AZTEC PARTS CATALOG

PIPER Aztec PA-23-250 · Parts Catalog

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Overview

The Piper Aztec PA-23-250 Parts Catalog provides detailed information for identifying and ordering replacement parts for the PA-23-250 Aztec and PA-23-235 Apache aircraft models. It includes a comprehensive parts list, illustrations, and guidelines for ordering parts, ensuring users can effectively maintain their aircraft.

The catalog is divided into eleven major sections.
It includes replacement parts for the PA-23-250 and PA-23-235 models.
Optional equipment parts are listed in the catalog.
Replacement parts for certain avionics and autopilot installations are not included for specific serial numbers.
Ordering parts requires specifying the model and serial number.
The catalog contains a standard paint chart for exterior finishes.
Revisions to the catalog are periodically issued to keep information current.
Attaching parts like nuts and bolts are generally not supplied by Piper.

Document

Source

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

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Document details

Type: Parts Catalog
Year: 1984
File size: 38 MB
Publisher: aeroelectric.com
Language: en

About this document

What is the AZTEC PARTS CATALOG?

The AZTEC PARTS CATALOG is a parts catalog for the PIPER Aztec PA-23-250, dated 1984.

Where does the AZTEC PARTS CATALOG come from?

This copy of the AZTEC PARTS CATALOG was originally published by aeroelectric.com and is hosted on Sprinkle as a free, searchable reference copy.

What year was the AZTEC PARTS CATALOG published?

The AZTEC PARTS CATALOG — the PIPER Aztec PA-23-250 parts catalog on file — is dated 1984.

Documentation completeness

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In this document

Introduction

This section explains the purpose of the Parts Catalog and emphasizes that it should not be used for rigging and installation purposes.

How to Identify a Part

Guidelines are provided for identifying parts based on their appearance and location within the aircraft.

How to Order Parts

Instructions for ordering parts, including necessary information to provide to ensure correct orders.

Serial Number Information

Details the serial number ranges for different models of the Aztec and Apache aircraft.

Revisions

Lists the history of revisions to the catalog, ensuring users have the most current information.

Standard Paint Chart

Provides a list of exterior paint colors available for the aircraft, including enamel and acrylic lacquer options.

Safety notes

This catalog should not be used for rigging and installation purposes.
Claims for errors or shortages must be made within three days after receipt of orders.
No material should be returned without prior written permission from Piper.
The Piper Aircraft Corporation is not liable for damages to parts in transit.

Full document text

AZTEC P A R T S CATALOG CARD 1 OF 3 PA-23-235 APACHE PA-23-250 AZTEC PA-23-250 [Six place) AZTEC PIPER A I R C R A F T C O R P O R A T I O N a 1 A l [PART NUMBER 753 5221 Courtesy of Bomar Flying Service www.bomar.biz PIPER PARTS CATALOG AEROFICHE EXPLANATION AND REVISION STATUS The Pans Catalog ~nformationincorporated i n this set of Aerofiche cards has been arranged i n accordance with the general specificat~onsof Aerofiche adopted by the General Aircraft Manufacturer's Association Conversion of Aerofiche alpha/numeric code numbers: First number is the Aerofiche card identifier Letter is the horizontal line reference per card Second number is the vertical line reference per card Example: 2J16 = Aerofiche card number two of given set, Grid location J16 To aid in locating the various sections and related information desired, the following is provided: A complete Catalog Table of Contents is given at Grid 1A8 of Aerofichecard number 1 of this set Each additional card in this set will have a Table of Contents for all sections on that particular card This table will start at Grid A 3 REVISIONS The information compiled In this Aerofiche Parts Catalog will be kept current by revisions distributed periodically These revisions will supersede all previous revisions and will be complete Aerofiche card replacementsand shall supersede Aerofiche 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 NOTE: Refer to the last card of the Piper - Pans Price List - Aerofichefor a check list of current revision dates and card effectivities for this pans catalog REVISED JULY 1984 PA-23-250 (Six Place) PA-23-250, PA-23-235 a PIPER PARTS CATALOG INTRODUCTION T h ~ s~llustraredParts Catalog IS des~gnedto prov~des~mplebut posltlve ldentlflcat~onof replacement parts for the P~perModels PA-23-250. PA-23-250 (SIX Place) Aztec. and Model PA-23-235 Apache. manufactured by the P~perA~rcraftCorporat~onof Lock Haven. Pennsylvan~a NOTE UNDER NO CIRCUMSTANCES SHALL THIS CATALOG BE USED FOR RIGGING AND INSTALLATION PURPOSES It IS suggested that t h ~ scatalog be thoroughly studied to determ~neits arrangement prlor to its utilization 1 The catalog IS d ~ v ~ d e d Into eleven (1 1 ) major sectlons described as follows a Sect~onsI to X ~ n c l u s ~ v e contaln all replacement parts for the complete a~rplaneEach sectlon IS subd~v~ded and each dlv~slonIncludes an ~llustrat~on and a parts llstlng b Sect~onXI 1s the M~scellaneousGroup Thls group Includes a llstlng of the Opt~onalEquipment K~ts,Repa~rK ~ t sand Specla1 Tools 2 The follow~ng1s a br~efexplanat~onof the columns In the parts llsts (Refer to EXAMPLE below) a The "FIGURE AND INDEX NUMBER"column ~nd~catesthe~llustrat~onf~gure numberand~tspartsIndexnumber EXAMPLE (2-1).the 2 IS the f~gurenumber and the 1 IS the Index number The f ~ g u r enumber appears only at the top of each parts 1st page b The "PART NUMBER" column contalns the ~ d e n t ~ f y ~ n g number of the replacement part and t h ~ snumber must be shown on all Parts Orders c The "CODE" column IS for the purpose of ~ n d ~ c a t ~ n g spec~aluses of the part An explanat~onof the letter code used IS shown on the grid (page) preced~ngeach parts l ~ s t ~ n g and pertalns to that llstlng only d The "NOMENCLATURE" column ~nd~cates the part name T h ~ sname must be shown on all Parts Orders e The "NO REQ" (Number Requ~red)column represents the total quantlty of parts used per a~rcraftper f ~ g u r ewhen the part IS not ~ndentedand the quant~tyof parts used per assembly when the part IS Indented The symbol "AR" llsted In t h ~ scolumn means "As Required" f The "SERIAL NUMBERS AFFECTED" column lnd~catesthe part appl~cat~on by a~rplaneser~alnumber Figure and Index Number 2- 1 -2 - 3 -4 EXAMPLE I I Part Number Code 1 NOMENCLATURE SERIAL NUMBERS 1 AFFECTED 1; the Nomenclature column, the next h~gherassembly relat~onshtpofitemscovered IS shown by thedegreeof lndent~onof each Item and IS ~ n d ~ c a t e d by an aster~sk(') One asterlsk s ~ g n ~ f ~ e s one ~ndent~on, t w o slgnlfles two ~ndentlons,etc The example l ~ s t ~ n g above IS Interpreted as follows XXXXX-XX XXXXX-XX XXXXX-XX XXXXX-XX If the DOOR ASSEMBLY (not Indented) IS ordered, it will include the three items indented under the Door Assembly If the TUBE ASSEMBLY (Indented one space) 1s ordered, it will include the two items indented under the Tube Assembly DOOR ASSEMBLY - Baggage compartment 'TUBE ASSEMBLY - Baggage door latch ' ' CLEVIS - Door latch tube assembly ' CLIP - Door latch tube assembly If you want only a CLEVIS or CLIP, you order only that item , X X X X 3 The "ATTACHING PARTS" such as nuts, bolts, screws. etc . that are available as commercial hardware items, are not generally supplied by the

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P~perA~rcraftCorporat~or! Thls catalog lists for your convenience, those attaching pans required for main assemblies and lnstallat~onsThe Identifying number for these parts appears after the part name 4 All Items of Opr~onalEqu~pmentare conta~nedIn the parts 1st In thew proper sequence and sectlons These Items were not marked optional. slnce they are fully ldent~f~ed by t h e ~ rdescr~pt~ons REVISED JULY 1984 PA-23-250 (SIX Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG SPECIAL NOTE I Effectlve on PA-23-250 (Six Place) with serial numbers 27-7954061 and up, replace- ment parts for Optional Avlonlcs and Electronics lnstallat~ons( i e radar, radio altimeter, encoding altimeter. etc ) are not being listed or illustrated i n this parts catalog Effective on PA-23-250 (Six Place) wlth serial numbers 27-8054001 and up. replace- ment parts for Optlonal Autopilot lnstallat~onsare not being listed or illustrated i n this parts catalog If replacement parts are required for aircraft with these serial numbers, refer to the Avlonics Drawing lndex Llst and the approprlate drawings supplied with each alrcraft to determine part number of deslred part HOW TO IDENTIFY A PART IF YOU KNOW WHAT IT LOOKS LIKE AND KNOW WHERE IT IS LOCATED 1 Refer to Flgure 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 i n thls group 4 Refer to the "Flgure and lndex Number" I n the Parts Listing for complete description of the part HOW TO ORDER PARTS I n ordering parts for your Piper airplane, observe the following rnstructions which will aid i n your gettlng the right parts requlred without delay a Place your order wlth the distributor or dealer for your territory, since parts are available only through our distributor organlzatlon b Always specify the model and serial number of your airplane c Always specify Part Number, Name. Type and Quantlty required d Specify the method of shlpment - freight, express, parcel post, air express, air freight, or air parcel post Where the nature of the shipment requlres 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 clalms for errors or shortages must be made withln 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 i n 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 Corporat~oncannot be held liable for damages to parts i n transit from the factory If a shipment is received i n a damaged condition, have the delivery man or Transportation Company make a notation of the damage and file your claim with the Carrier I n case of concealed damage, do not attempt to remove the pan 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 REVISED AUGUST 1981 PA-23-250 (Six Place) PA-23-250. PA-23-235 PIPER PARTS CATALOG a PA-23-235, PA-23-250 AND PA-23-250 (SIX PLACE) SERIAL NUMBER INFORMATION The followtng information should be kept in mind when ordertng from this Catalog: a The serial numbers of the aircrah covered by this Pans Catalog are as follows: (1) Serial numbers of the 1960 "Aztec" PA-23-250 Models are 27-1 to 27-366 inclusive (2) Serial numbers of the 1961 "Aztec" PA-23-250 Models are 27-367 to 27-504 inclusive (3) Serial numbers of the "Apache" PA-23-235 Models are 27-505 to 27-622 inclusive (4) Serial numbers of the "Aztec" PA-23-250 (Six Place) Model "B" are 27-2000 to 27-2504 inclusive. (5) Serial numbers of the "Aztec" PA-23-250(Six Place) Model "C" are 27-2505 to 27-3836 inclusive, 27-3838 to 27-3943 inclusive (6) Serial numbers of the "Aztec" PA-23-250(Six Place) Model "D" are 27-3837.27-3944 to 27-4425 inclusive. 27-4427 to 27-4573 inclusive (7) Serial numbers of the "Aztec" PA-23-250 (Six Place) Model "EMare 27-4426, 27-4574 to 27-7554168 inclusive (8) Serial numbers of the "Aztec" PA-23-250 (Six Place) Model "F" are 27-7654001 and up REVISED: SEPTEMBER 1978 PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG STANDARD PAINT CHART EXTERIOR ENAMEL Dmona White Santa Fe Red Behama Blue Hershey Brawn Montego Green Yukon Yellow Pontiac Red Phoenix Tan Orlando Green Lakeland Blue Dakota Black El Pam Brown Tamps Green Nbwport Blue ACRYLIC LACQUER Daytona White Pontiac Red Phoenix Tan Orlando Green Lakeland Blue Dakota B l a l El Pam Brown Tamps Green (base coat) Tamp. Green (top coat) Nbwpon Blue (base coat) N q Blue (top coat) Juneau White Mocha Tan Denver B r m (bas4 cow) Denver B r m (top coat) Madrid Red (ku,colt) Madrid red (top coat) Lincoln Gray Bimini Turquoise N a s ~ uTurquoise Reno Gold (bare coat) Reno Gold (top corn) B ~ u m o mBlue Dallas Yellow Ocala Orange (base coat) Ocala Orange (top coat) Polar Gray Montwey Marwn (base coat) Montwey Maroon (top coat) Bahama Blue Lam V q a s GoM ( b a n coat) Lar Vogn Gold (tap coat) Avocado MFG. NO. PIPER PART NUMBER QUART GALLON REVISED: MARCH 1980 PA-23-260 (Six Place) PA-23-260, PA-23-236 PIPER PARTS CATALOG STANDARD PAINT CHART MFG. NO ACRYLIC LACQUER (cont ) Baja Yellow (base coat) Baja Yellow (top coat) Lime Green (base coat) Lime Green (top coat) Saffron Claret (base coat) Claret (top coat) Firethorn (base coat) Firethorn (top coat) Dark Blue Sage Green Buckskin Hickory Brown Silver Sandalwood Tan Platinum Gray Thinner (fast drying) Titanine Thinner (slow drying) Titanine POLYURETHANE ENAMEL (Titanine) Flat Black Juneau White Claret Silver Sage Green Firethorn Saffron Buckskin Dark Blue Hickory Brown Sandalwood Tan Dakota Black Las Vegas Gold Lime Green Platinum Gray Bahama Blue Madrid Red Baja Yellow Ocala Orange Catalyst Reducer POLYURETHANE PRIMER (Titanine) Primer Reducer Catalyst Epoxy Primer Epoxy Reducer Epoxy Converter PIPER PART NUMBER QUART GALLON REVISED: MARCH 1980 PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER 1 FIGURE TITLE View of Complete Airplane ............................................................ SECTION I WING GROUP Wing Installation ..................................................................... Flap Assembly and Aileron Assembly .................................................. Wing and Wing Tip Construction ....................................................... Wing and Wing Tip Skin .............................................................. SECTION II FUSELAGE GROUP Complete Fuselage .................................................................. Fuselage Forward Section (PA.23.235. PA-23-250) ..................................... Fuselage Forward Section (PA.23.25016) ............................................... Fuselage Center Section .............................................................. .............................................................. Fuselage Bonom Fairing Fuselage Aft Section .................................................................. ...................................................................... Fuselage Frame lnstrument Panel lnstallation (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl . 27-3838 to 27-3943 incl ) ........................................................ lnstrument Panel lnstallation (PA-23-250(6)S/N 27.3837. 27-3944 to 27-7305221 incl . 27-7305223 to 27-7305234 incl ) .................................... lnstrument Panel lnstallation (PA-23-250(6) S/N 27.7305222 . 27-7405235 to 27-7405476 incl ) .................................................................... Instrument Panel Installation (PA-23-250(6) S/N 27-7554001 and up) ................... Dual Instrument Panel lnstallation (PA-23-250(6) S/N 27-7405235 to .................................................................... 27-7405476 incl ) Dual Instrument Panel Installation (PA-23-250(6) S/N 27-7554001 and up) .............. Dual Instrument Lines and Right Pitot Static System Installation ......................... Control Pedestal Installation ........................................................... Floorboard and Cockpit Finishing lnstallation (PA-23-235/2SO/250(6) S/N 27-1 to 27-3836 incl . 27-3838 to 27-3943 incl ) ............................................ Cockpit Finishing Installation (PA-23-25q6) S/N 27.3837. 27-3944 and up) .............. Floorboard Installation (PA-23-250(6) S/N 27.3837. 27-3944 and up) .................... Window Curtains Installation .......................................................... Fuselage Enclosure Installation ........................................................ Baggage Door Assembly and Cabin Door Assembly (PA-23-235/250/250(6) S/N 27-1 to 27-7554168 incl ) ............................................................. Baggage Door Assembly and Cabin Door Assembly (PA-23-25016)S/N 27-7654001 and up) .................................................................. Oxygen System Installation (PA-23-250) ............................................... Oxygen System lnstallation (PA-23-250(6) S/N 27-2000 to 27-3049 incl . 27-3051 to 27-3163 incl ) ............................................................. Oxygen System lnstallation (PA-23-250(6) S/N 27.3050 . 27-3154 to 27-3836 incl . 27-3838 to 27-3943 incl ) ........................................................ Oxygen System Installation (PA-23-250(6)S/N 27.3837. 27-3944 and up) ............... Seats lnstallation (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl . 27-3838 ..................................................................... to 27-3943 incl ) Seats Installation (PA-23-2W6) S/N 27.3837 . 27-3944 to 27-7554168 incl ) ............ Seats Installation (PA-23-250(6) S/N 27-7654001 and up) .............................. GRID NUMBER 1A13 1J10 1K1 1K l O REVISED JULY 1984 PA-23-250 (Six Place) PA.23.250. PA-23-235 PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER SECTION Il (cont ) FUSELAGE GROUP Vacuum Pump Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.). .......... Vacuum Pump Installation (PA-23-250(6) S/N 27-2505 and up) ......................... Airspeed. Static. Oil Pressure and Manifold Pressure Lines .............................. Ventilating System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl ) ....... Ventilating System lnstallation (PA-23-250(6) S/N 27-2505 to 27-3836 incl . ............................................................. 27-3838 to 27-3943 ~ n c l) Ventilating System Installation (PA-23-250(6) S/N 27.3837. 27-3944 and up) ............ Heater Instajlation (PA-23-235/250/250(6) S/N 27-1 to 27-3049 incl . 27-3051 ..................................................................... to 27-31 53 incl ) Heater Installation (PA-23-250(6)S/N 3050. 27-3154 and up) ........................... Heater Assembly (Stewart Warner) .................................................... ............................................................. Janitrol Heater Assembly Janitrol Heater Components ........................................................... SECTION Ill CHASSIS GROUP ... ................................................................ 2 3 ................................................................ Gear Strut Assemblies 24 Nose Gear Installation ............................................................... 24A Nose Wheel Assembly 25 Main Gear Installation ................................................................ 26 Main Wheel Assembly ................................................................ ..................................................................... 27 Brake Installation ................................................................ 27A Dual Brake Installation ...................................................................... 28 Brake Assembly SECTION IV TAIL SURFACES GROUP Tail Installation ...................................................................... 2016 Stabilator Assembly (PA-23-235/250/250(6) S/N 27-1 to 27-76541 68 incl . 27-8054001 and up) .................................................................. 2B20 Stabilator Assembly (PA-23-250(6) S/N 27-7654001 to 27-7954121 incl ) ............... 2822 Rudder Assembly ..................................................................... 2Cl Fin Assembly ......................................................................... 2C4 SECTION V POWER PLANT GROUP Power Plant Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl ) ............. Power Plant Installation (PA-23-250(6) S/N 27-2505 and up) ............................ Turbocharger Installation (Airesearch) .................................................. Turbochargerlnstallation (Lycoming) ................................................... Propeller (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ........................... Propeller (PA-23-250(6) S I N 27-2505 and up) .......................................... Propeller Synchronizer System Installation ............................................. Propeller Synchrophaser System Installation ............................................ Engine Baffle Installation.............................................................. REVISED JULY 1984 PA-23-250 (Six Place) PA.23.250. PA-23-235 PIPER PARTS CATALOG TABLE OF 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 ) ....... 2012 33A Exhaust System Installation (PA-23-25016)S/N 27-2505 and up) ........................ 2014 34 Nacelle Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ................. 2016 34A Nacelle Installation (PA-23-2W6) S/N 27-2505 and up) ................................ 2E1 348 Nacelle Installation (Lycoming Turbocharger) ........................................... 2E8 SECTION VI FUEL SYSTEM GROUP Fuel System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl ) ............. Fuel Injection System Installation (PA-23-250(6) S/N 27-2322 to 27-2504 incl ) .......... Fuel System Installation (PA-23-250(6) S/N 27-2505 and up) ............................ Fuel Cell Installation (PA-23-235/250/250(6) S/N 27-1 to 27-4815 incl ) ............... Fuel Cell lnstallat~on(PA-23-2W6) S/N 27-4816 and up) ............................... Wing Tip Fuel Tank Installation (PA-23-250(6) S/N 27-7654001 and up) ................. Fuel System Control Box (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl ) ............ Fuel System Control Box (PA-23-2W6) S/N 27-2505 and up) .......................... SECTION VII ELECTRICAL SYSTEM GROUP Fuselage Electrical System Installation (PA-23-235/250) ................................ Fuselage Electrical System Installation (PA-23-250(6) ................................... Wing Electrical System Installation (PA-23-235/250) ................................... Wing Electrical System Installation (PA.23.250(6) ....................................... Battery Box Installation (PA-23-235/250) .............................................. Battery Box Installation (14-Volt) (PA.23.250(6) ......................................... Battery Box Installation (28-Vott) (PA-23-25016)S/N 27-2298 to 27-7954097 incl ) ....... ................ Battery Box lnstallation (28-Volt) (PA-23-250(6) S/N 27-7954098 and up) ......................................................... Pedestal Electrical lnstallation lnstrument Panel Electrical lnstallation (PA-23-235/250/250(6) S/N 27-1 to ........................................................................ 27-2504 incl ) Instrument Panel Electrical Installation (PA-23-25016) S/N 27-2505 to 27-3836 ........................................................ incl . 27-3838 to 27-3943 incl ) Instrument Panel Electrical Installation (PA-23-25016)S/N 27.3837. 27-3944 and up) .... Taxi Light Installation ................................................................. .............................................................. Strobe Lights Installation .......... External Power Supply (PA-23-235/250/250(6) S/N 27-1 to 27-7954097 incl ) External Power Supply (PA-23-250(6) S/N 27-7954098 and up) ......................... Propeller Deicer Installation (PA-23-250) ............................................... ............................................. Propeller Deicer Installation (PA-23-250(6) Pneumatic Deicer Installation (B F. Goodrich) .......................................... .......................................... Pneumatic Deicer Installation (B F Goodrich) Pneumatic Deicer lnstallation (Airborne/Goodyear) (PA-23-2-6) S/N ..................................................... 27-75541 12 to 27-7554168 incl ) REVISED JULY 1984 PA-23-250 (Six Place) PA.23.250. PA-23-236 PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER FIGURE TITLE GRID NUMBER SECTION Vlll HYDRAULIC SYSTEM GROUP Hydraulic System Installation (PA-23-235/250/250(6) S/N 27-1 to 27-2504 incl.) ........ 2J1 Fuselage Hydraulic System Installation (PA-23-25q6) S/N 27-2505 and up) .............. 2J7 Wing Hydraulic System Installation (PA-23-250(6) S/N 27-2505 and up) ................. 2 J l l Hydraulic System Components (PA-23-25q6) S/N 27-2505 and up) ..................... 2J14 Landing Gear Anti-Retraction Valve Installation ......................................... 2J18 Hydraulic Powerpak Components ......................................................2J20 Hydraulic Powerpak Components ......................................................2K1 EmergencyGear Extender lnstallation (PA-23-235/250/250(6) S/N 27-1 to .................................................................... 27-7954121 incl ) 2K4 SECTION IX CONTROL SYSTEM GROUP Engine Controls Installation ...........................................................2K7 Stabilator Control Installation .......................................................... 2K10 Aileron Controls Installation ...........................................................2K13 Rudder Control Installation ............................................................ 2K16 Tail Trim Mechanism Installation ...................................................... 2K19 Trim Tab Interconnect System Installation .............................................. 2L1 SECTION X ELECTRONICS GROUP ..................................................... Collins and ARC Radio lnstallation Radio Junction Boxes (PA-23-235/250/250(6) S/N 27-1 to 27-3836 incl . ............................................................. 27-3838 to 27-3943 incl ) Radio Junction Boxes (PA-23-2m6) S/N 27.3837. 27-3944 to 27-4784 incl ) ............ Radio Junction Boxes (14-Volt) (PA-23-250(6) S/N 27-4785 and up) ..................... Radio Junction Boxes (28-Volt) (PA-23-250(6) S/N 27-4902 and up) ..................... ...................................................... Ail Weather Antenna Installation Piper Automatic Locator (ELT) Installation (Garrett Mfg. Ltd ) ............................. Piper Automatic Locator (ELT) Installation (Communications Components Corp ) ........... Piper Automatic Locator (ELT) Installation (Narco Avionics) ............................... Piper PM-1 Marker Beacon Installation (PA.23.250(6) ................................... .............................................................. Autocontrol l Installation 386 ............................................................. Autocontrol ll Installation 389 Autocontrol 111 Installation (PA-23-250(6) S/N 27-3457 to 27-7554071 incl.) ............. 3812 Autocontrol 111 B Installation (PA-23-250(6) S/N 27-7554071 and up) .................... 3814 ................................................................ AltiMatic I Installation 3816 ................................................................ AltiMatic II Installation 3819 ....................................................... AltiMatic Ill and Ill B Installation 3C1 ........................................................... AltiMatic Ill 0-1 Installation 3C5 AltiMatic Ill C Installation (PA-23-250(6)S/N 27.7554001. 27-7554074 and up) .......... 3C8 AltiMatic X F/D Autopilot Installation (PA-23-250(6) S/N 27-7854001 and up) ........... 3C12 AltiMatic X Autopilot Installation (PA-23-250(6) S/N 27-7864001 and up) ................ 3C15 AltiMatic V F/D and V F/D-1 Autopilot lnstallation (PA-23-250(6)S/N 27.4426. 27-4674 to ......................................................... 27-4574 to 27-7754093 incl.) 3C18 AltiMatic V and V-1 Autopilot lnstallation (PA-23-2m6) S/N 274426 . 27-4574 to .................................................................... 27-7754093 incl ) 3Dl REVISED JULY 1984 PA-23-250 (Six Place) PA.23.250. PA-23-235 PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER REVISED JULY 1984 FIGURE TITLE GRID NUMBER SECTION X (cont ) ELECTRONICS GROUP Autopilot/Flight Director lnstallation (Bendix FCS-810) (PA-23-25q6) S/N 27-7754094 to 27-79541 21 incl ) ..................................................... Autopilot lnstallation (Bendix FCS-810)(PA-23-250(6) S/N 27-7754094 .................................................................. to27-7954121 incl) King Autopilot (KAP-200) and King Autopilot F/D (KFC-200) Installation .................. Radar Altimeter Installation (PA-23-25q6)S/N 27-4794 and up) ........................ Glide Slope Coupler lnstallation (PA-23-25q6) S/N 27-7554001, 27-7554074 and up) .............................................................................. Radio Magnetic Indicator Installation (PA-23-25q6) S/N 27-4426, 27-4574 and up) ...... King Radar Installation (KWX-40) (PA-23-25q6) S/N 27-7554001 and up) ............... Bendix Radar Installation (RDR-150)(PA-23-250(6) S/N 27-7754001 and up). ............ Encoding Altimeter Installation (PA-23-250(6) S/N 27-7554001 and up). ................. Radio Installation and Wiring Diagram Drawings.. ...................................... SECTION XI MISCELLANEOUS GROUP Optional Equipment Kits. Repair Kits and Special Tools.. ................................ 3E12 Decals.. ............................................................................. 3E18 NUMERICAL INDEX 3F2 PA-23-250 (Six Place) PA-23-250. PA-23-235 P I P E R A I R C R A F T C O R P O R A T I O N X ELECTRONICS MI ELECTRICAL SYSTEM Y ~ Y I FUEL SYSTEM 7 IX CONTROL SYSTEM REVISED: OCTOBER 1976 Figure 1. View of Complno Airplum 1 A 1 3 PA-23-250 (Six P l e a ) PA-23-260. PA-23-236 PIPER PARTS CATALOG a REVISED: FEBRUARY 1979 Figure 2 Wing Installation 1A14 PA-23-250 (Six Place) PA-23-250, PA-23-235 SECTION I Wing Group WING INSTALLATION When or-ring, a l w s s m i f y Pan Number, DaKJiption and Serial Number of Aircnft Figure and Index Number 2- -1 -2 Y -3 ' -4 : -5 - -6 6s -7 -8 -9 -10 -11 -12 -13 -14 -15 -16 -17 -18 -19 REVISED: OCTOBER 1976 PA-23-250 (Six PI-) PA-23-25Q. PA-P-235 Pa* Number 16292 30698 33304 33900 16662 32717 16170-00 1617041 1617(MO 1617041 1617W0 1617029 1617026 1617025 1617028 1617027 16170-32 1617a31 333- 3 3 3 0 0 1 333W-06 3330007 17477-00 1747703 17477-02 18283-00 1747642 401 189 401 188 401 889 400 462 404 887 1946902 1946803 19303-00 401 289 407 664 401 365 1747604 1 7 4 7 W 1747505 400 444 401 395 407 S 7 4 W aB0 Code x.2 Y Y Y Y A,C.X A,C,X A,C,Z A,C,Z A,Z A.2 A,B,Y A,B,Y A,Y A,Y A,Y A,Y A.Y A,Y A,Y A,Y X,z X.2 Y X,Z Y SERIAL NUMBERS AFFECTED 27-2000 to 274815 inclusive 27-4816 to 27-7554168 incl. 27-7854001 and up 27-1 to 273888 includvr 27-3889and up 27-505 to 27-524 inclusive 27-505 to 27.- inclusive 27-525and up 27-525endup 27-2000 to 27-2269 inclusive 27-2000 to 27-2269 inclusive 27-2270 to 27-2504 inclusive 27-2270 to 27-2504 inclusive 27-2506 to 274815 inclusive 27-2505 t o 274815 inclusive 274816to27-7554168incl. 27-4816 to 27-7554168 incl. . 27-7854001 and up 27-7654001 and up 27-2000 to 27-2299 inclusive 27-2300and up NOMENCLATURE DRAWING -Wing lnstallatlon DRAWING -Wing Installetion DRAWING -Wing lnsmllation DRAWING -Wing Insmlletion DRAWING -Wing Fairing Installation DRAWING -Wing Fairing Installation PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Right wing PANEL ASSEMBLY - Left wing PANEL ASSEMBLY - Ri&t vving 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 - bft wing PANEL ASSEMBLY - Right wing STRAP - Spar attachment, lonsr rear STRAP -Spar attachment, lower mar STRAP - Spw attachment, lower front SHIM - Spar attachment STRAP - Spar attachmmt, upper front BOLT - (AN511A) BOLT - (ANSlQA) NUT - Self laking (MS20365524C) BOLT - (ANSI 1A) NUT - Self locking (MS203651032C) SHIM - Main spar amchmant, front .I87 SHIM - Main spar attachment, reor .I25 SHIM - Main spar attachment, .313 BOLT - (ANBlOA) WASHER - (AN960101 BOLT - (ANb26A) PLATE - Front g a r atmchmmt, bottom PLATE - Front g a r a t m c h m t , bottom PLATE - Front g a r attechant, top BOLT - (AN613A) BOLT - (AN614A) WASHER - (ANgB0616) NUT - (AN365424C) A -Sea Figumr 3 and 4 for cunponent wrts. B - I f Kit No. 754 493 has been installed, ordar wing p m r l 1617028 left or 1617027 right. C - I f Kit No. 754 493 has been installed, order wing pmal 1617W0 left or 1617G29 right. X - U d on PA-23.260 airplams only. Y - Umd on PA-23-250 (Six Place) alrplmm only. Z - Umd on PA-23-235airplanes only. No. Req. 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 AR 1 4 4 14 4 10 1 1 1 6 6 2 1 1 1 16 16 32 32 WING INSTALLATION SECTION I Wing G r w p When ordaring, a l w s specify Pan N u b r . Description and Snial Number of A i r m f t REVISED: SEPTEMBER 1977 1 A 1 6 Figure and Index Number 2-20 -20a -21 -22 -23 - 24 -25 -26e -26 -27 - 28 - 29 -30 -3 1 -32 -33 -34 -35 -36 -37 -38 -39 4 0 4 1 4 2 43 44 4 5 46 4 7 48 Pa* Number 162S-00 3Ce9740 61402-09 1 7 B M 3-96-00 176-5 30696-01 401 332 401 335 401336 407 565 404888 80122-87 174m-430 401 363 400 168 407 566 1752904 1S14-02 1e38Q02 18380-03 le3m-04 402 350 407 B 7 404 889 18166-06 18166-07 1979500 16674-00 1667441 3 x 6 4 4 0 3-1 1979600 1665900 1666901 1979540 1817640 18128-00 1812900 1813 W O 18131-00 1645740 410 044 17100-00 171DW1 Coda X,Z Y X,Z Y X,Z Y X,Z Y Y Y Y A A NOMENCLATURE BLOCK - Front war spacer, top BLOCK - Front spar spacer, top BUSHING - Front war apser, top BLOCK - F r m t spar spacer, front left top BLOCK - Front spar w e r . front left top BLOCK - Front spar spacur, front r i e t top BLOCK - Front spar spacer, front right top BOLT - (AN434A) BOLT - (AN440A) BOLT - (AN437AI WASHER - (AN9604161 NUT - Self locking (AN3654281 BUSHING - Rear spar attachment BLOCK - Front spar side attachment specer BOLT - (AN524A) BOLT - (AN5251 WASHER (AN96Q516) PIN -Wing tip hinm PIN -Wing tip hinge SHIM - (.020) SHIM - (.432) SHIM - (.0641 BOLT - Raar spar attachment (AN176-10A) WASHER - (AN0606161 NUT -Self locking (M-5624C) FAIRING ASSEMBLY - Left wing root. upper FAIRING ASSEMBLY - Right wing root, upper EXTRUSION - Rubber FAIRING ASSEMBLY - Left wing root, upper (Aluminum) FAIRING ASSEMBLY - Right wing root, upper (Aluminun) FAIRING ASSEMBLY - Left wing root, upper (Fihrglas) FAIRING ASSEMBLY - Right wing root, upper (FibargI~) EXTRUSION - Rubber FAIRING ASSEMBLY - Left wing root, l o w r FAIRING ASSEMBLY - Right wing mot, lower EXTRUSION - Rubber PLATE -Wing fmnt spar bolt c m r PLATE - Left wing root resr fairing PLATE - R i e t wing root mar fairing FAIRING ASSEMBLY - Left wing root mar FAIRING ASSEMBLY - Right wing root rear RING - T i dorm SCREW - (ANSOBIOR-15) AILERON ASSEMBLY - Left wing AILERON ASSEMBLY - Right wing A - See Figum 2A for component parts. X - Uaed on PA-23-250airplam only. Y - Usai on PA-23-250 (Six Place) airplmes only. Z - Uwd on PA-23-236airplanes only. No. RW . 2 2 2 1 1 1 1 2 2 2 2 2 AR 4 2 2 4 2 2 AR AR AR 2 2 2 1 1 5 1 1 1 1 7' 1 1 6' 2 1 1 1 1 2 4 1 1 I SERIAL NUMBERS AFFECTED 27-1 to 27-7554168inclusive 27-7664001 and up 27-1 to 27-3888 inclusive 27-1 to 273888 inclusive 27-3889 end up 27-3889 end up SECTION I Wlng Group WING INSTALLATION -Figure and Index Number Code A.B A.B A.9.Y A.B.Y A.9.Y A.B.Y A.B.Y A.Y A.Y Y Y Y Y Y Y C.0.X C.0.X C.D.2 C.D.2 C.2 c.z C.0.Y C.D.Y C.Y C.Y C.Y C.Y C.Y C.Y C.Y C.Y PIPER PARTS CATALOG I NOMENCLATURE FLAP ASSEMBLY - Left wlng FLAP ASSEMBLY - R~ghtwlng FLAP ASSEMBLY - Left wing IFLAP ASSEMBLY - Right wlng FLAP ASSEMBLY - Left wing IFLAP ASSEMBLY - Right wlng FLAP ASSEMBLY - R~ghtwlng FLAP ASSEMBLY - Left wlng FLAP ASSEMBLY - R~ghtwlng LUG - Wlng t ~ pattaching SCREW - Truss head machlne (MS35206-245) FAIRING ASSEMBLY - Nacelle Inboard left (alumlnum) FAIRING ASSEMBLY - Nacelle ~nboard,rrght (alumlnum) FAIRING ASSEMBLY - Nacelle Inboard. left (alumlnum) FAIRING ASSEMBLY - Nacelle ~nboard.r ~ g h t(alumlnum) FAIRING ASSEMBLY - Nacelle Inboard, left ff~berglass) FAIRING ASSEMBLY - Nacelle ~nboard,r ~ g h t(f~berglass) FAIRING ASSEMBLY - Nacelle outboard, left falumlnum) FAIRING ASSEMBLY - Nacelle outboard. r ~ g h t(alumlnum) FAIRING ASSEMBLY - Nacelle outboard, left (f~berglass) FAIRING ASSEMBLY - Nacelle outboard, r ~ g h t(f~berglass) BUSHING - Alleron center hlnge BOLT - (AN4-1OAi BOLT - (AN4-13A) NUT - Self locking (MS20365-428C) TIP ASSEMBLY - Left wing TIP ASSEMBLY - R ~ g h twrng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twlng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twtng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twlng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twlng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twlng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R~ghtwlng TIP ASSEMBLY - Left wlng TIP ASSEMBLY - R ~ g h twlng A - See F~gure2A for component parts B - When orderlng new Flap Assembly. ascerraln part number stamped on ~dentlflcat~on plate attached to outboard r ~ bReorder the Flap Assembly of same part number C - See Figure 4 for component parts D - If Kit No 754 493 IS used. order t ~ p17531 -40 left or 17531 -41 r ~ g h t X - Used on PA-23-250 alrplanes only Y - Used on PA-23-250 (SIX Place) alrplanes only Z - Used on PA-23-235 a~rplanesonly SERIAL NUMBERS 1 1 AFFECTED and 1 1 1 1 1 1 1 1 1 4 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 When orderlng, always spec~fyPart Number. Descr~pt~on and Ser~alNumber of Alrcraft 27-1 to 31 -2504 lncluslve 2 7 - 1 to 27-2504 lncluslve 27-2505 to 27-3049 lncluslve 27-3051 to 27-3153 lncluslve 27-2505 to 27-3049 ~ncluslve. 27 3051 to 27-31 53 lncluslve 27-3050. 27-3154 10 27-7405300 lncluslve 27-3050. 27-3154 to 27-3784 ~ n c l u s ~ v e 27-3785 to 27-7405300 lncl 27-7405301 and up 27-7405301 and up 27-1 to 27-7554168 lncluslve 27-1 to 27-2504 lncluslve 27-1 to 27-2504 lnclustve 27-2505 to 27-3888 ~ n c l u s ~ v e 27-2505 to 27-3888 lncluslve 27-3889 and up 27-3889 and up 27-1 to 27-3888 ~ n c l u s ~ v e 27-1 to 27-3888 lncluslve 27-3889 and up 27-3889 and up 27-505 to 27-524 lncluslve 27-505 to 27-524 lncluslve 27-525 and up 27-525 and up 27-2000 to 27-2269 lncluslve 27-2000 to 27-2269 lncluslve 27-2270 to 27-4815 lncluslve 27-2270 to 27-4815 mnclus~ve 27-4816 to 27-7554168 lncluslve 27-4816 to 27-7554168 lncluslve 27-7654001 to 27-7954087 lncl 27-7654001 to 27-7954087 lncl 27-7954088 and up REVISED OCTOBER 1980 PA-23-250(SIXPlace) PA-23-250. PA-23-235 WING INSTALLATION SECTION I REVISED OCTOBER 1980 PIPER PARTS CATALOG a REVISED MARCH 1980 F~gure2A Flap Assembly and A~leronAssembly 1 A 1 9 PA-23-250 (SIXPlace PA-23-250. PA-23-23! FLAP ASSEMBLY AND AILERON ASSEMBLY Figure PIPER PARTS CATALOG - and Part Index Number Code NOMENCLATURE Number 2A- 17104 DRAWING . Flap Assembly 17100 DRAWING - Alteron Assembly FLAP ASSEMBLY - Left wlng FLAP ASSEMBLY - R~ghtwlng FLAP ASSEMBLY - Left wing 117104-57 ICY IFLAP ASSEMBLY - R~ghtwlng 117104-60 IC,Y IFLAP ASSEMBLY - Left wlng 11 7104-59 ICY (FLAP ASSEMBLY . ~ l g h twlng FLAP ASSEMBLY R~ghtwtng FLAP ASSEMBLY - Left wlng FLAP ASSEMBLY - R~ghtwlng SPAR - Left flap SPAR ASSEMBLY - Rlght flap SPAR ASSEMBLY - R ~ g h tflap ' SKIN - Leadlng edge left flap outboard SKlN - Leadlng edge r ~ g h tflap, outboard SKlN - Leadlng edge left flap Inboard SKlN - Leadlng edge r ~ g h tflap. Inboard SKIN ASSEMBLY - Left flap top SKlN ASSEMBLY - R ~ g h tflap top SKIN ASSEMBLY - R~ghtflap top ' ' STRIP - Beaded ' ' PLATE - Re~nforcementr ~ g h tflap top skln (Sta 0 to Sta 18) ' PLATE - Relnforcement r ~ g h tflap top skln (Sta 18 to Sta 32) RIB - R ~ g h tflap ' SKIN ASSEMBLY - Left flap bottom ' SKIN ASSEMBLY - R ~ g h tflap bottom. outboard SKlN ASSEMBLY - R ~ g h tflap. bottom. outboard SKlN ASSEMBLY - R ~ g h tflap, bottom Inboard ' BULKHEAD - Flap Inboard BULKHEAD - Left flap BULKHEAD - R~ghtflap BULKHEAD - Left flap BULKHEAD - R~ghtflap BULKHEAD Left flap BULKHEAD - R~ghtflap IA- Ascertain part number of flapassembly An identificat~on plate w ~ t hthe flap assembly part number IS hated on the outboard r ~ bIf 17104-71 or 17104-72 or 1.7104-73 or 17104-74 IS ~nstalled,order pafl for serlal number 27-3785 and up B - Used on alrcraft w ~ t hser~alnumbers 27-1 to 27-3784 lncluslve ~fflap assembly 17104-71 or 17104-72 or 17104-73 or 17104-74 1s ~nstalled C - When orderlng new flap assembly, aSCertaln part number stamped on ~dent~flcat~on plate anached to outboard rlh Reorder the flap assembly of same part number Y - Used on PA-23-250(SIX Place) airplanes only SECTION 1 W ~ n gG r o i l p SERIAL NUMBERS AFFECTED inclusive 27-3785 to 27-7405300 lncluslve 27-7405301 and up 27-7405301 and up 27-1 to 27-3784 lncluslve 27-3785 and up 27-4 to 27-3784 lncluslve 27-3785 and up When order~ngalways spec~fyPart Number Descr~pt~on and S e r ~ a lNumber of Alrcraft 1 1 1 1 1 1 1 1 1 1 1 8 8 2 REVISED MARCH 1980 27-3785 and up 27-3785 and up 27-1 to 27-3784 27-3785 a d up PA-23-250 61% Place) PA-23-250 PA.23-235 FLAP ASSEMBLY AN0 AILERON ASSEMBLY Figure N u m k r rPIPER PARTS CATALOG - I I NOMENCLATURE REVISED: MARCH 1980 RIB - Left flap RIB - Right flap ' REINFORCEMEKT - Flap outboard rib, left ' 'REINFORCEMENT - Flap outboard rib. right 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, Ieft CHANNEL - Flap hinge reinforcement, right CHANNEL - Flap hinge reinforcement, left ' CHANNEL - Flap hinge reinforcement, right ' HINGE - Flap, inboard, left ' HINGE - Flap. inboard. right ' HINGE - Flap, inboard, left 1' HINGE - Flap, inboard. right HINGE - Flap, inboard, left * HINGE - Flap, inboard, right ' HINGE - Flap, outboard, left 'HINGE - Flap, outboard, right HINGE - Flap. outboard, left I*HINGE - Flap. outboard. right HINGE - Flap, outboard, left HINGE - Flap, outboard, right ' HINGE - Flap. outboard, left ' HINGE - Flap, outboard, right A - Ascertain part number of flap assembly on identification plate, located on fhe outboard rib If 17104-71. 17104- 72, 17104-73 or 17104-74 is installed, order pert for serial numbers 27-7406301 and up B - Ascertain if hinge is an angle or a channel type If the angle type is installed, order the appropriate pert 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 Ieft or 33608-03 right for serial numbers 27-3050. 27-31 54 to 27-7405330 inclusive Y - Umd on PA-23-250 (Six Place) airplanes only SECTION I Wing Group 27-1 to 27-7405300 inclusive No. Rw. 27-7405301 and up SERIAL NUMBERS AFFECT ED 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 to 27-3049 inclusive. 27-3051 to 27-3153 inclusive 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 27-3050. 27-3154 and up 27-3050, 27-31 54 and up 27-1 to 27-2504 inclusive 2 7 - 1 to 27-2504 inclusive 27-2505 to 27-3049 inclus~ve. 127-3051to 27-3153 inclusive 27-2505 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 27-3050, 27-3154 to 27-7405330 inclusive 27-3060, 27-3154 to 27-7405330 inclusive 27-7405331 and up 27-7405331 and up When ordering, always specify Pan Number. Description and Serial Number of Aircraft PA-23-250 (Six Place) PA-23-250, PA-23-235 FLAP ASSEMBLY AND AILERON ASSEMBLY SECTION l Wing Group Number Part N u m k r 17102-00 17102-01 17102-02 17102-03 17100-00 17100-01 17126-03 17126-09 17202-00 17100-18 17100-12 17100-11 17100-16 17100-17 17100-17 17100-16 18379-00 1710098 17100-20 17100-19 17100-04 17100-05 17100-05 17100-04 17100-14 17100-21 17100-13 17095-00 17095-01 17097-00 IPIPER PARTS CATALOG code I NOMENCUTURE - - - - - HINGE - Flap, centw, left HINGE - Flap. center. right Y HINGE - Flap, center. ldt HINGE - Flap, center, right AILERON ASSEMBLY - Left wing AILERON ASSEMBLY - Right wing BALANCE ASSEMBLY - Aileron. Ieft * BALANCE ASSEMBLY - Aileron, right SHIM SPAR ASSEMBLY - Aileron SKIN - Leading edge, left SKlN - Leading edge. right SKIN ASSEMBLY - Left top SKlN ASSEMBLY - Right, top SKIN ASSEMBLY - Left, bottom ,* SKlN ASSEMBLY - Right. bottom TAB - Aileron trim RIB - Aileron, outboard * RIB ASSEMBLY - Leading edge, outboard. Ieft RIB ASSEMBLY - Leading edge, outboard, right RIB - Leading edge RIB - Leading edge RIB - Leading edge, left RIB - Leading edge, right RIB - Aileron center PLATE ASSEMBLY - Aileron hinge. reinforcement. center RIB - Aileron inboard HINGE - Aileron inboard, left HINGE - Aileron inboard. right HINGE - Aileron center. left HINGE - Aileron center. right r - U d on PA-23-250 (Six Place) airplanes only When ordering, always specify Par? Number. Description and Serial N u m k r of Aircraft No. Rm. 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 9 9 1 1 2 1 1 1 1 1 1 REVISED: MARCH 1980 SERIAL NUMBERS AFFECTED 27-1 to 27-2504 inclusive 27-1 to 27-2504 inclustve 27-2505 to 27-3049 inclusive 27-3051 to 27-31 53 inclusive 27-2505 to 27-3049 inclusive 27-3051 to 27-3153 inclusive PA-23-250 (Six Place) PA-23-250. PA-23-235 1A23 M R U 1A24 INTENTIONALLY LEFT BLANK PIPER PARTS CATALOG REVISED JULY 1984 F ~ g u r e3 W ~ n gand Wlng TIP Construct~on 1 B 1 P A - 2 3 - 2 5 0 (SIX Place) P A - 2 3 - 2 5 0 . P A . 2 3 - 2 3 5 SECTION I Wing Group WlNG AND WlNG TIP CONSTRUCTION When ordering, always specify Pan Numkr, Description and Serial Number of Aircraft REVISED: OCTOBER 1076 182 PA-23.250 (Six Place) PA-23-250. P A - B - B 5 Figure md Index Number 3- -1 - l a -2 -3 4 -5 6 -7 -8 -0 -10 -11 -12 Code x.2 Y Y X.2 Y Y C.X COX C,Z C,Z Z Z D,Y D,Y Y Y Y Y Y Y y Y A B B B B Number 16170 16170 33300 17631 34282 16067 16292 30698 33304 33900 16170-00 1617041 1 6 1 7 0 1617041 1617030 1617029 1617026 1617025 1617028 1617027 1617032 1617031 3330000 3330001 33300-m 3330007 1733003 462 346 2570C00 1733002 452 346 2S70+00 1733142 462 346 2670+00 1839801 1839800 462 345 2670+00 1762902 1752W3 1762904 1661402 3301742 33917-03 NOMENCLATURE DRAWING - Wing Panel DRAWING - Wing Pand DRAWING -Wing Panel DRAWING -Wing l i p DRAWING -Wing K p DRAWING -Outboard L d i n g Edge Ammbly DRAWING - Wing Installation DRAWING -Wing Installation DRAWING - Wing Installation DRAWING -Wing Installation PANEL ASSEMBLY - Left wing PANEL ASSEMBLY -Right vvlng 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 PAN E L 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 BRACKEf - Flap hinge, center BEARING BEARING BRACKET - Flep hinw, inboard, left BRACKET - Flep hinge, i n b d , right BEARING BEARING HINGE -Wing tip HINGE - Wing tip atmdmant PIN - Wing tip hingu PIN - Wlng tip h i m R I B ASSEMBLY - Wing trailing dge, left RIB ASSEMBLY - WIng tralling dgr,right A - C m p o n m t pmrt of wing tip m l y . 0 - Not a component of wing panel or wing tip. C - I f K i t No. 754 493 has beon installad, order wing panol 16170-20 R.H. or 16170-30 L.H. D - I f K i t No. 754 493 has bmn inaMled, order wing prnel 16170-27 R.H. or 1617028 L.H. X - Uad on PA-a-260 airplrres only. Y - U d on PA-23-260 (Six %a)rirplmm only. Z - Umad on PA-23-236 airplrres only. No. Req. 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 SERIAL NUMBERS AFFECTED 27-2000 t o 274815 inclusim 274816 end up 27-1 t o 27-7554168 inclusive 27-7854001 and up 27-MOO t o 274815 inclusive 27-4816 t o 27-7554168 incl. 27-7654001 and up 27-505 to 27-524 inclusive 27-505 to 27-624 inclusive 27-525and up 27-525and up 27-2000 t o 27-n69 inclusive 27-2000 t o 27-2200 inclusim 27-2270 t o 27.2504 inclusive 27-2270 t o 27-2504 inclusive 27-2605 t o 274816 Inclusive 27-2505 t o 274815 inclusive 274816 to 27-7554168 incl. 274816 to 27-7554168 incl. 27-7654001 and up 27-7654001 and up 27-1 t o 27-3483inclusive 2 7 W a n d up 27-1 t o 27- inclusive 273484andup 27-1 t o 27-3483 inclusive 273484and up 27-1 to 27-3483 inclusive 27-3484and up 27-1 t o 27-7554168 inclusive 27-1 t o 27-7654168 inclusive 27-7654001 and up WlNG AND WlNG TIP CONSTRUCTION SECTION I Wing Group When ordering, aluruayc spacify Part Number, Description and Serial Number of Aircraft Figure and Index Number 3-13 -14 -15 -16 -17 -18 -19 -20 -21 -22 -23 -.-a -25 -26 -27 -28 -288 -29 -298 -30 -3 1 -32 -33 -34 REVISED: OCTOBER 1976 PA-23-250 (Six PI-) PA-23260. PA-B-236 Number 18253-02 18263-20 18253-17 18263.19 18253-10 18263.11 18263-03 18263-12 17531-12 17631-13 17631-16 17531-17 17631-06 17631-07 17531-14 17631-15 17531-08 17531-09 1732912 1 7 3 a 1 3 17329-28 1732929 1732929 1732928 1732828 1732929 1732B-23 1732908 1732930 1732927 1732930 1732927 19283-09 19283-10 1732927 1732930 19283-10 19283-12 19283-13 19283-04 19283-03 17329-34 1732831 752 959 149 063 Code B A,B A.B A,B A,B A.B A,B A,B A,B A,B A,B SERIAL NUMBERS AFFECTED 27-7654001 and up 27-1 t o 27-7554168 inclusive 27-7654001 and up 27-1 t o 27-7554168 inclusive 27-7654001 and up NOMENCLATURE STRIP ASSEMBLY - W ~ n gt i p atpchmant, top, rear STRIP ASSEMBLY - Wing t i p atochmmt. top, rear STRIP ASSEMBLY - Wing t i p attachment, top, center STRIP ASSEMBLY - Wing t i p atpchment, front STRIP ASSEMBLY - Wing t i p attschment, bottom center, ri&t STRIP ASSEMBLY - Wing t i p att&hment, bottom center, ri&t STRIP ASSEMBLY - Wing t i p atechmant, bottom center, left STRIP ASSEMBLY - Wing t i p attachment. bottom center, left RIB -Wing t i p front. left R I B -Wing tip f r o n t ri&t R I B -Wing tip rear, left R I B -Wing tip rear, right SPAR - Wing tip front, left SPAR -Wing t i p front, right R I B -Wing tip center, left R IB - Wing tip center, right SPAR - Wing t i p rear, left SPAR -Wing tip rear, right BULKHEAD - Rear sper, left, Sta. 146,191 BULKHEAD - Rear war. right, Sto. 146,191 BULKHEAD - Rear spar, left, Sta. 167,168,180 BULKHEAD - Rear spr, right, Sm. 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, Sm. 127 BULKHEAD - Raar war. left, Sta. 110 BULKHEAD - Rear spar, r i g h t Sm. 110 BULKHEAD - Rear spar, left, Sta. 96 BULKHEAD - Rear spar, r i g h t Sm. 95 BULKHEAD - Rear spur, left, Sta. 87, w t b o e r d of t o q u e r i b BULKHEAD - Reer spar, r i g h t SP. 87, outboard of t o q u e r i b BULKHEAD - Rear spar, left, Sta. S . 6 1 and 74, outbowd of torque r i b BULKHEAD - Rear spar, r i g h t Ste. 58.61 md 74, outboard o f torque rib BULKHEAD - Rear spar, left, Sta. 80 BULKHEAD - Rear spr, right, Sta. 80 BULKHEAD - R w r cpr, Sta. 49 BULKHEAD - Rear spar, Mt ( t o q u e rib) BULKHEAD - Rear cpr, right (torque rib1 BULKHEAD - Rear spar, Idt.S t a 34.42 BULKHEAD - Rear rpu, r i g h t Sta. 34.42 BULKHEAD - Rear spr, left, Sta. 27 BULKHEAD - Rear spar, r i g h t Sta. 27 STIFFENER - (6' n t i o n l ANGLE - Exwucion (6' u c t i o n l A - Canponent part o f wing tip m b l y . B - U a d on PA-23.250 and PA-23-235 Ath -rial numbsn 27-1 to 27422 and PA-23-260 (Six P l w ) with wrial numbera 27-2000 t o 27-7554172 inclusiw. No. Req. 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 2 2 3 3 3 3 1 1 1 1 1 1 2 2 . 2 2 1 1 2 1 1 2 2 1 1 SECTION I Wing Group WlNG AND WlNG TIP CONSTRUCTION When ordRring, a~wayst w i f y Part N u m k r , Description and Serial Number of Aircraft REVISED: OCTOBER 1976 164 Figure and Index Numbr 3-36 -36 -37 -37a -38 -39 40 4 1 4 2 4 3 4 3 a 44 4 5 -46 4 7 -48 4 9 -50 Part Number 16064oO 1606400 3376742 16064-01 1605401 3376743 16047-00 16047-01 16053-05 1572W2 16063-04 1572002 1606342 16063-12 1606304 1572042 1605345 15720-02 16063.02 16053-12 16052-00 1605240 33302-00 16062-01 1606241 33302-01 1666602 l666BOG 17387-00 16668-04 166S6-08 17423-00 18858-05 1665809 1665803 16868-07 16027-00 16027-01 1601805 1601894 1601802 1601803 16024-00 16024-01 l6OOsO2 16oo&o3 leOOsM 1600805 16008-04 1800805 19287-00 192874 1 Code X.Z Y Y X.2 Y Y A A A A A A X,Z Y Y X,Z Y Y X,Z X.Z Y Y NOMENCLATURE R I B ASSEMBLY - Wing, left, Su. 191 RIB ASSEMBLY - Wing, left, Sta. 191 RIB ASSEMBLY - Wing, left, Sta. 191 RIB ASSEMBLY - Wing, right, Sta. 191 R I B ASSEMBLY - Wnng, r i g h t Sta. 191 RIB ASSEMBLY - Wing, right, Sta. 191 RIB ASSEMBLY -Wing, left, Sta. 146 R I B ASSEMBLY - Wing, right, Str. 146 R I B ASSEMBLY - Wine Mt top, Sta. 175 R lB ASSEMBLY - Wing, left top, Sta. 175 R I B ASSEMBLY -Wing, right top, So. 175 RIB ASSEMBLY -Wing, right top, Sm. 176 RIB ASSEMBLY - Wnng, bottom, Sta. 175 R IB ASSEMBLY - Wing, bottom, Sta. 175 RIB ASSEMBLY - Wing, left top, Sts. 160 R I B ASSEMBLY - Wing, left top, Sta. 160 RIB ASSEMBLY - Wing, right top, Sta. 160 RIB ASSEMBLY - Wnng, right top, Sta. 160 R I B ASSEMBLY - Wing, bottun, Sta. 160 RIB ASSEMBLY -Wing, bonan, Sm. 160 R I B ASSEMBLY -Wing, left. Sta. 127 R IB ASSEMBLY - Wing, left, Sta. 127 R I B ASSEMBLY - Wing, loft, Sta 127 RIB ASSEMBLY - Wlng, right, Sm. 127 RIB ASSEMBLY - Wing, right, Sm. 127 RIB ASSEMBLY - Wing, right, Sm. 127 RIB ASSEMBLY - Wing, Mt top, Sta. 110 RIB ASSEMBLY - Wing, right top, SP. 110 ANGLE -Rib, S a . 86,109 RIB ASSEMBLY - Wing, left, Sta. 96, top RIB ASSEMBLY - Wing, right. SP. S,top SHIM - Rib, Sta. 58.80 R I B ASSEMBLY - Wing left, Sta. 96, bottom RIB ASSEMBLY - Wing, right, SD. 95, b o r n RIB ASSEMBLY - Wing, left, Sta. 110, botunn RIB ASSEMBLY - Wing. right, Sm. 110, bottom RIB ASSEMBLY - Wing. left, Sta. 80 RIB ASSEMBLY - Wing, right, SD. 8Q RIB ASSEMBLY - W i n g outboard torque, )eft RIB ASSEMBLY -Wing, outboard torque, right RIB ASSEMBLY -Wing, i-d torque, left R IB ASSEMBLY - Wing, inboard torque, ri&t RIB ASSEMBLY - Wing, left, Sta. 66 RIB ASSEMBLY - Wing, r i g h t Sm. 66 R I B ASSEMBLY - Wing, Mt, Sta. 42.49 R I B ASSEMBLY - Wing, right Sm. 42.49 R IB ASSEMBLY - Wing, left, Sta. 42.48 R I B ASSEMBLY -Wing, right, So. 42.49 RIB ASSEMBLY - Wing, left, Sta. 34 RIB ASSEMBLY - Wing, right, Sm. 34 R I B ASSEMBLY -Wing butt, bft RIB ASSEMBLY -Wing butt, rlght A - Uvd on PA-23-260 and PA-23-236 wlth aria1 n u m k n 27-1 t o men m d PA-23.2~( s x PI-) wittt wrial n u m b 27-1000 t o 27-7664168 lnclusiw. X - Uvd on PA-23-250 airplanas only. Y - U d on PA-P-260 (Six P k e ) airplmea only. Z - Uad on PA-23-236 airplems only. No. Req. 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 1 1 1 2 2 2 2 1 1 1 1 SERIAL NUMBERS AFFECTED 27-2000 t o 274815 inclusive 274816and up 27-2000 t o 274815 inclusive 274816 and up 27-7654001 and up 27-7654001 andup 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 andup 27-2000 t o 274815 inclusive 274816and up 27-2000 t o 274815 inclusive 274816 and up WING AND WING TIP CONSTRUCTION Code PIPER PARTS CATALOG NOMENCLATURE ' SPAR ASSEMBLY - Wing rear, left SPAR ASSEMBLY - Wing rear, right ' ' PLATE - Rear spar, left front, rlght rear PLATE - Rear spar, left rear, right front ' SPAR . Outboard sectton. Sta 99 31 to Sta 192 07, left SPAR - Outboard sectlon, Sta 9 9 31 to Sta 192 07, rtght ' ' BUSHING SPAR ASSEMBLY - lnboard section, Sta 23 75 to Sta 99 31. left ' SPAR ASSEMBLY - Inboard section, Sta 23 75 to Sta 9 9 31, r ~ g h t SPAR ASSEMBLY - W ~ n gfront, left SPAR ASSEMBLY - Wing front, right ' SPAR ASSEMBLY - Wtng front, left SPAR ASSEMBLY - Wing front, rtght SPAR ASSEMBLY - Wing front, left SPAR ASSEMBLY - Wing front, right ' PLATE - Front spar end ' ' CHANNEL - Front spar tip, left " CHANNEL - Front spar tip, right ' CHANNEL - Front spar tlp, left ' CHANNEL - Front spar tlp, right ' ' REINFORCEMENT - Spar tip channel ' BLOCK - Bear~ng,main gear door actuator BRACKET - Hydraulic llne support, left BRACKET - Hydraulic line support, right BRACKET - Hydraulic llne support, left BRACKET - Hydraulic ltne support, right + BRACKET - Fuel valve shutoff, left BRACKET - Fuel valve shutoff, left BRACKET - Fuel valve shutoff, left BRACKET - Fuel valve shutoff, left BRACKET - Fuel valve shutoff, r ~ g h t ' BRACKET - Fuel valve shutoff, right BRACKET - Fuel valve shutoff. right BRACKET - Fuel valve shutoff, right RIB ASSEMBLY - Wing nose, left. Sta 180 + RIB ASSEMBLY - Wtng 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 - W ~ n gnose. 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 - Wtng nose. right. Sta 118 RIB ASSEMBLY - Wing nose, left. Sta 109 RIB ASSEMBLY - Wing nose, right, Sta 109 X - Used on PA-23-250 a~rplanesonly Y - Used on PA-23-250 (Six Place) airplanes only Z - Used on PA-23-235 airplanes only SECTION 1 Wtng Group wSERIAL NUMBERS AFFECTED 27-2000 to 27-7554168 ~ncluslve 27-2000 to 27-7554168 ~nclustve 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 tnclustve 27-1 to 27-75541 68 ~ n c l u s ~ v e 27-7654001 and up 27-7654001 and up 27-2505 and up 27-1 to 27-7954121 tnclusive 27-1 to 27-7954121 ~ncluslve 27-8054001 and up 27-8054001 and up 27-2000 to 27-2222 inclusive 27-2223 and up and 1 1 1 1 2 2 2 2 1 1 1 1 2 2 2 When ordering, always specify Part Number. Description and Serial Number of Alrcraft 27-2000 to 27-2222 lnclus~ve 27-2223 and up 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-504 ~ncluslve 27-505 and up 27-1 to 27-75541 68 ~nclusive 27-1 to 27-7554168 ~ n c l u s ~ v e 27-7654001 and up 27-7654001 and up 27-1 to 27-504 inclus~ve 27-505 and up 27-1 to 27-504 inclusive REVISED JULY 1984 PA-23-250 (SIX Place) PA-23-250, PA-23-235 WING AND WING TIP CONSTRUCTION SECTION I Wing Group Figure and Index Number -3-65 -66 -67 - 68 -69 -70 -71 -71a -72 -73 -73a -74 -75 -76 - 77 - 78 -79 -80 -81 -82 -83 - 84 -85 -86 PIPER PARTS CATALOG NOMENCLATURE ' RIB ASSEMBLY - Wing nose. left. Sta 102 ' RIB ASSEMBLY - Wlng nose. right. Sta 102 ' RIB ASSEMBLY - Wing nose. left, Sta 95 ' RIB ASSEMBLY - Wing nose, left. Sta 95 ' RIB ASSEMBLY - Wing nose, r~ght.Sta 95 ' RIB ASSEMBLY - Wing nose. nght. Sta 95 ' RIB ASSEMBLY - Wing nose. left. Sta 87 RIB ASSEMBLY - Wing nose. right. Sta 87 ' RIB ASSEMBLY - Wlng nose, left. Sta 80 RIB ASSEMBLY - Wing nose, rlght. Sta 80 ' RIB ASSEMBLY - Wlng nose. left. Sta 56 ' RIB ASSEMBLY - Wing nose. right. Sta 56 ' RIB ASSEMBLY - Wing nose. left. Sta 56 ' RIB ASSEMBLY - Wing nose. rlght. 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 RIB ASSEMBLY - Wing nose. left. Sta 34 ' RIB ASSEMBLY - Wing nose. right. Sta 34 'RIB ASSEMBLY - Wing nose. left. Sta 34 ' RIB ASSEMBLY - Wing nose. right. Sta 34 ' RIB ASSEMBLY - Wing nose. left. Sta 27 ' RIB ASSEMBLY - Wlng 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, r~ght PLATE - Wlng rib cover BRACKET ASSEMBLY - Aileron bellcrank, left BRACKET ASSEMBLY - A~leronbellcrank, left BRACKET ASSEMBLY - Aileron bellcrank, left ' BRACKET ASSEMBLY - Aileron bellcrank, right BRACKET ASSEMBLY - Aileron bellcrank, right BRACKET ASSEMBLY - Alleron bellcrank. right BRACKET - Aileron cable pulley ' ANGLE - Bun rib, left. Sta. 27 'ANGLE - Bun rib. r~ght.Sta 27 'SHIM - Bun, rib. Sta 27 ' CONDUIT - Wire harness (1 -114") ' BOLT - "U" PLATE -Wheel well attachment, left ' PLATE - Wheel well attachment, right 'PLATE - Wheel well attachment, left .PLATE -Wheel well attachment, right . 'SHIM - Rib, Sta 42.49 ' SHIM - Rib, Ste 34 BRACKET - Fuel strainer, left ' BRACKET - Fuel strainer, left ' BRACKET - Fuel strainer, right BRACKET - Fuel strainer, right Part Number 17187-10 17187-11 17188-10 17188-12 17188-11 17188-13 17189-10 17189-11 16034-00 16034-01 16042-00 16W2-01 16042-10 16042-11 1601 2-02 16012-03 16017-00 16017-01 16016-00 16016-01 16014-00 16014-01 16014-02 1 6014-03 16013-00 16013-01 16015-00 16015-01 17375-00 17382-00 17382-01 17193-00 17428-00 17428-02 17428-04 17428-01 17428-03 17428-05 17459-00 18614-00 18614-01 18606-00 17752-02 18329-02 18358-00 18358-01 31404-00 31404-01 18942-02 18942-00 16216-00 16216-00 16216-01 16216-01 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 SERIAL NUMBERS •IRq I AFFECTED 27-1 to 27-504 inclusive 27-505 and up 27-1 to 27-504 ~nclus~ve 27-505 and up 27-1 to 27-7954089 ~ncluslve 27-1 to 27-7954089 ~nclus~ve 27-7954090 and up 27-7954090 and up 27-1 to 27-504 ~nclus~ve 27-505 to 27-7554168 lncluslve 27-7654001 and up 27-1 to 27-504 inclusive 27-505 to 27-7554168 ~nclus~ve 27-7654001 and up 27-1 to 27-2504 lncluslve 27-1 to 27-2504 ~nclus~ve 27-2505 and up 27-2505 and up When ordering, always specify Part Number. Description and Serial Number of Aircraft REVISED OCTOBER 1980 PA-23-250 (SIX Place) PA-23-250.PA-23-235 REVISED: AUGUST 1979 WING AND Figure and Index Number 3-87 -88 -89 -90 -91 -92 -93 -94 -95 -96 -97 -98 -99 a -100 , 1 -101 -102 -103 -104 -106 -106 -107 PA-23-250(Six Place) PA-23-250. PA-23-235 WING TIP Part Number 18572-00 18572-01 18571-00 18571-01 17209-04 17209-05 16046-00 19302-00 19294-00 19294-01 19295-00 16010-00 16010-01 19976-00 19976-01 31409-00 31409-01 33159-00 33159-01 33158-00 33158-01 33792-02 33792-03 33791-02 33791-03 33770-02 33770-03 33760-02 33760-03 34220-00 34220-14 34220-01 34220-15 33773-02 33774-02 33772-02 33772-03 15797-02 15797-03 CONSTRUCTION Code Y Y A A A A A A A A A A A A A A When SECTION I Wing Group SERIAL NUMBERS AFFECTED 27-505 and up 27-505 and up 27-2505 and up 27-2505 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 27-7964098 and up 27-7654001 to 27-7954087 incl 27-7954088 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654003 and up 27-7654003 and up Aircraft PIPER PARTS CATALOG NOMENCLATURE FllTlNG - Landing gear reinforcement, left FIUJNG - Landing gear reinforcement, right PLATE - Filler, left PLATE - Filler, right ANGLE - Torque rib stiffener (right wing outboard or left wing inboard) ANGLE - Torque rib stiffener (right wing inboard or left wing outboard) ANGLE - Rib attachment, Sta. 42. 49 ANGLE - Rib attachment. Sta 34 PLATE - Torque rib reinforcement. left PLATE - Torque rib reinforcement, right SHIM - Torque rib SPAR ASSEMBLY - Front. left SPAR ASSEMBLY - Front, right STRINGER ASSEMBLY - Left STRINGER ASSEMBLY - Right BRACKET ASSEMBLY - Main gear door actuator, left BRACKET ASSEMBLY - Main gear door actuator, right DOUBLER - Wing, front spar. left DOUBLER - Wing, front spar. right BRACKET - Wing. rib attachment, left BRACKET - Wing, rib attachment, right BULKHEAD - Wing tip, left BULKHEAD - Wing tip, right BULKHEAD - Wing tip, left BULKHEAD - Wing tip, right RIB ASSEMBLY - Wing tip, left RIB ASSEMBLY - Wing tip, right HINGE - Wing tip, left HINGE - Wing tip, right RIB ASSEMBLY - Wing tip, left RIB ASSEMBLY - Wing tip, left RIB ASSEMBLY - Wing tip, right RIB ASSEMBLY - Wing tip, right SPAR - Wing tip, upper SPAR - Wing tip, lower BRACKET ASSEMBLY - Strobe power supply, left BRACKET ASSEMBLY - Strobe power supply. right CHANNEL ASSEMBLY - Tip guide, left CHANNEL ASSEMBLY - Tip guide, right A - Component part of wing tip assembly. Y - Used on PA-23-250 (Six Place) airplanes only ordering. always specify Part Number. Description and Serial Number No. Rw. 1 1 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 of P I P E R A I R C R A F T C O R P O R A T I O N REVISED: OCTOBER 1976 Figure 4. Wing and Wing Tip Skin 188 PA-23-250 (Six PIRXJ) PA-23-2W. PA-23-P6 WlNG AND WlNG TIP SKlN SECTION I Wing Group PA-23-250 (Six Place) PA-23.250. PA-23-235 Figure and I n d e x N u m b e r 4- - 1 - l a a -2 -3 -4 -5 - 5a -6 -7 -7a -8 -8a -9 -9a aREVISED: Part N u m b e r 16170 16170 33300 16292 30698 33304 33900 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 16170-16 16170-17 33300-14 33300-15 16170-10 16170-09 33300-12 16170-02 1600900 17318-02 17318-02 1731804 16170-06 16170-05 16170-36 16170-35 16057-07 17422-35 173 15-00 17422-36 17422-37 173 17-00 16057-04 16057-05 17317-00 OCTOBER Code x.z Y Y x.2 Y Y Y A,X A,X A,Z A.Z Z Z B,Y B,Y Y Y Y Y Y Y Y Y Y Y Y Y When ordering, 1976 N O M E N C L A T U R E DRAWING - Wing Panel DRAWING -Wing Panel DRAWING -Wing Panel DRAWING -Wing Installation DRAWING -Wing Installation DRAWING -Wing Installation DRAWING -Wing Installation 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 access hole cover PLATE - Access hole c w e r PLATE - Access hole cover PLATE - Access hole c w e r 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 A - I f K i t No. 754 493 has been installed, order wing panel 16170-30 left or 16170-29 right. B - I f 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. always specify Part Number, Description and Serial Number of 1B 9 No. Req. 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 1 1 1 Aircraft S E R I A L N U M B E R S AFFECTED 27-2000 t o 274815 inclusive 274816 and up 27-2000 t o 274815 inclusive 274816 t o 27-7554168 incl 27-7654001 and up 27-505 to 27-524 inclusive 27-505 to 27-524 inclusive 27-525 and up 27-525 and up 27-2000 t o 27-2269 inclusive 27-2000 t o 27-2269 inclusive 27-2270 t o 27-2504 inclusive 27-2270 t o 27-2504 inclusive 27-2505 t o 274815 inclusive 27-2505 t o 274815 inclusive 27-4816 t o 27-7554168 incl 27-4816 t o 27-7554168 incl 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclus~ve 27-1 to 27-7554168 inclusive 27-7654001 and up 27-7654001 and up 27-1 to 27-7554168 inclustve 27-1 to 27-7554168 tnclustve - 27-7654001 and up 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up 27-1 t o 27-2504 inclusive 27-1 to 27-2504 inclusive 27-2505 and up 27-2505 and up SECTION I Wing Group WlNG AND WlNG TIP SKlN Figure I I I PIPER PARTS CATALOG and Part Index I Number 1 Code /Number NOMENCLATURE SKlN ASSEMBLY - Left leading dge, inboard SKlN ASSEMBLY - Right leading edge, inboord SKlN ASSEMBLY - Left leading edge, inboard SKlN ASSEMBLY - Right leading edge, inboard SKlN ASSEMBLY - Left leading edge, inboard SKlN ASSEMBLY - Right Ieading edge, inboard PLATE - Reinforcement PLATE ASSEMBLY - Reinforcement PLATE ASSEMBLY - Reinforcement PLATE - Aileron bellcrank access hole cwer PLATE - Access hold cover FAIRING - False spar, 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 SKlN ASSEMBLY - Outboard bottom. L H SKlN ASSEMBLY - Outboard bottom, L H SKlN ASSEMBLY - Outboard bonom, R H SKlN ASSEMBLY - Outboard bottom, R H SKlN ASSEMBLY - Center bottom, L H SKlN ASSEMBLY - Center bonom, R H SKlN ASSEMBLY - Inboard bonom. L H SKlN ASSEMBLY - lnboard bottom, R H PLATE - Reinforcement PAD - Jack COVER - Fuel cell access PLATE ASSEMBLY - Access hole reinforcement PLATE ASSEMBLY - Fuel cell access, left PLATE ASSEMBLY - Fuel cell access, right FLOW STRIP - Wing, right COVER ASSEMBLY - 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 TIP ASSEMBLY - Wing, left TIP ASSEMBLY - Wing. right TIP ASSEMBLY - Wing, left TIP ASSEMBLY - Wing, right A - If Kit No 754 493 is used, order wing tip 175314 0 left or 1753141 right B - Refer to Figure 42C if Pneumatic Deicer Installation is installed 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 SERIAL NUMBERS I: : . 1 AFFECTED 1 1 1 1 1 1 2 1 1 1 2 1 1 1 1 1 1 1 1 1 1 1 When ordering, always specify Part Number, Description and Serial Number of Aircraft 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 27-481 5 inclusive 2 7 4 8 16 and up 27-1 to 27-481 5 inclusive 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 REVISED: AUGUST 1979 27-7654001 and up 27-7650001 and up 27-7654001 and UP 27-7654001 and UP 27-7654001 and up 27-1 to 27-75541 68 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 274815 inclusive 27-2270 to 274815 inclusive 27-481 6 to 27-7554168 inclusive 27-4816 to 27-7554168 inclusive PA-23-250 (Six Place) PA-23-250. PA-23-235 WlNG AND WlNG TIP SKlN Figure PIPER PARTS CATALOG and Part Indax Number I Numbw I =Ode I NOMENCLATURE SKlN - Left wing tip. lower SKlN - Right wing tip, lower SKlN - Left wing tip, lower SKlN - Right wing tip, lower SKlN - Left wing tip. lower SKlN - Right wing tip, lower SKlN - Left wing tip, upper SKlN - Right wing tip, upper CHANNEL - Section (six toot section) REINFORCEMENT - Aileron balance weight, left REINFORCEMENT - Aileron balance weight, right VENT ASSEMBLY - Fuel cell TUBE ASSEMBLY - Fuel cell vent drain TIP ASSEMBLY - Wing, left TIP ASSEMBLY - Wing, left TIP ASSEMBLY - Wing, right TIP ASSEMBLY - Wing, right SKlN - Left wing tip, lower SKlN - Right wing tip, lower SKlN - Left wing tip, upper SKlN - Right wing tip, upper SKlN - Wing tip leading edge, left SKlN - Wing tip leading edge, right REINFORCEMENT - Aileron balance weight, left REINFORCEMENT - Aileron balance weight, right REINFORCEMENT - Tip skin COVER ASSEMBLY - Fuel cell access COVER - Fuel cell GASKET - Fuel cell ANGLE - Nacelle attaching, left wing, outboard nose ANGLE - Nacelle anaching, right wing, outboard nose STRIP - Vent drain ' CONE FAIRING ASSEMBLY - Wing Tip, Left (Fiberglass) FAIRING ASSEMBLY - Wing Tip, Left (Thermoplastic) FAIRING ASSEMBLY - Wing Tip, Right (Fiberglass) FAIRING ASSEMBLY - Wing Tip, Right (Thermoplastic) COVER - Fuel cell RING - Fuel cell attachment GASKET - (FCB-25722) A - Used with wing tip 17531-46 or 17531-47 B - Used with wing tip 17531-40 or 17531-41. C - Used with wing tip 17531-00 or 17531-01 D - Used with wing tip 17531-48. E - Used if wing tip fuel tank is not installed F - Used if wing tip fuel tank is installed. G - Refer to Figure 3 for balance of component pans Y - Used on PA-23-250 (Six Place) airplanes only SECTION I Wing Group SERIAL NUMBERS 1 . 1 AFFECTED When ordering. a l w a ~specify Pan Number, Dewription and Serial Number of Aircraft 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 REVISED: AUGUST 1979 l B l l 27-1 to 27-7564168 inclusive 27-1 to 27-7654168 inclusive 27-1 to 27-7554168 inclusive 27-1 to 27-75541 88 inclusive 27-1 to 27-75541 68 inclusive 27-1 to 27-7654168 inclusive 27-1 to 27-7554168 inclusive 27-7654001 to 27-7954087 incl 27-7954088 and up 27-7654001 to 27-7954087 incl 27-7964088and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 and up 27-7654001 end 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 27-7664001 to 27-7950087 incl. 27-7964088 and up 27-7660001 and up 27.7664001 and up PA-23-250 (Six Place) PA-23-250, PA-23-235 PIPER PARTS CATALOG a REVISED: FEBRUARY 1979 Figure 5 Complete Fuselage l B l 2 PA-23-250 (Six Place) PA-23-250, PA-23-235 SECTION II Fuselage Group COMPLETE FUSELAGE Y DRAWING - Complete Fuselage Assembly Figurn PIPER PARTS CATALOG FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY FUSELAGE ASSEMBLY and Indox N m b u 6- ~FUSEUGE ASSEMBLY A.Y FUSELAGE ASSEMBLY BXX 'FUSELAGE ASSEMBLY - (Center soction) B.Y FUSELAGE ASSEMBLY - (Center m i o n ) 0.Y FUSELAGE ASSEMBLY - (Center soction) 0.Y FUSELAGE ASSEMBLY - (Canter section) Part Numbof 16919 16475 30020 30717 31588 B.Y FUSELAGE ASSEMBLY - (Cmtff ~ c t i o n ) C X 2 FUSELAGE ASSEMBLY - (Aft wction) C.Y FUSELAGE ASSEMBLY - (Aft wction) C.Y FUSELAGE ASSEMBLY - (Aft wction) 132044-00 I C.Y I*FUSELAGE ASSEMBLY - (Aft m a i m ) C o d . X X L DX Y Y 132609-02 1 C.Y I*FUSELAGE ASSEMBLY - (Aft section) NOMENCLATURE DRAWING - Platbs Inst8llation. Iw Shmld DRAWING - Complete Funloge h m M y DRAWING - Camphe Fuselage As#embly DRAWING - Compht. Fuselwe DRAWING - Complete Funlage As#embly c*y I FUSELAGE ASSEMBLY - (Aft section) A - See Figure 6,6A, 7 . 7 k 8 a d 9 for component pam. B - See Figure 7 for component p a r . C - See Figure 8 for component parts. D - Used when 28-volt alemicrl ryrtm is inatollrd. E - Used when 14-volt alectrical ryrtmn is i n m l l d . X - Usad on PA-23-260 airplanm only Y - Used on PA-23-260 (Six Plow) airplaner only. Z - Used on PA-23-236 airplanes only SERIAL NUMBERS 1 2 1 AFFECTED 27-259 to 27-364 indusive 27-2000 to 27-2604 inclusive 27-2606 to 27-3836 inclusive, 27-3838 to 27-3943 inclusive 27-3837, 27-3944 to 27.76541 68 inclusive 27-7664001 and up 27-1 to 27402 indusive 27-403 to 27-504 indusive 27-259 to 27-364 indusive 27-2000 to 27-2299 inclusive 27-2306 to 27-2504 inclusive 27-2606 to 27-3049 inclusive, 27-3051 to 27-3153 inclusive 27-3050, 27-31M to 27-3836. 27-3838 to 27-3943 inclusive 27-3837.27-3944 to 27-4425. 274427 to 274673 inclusive 274426,274674 27-7654168 inclusive to 27-7664001 a d up 27-2060 to 27-2299 inclusive 27-2300 to 27-2604 inclusive 27-2606 to 27-3836 inclusive. 27-3838 to 27-3943 inclusive 27-3837, 27-3944 and up 27-2000 to 27-2504 inclusive 27-2506 to 27-3049 inclusive. 27-3051 to 27-3163 inclusive 27-3060. 27-3154 to 27-3836. 27-3838 to 27-3943 inclusive 27-3837, 27-3944 to 2 7 4 2 5 . 274427 to 274673 indusive 274426,274574 to 27-7654168 inclusive When ordering. a h y r m i f y Pan Number, Description and Serial Number of Aircraft REVISED: MARCH 1980 PA-23-250 (Six Place) PA-23-250. PA-23-235 COMPLETE FUSELAGE Figure PIPER PARTS CATALOG - 1:::~ 1 N::ier 1 :do Number 5-4 16228-00 A.X,Z 30392-00 30392-04 A.Y I ' NOMENCLATURE + FRAME ASSEMBLY - Fuselage FRAME ASSEMBLY - Fuselage 130392-05 1 A,Y 1. FRAME ASSEMBLY - Fuselage FRAME ASSEMBLY - Fuselage HANDLE - Cabin assist GAUGE - Air temperature GAUGE - Air temperature (Maxwell, M a n n ~ n g& Moore, Inc ) GAUGE - Air temperature (Rochester) NUT - (AN365-428) SUPPORT ASSEMBLY - Fuselage skin ' BRACKET ASSEMBLY - Fuselage skin support PAD ASSEMBLY - Fuselage skin support GROMMET - Engine control support STEP ASSEMBLY - Fuselage STEF! ASSEMBLY - Fuselage BOLT - (AN4-14A) WASHER - (AN960-416) PLATE - Ice shield center, left PLATE - Ice shield center, right PLATE - Ice shield lower, left PLATE - Ice shield lower, right PLATE - Ice shield upper, left PLATE - Ice shield upper, right STUD - (#2600-5) WASHER - Split (#26W-SW2) HANDLE - Cab~nassist GASKET - Air temperature gauge attachment BUSHING - Air temperature gauge, interior BUSHING - Air temperature gauge, exterior WASHER - Air temperature gauge WASHER - Air temperature gauge 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 SECTION II Fuselage Group SERIAL NUMBERS AFFECTED 27-2000 to 27-2504 inclusive 27-2505 to 27-3049 inclus~ve, 27-3051 to 27-31 53 inclus~ve 27-3050. 27-315 4 to 27-7554168 inclus~ve 27-7654001 and up 27-1 to 27-271 2 ~nclusive 27-2713 and up 27-8054001 and up 27-1 to 27-4080 lnclus~ve 27-4081 and up 27-3623 and up 27-2713 and up 27-271 3 and up 27-2713 and up 27-2713 and up 27-271 3 and up 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 P I P E R A I R C R A F T C O R P O R A T I O N REVISED: OCTOBER 1976 Figure 6. Fuselea Forward Section 1815 FUSELAGE FORWARD SECTION (PA-23-250 and PA-23-235) SECTION I1 Fuselage Group When order~ng,olwoys spcc~fyPart Number, Description and Serial Numberaof Aircraft REVISED: MAY 1975 1 B l 6 Figure and index Number 6 - -1 -2 -3 -4 -5 -6 -7 - 8 -9 -10 -11 -12 -13 -14 - 15 -16 - 17 - I 8 - 19 -20 -21 -22 -23 -24 z0 mXI P 1 1 1 1 I 1 1 1 AR AR AR I 1 1 1 I 1 1 1 1 1 1 1 1 1 1 1 1 1 1 1 I 1 1 Part Number 16300 30049 19447 16828 30 186 17262-00 17216-00 17244-00 17214-00 17247-00 17245-00 17248-00 17252-00 751 228 80122-69 80122-70 80122-71 19447-19 17787-00 16819-00 16827 -00 16827-02 17785-00 16825-00 17786-00 16826-00 16823-00 16823-01 30663-02 30662 -02 16866-00 30035-00 16885-00 19860-00 19860-03 30340-00 19553-04 19553-02 17360-10 19515-00 k m D B CX A B E F A B A B B B D B B B SERIAL NUMBERS AFFECTED 27 - 1 to 27 -402 ~nclusivc 27-259 to 27-364 ~nclusivc 27 -403 and up 27- 1 to 27-402 inclusive 27-259 to 27-364 ~nclusive 27 - 1 to 27 -366 inclusive 27-367 to 27-430 ~nclusive 27-431 and up 27-403 and up NOMENCLATURE DRAWING - Fuselage Assembly DRAWING - Pusclage Assembly DRAWING - Fusclage Forward Scction DRAWING - Shclves Installation DRAWING - Fuselage Assembly ANGLE - Baggage compartment door frame, upper r e a r corner ANGLE - 6aggage compartment door frame, r e a r ANGLE - Baggage compartment door frame, lower r e a r corner FAlRING - 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 f t . section) WASHER - Shim (.032) WASHER - Shim (.064) WAStlER - Shim (. 125) PANEL ASSEMBLY - Right r e a r , side SHELF - Radio power supply SHELF ASSEMBLY - Rear radio support SHELF - Lower radio support SHELF - Lower radio support BRACKET - Radio shelf, left BRACKET - Radio shelf support, left BRACKET - Radio shelf, right BRACKET - Radio shelf support, right SHELF ASSEMBLY - Side radio support, left SHELF ASSEMBLY - Side radio suppon. rlght PANEL - Fuselage access, left r e a r PANEL - Fuselage access. right front PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - Instrument PANEL ASSEMBLY - lnstrument TOP ASSEMBLY - Forward section SKIN - Rear top SKIN - Center top assembly STRINGER A - Used when Collins Radio installation i s not used. B - Used when Collins Radio installation is installed. C - Used when 14 Volt electrical system i s ~ n a a l l e d . D - Used when 28 Volt electrical system i s installed. E - This cannot be used when receptacle i s ~nstalled. F - Used when receptacle 1s installed. X - Used on PA-23-250 airplanes only. SECTION 11 F u s e l a g e Group FUSELAGE 1-ORWARD SEC'I ION (PA -23-250 and I ' A - 2 3-235) W h e n ordering, always specify Port N u m b e r , Description a n d Seriol Number of Aircraft REVISED: h4AY 1975 Z 0 P m P I 1 1 I 1 1 1 1 1 2 1 1 I I 1 1 1 1 I 1 1 1 I I 2 1 1 I 1 1 1 1 1 1 1 1 4 '4 1 1 1 1 I 3 I 1 I 1 1 Figure and Index Number 6-25 -26 -27 -28 -29 -30 -3 1 -32 -33 -34 -35 -36 -37 -38 -39 -39a -39b - 3 9 ~ -39d -3% - 3 -3Yg -40 -4 1 -42 -43 -44 -45 -46 -47 -48 -49 -50 -51 -52 -53 -54 -54a -54b -55 -56 SERIAL N U M B E R S AFFECTED 27-1 l o 27-366 ~ n c l u s i v e 27 -367 ant1 up 27-1 ro 27-366 ~ n c l u s ~ v r 27-367 and i ~ p 27-1 to 27-366 ~ n c l u s ~ v c 27-367 and up 27-1 t o 27 - 3 b 6 lnclusivc 27 -367 and up Port Number 19535-00 19535 -0 1 17360-23 17346-00 17345-00 17345-01 17346-01 17504-02 19826-00 17344 -00 17358-06 17358-05 484 342 17354-01 17354-00 17348-01 17348-00 19447-18 19802-02 487584 494 060 19802-03 487 584 4 9 4 0 ( ~ 0 484 342 19327-00 19327-05 17360- 12 17360-13 17360-14 17360-15 19327-03 19326-00 17497-04 17497-05 19447-13 487 584 494 057 19447-20 19830-00 30063-00 30063-03 18617-00 17758-OJ 30060-02 30060-03 16340-00 17504-05 19827 -00 a m X A B A A B D B B NOMENCLATURE BULKIiEAD ASSEMBLY - T'op, station 55, LI I BULKHEAD ASSEMBLY - Top. station 55, RII BULKIIEAD ASSEMBLY - Fuselage forward section CIiANNEL - F u s c l a g c bulkllcad, upper left CllANNEL - F u s e l a g e bulkhead, upper left CHANNEL - F u s c l a g e bulkhead, upper right CtIANNEL - Fuselage bulkhead, upper right BULKHEAD - Upper BULKHEAD - Upper IIRACKET - 1-usclngc bulkl~cnd CHANNEL - Fuseloge forward scct ion, lcft CHANNEL - F u s e l a g e forward section, right RECEPTACLE - (42600-2 12 -12D) ANGLE - F u s e l a g e forward section, right ANGLE - F u s e l a g e forward section, left ANGLE - F u s e l a g e forward section, right ANGLE - F u s e l a g e forward section, left PANEL ASSEMBLY - Lcft front s l d e PLATE ASSEMBLY - A c c e s s , powerpak filler line STUD - Slotted head (12600-2) LOCK WASI1ER - (#2600-LW) PLATE A,SSEMBLY - A c c e s s . b r a k e fluid r e s e r v o i r STUD - Slortcd head (U2h00-2) L ( K K \VASI IER - (t3.000- I,W) RECEP'I'ACLE - Scud (r1212-121)) SECTION ASSEbIBLY - Fusclage nosc SECTION ASSEMBLY - Fuselage nose SKIN - Nose, Icfc sitlr S K h ' - Nosc, rig111 s i d e SKIN - Nose, front top SKIN - Nose, front bottom PLATE ASSEMBLY - Landing light c o m p a r t m e n t back FAIRING - Fuselage nose BULKHEAD ASSEMBLY - T o p , station 6 BULKtlEAD ASSEMBLY - Bottom, station 6 PANEL ASSEMBLY - Right front s i d e STUD - (#2600-2) WASHER - (#2600-SW2) BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward section BOTTOM ASSEMBLY - Fuselage forward scctioli PLATE - Nose wlleel well reinforcement TUBE ASSEMBLY - Vent, b a t t e r y box TUBE ASSEMBLY - Battery box ventilating TUBE ASSEMIILY - Battery box ventilating PLATE - Wliccl wcll stiffener BULKI-IEAD ASSEMBLY - Lower BULKtlEAD ASSEMBLY - Lower A - Used with 14 Volt electrical systcrn. B - Used.with 28 Volt clectl-ical systcrn. X - Used on PA-23-250 a i r p l a n e s only.

All PIPER Aztec PA-23-250 parts catalog