AZTEC PARTS CATALOG
Piper PA-23 Aztec · Parts Catalog
Overview
This Parts Catalog is specifically designed for the Piper PA-23-250 Aztec and PA-23-235 Apache models. It provides detailed identification of replacement parts, ensuring that users can accurately order the necessary components for maintenance and repairs. The catalog is organized into major sections, each containing illustrations and parts listings, making it user-friendly for both mechanics and aircraft owners. The document emphasizes the importance of using the correct part numbers and serial numbers when ordering to avoid delays and errors. It also includes information on optional equipment and special tools relevant to these aircraft models.
- The catalog is for Piper PA-23-250 Aztec and PA-23-235 Apache models.
- It includes detailed parts listings with illustrations for easy identification.
- Ordering parts requires specifying the model, serial number, and part number.
- Serial number ranges for each model are provided to ensure correct part ordering.
- A standard paint chart is included for maintenance and restoration.
Document
Source
Originally published by cdn.imagearchive.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.
Document details
- Type
- Parts Catalog
- Year
- 2009
- Pages
- 342
- File size
- 9.9 MB
- Publisher
- cdn.imagearchive.com
Common. Rarer than 17% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the Piper PA-23 Aztec.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins
- Type Certificate (TCDS)
Free — save the PA-23 Aztec 250 to your watchlist and track it in one place.
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- AIRWORTHINESS DIRECTIVE AD/PA-23/46Airworthiness Directives
- SCHEDULE OF AIRWORTHINESS DIRECTIVESAirworthiness Directives
- HEATER INSTALLATION INSTRUCTIONS FOR MODEL CD25K KIT, P/N CD940-25K12 AND CD940-25K24, MODEL CD35K KIT, P/N CD940-35K12 AND CD940-35K24, MODEL CD45K KIT, P/N CD940-45K12 AND CD940-45K24Wiring Diagram
- AZTEC F INFORMATION MANUALTraining Manual
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In this document
Introduction
The introduction outlines the purpose of the Parts Catalog, which is to facilitate the identification of replacement parts for the Piper PA-23-250 and PA-23-235 models. It stresses that the catalog should not be used for rigging and installation purposes and encourages users to familiarize themselves with its layout before use.
Parts Listing Structure
This section explains the format of the parts listings, including columns for figure and index numbers, part numbers, codes, nomenclature, quantity required, and affected serial numbers. It provides an example to illustrate how to interpret the listings, emphasizing the importance of understanding the relationship between parts.
Ordering Parts
Guidelines for ordering parts are provided, including the necessity of specifying the aircraft model and serial number, as well as the part number, name, type, and quantity. It advises users to place orders through authorized distributors and outlines procedures for handling shortages and returns.
Serial Number Information
This section details the serial number ranges for the various models covered in the catalog, including specific ranges for the PA-23-250 and PA-23-235. This information is crucial for ensuring that the correct parts are ordered for the appropriate aircraft.
Standard Paint Chart
The catalog includes a standard paint chart listing various exterior enamel and acrylic lacquer colors along with their corresponding Piper part numbers for both quart and gallon sizes. This is useful for maintenance and restoration purposes.
Safety notes
- This catalog should not be used for rigging and installation purposes.
Full document text
AZTEC PARTS CATALOG CARD 1 OF 3 PA-23-235 APACHE PA-23-250 AZTEC PA-23-250 (Six place) AZTEC PIPER AIRCRAFT CORPORATION (PART NUMBER 753 522) REVISED: JANUARY 10, 2009 1A1 REVISIONS STATUS The information compiled in this Parts Catalog will be kept current by revisions distributed periodically. These revisions will supersede all previous revisions and will be complete card replacements and shall supersede cards of the same number in the set. Current Revisions to this PA-23-235 and PA-23-250 Parts Catalog issued August 15, 1972 are as follows: 753 522 (PR741122)............................................................................Dated November 1974 753 522 (PR750530) .....................................................................................Dated May 1975 753 522 (PR751205)............................................................................Dated December 1975 753 522 (PR761018) ...............................................................................Dated October 1976 753 522 (PR770429) .....................................................................................Dated April 1977 753 522 (PR770902)...........................................................................Dated September 1977 753 522 (PR780906)...........................................................................Dated September 1978 753 522 (PR790205)..............................................................................Dated February 1979 753 522 (PR790816) .................................................................................Dated August 1979 753 522 (PR800314) ..................................................................................Dated March 1980 753 522 (PR801017) ...............................................................................Dated October 1980 753 522 (PR810813) .................................................................................Dated August 1981 753 522 (PR840712)......................................................................................Dated July 1984 753 522 (PR870301) ..................................................................................Dated March 1987 753 522 (IR880415) ......................................................................................Dated April 1988 753 522 (PR071210)......................................................................Dated December 10, 2007 753 522 (PR080610) ..............................................................................Dated June 10, 2008 753 522 (PR080910).....................................................................Dated September 10, 2008 753 522 (PR090110) .........................................................................Dated January 10, 2009 *Piper has ceased production of all Aerofiche (ie. microfiche) products. Parts Catalog subscriptions are available exclusively from Avantext Inc. (www.Avantext.com) on CD-ROM or DVD. The CDs/DVDs include applicable Service Bulletins and Service Letters. PIPER PARTS CATALOG REVISED: JANUARY 10, 2009 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A2 PIPER PARTS CATALOG INTRODUCTION This illustrated Parts Catalog is designed to provide simple but positive identification of replacement parts for the Piper Models PA-23-250. PA-23-250 (Six Place) Aztec. and Model PA-23-235 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 Sections I to X inclusive contain all replacement parts for the complete airplane Each section is subdivided and each division includes 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 parts lists (Refer to EXAMPLE below) a The "FIGURE AND INDEX NUMBER "column indicates the Illustration figure number and its parts Index number EXAMPLE (2-1),the 2 is the figure number and the 1 is the index number The figure number appears only at the top of each parts list page 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 part An explanation of the letter code used is shown on the grid (page) preceding each parts listing and pertains to that listing only 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 The symbol "AR" listed in this column means "As Required" f The "SERIAL NUMBERS AFFECTED" column indicates the part application by airplane serial number Figure EXAMPLE Figure and Part No SERIAL NUMBERS Index Number Code NOMENCLATURE Req AFFECTED Number 2-1 XXXXX-XX DOOR ASSEMBLY - Baggage compartment X -2 XXXXX-XX *TUBE ASSEMBLY - Baggage door latch X -3 XXXXX-XX ** CLEVIS - Door latch tube assembly X -4 XXXXX-XX * * CLIP - Door latch tube assembly X In the Nomenclature column, the next higher assembly relationship of items covered is shown by the degree of indention of each item and is indicated by an asterisk (*) One asterisk signifies one indention, two signifies two indentions, etc The example listing above is interpreted as follows If the DOOR ASSEMBLY (not indented) is ordered, it will include the three items indented under the Door Assembly
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If the TUBE ASSEMBLY (indented one space) is ordered, it will include the two items indented under the Tube Assembly If you want only a CLEVIS 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 This catalog lists for your convenience, those attaching parts required for main assemblies and installations The identifying number for these parts appears after the part 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 JULY 1984 PA-23-250 (Six Place) 1A3 PA-23-250, PA-23-235 SPECIAL NOTE Effective on PA-23-250 (Six Place) with serial numbers 27-7954061 and up, replacement parts for Optional Avionics and Electronics Installations (i.e. radar, radio altimeter, encoding altimeter, etc.) are not being listed or illustrated in this parts catalog. Effective on PA-23-250 (Six Place) with serial numbers 27-8054001 and up, replacement parts for Optional Autopilot Installations are not being listed or illustrated in this parts catalog. If replacement parts are required for aircraft with these serial numbers, refer to the Avionics Drawing Index List and the appropriate drawings supplied with each aircraft to determine part number of desired part. GRID NUMBERING Piper has ceased production of all Aerofiche (i.e., microfiche) products. The Aerofiche grid numbers will be removed in the next complete revision. In the interim, as partial revisions occur, the Aerofiche grid numbering system may be modified, as explained below, to simplify production. Deviations from the legacy Aerofiche grid numbering system will occur when it becomes necessary to add pages to the manual and will typically take two forms: A. Inserting pages between two existing grids in the same row. When inserting two pages between the existing grids 1A8 and 1A9, the two new pages will be numbered 1A8A and 1A8B. B. Inserting pages at the end of an Aerofiche grid row. The legacy Aerofiche grid numbering system limited page numbers in a row to a maximum of 24 (i.e., row 1A would be numbered 1A1- 1A24). That limit no longer applies. Accordingly, if two pages need to be added between any existing grid row end and grid row start (ie., 1A24 and 1B1), the new pages will simply be numbered 1A25 and 1A26. HOW TO IDENTIFY A PART IF YOU KNOW WHAT IT LOOKS LIKE AND KNOW WHERE IT IS LOCATED 1. Refer to Figure 1 to determine the Section number in which the part is used. 2. Refer to the Table of Contents and 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 to identify and proceed to the grid (page) specified. 3. Find the part on the illustration and note the index number. NOTE: If you don’t find the part on this illustration, try another figure in this group. 4. Refer to the ‘’Figure and Index Number’’ in the Parts Listing for complete description of the part. HOW TO ORDER PARTS In ordering parts for your Piper airplane, observe 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, express, 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. Shortages All 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 (3) days after receipt of orders. b. Returned Goods No material should be returned to 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 see fit. Transportation charges must be PREPAID on returned goods or the shipment will be refused. c. Transportation Liabilities The Piper Aircraft Corporation cannot be held liable for damages to parts in transit from the factory. If a shipment is received in a dam- aged condition, have the delivery man or Transportation Company make a notation of the damage and file your claim with the Carrier. In case of concealed damage, do not attempt to remove the part from the shipping container, or endeavor to repair the damage, but call the Carrier and have his Claim Agent inspect the damage before filing your claim with the Carrier. PIPER PARTS CATALOG REVISED: JANUARY 10, 2009 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A4 PIPER PARTS CATALOG PA-23-235. PA-23-250AND PA-23-250(SIX PLACE)SERIALNUMBERINFORMATION The following information should be kept in mind when ordering from this Catalog: a The serial numbersof the aircraft coveredby this PartsCatalogare as follows: (1) Serial numbersof the 1960 "Aztec" PA-23-250 Modelsare 27-1 to 27-366 inclusive (2) Serial numbersof the 1961 "Aztec" PA-23-250Models are 27-367 to 27-504 inclusive (3) Serial numbersof the "Apache" PA-23-235 Modelsare 27-505 to 27-622 inclusive (4) Serial numbersof the "Aztec" PA-23-250(Six Place)Model "B" are 27-2000 to 27-2504 inclusive. (5) Serial numbersof the "Aztec" PA-23-250(Six Place)Model "C" are 27-2505 to 27-3836 inclusive,27-3838 to 27-3943 inclusive (6) Serial numbersof the "Aztec" PA-23-250(Six Place)Model "D" are 27-3837. 27-3944 to 27-4425 inclusive,27-4427to 27-4573 inclusive (7) Serial numbersof the "Aztec" PA-23-250(Six Place)Model "E" are 27-4426. 27-4574 to 27-7554168 inclusive (8) Serial numbersof the "Aztec" PA-23-250(Six Place)Model "F" are 27-7654001 and up REVISED:SEPTEMBER1978 1A5 PA-23-250(Six Place) PA-23-250 PA-23-235 PIPERPARTSCATALOG STANDARDPAINTCHART MFG. PIPERPARTNUMBER NO. QUART GALLON EXTERIOR ENAMEL Daytona White J-9545 751 700 751 701 Santa Fe Red H-9150 751 712 751 713 Bahama Blue H-9170 751 714 751 715 Hershey Brown H-9160 751 716 751 717 Montego Green F-5830 751 718 751 719 Yukon Yellow W-0232 751 720 751 721 Pontiac Red W-3665 754716 754717 Phoenix Tan W-3557 754 718 754 719 Orlando Green W-3680 754 720 754 721 Lakeland Blue W-3554 754 722 754 723 Dakota Black H-6117 754 710 754 711 El PasoBrown W-8433 754 737 754 738 TampaGreen W-8427 754 739 754 740 Newport Blue W-8430 754 741 754 742 ACRYUCLACQUER Daytona White 890-910 4175 650 1175 650 Pontiac Red 8954 4175 590 1175 590 Phoenix Tan 890-908 4175 625 1175 625 Orlando Green 8981 4175 206 1175 206 Lakeland Blue 8979 4175 753 1175 753 Dakota Black 8906 4175 375 1175 375 El PasoBrown 893-62885 4175 403 1175 403 Tampa Green(base coat) 8998 4175 208 1175 208 Tampa Green(top coat) 8997 4175 207 1175 207 Newport Blue(base coat) 8988 4175 756 1175 756 Newport Blue(top coat) 8991 4175 755 1175 755 Juneau White L8973 4175 655 1175 655 Mocha Tan 8985 4175 750 1175 750 Denver Brown (base coat) 8989 4175 297 1175 297 Denver Brown (top coat) 8977 4175 298 1175 298 Madrid Red (basecoat) 8276 4175 131 1175 131 Madrid red (top coat) 8910 4175589 1175589 Lincoln Gray 8987 4175 205 1175 205 Bimini Turquoise 8992 4175 752 1175 752 NassauTurquoise 8978 4175 751 1175 751 Reno Gold (basecoat) 8976 4175 343 1175 343 Reno Gold (top coat) 8974 4175 342 1175 342 Beaumont Blue 8993 4175 754 1175 754 Dallas Yellow 8975 4175 702 1175 702 Ocala Orange(basecoat) 8909 4175 503 1175 503 Ocala Orange(top coat) 8907 4175 502 1175 502 Polar Gray 8986 4175 204 1175 204 Monterey Maroon (base coat) 8908 4175 758 1175 758 Monterey Maroon (top cost) 8904 4175757 1175757 Bahama Blue 8911 4175442 1175442 Las Vegas Gold(base coat) 8931 4175327 1175327 Las Vegas Gold (top coat) 8929 4175 328 1175 328 Avocado 8955 4175 209 1175 209 REVISED:MARCH1980 PA-23-250 (Six Place) 1A6 PA-23-250, PA-23-235 STANDARD PAINT CHART MFG. PIPER PART NUMBER NO. QUART GALLON EXTERIOR ACRYLIC LACQUER (cont.) Baja Yellow (base coat) 8212 4175 704 1175 704 Baja Yellow (top coat) 8209 4175 703 1175 703 Lime Green (base coat) 8211 4175 214 1175 214 Lime Green (topcoat) 8210 4175 213 1175 213 Saffron 8228 4175 385 1175 385 Claret (base coat) 8250 4175 397 1175 397 Claret (top coat) 8223 4175 381 1175 381 Firethorn (base coat) 8247 4175 396 1175 396 Firethorn (top coat) 8246 4175 384 1175 384 Dark Blue 8230 4175 387 1175 387 Sage Green 8226 4175 383 1175 383 Buckskin 8229 4175 386 1175 386 Hickory Brown 8231 4175 388 1175 388 Silver 8224 4175 382 1175 382 Sandalwood Tan 8271 4175 215 1175 215 Platinum Gray 8270 4175 216 1175 216 -Thinner (fast drying) Titanine 8930 4179 138 1179 138 -Thinner (slow drying) Titanine 8970 4179 134 1179 134 POLYURETHANE ENAMEL (Titanine) Flat Black 6325 4170 900 1170 900 Juneau White 6373 4170 901 1170 901 Claret 6339 4176 011 1176 011 Silver 6341 4176 012 1176 012 Sage Green 6345 4176 013 1176 013 Firethorn 6347 4176 014 1176 014 Saffron 6358 4176 015 1176 015 Buckskin 6385 4176 016 1176 016 Dark Blue 6386 4176 017 1176 017 Hickory Brown 6387 4176 018 1176 018 Sandalwood Tan 6818 4176 019 1176 019 Dakota Black 6306-N 4176 181 1176 181 Las Vegas Gold 6328-N 4177 000 1177 000 Lime Green 6326 4177 029 1177 029 Platinum Gray 6817 4177 030 1177 030 Bahama Blue 6348-N 4177 260 1177 260 MadridRed 6310-N 4177 386 1177 386 Baja Yellow 6327 4177 454 1177 454 Ocala Orange 6307-N 4175 575 1177 575 -Catalyst 6352 4170 807 1170 807 -Reducer 6350 4179 141 1179 141 POLYURETHANE PRIMER (Titanine) Primer 6351 4170 735 1170 735 Reducer 6350 4179 141 1179 141 Catalyst 6352 4170 807 1170 807 Epoxy Primer 8951 4170 729 1170 729 Epoxy Reducer 8905-A 4179 139 1179 139 Epoxy Converter 8678 4179 825 1179 825 COLOR PAINT (For Thermoplastic Interior Trim Panels Only) AVAILABLE IN 16-OUNCE AEROSAL CANS Avocado Green 766-007 White 766-008 Tan 766-009 Red 766-010 Dark Blue 766-011 Light Blue 766-012 Sandstone 766-013 Gloss Black 766-014 Dark Brown 766-015 Brown 766-016 Blue-Green 766-017 Optical Flat Black 766-018 PIPER PARTS CATALOG REVISED: DECEMBER 10, 2007 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A7 TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER 1 View of Complete Airplane .......................................................................................................................1A13 SECTION I WING GROUP 2 Wing Installation .......................................................................................................................................1A14 2A Flap Assembly and Aileron Assembly ......................................................................................................1A19 3 Wing and Wing Tip Construction ..............................................................................................................1B1 4 Wing and Wing Tip Skin ...........................................................................................................................1B8 SECTION ll FUSELAGE GROUP 5 Complete Fuselage ..................................................................................................................................1B12 6 Fuselage Forward Section (PA-23-235, PA-23-250)................................................................................1B15 6A Fuselage Forward Section (PA-23-250(6)................................................................................................1C1 7 Fuselage Center Section..........................................................................................................................1C11 7A Fuselage Bottom Fairing ..........................................................................................................................1C18 8 Fuselage Aft Section ................................................................................................................................1D1 9 Fuselage Frame .......................................................................................................................................1D9 10 Instrument Panel Installation (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl., 27-3838 to 27-3943 incl.) .................................................................................................................1D13 10A Instrument Panel Installation (PA-23-250(6) S/N 27-3837, 27-3944 to 27-7305221 incl., 27-7305223 to 27-7305234 incl.).................................................................................1E1 10B Instrument Panel Installation (PA-23-250(6) S/N 27-7305222, 27-7405235 to 27-7405476 incl.)......................................................................................................................................1E11 10C Instrument Panel Installation (PA-23-250(6) S/N 27-7554001 and up)....................................................1E 16 10D Dual Instrument Panel Installation (PA-23-250(6) S/N 27-7405235 to 27-7405476 incl.)......................................................................................................................................1E21 10E Dual Instrument Panel Installation (PA-23-250(6) S/N 27-7554001 and up) ...........................................1F1 10F Dual Instrument Lines and Right Pitot Static System Installation.............................................................1F4 11 Control Pedestal Installation.....................................................................................................................1F6 12 Floorboard and Cockpit Finishing Installation (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl., 27-3838 to 27-3943 incl.)...............................................................................................1G1 12A Cockpit Finishing Installation (PA-23-250(6) S/N 27-3837, 27-3944 and up) ..........................................1H1 12B Floorboard Installation (PA-23-250(6) S/N 27-3837, 27-3944 and up) ....................................................1H11 13 Window Curtains Installation ....................................................................................................................1H15 14 Fuselage Enclosure Installation ...............................................................................................................1I1 15 Baggage Door Assembly and Cabin Door Assembly (PA-23-235/250/250(6) S/N 27-1 to 27-7554168 incl.) .........................................................................................................................1I9 15A Baggage Door Assembly and Cabin Door Assembly (PA-23-250(6) S/N 27-7654001 and up) .................................................................................................................................1I18 16 Oxygen System Installation (PA-23-250) .................................................................................................1I22 16A Oxygen System Installation (PA-23-250(6) S/N 27-2000 to 27-3049 incl., 27-3051 to 27-3153 incl.) .........................................................................................................................1J1 16B Oxygen System Installation (PA-23-250(6) S/N 27-3050, 27-3154 to 27-3836 incl., 27-3838 to 27-3943 incl.) .................................................................................................................1J4 16C Oxygen System Installation (PA-23-250(6) S/N 27-3837, 27-3944 and up) ............................................1J7 17 Seats Installation (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl., 27-3838 to 27-3943 incl.)........................................................................................................................................1J10 17A Seats Installation (PA-23-250(6) S/N 27-3837, 27-3944 to 27-7554168 incl.) .........................................1K1 17B Seats Installation (PA-23-250(6) S/N 27-7654001 and up)......................................................................1K10 PIPER PARTS CATALOG REVISED: DECEMBER 10, 2007 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A8 TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER SECTION ll (cont.) FUSELAGE GROUP 18 Vacuum Pump Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ........................................1K15 18A Vacuum Pump Installation (PA-23-250(6) S/N 27-2505 and up) .............................................................1K20 19 Airspeed, Static, Oil Pressure and Manifold Pressure Lines ....................................................................1L1 20 Ventilating System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.)..................................1L6 20A Ventilating System Installation (PA-23-250(6) S/N 27-2505 to 27-3836 incl., 27-3838 to 27-3943 incl.) .........................................................................................................................1L9 20B Ventilating System Installation (PA-23-250(6) S/N 27-3837, 27-3944 and up) ........................................1L12 21 Heater Installation (PA-23-235/250/250(6) S/N 27-1 to 27-3049 incl., 27-3051 to 27-3153 incl.)........................................................................................................................................1L14 21A Heater Installation (PA-23-250(6) S/N 3050, 27-3154 and up) ................................................................1L18 22 Heater Assembly (Stewart Warner)..........................................................................................................1L22 22A Janitrol Heater Assembly .........................................................................................................................2A6 22B Janitrol Heater Components.....................................................................................................................2A10 SECTION lll CHASSIS GROUP 23 Gear Strut Assemblies .............................................................................................................................2A13 24 Nose Gear Installation ..............................................................................................................................2A16 24A Nose Wheel Assembly .............................................................................................................................2A21 25 Main Gear Installation ..............................................................................................................................2B1 26 Main Wheel Assembly ..............................................................................................................................2B5 27 Brake Installation. .....................................................................................................................................2B7 27A Dual Brake Installation .............................................................................................................................2B10 28 Brake Assembly .......................................................................................................................................2B13 SECTION IV TAIL SURFACES GROUP 29 Tail Surfaces Installation ..........................................................................................................................2B16 29A Stabilator Assembly (PA-23-235/250/250(6) S/N 27-1 to 27-7554168 incl., 27-8054001 and up) .................................................................................................................................2B20 29B Stabilator Assembly (PA-23-250(6) S/N 27-7654001 to 27-7954121 incl.) ..............................................2B22 29C Rudder Assembly .....................................................................................................................................2C1 29D Fin Assembly. ...........................................................................................................................................2C4 SECTION V POWER PLANT GROUP 30 Power Plant Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ............................................2C7 30A Power Plant Installation (PA-23-250(6) S/N 27-2505 and up)..................................................................2C10 30B Turbocharger Installation (Airesearch) .....................................................................................................2C15 30C Turbocharger Installation (Lycoming) .......................................................................................................2C17 31 Propeller (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ...................................................................2C22 31A Propeller (PA-23-250(6) S/N 27-2505 and Up) ........................................................................................2D1 31B Propeller Synchronizer System Installation ..............................................................................................2D5 31C Propeller Synchrophaser System Installation...........................................................................................2D7 32 Engine Baffle Installation..........................................................................................................................2D9 PIPER PARTS CATALOG REVISED: JUNE 10, 2008 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A9 PIPER PARTS CATALOG TABLEOF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER SECTION V (cont.) POWER PLANT GROUP 33 Exhaust Collectors Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl )....... 2D12 33A Exhaust System Installation (PA-23-250(6) S/N 27-2505 and up) ........................ 2D14 34 Nacelle Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ................. 2D16 34A Nacelle Installation (PA-23-250(6) S/N 27-2505 and up) ................... ............. 2E1 34B Nacelle Installation (Lycoming Turbocharger) ........................................... 2E8 SECTION VI FUEL SYSTEM GROUP 35 Fuel System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl )............. 2E13 35A Fuel Injection System Installation (PA-23-250(6) S/N 27-2322 to 27-2504 incl ) .......... 2F1 35B Fuel System Installation (PA-23-250(6) S/N 27-2505 and up) ............................ 2F5 36 Fuel Cell Installation (PA-23-235/250/250(6) S/N 27-1 to 27-4815 incl ) ............... 2F11 36A Fuel Cell Installation (PA-23-250(6) S/N 27-4816 and up) ............................... 2F15 36B Wing Tip Fuel Tank Installation (PA-23-250(6) S/N 27-7654001 and up) ......... ........ 2F18 37 Fuel System Control Box (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl) ........... . 2F20 37A Fuel System Control Box (PA-23-250(6) S/N 27-2505 and up) .......................... 2G1 SECTION VI) ELECTRICALSYSTEM GROUP 38 Fuselage Electrical System Installation (PA-23-235/250) ................................ 2G4 38A Fuselage Electrical System Installation (PA-23-250(6) ................................... 2G7 38B Wing Electrical System Installation (PA-23-235/250) ................................... 2G13 38C Wing Electrical System Installation (PA-23-250(6) ....................................... 2G16 38D Battery Box Installation (PA-23-235/250) .............................................. 2G20 38E Battery Box Installation (14-Volt) (PA-23-250(6) ......................................... 2G22 38F Battery Box Installation (28-Volt) (PA-23-250(6) S/N 27-2298 to 27-7954097 incl ) ....... 2H1 38G Battery Box Installation (28-Volt) (PA-23-250(6) S/N 27-7954098 and up) ......... ....... 2H4 39 Pedestal Electrical Installation ......................................................... 2H6 39A Instrument Panel Electrical Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl ) ............................. ..................................... 2H9 398 Instrument Panel Electrical Installation (PA-23-250(6) S/N 27-2505 to 27-3836 incl, 27-3838 to 27-3943 incl )........................................................ 2H13 39C Instrument Panel Electrical Installation (PA-23-250(6) S/N 27-3837, 27-3944 and up) .... 2H16 40 Taxi Light Installation ............................ ......................... 2H20 40A Strobe Lights Installation .............................................................. 2H22 41 External Power Supply (PA-23-235/250/250(6) S/N 27-1 to 27-7954097 incl) .......... 211 41A External Power Supply (PA-23-250(6) S/N 27-7954098 and up) ......................... 214 42 Propeller Deicer Installation (PA-23-250) ............................................... 216 42A Propeller Deicer Installation (PA-23-250(6) ............ ................................. 218 42B Pneumatic Deicer Installation (B F. Goodrich) ......................................... 2111 42C Pneumatic Deicer Installation (B F Goodrich) ...................................... .... 2117 42D Pneumatic Deicer Installation (Airborne/Goodyear) (PA-23-250(6) S/N 27-7554112 to 27-7554168 incl ) ......... ...................... ............... 2121 REVISED JULY 1984 1A10 PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER SECTION VIII HYDRAULIC SYSTEM GROUP 43 Hydraulic System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ........ 2J1 43A Fuselage Hydraulic System Installation (PA-23-250(6) S/N 27-2505 and up).............. 2J7 43B Wing Hydraulic System Installation (PA-23-250(6) S/N 27-2505 and up) ............. .... 2J 1 43C Hydraulic System Components (PA-23-250(6) S/N 27-2505 and up) ..................... 2J14 44 Landing Gear Anti-Retraction Valve Installation ......................................... 2J18 45 Hydraulic Powerpak Components ...................................................... 2J20 45A Hydraulic Powerpak Components ...................................................... 2K1 46 Emergency Gear Extender Installation (PA-23-235/250/250(6) S/N 27-1 to 27-7954121 incl ) ............. .............................................. 2K4 SECTION IX CONTROL SYSTEM GROUP 47 Engine Controls Installation ........................................................... 2K7 48 Stabilator Control Installation ......... ......................................... . 2K10 49 Aileron Controls Installation ........................................................... 2K13 50 Rudder Control Installation ......... .................. ......................... 2K16 51 Tail Trim Mechanism Installation ....... ............................. ............... 2K19 51A Trim Tab Interconnect System Installation ...................... ................. 2L1 SECTION X ELECTRONICSGROUP 52 Collins and ARC Radio Installation ..................................................... 3A5 53 Radio Junction Boxes (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl, 27-3838 to 27-3943 incl ) ......... .. ............ ...................................... 3A9 54 Radio Junction Boxes (PA-23-250(6) S/N 27-3837. 27-3944 to 27-4784 incl )............ 3A13 54A Radio Junction Boxes (14-Volt) (PA-23-250(6) S/N 27-4785 and up) ..................... 3A15 54B Radio Junction Boxes (28-Volt) (PA-23-250(6) S/N 27-4902 and up) ..................... 3A17 55 - All Weather Antenna Installation ...................................................... 3A19 55A Piper Automatic Locator (ELT) Installation (Garrett Mfg. Ltd) ............................. 3A21 55B Piper Automatic Locator (ELT) Installation (Communications Components Corp ) ........... 3A23 55C Piper Automatic Locator (ELT) Installation (Narco Avionics) ............................... 3B1 56 Piper PM-1 Marker Beacon Installation (PA-23-250(6) ................................... 3B3 57 AutoControl I Installation .............................................................. 3B6 58 AutoControl II Installation ............................................................. 3B9 59 AutoControl III Installation (PA-23-250(6) S/N 27-3457 to 27-7554071 incl.) ............. 3B12 59A AutoControl III B Installation (PA-23-250(6) S/N 27-7554071 and up) .................... 3B14 60 AltiMatic I Installation ................................................................ 3B16 61 AltiMatic II Installation ............................. ................................... 3B19 61A AltiMatic III and III B Installation ....................................................... 3C1 62 AltiMatic III B-1 Installation ........................................................... 3C5 63 AltiMatic III C Installation (PA-23-250(6) S/N 27-7554001. 27-7554074 and up).......... 3C8 64 AltiMatic X F/D Autopilot Installation (PA-23-250(6) S/N 27-7854001 and up) ........... 3C12 65 AltiMatic X Autopilot Installation (PA-23-250(6) S/N 27-7854001 and up) ................ 3C15 66 AltiMatic V F/D and V F/D-1 Autopilot Installation (PA-23-250(6) S/N 27-4426, 27-4574 to 27-4574 to 27-7754093 incl.) ............................ ........................ 3C18 67 AltiMatic V and V-1 Autopilot Installation (PA-23-250(6) S/N 27-4426. 27-4574 to 27-7754093 incl ) .................................................................... 3D1 REVISED JULY 1984 1All PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG TABLEOF CONTENTS FIGURENUMBER FIGURETITLE GRIDNUMBER SECTIONX (cont) ELECTRONICS GROUP 68 69 69A 70 71 72 73 74 75 Autopilot/Flight Director Installation(BendixFCS-810)(PA-23-250(6)S/N 27-7754094to 27-7954121 incl) ............................ ......................... Autopilot Installation(BendixFCS-810)(PA-23-250(6)S/N 27-7754094 to 27-7954121 inc ) .................................................................. King Autopilot (KAP-200)and King Autopilot F/D (KFC-200)Installation .................. RadarAltimeter Installation (PA-23-250(6)S/N 27-4794 and up) ........................ Glide SlopeCoupler Installation(PA-23-250(6)S/N 27-7554001. 27-7554074 and up) ... ............................................... ........................... RadioMagnetic Indicator Installation(PA-23-250(6)S/N 27-4426, 27-4574 and up) ...... King RadarInstallation (KWX-40)(PA-23-250(6)S/N 27-7554001 and up) ............... BendixRadar Installation(RDR-150)(PA-23-250(6)S/N 27-7754001 and up)............. EncodingAltimeter Installation (PA-23-250(6)S/N 27-7554001 and up).................. RadioInstallation and Wiring DiagramDrawings ......... ............................. 3D5 3D8 3011 3D13 3D15 3D17 3D19 3D21 3E1 3E3 SECTIONXI MISCELLANEOUSGROUP Optional EquipmentKits, RepairKits and SpecialTools............. ................. 3E12 Decals................................................................ 3E18 NUMERICALINDEX 1A12 3F2 PA-23-250 (Six Place) PA-23-250, PA-23-235 REVISEDJULY 1984 WING P I P E R A I R C R A FT C O R P O R A T I O N II FUSELAGE IV X ELECTRONICS VIIELECTRICAL SYSTE -XI MISCELLANEOUS SYSTEM III -V POWER PLANT VIIIIIYDRAULIUC Figure 1. View of Complete Airplane 1A13 REVISED: OCTOBER 1976 PA-23-250(SixPlace) PA-23-250. PA-23-235 PIPER PARTS CATALOG -25 31-32-33 0 Figure 2 Wing Installation 1A14 REVISED:FEBRUARY1979 PA-23-250 (Six Place) PA-23-250. PA-23-235 PIPER PARTS CATALOG REVISED: SEPTEMBER 10, 2008 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A15 Figure and Index Number Part Number Code NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED SECTION I WING INSTALLATION Wing Group 2- 16292 X,Z DRAWING - Wing Installation 30698 Y DRAWING - Wing Installation 27-2000 to 27-4815 inclusive 33304 Y DRAWING - Wing Installation 27-4816 to 27-7554168 incl. 33900 Y DRAWING - Wing Installation 27-7654001 and up 16662 DRAWING - Wing Fairing Installation 27-1 to 27-3888 inclusive 32717 Y DRAWING - Wing Fairing Installation 27-3889 and up -1 16170-00 A,C,X PANEL ASSEMBLY - Left wing 1 16170-01 A,C,X PANEL ASSEMBLY - Right wing 1 16170-00 A,C,Z PANEL ASSEMBLY - Left wing 1 27-505 to 27-524 inclusive 16170-01 A,C,Z PANEL ASSEMBLY - Right wing 1 27-505 to 27-524 inclusive 16170-30 A,Z PANEL ASSEMBLY - Left wing 1 27-525 and up 16170-29 A,Z PANEL ASSEMBLY - Right wing 1 27-525 and up 16170-26 A,B,Y PANEL ASSEMBLY - Left wing 1 27-2000 to 27-2269 inclusive 16170-25 A,B,Y PANEL ASSEMBLY - Right wing 1 27-2000 to 27-2269 inclusive 16170-28 A,Y PANEL ASSEMBLY - Left wing 1 27-2270 to 27-2504 inclusive 16170-27 A,Y PANEL ASSEMBLY - Right wing 1 27-2270 to 27-2504 inclusive 16170-32 A,Y PANEL ASSEMBLY - Left wing 1 27-2505 to 27-4815 inclusive 16170-31 A,Y PANEL ASSEMBLY - Right wing 1 27-2505 to 27-4815 inclusive 33300-00 A,Y PANEL ASSEMBLY - Left wing 1 27-4816 to 27-7554168 incl. 33300-01 A,Y PANEL ASSEMBLY - Right wing 1 27-4816 to 27-7554168 incl. 33300-06 A,Y PANEL ASSEMBLY - Left wing 1 27-7654001 and up 33300-07 A,Y PANEL ASSEMBLY - Right wing 1 27-7654001 and up -2 17477-00 STRAP - Spar attachment, lower rear 1 27-2000 to 27-2299 inclusive 17477-03 STRAP - Spar attachment, lower rear 1 27-2300 and up -3 17477-02 STRAP - Spar attachment, lower front 1 -4 18283-00 SHIM - Spar attachment AR -5 17476-02 STRAP - Spar attachment, upper front 1 -6 401 189 BOLT - (AN5-11A) 4 -6a 401 188 BOLT - (AN5-10A) 4 -7 404 889 NUT - SeIf locking (MS20365-524C) 14 -8 400 452 BOLT - (AN3-11A) 4 -9 404 887 NUT - SeIf locking (MS20365-1032C) 10 -10 19459-02 X,Z SHIM - Main spar attachment, front .187 1 19459-03 X,Z SHIM - Main spar attachment, rear .125 1 19303-00 Y SHIM - Main spar attachment, .313 1 -11 401 269 BOLT - (AN3-10A ) 6 -12 690 612 WASHER - (NAS1149F0363P) 6 -13 401 365 BOLT- (AN5-26A) 2 -14 17475-04 X,Z PLATE - Front spar attachment, bottom 1 17475-06 Y PLATE - Front spar attachment, bottom 1 -15 17475-05 PLATE - Front spar attachment, top 1 -16 400 444 BOLT - (AN6-13A) 16 -17 401 395 BOLT- (AN6-14A) 16 -18 690 629 WASHER - (NAS1149F0663P) 32 -19 404 890 NUT - (AN365-624C) 32 A - See Figures 3 and 4 for component parts. B - If Kit No. 754 493 has been installed, order wing panel 16170-28 left or 16170-27 right. C - If Kit No. 754 493 has been installed, order wing panel 16170-30 left or 16170-29 right. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place) airplanes only. Z - Used on PA-23-235 airplanes only. When ordering, always specify Part Number, Description, and Serial Number of Aircraft PIPER PARTS CATALOG REVISED: SEPTEMBER 10, 2008 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A16 Figure and Index Number Part Number Code NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED WING INSTALLATION SECTION I Wing Group 2-20 16296-00 X,Z BLOCK - Front spar spacer, top 2 30697-00 Y BLOCK - Front spar spacer, top 2 -20a 61402-09 BUSHING - Front spar spacer, top 2 -21 17694-06 X,Z BLOCK - Front spar spacer. front left top 1 30696-00 Y BLOCK - Front spar spacer, front left top 1 -22 17694-05 X,Z BLOCK - Front spar spacer, front right top 1 30696-01 Y BLOCK - Front spar spacer, front right top 1 -23 401 332 X,Z BOLT- (AN4-34A) 2 401 335 Y BOLT- (AN4-40A) 2 401 336 Y BOLT- (AN4-37A) 2 -24 690 611 WASHER - (NAS1149F0463P) 2 -25 404 888 NUT - self locking (AN365-428) 2 -25a 80122-87 BUSHING - Rear spar attachment AR -26 17480-00 BLOCK - Front spar side attachment spacer 4 -27 401 363 BOLT- (AN5-24A) 2 -28 400 168 BOLT- (AN5-25) 2 -29 690 628 WASHER - (NAS1149F0563P) 4 -30 17529-04 PIN - Wing tip hinge 2 27-1 to 27-7554168 inclusive 15514-02 PIN - Wing tip hinge 2 27-7654001 and up -31 18380-02 SHIM- (.020) AR -32 18380-03 SHIM - (.032) AR -33 18380-04 SHIM- (.064) AR -34 402 350 BOLT - Rear spar attachment (AN176-10A) 2 -35 690 629 WASHER - (NAS1149F0663P) 2 -36 404 889 NUT - self locking (MS20365-624C) 2 -37 18166-06 FAIRING ASSEMBLY - Left wing root, upper 1 18166-07 FAIRING ASSEMBLY - Right wing root, upper 1 -38 19795-00 EXTRUSION - Rubber 5 -39 16574-00 FAIRING ASSEMBLY - Left wing root, upper (Aluminum) 1 27-1 to 27-3888 inclusive 16574-01 FAIRING ASSEMBLY - Right wing root, upper (Aluminum ) 1 27-1 to 27-3888 inclusive 32464-00 Y FAIRING ASSEMBLY - Left wing root, upper (Fiberglas) 1 27-3889 and up 32464-01 Y FAIRING ASSEMBLY - Right wing root, upper (Fiberglas) 1 27-3889 and up -40 19795-00 EXTRUSION - Rubber 7’ -41 16659-00 FAIRING ASSEMBLY - Left wing root, lower 1 16659-01 FAIRING ASSEMBLY - Right wing root, lower 1 -42 19795-00 EXTRUSION - Rubber 6’ -43 18176-00 PLATE - Wing front spar bolt cover 2 -44 18128-00 PLATE - Left wing root rear fairing 1 18129-00 PLATE - Right wing root rear fairing 1 -45 18130-00 FAIRING ASSEMBLY - Left wing root rear 1 18131-00 FAIRING ASSEMBLY - Right wing root rear 1 -46 18457-00 RING - Tie down 2 -47 410 044 SCREW - (AN509-10R-15) 4 -48 17100-00 A AILERON ASSEMBLY- Left wing 1 17100-01 A AILERON ASSEMBLY - Right wing 1 A - See Figure 2A for component parts. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place) airplanes only. Z - Used on PA-23-235 airplanes only. When ordering, always specify Part Number, Description, and Serial Number of Aircraft SECTION I Wing Group WING INSTALLATION Figure and Index Number 2-49 Part Number Code PIPER PARTS CATALOG No NOMENCLATURE Req SERIAL NUMBERS AFFECTED 17104-40 A,B FLAP ASSEMBLY - Left wing 17104-01 A.B FLAP ASSEMBLY - Right wing 17104-58 A,B,Y FLAP ASSEMBLY - Left wing 17104-57 A.BY FLAP ASSEMBLY - Right wing 17104-60 A,B.Y FLAP ASSEMBLY - Left wing 17104-59 A,B.Y FLAP ASSEMBLY- Right wing 1 27-1 to 31-2504 inclusive 1 27-1 to 27-2504 inclusive 1 27-2505 to 27-3049 inclusive. 27-3051 to 27-3153 inclusive 1 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 1 27-3050, 27-3154 to 27-7405300 inclusive 1 27-3050. 27-3154 to 27-3784 inclusive 1 27-3785 to 27-7405300 incl 1 27-7405301 and up 1 27-7405301 and up 4 27-1 to 27-7554168 inclusive 17104-65 17104-68 17104-69 -50 81172-70 -51 415535 -52 16617-00 16617-01 16617-08 16617-09 32466-00 32466-01 -53 16777-00 16777-01 32471-00 32471-01 -54 80012-94 -55 401 310 -56 400 008 -57 404 888 -58 17531-00 17531-01 17531-00 17531-01 17531-40 17531-41 17531-00 17531-01 17531-40 17531-41 17531-46 17531-47 34282-00 34282-01 34282-14 34282-15 A,B,Y FLAP ASSEMBLY - Right wing A.Y FLAP ASSEMBLY - Left wing A.Y FLAP ASSEMBLY - Right wing LUG - Wing tip attaching SCREW - Truss head machine (MS35206-245) FAIRING ASSEMBLY - Nacelle inboard, left (aluminum) FAIRING ASSEMBLY - Nacelle inboard, right (aluminum) Y FAIRING ASSEMBLY - Nacelle inboard, left (aluminum) Y FAIRING ASSEMBLY - Nacelle inboard. right (aluminum) Y FAIRING ASSEMBLY - Nacelle inboard, left (fiberglass) Y FAIRING ASSEMBLY - Nacelle inboard, right (fiberglass) FAIRING ASSEMBLY - Nacelle outboard, left (aluminum) FAIRING ASSEMBLY - Nacelle outboard, right (aluminum) Y FAIRING ASSEMBLY - Nacelle outboard, left (fiberglass) Y FAIRING ASSEMBLY - Nacelle outboard, right (fiberglass) BUSHING - Aileron center hinge BOLT - (AN4-10A) BOLT - (AN4-13A) NUT - Self locking (MS20365-428C) C.D.X TIP ASSEMBLY - Left wing C.D,X TIP ASSEMBLY - Right wing C.D.Z TIP ASSEMBLY - Left wing C.D,Z TIP ASSEMBLY - Right wing C,Z TIP ASSEMBLY - Left wing C.Z TIP ASSEMBLY - Right wing C.D.Y TIP ASSEMBLY - Left wing C.D.Y TIP ASSEMBLY - Right wing C.Y TIP ASSEMBLY - Left wing C.Y TIP ASSEMBLY - Right wing C.Y TIP ASSEMBLY - Left wing C.Y TIP ASSEMBLY - Right wing CY TIP ASSEMBLY - Left wing C.Y TIP ASSEMBLY - Right wing C.Y TIP ASSEMBLY - Left wing C.Y TIP ASSEMBLY - Right wing 58 1 1 1 1 1 1 1 1 1 1 4 4 8 6 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 to 27-3888 inclusive 27-2505 to 27-3888 inclusive 27-3889 and up 27-3889 and up 27-1 to 27-3888 inclusive 27-1 to 27-3888 inclusive 27-3889 and up 27-3889 and up 27-505 to 27-524 inclusive 27-505 to 27-524 inclusive 27-525 and up 27-525 and up 27-2000 to 27-2269 inclusive 27-2000 to 27-2269 inclusive 27-2270 to 27-4815 inclusive 27-2270 to 27-4815 inclusive 27-4816 to 27-7554168 inclusive 27-4816 to 27-7554168 inclusive 27-7654001 to 27-7954087 Incl 27-7654001 to 27-7954087 incl 27-7954088 and up 27-7954088 and up A - See Figure 2A for component parts B - When ordering new Flap Assembly, ascertain part number stamped on identification plate attached to outboard rib Reorder the Flap Assembly of same part number C - See Figure 4 for component parts D - If Kit No 754 493 is used. order tip 17531-40 left or 17531-41 right X - Used on PA-23-250 airplanes only Y - Used on PA-23-250 (Six Place) airplanes only Z - Used on PA-23-235 airplanes only When ordering, always specify Part Number. Description and Serial Number of Aircraft REVISED OCTOBER 1980 1A17 PA-23-250 (Six Place) PA-23-250. PA-23-235 PIPER PARTS CATALOG REVISED: SEPTEMBER 10, 2008 PA-23-250 (Six Place) PA-23-250, PA-23-235 1A18 Figure and Index Number Part Number Code NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED WING INSTALLATION SECTION I Wing Group 2-59 80122-68 WASHER - Flap inboard and center hinge 8 -60 17125-00 BLOCK - Aileron balance (Wt 3 lb 8 oz ) 2 17125-02 BLOCK - Aileron balance (Wt 3 lb 13 oz ) 2 -61 690 611 WASHER - (NAS1149F0463P) 2 -62 404 888 NUT - self locking (MS20365 428C) 6 -63 14175-46 BUSHING - Flap outboard hinge (1 /4’’ L ) 2 14175-89 BUSHING - Flap outboard hinge (3/16’’ L ) 2 -64 82732-121 BUSHING - Flap outboard hinge (3/4” L.) 2 When ordering, always specify Part Number, Description, and Serial Number of Aircraft PIPER PARTS CATALOG 27 Figure 2A Flap Assembly and Aileron Assembly REVISED MARCH 1980 PA-23-250 (Six Place PA-23-250. PA-23-23F 1A19 FLAP ASSEMBLY AND AILERON ASSEMBLY Figure and Index Number 2A- Part Number Code PIPER PARTS CATALOG No NOMENCLATURE Req DRAWING - Flap Assembly DRAWING - Aileron Assembly SECTION I Wing Group SERIAL NUMBERS AFFECTED 17104 17100 -1 17104-40 C FLAPASSEMBLY - Left wing 1710401 C FLAPASSEMBLY - Right wing 17104-58 C.Y FLAP ASSEMBLY - Left wing 17104-57 C Y FLAPASSEMBLY - Right wing 17104-60 C.Y FLAP ASSEMBLY - Left wing 17104-59 C.Y FLAP ASSEMBLY - Right wing 1 27-1 to 27-2504 inclusive 1 27-1 to 27-2504 inclusive 1 27-2505 to 27-3049 inclusive 27-3051 to 27-3153 inclusive 1 27-2505 to 27-3049 inclusive 27-3051 to 27-3153 inclusive 1 27-3050, 27-3154 to 27-7405300 inclusive 1 27-3050, 27-3154 to 27-3784 inclusive 1 27-3785 to 27-7405300 inclusive 1 27-7405301 and up 1 27-7405301 and up 17104-65 C Y FLAP ASSEMBLY - Right wing 17104-68 Y FLAP ASSEMBLY - Left wing 17104-69 Y FLAP ASSEMBLY - Right wing -2 17104-02 * SPAR - Left flap 17104-37 A * SPAR ASSEMBLY - Right flap 17104-62 Y SPAR ASSEMBLY - Right flap -3 17104 22 SKIN - Leading edge left flap. outboard 17104-23 *SKIN - Leading edge right flap, outboard -4 17104-26 * SKIN - Leading edge left flap, inboard 17104-27 *SKIN - Leading edge right flap, inboard -5 17104-47 SKIN ASSEMBLY - Left flap, top 17104-46 A * SKIN ASSEMBLY - Right flap, top 17104-63 Y SKIN ASSEMBLY - Right flap, top -5a 17104-77 STRIP - Beaded -5b 17104-25 PLATE - Reinforcement, right flap, top skin (Sta 0 to Sta 18) -5c 17104-61 B PLATE - Reinforcement, right flap, top skin (Sta 18 to Sta 32) 1 1 1 1 1 1 1 1 1 1 1 27-1 to 27-3784 inclusive 27-3785 and up 27-4 to 27-3784 inclusive 27-3785 and up 1 -5d 17104-10 -6 17104-49 17104-52 17104-66 -7 17104-48 -8 17104-05 -9 17104-07 17104-06 -10 17104-05 17104-04 -11 17104-04 17104-05 B.Y * RIB - Right flap SKIN ASSEMBLY - Left flap, bottom A SKIN ASSEMBLY - Right flap. bottom, outboard Y SKIN ASSEMBLY - Right flap, bottom, outboard * SKIN ASSEMBLY - Right flap, bottom, inboard BULKHEAD - Flap. inboard • BULKHEAD - Left flap BULKHEAD - Right flap BULKHEAD - Left flap * BULKHEAD - Right flap BULKHEAD -Left flap BULKHEAD - Right flap 1 1 1 1 1 1 1 1 1 8 8 2 2 27-3785 and up 27-3785 and up 27-1 to 27-3784 inclusive 27-3785 and up A - Ascertain part number of flap assembly An identification plate with the flap assembly part number is located on the outboard rib If 17104-71 or 17104-72 or 1-7104-73 or 17104-74 is installed, order part for serial number 27-3785 and up B - Used on aircraft with serial numbers 27-1 to 27-3784 inclusive if flap assembly 17104-71 or 17104-72 or 17104-73 or 17104-74 is installed C - When ordering new flap assembly, ascertain part number stamped on identification plate attached to outboard rib Reorder the flap assembly of same part number Y - Used on PA-23-250 (Six Place) airplanes only When ordering always specify Part Number Description and Serial Number of Aircraft REVISED MARCH 1980 1 A20 PA-23-250 (Six Place) PA-23-250 PA-23-235 FLAP ASSEMBLY AND AILERON ASSEMBLY Figure and Index Number Part Number Code PIPER PARTS CATALOG No. NOMENCLATURE Req. SECTION I Wing Group SERIAL NUMBERS AFFECTED 27-1 to 27-7405300 inclusive 27-7405301 and up 2A-12 17104-42 17104-43 -12a 31002-00 31002-01 -13 17104-41 17104-70 17104-08 -14 17104-10 17104-09 -15 17104-12 17104-11 -16 17120-00 -17 17104-10 17104-09 -18 33518-00 -19 33541-00 33541-01 -19a 33555-00 33555-01 -20 17101-00 31003-00 17101-02 · RIB - Left flap * RIB - Right flap ** REINFORCEMENT- Flap outboard rib, left ** REINFORCEMENT- Flap outboard rib, right A * RIB - Left flap * RIB - Left flap * RIB - Right flap * RIB - Left flap * RIB - Right flap * RIB - Left flap * RIB - Right flap *STOP * RIB - Left flap * RIB - Right flap * CHANNEL - Left flap * CHANNEL - Flap hinge reinforcement, left * CHANNEL - Flap hinge reinforcement, right 8 CHANNEL - Flap hinge reinforcement, left CHANNEL - Flap hinge reinforcement, right * HINGE - Flap. inboard, left * HINGE - Flap. inboard, right Y * HINGE - Flap, inboard, left 1 1 1 1 1 1 1 3 3 1 1 1 1 1 1 1 1 1 1 31003-05 Y * HINGE - Flap, inboard, right 17101-03 31003-07 -21 17103-00 17103-01 17103-02 Y * HINGE - Flap. inboard, left Y * HINGE - Flap. inboard, right B * HINGE - Flap, outboard, left B * HINGE - Flap, outboard, right B,Y * HINGE - Flap. outboard, left 1 27-1 to 27-2504 inclusive 1 27-1 to 27-2504 inclusive 1 27-2505 to 27-3049 inclusive. 27-3051 to 27-3153 inclusive 1 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 1 27-3050, 27-3154 and up 1 27-3050. 27-3154 and up 1 27-1 to 27-2504 inclusive 1 27-1 to 27-2504 inclusive 1 27-2505 to 27-3049 inclusive. 27-3051 to 27-3153 inclusive 1 27-2505 to 27-3049 inclusive. 27-3051 to 27-3153 inclusive 1 27-3050. 27-3154 to 27-7405330 inclusive 1 27-3050, 27-3154 to 27-7405330 inclusive 1 27-7405331 and up 1 27-7405331 and up 17103-03 B,Y * HINGE - Flap. outboard, right 17103-04 B,Y * HINGE - Flap, outboard, left 17103-05 BY * HINGE - Flap. outboard, right 33608-02 Y * HINGE - Flap. outboard, left 33608-03 Y * HINGE - Flap, outboard, right A - Ascertain part number of flap assembly on identification plate, located on the outboard rib If 17104-71, 17104- 72, 17104-73 or 17104-74 is installed, order part for serial numbers 27-7405301 and up B - Ascertain if hinge is an angle or a channel type If the angle type is installed, order the appropriate part number listed If the channel type is installed, order the appropriate following part number: 33608-04 left or 33608-05 right for serial numbers 27-1 to 27-2504; 33608-06 left or 33608-07 right for serial numbers 27- 2505 to 27-3049. 27-3051 to 27-3153 inclusive; 33608- 02 left or 33608-03 right for serial numbers 27-3050. 27-3154 to 27-7405330 inclusive Y - Used on PA-23-250 (Six Place) airplanes only When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: MARCH 1980 PA-23-250 (Six Place) PA-23-250, PA-23-235 'IA21 SECTIONI Wing Group FLAPASSEMBLYAND AILERONASSEMBLY Figure and Index Number 2A-22 PIPER PARTS CATALOG Part Number Code NOMENCLATURE 17102-00 * HINGE- Flap,center, left 1 17102-01 * HINGE- Flap,center, right 1 17102-02 Y HINGE- Flap, center, left 1 17102-03 Y * HINGE- Flap,center, right 1 SERIAL NUMBERS AFFECTED -23 17100-00 17100-01 -24 17126-08 17126-09 -25 17202-00 -26 17100-18 -27 17100-12 17100-11 -28 17100-16 17100-17 -29 17100-17 17100-16 -30 18379-00 -31 17100-08 -32 17100-20 17100-19 -33 17100-04 17100-05 -34 17100-05 17100-04 -35 17100-14 -36 17100-21 -37 17100-13 -38 17095-00 17095-01 -39 17097-00 17097-01 AILERONASSEMBLY- Left wing AILERONASSEMBLY- Rightwing * BALANCEASSEMBLY- Aileron, left * BALANCEASSEMBLY- Aileron, right * SHIM * SPARASSEMBLY- Aileron * SKIN- Leadingedge,left * SKIN- Leadingedge.right * SKINASSEMBLY- Left, top * SKINASSEMBLY- Right,top * SKINASSEMBLY- Left, bottom * SKINASSEMBLY- Right, bottom * TAB - Aileron trim * RIB - Aileron, outboard * RIBASSEMBLY- Leadingedge,outboard,left * RIBASSEMBLY- Leadingedge,outboard,right * RIB - Leadingedge * RIB - Leadingedge * RIB - Leadingedge,left * RIB- Leadingedge,right * RIB- Aileron center * PLATEASSEMBLY- Aileron hinge, reinforcement, center * RIB- Aileron inboard * HINGE- Aileron inboard,left * HINGE- Aileron inboard,right * HINGE- Aileron center, left * HINGE- Aileron center, right 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 9 9 1 1 2 27-1 to 27-2504 inclusive 27-1to 27-2504 inclusive 27-2505to 27-3049 inclusive 27-3051to 27-3153 inclusive 27-2505to 27-3049 inclusive 27-3051to 27-3153 inclusive 1 1 1 1 1 1 Y - Usedon PA-23-250(Six Place)airplanesonly When ordering, always specifyPart Number,Descriptionand Serial Numberof Aircraft REVISED:MARCH1980 PA-23-250(Six Place) PA-23-250,PA-23-235 1A22 1A23 THRU 1A24 INTENTIONALLY LEFT BLANK Figure 3. Wing and Wing Tip Construction PIPER PARTS CATALOG REVISED: DECEMBER 10, 2007 PA-23-250 (Six Place) PA-23-250, PA-23-235 1B1 SECTION I Wing Group Figure and Index Number 3- Part Number 16170 16170 33300 17631 34282 16067 16292 30698 33304 33900 -1 1617000 16170-01 1617000 16170-01 1617030 16170-29 16170-26 16170-25 16170-28 16170-27 16170-32 16170-31 3330000 33300-01 3330006 3330007 -la 1733003 -2 462 346 2670400 -3 1733002 -4 462 346 2570400 -5 17331-02 -6 462 345 26704-00 -7 1839801 1839800 -8 462 345 26704-00 -9 17629-02 -10 1752903 -11 1762904 15661402 -12 33917-02 33917-03 Code x,z Y Y x,Z Y Y C,x C,x C,Z C.Z z z D,Y D,Y Y Y Y Y Y Y Y Y A B B B B NOMENCLATURE DRAWING - Wing Panel DRAWING -Wing Panel DRAWING -Wing Panel DRAWING -Wing Tip DRAWING - Wing Tip DRAWING - Outboard Leading Edge Asembly DRAWING -Wing Installation DRAWING -Wing Installation DRAWING- Wing Installation DRAWING -Wing Installation WING AND WING TIP CONSTRUCTION No. SERIAL NUMBERS Req. AFFECTED 27-2000 to 274815 inclusive 274816 and up 27-1 to 27-7554168 inclusive 27-7654001 and up 27-2000 to 274815 inclusive 27-4816 to 27-7554168 incl. 27-7654001 and up PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing BRACKET - Aileron hinge BEARING BEARING BRACKET - Aileron and flap hinge BEARING BEARING BRACKET - Flap hinge, center BEARING BEARING BRACKET - Flap hinge, inboard, left BRACKET - Flap hinge, inboard, right BEARING BEARING HINGE -Wing tip HINGE - Wing tip attachment PIN - Wing tip hinge PIN -Wing tip hinge RIB ASSEMBLY - Wing trailing edge,left RIB ASSEMBLY - Wing trailing edge,right 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 121 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 27-505 to 27-524 inclusive 27-505 to 27-524 inclusive 27-525 and up 27-525 and up 27-2000 to 27-2269 inclusive 27-2000 to 27-2269 inclusive 27-2270 to 27-2504 inclusive 27-2270 to 27-2504 inclusive 27-2605 to 27-4816 Inclusive 27-2505 to 274815 inclusive 27-4816 to 27-7554168 incl. 274816 to 27-7554168 incl. 27-7654001 and up 27-7654001 and up 27-1 to 27-3483 inclusive 27-3484 and up 27-1 to 27-3483 inclusive 27-3484 and up 27-1 to 27-3483 inclusive 27-3484 and up 27-1 to 27-3483 inclusive 27-3484 and up 27-1 to 27-7554168 inclusive 27-1 to 27-7664168 inclusive 27-7654001 and up A - Component pert of wing tip assembly. B - Not a component of wing panel or wing tip. C - If Kit No. 754 493 hasbeen installed, order wing panel 16170-29 R.H. or 1617030 L.H. D - If Kit No. 754 493 has been Installed, order wing panel 16170-27 R.H. or 16170-28 L.H. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place) airplanes only. Z - Used on PA-23-236 airplanes only. When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: OCTOBER 1976 1B2 PA-23-250 (Six Place) PA-23-250, PA-23-235 WING AND WING TIP CONSTRUCTION SECTION I Wing Group Figure and Index Number Part Number Code 3-13 18253-02 18253-20 -14 18253-17 -15 18253-19 -16 18253-10 B 18253-11 18253-03 18253-12 -17 17531-12 17531-13 -18 17531-16 17531-17 -19 17531-06 17531-07 -20 17531-14 17531-15 -21 17531-08 17531-09 -22 17329-12 17329-13 -23 17329-28 17329-29 -24 17329-29 17329-28 -25 17329-28 17329-29 -26 17329-23 17329-08 -27 17329-30 17329-27 -28 17329-30 A,B A,B A,B A,B A,B A,B A,B A,B A,B A,B NOMENCLATURE STRIP ASSEMBLY Wing tip attachment, top, rear STRIP ASSEMBLY - Wing tip attachment, top, rear STRIP ASSEMBLY - Wing tip attachment, top, center STRIP ASSEMBLY - Wing tip attachment, front STRIP ASSEMBLY - Wing tip attachment, bottom center, right STRIP ASSEMBLY - Wing tip attachment, bottom center, right STRIP ASSEMBLY - Wing tip attachment, bottom center, left STRIP ASSEMBLY - Wing tip attachment, bottom center, left RIB -Wing tip front, left RIB - Wing tip front, right RIB - Wing tip rear, left RIB - Wing tip rear, right SPAR - Wing tip front, left SPAR - Wing tip front, right RIB - Wing tip center, left RIB - Wing tip center, right SPAR - Wing tip rear, left SPAR - Wing tip rear, right BULKHEAD - Rear spar, left, Sta. 146, 191 BULKHEAD - Rear spar,right, Sta. 146, 191 BULKHEAD - Rear spar, left, Sta. 157, 168, 180 BULKHEAD - Rear spar, right, Sta. 157, 168, 180 BULKHEAD- Rear spar, left, Sta. 102,118,136 BULKHEAD - Rear spar, right, Sta. 102, 118, 136 BULKHEAD - Rear spar, left, Sta. 27 BULKHEAD - Rear spar, right, Sta. 127 BULKHEAD - Rear spar, left, Sta. 110 BULKHEAD · Rear spar, right, Sta. 110 BULKHEAD- Rear spar, left, Sta. 95 BULKHEAD - Rear spar, right, Sta. 95 BULKHEAD - Rear spar, left, Ste. 87, outboard of torque rib BULKHEAD - Rear spar, right, Sta. 87, outboard of torque rib BULKHEAD - Rear spar, left, Sta. 56,61 and 74, outboard of torque rib BULKHEAD - Rear spar, right, Sta. 56,61 and 74, outboard of torque rib BULKHEAD - Rear spar,left, Ste. 80 BULKHEAD - Rear spar,right, Ste. 80 BULKHEAD - Rear spar, Ste. 49 BULKHEAD - Rear spar, left (torque rib) BULKHEAD - Rear spar, right (torque rib) BULKHEAD - Rear spar, left, Sta 34, 42 BULKHEAD - Rear spar,right, Sta. 34,42 BULKHEAD - Rear spar,left, Sta. 27 BULKHEAD - Rear spar,right, Sta. 27 STIFFENER - (6' section) ANGLE - Extrusion (6'section) 1 1 1 1 1 1 1 1 1 22 2 3 3 3 3 1 1 1 1 1 1 27-7654001 and up 1 27-1 to 27-7554168 inclusive 1 27-7654001 and up 1 27-1 to 27-7554168 inclusive No. SERIAL NUMBERS Req. AFFECTED 1 27-7654001 and up 1 1 17329-27 1928309 -28a 19283-10 -29 17329-27 17329-30 -29a 19283-10 -30 19283-12 19283-13 -31 19283-04 19283-03 -32 17329-34 17329-31 -33 752 959 -34 149 063 2 2 2 2 1 1 2 1 1 2 2 1 1 A - Component part of wing tip assembly. B - Used on PA-23-250 and PA-23-235 with serial numbers 27-1 to 27-622 and PA-23-250 (Six Place) with serial numbers 27-2000 to 27-7554172 inclusive. When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: OCTOBER 1976 1B3 PA-23-250 (Six Place) PA-23-250, PA-23-235 SECTION I Wing Group Figure and Index Number NOMENCLATURE Part Number 1-35 16054-00 16064-00 33767-02 16064-01 1606401 33767-03 -36 16047-00 16047-01 -37 16053-05 15720-02 16063-04 15720-02 16063-02 16053-12 -37a 16063-04 1572002 16053-05 1572002 16053-02 16063-12 -38 16062-00 16052-00 33302-00 16052-01 16052-01 33302-01 -39 16658-02 1665806 -40 17367-00 -41 16658-04 16658-08 -42 17423-00 -43 18658-05 16658-09 -43a 16658-03 1665807 -44 16027-00 16027-01 -45 1601805 1601804 -46 1601802 16018-03 -47 16024-00 16024-01 -48 16008-02 1600o803 16008-04 1600805 -49 16008-04 1600805 -50 19287-00 1928701 Code xz Y Y xZ Y Y A A A A AAXZ A AA X,Z YY, WING AND WING TIP CONSTRUCTION No. SERIAL NUMBERS Req. AFFECTED RIB ASSEMBLY - Wing left, Sta. 191 RIB ASSEMBLY -Wing, left, Sta. 191 RIB ASSEMBLY - Wing, left, Sta. 191 RIB ASSEMBLY - Wing, right, Sta. 191 RIB ASSEMBLY -Wing, right, Sta. 191 RIB ASSEMBLY - Wing, right, St. 191 RIB ASSEMBLY - Wing, left, Sta. 146 RIB ASSEMBLY - Wing, right, Sta. 146 RIB ASSEMBLY - Wing, left top, Sta. 175 RIB ASSEMBLY - Wing, left top, Sta. 175 RIB ASSEMBLY - Wing, right top, Sta. 175 RIB ASSEMBLY - Wing, right top, Sta. 175 RIB ASSEMBLY - Wing, bottom, Sta. 175 RIB ASSEMBLY - Wing, bottom, Sta. 175 RIB ASSEMBLY - Wing, left top, Sta. 160 RIB ASSEMBLY - Wing, left top, Sta. 160 RIB ASSEMBLY - Wing, right top, Sta. 160 RIB ASSEMBLY - Wing, right top, Sta. 160 RIB ASSEMBLY - Wing, bottom. Sta. 160 RIB ASSEMBLY - Wing, bottom, Sta. 160 RIB ASSEMBLY - Wing, left, Sta. 127 RIB ASSEMBLY - Wing, left, Sta. 127 RIB ASSEMBLY- Wing, left, Sta 127 RIB ASSEMBLY - Wing, right, Sta. 127 RIB ASSEMBLY - Wing, right, Sta. 127 RIB ASSEMBLY - Wing, right, Sta. 127 RIB ASSEMBLY - Wing, left top, Sta. 110 RIB ASSEMBLY - Wing, right top, Sta. 110 ANGLE -Rib, Sta. 96, 109 RIB ASSEMBLY - Wing, left, Sta. 95, top RIB ASSEMBLY - Wing, right, Sta. 96, top SHIM - Rib, Sta. 56, 80 RIB ASSEMBLY - Wing, left, Sta. 96, bottom RIB ASSEMBLY - Wing, right, Sta. 95, bottom RIB ASSEMBLY - Wing, left, Sta. 110, bottom RIB ASSEMBLY - Wing, right, Sta. 110, bottom RIB ASSEMBLY - Wing, left, Ste. 80 RIB ASSEMBLY - Wing, right. Sta. 80 RIB ASSEMBLY - Wing, outboard torque, left RIB ASSEMBLY - Wing, outboard torque, right RIB ASSEMBLY - Wing, inboard torque, left R IB ASSEMBLY - Wing, inboard torque, right RIB ASSEMBLY - Wing, left, Sta. 56 RIB ASSEMBLY - Wing, right, Sta. 56 RIB ASSEMBLY - Wing, left, Sta. 42,49 RIB ASSEMBLY - Wing, right, St. 42 49 RIB ASSEMBLY - Wing, left, Sta. 42,49 RIB ASSEMBLY - Wing, right, St. 42, 49 RIB ASSEMBLY - Wing, left, Sta. 34 RIB ASSEMBLY - Wing, right, Sta. 34 RIB ASSEMBLY - Wing butt, left RIB ASSEMBLY - Wing butt, right 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 2 1 1 1 1 1 1 1 1 1 2 2 2 2 1 1 1 1 27-2000 to 27-4815 inclusive 27-4816 and up 27-2000 to 27-4815 inclusive 27-4816 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 end up 27-2000 to 27-4815 inclusive 27-4816 and up 27-2000 to 27-4815 inclusive 27-4816 and up XZ X,Z Y Y A - Useedon PA-23-250 and PA-23-235 with serial numbers 27-1 to 27-622 and PA-23-260 (Six Place) with Serial numbers 27-2000 to 27-7664168 inclusive. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place) airplanes only. Z - Used on PA-23-235 airplanes only. When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: OCTOBER 1976 1 B4 PA-23-250 (Six Place) PA-23-250 PA-23-235 WING AND WING TIP CONSTRUCTION Figure and Index Number Part Number Code PIPER PARTS CATALOG No. NOMENCLATURE Req SECTION I Wing Group SERIAL NUMBERS AFFECTED 3-51 -52 -53 -53a 16055-00 16055-01 17230-06 17230-07 16055-02 16055-03 -53b 80012-96 -53c 16055-06 16055-07 -54 17412-40 17412-41 30646-00 30646-01 30646-10 30646-11 -55 17412-22 -55a 30646-06 30646-07 30646-14 30646-13 -55b 30646-08 -55c 31408-00 -56 18688-00 18688-01 18688-02 18688-03 -57 16231-00 16231-00 30859-02 30859-02 16231-01 16231-01 30859-03 30859-03 -58 17184-14 17184-22 17184-16 17184-23 -58a 17184-14 17184-16 15782-02 15782-03 -59 17184-12 17184-20 17184-17 17184-21 -60 17185-18 17185-17 -61 17185-16 17185-15 -62 17184-11 17184-15 -63 17186-08 17186-09 -64 17184-18 17184-19 * SPAR ASSEMBLY - Wing rear, left * SPAR ASSEMBLY - Wing rear, right ** PLATE - Rear spar, left front, right rear ** PLATE - Rear spar, left rear, right front ** SPAR - Outboard section, Sta 99 31 to Sta 192 07, left ** SPAR - Outboard section, Sta 99 31 to Sta 192 07, right ** BUSHING ** SPAR ASSEMBLY - Inboard section, Sta 23 75 to Sta 99 31. left ** SPAR ASSEMBLY - Inboard section. Sta 23 75 to Sta 99 31, right X,Z * SPAR ASSEMBLY - Wing front, left X,Z * SPAR ASSEMBLY - Wing front, right Y * SPAR ASSEMBLY - Wing front, left Y * SPAR ASSEMBLY - Wing front, right Y * SPAR ASSEMBLY - Wing front, left Y * SPAR ASSEMBLY - Wing front, right ** PLATE - Front spar end ** CHANNEL - Front spar tip, left * CHANNEL - Front spar tip, right ** CHANNEL - Front spar tip, left ** CHANNEL - Front spar tip, right ** REINFORCEMENT- Spar tip channel Y ** BLOCK - Bearing, main gear door actuator * BRACKET- Hydraulic line support, left * BRACKET- Hydraulic line support, right * BRACKET- Hydraulic line support, left * BRACKET- Hydraulic line support, right X * BRACKET- Fuel valve shutoff, left Y * BRACKET- Fuel valve shutoff, left Y * BRACKET- Fuel valve shutoff, left Z * BRACKET- Fuel valve shutoff, left X BRACKET - Fuel valve shutoff, right Y BRACKET- Fuel valve shutoff, right Y * BRACKET- Fuel valve shutoff, right Z * BRACKET- Fuel valve shutoff, right * RIB ASSEMBLY - Wing nose, left, Sta 180 * RIB ASSEMBLY - Wing nose, left, Sta 180 * RIB ASSEMBLY - Wing nose, right, Sta 180 * RIB ASSEMBLY - Wing nose, right, Sta 180 * RIB ASSEMBLY - Wing nose, left, Sta 191 * RIB ASSEMBLY - Wing nose, right, Sta 191 * RIB ASSEMBLY - Wing nose, left, Sta 191 RIB ASSEMBLY - Wing nose, right, Sta 191 * RIB ASSEMBLY - Wing nose, left, Sta 157, 168 * RIB ASSEMBLY - Wing nose, left, Sta 157, 168 * RIB ASSEMBLY - Wing nose, right, Sta 157, 168 * RIB ASSEMBLY - Wing nose. right, Sta 157, 168 * RIB ASSEMBLY - Wing nose, left, Sta 146 * RIB ASSEMBLY - Wing nose, right, Sta 146 * RIB ASSEMBLY - Wing nose, left. Sta 136 * RIB ASSEMBLY - Wing nose, right, Sta 136 * RIB ASSEMBLY - Wing nose, left. Sta 127 * RIB ASSEMBLY - Wing nose, right, Sta 127 * RIB ASSEMBLY - Wing nose, left. Sta 118 * RIB ASSEMBLY - Wing nose, right, Sta 118 * RIB ASSEMBLY - Wing nose, left, Sta 109 * RIB ASSEMBLY - Wing nose, right, Sta 109 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 2 2 2 1 1 1 1 2 2 2 2 1 1 1 1 2 2 2 2 1 1 1 1 1 1 1 1 1 1 27-2000 to 27-7554168 inclusive 27-2000 to 27-7554168 inclusive 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 and up 27-7654001 and up 27-2505 and up 27-1 to 27-7954121 inclusive 27-1 to 27-7954121 inclusive 27-8054001 and up 27-8054001 and up 27-2000 to 27-2222 inclusive 27-2223 and up 27-2000 to 27-2222 inclusive 27-2223 and up 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 and up 27-7654001 and up 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-504 inclusive 27-505 and up X - Used on PA-23-250 airplanes only Y - Used on PA-23-250 (Six Place) airplanes only Z - Used on PA-23-235 airplanes only When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED JULY 1984 PA-23-250 (Six Place) PA-23-250, PA-23-235 1B5 SECTION I Wing Group Figure and Index Number WING AND WING TIP CONSTRUCTION Part Number Code PIPER PARTS CATALOG No NOMENCLATURE Req 3 -65 17187-10 17187-11 -66 17188-10 17188-12 17188-11 17188-13 -67 17189-10 17189-11 -68 16034-00 16034-01 -69 16042-00 16042-01 16042-10 16042-11 -70 16012-02 16012-03 -71 16017-00 16017-01 -71 a 16016-00 16016-01 -72 16014-00 16014-01 16014-02 16014-03 -73 16013-00 16013-01 -73a 16015-00 16015-01 -74 17375-00 -75 17382-00 17382-01 -76 17193-00 -77 17428-00 17428-02 17428-04 17428-01 17428-03 17428-05 -78 17459-00 -79 18614-00 18614-01 -80 18606-00 -81 17752-02 -82 18329-02 -83 18358-00 18358-01 31404-00 31404-01 -84 18942-02 -85 18942-00 -86 16216-00 16216-00 16216-01 16216-01 * RIB ASSEMBLY - Wing nose, left, Sta 102 * RIB ASSEMBLY - Wing nose, right, Sta 102 * RIB ASSEMBLY - Wing nose, left, Sta 95 * RIB ASSEMBLY - Wing nose, left, Sta 95 * RIB ASSEMBLY - Wing nose, right, Sta 95 * RIB ASSEMBLY - Wing nose. right, Sta 95 * RIB ASSEMBLY - Wing nose, left, Sta 87 * RIB ASSEMBLY - Wing nose, right, Sta 87 RIB ASSEMBLY - Wing nose, left. Sta 80 * RIB ASSEMBLY - Wing nose, right, Sta 80 * RIB ASSEMBLY - Wing nose, left. Sta 56 * RIB ASSEMBLY - Wing nose, right, Sta 56 * RIB ASSEMBLY - Wing nose. left. Sta 56 * RIB ASSEMBLY - Wing nose, right, Sta 56 RIB ASSEMBLY - Wing, left, Sta 49 * RIB ASSEMBLY - Wing, right, Sta 49 * RIB ASSEMBLY - Wing, left, Sta 42 * RIB ASSEMBLY - Wing, right, Sta 42 * BULKHEAD - Wing, leading edge, left, Sta 42 BULKHEAD - Wing, leading edge, right. Sta 42 X.Z * RIB ASSEMBLY - Wing nose, left, Sta 34 X,Z RIB ASSEMBLY - Wing nose, right, Sta 34 Y RIB ASSEMBLY - Wing nose, left. Sta 34 Y * RIB ASSEMBLY - Wing nose, right. Sta 34 * RIB ASSEMBLY - Wing nose, left. Sta 27 * RIB ASSEMBLY - Wing nose, right, Sta 27 * RIB ASSEMBLY - Wing nose. left, Sta 27 * RIB ASSEMBLY - Wing nose, right, Sta 27 ANGLE - Rib. Sta 56,80 BULKHEAD - Nose rib, outboard, left * BULKHEAD - Nose rib, outboard, right * PLATE - Wing rib cover * BRACKETASSEMBLY - Aileron bellcrank, left * BRACKET ASSEMBLY - Aileron bellcrank, left * BRACKETASSEMBLY - Aileron bellcrank, left * BRACKETASSEMBLY - Aileron bellcrank, right * BRACKETASSEMBLY - Aileron bellcrank, right * BRACKETASSEMBLY - Aileron bellcrank, right BRACKET- Aileron cable pulley ANGLE - Butt rib, left, Sta. 27 ANGLE - Butt rib, right, Sta 27 *SHIM - Bun, rib. Sta 27 CONDUIT - Wire harness (1 -1/4) *BOLT- "U" PLATE - Wheel well attachment, left PLATE - Wheel well attachment, right Y PLATE - Wheel well attachment, left Y * PLATE - Wheel well attachment, right SHIM - Rib. Ste 42,49 SHIM - Rib, Sta 34 X * BRACKET- Fuel strainer, left Y * BRACKET - Fuel strainer, left X BRACKET- Fuel strainer, right Y * BRACKET- Fuel strainer, right 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 4 1 1 2 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 2 3 1 1 1 1 SERIAL NUMBERS AFFECTED 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-7954089 inclusive 27-1 to 27-7954089 inclusive 27-7954090 and up 27-7954090 and up 27-1 to 27-504 inclusive 27-505 to 27-7554168 inclusive 27-7654001 and up 27-1 to 27-504 inclusive 27-505 to 27-7554168 inclusive 27-7654001 and up 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up 27-2000 to 27-2222 inclusive 27-2000 to 27-2222 inclusive X - Used on PA-23-250 airplanes only Y - Used on PA-23-250 (Six Place) airplanes only Z - Used on PA-23-235 airplanes only When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED OCTOBER 1980 1B6 PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG REVISED: DECEMBER 10, 2007 PA-23-250 (Six Place) PA-23-250, PA-23-235 1B7 Figure and Index Number Part Number Code NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED WING TIP AND WING TIP CONSTRUCTION SECTION I Wing Group 3-87 18572-00 FITTING - Landing gear reinforcement, left 1 18572-01 FITTING - Landing gear reinforcement, right 1 -88 18571-00 PLATE - Filler, left 1 18571-01 PLATE - Filler, right 1 -89 17209-04 ANGLE - Torque rib stiffener (right wing outboard or left wing inboard) 1 17209-05 ANGLE - Torque rib stiffener (right wing inboard or left wing outboard) 1 -90 16046-00 ANGLE - Rib attachment, Sta. 42, 49 2 -91 19302-00 ANGLE - Rib attachment, Sta. 34 1 -92 19294-00 PLATE - Torque rib reinforcement, left 1 19294-01 PLATE - Torque rib reinforcement, right 1 -93 19295-00 SHIM - Torque rib 2 -94 16010-00 SPAR ASSEMBLY - Front, left 1 16010-01 SPAR ASSEMBLY - Front, right 1 -95 19976-00 STRINGER ASSEMBLY - Left 1 27-505 and up 19976-01 STRINGER ASSEMBLY - Right 1 27-505 and up -96 31409-00 Y BRACKET ASSEMBLY - Main gear door actuator, left 1 27-2505 and up 31409-01 Y BRACKET ASSEMBLY - Main gear door actuator, right 1 27-2505 and up -97 33159-00 DOUBLER - Wing, front spar, left 1 33159-01 DOUBLER - Wing, front spar, right 1 -98 33158-00 BRACKET - Wing, rib attachment, left 1 33158-01 BRACKET - Wing, rib attachment, right 1 -99 33792-02 A BULKHEAD - Wing tip, left 1 27-7654001 and up 33792-03 A BULKHEAD - Wing tip, right 1 27-7654001 and up -100 33791-02 A BULKHEAD - Wing tip, left 1 27-7654001 and up 33791-03 A BULKHEAD - Wing tip, right 1 27-7654001 and up -101 33770-02 A RIB ASSEMBLY - Wing tip, left 1 27-7654001 and up 33770-03 A RIB ASSEMBLY - Wing tip, right 1 27-7654001 and up -102 33760-02 HINGE - Wing tip, left 1 27-7654001 and up 33760-03 HINGE - Wing tip, right 1 27-7654001 and up -103 34220-00 A RIB ASSEMBLY - Wing tip, left 1 27-7654001 to 27-7954087 incl. 34220-14 A RIB ASSEMBLY - Wing tip, left 1 27-7954088 and up 34220-01 A RIB ASSEMBLY - Wing tip, right 1 27-7654001 to 27-7954087 incl. 34220-15 A RIB ASSEMBLY - Wing tip, right 1 27-7954088 and up -104 33773-02 A SPAR - Wing tip, upper 1 27-7654001 and up -105 33774-02 A SPAR - Wing tip, lower 1 27-7654001 and up -106 33772-02 A BRACKET ASSEMBLY - Strobe power supply, left 1 27-7654001 and up 33772-03 A BRACKET ASSEMBLY - Strobe power supply, right 1 27-7654001 and up -107 15797-02 CHANNEL ASSEMBLY - Tip guide, left 1 27-7654003 and up 15797-03 CHANNEL ASSEMBLY - Tip guide, right 1 27-7654003 and up -108 80013-42 PLATE - Shim 1 A - Component part of wing tip assembly. Y - Used on PA-23-250 (Six Place) airplanes only. When ordering, always specify Part Number, Description, and Serial Number of Aircraft PIPER A I R C R A FT C O R P O R A T I O N Figure 4. Wing and Wing Tip Skin REVISED: OCTOBER 1976 1B8 PA-23-250 (Six Place) PA-23-250, PA-23-235 WING AND WING TIP SKIN SECTION I Wing Group Figure and Index Number 4- Part Number 16170 16170 33300 16292 30698 33304 33900 Code x,z Y X,Z Y Y Y NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED DRAWING - Wing Panel DRAWING -Wing Panel DRAWING -Wing Panel DRAWING -Wing Installation DRAWING -Wing Installation DRAWING -Wing Installation DRAWING -Wing Installation 27-2000 to 27-4815 inclusive 27-4816 and up 27-2000 to 27-4815 inclusive 27-4816 to 27-7554168 incl 27-7654001 and up -1 16170-00 16170-01 16170-00 16170-01 16170-30 16170-29 16170-26 16170-25 16170-28 16170-27 16170-32 16170-31 33300-00 33300-01 33300-06 33300-07 -la 16170-16 16170-17 33300-14 33300-15 -2 16170-10 16170-09 33300-12 -3 16170-02 -4 16009-00 -5 17318-02 17318-02 -5a 17318-04 -6 16170-06 16170-05 16170-36 16170-35 -7 16057-07 17422-35 -7a 17315-00 -8 17422-36 17422-37 -8a 17317-00 -9 16057-04 A,X A,X A,Z A,Z Z z BY B,Y Y Y Y Y Y Y Y Y Y Y Y Y PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing SKIN ASSEMBLY - Outboard top, L.H. SKIN ASSEMBLY - Outboard top, R.H. SKIN ASSEMBLY - Outboard top, L H. SKIN ASSEMBLY - Outboard top, R.H. SKIN ASSEMBLY - Wing center top, L.H. SKIN ASSEMBLY - Wing center top, R.H SKIN ASSEMBLY - Wing center top SKIN - Wing top, inboard PLATE - Fuel cell accesshole cover PLATE - Accesshole cover PLATE - Accesshole cover PLATE - Accesshole cover SKIN ASSEMBLY - Left SKIN ASSEMBLY - Right SKIN ASSEMBLY - Left SKIN ASSEMBLY -Right SKIN ASSEMBLY - Left wing leading edge,outboard SKIN ASSEMBLY - Right wing leading edge, outboard PLATE - Reinforcement SKIN ASSEMBLY - Left wing leading edge,center SKIN ASSEMBLY - Right wing leading edge,center PLATE - Reinforcement SKIN ASSEMBLY - Left wing leading edge,inboard center SKIN ASSEMBLY - Right wing leading edge,inboard center PLATE - Reinforcement 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 3 2 1 1 1 1 1 1 1 1 1 1 1 27-505 to 27-524 inclusive 27-505 to 27-524 inclusive 27-525 and up 27-525 and up 27-2000 to 27-2269 inclusive 27-2000 to 27-2269 inclusive 27-2270 to 27-2504 inclusive 27-2270 to 27-2504 inclusive 27-2505 to 27-4815 inclusive 27-2505 to 27-4815 inclusive 27-4816 to 27-7554168 incl 27-4816 to 27-7554168 incl 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 and up 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up 16057-05 -9a 17317-00 1 1 A - If Kit No. 754 493 has been installed, order wing panel 16170-30 left or 16170-29 right. B - If Kit No. 754 493 has been installed, order wing panel 16170-28 left or 16170-27 right. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place)airplanes only. Z - Used on PA-23-235 airplanes only. When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: OCTOBER 1976 1B9 PA-23-250 (Six Place) PA-23-250, PA-23-235 SECTIONI Wing Group Figure and Index Number WING AND WINGTIP SKIN PIPER PARTS CATALOG Part No. Number Code NOMENCLATURE Req. 4-10 16045-04 16045-05 16045-10 16045-11 16045-14 16045-15 -10a 17317-03 31596-00 -10b 17317-03 -11 17316-00 -12 17318-03 -13 17383-00 17383-01 -14 17361-02 17361-03 -15 17361-04 17361-05 -16 17362-02 17362-03 -17 16170-18 33300-04 16170-19 33300-05 -18 16170-12 16170-11 -19 16170-20 16170-21 -19a 17317-03 -20 17365-00 -21 15713-02 -22 15717-02 -23 15718-02 15718-03 -24 44275-08 -25 18480-00 -26 17531-00 17531-01 17531-00 17531-01 17531-40 17531-41 17531-00 17531-01 17531-40 17531-41 17531-46 17531-47 Y Y Y Y Y Y B A,X A,X A,Z AZ Z Z A,Y A,Y Y Y Y Y SKINASSEMBLY- Left leadingedge, inboard SKINASSEMBLY- Right leadingedge, inboard SKINASSEMBLY- Left leading edge,inboard SKIN ASSEMBLY- Right leadingedge, inboard SKIN ASSEMBLY- Left leading edge,inboard SKINASSEMBLY- Right leadingedge, inboard PLATE- Reinforcement PLATEASSEMBLY- Reinforcement PLATEASSEMBLY- Reinforcement PLATE- Aileron bellcrankaccesshole cover PLATE- Accesshold cover FAIRING- Falsespar, left FAIRING- False spar,right SPAR- False,left wing outboard SPAR- False,right wing outboard SPAR- False,left wing center SPAR- False,right wing center SPAR- False,left wing inboard SPAR- False,right wing inboard SKINASSEMBLY- Outboard bottom,L H SKIN ASSEMBLY- Outboard bottom,L H SKINASSEMBLY- Outboard bottom,R H SKINASSEMBLY- Outboard bottom,R H SKINASSEMBLY- Centerbottom,L H SKINASSEMBLY- Centerbottom,R H SKINASSEMBLY- Inboard bottom,L H SKINASSEMBLY- Inboard bottom,R H PLATE- Reinforcement PAD - Jack COVER- Fuel cell access PLATEASSEMBLY- Accesshole reinforcement PLATEASSEMBLY- Fuel cell access,left PLATEASSEMBLY- Fuel cell access,right FLOWSTRIP- Wing, right COVERASSEMBLY- Wing tip access TIP ASSEMBLY- Wing, left TIP ASSEMBLY- Wing, right TIP ASSEMBLY- Wing, left TIP ASSEMBLY- Wing, right TIP ASSEMBLY- Wing, left TIP ASSEMBLY- Wing, right TIP ASSEMBLY- Wing, left TIP ASSEMBLY- Wing, right TIPASSEMBLY- Wing, left TIPASSEMBLY- Wing, right TIP ASSEMBLY- Wing, left TIP ASSEMBLY- Wing, right 1 I 1 1 1 1 2 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 1 SERIALNUMBERS AFFECTED 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 to 27-7954089 inclusive 27-2505 to 27-7954089 incl 27-7954090 and up 27-7954090 and up 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up 27-1 to 27-4815 inclusive 27-4816 and up 27-1 to 27-4815 inclusive 27-4816 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclusive 27-505 to 27-524 inclusive 27-505 to 27-524 inclusive 27-525 and up 27-525 and up 27-2000 to 27-2269 inclusive 27-2000 to 27-2269 inclusive 27-2270 to 27-4815 inclusive 27-2270 to 27-4815 inclusive 27-4816 to 27-7554168 inclusive 27-4816 to 27-7554168 inclusive A - If Kit No 754 493 is used, orderwing tip 1753140 left or 17531-41 right B - Referto Figure 42C if PneumaticDeicerInstallation is installed X - Usedon PA-23-250 airplanesonly Y - Used on PA-23-250 (Six Place)airplanesonly Z - Usedon PA-23-235airplanesonly When ordering, always specify Part Number, Description and Serial Number of Aircraft 1B10 REVISED:AUGUST1979 PA-23-250 (Six Place) PA-23-250, PA-23-235 WINGAND WINGTIP SKIN Figure and Index Number PIPER PARTS CATALOG Part No. Number Code NOMENCLATURE Req. 4-27 17531-34 17531-35 17531-36 17531-37 17531-42 17531-43 -28 17531-32 17531-33 -29 18694-00 -30 17531-18 17531-19 -31 30988-00 -32 31075-00 -33 34282-00 34282-14 34282-01 34282-15 -34 34282-04 34282-05 -35 34282-02 34282-03 -36 34282-06 34282-07 -37 15586-02 15586-03 -38 33808-03 -39 40546-08 -40 33803-02 -41 33797-02 -42 16541-02 16541-03 -43 33330-00 -44 33329-00 -45 34267-00 28366-02 34267-01 28366-03 -46 15711-02 -47 15736-02 -48 462 000 C C B 8 A A B,D G,Y G.Y G.Y G,Y Y Y Y Y Y Y Y Y Y Y E,Y Y Y Y Y Y F,Y F.Y F,Y SKIN- Left wing tip, lower SKIN- Rightwing tip, lower SKIN- Left wing tip, lower SKIN- Right wing tip, lower SKIN- Left wing tip, lower SKIN- Right wing tip, lower SKIN- Left wing tip, upper SKIN- Rightwing tip, upper CHANNEL- Section (six foot section) REINFORCEMENT - Aileron balanceweight, left REINFORCEMENT - Aileron balanceweight, right VENTASSEMBLY- Fuel cell TUBEASSEMBLY- Fuel cell vent drain TIPASSEMBLY- Wing, left TIPASSEMBLY- Wing, left TIPASSEMBLY- Wing, right TIP ASSEMBLY- Wing, right SKIN - Left wing tip, lower SKIN- Right wing tip, lower SKIN- Left wing tip, upper SKIN- Right wing tip, upper SKIN- Wing tip leadingedge, left SKIN- Wing tip leadingedge, right REINFORCEMENT - Aileron balance weight, left REINFORCEMENT - Aileron balance weight, right REINFORCEMENT - Tip skin COVERASSEMBLY- Fuel cell access COVER - Fuel cell GASKET- Fuel cell ANGLE- Nacelleattaching, left wing, outboard nose ANGLE- Nacelleattaching,right wing, outboard nose STRIP- Vent drain CONE FAIRINGASSEMBLY- Wing Tip, Left (Fiberglass) FAIRINGASSEMBLY- Wing Tip, Left (Thermoplastic) FAIRINGASSEMBLY- Wing Tip, Right (Fiberglass) FAIRINGASSEMBLY- Wing Tip. Right (Thermoplastic) COVER- Fuel cell RING- Fuel cell attachment GASKET- (FCB-25722) 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 14 1 1 1 1 2 2 2 SECTIONI Wing Group SERIALNUMBERS AFFECTED 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 to 27-7954087 incl 27-7954088 and up 27-7654001 to 27-7954087 incl 27-7964088 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 to 27-7954087 incl. 27-7954088 and up 27-7654001 to 27-7954087 incl. 27-7954088 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up A - Usedwith wing tip 17531-46 or 17531-47 B - Usedwith wing tip 17531-40 or 17531-41. C - Usedwith wing tip 17531-00 or 17531-01 D - Usedwith wing tip 17531-48. E - Usedif wing tip fuel tank is not installed F - Usedif wing tip fuel tank is installed. G - Referto Figure3 for balanceof component parts Y - Usedon PA-23-250(Six Place)airplanes only When ordering,always specify Part Number, Descriptionand Serial Number of Aircraft 1B11 REVISED:AUGUST 1979 PA-23-250(Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG 7- 14- 13- 12- 9- 10 Figure5 CompleteFuselage REVISED:FEBRUARY1979 1B'12 PA-23-250 (Six Place) PA-23-250, PA-23-235 SECTIONII FuselageGroup COMPLETEFUSELAGE Figure and Index Number 5- Pert Number Code PIPER PARTS CATALOG No. NOMENCLATURE Req. 16919 16475 30020 30717 31588 X DRAWING- PlatesInstallation, Ice Shield X2 DRAWING- CompleteFuselageAssembly DX DRAWING- Complete FuselageAssembly Y DRAWING- CompleteFuselageAssembly Y DRAWING- Complete FuselageAssembly Y DRAWING- CompleteFuselageAssembly Y DRAWING- CompleteFuselageAssembly SERIALNUMBERS AFFECTED 27-259 to 27-364 inclusive 27-2000 to 27-2504 inclusive 27-2505 to 27-3836 inclusive, 27-3838 to 27-3943 inclusive 27-3837, 27-3944 to 27-7554168 inclusive 27-7654001 and up 32650 33700 -1 16300-00 30186-00 30049-00 30186-02 30700-00 30700-02 30700-03 AX A,E,X A.DX A,Z A,Y A,Y A,Y AY FUSELAGEASSEMBLY FUSELAGEASSEMBLY FUSELAGEASSEMBLY FUSELAGEASSEMBLY FUSELAGEASSEMBLY FUSELAGEASSEMBLY FUSELAGEASSEMBLY 1 1 1 1 27-1 to 27-402 inclusive 27-403 to 27-504 inclusive 27-259 to 27-364 inclusive 32137-00 A,Y FUSELAGEASSEMBLY 32617-00 A,Y FUSELAGEASSEMBLY 32617-02 A,Y FUSELAGEASSEMBLY 1 27-2000 to 27-2299 inclusive 1 27-2300 to 27-2504 inclusive 1 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 1 27-3050, 27-3154 to 27-3836, 27-3838 to 27-3943 inclusive 1 27-3837, 27-3944 to 27-4425, 27-4427 to 27-4573 inclusive 1 27-4426, 27-4574 to 27-7554168 inclusive 1 27-7654001 and up 33701-02 -2 16230-00 30660-00 30660-02 30660-03 32616-00 -3 16210-00 30410-00 30410-12 A,Y BX,Z B,Y B.Y B,Y B,Y C,X,Z C,Y C.Y FUSELAGEASSEMBLY * FUSELAGEASSEMBLY- (Centersection) * FUSELAGEASSEMBLY- (Centersection) * FUSELAGEASSEMBLY- (Centersection) * FUSELAGEASSEMBLY- (Centersection) 1 1 1 1 27-2000 to 27-2299 inclusive 27-2300 to 27-2504 inclusive 27-2605 to 27-3836 inclusive, 27-3838 to 27-3943 inclusive 27-3837, 27-3944 and up FUSELAGEASSEMBLY- (Center section) * FUSELAGEASSEMBLY- (Aft section) FUSELAGEASSEMBLY- (Aft section) * FUSELAGEASSEMBLY- (Aft section) 1 1 32044-00 C,Y * FUSELAGEASSEMBLY- (Aft section) 32609-00 CY * FUSELAGEASSEMBLY- (Aft section) 32609-02 CY * FUSELAGEASSEMBLY- (Aft section) 32609-03 C,Y * FUSELAGEASSEMBLY- (Aft section) 1 27-2000 to 27-2504 inclusive 1 27-2506 to 27-3049 inclusive, 27-3061 to 27-3153 inclusive 1 27-3050, 27-3154 to 27-3836, 27-3838 to 27-3943 inclusive 1 27-3837, 27-3944 to 27-4425 27-4427 to 27-4573 inclusive 1 27-4426, 27-4574 to 27-7554168 inclusive 1 27-7654001 and up A - See Figure 6, 6A, 7, 7A, 8 and 9 for componentparts. B - See Figure 7 for componentparts. C - See Figure 8 for componentparts. D - Usedwhen 28-volt electrical system is installed. E - Usedwhen 14-volt electrical system is installed. X - Usedon PA-23-250 airplanes only Y - Usedon PA-23-250(Six Place)airplanesonly. Z - Used on PA-23-235 airplanes only When ordering, always specify Part Number, Descriptionand Serial Numberof Aircraft REVISED:MARCH1980 PA-23-250 (Six Place) PA-23-250, PA-23-235 1B13 PIPER PARTS CATALOG REVISED: SEPTEMBER 10, 2008 PA-23-250 (Six Place) PA-23-250, PA-23-235 1B14 Figure and Index Number Part Number Code NOMENCLATURE No. Req. SERIAL NUMBERS AFFECTED COMPLETE FUSELAGE SECTION II Fuselage Group 5-4 16228-00 A,X,Z * FRAME ASSEMBLY - Fuselage 1 30392-00 A,Y * FRAME ASSEMBLY - Fuselage 1 27-2000 to 27-2504 inclusive 30392-04 A,Y * FRAME ASSEMBLY - Fuselage 1 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 30392-05 A,Y * FRAME ASSEMBLY - Fuselage 1 27-3050, 27-3154 to 27-7554168 inclusive 30392-06 A,Y * FRAME ASSEMBLY - Fuselage 1 27-7654001 and up -5 17413-03 HANDLE - Cabin assist 1 -6 99479-02 V GAUGE - Air temperature 1 27-1 to 27-2712 inclusive 41707-00 Y GAUGE - Air temperature (Maxwell, Manning & Moore, Inc.) 1 27-2713 and up 54507-04 GAUGE - Air temperature (Rochester) 1 27-8054001 and up -7 404 999 NUT - (AN365-428) 1 -8 18230-00 X,Z SUPPORT ASSEMBLY - Fuselage skin 1 -9 18231-00 * BRACKET ASSEMBLY - Fuselage skin support 1 -10 17387-00 * PAD ASSEMBLY - Fuselage skin support 1 758 745 * BUMPER 1 404 224 * HEX NUT (AN315-3R) 1 416 780 * SCREW (MS35191-280) 1 -11 189 625 GROMMET - Engine control support 2 -12 19734-00 STEP ASSEMBLY - Fuselage 1 27-1 to 27-4080 inclusive 19734-07 STEP ASSEMBLY - Fuselage 1 27-4081 and up -13 400 009 BOLT - (AN4-14A) 1 -14 690 611 WASHER - (NAS1149F0463P) 1 -15 19883-02 X,Z PLATE - Ice shield center, left 1 19883-03 X,Z PLATE - Ice shield center, right 1 -16 19883-06 X,Z PLATE - Ice shield lower, left 1 19883-07 X,Z PLATE - Ice shield lower, right 1 -17 19883-04 X,Z PLATE - Ice shield upper, left 1 19883-05 X,Z PLATE - Ice shield upper, right 1 -18 487 587 X,Z STUD - (#2600-5) 2 -19 494 057 X,Z WASHER - Split (#2600-SW2) 2 -20 17413-03 Y HANDLE - Cabin assist 1 27-3623 and up -21 31711-00 Y GASKET - Air temperature gauge attachment 2 27-2713 and up -22 31710-02 Y BUSHING - Air temperature gauge, interior 1 27-2713 and up 31710-03 Y BUSHING - Air temperature gauge, exterior 1 27-2713 and up -23 81342-101 Y WASHER - Air temperature gauge 2 27-2713 and up -24 81342-08 Y WASHER - Air temperature gauge 1 27-2713 and up A - See Figure 9 for component parts. V - These parts must be ordered from Service Spares Department, Piper Aircraft Corporation, Vero Beach, Florida. X - Used on PA-23-250 airplanes only. Y - Used on PA-23-250 (Six Place) airplanes only. Z - Used on PA-23-235 airplanes only. When ordering, always specify Part Number, Description, and Serial Number of Aircraft P I P E R A I R AI C R A F T C O R P O R A T I O N Figure 6. FuselageForward Section 1B15 REVISED: OCTOBER1976 PA-23-250,PA-23-235 FUSELAGE FORWARD SECTION (PA-23-250 and PA-23-235) SECTION II Fuselage Group Figure and Index Number Port Number NOMENCLATURE SERIAL NUMBERS AFFECTED 27-1 to 27-402 inclusive 27-259 to 27-364 inclusive 6- 16300 30049 19447 16828 30186 DRAWING - D DRAWING - DRAWING - B DRAWING - CX DRAWING - Fuselage Assembly Fuselage Assembly Fuselage Forward Section Shelves Installation Fuselage Assembly 27-403 and up -1 17262-00 -2 17216-00 -3 17244-00 -4 17214-00 -5 17247-00 -6 17245-00 -7 17248-00 -8 17252-00 -9 751 228 -10 80122-69 -11 80122-70 -12 80122-71 -13 19447-19 -14 17787-00 16819-00 16827-00 16827-02 -15 17785-00 16825-00 -16 17786-00 16826-00 -17 16823-00 16823-01 -18 30663-02 -19 30662-02 -20 16866-00 30035-00 16885-00 19860-00 19860-03 30340-00 -21 19553-04 -22 19553-02 -23 17360-10 -24 19515-00 ANGLE - Baggage compartment door frame, upper rear corner ANGLE - Baggage compartment door frame, rear 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 ft. section) WASHER - Shim (.032) WASHER - Shim (.064) WASHER - Shim (.125) PANEL ASSEMBLY - Right rear, side A SHELF - Radio power supply B SHELF ASSEMBLY - Rear radio support E SHELF - Lower radio support F SHELF - Lower radio support A BRACKET - Radio shelf, left B BRACKET - Radio shelf support, left A BRACKET - Radio shelf, right B BRACKET - Radio shelf support, right B SHELF ASSEMBLY - Side radio support, left B SHELF ASSEMBLY - Side radio support, right PANEL - Fuselage access, left rear PANEL - Fuselage access, right front PANEL ASSEMBLY - Instrument D PANEL ASSEMBLY - Instrument B PANEL ASSEMBLY - Instrument B PANEL ASSEMBLY - Instrument B PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument TOP ASSEMBLY - Forward section SKIN - Rear top SKIN - Center top assembly STRINGER 1 1 1 1 I 1 1 1 AR AR AR I 1 1 I I1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 27-1 to 27-402 inclusive 27-259 to 27-364 inclusive 27-1 to 27-366 inclusive 27-367 to 27-430 inclusive 27-431 and up 27-403 and up A - Used when Collins Radio installation is not used. B - Used when Collins Radio installation is installed. C - Used when 14 Volt electrical system is installed. D - Used when 28 Volt electrical system is installed. E - This cannot be used when receptacle is installed. F - Used when receptacle is installed. X - Used on PA-23-250 airplanes only. When ordering, always specify Port Number, Descriptionand Serial Number of Aircraft 1B16 REVISED: MAY 1975 PA-23-250 PA-23-235 SECTION II Fuselage Group FUSELAGE FORWARD SECTION (PA-23-250 and PA-23-235) Figure and Index Number Port Number NOMENCLATURE 6-25 19535-00 19535-01 -26 17360-23 -27 17346-00 -28 17345-00 17345-01 -29 17346-01 -30 17504-02 19826-00 -31 17344-00 -32 17358-06 -33 17358-05 -34 484 342 -35 17354-01 -36 17354-00 -37 17348-01 -38 17348-00 -39 19447-18 -39a 19802-02 -39b 487 584 -39c 494 060 -39d 19802-03 -3 9 e 487 584 -39f 494 060 -39g 484 342 -40 19327-00 19327-05 -41 17300-12 -42 17360-13 -43 17360-14 -44 17360-15 -45 19327-03 -46 19326-00 -47 17497-04 -48 17497-05 -49 19447-13 -50 487 584 -51 494 057 -52 19447-20 19830-00 30063-00 30063-03 -53 18817-00 -54 17758-03 -54a 30060-02 -54b 30060-03 -55 18340-00 -56 17504-05 19827-00 BULKHEAD ASSEMBLY - Top, station 55, Lll BULKHEAD ASSEMBLY - Top, station 55, RH BULKHEAD ASSEMBLY - Fuselage forward section CHANNEL - Fuselage bulkhead, upper left CHANNEL - Fuselage bulkhead, upper left CHANNEL - Fuselage bulkhead, upper right CHANNEL - Fuselage bulkhead, upper right X BULKHEAD - Upper BULKHEAD - Upper BRACKET - Fuselage bulkhead CHANNEL - Fuselage forward section, left CHANNEL - Fuselage forward section, right RECEPTACLE - (#2600-212-12D) ANGLE - Fuselage forward section, right ANGLE - Fuselage forward section, left ANGLE - Fuselage forward section, right ANGLE - Fuselage forward section, left PANEL ASSEMBLY - Left front side PLATE ASSEMBLY - Access, powerpak filler line STUD - Slotted head (#2600-2) LOCK WASHER - (#2600-LW) PLATE ASSEMBLY - Access, brake fluid reservoir STUD - Slotted head (#2600-2) LOCK WASHER - (#2.600-LW) RECEPTACLE - Stud (#212-121)) A SECTION ASSEMBLY - Fuselage nose B SECTION ASSEMBLY - Fuselage nose SKIN - Nose, left side SKIN - Nose, right side SKIN - Nose, front top SKIN - Nose, front bottom PLATE ASSEMBLY - Landing light compartment back FAIRING - Fuselage nose BULKHEAD ASSEMBLY - Top, station 6 BULKHEAD ASSEMBLY - Bottom, station 6 PANEL ASSEMBLY - Right front side STUD - (#2600-2) WASHER - (#2600-SW2) A BOTTOM ASSEMBLY - Fuselage forward section A BOTTOM ASSEMBLY - Fuselage forward section B BOTTOM ASSEMBLY - Fuselage forward section B BOTTOM ASSEMBLY - Fuselage forward section PLATE - Nose wheel well reinforcement TUBE ASSEMBLY - Vent, battery box B TUBE ASSEMBLY - Battery box ventilating B TUBE ASSEMBLY - Battery box ventilating PLATE - Wheel well stiffener BULKHEAD ASSEMBLY - Lower BULKHEAD ASSEMBLY - Lower Zz 1 2 1 1 I I 1 1 1 1 1 1 1 2 1 12 1 1 1 1 11 1 1 4 4 1 1 1 1 1 3 1 1 1 1 1 SERIAL NUMBERS AFFECTED 27-1 to 27-366 inclusive 27-367 and up 27-1 to 27-366 inclusive 27-367 and up 27-1 to 27-366 inclusive 27-367 and up 27-1 to 27-366 inclusive 27-367 and up A - Used with 14 Volt electrical system. B - Used with 28 Volt electrical system. X - Used on PA-23-250 airplanes only. When ordering, always specify Port Number, Description and Serial Number of Aircraft 1B17 REVISED: MAY 1975 PA -23-251) PA-23-235 FUSELAGE FORWARD SECTION (PA-23-250 and PA-23-2351 SECTION II FuselageGroup Figure and Index Number Part Number C 6-57 17347-00 -58 19447-04 -59 19447-05 A 30063-02 B 19447-05 B -60 19447-02 -61 19447-03 -62 17356-12 X 17356-14 X 17356-14 Z -63 17356-01 X 17356-15 X 17356-15 Z -64 17353-01 -65 17353-00 -66 1664500 -67 16645-01 -68 484 342 -69 30068-00 B -70 30069-00 B -71 16822-00 C -72 22478-05 Z -73 22482-00 Z -74 31128-00 Z -75 16633-34 Z :ode NOMENCLATURE PLATE - Nose wheel well, end SKIN - Left forward SKIN - Right forward SKIN - Right forward SKIN - Right forward SKIN - Left rear SKIN - Right rear BULKHEAD AS