASSEMBLY - Fuselage forward section. left TUBE ASSEMBLY - Air take-off TUBE ASSEMBLY - Air take-off BULKHEAD ASSEMBLY - Fuselage forward section, right BULKHEAD - Fuselage forward section, right BULKHEAD - Fuselage forward section, left CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, right CHANNEL - Fuselage forward section, right CHANNEL - Fuselage forward section, right RECEPTACLE - (2600-212- 12D) PLATE - Nose wheel well, end BULKHEAD ASSEMBLY - Lower PLATE - Wheel well stiffener TUBE ASSEMBLY - Vent, battery box PLATE - Nose wheel well reinforcement FAIRING ASSEMBLY - Fuselage bottom FAIRING ASSEMBLY - Fuselage bottom PANEL - Removable, right PANEL ASSEMBLY - Fuselage bottom access GROMMET - Drain (AN231-4) PANEL - Insulator SKIN - Access panel ANGLE - Stringer section (6' section) SKIN - Fuselage bottom fairing, right SKIN - Fuselage bottom fairing SKIN - Fuselage bottom fairing BULKHEAD BULKHEAD ASSEMBLY - Fuselage lower fairing BULKHEAD ASSEMBLY - Fuselage lower fairing BULKHEAD ASSEMBLY SKIN - Fuselage bottom fairing, left ANGLE - Stringer section (6' section) PANEL - Removable, left Part Number 1 1 23-1 to 23-1870 inclusive 23-1 to 23-746 inclusive 23-747 to 23- 1390 inclusive 23- 1391 to 23- 1870 inclusive 23- 1871 and up 23-1 to 23-1390 inclusive 23-1391 and up 23- 1 to 23- 1390 inclusive 23-1391 and up 23-1 to 23-1390 inclusive 23- 1391 and up 1 23- 1 to 23- 1390 inclusive 23- 1391 and up I 23-1 to 23-209 inclusive 23-376 and up 23- 1 to 23-1390 inclusive 23- 1391 to 23- 1870 inclusive 23-1871 and up 23- 1 to 23- 1390 inclusive 23- 1391 to 23- 1870 inclusive 23-1871 and up 23-1 to 23- 1151 inclusive 23-1152 and up 23-1 to 23-1151 inclusive 23-1152 and up When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 FUSELAGE FORWARD SECTION SECTION I1 Fuselage Group When ordering, olways specify Port Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23- 1 to 23- 1870 inclusive 23-1871andup 23-1968 and up 23- 1968 and up 23- 1968 and up 23-1968 and up Z P mta 9 1 1 1 1 1 1 1 1 2 1 1 1 Figure and Index Number 7-90 -91 -92 -93 -94 -95 -96 -97 % A B B B B Part Number 17787-00 17785-00 17786-00 17967-00 17967-02 17543-00 17223-01 17223-00 16822-00 16823-00 16823-01 16824-00 NOMENCLATURE SHELF .- Lower radio support BRACKET - Radio shelf, left BRACKET - Radio shelf, right BRACKET - Bottom fairing support, right BRACKET - Bottom fairing support, right BRACKET - Bottom fairing support, center ANGLE - Removable panel support, right A N3LE - Removable panel support, left SHELF ASSEMBLY - Radio SHELF ASSEMBLY - Radio, left SHELF ASSEMBLY - Radio, right CHANNEL ASSEMBLY - Radio shelf support A - This cannot be used when receptacle i s installed. B - Used when Collins Radio Installation i s installed. P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 8. F u o e l e Center Section (Serial Nor. 23-1 to 23-1870 inclusive) SECTION Il Fuselage Group FUSELAGE CENTER SECTION (23- 1 to 23- 1870 incl.) When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23-1 to 23-1501 inclusive 23- 1502 and up 23-1502 and up 23- 1 to 23- 1501 inclusive 23- 1502 and up 23-1 to 23-1501 inclusive 23- 1502 and up 23- 1 to 23-1501 inclusive 23-1502 and up 23-1 to 23-1501 inclusive 23-1502 and up 23-1 to 23-1677 inclusive 23- 1 to 23-1196 inclusive 23- 1 to 23- 1196 inclusive 23- 1 to 23-80 inclusive 23-81 to 23-1501 inclusive 23- 1502 and up 23-1 to 23-80 inclusive 23-81 to 23-1501 inclusive 23- 1502 and up Figure and Index Number 8- -1 -2 - 3 -4 -5 -6 - 8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 -26 -27 -28 -29 -30 -31 -32 -33 -34 -35 -36 -37 -38 -39 -40 -41 -42 Part Number 17309 17309-02 17309-03 17309-04 17309-05 17309-06 17309-37 17309-38 17309-07 17309-08 17309-09 17309-40 17309-10 17309-42 17309-12 17309-13 17309-14 17309-15 17309-41 17309-16 17309-39 17309-21 17309-18 17309-22 751 228 18062-00 18062-01 17212-00 17212-01 17215-00 17215-01 17219-00 17219-01 17220-00 17220-01 17221-00 17221-01 17224-00 17224-01 17241-00 17679-00 17256-00 17236-01 17257-00 18509-00 19552-00 17257-01 18509-01 19552-01 19186-00 17258-01 17259-00 17260-01 17260-00 Z 0 A 8 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 2 2 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 % NOMENCLATURE DRAWING - Fuselage Center Section SKIN - Right window, front SKIN - Left r e a r window, front SKIN - Left r e a r window, r e a r SKIN - Right window, r e a r SKIN - Center fuselage section, front top SKIN - Center fuselage section, front top SKIN - Center fuselage section, rear top SKIN - Center fuselage section, center top SKIN - Center fuselage section, r e a r top SKIN - Windshield, left post SKIN - Windshield, left post SKIN - Center fuselage section, left side, lower front SKIN - Center fuselage section, left side, lower front SKIN - Center fuselage section, left side, r e a r SKIN - Center fuselage section, right side, r e a r SKIN - Center fuselage section, right side, lower center SKIN - Center fuselage section, right side, lower front SKIN - Center fuselage section, right side, lower front SKIN - Windshield, right post SKIN - Windshield, right post SKIN - Fuselage door sill CHANNEL - Fuselage door water drain PLATE - Center fuselage section reinforcement ANGLE - Seinger section (6' section) ANGLE - Headlining trim, left ANGLE - Headlining trim. right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right BULKHEAD - Fuselage center section BULKHEAD - Fuselage center section STRINGER - Fuselage center section, left STRINGER - Fuselage center section, right CHANNEL - Fuselage center section BRACKET ASSEMBLY - Dome light support STRINGER - Fuselage center section. left STRINGER - Fuselage center section, right BULKHEAD - Fuselage center section, left BULKHEAD - Fuselage center section, left BULKHEAD - Fuselage center section, left BULKHEAD - Fuselage center section, right BULKHEAD - Fuselage center section, right BULKHEAD - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right STRINGER - Fuselage center section, left STRINGER - Fuselage center section, right STRINGER - Fuselage center section, left FUSELAGE CENTER SECTION (23-1 t o 23-1870 inclusive) SECTION I 1 Fuselage Group Figure and lndex Number 8-43 4 4 4 5 4 6 4 7 4 8 4 9 -50 -51 -52 -53 -54 -55 -56 -57 -58 -59 -60 -61 -62 -63 -64 -65 -66 -67 -68 -69 -7 0 -71 -72 -73 -74 -75 Part Number NOMENCLATURE CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section. right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right STRINGER - Fuselage center section, rear t o p STRINGER - Fuselage center section, rear t o p CHANNEL - Left rear window, bottom CHANNEL - Right rear window, b o t t o m CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage upper door frame, reinforcement CHANNEL - Left front window, t o p CHANNEL - Left front window, bottom STRINGER - Fuselage center section, left CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right STRINGER - Fuselage center section, left CHANNEL - Fuselage center section, top f r o n t CHANNEL - Fuselage center section, top front STRINGER ASSEMBLY - Fuselage center section, center t o p STRINGER ASSEMBLY - Fuselage center section, center top STRINGER ASSEMBLY - Fuselage center section, front t o p STRINGER ASSEMBLY - Fuselage center section, front t o p B U L K H E A D ASSEMBLY - Fuselage center section, Sta. 141 B U L K H E A D ASSEMBLY - Fuselage center section, Sta. 141 B U L K H E A D ASSEMBLY - Fuselage center section, Sta. 110 B U L K H E A D ASSEMBLY - Fuselage center section, Sta. 110 BRACKET ASSEMBLY - Cockpit light mounting BRACKET ASSEMBLY - Cockpit light mounting HINGE - Baggage compartment door B U L K H E A D - Fuselage center section, left B U L K H E A D - Fuselage center section, right CHANNEL ASSEMBLY - Fuselage door frame, lower front CHANNEL - L e f t rear window CHANNEL - R i g h t rear window CHANNEL ASSEMBLY - Fuselage door frame, lower rear BRACKET ASSEMBLY - T a i l t r i m indicator plate mounting CHANNEL ASSEMBLY - Fuselage door frame, upper CHANNEL ASSEMBLY - Fuselage door frame. lower CHANNEL ASSEMBLY - Baggage compartment door frame B U L K H E A D ASSEMBLY - Fuselage center section, Sta. 79 BRACKET - Door hinge SERIAL NUMBERS AFFECTED 23-1 t o 23-1SUT lncluslve 23-1502 and up 23-1 t o 23-1501 inclusive 23-1502 and u p 23-1 t o 23-1501 inclusive 23-1502 end u p 23-1 t o 23-1501 inclusive 23-1502 end u p 23-1 t o 23-1501 inclusive 23-1502 and u p 23-1 t o 23-1501 inclusive 23-1502 and u p 23-1 t o 23-1501 inclusive 23-1502 and u p 23-1 t o 23-1501 inclusive 23-1502 and u p When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: M A Y 1977 P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figure 9. Fuselage Center Section (Serial Nos. 23-1871 and up) SECTION II Fuselage Group FUSELAGE CENTER SECTION (23-1871 and up) SERIAL NUMBERS AFFECTED Z P ?9 Figure and Index Number 9- - 1 -la -2 -3 -4 -5 -6 -7 -8 -9 -10 - 1 1 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 -26 -27 -28 -29 -30 -31 -32 -33 -34 -35 -36 -37 -38 -39 -40 -41 When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 Port Number 16230 16230-00 17309-02 17309-03 16230-04 16230-03 17309-37 17309-38 16230-02 17309-08 17309-40 17309-44 16230-06 16230-05 17309-14 17309-43 17309-39 17309-21 17496-00 17501-00 17309-17 16221-00 16221-01 16043-01 16043-00 17212-00 17212-01 17215-02 17215-03 17219-00 17219-01 17220-00 17220-01 17221-00 17221-01 17224-M) 17224-01 17241-00 17679-00 17256-00 17256-01 19552-00 19552-01 19186-00 17258-01 17259-00 P ca FUSELAGE CENTER SECTION SKIN - Right front window, front SKIN - Left center window, front SKIN - Left center window, r e a r SKIN - Right front window, rear SKIN - Center fuselage section, front top SKIN - Center fuselage section, r e a r top SKIN - Center fuselage section, center top SKIN - Center fuselage section, r e a r top SKIN - Windshield, left post SKIN - Center fuselage section, left side, lower front SKIN - Center fuselage section, left side, r e a r SKIN - Center fuselage section, right side, r e a r SKIN - Center fuselage section, right side. lower center SKIN - Center fuselage section, right side, lower front SKIN - Windshield, right post SKIN - Fuselage door sill CHANNEL ASSEMBLY - Fuselage door frame, upper CHANNEL ASSEMBLY - Fuselage door frame, lower ANGLE - Stringer section (6' section) CHANNEL ASSEMBLY - Fuselage center section, r e a r window, bottom left CHANNEL ASSEMBLY - Fuselage center section, r e a r window, bottom right CHANNEL ASSEMBLY - Fuselage center section, r e a r window, right CHANNEL ASSEMBLY - Fuselage center section, r e a r window, left CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right CHANNEL - Fuselage center section, left CHANNEL - Fuselage center section, right BULKHEAD - Fuselage center section BULKHEAD - Fuselage center section STRINGER - Fuselage center section, left STRINGER - Fuselage center section, right CHANNEL - Fuselage center section BRACKET ASSEMBLY - Dome light support STRINGER - Fuselage center section, left STRINGER - Fuselage center section, right BULKHEAD - Fuselage center section, left BULKHEAD - Fuselage center section, right CHANNEL ASSEMBLY - Fuselage center section, left CHANNEL ASSEMBLY - Fuselage center section, right STRINGER - Fuselage center section NOMENCLATURE DRAWING - Fuselage Center Section 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 1 1 2 1 1 1 1 1 1 1 1 FUSELAGE CENTER SECTION (Serial Nos. 23-1871 and up) SECTION II Fuselage Group When ordering, always specify Part Number, Description and Serial Number of Aircraft Figure and Index Number 9 4 2 4 3 -44 4 5 4 6 ' 4 7 4 8 4 9 -50 -51 -52 -53 -54 -55 3 6 -57 -58 -59 -60 -61 -62 . -63 -64 -65 -66 -67 -68 -69 -70 -7 1 REVISED: M A Y 1977 Part Number 1726040 17260-02 16084-00 16084-01 17265-00 17265-01 19564-00 17276-00 17276-05 17277-00 17277-05 17278-00 17279-00 17282-00 17284-00 17285-00 17285-01 17288-00 19534-00 17304-06 17305-08 16305-00 17307-09 16899-00 16088-00 16088-01 17222-00 17222-01 32910-00 19525-00 17557.00 17537-00 17308-00 17550-00 Code NOMENCLATURE STRINGER - Fuselage center section, left STRINGER - Fuselage center section, right CHANNEL - Fuselage center section, l e h CHANNEL -Fuselage center section, right CHANNEL -Fuselage center section, left CHANNEL - Fuselage center section, right STRINGER - Fuselage center section, rear top CHANNEL - Left rear window, bottom CHANNEL -Right front window, bottom CHANNEL - Fuselage canter section, l e h CHANNEL - Fuselage center section, right CHANNEL - Fuselage upper door frame reinforcement CHANNEL - Left front window, t o p CHANNEL - Left front window, b o t t o m STRINGER - Fuselage center section, left CHANNEL -Fuselage center section, left CHANNEL -Fuselage canter section, right STRINGER - Fuselage center section, left CHANNEL -Fuselage center section, t o p front STRINGER ASSEMBLY - Fuselage center section, center t o p STRINGER ASSEMBLY - Fuselage center section, front t o p BULKHEAD ASSEMBLY - Fuselage center section, Sta. 141 BULKHEAD ASSEMBLY - Fuselage center section, Sta. 110 BRACKET ASSEMBLY - T a i l t r i m indicator plate mounting CHANNEL ASSEMBLY - Fuselage center section, rear window, left CHANNEL ASSEMBLY - Fuselage center section, rear window, right BULKHEAD - Fuselage center section, left BULKHEAD - Fuselage center section, right CHANNEL ASSEMBLY - Fuselage door frame, lower front BRACKET ASSEMBLY - Cockpit light mounting CHANNEL ASSEMBLY - Baggage compartment door frame CHANNEL ASSEMBLY - Fuselage door frame, lower rear BULKHEAD ASSEMBLY - Fuselage center section, Sta. 79 BRACKET - Door hinge No. Req. 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 SERIAL NUMBERS AFFECTED INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T REVISED: FEBRUARY 1983 Figure 10. Fumlape A h Section SECTION I1 Fuselage Group FUSELAGE AFT SECTION Figure and l ndex Numbel Part Number NOMENCLATURE A DRAWING - Fuselage Aft Section SKIN - Fuselage aft section, top SKIN - Fuselage aft section, left side SKIN - Fuselage aft section, bottom front SKIN - Fuselage aft section, bottom r e a r SKIN - Fuselage aft section, right side BRACKET - Tail s k d support BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 290 BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 253 BRACKET - Elevator control tube, right r e a r roller BRACKET - Elevator control tube, left r e a r roller PLATE - Whip antenna mounting CHANNEL - Fuselage aft section, upper right, Sta. 169 and 192 CHANNEL - Fuselage aft section. upper left. Sta. 169 and 192 FITTING ASSEMBLY - Fuselage aft section, upper left attachment FITTING ASSEMBLY - Fuselage aft section, upper right attachment BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 171 BULKHEAD ASSEMBLY - Fuselage aft section. Sta. 171 PLATE - Antenna mast mounting FITTING ASSEMBLY - Fuselage aft section, lower right attachment FITTING ASSEMBLY - Fuselage aft section, lower left attachment CHANNEL - Fuselage aft section, lower right, Sta. 153 and 192 CHANNEL - Fuselage aft section, lower left, Sta. 153 and 192 ANGLE - Fuselage aft section BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 192 BULKHEAD ASSEMBLY - Fuselage aft section, Sta. 192 ANGLE - Stringer section (6' section) ANGLE - Fuselage aft section BULKHEAD ASSEMBLY - Fuselage aft section, Sta. 229 BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 229 ANGLE - Fuselage aft section, right, Sta. 229 to 290 A I S L E - Fuselage aft section, left, Sta. 229 to 290 BULKHEAD ASSEMBLY - Fuselage aft section, Sta . 266 BULKHEAD - Fuselage aft section, Sta. 285 BRACKET - Elevator control tube, left front roller BRACKET - Elevator control tube tube, right front roller FITTING ASSEMBLY - Stabilizer front attachment BRACKET ASSEMBLY - Fuselage bulkhead A - Complete assembly available a s 17121-47 without bungee mechanism for airplane serial numbers 23-1 to 23- 1871 inclusive and complete assembly available a s 17121-50 without bungee mechanism for airplane serial numbers 23- 1871 and up. SERIAL NUMBERS AFFECTED 23- 1 to 23- 1501 inclusive 23- 1502 and up 23- 1 to 23-1870 inclusive 23- 1871 and up 23- 1 to 23-1870 inclusive 23- 1871 and up W h e n ordering, always specify Port Number, Description and Serial Number of Aircmft ISSUED: APRIL 1973 FUSELAGE AFT SECTION SECTION I1 Fuselage Group When ordering, olwoys specify Port Number, Description ond Serial Number of Aircraft REVISED: FEBRUARY 1983 Figure and Index Number 10-28 -29 - 3 0 -31 -32 -33 - 3 4 -35 -36 -37 Z P lnio P 1 1 1 1 1 1 1 1 AR A R A R A R AR I I Part Number 17115-00 17116-00 19938-01 19938-00 17119-00 17118-00 19777-00 17121-24 19119-02 19119-03 18564-02 18564-03 18564 -04 28618-02 28619-02 SERIAL NUMBERS AFFECTED 6n ID A A NOMENCLATURE BRACKET ASSEMBLY - Pulley GUSSET - Fuselage aft section CHANNEL - Fuselage aft section, right CHANNEL - Fuselage aft section, left BRACKET ASSEMBLY - Elevator bellcrank, right BRACKET - Elevator bellcrank, left STRINGER CHANNEL - Fuselage aft section, tail SHIM - Stabilizer attachment fitting. forward (. 064) SHIM - Stabilizer attachment fitting, forward (. 032) SHIM - Stabilizer attachment fitting, bottom ( .016) SHIM - Stabilizer attachment fitting, bottom (.032) SHIM - Stabilizer attachment fitting. bottom (.064) CHANNEL REINFORCEMENT BRACKET - Support A - Used on aircraft that have complied with Service Bulletin lrio.672. P I P E R A I R C R A F T C O R P O R A T I O N REVISED: MAY 1977 Figrre 11. Fuselage Frame SECTION I1 Fuselage Group FUSELAGE FRAME When ordering, olways specify Port Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 SERIAL NUMBERS AFFECTED 23- 1 to 23- 1870 inclus~ve 23-1871 and up 23- 1 to 23- 1870 inclusive 23- 1871 and up 23-1 to 23- 1151 inclusive 23-1152 to 23-1870 inclusive 23- 1871 and up 23- 1 to 23-1151 inclusive 23-1152 to 23-1870 inclusive 23-1 to 23-1151 inclusive 23- 1152 to 23-1870 inclusive Z 0 A rn P 1 1 1 1 1 2 5 2 2 2 1 1 1 1 1 1 1 2 1 1 1 1 1 2 1 2 1 1 1 1 1 1 1 Figure and Index Number 11- - 1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -24 -25 NOMENCLATURE DRAWING - Rudder Pedal Torque Tube Bracket Installation DRAWING - Fuselage Frame Assembly DRAWING - Fuselage F r a m e Assembly DRAWING - Fuselage Fitting Installation DRAWING - Fuselage Fitting Installation FUSELAGE FRAME ASSEMBLY FUSELAGE FRAME ASSEMBLY FUSELAGE FRAME ASSEMBLY TUBE - Step attachment BRACKET ASSEMBLY - Flap actuating cylinder, mounting BRACKET - Rudder cable pulley BRACKET - Baggage tie down r e a r PLATE - Elevator tube idler channel PLATE - Elevator tube idler channel PLATE - Elwator tube idler channel BRACKET - Step reinforcement BRACKET - Safety belt attachment, left BRACKET - Safety belt attachment, right FITTING - Rear seat attachment, left FITTING - Fuselage frame FITTING - Rear seat attachment, right FITTING - Fuselage frame FITTING ASSEMBLY - Top deck attachment BRACKET ASSEMBLY - Nose gear cylinder attachment, right BRACKET ASSEMBLY - Nose gear cylinder attachment, left ANGLE - Heater support BRACKET - Heater mounting, upper BRACKET - Heater mounting, lower BUSHING - Nose gear mounting BUSHING - Rudder pedal torque tube attachment bracket BRACKET - Rudder pedal torque tube attachment, outboard BRACKET ASSEMBLY - Rudder pedal torque tube attachment FITTING - Nose wheel drag link attachment, right FITTING - Nose wheel drag link attachment, left BRACKET - Rudder pedal torque tube attachment. center FITTING ASSEMBLY - Control column attachment, right FITTING ASSEMBLY - Control column attachment. left BRACKET - E l w a t o r control tube idler Part Number 17147 17162 16228 18868 16257 17162-05 17162-06 16228-00 17401-00 17168-00 17150-00 18433-00 17175-02 17175-03 17175-04 18357-00 17080-00 17080-01 17081-00 19352-00 17081-01 19352-01 17171-00 17313-01 17313-00 17327-00 17326-02 17326-03 17164-00 86102-28 17145-00 17144-00 17082-01 17082-00 17146-00 17173-00 17172-00 17160-00 % FUSELAGE FRAME SECTION II Fuselage Group Figure and Part Index Number Number NOMENCLATURE CHANNEL - Brake pedal attachment, outboard CHANNEL - Brake pedal attachment, outboard CHANNEL - Brake pedal attachment, outboard CHANNEL - Brake pedal attachment, inboard CHANNEL - Brake pedal attachment, inboard CHANNEL - Brake pedal attachment, inboard FITTING 4SSEMBLY - Wing front s p a r attachment FITTING ASSEMBLY - Wing front spar attachment BRACKET - Seat track attachment, left outer and right inner BRACKET - Seat track attachment, left outer BRACKET - Seat track attachment, right inner BRACKET - Seat track attachment, right outer and left inner BRACKET - Seat track attachment, right outer BRACKET - Seat track attachment, left inner TUBE - Liner BRACKET - Top deck attachment, left BRACKET - Top deck attachment, left BRACKET - Top deck attachment, right BRACKET - Top deck attachment, right A K L E - Floorboard support, front, left ANGLE - Floorboard support, front, right BRACKET - Seat track support, right BRACKET - Seat track support, left BRACKET - Front spar mounting, lower left BRACKET - Front spar mounting, lower right BRACKET - Front spar mounting, upper FITnNG - Rear seat belt attachment FITTING ASSEMBLY - Rear seat belt attachment FITTING - Fuselage bottom panel attachment FITTING ASSEMBLY - Rear spar attachment, right FITTTNG ASSEMBLY - Rear s p a r attachment left BRACKET ASSEMBLY - Flap torque tube attachment, left BRACKET ASSEMBLY - Flap torque tube attachment, right FITTING - Fuselage aft section attachment, lower right FI'TTING - Fuselage aft section attachment, lower left FITTING ASSEMBLY - Wing front s p a r r e a r attachment TUBE ASSEMBLY - Brake channel support, right, outboard TUBE ASSEMBLY - Brake channel support, right, inboard A - Used on PA-23-160 with serial nos. 23-1871 to 23-1976, 23-1978 to 23- 1980, 23- 1982, 23- 1983 and 23- 1988 to 23-2043 inclusive. B - Used on PA-23-160 with serial nos. 23-1977, 23-1981 23-1984 to 23-1987 and 23-2044 to 23-2046. SERIAL NUMBERS AFFECTED 23- 1 to 23- 1870 inclusive 23- 1 to 23- 1870 inclusive 23-1 to 23-1151 inclusive 23-1152 andup 23- 1 to 23- 1870 inclusive 23- 1871 and up 23- 1871 and up 23-1 to 23-1870 inclusive 23-1871 and up 23- 1871 and up 23-1152 to 23-1870 inclusive 23- 1 to 23- 1870 inclusive 23-1871 and up 23- 1 to 23- 1870 inclusive 23- 1871 and up 23-1152 and up When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: FEBRUARY 1983 INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T C O R P O R A T I O N ISSUED: APRIL 1973 Figure 12. Instrument Panel Installation (Serial Nos. 23-1 to 23-1501 inclusive) INSTRUMENT PANEL INSTALLATION (Serial Nos., 23-1 to 23-1501 Inclusive) SECTION II Fuselage Group Figure and Index Number PIPER PARTS CATALOG I I NOMENCLATURE DRAWING - Instrument Panel Installation INSTRUMENT - Directional gyro PLUG - (WM 3152 x 4) ELBOW - (AN842-6D) BRACKET ASSEMBLY - Support, gyro horizon INSTRUMENT - Gyro horlzon indicator TUBE ASSEMBLY - Air (static) ELBOW - (AN844-4D) BUSHING - (AN912-1D) HOSE - Airspeed 1 (pitot) HOSE - Flexible INSTRUMENT - Alrspeed indicator INSTRUMENT - Airspeed indicator INSTRUMENT - Airspeed indicator INSTRUMENT - True speed indicator "150" (3500 Ib. gross weight) INSTRUMENT - True speed indicator TEE - (AN825-3D) INSTRUMENT - Manifold pressure gauge NIPPLE - (AN816-3D) INSTRUMENT - Tachometer SHAFT - Tachometer, 140" CORE -138" CORE -140" WASHER WASHER INSTRUMENT - Suction gauge INSTRUMENT - flap position indicator ADAPTER ASSEMBLY -12 Volt SEPARATOR - Terminal INSTRUMENT - Altimeter, sensitive (scale in inches of mercury) INSTRUMENT - Altimeter, sensitive (scale in millibars) ELBOW - (AN822-3D) TUBE ASSEMBLY - Air (static) INSTRUMENT - Tum and bank indicator INSTRUMENT - Rate of climb INSTRUMENT - Clock, 8 day PLATE ASSEMBLY - Cover EMBLEM ADAPTER ASSEMBLY -12 Volt REDUCER - Oil pressure gauge (AN919-OD) A - Used when 150 H. P. engines are installed. B - Used when 160 H.P. engines are Installed. C - Measure length of core before ordering. D - Used with 6 Volt instruments only. E - Used 17419-08 when 150 H. P, engines are installed and airplanes is approved for 3800 Ib. gross weight. No. Req. SERIAL NUMBERS AFFECTED 23-1 to 23-1501 inclusive 23-1152 and up 2 3 - i i n , 23-1183 ~OB-I~OI When ordering, always specify Part Number, Description, and Serial Number of Aircraft Interim Revision: September 1998 SECTION II Fuselage Group Figure and index Number When ordering, always specify Part Number, Description and Serial Number of Aircraft PIPER PARTS CATALOG NOMENCLATURE INSTRUMENT CLUSTER REPLACEMENT KIT INSTRUMENT - Fuel quantity gauge ' INSTRUMENT - Ammeter + INSTRUMENT - 011pressure gauge + INSTRUMENT - Fuel pressure gauge INSTRUMENT - Oil temperature gauge PLATE ASSEMBLY - Radio opening cover, right side TRACK ASSEMBLY - Map drawer, left TRACK ASSEMBLY - Map drawer, left TRACK ASSEMBLY - Map drawer, right TRACK ASSEMBLY - Map drawer, right CLAMP ASSEMBLY - Map drawer track attachment, left CLAMP ASSEMBLY - Map drawer track attachment, right WASHER WASHER MOUNTING - Instrument, shock MOUNTING - Instrument, shock PANEL ASSEMBLY - Instrument panel, right insert PANEL ASSEMBLY - Instrument panel, left insert PANEL ASSEMBLY - lnstrument panel, left insert PANEL ASSEMBLY - Instrument panel, left insert PANEL ASSEMBLY - lnstrument panel. left insert BUMPER - Rubber PLACARD - Operating limitations, brown PLUG - Button PLACARD - Parking brake and phone jack. brown PLACARD - Parking brake and phone jack, black KNOB - Tee, parking brake (KN578A) PLACARD - Panel switches, brown PLACARD - Panel switches, black PLATE ASSEMBLY - Radio opening cover, left side PLACARD - Check list, brown PLACARD - Check list, black ANGLE ASSEMBLY - Instrument panel support PANEL ASSEMBLY - Instrument panel cover PANEL ASSEMBLY - Instrument panel cover JACK - Phone JACK - Mike WASHER PLACARD - Phone jack. brown PLACARD - Phone jack, black BUSHING DRAWER ASSEMBLY - Map DRAWER ASSEMBLY - Map A - Used when LTRA-6 radio is installed. B - Used when 150 H.P. engines are installed. C - Used when 160 H.P. engines are installed. D - Used with Rochester Gauge lnstrument Cluster Assembly only. If A.C. Spark Plug instruments are installed, order lnstrument Cluster Replacement Kit 764 429 which contains a new Rochester Gauge lnstrument Cluster Assembly complete with all instruments. REVISED: FEBRUARY 1983 Part Number (Serial No. Rw. 1 2 1 2 2 2 1 1 1 1 1 1 1 9 9 6 4 1 1 1 1 1 17 1 2 1 1 1 1 1 1 1 1 1 1 1 2 2 4 1 1 4 1 1 Code INSTRUMENT PANEL INSTALLATION Nos. 23- 1 to 23- 1501 inclusive) SERIAL NUMBERS AFFECTED 23-1 to 23-746 inclusive 23-747 and up 23-1 to 23-746 inclusive 23-747 and up 23-1 to 23-746 inclusive 23-747 and up 23-1 to 23-746 inclusive 23-747 and up 23-1 to 23-746 inclusive 23-1 to 23-746 inclusive 23-747 and up 23-747 and up 23-1 to 23-375 inclusive 23-376 and up 23-1 to 23-375 inclusive 23-376 and up 23- 1 to 23-375 inclusive 23-376 and up 23-1 to 23-1967 inclusive 23-1968 and up 23-1 to 23-746 inclusive 23-747 and up INSTRUMENT PANEL INSTALLATION (Serial Nos. 23-1 to 23-1501 inclusive) SECTION I1 Fuselage Group When ordering, olwoys specify Port Number, Description and Serial Number of Aircroft ISSUED: APRIL 1973 1 c9 Figure and Index Number 12-64 -65 -66 -67 -68 -69 -70 -71 -72 -73 -74 -75 -76 -77 -78 -79 -80 -81 -82 -83 -84 -85 -86 -87 -88 -89 -90 -91 Part Number 17900-00 17900-03 17767-00 17754-00 17754-03 13541-04 487 570 458 941 451 854 17790-03 17741-00 18414-00 19379-00 18285-00 17425-00 18964-00 80122-83 453 602 19200-00 455 129 450 710 487814 81102-25 755 824 752 119 756 907 756 307 753 948 753 949 756 256 753 213 6 % NOMENCLATURE PLACARD - "APACHE", brown PLACARD - "APACHE", black PLATE - Map drawer cover PLATE ASSEMBLY - Wire support, right PLATE ASSEMBLY - Wire support, right TUBE - Airspeed (pitot) MOUNTING STRAP - Flap indicator (tt1500666) ELBOW - (AN844-6D) ADAPTER - (W/H 3200 x 2) PLATE ASSEMBLY - Cover EMBLEM COMPASS - 6 Volt COMPASS - 12 Volt GASKET - Compass PANEL ASSEMBLY - Instrument SPACER - Rubber WASHER - (.032) BUTTON - Plug (48152) PLACARD - Parking brake (standard) CONNECTOR - Carburetor a i r temperature (AN3106A-14s-2s) GAUGE - Carburetor a i r temperature (AN5790-6) SWITCH - Carburetor a i r temperature (a8482Kl) SPACER - Carburetor a i r temperature switch PAD - Standard instrument filter (2 per instrument) GAUGE - Mixture control indicator THERMOCOUPLE ASSEMBLY - (With mounting h t ) THERMOCOUPLE - (Less mounting kit) CLAMP - Thermocouple probe attachment CLAMP ASSEMBLY - Thermocouple probe attachment MOUNTING SLEEVE - Thermocouple probe attachment WIRE ASSEMBLY - Mixture control gauge z 0 ~n ;D P 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 6 A R 4 1 1 1 1 1 AR 1 2 1 1 1 1 2 SERIAL NUMBERS AFFECTED 23-1 to 23-375 inclusive 23-376and up 23-1 to 23-746 inclusive 23-747 and up 23-1 to 23-1222 inclusive 23-1223 and up 23-920 and up 23-920 and up 23-920and up 23-920 and up P I P E R A I R C R A F T C O R P O R A T I O N ISSUED: APRIL 1973 Figure 13, Instrument Panel Installation (Serial Nos. 23-1502 and up) SECTION II Fuselage Group F : : : 1 Part 1 Code Index Number Number I I INSTRUMENT PANEL INSTALLATION (Serial Nos. 23-1 502 and up) PIPER PARTS CATALOG 0 NOMENCLATURE SERIAL NUMBERS 1 +. 1 AFFECTED DRAWING - Instrument Panel lnstallation DRAWING - lnstrument Panel lnstallation DRAWING - lnstrument Panel Installation DRAWING - lnstrument Panel lnstallation INSTRUMENT - Carburetor air temperature INSTRUMENT - Suction gauge INSTRUMENT - Ammeter (35 AMP) INSTRUMENT - Ammeter (50 AMP) INSTRUMENT - Flap indicator INSTRUMENT - Tachometer INSTRUMENT - Manifold pressure gauge INSTRUMENT - Airspeed indicator, '150" INSTRUMENT - Alrspeed indicator, '1 60" INSTRUMENT - Airspeed indicator, '1 60" INSTRUMENT - Airspeed Indicator, '160" INSTRUMENT - True speed indicator INSTRUMENT -True speed indicator INSTRUMENT - Altimeter, sensitive (Scale in inches of mercury) INSTRUMENT - Altimeter, sensitive (Scale in millibars) INSTRUMENT - Clock INSTRUMENT - Rate of climb (0-4000 ft/min) INSTRUMENT - Directional gyro INSTRUMENT - Gyro horizon INSTRUMENT - Tum and bank PLUG - Pipe (3152 x 4) PLUG - (AN932-3) BUSHING - (AN912-1D) ELBOW - (AN844-6D) 45" ELBOW - (#134A3) ELBOW - (AN844-4D) 45" CONNECTOR ASSEMBLY ELBOW - (AN842-6D) 90" ELBOW - (#134A3) TEE - (AN826-3D) PANEL - lnstrument insert PANEL - lnstrument insert PANEL - lnstrument insert BRACKET ASSEMBLY - Gyro panel mounting PANEL - Cover, right PANEL ASSEMBLY - Cover, right (complete) A - Optional equipment on 12 Volt system. B - Used on PA-23-160 with serial numbers 23-1871 to 23- 1976, 23-1978 to 23-1980, 23-1982, 23-1983 and 23- 1988 to 23-2043 inclusive. C - Used on PA-23-160 with serial numbers 23-1977, 23- 1981,23-1984to 23-1987 and 23-2044 to 23-2046. D - Used on PA-23-160 with serial numbers 23-1968 to 23- 1976, 23-1978 to 23-1980, 23-1982, 23-1983 and 23- 1988 to 23-2043 inclusive. 23-1502 to 23-1870 inclusive 23-1871 to 23-1967 inclusive 23-1502 to 23-1683 inclusive 23-1684 and up 23-1502 to 23-1870 lnclusive 23-1502 to 23-1773 inclusive, 23-1775 to 23-1870 inclusive 23-1774,23-1871 and up 23-1 to 23-201 2 inclusive 23-2013 and up 23-1502 to 23-2012 incluslve 23-1502 to 23-2012 inclusive 23-2013 and up 23-1502 to 23-2012 inclusive 23-2013 and up 23-1502 to 23-2012 inclusive 23-2013 and up 23-1502 to 23-1870 inclusive 23-1871 to 23-1967 Inclusive 23-1968 and up When ordering, always specify Pan Number, Description, and Serial Number of Aircraft Interim Revision: September 1998 1C11 INSTRUMENT PANEL ISTALLATION (Serial Nos. 23- 1502 and up) SECTION I1 Fuselage Group Figure and lndex Numbel Part Number NOMENCLATURE PANEL - Instrument panel, right cover PLATE - Instrument light plug attachment WASHER PLUG - (Banana - 100) RECEPTACLE - (GB-5952-3RH-R) BULB - Indicator (#330) RECEPTACLE - (GB-5952-3LH-R) BULB - Indicator (#330) PANEL - Cover, left PANEL - Cover, left PANEL ASSEMBLY - Instrument panel, left (complete) PANEL ASSEMBLY - Instrument panel, let? cover PLACARD - Operating limitations PLATE - Instrument light plug attachment WASHER PLUG - (Banana - 100) RECEPrACLE - (GB-5952-3RH-R) BULB - Indicator RECEPrACLE - (GB-5952-3LH-R) BULB - Indicator DOOR ASSEMBLY - Glove compartment LIGHTER ASSEMBLY - Cigar PLATE ASSEMBLY - Hole a v e r PLATE ASSEMBLY - Hole cover PLACARD - "APACHE" PLACARD - Switch PLACARD - Switch DRAWER ASSEMBLY - Map TRACK ASSEMBLY - Map nacker, left TRACK ASSEMBLY - Map tracker, right PLACARD - Check list PLACARD - Check list PLACARD - Check list PLACARD - Parking brake HANDLE - Parking brake NIPPLE - (AN816-3D) ADAPTER - (W/H 3200 x 2) HOSE - Flexible TUBE ASSEMBLY - Airspeed SEPARATOR - (1515642) PLACARD - Limitations PLATE - Control wheel shaft BLOCK A - Optional equipment on 12 Volt system. B - Used on PA- 23-150, PA-23- 160 with serial nos. 23-1 to 23-1976. 23-1978 to 23-1980. 23-1982. 23-1983 and 23-1988 to 23-2043. C - Used on PA -23- 160 with serial nos. 23- 1977, 23- 1981 23- 1984 to 23- 1987 and 23-2044 to 23-2046. D - Used on PA-23-160 with serial nos. 23-1871 to 23-1976, 23-1978 to 23-1980, 23-1982, 23-1983 and 23- 1988 to 23-2043 inclusive. SERIAL NUMBERS AFFECTED 23- 1502 and up 23- 1502 and up 23-1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 to 23- 1967 inclusive 23- 1968 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23-1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 and up 23- 1502 to 23- 1870 inclusive W h e n ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 INSTRUMENT PANEL INSTALLATION (Serial Nos. 23-1 502 and UDI SECTION II Fuselage Group I k x 1 N:cler 1Number 1PIPER PARTS CATALOG NOMENCLATURE BUlTON - Plug (48152) STRAP - Mounting (1500666) SHAFT - Tachometer (146" L) 'CORE - Tachometer shaft (140" L) ' CORE - Tachometer shaft (146" L) ELBOW - 45" (AN844-4D) WASHER - (.064) WASHER - (.032) HOSE - Flexible LlNE ASSEMBLY - Static air LlNE ASSEMBLY - Static air TUBE ASSEMBLY - Static air y REDUCER - (AN919-OD) INSTRUMENT CLUSTER REPLACEMENT KIT 'INSTRUMENT - Fuel quantity 'INSTRUMENT - Fuel pressure 'INSTRUMENT - Oil pressure ' INSTRUMENT - Oil temperature COMPARTMENT ASSEMBLY - Glove PLATE - Map drawer cover PLATE - Map drawer cover PLATE ASSEMBLY - Wire support PLATE ASSEMBLY - Wire support PANEL - Radio opening cover, left PANEL - Radio opening cover, left PANEL - Radio opening cover, left PANEL - Radio opening cover, right PANEL - Radio opening cover, right PANEL - Radio opening cover, right COMPASS ASSEMBLY - 12 Volt 1 PANEL ASSEMBLY - lnstrument PANEL ASSEMBLY - lnstrument PANEL ASSEMBLY - lnstrument PANEL ASSEMBLY - lnstrument PANEL ASSEMBLY - Radio opening cover PANEL ASSEMBLY - Radio opening cover NIPPLE - (AN816-4D) GROMMET - (AN931-6-10) Shock mounting A - Measure length of core before ordering. B - Used on PA-23-160 with serial nos. 23-1968 to 23-1976 23-1 978 to 23-1 980, 23-1 982, 23-1 983 and 23-1 988 to 23-2043 inclusive. C - Used on PA-23-16 0 with serial nos. 23-1977, 23-1981, 23-1 984 to 23-1 987 and 23-2044 to 23-2046. D - Used on PA-23-16 0 with serial nos. 23-1 871 to 23-1976 23- 1978 to 23- 1980. 23- 1982. 23- 1983 and 23- 1988 to 23-2043 inclusive. E - Used with Rochester Gauge lnstrument Cluster Assembly only. If A.C. Spark Plug instruments are installed, order lnstrument Cluster Replacement Kit 764 430 which contains a new Rochester Gauge lnstrument Cluster Assembly complete with all instruments. 23-1 502 to 23-1 870 inclusive No. Req. 23-1 502 to 23-201 2 inclusive 23-201 3 and up 23-1 to 23-1 870 inclusive 23-1 871 and up 23-1 502 to 23-1967 inclusive SERIAL NUMBERS AFFECTED 23-1 502 to 23- 1967 inclusive 23-1 502 to 23-1 870 inclusive 23-1 871 to 23-1967 inclusive 23-1 9 6 8 to 23-2012 inclusive 23-2013 and up 23- 1 to 23-1967 inclusive 23- 1968 and up When ordering, always specify Part Number, Description and serial Number of Aircraft REVISED: FEBRUARY 1983 1C13 INSTRUMENT PANEL INSTALLATION (Serial Nos. 23- 1502 and up) -Figure and l ndex Number Part Number NOMENCLATURE PAD - Autocontrol instrument filter (2 per instrument) SWITCH - Carburetor a i r temperature CLAMP ASSEMBLY - Map drawer track attachment CLAMP ASSEMBLY - Map drawer track attachment PLACARD - Radio circuit breaker BUTTON - Plug (SS48192) MOUNTING - Instrument shock (#100PD-4) PLACARD - Fuel pump switches ANGLE - Mike and phone jack mounting, LH PLACARD - Landing light and taxi light GAUGE ASSEMBLY - Mixture control indicator GAUGE ASSEMBLY - Mixture control indicator THERMOCOUPLE ASSEMBLY - (with mounting kit) THERMOCOUPLE - (less mounting kit) CLAMP - Thermocouple probe attachment CLAMP ASSEMBLY - Thermocouple probe attachment MOUNTING SLEEVE - Thermocouple probe attachmept WIRE ASSEMBLY - Mixture control gauge AMPLIFIER ASSEMBLY - Mixture control gauge A - Used on PA-23-160 with s e r i a l numbers 23-1977, 23-1981, 23-1984 to 23-1987 and 23-2044 to 23-2046. B - Used if Mixture Control Gauge Amplifier installed. SECTION II Fuselage Group SERIAL NUMBERS AFFECTED When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: APRIL 1973 INTENTIONALLY LEFT BLANK P I P E R A I R C R A F T ml C O R P O R A T I O N ISSUED: APRIL 1973 Figure 14. Control Pedestal Installation CONTROL PEDESTAL INSTALLATION SECTION I1 Fuselage Group When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: AF'RIL 1973 Figure and Index Number 14- - 1 -2 -3 -4 -5 -6 -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 -20 z0 ;O 9" 1 1 1 2 2 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 SERIAL NUMBERS AFFECTED 23- 1 to 23- 1501 inclusive 23- 1502 to 23- 1870 inclusive 23- 1871 and up 23- 1 to 23- 1967 inclusive 23- 1968 and up 23-1 to 23-746 inclusive 23-747 to 23-1501 inclusive 23- 1502 to 23- 1835 and 23- 1840 23-1836 to 23-1839. 23- 1841 and up 23-1 to 23-1870 inclusive 23- 1871 and up 23- 1 to 23-1870 inclusive 23- 1989 and up 23-1871 to 23-1988 inclusive 23- 1 to 23- 1870 inclusive 23-1871 to 23-1988 inclusive 23-1989 and up 23-1 to 23-375 inclusive 23-376andup 23-1 to 23-375 inclusive 23-376 to 23-1151 inclusive 23-1 to 23-375 inclusive 23-376 to 23-746 inclusive 23-747 and up 23-1 to 23-375 inclusive 23-376 to 23-739 inclusive 23-740 to 23-1163 inclusive 23-1164 to 23-1173 inclusive 23-1174 to 23-1501 inclusive 23- 1502 to 23- 1870 inclusive 23-1871andup 23-1 to 23-375 inclusive 23-376 to 23-739 inclusive 23-740 to 23- 1163 inclusive 23- 1164 to 23-1173 inclusive 23-1174 to 23-1501 inclusive 23- 1502 to 23- 1870 inclusive 23-1871 and up 23-1 to 23-1501 inclusive 23-1502to23-1835and 23- 1840 inclusive 23-1836 to 23-1839, 23-1841 and up Part Number 17986 19152 16298 18356-00 17603-00 19864-00 17483-00 17834-00 17929-00 17065-00 17065-03 17065-05 17065-03 80002-53 17892-00 16975-00 17966-00 17891-02 17820-00 17820-02 18330-00 19715-00 19715-02 17861-00 17861-03 17457-02 18875-05 17894-00 18867-00 19065-00 17640-00 17640-06 17640-07 17640-09 17640- 11 17640- 13 17640-23 17640-04 17640-05 17640-08 17640-10 17640- 12 17640- 14 16681-00 13945-28 17736-00 17736-03 17736-00 18323-00 % NOMENCLATURE DRAWING - Pedestal Installation DRAWING - Pedestal Installation DRAWING - Pedestal Installation GASKET - Nose wheel cover BASE - Pedestal BASE - Pedestal PLATE - Pedestal, access ANGLE ASSEMBLY - Pedestal support CHANNEL - Hydraulic pump lever guide PLATE ASSEMBLY - Pedestal, left side PLATE ASSEMBLY - Pedestal, left side PLATE ASSEMBLY - Pedestal, l e h side PLATE ASSEMBLY - Pedestal, left side CLAMP - Offset BRACKET ASSEMBLY - Engine control support BRACKET ASSEMBLY - Engine control support ANGLE - Pedestal control placard attachment TUBE - Engine controls stop, forward PLATE - Pedestal front cover PLATE - Pedestal front cover PLATE - Propeller control lever, friction PLATE - Propeller control lever, friction PLATE - R o p e l l e r control l w e r , friction PLACARD - Pedestal control, brown PLACARD - Pedestal control, black KNOB - Plastic, carburetor, brown KNOB - Plastic, carburetor, black PLACARD - Heater panel, brown PLACARD - Heater panel, black PLACARD - Heater panel, black COVER ASSEMBLY - Nose wheel, brown COVER ASSEMBLY - Nose wheel, gray COVER ASSEMBLY - Nose wheel, dark gray COVER ASSEMBLY - Nose wheel, dark gray COVER ASSEMBLY - Nose wheel, dark gray COVER ASSEMBLY - Nose wheel, dark gray BACKING - Less plastic cover CARPET - Brown CARPET - Gray CARPET - Dark gray CARPET - Drak gray CARPET - Dark gray CARPET - Dark gray COVER ASSEMBLY - Thermoplastic STRIP - Rubber PLATE ASSEMBLY - Pedestal, right side PLATE ASSEMBLY - Pedestal, right side PLATE ASSEMBLY - Pedestal, right side NUT - Special SECTION I1 Furelage Group CONTROL PEDESTAL INSTALLATION Figum and Index Number Part Number Code A B A B A B A B A B A B NOMENCLATURE ANGLE - Landing gear contrd latch attachment, left LATCH - Landing gear contrd ANGLE - Landing gear contrd latch attachment, right SPRING - Landing p a r contrd lock BUSHING BUSHING PIN - Landing gear control latch TUBE - Engine controls nop, aft WASHER CLEVIS - Engine control cables (MS35812-1) CHANNEL ASSEMBLY - Pedsstal support CONTROL ASSEMBLY - PedBstal CONTROL ASSEMBLY - Pedestal CONTROL ASSEMBLY - Pedestal CONTROL ASSEMBLY - Pedecml LINK - Pedestal contrd brace BRACKET -Pedestal control LINK - Pedestal contrd bracket brace KNOB - Black BEARING -Pedestal control ahaft WASHER - Spring LEVER - Mixture control LEVER - Mixture control LEVER -Mixture control LEVER - Mixture control LEVER -Mixture control LEVER - Mixture control LEVER - Mixture control LEVER - Mixture control LEVER - Propeller control, right LEVER - Propeller contrd, right LEVER -Propeller control, right LEVER - Propeller control, right LEVER - Propeller control, left LEVER - Propeller control, left LEVER - Propeller control, left LEVER - Propeller control, left BEARING - (A306-11) LEVER - Throttle LEVER -Throttle LEVER -Throttle LEVER -Throttle A - U s d with serial nos. 23-1836 t o 23-1839 incl., 23-1841 t o 23-1922 incl., 23-1924.23-1 925.23-1 927.23-1928 and 23-1934 inclusive. B - U s d wiht serial nos. 23-1923.23-1926.23-1929 to 23-1933 and 23-1935 and up. When ordering, always specify Part Number, Deralption and Serial Number of A i r d SERIAL NUMBERS AFFECTED 23-1 t o 23-1501 inclusive 23-502 to 23-1

All Piper PA-23 Apache checklist