PIPER PA-30 AND PA-39 TWIN COMANCHE PARTS CATALOG

Piper PA-39 Twin Comanche C/R · V Speeds Reference

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Overview

This document is a Parts Catalog for the Piper PA-30 and PA-39 Twin Comanche aircraft. It provides detailed information on replacement parts, including part numbers, descriptions, and serial number applicability. The catalog is organized into sections that cover various components of the aircraft, such as the wing group, fuselage group, and power plant group. Each section includes illustrations and lists of parts required for assembly or replacement. The catalog is intended for use by maintenance personnel and aircraft owners to ensure proper identification and ordering of parts. It is important to note that this catalog should not be used for rigging and installation purposes, as it is strictly for parts identification.

The catalog covers parts for both Piper PA-30 and PA-39 models.
It is divided into ten major sections for easy navigation.
Users must specify part numbers and aircraft serial numbers when ordering.
The catalog should not be used for rigging and installation purposes.
Revisions are periodically issued, and users should keep their copies current.

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Originally published by docs.northeastcomanche.org. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type: V Speeds Reference
Year: 1982
Pages: 379
File size: 12 MB
Publisher: docs.northeastcomanche.org

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In this document

Introduction

The Parts Catalog is designed to provide clear identification of replacement parts for the Piper Twin Comanche models PA-30 and PA-39. It is divided into ten major sections, each containing illustrations and part listings. Users are advised to study the catalog thoroughly before use.

How to Identify a Part

To identify a part, refer to the figure number and index number in the catalog. Locate the section where the part is used and find the part on the corresponding illustration. If the part is not found, check other figures within the same section.

How to Order Parts

When ordering parts, always specify the part number, description, and serial number of the aircraft. Orders should be placed through authorized distributors, and it is essential to provide accurate information to avoid delays.

The catalog includes a comprehensive table of contents that outlines the various sections and their corresponding grid numbers, making it easier to navigate through the document.

Revisions

The catalog is periodically revised, and users are encouraged to keep their copies up to date. Current revisions are noted within the document, and users should refer to the last card of the parts price list for a checklist of current revision dates.

Safety notes

Under no circumstances shall this catalog be used for rigging and installation purposes.

Full document text

• -. • PIPER· PA·30 AND PA·39 TWIN COMANCHE PARTS CATALOG CARD 1 OF 2 PIPER AIRCRAFT CORPORATION (PART NUMBER 753 646) 1Al r - WARNING ne information contained in this manual Is perlodlcaUy revised. Piper Aircraft Corpondon uri" aU users of this manual to keep It current. Contact your ne.r~$t Piper Aircraft Corpondon distributor to arrange for a subscrlpdon to future revisions. NOTE Revision service is available in aerofiche format only. ,. • • • • • PIPER PARTS CATALOG AEROFICHE EXPLANATION The Parts Catalog information incorporated in this sat of Aeroficha ClJrds has been arranged in accordance with the general specrncanons of Aerofiche adopted by the General Aircraft Manufacturer's Association. Conversion of Aerofiche alphal numeric code numbers: First number is the Aerofiche card identifier. Lener 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 lA7 of Aerofiche card number 1 of this set. Each additional card In this set will hava a Tabla of Contants for all sections on that particular card. This table will start at Grid A3. REVISIONS The information compiled in this Aerofiche Parts Catalog will be kept current by revisions distributed periodically Thase revisions will supersede all previous revisions and will be complete Aeroficha card replacements and shall supersede Aerofiche cards of the same number in the set. Current Revisions to the PA-30 and PA·39 Parts Catalog issued February 1973 are as follows: 753 646 (PR770211). • • • . . • . . . • . . . • . . . . . . . . . . . . . . . . . • • • . .. Dated February 1977 753 646 (PR800514) •..••..•.•.............•....•••...••••..... Dated May 1980 753646 (PR820910) Dated September 1982 NOTE: Refer to the last card of the Piper. Parts Prica Ust - Aerofiche for a check list of current revision dates and card effectivities for this parts catalog. REVISED: SEPTEMBER 1982 1A2 PA·30 PA·39 PIPER PARTS CATALOG INTRODUCTION Thil illustrated P.rtl C.tslog II designed to provide limpl. but positive identlfic.tlon of replacement part. for the Piper "TWIN COMANCHE" Modell PA·30 and PA·39, m.nuf.ctured by the Piper Aircr.ft Corporation ot"Lock Haven, Pennsylvania. NOTE: UNDER NO CIRCUMSTANCES SHALL THISCATALOG BE USED FOR RIGGING AND INSTALLATION PURPOSES. It is suggested th.t this c.talog be thoroughly Itudied to determine ItI .rr.ngement prior to it. utilization. 1. Th. cat.'og il divided Into ten (10) m.jor netlonl dMeribed.a follows: •. Section I I to IXinclusive containl .11 replacement part. for the completed .'rplane. E.ch netion II aubdlvided and e.ch division includel an illultratlon and • peril listing. b. Section X i. the MlsceUaneou. Group. Thil group includes a listing of the Option.' Equipment Kit., Repair Kit•• nd Special Tool•. • 2. Th. following is a brief explanation of the columns in.the partl lilting: a. Th. "FIGURE AND INDEX" column indicat.. the lHultration figure number and ill part Index number. exampl.: (2·1), the 2 is tha flgur. number and the 1 is the Index number. The figure number appe.rl only at the top of .ach peril lilting page or at the beginning of each new peril lilting. b. The "PART NUMBER" column cont.ins the Identifying number of the replacement pen and this number mUlt be Ihown on all P.rts Orderl. . , c. The "CODE" column is for the purpo .. of Indicating special UHS of the pan. An explanation of the lett.r code uHd is shown belOW e.ch listing. d. Th. "NOMENCLATURE" column indicat.s the part name. Thil n.me must be Shown on.1I Parta Ordara. e. The "NO. REa." (Number Required) column rapre •• ntl the tot.' quantity of parll uHd per aircraft p. figure when the part il not indented .nd the quantity of parll uHd per ....mbly when the part il indented. The sYmbol "AR" lilted In thl. column me.ns "AI Required:' • f. Th. "SERIAL NUMBERS AFFECTED" column Indicatal the part .pplicatlon by airplane ..,., number. . Indention Exampl.: Indent.tlons of Iistingl in the "Nomenclature column" indicates ...... mbl..l .. and "componentl" or "peru," In order of th.ir Indentations. . Figure EXAMPLE and P.rt No. SERIAL NUMBERS Index Number Cocle NOMENCLATURE R~. AFFECTED Number DOOR ASSEMBLY - Bagg.gecompartment 1 • FRAME ASSEMILY - Baog.g. compartment door 1 • • HINGE ASSEMBLY· l.gg80e door 1 • • CLIP· Bagg.ge door spring 1 This lilting is int.rprsted as follows: If the DOOR ASSEMBLY (not Indented) is ordered, it willinciud. the three It.ms lilted under that it.m. If the FRAME ASSEMBLY (indented one space) is ordered, it will Includ. the two ite~ lilted under the sub .... mbly. If you want only a HINGE ASSEMBLY or CLIP, you order only th.t It.m. 3. The "ATTACHING PARTS" such III nuts. bolts, scr.ws, ete., th.t .re .v.i1abl. as comm.rcial hardw.r. items, .re not generally supplied by the Piper Aircraft Corporation. Th. catalog lilts, for your conveni.nce, those attaching parts required for main assemblies and installations. Th. identifying number for these parts appears after the part name. 4. All items of Optional Equipment are contained in the pans list in their proper sequence and sections. These items were not marked optional. since they ar. fully identified by their descriptions. • REVISED: MAY 1980 1A3 HOWTO IDENTIFY A PART IF YOU KNOW WHAT IT LOOKS UKE AND KNOW WHERE IT IS LOCATED • P I PER A I R C R AFT CORPORAT o N • - • (11 R.fer to Figure 1 to determine the section numt:.r In vIIich the pert is UIId. (2) . R.f. to the Tabl. of Contenu Ind locat. the Hetlon. Notll the figure numt:.rs that ilIustret. the venous wbgroup' of this rntlin Hetion. Ie) Select the figure tltJ. you think m1~ contain the pert you wiUl to identify end tum to the grid (.,.ge) 'PIclfied.

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(3) Find the pert on th.lIl~retlonlnd notl thllndell number. NOTE: If you don't find thl pen on this lIIum-tion. try lnother figUre in th.. woup. (4) Rlfer to the "FllJ.lfl end Indell Numt:.r" In thl Plru l"tlng for complatl dnc:rlptJon of thl pert. HOW TO ORDER PARTS In ordering Plru for your Piper Airpllflll. obIwve the following Innrue:tlons which will lid In yoII' getting the right peru r.quired without dlliay. I. Pi.... your order with the dlltflbutor or ct.ler for your territory. "nc::eperu lfIevlll'bI. only throuWl our d1uributor orgeniution. b. Alwe'i~ 'Platy the model end ..rill number of YOUr lirpllnl. c. AIWIY' 'PIafy plrt numt:.r. ne~. typllnd qullntlty required. d. Specify the method of shipment. frlight••lIPr.... percel pan.Ill' Illp,...••r frelWlt or lir plrlllli pou, Where the neture of the shipment requlrn it or when no InltfuctJons IfI gllIIn. we ....rw the right to ship the mon suitlbl. way. GENERAL INFORMATlON I. Shol"tl9" All orden IfI checked Ind rechecked t:.fore INvIng our Shipping Department. A pecking slip Is enao.cl with the shipment Ind claims for II"Ors or "'orugn mint t:. made within three days efter receipt of orders. b. Returned Gocxk No meterill "'ould be ",turned to ut without flm MQJrlng our wrltt.n pennl.lon. Meterlel sent In without notJce will be held at the owner's risk for thirty (JO) deys Ind will th.n be d1spo.cl of. we see fit. Tnmsportatlon cherges mutt t:. PREPAID on ",tumed goods 01' the shlplNflt will be refullld, c. Transportetion Liabilities The Piper Ain:nlh COf1)oretlon c::lInnot be held nlble for d~ to PlrU In trenslt from the flCtory. If I shipment is r_illed in a damaged condition. he". the dell_y man 01' Tl'ensportMlon Compeny rnlb I notlltlon of the den'llgll end fli. your dllm with the Carrier. In caM Of con_l.d dim•• do not et1llmpt to remow the plrt from the shipping contllnar CIt end_or to repell' the dem•• but call the C,"ier and hive his Claim AlJII'1t inspect the demllllJl before filing your claim with the Carrier. REVISED: FEBRUARY 19n 1 A4 PA-30 AND PA-38 SERIAL NUMBERS INFORMATION PIPER AIRCRAFT COR P 0 RAT ION •The foIlowtng Informetion should be kIP' In mind whenordwlno from thilllIt8Iot: e. The wi" numbln of 1ft. IIrcraft cownld by thl..... ClltIlot...foIlowI: 111 8eriaI numbln of the 1983 PA-3Q ModIII..3C).211O »1421M1u11w. 121 Sertal numbln of the '884 PA-30 ModIII ..30-143 to 300827 Inc...... C31 Be..... numbln of m. 19815 PA-30 ModIII..300828to 3Q.81S2, 3l).8&4 to 3lH101 InclUliw. C41 SIrieInumben of the PA-30 ModIt 'T' .. ~,30802 to 30-1711,:JO.1718 to 3Q.1'744lnc1Ut1w. ell .... nurne:-. of the PA-3Q ModII "e" ..»"'7, 30-1745 to 304000 1noIUII•• Cel SerIeI rumbln of the PA-38 ModIl .."" fD 38-1.1noIuIM. • • REVISED: FEBRUARY 1977 1 A5 PA-30 PA-39 • PIPER PARTS CATALOG STANDARD PAINT CHART MFG. PIPER PART NUMBER NO. QUART GALLON EXTERIOR ACRYUC LACQUER Juneau White LS973 4175655 1175655 Monterey Maroon (ba.. coat) 8908 4175758 1175758 Monterey Maroon (top colt) 8904 4175757 1175757 Madrid Red (base coat) 8276 4175131 1175 131 Madrid Red (top coat) 8910 4175589 . 1175589 Denver Brown (base coati 8989 4175297 1175297 Denver Brown (top coat) 8977 4175298 1175298 Tampa Green (ba.e coltl 8998 4175208 1175208 Tampa Green (top colt) 8997 4175207 1175207 Newpon Blue (base coltl 89BB 4175756 1175756 Newpon Blue (top coat) 8991 4175755 1175755 Beaumont Blue 8993 4175754 1175754 Bahama Blue 8911 4175442 1175442 Lakeland Blue 8979 4175753 ·1175753 Orlando Green 8981 4175206 1175206 Mocha Tan 8985 4176760 1176750 Pontiac Red 8954 4175590 1175590 Dakota Black 8906 4175375 1175375 Polar Gray 8986 4175204 1175204 • Reno Gold (base coat) 8976 4\75343 1175343 Reno Gold (top coati 8974 4175342 1175342 Nassau Turquoise 8978 4175751 1175 751 Bimini Turquoise 8992 4175752 1175752 Oca.a Orange (base coati 8909 4175503 1175503 Ocala Orange (top coat) 8907 4175502 1175502 Dallas Yellow 8975 4175702 1175702 Lincoln Gray 8987 4175205 1175 205 Avocado 8955 4175209 1175209 Las Vegas Gold (base coat) 8931 4175327 1175327 Las Vegas Gold (top coati 8929 4175328 1175328 Thinner (fast drying) Titanine 8930 4179 138 1179138 Thinner (slow drying) Tit,nine 8970 4179 134 1179134 REVISED: MAY 1980 1A6 PA·30 PA·39 PIPER PARTS CATALOG TABLE OF CONTENTS • FIGURE NUM8ER FIGURE nTLE GRID NUMBER View of Compl.t. Airpl.n............................................................. lAl0 SECTION I WING GROUP 2 3 4 5 8 7 8 SA 9 9A 10 11 l1A 118 12 13 14 14A 15 1SA 15B 16 16A 17 17A 18 lSA 188 19 20 20A 20B 21 22 23 23A 238 23C Wing Inst.lI.tion '................................................... lA 11 Flep and Aileron AssemblieS lA16 Wing Leadino Edge •. •••• . •• •. . . •. •••••••. . . . . •••••••. . . . . ••. •••••••. . . •. . . . . ••• •••. . • lA20 Wing R.ar Spar Sfttion. .. .. .. .. . . . . . . • • • • • . • .. • • . • .. .. • .. .. . • .. .. .. .. .. .. • .. . . . .. . • .. 1B1 Wing Skin 185 SEcnONII FUSELAGE GROUP Fusel. Forward Section. . . . •••• ... . . . .. ••••••. . . .. . .. •• .. . •. . . •. . •. .. • • .. ••. . . .. . . . . 1BB Complete Fus.I.ge (PA-3O SIN 30-2 to 30·852, 30-854 to 30-901 ind.l .......•••.••.... 1B12 Complet. FUI.I. (PA-3O SIN 30-853. 30-902 and upl(PA-39 SIN 39·1 .nd upl........ lB15 Fuselag. Top Section (PA·30 SIN 30-2 to 3O-B52. 30·854 to 30-901 Incl.)•. ••. •. . . . . . . .• . 1819 FuHl8g' Top Section (PA-30 SIN 30·853. 30·902 .nd upl (PA·39 SIN 39·1 .nd upl .•••. 1822 Fu..lag. Front Fram. A mbly .. . .. • .. .. .. . .. • .. .. . . . . .. • .. • •••• .. . . . . . . .. •• .. .. . . . .. 1C2 Fuselag. R•• r Fr.me A mbly (PA·30 SIN 30·2 to 30-852. 30-854 to 30-901 incl.) ••••• lC7 FuHl8g' R•• r Fr.m. Au·y. (PA-3O SIN 30-853. 30-902 .nd upl (PA-39 SIN 39- 1 .nd upl 1C11 Fu••I8g. Firewall Au.mbly............................................. lC16 Fus.lag•• Aft Section ••••.•.......••.•........ •. . . . . . . . . . • •. . ••. •. . . . . . . •••••• . . •. . . . 1C22 Floorbo.rd Initallltion 103 Instrum.nt Pan.llnltl. (PA-30 SIN 30-2 to 30-1716 indo 30-1718 to 30-1744 incl.l...... 108 Inltrum.nt P.ne! Instl. (PA·30 SIN 30·1717. 30·1745.nd upllPA·39 SIN 39·1 .nd upl.. 1014 CockpitFinishing Inltl. (PA-30 SIN 30·2 to 30-852. 30-854 to 30·901 incl.l.............. 1021 CockpitFinishing Instl. (PA-3O SIN 30-853. 30·902 .nd upl (PA-39 SIN 39·1 .nd upl . . •• 1E2 Window Curtain Inst.lI.tion •••. . . . . . ••••••. . . . . . . . . • . . . . . . . •. . . •. •. •. . . . . . ••. . . •••• . . . 1E8 Enclosur. Inlt.lI.tion (PA-3O SIN 30-2 to 30-852. 30-864 to 30-901 incl.l............... 1El0 Enclosur. Inltlllation (PA-30 SIN 30-853, 30-902 and upl (PA-39 SIN 39-1 .nd upl .•... 1El 3 Cabin Door................ lE17 Baggao. Compartm.nt Door An.mbly .. .. . .. .. .. .. .. .. .. .. .. . .. . .. .. .. . .. .. . .. . .. .. .. . 1E21 Se.ts Inst.llltion (PA·3O SIN 30-2 to 30-852. 30·854 to 30·901 incl.l................... 1Fl S•• tl Install.tlon (PA-30 SIN 30-853. 30-902 .nd upl (PA-39 SIN 39-1 .nd upl .. . . . . . . . 1F7 V.rtically Adjult.bl. S.ats Inltl. (PA-30 SIN 30· 1717. 30-1745 and upl (PA·39 SIN 39- 1 and upl.............................................................................. lF14 H.ater .nd o.frost.r Syst.m . . ... •••. . . . . . . . . ••. . . .. . . . . ... .. .. . ••. . . . . . . . ••. . . . . . . . . . 1Fl 7 Stew.rt-Warner H•• ter Ass.mbly (PA·30 onlyl .•..•..•.........•.••........ ••• . ••. . . . . . 1F22 Janitrol He.ter Au.mbly 1G1 Janinol H•• t.r Compon.nts. •. . . . . . . . . •••. . . . . . . . . •. •. . . . . . . . . . . . . . • •. . . . . . . . . . . . . . . . . 104 Ventil.ting System................................................................... 107 V.cuum Sy.t.m Inst.lI.tion . . . . . . . ••. . .. .. . . . •. •. . •. . . . .. . . .. . .. ••. . . . . . . . . . . . . . . . •. . . 101 1 Airspeed. Static. Oil Pressure .nd M.nifold Pres.ur. Lin.s ....•.......•...••••.......... lG14 Oxyg.n Syst.m Installation (PA-30 SIN 30-2 to 30-852. 30-854 to 30-901 incl.l 1018 Oxyg.n Syst.m Instl. (PA·30 SIN 30·853. 30-902 to »1716. 30-1718 to 3O-1744incl.l. 1021 Oxyg.n Sylt.m Inltl. (PA-30S/N 30-1717. 30·1745.nd upl (PA·39 SIN 39-1 .nd upl ... lHl • •REVISED: SEPTEMBER 1982 1A7 • PIPER PARTS CATALOG TABLE OF CONTENTS FIGURE NUMBER 24 25 26 27 27A 28 29 30 30A FIGURE TITLE SECTION III CHASSIS GROUP Nose Gear Installation ..•.........•••.•..••••......•...•.................. ' . Main Landing Gear Installation .•..•...................... _.....•...•••....•............ Landing Gear Strut Assemblies ..•...•....••..•.••..............•••.....•..•..•........ Main Wheel and Brake Assembly .•.••...•...••.....••..•......•.•..................... Nose Wheel Assembly •...••..•••.••...••..••...••............•..•...•....•.•......... Landing Gear Door Installation ..•....•..•.••.•.•.....•......•..•...•.••..•............ Landing Gear Retraction System ....•...........•.........•.•..•..•..••...•............ Toe Brake Installation ....••.•..•.•.•...•••..••..........................•••........•.. Dual Brake Installation ..•.....•.•..........•......•.....•........•....•.••............ SECTION IV TAIL SURFACES GROUP GRID NUMBER lH5 lHl0 1H15 lH20 lH23 112 114 117 1110 • 31 32 33 34 Tall Surfaces Installation. . . • . . . . . . . • • . . . • • • . • • . • . . . . . • • . . . . . • • . • . . . . . . . . . . . . • • . • . . . . . . 1113 Stabilator Assembly............................................................ .. ... . 1117 Rudder Assembly. • • • . . . • . . . . • . . • . . • • . • . • • • . . . . • • • • . . . • • . • • • • • • • . . . . . • • . • • • . • • . . . . . . . . 1121 Fin Assembly ..•..•..•.....•......• : . • • • • . • • • • . . . . . • . . • . . • • . . • . • . . . . . . • • • . . . . . . . . . . • . . 1123 SECTION V POWER PLANT GI:IOUP 35 35A 35B 36 37 3B 39 40 40A 41 42 42A 42B 42C 420 42E Power Plant and 8affle Installation ...••......................•......•....•••••......... Propeller Assembly .•..................•.............•........•..•••.....•............ Propeller Synchrophaser System Installation •.•.....••.......................•.......... Engine Nacelle Installation ..•.......••.....•......•....................•.............. Engine Controls Installation . SECTION VI FUEL SYSTEM GROUP Fuel System Installation ..............•.....................•.......................... Fuel Cell Installation· Inboard ...........•............................................. Fuel Cell Installation - Outboard ...................•................................... Wing Tip Tank Installation ............................•.......•........................ SECTION VII ELECTRICAL SYSTEM GROUP Electrical System - Forward ..............•.......................•.................... Electrical System - Aft .................................•.............................. Cockpit Electricallnstl. (pA-30 SIN 30-2 to 30-1716, 30·1718 to 30-1744 incl.) . Cockpit Electricallnst!. (PA-30 SIN 30-1717, 30-1745 and up)(PA·39 SIN 39-1 and up) .. External Power Supply (PA-30 SIN 30-2 to 30-852, 30-854 to 30-901 incl.) . External Power Supply (PA-30 SIN 30-853, 30-902 and up) (pA-39 SIN 39-1 lind up) . Anti-Cclhsicn Strobe lightlnst!. (PA-39 only) ; - 1Jl lJ7 t.n i lJ13 lJ19 lKl lK6 lK9 lK13 lK16 lL1 lL4 lL6 lL9 lLll lL13 REViSED: SEPTEMBER 1982 1A8 PA·30 PA-39 PIPER PARTS CATALOG TABLE OF CONTENTS • FIGUAE NUMBER FIGURE nTLE SEcnONVIII CONTROL SYSTEMGROUP GRID NUMBER 43 44 45 48 47 48 49 50 51 52 52A 53 54 54A 548 55 58 57 57A Control Wh ..1Installetlon. . . .. . . . . .. .. • • . . . . .. • . .. .. • • • .. .. .. . • .. • . . . .. • • • • • . . . . . . • . • • 2A4 Rudder Pedalln"'"etlon.. • • . . . • • . . . . .. • • • . . . . • .. • • . . .. . • • • . .. . .. • • • • .. .. . . . • .. • . . . . . . 2A8 Control SurfllCea Control Systems ......•••....•••••...••••••••...••••....••.•••••..... 2A11 FIlIP Control Mechenlsm Instelletion 2A15 Rudder Trim Mechenlsm Instelletion. 2A19 St.biletor Trim Mechenllm Instelletion. . . • • • • • . • . • • • • • • .. • .. • • • • . • • • • • • • • . . • . . • • • • • . . . . 2A23 SECTION IX ELECTRONICS GROUP AutoControl II Instelletlon CPA-30 only) . . . . • • • . . . . . . . • • . . . . • • •• • •• . . . . • • • • • . . . . . . • . • . . . . 2B3 . AutoControl OIlnltelietion............................................................. 2B6 AltlMetic IIlnstelietlon CPA-30 only).. .. . • .. • .. .. • .. .. • . . • .. .. . . . . . .. • .. . . . • .. .. . .. .. . .. 2B8 AhiMetic III end AItlMetic HI 8 Inste"ltlons .. • .. . . . . • • • .. . .. • .. • • • .. . . . • • . . . .. . • . .. .. .. . 2B13 AltiMetic Pilot III B-1 Instelletlon CPA-:!9 on!t') .•... ,..................................... 2B18 Glide Slope Coupler Instelletion 2821 Anti-Stetlc Equipment Instelletlon .•••••...••...•..••.•...••••••...••••••..•.•••••..... 2B23 Piper Autometic \.ocetor CELT) Inltettetion (Garrett Mfg. LTD)............................. 2C1 Piper Autometic Locetor (ELT) Installetion CNerco Avionics)............................... 2C3 Piper PM-1 Merker Beacon Instelletion '.. .. .. .. .. .. .. 2CS Redio Junction 8ox.. CPA-30 SIN 30-2 to 30-1718. 30·1718 to 3O-1744lne1., .....•.•... 2C7 Redio Junction Box.. (PA-30 SIN 30-1717. 30-1745 and up' (PA-39 SIN 39-1 to 39-14& inclulive) .••••...•••.... , • • •• . . . . • • • . • . . . . • • • . • . . • •• •• • . . . . • • • •• . . . . • • • • • • . . . . 2C10 Radio Junction Box.. CPA·39SIN 39-148 end up) • .. .. . . . .. • .. • .. . . . .. .. . . . .. • • • . • . . .. . 2C12 Redlo Drawings 2C14 SECTION X MISCELLANEOUS GROUP Optional Equipment Kits end Repair Kits............................................... 2C16 Decals. • •. . . . .. • •. . . •. • • • • . . . . • .. .. . . • • .. • .. . • • • .. • . • . • • • • . . .. .. • . • • • • . . .. • • • .. . . . . . . 2C21 • REVISED: SEPTEMBER 1982 NUMERICAL INDEX \ 1A9 201 PA·30 PA·39 • • IRCRAFT PIP ERA " ~ .. ' .- .... .- , A T ION COR P 0 R . -,._,.. ------.....-- ! <! -- MISCElLANEOUS I - ElECTRICAl VII El£CTROIUCS IX FUEl SYSTEM VI CONTROLS / _/ YI~ // .: / ~~/ .: .~ .: ~'7 •• ; .... r V TAil IV • • pllrteAirplene VI_of Com Figure 1. ISSUED: fEBRUARY 1973 1 Al0 PA-30 PA-39 PIPER AIRCRAFT COR 'OR A T ION • 1 Figure 2. WIng.....lln..latlon • • ISSUED: FEBRUARY UJ73 1 All PA-3Q PA-39 Figure Z end Port () '!=' SERIAL NUMBERS Index Number 8. NOMENCLATURE ~ AFFECTED ttl ttl Number ~ 2- 24017 DRAWING - Wing Installation 20958 DRAWING - Wing Root Fairing Installation 24005 DRAWING - Nacelle Fairing Installation -I 11473-91 PLATE - Spar, seal 2 -2 13945-42 BUMPER - Main wheel 2 -3 401 312 BOLT - Inboard aileron hinge and control rod (AN4-12A) 4 407585 WASHER - Inboard aileron hinge and cont rol rod (AN960-416L) 4 404888 NuT - Inboard aileron hinge and control rod (MS20365 -42l:lC) 4 -4 401270 BOLT - Flap hinge attachment (AN3-I1A) 12 407564 WASHER - Flap hinge attachment (AN960-IO) 12 404835 NUT - Flap hinge attachment (MS20364 -1032C) 12 -s 14976-73 Y BUSHING - Flap hinge, outer (Steel) 12 30-2 to 30-11179 mc lu s rve -Sa 26343-00 YZ ROLLER - Flap hinge, outer (Nylon) 24 30-1680 ami up, 39-1 and up -6 14976-72 BUSHING - Flap hinge, Inner 12 -7 401 311 BOLT - Outboard aileron hinge (AN4 -I1A) 2 407585 WASHER - Outboard aileron hinge (AN960-416L) 2 404 888 NUT - Outboard aileron hinge (MS20365 -428C) 2 -8 19513-37 Y WASHER - Flap hinge 24 30 -2 to 30 -1679 inc lustv c -9 20272-06 RIB - Wing nose, Sta , 211, LH 1 20272-07 RIB -Wingnose, Sta . 211, RH 1 -10 20274-08 RIB - Wing. Sta. 211. LH I 20274-09 RIB - Wing. Sta. 211. RH 1 -11 21918-00 PLATE ASSEMBLY, Fuselage rear seal. LH 1 21918-01 PLATE ASSEMBLY - Fuselage rear seal, RH 1 -12 20311-00 PLATE - Main spar attachment I -13 20313-00 PLATE - Upper spar attachment I -14 20314-00 CHANNEL - Spar attachment 1 -15 20315-00 STRAP - Main Spar attachment. upper 1 20315-02 STRAP - Main spar attachment. lower I -16 20348-00 WINDOW - Landing light I 20348-01 WINDOW - Landing light 1 ·17 20433-00 PLATE - Lower spar attachment I -Ill 401 ias BOLT - Main spar attachment, rear (AN5 -lOA) I 407586 WASHER - Main spar attachment, rear (AN960-516L) I 404890 NUT - Main spar attachment, rear (MS20365 -524C) I ·19 20476-00 FITTING - Main spar bottom attachment, LH 1 20476-01 FITTING· Main spar bottom attachment. RH 1 -20 20489-00 PLATE ASSEMBLY - Main gear wheel well splash, LH I 20489-07 PLATE ASSEMBLY - Main gear wheel well splash, RH I -21 20527-00 ANGLE - Main spar center support attachment, LH I 20527-01 ANGLE· Main spar center support attachment. RH I -22 20535-00 PLATE - Fuselage cover. LH I 20535-01 PLATE - Fuselage cover, RH I -23 401 1Ho BOLT - Main spar attachment. front (AN5 -6A) 2 407566 WASHER - Main spar attachment. front (AN960 -516) 2 404889 NUT· Main spar attachment, front (MS20365 -524C) 2 -24 20593-00 Y SUPPORT ASSEMBLY' Rear seat I 30-2 to 30-852 Inclusive, 30-HS4 to 30-901 Inclusive Y - Used on PA-30 airplanes only. Z - Used on PA -39 airplanes only. • • SECTION I Wing Group .a WING PANEL INSTALLATIOi\ When ordering, always specify Port Number. Description and Serial Number of Aircraft ISSUED: FEIlRUARY 1973 1 A12 PA-30 PA-39 • • • SECTION I Wing-Group PI ER PARTS CATALOG When ordering. always specify Part Number, Description and Serial Number of Aircraft WING PANEL INSTALLATION Figur. P Mel Pa,. No. SERIAL NUMBERS I.,.. Number COft NOMENCLATURE Req. AFFECTED Num_ 2-25 20720·00 ARM· Aileron balance weight 2 ·28 20721-00 WEIGHT - Aileron balance 2 -27 401 189 BOLT- Main spar altllchment. top (ANS-ll AI 2 407568 WASHER • Main spar altllchmel1t, top (AN960·51811 2 4Q4 889 NUT. Main ~r anachment. top (MS20365-524C1 2 ·28 419808 SCREW· Wing tip anachment. canter (MS21207C6-81 30 494071 WASHER - Wing tip anachment, centar (A3236-012-11 30 ·29 20983-00 FAIRING ASSEMBLY - Wing root. front. left 1 20983·01 FAIRING ASSEMBLY • Wing root. front, riGht 1 ·30 20984-00 FAIRING ASSEMBLY· Wing roOt. 1oWer.1.tt 1 20984·01 FAIRINGASSEMBLY· Wing root. lower. riGht 1 ·31 21287-00 FAIRING ASSEMBLY- Flap. left 1 21287-01 FAIRING ASSEMBLY· Flap. right 1 -32 20668-02 • MOULDING 3' ·33 18457-00 RING - Tie down 2 ·34 20345-00 BRACKET - landing light 2 ·35 20347·02 CLAMP· Landing liGht moulding 4 ·38 20234·00 AY AILERON ASSEMBLY - left (with trim tabl 1 30·2 to 30-1613 inclu,ive 20234·44 AVZ AILERON ASSEMBLY - Left (with trim labl 1 30·1114 and UP. 39·1 and up 20234·01 AY AILERONASSEMBLY - Right (leu trim tabl 1 30-2 to 30-1223 inclu,ive 20234·27 AY AILERON ASSEMBLY - Right (with trim tabl 1 30-1224 to 30-1813 im:lusiye 20234.43 AVZ AILERON ASSEMBLY· Right (with trim tabl 1 30·1614 and up, 39·1 and up -37 80122-99 SHIM· (.0911 2 ·38 21919·08 SEAL - Main ~r. front, left 1 21919-09 SEAL· Main .r. front, riGht 1 -39 22899-00 AY FLAP ASSEMBLY - L.tt 1 30·2 and up 22899·00 AZ FLAP ASSEMBLY. Laft 1 38·1 to 38-127 InclUsive 27247-02 AZ FLAP ASSEMBLY - L.tt . 1 3'-128 and up 22899·01 A FLAP ASSEMBLY - Right 1 ·40 419808 SCREW· Wing tip anachment. front (MS21207C8~81 8 494071 WASHER· Wing tip altllchment, front (A3238.Q12-11 8 -41 80012·94 BUSHING - Aileron rod spacer 2 -42 401393 BOLT - Main aper anachment. bonom (AN6·12A1 14 407587 WASHER· Main sPar anachment. bonom (ANHO-8161 14 404890 NUT - Main spl.r anachment. bottom (MS20365-624CI 14 ·43 206B6-02 MOULDING· Wing root top 2 -44 401 398 BOLT· Main spar attachment. bottom IANB-15AI 2 407587 WASHER - Main spar anachment. bottom (AN960.616, 2 404890 NUT - Main spar altllchment. bottom IMS20385-824CI 2 -45 410047 SCREW- Main spar attachment, center (AN509-10R-18, 4 407584 WASHER - Main spar anachment. center (AN960-10LI 4 404 887 NUT· Main spar anachment. center (MS20386.1032C) 4 ·46 400440 BOLT- Main spar anachment. center (AN3-6A, 8 407584 WASHER - Main spar anachment. center IAN980.1OL, 6 4Q4 887 NUT • Main IPBr anachment. canter IMS20366·1 oo2CI 8 -47 401 189 BOLT - Main spar anachment. center (AN5-11AI 8 407566 WASHER· Main spar anachment, center IAN960-5181 8 404 889 NUT • Main spar anachment. center IMS20385.524C, 8 -48 401394 BOLT· Main spar splice. top IAN8·13A1 1 407587 WASHER· Main spar splica. top (AN960·6181 1 404 890 NUT • Main spar splice, top (MS20386-824C1 1 A • See Figure 3 for component pa"s. Y - Used on PA·30 airplane, only. ~ • Used on PA-39 airplanes only. , REVISED: MAY 1980 1A13 Figure PIPER PARTS CATALOG and Part No. SERIAL NUMBERS Inde. Number Code NOMENCLATURE Req. AFFECTED Number 2·49 13945-60 STRIP - Nacelle fairing 8 -50 23990·00 FAIRING ASSEMBLY - Outboard, left wing 1 23990-01 FAIRING ASSEMBLY - Outboard, right wing 1 -51 23991-00 FAIRING ASSEMBLY - Inboard, left wing 1 23991·01 FAIRING ASSEMBLY - Inboard, right wing 1 ·52 20447-04 C,Y TIP ASSEMBLY - Wing, LH (with navigation light) 1 ~0-2 to 30-709 mclusive 20447-05 C,Y TIP ASSEMBLY- Wing, RH (with navigation lightl 1 ~0-2 to 30-709 inclusive 20447-08 E,Y,Z TIP ASSEMBLY· Wing, LH (with navigation light) 1 ~O- 710 and up, 39- 1 and up 20447-07 E.Y.Z TIP ASSEMBLY- Wing, RH (with nevigation light) 1 ~O- 710 end up, 39-1 and up ·53 472 666 E • LIGHT - Nevigation, right Wing, green 1 -54 751 381 E • • BULB - (#1512) 1 -55 751 201 E • • LENS - Green 1 -56 472 665 E • LIGHT - Navigation, left Wing, red 1 -57 751 381 E •• BULB - (#1512) 1 -58 751 202 E • • LENS - Red 1 ·59 20587-02 E • REFLECTOR - Navigation light 1 -60 21552-00 C,Y • TIP ASSEMBLY- Left wing 1 ~0·2 to 30-709 inclusive 21552-01 C,Y • TIP ASSEMBLY- Right wing 1 ~0-2 to 30-709 inclusive 24870-00 E,Y,Z • TIP ASSEMBLY- Left wing 1 ~-710 and up. 39-1 and up 24870-01 E,Y,Z • TIP ASSEMBLY· Right wing 1 130-710 and up, 39·1 and up -61 401 393 BOLT- Main spar splice. top (AN6-12A) 15 407567 WASHER - Main spar splice. top (AN960-616) 15 404 890 NUT - Main spar splice, top (MS20365-624CI 15 ·62 402350 BOLT- Rear spar attachment (AN 176-1 OAI 2 81342-05 WASHER - Rear spar attachment 4 404 890 NUT - Rear spar attachment (MS20365-624CI 2 -63 401 393 BOLT- Front spar attachment (AN6-12A) 2 407567 WASHER - Front spar attachment (AN960-6161 2 404 890 NUT - Front spar attachment (MS20365-624CI 2 -64 23560-00 A,B PANEL ASSEM8LY - Wing, LH 1 23560-06 A.D PANEL ASSEMBLY- Wing, LH 1 23560-01 A,8 PANEL ASSEMBLY· Wing, RH 1 23560-07 AD PANEL ASSEMBLY- Wing, RH 1 A • All items on Figures 4. 5, 6. 39 and 40 are component parts of this assembly; also items 28 to 57 inclusive on Figure 36. B - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. C • Navigation light must be grounded to wing structure iNhen replacing metal tip with plestic tip. D - Used on PA-30 with serial numbers 30-853,30-902 and up, and PA-39 with Serial numbers 39-1 and up. E - See Figure 42E if anti-collision wing tip strobe lights are installed. Y - Used on PA-30 airplanes only. Z - Used on PA-39 airplanes only. • • SECTION I Wing Group WING PANEL INSTALLATION When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: SEPTEMBER 1982 1A14 PA·30 PA-39 Figure " ~ and Port i NOMENCLATURE SERIAL NUMBERS Index Number t AFFECTED Number 2-65 25597 -00 PAD - Jack I -66 44275-02 AZ STRIP - Flow. left wing 1 44275-04 B STRIP - Flow. left wtng 1 44275-02 AZ STRIP - Flow. right wing I 44275-02 B STRIP - Flow. right wing. inboard 1 44275-04 B STRIP • Flow. right wing. outboard 1 A - Used on PA·30 airplanes with counter-rotating rlgta engine. B - Used on PA-30 airplanea if Airnow Modification Kit 760 409 haa been installed per Service Letter 558. Z • Used,on PA-39 airplanes only. . " \ , WING PANEL INSTALLATION When ordering, always specify Part NumIMr. Dncrlptian and Serial NumIMrof Aircraft SECTION I Win. Group • • •ISSUED: FEBRUARY 1973 1A15 PA-30 PA·39 PIPER PARTS CATALOG PA·30 PA-39 1A16 Flap and Aileron Assemblies Figure 3. ~44 39 45~ REVISED: MAY 1980 • • Figure ~ and Port n SERIAL NUMBERS Index Number §. NOMENCLATURE f AFFECTED Number 3-1 22699-00 Y FLAP ASSEMBLY· Left 1 30-2 and up 22699-00 Z FLAP ASSEMBLY • Left 1 39·1 to 39-127 inclusive 27247-02 Z FLAP ASSEMBLY· Left 1 39-128 and up 22699-01 FLAP ASSEMBLY· Right 1 -2 22654-00 RIB - Flap nose, inboard, left 1 22654-01 RIB - Flap nose, inboard, right 1 -3 227QS·02 Rm ASSEMBLY· Flap, nose, left 3 22705·03 RIB ASSEMBLY • Flap, noae, right 3 -4 227QS-OS Rm ASSEMBLY - Flap, !lOse, left 1 22659-~ RIB ASSEMBLY _ Flap, !lOse, right 1 -5 22659-04 Rm ASSEMBLY _ Flap, !lOse, left 1 22659-03 Rm ASSEMBLY _ Flap, IIOse, right 1 -6 22659-07 RIB ASSEMBLY. Flap, IIOse 1 -6& 22659-06 RIB ASSEMBLY- Flap, nose, left 1 22659-07 Rm ASSEMBLY _ Flap, nose, right 1 -7 22659-07 Rm ASSEMBLY _ Flap, nose. left 6 22659-06 RIB ASSEMBLY _ Flap, nose, riaht 6 -8 22704-00 RIB ASSBMBLY - Flap, nos., left 1 22704-01 Rm ASSEMBLY • Flap, nose, right 1 ·9 22704-01 Rm ASSEMBLY - Flap, IIOse, left 1 22704-00 Rm ASSEMBLY - Flap, nose, right 1 -10 22705-03 RIB ASSEMBLY - Flap, nos., left 2 22705-02 RIB ASSE"MBLY - Flap, nose, right 2 -11 22683-00 SPAR _ Flap 1 -12 22669-00 Rm - Flap 1 -13 22668-02 RIB _ Flap 5 -14 22667-00 RIB - Flap 2 -15 22668·03 RIB • Flap, left 1 -16 27247-07 SKIN ASSEMBLY _ Flap, bottom, left 1 -17 22714-00 STIFFENER _ Bottom, left 4 22714-00 STIFFENER - Bottom, left outboard 2 -18 27247-06 SKIN ASSEMBLY - Flap, top, left 1 -19 22714-00 STIFFENER - Top, left 4 22714-00 STIFFENER· Top, left, outboard 2 -20 20304-30 STRIP - Edge stiffener 1 -21 22699-02 SKIN ASSEMBLY • Flap, top, right 1 -22 22714-00 STIFFENER - Top, right 3 -23 22699-03 PLATE - Reinforcement, right 1 -24 22699·17 SKIN ASSEMBLY - Flap, bottom outboard, right 1 ·25 22714·00 STIFFENER - Bottom outboard, right 3 -26 22699-19 SKIN ASSEMBLY - Flap, bottom inboard, right 1 -27 22726-00 STiFFENER • Bottom Inboard, right 1 -28 22699-14 SKIN - Inboard 1 -29 22699-12 SKIN· center, Inboard, left 1 22699-13 SKIN· center,. inboard, right 1 -30 22699-10 SKIN - center, outboard, left 1 22699-11 SKIN • Center, outboard, right 1 ·31 22699·08 SKIN - Onboard, left 1 22699-09 SKIN: O1tboard, right 1 Y • Used on PA·30 airplanes only. Z - Used on PA-39 airplanes only. SECTION I Wing Group FLAP AND AILERON ASSEMBLIES When ordering, olwoys specify Port Number, Description and Sel'iol Number of Aircraft • • •ISSUED: FEBRUARY 1973 1A17 Figure PIPER PARTS CATALOG and Pan No. SERIAL NUMBERS Index Number Code NOMENCLATURE Req. AFFECTED Number 3-32 22668-07 • RIB ASSEMBLY - Right 1 -33 2266B-06 • RIB ASSEMBLY· Right 1 -34 23196-00 • 8RACKET ASSEMBLY· Right 1 -35 22699·29 • RIB ASSEMBLY - Right 1 -36a 2266B-02 • RIB - Flap 2 ·36 20234-00 Y AILERON ASSEMBLY - Left (with trim tabl 1 30-2 to 30·1613 inclusive 20234-44 yz AILERON ASSEMBLY· Left (with trim tab) 1 30-1614 and up. 39·1 and up 20234-01 Y AILERON ASSEMBLY· Right (less trim tab) 1 30-2 to 30-1223 inclusive 20234-27 Y AILERON ASSEMBLY - Right (with trim tab) 1 30-1224 to 30-1613 inclusive 20234-43 yz AILERON ASSEMBLY - Right (with trim tab) 1 30-1614 and up. 39-1 and up -37 20234-17 • RIB - Aileron. nose 7 -38 20234-42 • BULKHEAD ASSEMBLY - Aileron, nose 2 -39 20234-16 • RIB - Aileron 5 -40 20213-00 • SPAR - Aileron 1 -41 20211-00 • BRACKET - Aileron inboard hinge 2 760 914 • BRACKETASSEMBLY - Aileron outboard hinge 1 -42 20234-40 • PLATE ASSEMBLY - Aileron reinforcement 1 -43 20234-15 • PLATE ASSEMBLY - Aileron reinforcement 1 ·44 21265-00 • TAB· Aileron trim 1 -45 21270-00 • STRIP - Aileron reinforcement 1 ·46 20234-19 • SKIN ASSEMBLY· Aileron 1 -47 20234·04 • • GUSSET - Left aileron, top, inboard and right aileron, bottom, inboard 1 20234-05 • • GUSSET - Left aileron, bottom, inboard and right aileron, top, inboard 1 -48 20234-02 • • GUSSET - Left aileron, top, outboard and right aileron, bottom, outboard 1 20234-03 • • GUSSET - Left aileron, bottom, outboard and right aileron, top, outboard 1 -49 20234-18 • • CHANNEL - Stiffener 8 -50 20234·06 • SKIN· Top 1 20234-07 • SKIN - Bottom 1 -51 20234-10 • SKIN - Top 1 20234-11 • SKIN - 8ottom 1 ·52 20234-08 • SKIN - Top 1 20234·09 • SKIN - Bottom 1 -53 400 438 • BOLT· (AN3-4A) Hinge attachment 6 407584 • WASHER· (AN960-10L) Hinge attachment 6 -54 20234-22 • PLATE ASSEMBLY - Ailaron reinforcemant 1 -55 23087-00 PLATE - Flap access 1 Y • Used on PA-3Q airplanas only. Z - Usad on PA-39 airplanes only. • • FLAP AND AILERON ASSEMBLIES Whan ordaring, always spacify Part Number, Description and Serial Numbar of Aircraft SECTION I Wing Group REVISED: MAY 1980 1A18 PA·30 PA·39 1AID INTENTIONALLY LEFT BLANK • • • • PIP E R AIRCRAFT P O R A T I COR o N •- 4 Wing· L..eadngEdge Figure . . FEBRUARY 1973 ISSUED. JA20 PA·30 PA·39 Figure Z ond Port i 9 SERIAL NUMBERS Index Number NOMENCLATURE t AFFECTED Number 4- 23562 DRAWING - Wing Leading Edge Allsembly -I 23562-00 AB LEADING EDGE ASSEMBLY - Wing. left I 23562-01 AS LEADING EDGE ASSEMBLY - Wing, right I -2 23508-00 TIP - Front spar. LH I 23508-01 TIP - Front spar. RH I -3 20386-02 SHIM - Sts. 25 2 -4 20235-02 ANGLE - Sta. 25 i -5 20235-03 ANGLE - Sta. 78, inboard I 20235-06 ANGLE - Sta. 78, outboard 1 -6 20236-00 ANGLE - Sta. 32, left I 20236-01 ANGLE - St •• 32, right 1 -, 20272-10 am • Wing, nose, Sta, 211, LH 1 20272-il Rm - Wing, nose, Sta. 211, RH I -ij 20275-06 Rm - Wing, nose and center section, Sta. 197, L11 1 20275-07 Rm - Wing, nose and center section, St a. 197, RH 1 -Q 20282-00 Rm - Wing. nose section, Sta. 143, LH 1 20282-03 Rm - Wing, nose section, Sta. 143, RH 1 -10 20296-08 SPAR ASSEMBLY - Wing, main, left 1 20296-07 SPAR ASSEMBLY - Wing, main, right 1 -II 20252-06 SPAR ASSEMBLY - Wing, main, outboard section, LH 1 ·20252-05 SPAR ASSEMBLY - Wing, main, outboard section. RH 1 -\2 2355\-00 SPAR ASSEMBLY - Wing, main, inboard section. LH I 23551-01 SPAR ASSEMBLY - Wing, main, inboard section, RH I -13 203Q6-00 FITTING - Main spar attachment 2 -14 20310-02 RIB - Wing. Sta. 169. LH I 20310-03 RIB - Wing. Sta. 169, RH I -15 20346-00 BRACKET - Landing light support I -16 23488-06 RIB ASSEMBLY - Wing, Sta. 120, LH I 23488-07 RIB ASSEMBLY - Wing, Sta_ 120. RH 1 -.17 23488-02 Rm - Wing. nose, Sta. 120. LH 1 23488-03 RIB - Wing, nose. Sta. 120, RH I -18 23530-06 Rm ASSEMBLY - Wing, Sta. 108, LH I 23530-07 RIB ASSEMBLY - Wing. Sta. 108, RH I -19 23530-02 RIB - Nose, wing, Sta. 108, LH 1 23530-03 RIB - Nose, wing, Sta. 108, RH 1 -20 2352.1-06 RIB ASSEMBLY - Wing, Sta. 97. LH 1 23523-07 RIB ASSEMBLY -Wing, Sta. 97. RH 1 -21 21523-02 RIB - Wing. nose, Sta. 97, LH I 2352.1-0;) RIB - Wing. nose, Sta. 97. RH I -22 22158-10 Rm ASSEMBLY - Wing. bottom, Sta. 88, LH I 22158-11 Rm ASSEMBLY - Wing, bottom, Sta. 88, RH I -23 22158-02 RIB ASSEMBLY - Wing. bottom, Sta. 88, LH 1 22158-03 Rm ASSEMBLY - Wing, bottom, St •• 88, RH I A - All items on Figures 39 and 40 are component parts of this assembly. B - See Figure 6 for Leading Edge Skins. WING - LEADING EDGE When ordering, olways specify Port Nunlber. Description and Seriol Number of Aircraft SECTION I Wing Group • • •ISSUED: FEBRUARY 1973 1A21 PA-30 PA-39 Figure Z and Part () 9 SERIAL NUMBERS Index Number 8- NOMENCLATURE ;0 AFFECTED ~ 111 Number .p ~-2~ 22158-08 Y RIB ASSEMBLY - Wing, top, Sta. !:I 8. LH I 22158-14 Z RIB ASSEMBLY - Wing, top, Sta. 88, LH I 22lS8-09 Y RIB ASSEMBLY - Wing, rap, Sta. 88, RH I 2215H-15 Z RIB ASSEMBLY - Wing, top. Sta. 88, RH I -25 2.1514-00 RIB - Wing, nose, SIa. 77, LH I 23514-01 RlB - Wing, !!·'"e, Sta. 77. RH l -2tl 22162-02 RIB - Wing, Sta. 77, LH I 22162-03 RIB - Wing, SIa. 77, RH I -27 22162-08 Y RIB ASSEMBLY - Wing, lap, Sta. 77, LH 1 22162-14 Z RIB ASSEMBLY - Wing, top. Sta. 77. LH I 22162-09 Y RIB ASSEMBLY· Wing, top. Sta. 77. RH I 22162-15 Z RIB ASSEMBLY - Wing. top, Sta. 77. RH I -28 22162-10 RIB - Wing. bottom, 5ta. 77. LH I 22162-11 RIB - Wing, bottom. SIa. 77. RH . 1 -29 23497-00 RIB ASSEMBLY - Wing. Sta , 62, LH I 23497-01 RIB ASSEMBLY - Wins, Sta. 62. RH I -30 20307 -10 Y RlB ASSEMBLY - Top. Sta. 52, LH I 20307 -14 Z RIB ASSEMBLY -Top. 5ta. 52. LH I 20307 -II Y RIB ASSEMBLY - Top, Sta. 52, RH I 20307 -15 Z RIB ASSEMBLY - Top, Sta, 52, RH I -31 20307-08 RIB ASSEMBLY - Bottom. Sta. 52, LH I 20307-09 RIB ASSEMBLY - Bottom, Sta. 52. RH I -32 20307-06 RIB ASSEMBLY - Sta. 52, LH I 20307 -07 RIB ASSEMBLY - Sta. 52, RH I -33 20303-16 Y RIB ASSEMBLY - Top. Sta. 41, LH I 20303-22 Z RIB ASSEMBLY - Top. Sea, 41, LH I 20303 -17 Y RIB ASSEMBLY - Top, Sta , 41, RH I 20303-23 Z RIB ASSEMBLY - Top, Sra , 4 l , RH I -34 20303 -18 RIB ASSEMBLY - Bottom, Sta. 4\, LH I 20303 -19 RlB ASSEMBLY - Bottom, Sta , 41, RH 1 -35 20303-08 RIB ASSEMBLY - Sta. 4\, LH I 20303-09 RIB ASSEMBLY - Sta. 41, RH I -30 20357-10 RIB ASSEMBLY - Top, Sta. 32, LH 1 20357-11 RIB ASSEMBLY - Top. Sta , 32. RH I -37 20357-08 RIB ASSEMBLY - Bottom, Sta. 32. LH I 20357 -09 RIB ASSEMBLY - Bottom, Sta. 32, RH I -'lH 20357 -06 RIB ASSEMBLY - Sta. 32, LH I 20357-07 RIB ASSEMBLY - Sta. 32, RH I -39 23565 -00 RlB ASSEMBLY - Wing butt. Sta. 25, LH I 23565-01 RIB ASSEMBLY - Wing butt, Sta. 25. RH I ·~O 23506-00 RIB - Nose. St a , 41, LH l 23506 -0 I RIB· Nose, St a, 41, RH I -·H 23l:l03-00 RIB ASSEMBLY - Wing butt. no se, Sta. 25, LH I 23H03-0l RIB ASSEMBLY· Wing butt, nose. 5ta. 25, RH I -~2 23~87-02 SPAR ASSEMBLY - Wing. front, LH I 23487-01 SPAR ASSEMBLY - Wing. front, RH 1 Y - Used on PA-30 airplanes only. Z - Used on PA-39 airplanes only . • • • SECTION I Wing Group la When ordering, always specify Port Number, Description and Serial Number of Aircraft WING· LEADIi'\G [-:1)(;1- ISSUED: FEBRUARY 1973 1A22 PA-30 PA-:~" Figure Z and Port n ., p SERIAL NUMBERS Index Number 8. NOMENCLATURE t AFFECTED no Number 4-43 2.1504-00 STIFFENER - Wing leading edge. top. LH i 23564-0i STIFFENER - Wing leading edge, top. RH I -44 20273-16 STIFFENER - Wing leading edge, top, LH I 20273-17 STIFFENER - Wing leading edge, top, RH I -45 20273-06 STIFFENER - Wing leading edge. top. LH I 20273-07 STIFFENER - Wing leading edge, top, RH I -46 20273-10 STIFFENER - Wing leading edge, top. LH 2 20273 -11 STIFFENER - Wing leading edge, top. RHo 2 -47 20273-20 STIFFENER -Wing leadi.. edge, top. LH 1 20273-21 STIFFENER - Wing leading edge. top. RH 1 -48 22157-04 ANGLE - Stiffener attachment, top, LH 1 22157-03 ANGLE - Stiffener attachment. top. RH I -49 22157-02 ANGLE - Stiffener attachment, top, LH I 22157-05 ANGLE - Stiffener attachment, top. RH I -50 22157-05 ANGLE - Stiffener attachment,. bottom, LH I 22157-02 ANGLE - Stiffener attachment, bottom, RH I -51 22157-03 ANGLE - Stiffener attachment. bottom, LH I 22157-04 ANGLE - Stiffener attachment, bottom, RH I -52 20273-17 STIFFENER - Wing leading edge, bottom. LH I 20273-16 STIFFENER - Wing lt~ading edge, bottom, RH I -53 20273-18 STIFFENER· Wing leading edge. bottom, LH I 20273-19 STIFFENER - Wing leading edge, bottom, RH I -54 23534-00 ANGLE - Nacelle attachment 1 2353.. ..01 . ANGLE - Nacelle attachment 1 -55 20386-03 SHIM - Sta, 32 2 -56 20237-02 ANGLE - Sta, 135 1 20237-03 ANGLE - Sta. 1..3 I 20237-04 ANGLE - Sta. 197 I 20237-05 ANGLE - Sta. 211 I 20237-06 ANGLE - Sta. 169 1 -57 202.15-04 ANGLE - Sta. 97 1 20235-05 ANGLE - Sta. 120 1 -58 23519-00 SPAR - Wing front, center section, LH I 23519-01 SPAR - Wing front, center section, RH 1 -59 22178-02 STIFFENER - Wing leading edge, LH I 22178-03 STIFFENER - Wing leading edge. RH I -60 22178-04 STIFFENER - Wing leading edge, LH I 22178-05 STIFFENER· Wing leading edge. RH 1 -61 22178-06 STIFFENER - Wing leading edge, LH 2 22178-07 STIFFENER - Wing leading edge. RH 2 -02 22208-00 LINER ASSEMBLY· Fuel cell corner. LH I 22268-01 LINER ASSEMBLY- Fuel cell corner. RH 1 -63 22302-00 STRINGER - Fuel cell. Ilner support, LH 1 22302-01 STRINGER - Fuel cell, Ilner suppon, RH 1 -04 2204Q-OO ANGLE - Suppon plate attachment 1 -65 20358-00 STRIP - Landing Ilght window mounting, LH I 20358-01 STRIP - Landing light window mounting, RH 1 -66 20359-00 STRIP - Landing light window mounting 2 ·67 751 228 ANGLE· Stringer (6 ft. section) 1 ., WING • LEADING EDGE When ordering, alW<JYS specify Port Number, Description and Serial Number of Aircraft SECTION I Wing Group • • •ISSUED: FEBRUARY 1973 1A23 PA-30 PA-39 • - • 1A24 INTENTIONALLY LEFT BLANK PIPER AIRCRAFT 41-'-'-'- COR P 0 RAT ION " • • ISSUED: FEBRUARY 1973 Flpe 6. Wing· R..&perSecdon 181 PA-30 PA-39 • Figure Z and Part o 9 SERIAL NUMBERS Index a NOMENCLATURE 7'3 AFFECTED Number III III Number .0 5- 234MO DRAWING - Rear Spar Assembly -I 23480-04 A TRAILING EDGE ASSEMBLY - Wing, left I 23480-08 B TRAILU'JG EDGE ASSEMBLY - Wing, left I 23480-05 A TRAILING EDGE ASSEMBLY - Wing: right I 23480-09 B TRAILU'JG EDGE ASSEMBLY - Wing, right I -2 23505-00 A RIB ASSEMBLY - Wing, Sta. 25, left I 25410-00 B RIB ASSEMBLY- Wing. Sta. 25, left I 23505 -01 A RlB ASSEMBLY - Wing. Sea, 25, right 1 25410-01 B RIB ASSEMBLY - Wing. Sta. 25, right I -3 22803-00 Y RIB ASSEMBLY - Wing, Sta. 33 1/16. left 1 10-2 to 30-5'J7 tnc lu sive 22803-01 Y RIB ASSEMBLY - Wing. Sta. 33 1/16, right I .30-2 10 30 -597 mc lu stve 22803-04 YZ RIB ASSEMBLY - Wing, Sta, 33 1/16. left l 30-59B and up. 39-1 and up 22803-05 YZ RIB ASSEMBLY - Wing, Sta. 33 1/16, right I 30-59ll and up, 19-1 and up -4 23479-00 SPAR ASSEMBLY - Wing rear (complete), left I 23479-01 SPAR ASSEMBLY - Wing rear (complete), right I -5 23476-00 SPAR ASSEMBLY - Wing rear, inboard, left I 23476-01 SPAR ASSEMBLY - Wing rear, inboard, right 1 -6 80022-92 BUSHING 1 -7 20266-02 SPAR ASSEMBLY - Wing rear, outboard. left I 20266-03 SPAR ASSEMBLY· Wing rear, outboard. right I -8 23479-04 PLATE - Splice, left 1 23479-05 PLATE - Splice, right I -9 23479-02 SHIM - Splice plate, left I 23479-03 SHIM - Splice plate, right I -10 22789-00 BRACKET ASSEMBLY, Flap bellcr ank, Sta. 68, left I 227119 -01 BRACKET ASSEMBLY, Flap bellcrank, Sta. 68, right 1 -II 22789-04 BRACKET ASSEMBLY - Flap bellcr ank , Sta. 68, left 1 22789 -05 BRACKET ASSEMBLY - Flap belle rank, Sta. 68. right 1 -12 22801-00 PLATE - Support, flap bellcrank, Sta , 68, left 1 22801-01 PLATE - Support, flap bel lc rank , Sta. 68, right 1 -13 23465-00 RIB - Wing, center, Sta. 78, left I 23465-01 RlB - Wing, center. Sta. 78, right I -14 23480-02 BULKHEAD ASSEMBLY· Landing gear rear support, left 1 234ll0-03 BULKHEAD ASSEMBLY - Landing gear rear support, right I -15 20324-02 BULKHEAD· Landing gear rear support, left: I 20324-03 BULKHEAD - Landing gear rear support, right I -16 22866-00 PLATE - Landing gear support, wing, Sta. 627/8, left I 22806 -0 I PLATE - Landing gear support. wing. Sea, 627/8. right I -17 20340-00 REINFORCEMENT - Landing gear support bulkhead, left I 20340-01 REINFORCEMENT - Landing gear support bulkhead. right I A - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. B - Used on PA-30 with serial numbers 30-853, 30-902 and up, and PA-39 with serial numbers 39-1 and up . Y - Used on PA-30 airplanes only. Z - Used on PA-39 airplanes only. • • • WINC - REAR SPAR SECTION When ordering, always specify Part Number. Description ond Seriol Number of Aircraft SECTIOl" I WIng Croup ISSUED: FEBRUARY 1973 182 PA-30 PA-39 Figure - 1 ond Port ~ SERIAL NUMBERS Index Number NOMENCLATURE I AFFECTED Number S-18 23456-00 DOUBLER - Landin. par ..pport bulkhead, left I 23456-01 DOUBLER - Landing gear support bulkhead, right I -19 20658-02 BRACKET - Flap return spring attachment I -20 20269-00 Rm - Wing. Sta. 120, left I 20269-01 RIB - Wing, Sra. 120, right I -21 20318'"00 Rm - Main, Sta. 1355/8. left I 20318-01 Rm - Main, Sta. 135 5/8. right I -22 20283-00 Rm - Main, St... 143, left I 20283-01 Rm - Main, Sta. 143, right I -23 20309-00 BRACKET ASSEMBLY - Aileron bellcrank, left I 20309-01 BRACKET ASSEMBLY- Aileron bellcrank, rigk I -24 20310-04 RIB - Wing, Sta. 169. left I 20310-05 RIB - Wing, Sra. 169, right I -25 20215-04 RIB - Wing, Sra. 191, left 1 20275-05 RIB - Wing, Sta. 197, right i ~26 20274-06 RIB ASSEMBLY - Wing, Sta. 211, left. 1 20274-07 RIB ASSEMBLY - Wing, Sta. 211, right 1 -27. 20288-00 BULKHEAD - Rear spar, Sta. 143 and 197, left 2 20288-01 BULKHEAD - Rear spar, Sta. 143 and 197, rigk 2 -28 20262-00 BULKHEAD - Rear spar. Sta. 169. left 1 20262-01 BULKHEAD - Rear spar. Sta. 169, right I -21) 20284-00 PLATE - Aileron hinge bracket reinforcell'!ent, outboard, left I 20284-01 PLATE - Aileron hinge bracket reinforcement, outboard, riJht I -30 20294-00 BRACKET ASSEMBLY - Aileron hinge, outboard 1 -31 25704-00 BEARING - Ailerort hinge 1 -32 22733-02 BULKHEAD - Rear spar. Sta. 47 and 131,90. rtaht 2 22733-03 BULKHEAD - Rear spar, Sta. 47 and 131,90, left 2 -33 20242-00 PLATE - Aileron hinge bracket reinforcement, inboard. left I 20242-01 PLATE· Aileron hinge bracket reinforcement, inboard, riJht I -34 2021)3-00 BRACKET ASSEMBLY- Aileron hinge. inboard 1 -35 25704-00 BEARING - Aileron hinge I -36 22733-06 BULKHEAD - Rear spar, Sta. 78 and 120, left 3 22733-07 BULKHEAD - Rear spar, Sta. 78 and 120, right 3 -37 22733-04 BULKHEAD - Rear spar, Sta. 33, 55, 68 and 97, left 4 22733-05 BULKHEAD - Rear spar, Sta. 33, 55, 68 and 97. right 4 -31\ 23227-03 TRACK ASSEMBLY - Flap 3 -39 22780-00 PLATE - Flap track spacer 2 -40 2273:J-08 BULKHEAD - Rear spar, Sta. 78. right 1 22733 -09 BULKHEAD - Rear spar, Sta. 78, left I -41 22708-00 BRACKET - Flap cable pulley 2 -42 2278.)-02 PLATE - Flap track reinforcing, left 1 22783-03 PLATE - Flap track reinforcing, right 1 -43 20247-00 ANGLE ASSEMBLY - Rear spar rib attachment, Sta. 211 1 -44 23475-06 RIB - Wing, Sta. 47, left 1 23475-07 RIB - Wing, Sta. 47, right 1 -45 20351-08 RIB - Wing, St a, 55, left I 20351-09 RIB - Wing, Sta. 55, right 1 -46 20263-04 RIB ASSEMBLY - Wing, Sta. 97, left I 20263-05 RIB ASSEMBLY - Wing. Sta. 97, right 1 -47 22787-00 RIB - Wing, Sta. 68, left 1 22787 -01 RIB - Wing, Sta. 68, right , 1 SECTION I Wing Group --- WING - REAR SPAR SECTION • • • When ordering, always specify Port Number, Description and S4trial Number of Airc:roft ISSUED: FEBRUARY 1973 183 PA-30 PA-39 Figure Z and Part () p SERIAL NUMBERS Index 8. NOMENCLATURE ;tl AFFECTED Number ., ., Number .a 5-48 20267~02 REINFORCEMENT ASSEMBLY - Walkway. left I 21290-02 REINFORCEMENT ASSEMBLY ~ Walkway. right 1 -49 20360~14 ANGLE ~ Gear opening reinforcement, left 1 20360-15 ANGLE - Gear opening reinforcement, right I ~50 21072-00 BULKHEAD - Landing gear door attachment, left 1 21072~01 BULKHEAD - Landing gear door attachment, right 1 -51 751 228 ANGLE ~ Stringer (6 ft. section) 1 e- - • WING ~ REAR SPAR SECTION ..... SECTION I Wing Group When ordering, always specify Part Number, Description and Sli!rial Number of Aircraft ISSUED: FEBRUARY 1973 184 PA~30 PA-39 PIPER AIRCRAFT COR P 0 RAT ION • Figure 6. Wing Skin • •ISSUED: FEBRUARV 1973 185 PA-30 PA-39 Figure Z and Part n 0 SERIAL NUMBERS Index a NOMENCLATURE ;:0 AFFECTED Number III III Number .a b- 23560 DRAWING - Wing Panel Assembly 235b2 DRAWING - Wing Leading Edge Assembly 2.'3540 DRAWING - Engine Nacelle Insta llatron ·1 20377-45 SKIN ASSEMBLY - Wing panel leading edge. outboard. right I 20377-46 SKIN ASSEMBLY - Wing panel leading edge. outboard, left I -2 23562 -10 SKIN ASSEMBLY - Wing panel leading edge. center. outboard. left j 23562-11 SKIN ASSEMBLY - Wing panel leading edge. center. outboard. right I -3 235b2-06 SKIN ASSEMBLY - Wing panel leading edge. center. inboard. left 1 23562 -07 SKIN ASSEMBLY - Wing panel leading edge. center. inboard. right I -4 20370-00 PLATE - Access hole COver I -5 2'35b2-08 SKl1\ ASSEMBLY - Wing panel leading edge. inboard. left I 235b2-09 SKI;\ ASSEYlBLY - Wing panel leading edge. inboard. right I -b 20377 -57 SKI;-.: ASSEMBLY - Wing panel. outboard, bottom. right 1 20377-58 SKI;\ ASSEMBLY - Wing panel. outboard. bottom. left I -7 17'315-00 PLATE ASSEMBLY - Reinforcement I -tl 270bS-00 PLATE ASSEMBLY - Reinforcement. lift detector 1 -'1 22982-02 PLATE ASSEMBLY - Fuel cell filler neck cover I -10 23575-00 BRACKET - Wire clamp support 1 -II 23520-00 ANGLE - Nacelle rib mounting. inboard, left 1 23520-01 ANGLE - Nacelle rib mounting, inboard. right I -12 2:1521-00 ANGLE - Nacelle rib mounting. outboard, left I 23521-01 ANGLE - Nacelle rib mounting. outboard. right I -l] 22700-14 SKIN ASSEMBLY - Wing panel. outboard. top, left I 22700-15 SKn\ ASSEMBLY - Wing panel, outboard, top, right I ·14 22700-12 SKIN ASSEMBLY - Wing panel. center. top. left I 22700-13 SKn\ ASSEMBLY - Wing panel. center, top, right I -15 22700-02 SKIN - Wing panel. inboard. top. left 1 22700-03 SKIN - Wing panel, inboard, top. right I -Ib 2.1054-04 SKIN ASSEMBLY - Wing panel leaoing edge. inboar.I, bottom, left I 23054-05 SKIN ASSEMBLY - Wing panel leading edge. Inboard, bottom. right I -17 20377-55 SKIN ASSEMBLY - Wing panel, center, bottom. right I 20377-56 SKIt' ASSEMBLY - Wing panel. center. bortorn. le.t I -18 23560-02 SKII\ - Wing panel. inboard, bottom. left I 23560-03 SKIl" - Wing panel, inboard, bottom, right I -19 227SI-Ob y SPAR - False. wing panel, outboard, left I 30-2 to 30-1503 inc lus ive 25867-06 yz SPAR - False. wing panel. outboard. left 1 30-1504 and up. 39·1 and up 22751-07 y SPAR - False. wing panel. outboard, right 1 30-2 to 30-1500 mc lus ive 258b7-07 YZ SPAR· False. wing panel. outboard. right 1 30-1501 and up. '3\.)-1 and up -20 22751-02 y SPAR - False. wing panel. center. left I 30-2 to 30-150:! Inclusive 25867-02 YZ SPAR - False, wing panel. center. left I 30-1504 anullp.l'1-1 and up 22751-03 y SPAR - False. wing panel, center, right I 30-2 to 10-1500 inc Ius ive 258fl7 -03 YZ SPAR - Fal se . wing panel. center, right I 10-1501 and up. \'1-: and \'p -21 22751-04 y SPAR - False. wing panel, Inboard. left 1 30-2 tolO-l,)Ul In,;L~I\"e :lS867-04 YZ SPAR - False. wing panel, inboard. left I 30-150.. .ir.d CP·. '1~1- " ' "I' 22751 -05 y SPAR - False. wing panel. inboard. right I 30 -2 to \0 -I :;oe m,: .. :'l\"C 25867-05 yz SPAR - False. wing panel. inboard, right I 30-1501 and up, l<l - I .ind up y - Used on PA -30 airplanes only. Z - Used on PA-39 airplanes only. • • • SECTION I Wing Group When ordering, always specify Port Number, Description and Serial Number of Aircraft W Il\G SKII\ ISSUED: FEBRUARY 1973 186 PAOlO PA ,,3'1 Figure Z and Port n \) SERIAL NUMBERS Index Number a NOMENCLATURE ;0 AFFECTED " .p Number /'1-22 17316-00 PLATE - Aileron belle rank access hole cover 1 -23 20370-00 PLATE - Access hole cover I -24 23474-00 PLATE - Wing access I -25 22998-02 PLATE· Wing acceas, left 1 22998-03 PLATE - Wing-access, right 1 ·26 23540-14 ANGLE - Nacelle mounting, bottom, outboard. LH I 23540-15 ANGLE - Nacelle mounting. bottom, outboard. RH I ·27 23540-04 ANGLE - Nacelle mounting. bottom, inboard. LH I 23540-05 ANGLE· Nacelle mounting, bottom, inboard. RH I -28 23540-12 ANGLE - Nacelle mounting, top. outboard, LH 1 23540-13 ANGLE - Nacelle mounting. top, outboard, RH 1 ·29 23543-03 ANGLE - Nacelle mounting, top 2 -30 23540-20 ANGLE - Nacelle mounting. top. outboard, LH I 23540-21 ANGLE - Nacelle mounting. top. outboard. RH 1 -31 24169-00 GUSSET - Wing reinforcement 1 -32 23543-02 ANGLE - Nacelle mounting 2 23543-03 ANGLE - Nacelle mounting 2 -33 23540-18 ANGLE - Nacelle mounting, outboard. LH 1 23540-19 ANGLE - Nacelle mountiDg. outboard. RH 1 -34 23540-02 ANGLE - Nacelle mounting. outboard, LH I 23540-03 ANGLE • Nacelle mounting. outboard, RH 1 -35 23494-00 ANGLE - Nacelle bulkbead mounting 1 -36 23526-00 ANGLE· Nacelle attachment bottom. Inboard. LH 1 23526-01 ANGLE - Nacelle attachment bottom, inboard, Rtf 1 WING SKIN When ordering, olways specify Po,t Number, Description ond Serial Number of Alreraft SECTION I Wing Grwp • • •ISSUED: FEBRUARY 1973 187 PA-30 PA-39 • PIPER AIRCRAFT IS COR P 0 RAT ION • ,- • Figure 7. Fu.le", FOl'Wlrd Section REVISED: FEBRUARY 19n 188 PA·30 PA·39 Figure Z ond Port ~ p SERIAL NUMBERS Index Number NOMENCLATURE I AFFECTED III Number 7- 23837 DRAWING" - Forward Fuselage Section Assembly -I 23837-00 Y SECTION ASSEMBLY - Forward fuselage 1 30-2 to 30-401 inclusive 23837-37 A SECTION ASSEMBLY - Forward fuselage 1 23837-39 B SECTION ASSEMBLY - Forward fuselage I -2 23837-02 BULKHEAD - Bottom, Sta. 30. LH I -3 23837"-03 BULKHEAD - Bottom, Sta. 30, RH I -4 23837-28 Y SKIN ASSEMBLY - Bottom 1 30-2 to "10-401 inclusive 23837-33 A SKIN ASSEMBLY - Bottom 1 23837-40 B SKIN ASSEMBLY - Bottom I -5 23837-08 SKIN ASSEMBLY - Top 1 -6 23837-06 BULKHEAD - Top, Sta. 40 1 -7 23837-07 BULKHEAD - Top, Sta. 20 1 -8 17866-04 COVER ASSEMBLY - Heater exhaust shroud 1 -9 19354-00 TUBE ASSEMBLY - Take -off 1 -10 23698-00 Y BRACKET - Heater, rear, risht 1 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive 25621-00 B BRACKET - Heater, rear, right 1 -11 23709-00 CHANNEL - Fuselage forward section, LH I 23709-01 CHANNEL - Fuaelage forward section, RH I -12 23719-00 Y TUBE ASSEMBLY - Heater overnow outlet 1 30-2 to 30-401 inclusive -13 23741-00 BRACKET - Heater attachment, front I -14 23788-00 BULKHEAD - Fuselage forward section. Sta. 17 1 -IS 23833-00 BULKHEAD - Fuselage. Sta. 11 1 -16 23834-00 Y CHANNEL ASSEMBLY - Forward section, lower LH 1 30-2 to 30-754 Inclusive 23834-04 YZ CHANNEL ASSEMBLY - ForWard section, lower LH 1 30-755 and up. 39-1 and up 23834-01 Cl-i.ANNEL ASSEMBLY - Forward section, lower RH 1 -17 23874-00 BRACKET ASSEMBLY - No,e wheel fairing hinge, forward, !ront, LH 1 23874-01 BRACKET ASSEMBLY - Nose wheel faIring hinge, forward, front, RH 1 -18 23875-00 BRACKET ASSEMBLY - Nose wheel fairing hinge, forward. rear. LH I 23875-01 . BRACKET ASSEMBLY - Nose wheel fairing hinge, forward, rear, RH I -19 23877-00 BRACKET ASSEMBLY - Nose wheel fairing hinge, aft, front, LH I 23877 -01 BRACKET ASSEMBLY - Nose wheel fairing hinge, aft. front, RH 1 -20 23878-00 BRACKET ASSEMBLY - Nose wheel fairing hinge, - aft. rear. LH 1 23878-01 BRACKET ASSEMBLY - Nose wheel fairing hinge, aft, rear. RH I A - Used on PA-30 with serial numbers 30-402 to 30-852 inclusive. 30-854 to 30-901 inclusive. B - Used on PA-30 with serial numbers 30-853. 30-902 and up. and PA-39 with serial numbers 39-1 and up. Y - Used on PA-30 airplanes only. Z - Used on PA-39 airplanes only. SECTION II Fusel..Group FUSELAGE FORWARD SECTION When ordering, alwoys specify Part Number. Description ond Seriol Number of Aircraft • • •ISSUED: FEBRUARY 1973 1 89 PA-30 PA-39 SECTION II Fuselage Group PIPER ARTS CATALOG FUSELAGE FORWARD SECTION Flgur. P and Part No. SERIAL NUMBERS Ind •• Numb.r Cod. NOMENCLATURE Req. AFFECTED Number 7·21 23835·00 • CLIP - Fuselage forward section channel. front, RH 1 23835-01 • CLIP - Fuselage forward section channel, front, LH 1 -22 23836-00 • CLIP· Fuselage forward section channel, rear 2 -23 23837-15 • BULKHEAD - Sta. 20. left 1 -24 484322 • RECEPTACLE - (#82-35-302-15) 19 -25 487660 • STUD· (#2·F·14O) 7 -26 23837·38 • BULKHEAD - Bottom, Sta. 40, LH 1 23837-13 • BULKHEAD· Bottom, Sta. 40. RH 1 -27 25490·00 A • TUBE ASSEMBLY· Battery vent 1 -28 25502-00 A • BRACKETASSEMBLY - 8attery support, front 1 25514-00 A • BRACKET ASSEMBLY· Battery support. rear 1 -29 23755-00 • NOSE - Fuselage section assembly 1 ·30 484482 • RETAINING RING - (PSloo17-2-64) 7 -31 180806 • WEBBING - Anti-squeak (1/32 It 7/8) 13' -32 24794-00 yz • ANGLE· Control cable support 1 30-422 and up, 39-1 and up -33 24796-00 yz • PlATE - Marker beacon bracket support 1 30-422 and up. 39- 1 and up ·34 24797-00 yz • 8RACKET - Marker beacon mounting 1 30·422 and up, 39-1 and up -35 487661 STUD· (#2·F·180) 15 -36 487661 STUD - (#2-F-180) 2 ·37 487670 STUD - (#2-F-24O) 2 -38 487671 STUD - (#2-F-260) 2 -39 484482 RETAINING RING - (PSloo17-2-B4) 21 A • Used on PA-3O with seriel numbers 30-853, 30-902 and up, and PA·39 with serial numbers 39-1 and up. Y - Used on PA-30 airpl.nes only. Z • Used on PA·39 airplanes only. • • When ordering, always specify Part Number, Description and Serial Number of Aircraft REVISED: MAY 1980 1810 PA-30 PA-39 - 1 811 . iNTENTIONALLY LEFT BLANK • • • • • . . ...... PIPER AIRCRAFT COR P 0 RAT ION • i 'I ~ ~11A r- • ISSUED: FEBRUARY 1973 Figure 8. Co~lete Fulllegt (PA-30 with Serial No•• 3()'2 to 30-862.30-854 to 3()'901 inclutlwl 1 812 PA·30 Figure - Part Code NOMENCLATURE No. SERIAL NUMBERS Index Number Aift AFFECTED Number So 24018 DRAWING - Fwe'- AaImbIy 23180 DRAWING - Fwe'- Anlmbly -1 23l8OoOO FUSELAGE ASSEMBLY 1 3002to 3O-S88 InclUllw 23180011 B FUSElAGE A.EMILY 1 ·2 2428BoOD e A" seCfION ASSEMBLY 1 ·3 . 22188-00 D FUSELAGE TOP SECTION ASlEMBLY 1 -4 208CJO.OI SKIN. ' ....top. f~ 1 .a 2OltOQ.8'7 SKIN ASi!M8LY - F~,- top. CIntW 1 .e :za-. SKIN AlllMiLY - F~""1DP.'" 1 -7 23820000 FUSELAGE BOTTOM SECTION ASBEMILY 1 3O-2·to 3O-lSB9 InciUllw 23820-17 B ,t.aELAGE BOlTOM SECTION ASSEMILY 1 -B 23820004 SKIN- &Aft ....frant 1 23B2OoOI SKIN· AW-t". front 1 .. 23B2O.Q8 SKIN. Left .... bottom. front 1 23B2047 SKIN. "W-t 1Idt. bottom. frant 1 ·10 23820-14 SKINAS8IMBLY• Bottom front.... 1 -11 23QIS.(l2 SKIN- lottom Glfttllt' 1 ·12 20800-18 SKIN- ' ....... Sta. lC1S to Ita. 113. left 1 208000115 SKIN• ,~..... Sta. lC1S to Ita. 113. right 1 ·13 23DI&:03 SKIN- Bottom eM_.... 1 ·14 22807oC15 SKINA8SIMlLY· Bottom.... 1 ·115 2280743 SKIN ~M8LY • left ....... 1 -18 22807008 SKINAllEMlLY •Sidl. Glfttllt' .... left 1 22107-23 SKINASSIMBLY·SIdI. «*11111' .... rltht 1 -17 208115004 SKIN- F~"", Sta. 1015 to .... 113, IIlft 1 237I8.Q2 SKIN· F......ta. 1015 to Ita. t.1.3. rltht 1 ·17a : 23820-18 SKIN· Bottam.front. CIIII1It 1 -1. 23'T78oOO E 'IAEWALL AND INSTRUMENT PANEL ASSEMBLY 1 ·18 23778-03 SKIN ASSEMBLY· Tap ftont 1 -20 23703000 , FRAMe ASSEMBLY. F....... front 1 -21 2282Q.OO G FRAME ASSEMBLY. F........, 1 30-2 to 3lHi88 InciUllw 22820-21 8G FRAME ASSEMBLY - F~I••,., 1 ·22 2388O.Q2 SKIN ASSEMBLY - RIIf' window. a.tt 1 238).07 .SKlN ASSEMBLY - RIIf' window. r.... t 1 -23 . 2388O.Q3 SKINAaEMILY • Left ...wIndow.1oww 1 ·24 2015115-02 PLATE· F....ClDWI' 1 .2IS 22120-02 PLATE ASSEMBLY - Fu" mai,._ 1 ·28 22QIO.(IO PLATE·V..- 2 -71 781 an KIT· e.tlIn .... ,........_",,.. 1 -28 483 391 GROMMET - Air WIlt (AN231-4) 15 A • \JIId on PA-30with ..... nunDn 30-2 to 3N62 ind....w. 300864to 3Q.801 1ncI...... B - \JIId on PA-30with ..... numbln 3lJ.88O to 30-8&2 Ind...... 3008154 to 3Q.801 lncI'-w. e -8ft Figu.. 12 for compol'llrit1*11. D- ..Fit... 9 for COi1'iPOMflt PII1I. E -..FigunI 11Bfor component PIi'tI. F ... Figunll0 far component 1*11. G·" ,... 11 for component .... \ • • •PA-30 COMPLETE FUSELAGE ("CodI"A"t 1 813 WhIn ordlrlng......,.lpICIfy Pert Number. Delerlption end s.rt.I Numblr of Alnnh REVISED: FEBRUARY 1977 SEC110NII FwNgeGraup 401 SECTION 11 Fuselage Group ISCOMPLETE FUSELAGE (See Code "A") Figure Z and Port () 9 SERIAL NUMBERS Index 8. NOMENCLATURE ;;0 AFFECTED Number 111 III Number .0 8-29 22117-00 SCOOP - Cabin air 1 -30 22122-00 TAKE-OFF ASSEMBLY - Cabin air exhaust 1 -31 23837~00 B FUSELAGE FORWARD SECTION ASSEMBLY 1 .10-2 to 30··Wl inclustve 23837-37 B FUSELAGE FORWARD SECTION ASSEMBLY 1 30-402 to 30-852, .,0-854 to :10· A - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. B ~ See Figure 7 for component parts. . • • When ordering, always specify Part Number, Description and Serial Number of Aircraft ISSUED: FEBRUARY 1973 1 814 PA-30 PIPER AIRCRAFT COR P 0 RAT ION • • ISSUED: FEBRUARY 1973 Figure SA. CcImplIt. F.... (PA-30 with seMI Not. 31)863. 30-902Iftd upt (PA-39wi1h SIrIII NOI...11nd upt 1 815 PA-30 PA039 • , Figure Z and Port ~ , 9 SERIAL NUMBERS Index NOMENCLATURE ::0 AFFECTED Number ell ell Number .p 8A- 25530 E DRAWING - Fuselage Assembly (Complete) 26726 F DRAWING - Fuselage Assembly (Complete) 25494 E DRAWING ,. Fuselage Assembly 2b450 F DRAWING - Fuselage Assembly -1 25494-00 E FUSELAGE ASSEMBLY I 26450-00 G FUSELAGE ASSEMBLY 1 26450-02 Z FUSELAGE ASSEMBLY 1 39-84 to 39-145 inclusive 26450-03 Z FUSELAGE ASSEMBLY I 39-146 and up -2 25384-00 CG AFT SECTION ASSEMBLY 1 25384~04 Z AFT SECTION ASSEMBLY 1 39-84 and up -3 25355-00 BY FUSELAGE TOP SECTION ASSEMBLY 1 30-853, 30~902 to 30-1548 25355-08 BYZ FUSELAGE TOP SECTION ASSEMBLY 1 30-1549 and up, 39-1 and up -4 20600-09 SKIN - Fuselage top, forward 1 -5 25355-03 SKIN ASSEMBLY - Fuselage top, center 1 -6 25355-06 SKIN ASSEMBLY - Fuselage top, rear 1 -7 25461-02 SKIN ~ Fuselage top, side 2 -8 25383-00 E FUSELAGE BOTTOMSECTION ASSEMBLY 1 26361-00 G FUSELAGE BOTTOM SECTION ASSEMBLY 1 26361-06 Z FUSELAGE BOTTOMSECTION ASSEMBLY 1 39-84 to 39-l45 inc lus ive 26361-07 .Z FUSELAGE BOTTOM SECTION ASSEMBLY 1 39-146 and up -9 25383-06 SKIN ~ Side, center, left 1 25383-07 SKIN ~ Side, center, right 1 -10 20600-15 SKIN - Side, bottom center, rear, left 1 206oo~16 SKIN - Side, bottom center, rear, right I -11 23820-04 SKIN - Lett side, front 1 23820-05 SKIN - Right side, front 1 -12 23056-02 SKIN - Bottom, center 1 -13 25383-02 SKIN - Bottom, rear 1 -14 23820-15 SKIN - Bottom, front, center 1 -15 25383-05 SKIN ASSEMBLY - Right side, rear I -Ib 25382~02 Y SKIN - Bottom, center, rear 1 30-853, 30-902 to .30-1552 25382-07 D SKiN ASSEMBLY - Bottom, center, rear 1 26360-03 F SKIN - Bottom, center, rear, right 1 26360-02 F SKIN - Bottom, center, rear, lett 1 -loa 17315-00 D PLATE ASSEMBLY - Reinforcement 1 A - Used on PA-30 with serial numbers 30-853,30-902 and up, and PA-39 with serial nwnbers 39-1 and up. B - See Figure 9A for component parts. C - See Figure 12 for component parts. D - Used on PA-30 with sertal nwnbers 30-1553 to 30-1716 inclusive, 30-1718 to 30-1744 inclusive. E - Used on PA-30 with serial numbers 30-853, 30-902 to 30-17Hi inclusive, 30-1718 to 30-1744 inclusive F - Used on PA-30with serial numbers 30-1717, 30-1745 and up, and PA-39 with serial numbers 39-1 and up. G - Used on PA-30 with serial numbers 30-1717, 30~1745 and up, and PA-39 with serial numbers 39~1 to 39-83 Inclusive. Y - Used on PA-30 airplanes only. Z ,. Used on PA-39 airplanes only. • • • SECTION II Fuselage Group < ~ '-- :',' -----.< COMP1-... _;;; FUSELAC' (See Code ", When ordering, always specify Port Number, Description and Seriol Number of Airc;raft ISSUED: FEBRUARY 1973 1 816 PA-30 PA-39 '..... IIId Part Code NOMENCLATURE No. SERIAL NUMBERS I'" Number '-eq AFFECTED Number 8A·17 20816004 SKIN· F....... Sta. 10&to Ita. 113. left 1 2376&02 SKIN· Fwe.... Sta. 101 to Ita. 113. rlPt 1 ·18 238:z0.08 SKIN. Uft .... bottom. front 1 23820-07 SKIN· Right .... bottom. front 1 ·1. 23820-18 SKIN· Bottom.frant. 0IfIW 1 ,19 23778-CM HY FIREWALL AND INSTRUMENT PANEL AllEMlLY 1 31-8&3.30-102 to 3().1700 283»00 HY FIRIWALL AND INSTRUMENT PANIL AISIMILY 1 30-1701 to 3o.1718Inclualw. 30-1718 to 3o.1744lncluah. 283158-00 HJ FIRIWALL AND INSTRUMENT PANEL AISIMILY 1 283!18-O4 HZ FIREWALL AND INSTRUMENT PANEL AIlE_LV 1 :J8.84 to 39-14& Inclualw 213.. HZ FIREWALL AND INlTftUMENT 'ANIL AlllMiLY 1 3I-1411ftdup ·20 2377tJ.03 G SKIN ASllMiLY • Top front 1 28318003 I SKIN AIIIM8LV • Top front 1 ·201 214-.00 I SKIN· Top front. left 1 21488-01 I SKIN· Top front. right 1 ·21 23703000 DO FRAME ASSEMBLV• FUill••front 1 23703-03 BD FAAME ASSEMBLY- FUIII..... front 1 ·22 2!i3:J3.00 EO FRAME ASSEMBLV• FUIII..... ...., 1 26333-17 IE FRAME AlSEMlLY • FIIIII..... ...., 1 ·23 2388Q.OB SKIN - Frant windclw.1eft 1 ·24 21481-04 SKIN· Clnnr window. 11ft 1 25411-01 SKIN. CInnr window. '1Ft 1 ·21 21411.03 SKIN· Top ".1Ift 1 ·28 21411.(11 SKIN· lAft "."" 1 ·27 22211.00 PLATE AlSIMILV • FUII"'_", ...nfonwm Nlnforolmlnt 1 ·28 205IIS-02 G PLATE· Fu...... bottom 0lMf 1 ·29 413 311 GROMMET· AI' wnt (AN231-4. 15 -30 711077 . KIT ·Clbln .......'--nwlt' 1 ·31 221520-02 PLATE AlSEMBL V • "'II,nI_... 1 ·32 2209040 PLATE • Vent 2 ·33 22117.00 SCOOP • c.bIn elr 1 ·34 23827·31 C FUSELAQE FORWARD seCTION ASSEMBLY 1 ·35 17311-00 F PLATE -Aconahole COVIr 1 ,38 25880-00 B PLATE ASSEMBLY· ",...bottom ClMr 1 ·37 27280000 Z BRACKET· OM! SUPPOrt 1 3I·l41Mdup A - Ihed on PA-30 with ..... numl)wa 3Q.tI3. 3Ot02 Md lIP. Md PA-39 with _I .. numt.n 31·1 Iftd up. B· u.ct on PA-30 with ..... numt.n 30-1717. 30-17415 Ind UP.Md PA-39 with ""II numbers 3I·llnd up. C • S. FlguN 7 for compon..,t Plru. D • S. FIguN 10 for c:ompo~t Pin,. E. S. FlguN llA for OOInpC)Mnt Pin,. F ,UaId on PA-3Q With_lei numt.n 30-1553 to 3().1716Indualw. 30-1718 to 3O-1744lnclualw. G • Ulld on PA·30 with .11 numbwa30-813. 30802 to 3G-1718Indualw. 30-1718 to 3().1744lndualw. H ... Figure 11B for component I*U. J. Ulid on PA~ with ......1numblrl :J)-1717. 30-17415 Ind UP.and PA-39 with ".1 numbln 31·1 to 3M3 Indualw. Y • UaId on PA-30 ..rpI .... only. Z • UaId on PA" "rpl..,. only. • • • PA-30 PA·39 SECTION II FUMf.... Group 1 817 Whenordlrlng. liway, 'PlCify Part Nu~. Dlacrlpdon .nd serial Numblr of Alrcnft REVISED: FEBRUARY 1977 .~;·JC~j~;i;;i;:~·:t::·:~··" .,yt~·~ J =~~~~ eLAG! " • • 1 818 INTENTIONALLY LEFT BLANK REVISED MAY 1980 PIPER PARTS CATALOG ncr (;J 12)-1 Figure 9. Fuselage Top Section (PA-30 with Senal Nos. 30-2 to 30-852. 30-854 to 30·901 inclusivel 1819 3' PA-30 • • • Figure Z and Port (j !J SERIAL NUMBERS Index 8. NOMENCLATURE ;:0 AFFECTED Number IV 10 Number .0 9- 22566 DRAWING - Fuselage Cabin Top -I 225M-00 SECTION ASSEMBLY - Fuselage cabin top I -2 21922-00 BOX ASSEMBLY - Ventilator. right rear I 21922·01 BOX ASSEMBLY - Ventilator. left rear I -J 20457-00 BRACKET - Wire clamp I -4 2a<,~9·00 PLATE - Wire attachment I -5 20000-24 STRINGER I -b 20600-38 CHANNEL - Right I -7 20600-89 CHANNEL - Left I -8 20600-135 CHANNEL ASSEMBLY - Right I -9 20600-136 CHANNEL ASSEMBLY, Left 1 -10 21747-03 BRACKET - Trim strip support. rear 1 21747-04 BRACKET - Trim strip support, front I -11 20507-00 CHANNEL· Fuselage center section top. rear. LH I 20507 -01 CHANNEL - Fuselage Center section top. rear. RH I -12 23284-00 GUSSET ASSEMBLY - Fuselage center section. RH I -13 23285-00 GUSSET ASSEMBLY· Fuselage c-enter section. LH 1 -14 21928-00 CONNECTOR TUBE ASSEMIl1...¥ - Right I -15 20561-03 CHANNEL - Top front 1 -16 61402-39 BUSHING 2 -17 20610-04 GUSSET I -18 20610-05 GUSSET I -19 20610-13 CHANNEL ASSEMBLY - Windshield I 30-2 to 30-611 mciusive 20610-03 CHANNEL - Windshield I 30-012 and up -20 20554-29 CHANNEL ASSEMBLY - Fuselage. Sta. 136 1 30-2 to 30-611 i nc lu s iv c -21 20900-00 BULKHEAD - Fuselage. Sta. 86 I -22 21748-00 PULLEY BRACKET ASSEMBLY I -23 21560-00 GUSSET ASSEMBLY - Coat hanger support, LH I 21560-01 GUSSET ASSEMBLY - Coat hanger support, RH I -24 20603-11 GUSSET - LH I -25 23283-00 BULKHEAD ASSEMBLY- Fuselage, Sta , 107. LH 1 23283-01 BULKHEAD ASSEMBLY - Fuselage, Sta. 107. RH I -26 22565-03 BULKHEAD ASSEMBLY - Fuselage, Sta. 121 1 -27 20902-00 BULKHEAD 1 -28 20904-00 CHANNEL ASSEMBLY I -29 20906-00 SUPPORT BRACKET - Left 1 20906-01 SUPPORT BRACKET· Right 1 -30 20603-10 BULKHEAD - Fuselage, Sta. 70 to Sta. 80, LH I 20603 -15 BULKHEAD - Fuselage. Sta. 70 to Sta. 80. RH I 30 -2 to 30 -611 mclus ive 20603-21 BULKHEAD - Fuselage, Sta. 70 to Sta. 80. RH I 30-612 and Up -31 20603 -Ib BULKHEAD· Fuselage. Sta. 70 to Sta. 80, top I 30-2 to 30-61l Inclusive 20603-09 BULKHEAD - Fuselage, Sta. 70 to Sta. 80. top 1 30-612 and up -32 21929-00 CONNECTOR TUBE ASSEMBLY - Left I -3.3 22675-02 BULKHEAD ASSEMBLY - Fuselage. Sta. 105 I 30-2 to 30-61l inclusive 23675-09 BULKHEAD ASSEMBLY - Fuselage, Sta. 105 1 .30-612 and up -34 22582-04 CHANNEL - Fuselage, Sta , lOS, RH 1 30-2 to 30-61l inclusive 23675·11 CHANNEL - Fuselage. Sta. 105, RH I 30-612 and up 20539-24 CHANNEL - Fuselage, Sta. 105. LH I 30 -2 to 30 -611 inc lu s iv e 23675-10 CHANNEL - Fuselage, Sta, 105, LH I 30-b 12 and up -35 21930-00 CONNECTOR TUBE ASSEMBLY - Ventilator, LH 1 30-2 to 30-611 mclusive -36 20539-07 CHANNEL· Fuselage, Sta. 105, top I A - Used on PA-30 with serial numbers 30-2 to 30-852 lnc lustve, 30-854 to 30-901 Inclustve , • • • SECTION II Fuselage Group When ordering, always specify Part Number. Description and Serial Number of Aircraft FUSELAGE TOP SECTION (See Code "A") ISSUED: FEBRUARY 1973 1820 Figure ~ ond Port .~ SERIAL NUMBERS Index Number NOMENCLATURE f AFFECTED Number 9-37 22582-07 ANGLE ASSEMBLY - FUlielage St•• lOS. RH I -38 24177-00 ANGLE ASSEMBLY - Stabllator trim cable .1I.l"ment 1 -39 20610-02 CHANNEL • Windshield I -fa 20617·07 ANGLE ASSEMBLY - Fuselage St•• 100 to St•• 105. top. riJbt I -41 20611-06 ANGLE ASSEMBLY - Fuselage St•• 80 to St•• 84, top, rtsht I . A - Used Oft PA-30 with serial,numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 Inclusive. , FUSELAGE TOP SECTION (See Code "A") When ordering, olways specify Part Number, Description and Serial Number of Aircraft SECTION II Fusehlge Group • • ISSUED: FEBRUARY 1973 1821 PA-30 • • PIPER AIRCRAFT 10 CORPORATION CD 14 -_ 39 1&~~-t·:::-"" U-I~41 40 rr: • rssuso. FEBRUARY 1973 Figure 9A. Fuselage Top Section (PA-30 with Serial Nos. 30-853, 30-902 and up) (PA-39 with Serial Nos. 39-1 and up) 1822 PA-30 PA·39 • • • FUSELAGE TOP SECTION /See Code "A") When ordering. always specify Part Number. Description and Serial Number of Aircraft F"ure PIPER PARTS CATALOG and Part No. SERIAL NUMBERS Ind •• Number Code NOMENCLATURE Req. AFFECTED Number A· 25355 DRAWING - FUHla,e Cabin Top -1 25355-00 Y SeenON ASSEMBLY - FUHlage cabin top 1 30·853. 30·902 to 30·1548 25355·08 YZ SEenON ASSEMBLY· Fu..la,. cabin top 1 30·1549 and up. 39·1 and up -2 20800·38 • CHANNEL· FUHlage. Sle. 80 to Sle. 105. top. right 1 -3 20600-24 • STRINGER· FUHlage. Sta. 80 to Sta. 105. top. left 1 -4 20600-34 Y • CHANNELASSEMBLY - FUHlag•• Sta. 78 to Sta. 106. top. left 1 30·853. 30-902 to 30·1548 25842-00 YZ • CHANNEL ASSEMBLY· Fu..lag•• Sta. 78 to Sle. 105. top.l.ft 1 30·1549 and up. 39-1 and up -5 20600·135 • CHANNELASSEMBLY· Fu..lao•• Sta. 80 10Sle. 105. toP. right 1 20600·138 • CHANNEL ASSEMBLY· Fuselage. Sta. 80 to Sta. 106. top. left 1 -6 23283-00 • BULKHEADASSEMBLY· Sta. 107. I.ft 1 23283-01 • 8ULKHEAD ASSEMBLY· Sta. 107. right 1 -7 20457-00 • BRACKET· Wlr. clamp 1 30·853 and up. 39·1 to 39-145 -8 25334-00 Y • CHANNEL· Fu..lage cent.r uetlon. top. r.ar. left 1 30·853. 30·902 to 30·1548 25334·01 Y • CHANNEL· FUHI.g. cent.r section. top. rear. right 1 30·863. 30·902 to 30·1 548 25832-00 VI • CHANNEL - Fu....oe center HC1ion. top. rear. I.ft 1 30·1549 and up. 39-1 and up 25832-01 YZ • CHANNEL - Fu..l.center MC110n. top. raar. right 1 30·1549 and up. 39-1 and up ·9 23284·00 • GUSSET ASSEMBLY· Fuselage top. right , 23285·00 • GUSSET ASSEMBLY· Fuselage toP. left , -10 23875-09 • CHANNELASSEMBLY· Fuulao•• Sta. '05 , ·11 20639·07 ... CHANNEL• Fuselao•• Sle. '06. top , -12 23675-'0 • .. CHANNEL· Fu....g•• Sta. '05. left , 23875-11 • .. CHANNEL· Funtaga. Stl. '05. right 1 ·13 25308·07 .. CHANNELASSeMBLY· FUHI8g•• Sta. '38. top 1 ·14 2056'-03 • CHANNELASSEMBLY· Fu..lag•• Sta. 70 to St•. 78. top , -15 20603-11 .. GUSSET , -16 20803-22 .. BULKHEADASSEMBLY· Fu..lao•• Sta. 70 to Sta. 80 1 -17 20977-03 ... BULKHEAD ASSEMBLY· FUHlag•• Sta. BOto Sta. B3. top 1 -tB 206'0-03· • CHANNEL - Fu..laga. Sta. 70 to Sta. 80. center , -'9 20610·04 .. GUSSET • FUHlaoe. Sta. 70. top. canter , -20 206'0·05 • GUSSET • Fu..I.ge. Sta. 80. top. c.nter , ·21 20977-06 .. BULKHEAD ASSEMBLY· Fuselage. Sta. B3. top , -22 2'560·02 • GUSSET ASSEMBLY· Fu..lage. Sta. 136. top. left 1 21560·03 • GUSSET ASSEMBLY· Fu..I•• Sta. , 36. top. right , -23 2'307-00 • BRACKET ASSEMBLY - Ant.nna mounting , -24 25344·00 • CHANNEL· Head guard 2 -25 25306-04 • CHANNEL - Window. Sta. 136. left , 25306-05 • CHANNEL· Window. Sta. , 36. right 1 -26 25323-02 • BULKHEAD • Sta. , 28 to Sta. , 33. left 1 25323-03 • BULKHEAD· Sta. 12B to Sle. , 33. right 1 -27 253'4-03 • CHANNELASSEMBLY· FUHlage. Sta. 12' , A • Used on PA·30 with Hrial numbars 30·B53. 30-902 and up. and PA·39 with sari.I numbers 39·' and up. Y • Used on PA·30 airplane. onlv. Z • Used on PA-39 airplane. onlV. SECTION II Fusela,e Group 9 REVISED: MAY 19BO 1823 PA·30 PA·39 Figure and Put Code NOMENCLATURE No. SERIAL NUMBERS Index Number Req. AFFECTED Number 9A·28 25843-02 CHANNEL· FUMI. IUppQrt, lett 1 25843.Q3 CHANNEL - Fu.11gI IUpport. rlWit 1 -29 25341.Q4 CHANNEL· FUMIllIIlUPPQrt, 11ft 1 25341-05 CHANNEL· FUIII. IUPPQrt. rlltJt 1 ·30 27002-00 Z BRACKET ASSEMBLY· Shouldlr hlrn.... 11ftfront 1 27002-01 Z BRACKET ASSEMBLY· Shouldlr heml... rl~t tront 1 -31 27003-00 Z BULKHEADASSEMBLY. FUMI"" Stt. 113. 11ft 1 27003-01 Z BULKHEADASSEMBLY· FlJIIl",. Stt. 113. rl~t 1 ·32 27001-00 Z BRACKET ASSEMBLY· Shouldlr herOlll. (lIntlr 2 ·33 27005-00 Z BULKHEAD· Clntlr Ihouldlr h.-n_.llft reer. rl"t tront 2 27006-01 Z BULKHEAD· Clntlr Ihouldlr h.-n.... 11ftfront, rlltJt relr 2 -34 241n-o:z ANGLE ASSEMBLY· Stlbliitor trIm Clblllllgnmtnt 1 -36 20817-08 ANGLE ASSEMBLY· Fueel"". Stl. 80 to Stl. 84. top. rlWit 1 ·38 20600-96 ANGLE ASSEMBLY· Fu.I••St•. 1(1). toP. rlWit 1 -37 25366-07 STRINGER· FUllIIgI. Ste. 138 to StI. 157. top 3 ·38 25355-04 STRINGER· FUll''''. Ste. 106 to StI. 136, top 3 -39 25821-00 CHANNEL ASSEM8LY • Ste. 66 to St•. 106. 11ft 1 -40 22421-00 CHANNEL ASSEMBLY· Arrnrllt IUpPQn 2 -41 20600-125 CHANNEL· FlJIII••Ste. 70 to Ste. 105. LH 1 -42 25321-00 CHANNEL - R.. ~ndow 1 25321'{)1 CHANNEL· R.. window 1 -43 25332·00 CHANNEL - Clntw window. left 1 30-853,30-902 to 30-15"8 25332-01 CHANNEL· Clnter window, ri~ 1 JO.e3, 30-902 to 30.1548 26099-00 CHANNEL· Clnter window. left 1 3O-1549.nd up 25829-01 CHANNEL· Center window. right 1 30-1549 and up -44 20803-OB STRIP - Fu"llII. Ste. 70 to St•. 78. top, lett 1 20603-08 STAIP • Fu..... StI. 70 to Ste. 78. tOP. right 1 -45 20603-12 ANGLE ASSEMBLY· Fu.lllII. St •. 70 to St•. 78. top. rllttt 1 -46 23288-00 STRIP - Moulding rltelnlr 2 -47 2061l).(12 CHANNEL - FUIII., Stl. 63 to Ste. 70. top. Qlntlr 1 -48 20617'{)7 ANGLE ASSEMBLY· Fu.IIlII, 5te. 100 to Sla. 106, top. rllttt 1 A • Used on PA-30 with ..,.Ial number. 30'-3, 30-902 end UP. end PA-39 with _lei number. 39·1 Ind up. Y • Used on PA-30 alrpl,nn only. Z - Used on PA-39 Ilrplan .. only. • • FUSELAGE TOP SECTION (See Com "A") Whln ordering, alway••pecify Plrt Number. Dncrlption end Siriel Number of Aircreft SECTION II Fusil. Group REVISED: FEBRUARY 1977 1 824 PA-30 PA-39 1 Cl INTENTIONALLY LEFT BLANK • • • .- • • PIPER PARTS CATALOG Figure 10. Fuselage Front Frame Assembly REVISED: MAY 1980 1C2 PA-30 PA39 Figure Z and Port ~ p SERIAL NUMBERS Index Number NOMENCLATURE ::a AFFECTED Number $ 10- 23703 DRAWING - Frame Assembly, Fuselage, Front -1 23703-00 B FRAME ASSEMBLY - Fuselage, front I 23703-03 A FRAME ASSEMBLY - Fuselage, front I -2 23675-13 BULKHEAD ASSEMBLY - Fuselage. Sta. lOS. LH 1 -3 23675-04 BULKHEAD ASSEMBLY - Fuselage. Sta. lOS. RH 1 -4 23675-05 B BULKHEAD ASSEMBLY - Fuselage. Sta. 105. bottom I 25977-03 A BULKHEAD ASSEMBLY· Fuselage, Sta. lOS, bottom I -5 23656-02 BULKHEAD ASSEMBLY - Sl:a. 87, LH I 23656-03 BULKHEAD ASSEMBLY - Sta. 87. RH I -6 23691-06 BULKHEAD ASSEMBLY - Sta. 66, LH I 23691-OS BULKHEAD ASSEMBLY - Sta. 66, RH I ·7 23660-06 BULKHEAD ASSEMBLY - Fuselage. St•• 96. LH I 23660-07 BULKHEAD ASSEMBLY - Fuselage. Sta. 96. RH 1 -8 20570-08 BULKHEAD ASSEMBLY - Fusel.... Sta. 77. bottom. left 1 20570-07 BULKHEAD ASSEMBLY - Fuselage. Sta. 77. bottom, rlghl: I -9 23617-00 BULKHEAD ASSEMBLY - Fuselage, Sta. 68 1 -10 23617-02 BULKHEAD ASSEMBLY - Fuselage, St •• 59 1 ·11 23645-00 BULKHEAD ASSEMBLY· Fuselage. Sta. 92 1 -12 23626-00 B BEAM ASSEMBLY· Longitudinal fuselage. St•• 49 to Sta. 105. LH 1 26355-00 A BEAM ASSEMBLY - Longitudinal fuselage. Sta. 49 to Sta. lOS. LH 1 2.1626-01 B BEAM ASSEMBLY - Longitudinal fuselage. Sta. 49 to Sta. 105. RH 1 26355-01 A BEAM ASSEMBLY - Longitudinal fusel•• Sl:a. 49 to St•• lOS. RH 1 -13 20557-06 ANGLE - Beam. upper. LH I 20557-07 ANGLE - Beam, upper. RH 1 -14 20557·08 ANGLE - Beam, bottom, LH I 20557-09 ANGLE - Beam, bottom. RH 1 -15 226.31·02 CHANNEL ASSEMBLY· Fuselage, Sta. 87 1 -15a 21760-00 LUG - Transmission attachment 1 -ISb 20954-00 CHANNEL ASSEMBLY - Gear motor support 1 -15c 25876-00 FITTING ASSEMBLY - Front seat belt attachment, left 1 25K76-01 FITTING ASSEMBLY - Front seat belt attachment. right I -16 22629-02 CHANNEL - Fuselage front 2 -17 20000-62 CHANNEL - Fuselage front, LH 1 20600-63 CHANNEL - Fuselage front. RH 1 -Ill 22272 -10 STRINGER ASSEMBLY - Fuselage, Sta. 49 to Sta. 66. LH 1 22272·09 STRINGER ASSEMBLY· Fuselage. Sta. 49 to Sta. 66. RH 1 A - Used on PA-30 with serial numbers 30-1717. 30-1745 and up, and PA-39 with serial numbers 39-1 and up. B - Used on PA-3O with serial numbers 30-2 to 30-1716 inclusive, 30-1718 to 30-1744 inclusive. FUSELAGE FRONT FRAME ASSEMBLY I -- SECTION II FUlj~lage Grnup • • • When ordering. always specify Port Number. Description and Serial Number of Aircraft ISSUED: FEBRUARY 1973 le3 PA-30 PA·39 SECTION II Fuseillge Group FUSELAGE FRONT FRAME ASSEMBLY • Figure PIPER PARTS CATALOG end Pan No. SERIAL NUMBERS Inde. Number Code NOMENCLATURE Req. AFFECTED Number 10-19 23690-04 • STRINGER ASSEMBLY - Fuselage, Sta. 87 to Sta. 105, LH 1 23690-05 • STRINGER ASSEMBLY· Fuselage, Sta. 87 to Sta. 105, RH 1 -20 23743-04 • STRINGER ASSEMBLY - Fuselage. Sta. 66 to Sta. 87. LH 1 23743-05 • STRINGER ASSEMBLY - Fuselage. sra. 66 to Sta. 87. RH 1 -21 23839-04 • ANGLE ASSEMBLY- Floorboard support, LH 1 23839-02 • ANGLE - Floorboerd support. RH 1 -22 22232-03 A CHANNEL - Fuselage. Sta. 49 to Sta. 130, left 1 25383-12 B CHANNEL - Fuselage, Sta. 49 to Sta. 130, left 1 20600·21 A CHANNEL· Fuselage, Sta. 49 to Sta. 130. right 1 25383-13 B CHANNEL - Fuselage, Sta. 49 to Sta. 130, right 1 -23 20443-00 C BRACKET ASSEMBLY - Rudder pedal torque tube bearing, left 1 20443-01 C BRACKET ASSEMBLY - Rudder pedal torque tube bearing. right 1 27111-00 Z BRACKET ASSEMBLY - Rudder pedal torque tube bearing, left 1 39-84 and up 27111-01 Z BRACKET ASSEMBLY· Rudder pedal torque tube bearing, right 1 39-84 and up -24 26860-00 CHANNEL - Fuselage side. Sta. 66 to Sta. 70. left , 1 26880-01 CHANNEL - Fuselage side. Sta. 66 to Sta. 70. right 1 -25 20600-50 CHANNEL - Fuselage. Sta. 49 to Sta. 66, left 1 20600-51 CHANNEL· Fuselage, Sta. 49 to Sta. 66. right 1 -26 23820-08 CHANNEL - Sta. 78, left 1 23820-09 CHANNEL - Sta. 78, right 1 -27 23820·10 CHANNEL - Sta. 61, left 1 23820·11 CHANNEL· Sta. 61, right 1 -28 23820-12 CHANNEL - Sta, 54. left 1 23820·13 CHANNEL - Sta. 54, right 1 -29 20601-05 GUSSET - Fuselage, Stlil. 87 lIInd St a, 96 3 -30 23660·04 CHANNEL - Fuselage, St •. 96 1 -31 23680·05 BULKHEAD - Fuselage, Sta. 96 1 -32 22572-10 BULKHEAD ASSEMBLY - Fuselage, Sta. 70. left, forward 1 22572-11 8ULKHEAD ASSEMBLY· Fuselage. Sta. 70, right, forward 1 ·32a 22572-12 BULKHEAD ASSEMBLY- Fuselage, Sta, 70, left, aft 1 22572-13 BULKHEAD ASSEMBLY- Fuselage, Sta. 70. right. aft 1 -33 23602-00 BULKHEAD ASSEMBLY 1 -34 21155-03 PLATE ASSEMBLY· Landing gear retraction 1 -35 21953-00 8RACKET ASSEM8LY - Seat track SUPPO", left 1 21953-01 8RACKET ASSEMBLY - Seat track SUPPO", right 1 -36 22257-00 PLATE ASSEMBLY - Fuel strainer access reinforcement 1 -37 23603-00 Y ANGLE ASSEMBLY - Circuit protector panel 1 30-2 to 30-1254 inclusive 23603-04 YZ ANGLE ASSEMBLY- Circuit protector panel 1 30-1255 and up. 39-1 and up A - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. B - Used on PA-30 with serial numbers 30-853, 30-902 and up, and PA-39 with serial numbers 39-1 and up. C - Used on PA-30 with serial numbers 30-2 and up, and PA-39 with serial numbers 39-1 to 39-83 inclusive. Y . Used on PA·30 airplanes only. Z - Used on PA-39 airplanes only. When ordering, always specify Part Number. Description and Serial Number of Aircraft REVISED: MAY 1980 1C4 PA·30 PA·39 Figure Iftd PI" Code NOMENCLATURE No. SERIAL NUMBERS Index Num.... ~eq AFFECTED Number 1~3B 23815-00 FITTING ASSEMBLY ·Llncln' .... mount Iowvtr ItUClwMnt.11ft 1 23815-01 FITTING ASSEMBLY. Lancln' .... mount Ioww en.chm..t. rfght 1 ·39 23818-00 GUSSET. FUll!. 1 2381&01 GUSSET· FuM!", 1 -eo 23833.00 GU$SET.F~ 2 -41 23818-00 FITTING ASSEMBLY .....dIng..mount uppM' nt.chrn..t. left 1 23811-01 FITTING ASSEMBLY ·l.MIclng..'"9U"t uppM' lttIChm..t. rfght 1 -42 23843-00 GUSSET - F......... ate. 101.'" left > 1 23643-01 GUSSIT - F....... a•. 101."', rtght 1 -43 211514-00 D BRACKET AIIIMILY - Utdng ..... _fetylOok 1 ..... 238t7.oe COVIR ASSEMBLY· Ne. whIII 1 -415 23817002 COVER • Left 1 23887-03 COVER-RWlt 1 -41 23B97.Q4 PLATI - He. wheII OCIVW 1 -47 2433&00 BRACKET MSEMILY· , ..I11 ........t 2 -48 23972-00 BRACKET ASSEMBLY - landing ller I'Itr1Ct1on InIr 2 -49 23828-00 FAIRING- Control abl' 2 -150 20813-03 GUSSET PLATE- ate. 88. lett 1 20813-04 GUSseT 'LATE· SU. 88. right 1 -151 22e07-18 CHANNEL - Pu.I.... StL 88 to ItL 17. left 1 22e07·22 CHANNEL - F...... Su. 88to ItL 17, rIFt 1 -152 2!587S.(JQ C IRACKET • Pitch -no mounting 1 26822.(IQ B BRACKET·Pitch .rvo mountl", 1 ·153 23BQ5.OO B ANGLE - Shunt and fuM panel 1 -l54 20812.Q4 A CHANNEL - F~"" upper. Su. 88. left 1 .'3-02 B CHANNEL ASSEMBLY· FutII... upper. SU. 88. left 1 20812-0& CHANNEL· Fu.11II upper. ItL 88. r!WIt 1 ·615 20804-12 A CHANNIL ASSEMBLY. Fu.I", upper. SU. 70,1,tt 1 2fJ6OI.03 B CHANNEL ASSEMBLY - Pu.l.....Ik8. 70. left 1 20804-10 CHANNEL ASSEMBLY - Fu.11II uppM'. SU. 70. rfght (with hl"l\l brKk"') 1 -l56 26E17S-OO B BRACKET·G__chm..t 2 -157 25162-00 ANGLE AISIMBLY • Left 1 :ZS162.Q1 ANGLE ASSEMBLY - R!WIt 1 -l58 20800-" ANGLE AISIMILY ·RI~t.ltI. 70.87& to ate. 101.375 1 A· UMd on PA-30wlth .,111 numblrs30-2 to 3~171"8 induslw. 3~1718 to »1744lnduslve. B· UIlId on PA-30with IIrIII nurnbln 30-1717. 30-1745 Ind UP. end PA-39with .11 numbers .,and up. C • Ulld on PA-30with tarlal numbln »12515 to 3~1718IndusIWl. 30-1718 to :JO.1744lnclusIWl. D· Usedon PA-30with .... numbers »1717. 30-1745 Ind lIP.end PA-39with serfal numbers 39-1 and up. Also ulld on PA·3O with ""al numbln 30-2 to »1718. 3M71a to 3Q.1744 Incl. If LanclngG_ Emartancy extension 5acurIty Installation KIt 780 827 g bien Instilled par SaMcI SperII Latter SP·325. • • •PA-30 PA·39 SECTION" F...... Grovp -- 1C5 When ordering. IIWllYs specify Part Nuneer. Description and8erIa1 Numberof Alrcreft REVISED: FEBRUARY 1977 FUSELAGE FRONT FRAME ASSEMBLY • • -- • 1C6 INTENTIONALLY LEFT BLANK PIPEIT AIRCRAFT COR 'OR A T ION • 2t 4' ~ ~ ~,'~~I 24 ~ 22-..../7 "~ ~" Figura 11. F.-I." R•• Frlme Asllmbly (PA·30 with serial Nos.3()'2 to 30-882, 30-864 to 30-901 inclusivel •ISSUED: FEBRUARY 1973 lC7 PA·30 Figure Z and Port n 9 SERIAL NUMBERS Index 8. NOMENCLATURE ]:J AFFECTED Number ell ell Number .p 11- 22620 DRAWING ~ Frame Assembly, Fuselage, Rear -1 22620-00 FRAME ASSEMBLY - Fuselage, rear 1 30-2 to 30-589 inclusive 22620-21 B FRAME ASSEMBLY ~ Fuselage, rear 1 -2 20455-00 BU LKHEAD - Fuselage bottom, Sta. lOS to Sta, 113, left 1 20455~OI BULKHEAD - Fuselage bottom, se. 105 to Sta. 113, right 1 -3 22562-00 BULKHEAD ASSEMBLY - Fuselage bottom, Sta, 136 to Sta. 157, left 1 22562·01 BULKHEAD ASSEMBLY - Fuselage bottom, Sta. 136 to sta, 157, right 1 -4 20477-00 BRACKET· Pulley, Sta. 113, center, left 1 -5 20515-00 BRACKET - Pulley, Sta. 113, outboard, left 1 20516·00 BRACKET - Pulley, Sta. 113, inboard, left 1 -0 20546-04 BULKHEAD ASSEMBLY - Fuselage bottom, sea. 113 to Sta, 136, left 1 20546-05 BULKHEAD ASSEMBLY - Fuselage bottom, Sta, 113 to Sta. 136, right 1 -7 226l)6-OS BULKHEAD ASSEMBLY - Fuselage, Sta. 136 1 ~8 20554-02 CHANNEL - Fuselage. Sta, 136. left 1 22606-03 CHANNEL - Fuselage. Sta, 136. right 1 -9 20554·05 CHANNEL - Reinforcement 1 -10 20442-02 BRACKET - Pulley, Sta. 136, rear, left 1 -11 20442-03 BRACKET· Pulley. Sta. 136, rear, left 1 -12 20497~00 BRACKET - Pulley. Sta. 136, rear, left 1 -13 20498-00 BRACKET - Pulley, Sta, 136, rear, left 1 -14 20504-02 BRACKET - Pulley, se. 136. front, left 1 20504-03 BRACKET - Pulley, Sta, 136, front, right 1 -15 20504-04 BRACKET - Pulley. Sta. 136, front 2 -16 20505-02 BRACKET - Pulley. Sta. 136, front, left 1 -17 20505·03 BRACKET - Pulley, Sta, 136, front, left 1 -18 20554~12 CHANNEL - Splice 1 -19 20554-16 ANGLE - Left 1 20554-17 ANGLE - Right 1 -20 23662-00 PLATE 2 -21 23663·00 FITTING ASS£MBLY 2 -22 80022-97 BUSHING - Rear spar attachment 1 -23 23665-02 DOUBLER ~ Fuselage, Sta, 136, left 1 23664-02 DOUBLER - Fuselage, Sta. 136, right 1 -24 22620-06 STRINGER - Fuselage bottom, Sta, 136 to Sta. 157. left 1 20600-75 STRINGER ~ Fuselage bottom, Sta. 136 to Sta, 157, right 1 A - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. B - Used on PA-30 with serial numbers 30-590 to 30-852 inclusive, 30-854 to 30-901 inclusive. • • .--.. • FUSELAGE REAR FRAME ASSEMBLY (See Code "A") -lam~. SECTIO:-; 11 Fuselage Group When ordering, always specify Part Number, Description ond Serial Number of Aircraft ISSUED: FEBRUARY 1973 1 C8 Figure Z ond Port ~ 9 SERIAL NUMBERS Index NOMENCLATURE :tl AFFECTED Number .pNumber 11-25 22620-10 STRINGER - Fuselage bottom, Sta. 113 to Sta. 136, left 1 22620-11 STRINGER - Fuselage bottom, Sta. 113 to Sta. 136, right 1 -26 20600-56 STRINGER CHANNEL - Fuselage bottom, Sta. lOS to Sra. 113 .. -27 206lJO.S8 STRINGER CHANNEL - Fuselage bottom, Sta. 113 to Sta. 136. left 1 20600-59 STRI1I«jER CHANNEL - Fuselage bottom, Sta. 113 to Sta. 136, right 1 -28 20600-101 STRIOOER ASSEMBLY - Fuselage. Sta. 124 1 -29 206lJ0.132 STRINGER ASSEMBLY - Fuselage, Sta. 136 to Sta. 157, left 1 20600-131 STRINGER ASSEMBLY - Fuselage, Sta. 136 to Sta. 157, right 1 -30 22620.04 STRINGER - Fuselap side, Sta. 11310 $ta. 136, left 1 30-2 to 30-589 inclusive 22620-23 B STRINGER - Fuselage side, Sta. 113 to Sta. 136, left 1 22620-05 STRIIICER - Fuselage side, Sta. 11310 Sta. 136, right 1 30-2 to 30-589 inclusive 22620.24 B STRINGER - Fuselage side, Sta. 11310 Sta. 136, right 1 -31 20496-00 BRACKET ASSEMBLY - Rear seat support 1 -32 22620-14 STRlOOBR ASSEMBLY - Fuselage, Sta. 13210 Sta. 136, left 1 22620-15 STRINGER ASSEMBLY - Fuselage, Sra. 132 to Sta. 136, right 1 ·33 22604-00 CHANNEL - J:uselage, Sta. 132 to Sta. 136, right bottom 1 22604-01 CHANNEL - Fuselage, Sra. 132 to Sta. 136, right top, left top and bottom 3 -34 22620-08 STRINGER - Fuselage bottom, Sta, 136 to Sta. 157, left 1 22620-09 STRINGER - Fuselage bottom, Sta. 136 to Sta. 157, right 1 -35 20554-23 STRJP ASSEMBLY - ~lkhead, Sta. 136 1 -36 22618-04 BULKHEAD ASSEMBLY - Fuselage, Sta. 113 1 -37 22618-02 CHANNEL - Left 1 22618-03 CHANNEL - Right 1 ·38 22618-OS PLATE - Splice 1 -39 20616-04 DOOBLER - Left 1 20616-OS DOUBLER - Right 1 -40 22600-02 BULKHEAD - Fuselage, Sra. 132, left 1 22600-03 BULKHEAD - Fuselage, Sra. 132, right 1 -41 22581-00 GUSSET - Fuselage, Sta. 132 2 -42 22232-03 CHANNEL • Fuselage, 5ta. 49 to Sta. 130. left 1 20600-21 CHANNEL - Fuselage. Sta. 49 to $ta. 130, right 1 -43 20445-00 BULKHEAD - seat support, Sta. 123 1 -44 206lJO.22 CHANNEL - F~lage, Sta. 136 10 Sta. 157, left 1 20600-23 CHANNEL - Fuselage, Sta. 136 to Sta. 157, risht 1 A • Used on PA-30 with serial numbers 30·2 to 30-852 inclusive. 30-854 to 30-901 inclusive. B - Used on PA-30 with serial numbers 30-590 to 30-852 inclusive, 30-854 to 3Q-9011nclusive. - SECTION II Fuselage Group FUSELAGE REAR FRAME ASSEMBLY (see COde "A") ~ ord.rirtg. olways spec::lfy Port Number, Daerlptlon and Serlol Number of A.ln::roft • • •ISSUED: FEBRUARY 1973 1C9 PA-30 Figure Z and Port (i 0 SERIAL NUMBERS Index 8. NOMENCLATURE ;;lJ AFFECTED Number III III Number .p 11-45 20646-00 ANGLE - Fuselage channel attachment, sra. 157 1 -46 21328-02 BRACKET· Radio cable clamp 2 21328-03 BRACKET - Radio cable clamp I -47 20616-06 GUSSET - Bulkhead, Sta, 113, left 1 20616-07 GUSSET - Bulkhead, Sta, 113, right 1 -48 20411-00 FITTING - Main spar top attachment, left 1 20411-01 FITTING - Main spar top attachment, right 1 -49 30304-00 BRACKET ASSEMBLY - Antenna mounting 1 -50 22586-00 GUSSET - Fuselage wlkhead 2 A - Used on PA-30 with serial numbers 30-2 to 30-852 inclusive, 30-854 to 30-901 inclusive. • • ,--, • FUSELAGE REAR FRAME ASSEMBLY (See Code "A") When ordering, olwoys $pe<:ify Port Number, DeKription and Serial Number of Aircraft SECTION 11 Fuselage Group ISSUED: FEBRUARY 1973 1 Cl0 PA-3D PIPER AIRCRAFT COl P 0 RAT ION • Filld 11A. F'*'-l!I R.., F,In'Ie ~b1y (PA-30with sertll Not. 3008&3, 30-9028nd up) (PA-39with kill NOI. 38-1 -"d up) • •ISSUED: FEBRUARY 1973 1ell PA-3Q PA·39 Figure Z and Part n 5' SERIAL NUMBERS Index Number a NOMENCLATURE ;lJ AFFECTED .." .,. Number ~ IIA- 25333 DRAWING - Frame Assembly, Fuselage, Rear -I 25333-00 C FRAME ASSEMBLY - Fuselage, rear I 25333 -17 0 FRAME ASSEMBLY.- Fuselage, rear I -2 20455-00 BULKHEAD - Fuselage bottom. Sta. 105 to Sta , 113. left I 20455 -01 BULKHEAD - Fuselage bottom. Sta. 105 to Sta. 113. right I -3 22562-00 BULKHEAD ASSEMBLY - Fuselage bottom, Sta. 1.']6 to Sta. 157, left I 22562 -01 BULKHEAD ASSEMBLY - Fuselage bottom. Sta. 136 to Sta. 157. right I -4 20477-00 BRACKET - Pulley, Sta. 113, center, left I -5 20515-00 BRACKET - Pulley, Sta. 113, outboard, left I 20516-00 BRACKET - Pulley, Sta. 113, inboard. left I -/j 25286-00 C BULKHEAD ASSEMBLY - Fuselage bottom. Sta. 113 to Sta. 136. left I 26614-00 0 BULKHEAD ASSEMBLY - Fuselage bottom, Sta. 113 to Sta. 136, left I 25286-01 BULKHEAD ASSEMBLY - Fuselage bottom. Sta. 113 to Sta. 136. right I -7 25320-04 Y BULKHEAD ASSEMBLY - Fuselage, Sta. 136, lower I 30-853, 30-902 to 30-1254 25320-08 B BULKHEAD ASSEMBLY- Fuselage, Sa. 136. lower I 25320-09 0 BULKHEAD ASSEMBLY - Fuselage. Sta. 136, lower I -8 25320-02 Y CHANNEL - Fuselage. Sta. 136. left I 30-853. 30-902 to 30-1254 25320-10 YZ CHANNEL - Fuselage, Sta. 136. left I 30-1255 and up, 39-1 and up 25320-03 CHANNEL - Fuselage, Sa. 136, right I -9 25320-06 CHANNE L - Reinforcement I -10 20442-02 BRACKET - Pulley, Sta . 136, rear, left 1 -II 20442-03 BRACKET - Pulley, Sta. 136. rear. left I -12 20497-00 BRACKET - Pulley, Sta. 136. rear. left I -13 20498-00 BRACKET - Pulley, Sta. 136. rear, left I -14 20504-02 BRACKET - Pulley, Sta. 136, front. left I 20504-03 BRACKET - Pulley, Sta. 136. front, right I -15 20504-04 BRACKET - Pulley, Sta. 136, front 2 -It> 20505 -02 BRACKET - Pulley. Sta. 136, front, left I -17 20505 -03 BRACKET - Pulley. Sta, 136, front, left I -18 20554 -12 CHANNEL - Splice 1 -19 20554-16 ANGLE - Left I 20554-17 ANGLE - Right I -20 23062-00 PLATE 2 -21 23M3-DO FITTING ASSEMBLY 2 -22 80022-97 BUSHING - Rear spar artachment I A - Used on PA-30 with serial numbers 30-853, 30-902 and up. and PA-39 with serial numbers 39-1 and up . B • Used on PA-30 with serial numbers 30-1255 to 30-1716 inclusive, 30-1718 to 30-1744 inclustve . C • Used on PA-30 with serial numbers 30-853, 30-902 to 30-1716 inclusive, 30-1718 to 30-1744 mclustve . 0 - Used on PA-30 with serial numbers 30-1717, 30-1745 and up. and PA-39 with serial numbers 39-1 and up. Y - Used on PA-30 airplanes only. Z - Used on PA -39 airplanes only. • • • FUSELAGE REAR FRAME ASSEMBLY (See Code "A") .Ill- SECTION II Fuselage Group When ordering, olways spe<;ify Port Number, Description and Serial Number of AircrQft ISSUED: FEBRUARY 1973 1C12 PA-30 PA-]9 Figure J and Part ~ SERIAL NUMBERS Index Number NOMENCLATURE f AFFECTED 1\1 Number 11A-23 23665-02 DOUDLER - Fuselage, Sta. 136, left. I 23664-02 DOUBLER - Fuselage, Sta, 136, left I -24 25318-02 BRACKET - 51: •• 136. front, left I 25318-03 BRACKET - Sta, 136. front. dlhl 1 -25 25318-04 BRACKET - Sta. 136, front. left 1 25318-05 BRACKET - Sta. 136. front, right I -26 25320-05 STRIP - Bulkhead. St.. 136 I -27 20600-56 STRINGER - Fuselage bottom. St•. lOS [0 Sta. 113 3 -27a 26103-00 STRINGER - Fuselage bottom. Sta. lOS [0 Sta. 113 1 -28 20600-58 STRINGER - Puselqe bottom. St•• 113 [0 Sta. 136. lett I 20600-59 STRINGER - Fuselqe bottom. ·St •• 113 to 5I:a. 136. right I -29 25333-04 STRINGER • Fuselage bottom. 51:•• 113 [0 St•• 136. lett I 25333-05 STRINGER - Fuselage bottom. Sta. 113 to Sta. 136. right 1 -30 20600-70 STRINGER - Fuselage bottom. St.. 122 1 -31 25333-02 CHANNEL - Fuselage. Sta. 136 to St•• 157. bottom. left I 25333-03 CHANNEL - Fuselaae. Sta. 136 to 51:•• 157. bottom. right 1 -32 25333-12 CHANNEL - St.. 136 to St.. 157. right 1 -33 22620-08 STRINGER - Fuselage bottom. Sta. 136 to St•• 157. left 1 22620-09 STRINGER - Fuselage bottom. St•• 136 to Sta. 157. right: I -.14 20600-75 CHANNEL - Fuselage bottom. Sta. 136 to Sta. 157. right 1 -35 22618-04 B BULKHEAD ASSEMBLY: Fuselage. Sta. 113 1 22M8-08 C BULKHEAD ASSEMBLY - Fuselage. Sta. 113 1 -36 22618-02 CHANNEL - Fuselap. Sta. 113. left: 1 22618-03 CHANNEL - Fuselage. Sta. 113, right 1 -37 22618-os PLATE - Splice 1 ·38 20616-04 DOUBLER - Left 1 20616~05 DOUBLER - Right 1 -39 25316-00 STRINGER - Fuselage side, Sta. 113 to Sta. 136. lett I 25316-01 STRINGER - Fuselage side. St•• ·113 to Sta. 136. right 1 -40 25313-00 CHANNEL.ASSEMBLY - Fuselage stiffener. lett I 25313-01 CHANNEL ASSEMBLY - Fuselage stiffener. right I -41 25292-02 CHANNEL - Fuselage. left I 25292-03 CHANNEL - Fuselage. right 1 -42 25274-00 STRINGER ASSEMBLY - Fuselqe. left: I 25274-01 STRINGER ASSEMBLY - Fuselage. right I A - Used on PA-30 with serial numbers 30-853, 30-902 and up. and PA-39 with serial numbers 39-1 and up. B - Used on PA-30 with serial numbers 30-853. 30-902 to 30-1716 inclusive. 30-1718 to 30-1744 inclusive. C - Used on PA-30 with serial numbers 30-1717. 30-1745 and up. and PA-39 with serial numbers .39-1 and up. SECTION n Fuselage Group FUSELAGE REAR FRAME ASSF.MDLY (S<:e ClIde "A") When ordering. olways spec:ify Port Number. Description and Seriol N,,",,- of Alrcroft • • •ISSUED: FEBRUARY 1973 1. C13 PA-30 PA-39 Figure lind Part Code NOMENCLATURE No. SERIAL NUMBERS Index Number Req. AFFECTED Number 11A~ 25306-02 BULKHEAD· Su. 130. left 1 25306-03 BULKHEAD· Su. 130. right 1 .44 22587·00 GUSSET. Fusel. bulkhead 2 ~ 2531rMlO BRACKET ASSEMBLY· Sellt lupport, c:enur.llft 1 25315-04 BRACKET ASSEMBLY· Sellt IUpport, center, right 1 -46 25319-00 D

All Piper PA-39 Twin Comanche C/R v speeds reference