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Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522

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Illustrated Piper parts catalog 753 522 for PA-23-250 Aztec and PA-23-235 Apache airplanes, revised January 10, 2009, with figure-indexed replacement parts by serial number.

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Description

Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522

This download is the Piper Aircraft Corporation illustrated parts catalog issued for replacement-part identification on the PA-23-250 Aztec, the PA-23-250 six-place Aztec, and the PA-23-235 Apache. The catalog carries Piper part number 753 522, was first issued August 15, 1972, and is revised through January 10, 2009. Use it to match a visible assembly on the airframe to a figure index number, then to the listed Piper part number, nomenclature, quantity, and serial-number effectivity. The introduction states that under no circumstances shall this catalog be used for rigging and installation purposes.

File Details

  • Manual type: Illustrated parts catalog
  • Brand / models: Piper PA-23-235 Apache, PA-23-250 Aztec, PA-23-250 (Six Place) Aztec
  • Document number: 753 522
  • First issued: August 15, 1972
  • Revision date: January 10, 2009
  • Language: English
  • Page count: 684
  • File format: PDF
  • Manufacturer listed: Piper Aircraft Corporation, Lock Haven, Pennsylvania

Airplanes and Serial Effectivity

The Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 applies part numbers by airplane serial number. Keep the serial block in mind before you order:

  • 1960 Aztec PA-23-250: serials 27-1 through 27-366
  • 1961 Aztec PA-23-250: serials 27-367 through 27-504
  • Apache PA-23-235: serials 27-505 through 27-622
  • Aztec PA-23-250 (Six Place) Model B: serials 27-2000 through 27-2504
  • Aztec PA-23-250 (Six Place) Model C: serials 27-2505 through 27-3836 and 27-3838 through 27-3943
  • Aztec PA-23-250 (Six Place) Model D: serials 27-3837, 27-3944 through 27-4425, and 27-4427 through 27-4573
  • Aztec PA-23-250 (Six Place) Model E: serials 27-4426 and 27-4574 through 27-7554168
  • Aztec PA-23-250 (Six Place) Model F: serials 27-7654001 and up

Letter codes in the parts lists further restrict usage. X marks PA-23-250 only, Y marks the six-place Aztec, and Z marks the PA-23-235 Apache. Additional letter notes call out kits already installed, 14-volt versus 28-volt electrical systems, turbocharged versus naturally aspirated powerplants, and color or vendor options.

How the Listings Are Arranged

Each illustrated group opens with an exploded view. The facing parts list uses six columns: figure and index number, part number, code, nomenclature, number required, and serial numbers affected. Indentation and asterisks show next-higher-assembly relationships. Order the top-level assembly and you receive the indented items; order a single indented item and you receive only that piece. Commercial attaching hardware such as AN bolts and MS nuts is listed after the part name for convenience, even though Piper generally does not stock those items as catalog merchandise.

IMAGES PREVIEW

Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 — PDF page 1 preview
Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 — PDF page 13 preview
Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 — PDF page 14 preview

The catalog also explains how to work from a part you can see: start with Figure 1 (complete airplane) to pick the major group, open the matching figure, read the index number off the drawing, then read the full line in the parts list. Orders must include model, serial number, part number, name, type, and quantity.

Limitations printed in the catalog

On PA-23-250 six-place airplanes serial 27-7954061 and up, replacement parts for optional avionics and electronics installations (radar, radio altimeter, encoding altimeter, and similar equipment) are not listed or illustrated. On serial 27-8054001 and up, optional autopilot parts are likewise omitted. For those airplanes the catalog directs you to the avionics drawing index list and the drawings supplied with the aircraft. The cover also identifies this issue as Card 1 of 3 in the original card-set format; the compiled file presented here runs through Section XI and the numerical index.

Chapters Covered

  • Introduction, revisions status, serial-number information, standard paint chart, and table of contents
  • Figure 1 — View of complete airplane
  • Section I Wing Group — Wing installation; flap and aileron assemblies; wing and wing-tip construction; wing and wing-tip skin
  • Section II Fuselage Group — Complete fuselage; forward, center, and aft sections; bottom fairing; fuselage frame; instrument panel installations (single and dual, by serial block); control pedestal; floorboard and cockpit finishing; window curtains; enclosure; baggage and cabin doors; oxygen systems; seats; vacuum pumps; airspeed, static, oil-pressure and manifold-pressure lines; ventilating systems; Stewart Warner and Janitrol heater assemblies
  • Section III Chassis Group — Gear strut assemblies; nose gear and nose wheel; main gear and main wheel; brake and dual-brake installations; brake assembly
  • Section IV Tail Surfaces Group — Tail surfaces installation; stabilator assemblies by serial block; rudder assembly; fin assembly
  • Section V Power Plant Group — Power-plant installation by serial block; AiResearch and Lycoming turbocharger installations; propellers; propeller synchronizer and synchrophaser systems; engine baffles; exhaust collectors and exhaust system; nacelle installations including the Lycoming-turbocharger nacelle
  • Section VI Fuel System Group — Fuel system and fuel-injection installations; fuel cells; wing-tip fuel tanks; fuel-system control boxes
  • Section VII Electrical System Group — Fuselage and wing electrical installations; 14-volt and 28-volt battery boxes; pedestal and instrument-panel electrical installations; taxi and strobe lights; external power supply; propeller deicers; pneumatic deicers (B.F. Goodrich and Airborne/Goodyear)
  • Section VIII Hydraulic System Group — Hydraulic system and component installations; landing-gear anti-retraction valve; hydraulic powerpak components; emergency gear extender
  • Section IX Control System Group — Engine controls; stabilator, aileron, and rudder controls; tail-trim mechanism; trim-tab interconnect
  • Section X Electronics Group — Collins and ARC radios; radio junction boxes (14-volt and 28-volt); all-weather antenna; ELT installations (Garrett, Communications Components Corp., Narco); marker beacon; AutoControl I/II/III/III B; AltiMatic I through V and related flight-director installations; Bendix FCS-810; King KAP-200 / KFC-200; radar altimeter; glide-slope coupler; RMI; King KWX-40 and Bendix RDR-150 radar; encoding altimeter; radio installation and wiring-diagram drawing list
  • Section XI Miscellaneous Group — Optional equipment kits, repair kits and special tools; decals
  • Numerical index of part numbers to figure and index numbers

Taken as a whole, the Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 is a parts-identification book rather than a workshop procedure manual. A technician uses the figures and serial-coded lists to decide which wing panel, flap hinge, nacelle cowl, fuel cell, powerpak component, or radio junction box belongs on a given serial number, then places the order with the correct Piper number and nomenclature.

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the “Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522” are as follows:

753-522 – AZTEC PARTS CATALOG – PA-23-235 APACHE, PA-250 AZTEC, PA-23-250 (SIX PLACE) AZTECp. 1
AEROFICHE EXPLANATION AND REVISION STATUSp. 2
INTRODUCTIONp. 3
TABLE OF CONTENTSp. 8
FIGURE 1. VIEW OF COMPLETE AIRPLANEp. 13
SECTION I – WING GROUPp. 14
FIGURE 2. WING INSTALLATIONp. 14
FIGURE 2A. FLAP ASSEMBLY AND AILERON ASSEMBLYp. 19
FIGURE 3. WING AND WING TIP CONSTRUCTIONp. 24
FIGURE 4. WING AND WING TIP SKINp. 31
SECTION II – FUSELAGE GROUPp. 35
FIGURE 5. COMPLETE FUSELAGEp. 35
FIGURE 6. FUSELAGE FORWARD SECTION (PA-23-235, PA-23-250)p. 38
FIGURE 6A. FUSELAGE FORWARD SECTION (PA-23-250(6))p. 43
FIGURE 7. FUSELAGE CENTER SECTIONp. 53
FIGURE 7A. FUSELAGE BOTTOM FAIRINGp. 60
FIGURE 8. FUSELAGE AFT SECTIONp. 64
FIGURE 9. FUSELAGE FRAMEp. 72
FIGURE 10. INSTRUMENT PANEL INSTALLATION (PA-23-235/250/250(6))p. 76
FIGURE 10A. INSTRUMENT PANEL INSTALLATION (PA-23-250(6))p. 87
FIGURE 10B. INSTRUMENT PANEL INSTALLATION (PA-23-250(6))p. 97
FIGURE 10C. INSTRUMENT PANEL INSTALLATION (PA-23-250(6))p. 102
FIGURE 10D. DUAL INSTRUMENT PANEL INSTALLATION (PA-23-250(6))p. 107
FIGURE 10E. DUAL INSTRUMENT PANEL INSTALLATION (PA-23-250(6))p. 111
FIGURE 10F. DUAL INSTRUMENT LINES AND RIGHT PITOT STATIC SYSTEM INSTALLATIONp. 114
FIGURE 11. CONTROL PEDESTAL INSTALLATIONp. 116
FIGURE 12. FLOORBOARD AND COCKPIT FINISHING INSTALLATION (PA-23-235/250/250(6))p. 122
FIGURE 12A. COCKPIT FINISHING INSTALLATION (PA-23-250(6))p. 142
FIGURE 12B. FLOORBOARD INSTALLATION (PA-23-250(6))p. 152
FIGURE 13. WINDOW CURTAINS INSTALLATIONp. 156
FIGURE 14. FUSELAGE ENCLOSURE INSTALLATIONp. 160
FIGURE 15. BAGGAGE DOOR ASSEMBLY AND CABIN DOOR ASSEMBLY (PA-23-235/250/250(6))p. 168
FIGURE 15A. BAGGAGE DOOR ASSEMBLY AND CABIN DOOR ASSEMBLY (PA-23-250(6))p. 177
FIGURE 16. OXYGEN SYSTEM INSTALLATION (PA-23-250)p. 181
FIGURE 16A. OXYGEN SYSTEM INSTALLATION (PA-23-250(6))p. 184
FIGURE 16B. OXYGEN SYSTEM INSTALLATION (PA-23-250(6))p. 187
FIGURE 16C. OXYGEN SYSTEM INSTALLATION (PA-23-250(6))p. 190
FIGURE 17. SEATS INSTALLATION (PA-23-235/250/250(6))p. 193
FIGURE 17A. SEATS INSTALLATION (PA-23-250(6))p. 208
FIGURE 17B. SEATS INSTALLATION (PA-23-250(6))p. 217
FIGURE 18. VACUUM PUMP INSTALLATION (PA-235/250/250(6))p. 222
FIGURE 18A. VACUUM PUMP INSTALLATION (PA-23-250(6))p. 227
FIGURE 19. AIRSPEED, STATIC, OIL PRESSURE AND MANIFOLD PRESSURE LINESp. 231
FIGURE 20. VENTILATING SYSTEM INSTALLATION (PA-23-235/250/250(6))p. 236
FIGURE 20A. VENTILATING SYSTEM INSTALLATION (PA-23-250(6))p. 239
FIGURE 20B. VENTILATING SYSTEM INSTALLATION (PA-23-250(6))p. 242
FIGURE 21. HEATER INSTALLATION (PA-23-235/250/250(6))p. 244
FIGURE 21A. HEATER INSTALLATION (PA-23-250(6))p. 248
FIGURE 22. HEATER ASSEMBLY (STEWART WARNER)p. 252
FIGURE 22A. JANITROL HEATER ASSEMBLYp. 260
FIGURE 22B. JANITROL HEATER COMPONENTSp. 264
SECTION III – CHASSIS GROUPp. 267
FIGURE 23. GEAR STRUT ASSEMBLIESp. 267
FIGURE 24. NOSE GEAR INSTALLATIONp. 270
FIGURE 24A. NOSE WHEEL ASSEMBLYp. 275
FIGURE 25. MAIN GEAR INSTALLATIONp. 278
FIGURE 26. MAIN WHEEL ASSEMBLYp. 282
FIGURE 27. BRAKE INSTALLATIONp. 284
FIGURE 27A. DUAL BRAKE INSTALLATIONp. 287
FIGURE 28. BRAKE ASSEMBLYp. 290
SECTION IV – TAIL SURFACES GROUPp. 293
FIGURE 29. TAIL INSTALLATIONp. 293
FIGURE 29A. STABILATOR ASSEMBLY (PA-23-235/250/250(6))p. 297
FIGURE 29B. STABILATOR ASSEMBLY (PA-23-250(6))p. 299
FIGURE 29C. RUDDER ASSEMBLYp. 302
FIGURE 29D. FIN ASSEMBLYp. 305
SECTION V – POWER PLANT GROUPp. 308
FIGURE 30. POWER PLANT INSTALLATION (PA-23-235/250/250(6))p. 308
FIGURE 30A. POWER PLANT INSTALLATION (PA-23/250(6))p. 311
FIGURE 30B. TURBOCHARGER INSTALLATION (AIRESEARCH)p. 316
FIGURE 30C. TURBOCHARGER INSTALLATION (LYCOMING)p. 318
FIGURE 31. PROPELLER (PA-23-235/250/250(6))p. 323
FIGURE 31A. PROPELLER (PA-23-250(6))p. 326
FIGURE 31B. PROPELLER SYNCHRONIZER SYSTEM INSTALLATIONp. 330
FIGURE 31C. PROPELLER SYNCHROPHASER SYSTEM INSTALLATIONp. 332
FIGURE 32. ENGINE BAFFLE INSTALLATIONp. 334
FIGURE 33. EXHAUST COLLECTORS INSTALLATION (PA-23-235/250/250(6))p. 337
FIGURE 33A. EXHAUST SYSTEM INSTALLATION (PA-23-250(6))p. 339
FIGURE 34. NACELLE INSTALLATION (PA-23-235/250/250(6))p. 341
FIGURE 34A. NACELLE INSTALLATION (PA-23-250(6))p. 345
FIGURE 34B. NACELLE INSTALLATION (LYCOMING TURBOCHARGER)p. 352
SECTION VI – FUEL SYSTEM GROUPp. 357
FIGURE 35. FUEL SYSTEM INSTALLATION (PA-23-235/250/250(6))p. 357
FIGURE 35A. FUEL INJECTION SYSTEM INSTALLATION (PA-23-250(6))p. 364
FIGURE 35B. FUEL SYSTEM INSTALLATION (PA-23-250(6))p. 368
FIGURE 36. FUEL CELL INSTALLATION (PA-23-235/250/250(6))p. 374
FIGURE 36A. FUEL CELL INSTALLATION (PA-23-250(6))p. 378
FIGURE 36B. WING TIP FUEL TANK INSTALLATION (PA-23-250(6))p. 381
FIGURE 37. FUEL SYSTEM CONTROL BOX (PA-23-235/250/250(6))p. 383
FIGURE 37A. FUEL SYSTEM CONTROL BOX (PA-23-250(6))p. 387
SECTION VII – ELECTRICAL SYSTEM GROUPp. 390
FIGURE 38. FUSELAGE ELECTRICAL SYSTEM INSTALLATION (PA-23-235/250)p. 390
FIGURE 38A. FUSELAGE ELECTRICAL SYSTEM INSTALLATION (PA-23-250(6))p. 393
FIGURE 38B. WING ELECTRICAL SYSTEM INSTALLATION (PA-23-235/250)p. 399
FIGURE 38C. WING ELECTRICAL SYSTEM INSTALLATION (PA-23-250(6))p. 402
FIGURE 38D. BATTERY BOX INSTALLATION (PA-23-235/250)p. 406
FIGURE 38E. BATTERY BOX INSTALLATION (14-VOLT) (PA-23-250(6))p. 408
FIGURE 38F. BATTERY BOX INSTALLATION (28-VOLT) (PA-23-250(6))p. 411
FIGURE 38G. BATTERY BOX INSTALLATION (28-VOLT) (PA-23-250(6))p. 414
FIGURE 39. PEDESTAL ELECTRICAL INSTALLATIONp. 416
FIGURE 39A. INSTRUMENT PANEL ELECTRICAL INSTALLATION (PA-23-235/250/250(6))p. 419
FIGURE 39B. INSTRUMENT PANEL ELECTRICAL INSTALLATION (PA-23-250(6))p. 423
FIGURE 39C. INSTRUMENT PANEL ELECTRICAL INSTALLATION (PA-23-250(6))p. 426
FIGURE 40. TAXI LIGHT INSTALLATIONp. 430
FIGURE 40A. STROBE LIGHTS INSTALLATIONp. 432
FIGURE 41. EXTERNAL POWER SUPPLY (PA-23-235/250/250(6))p. 435
FIGURE 41A. EXTERNAL POWER SUPPLY (PA-23-250(6))p. 438
FIGURE 42. PROPELLER DEICER INSTALLATION (PA-23-250)p. 440
FIGURE 42A. PROPELLER DEICER INSTALLATION (PA-23-250(6))p. 442
FIGURE 42B. PNEUMATIC DEICER INSTALLATION (B. F. GOODRICH)p. 445
FIGURE 42C. PNEUMATIC DEICER INSTALLATION (B. F. GOODRICH)p. 451
FIGURE 42D. PNEUMATIC DEICER INSTALLATION (AIRBORNE/GOODYEAR) (PA-23-250(6))p. 455
SECTION VIII – HYDRAULIC SYSTEM GROUPp. 459
FIGURE 43. HYDRAULIC SYSTEM INSTALLATION (PA-23-235/250/250(6))p. 459
FIGURE 43A. FUSELAGE HYDRAULIC SYSTEM INSTALLATION (PA-23-250(6))p. 465
FIGURE 43B. WING HYDRAULIC SYSTEM INSTALLATION (PA-23-250(6))p. 469
FIGURE 43C. HYDRAULIC SYSTEM COMPONENTS (PA-23-250(6))p. 472
FIGURE 44. LANDING GEAR ANTI-RETRACTION VALVE INSTALLATIONp. 476
FIGURE 45. HYDRAULIC POWERPAK COMPONENTSp. 478
FIGURE 45A. HYDRAULIC POWERPAK COMPONENTSp. 482
FIGURE 46. EMERGENCY GEAR EXTENDER INSTALLATION (PA-23-235/250/250(6))p. 485
SECTION IX – CONTROL SYSTEM GROUPp. 488
FIGURE 47. ENGINE CONTROLS INSTALLATIONp. 488
FIGURE 48. STABILATOR CONTROL INSTALLATIONp. 491
FIGURE 49. AILERON CONTROLS INSTALLATIONp. 494
FIGURE 50. RUDDER CONTROL INSTALLATIONp. 497
FIGURE 51. TAIL TRIM MECHANISM INSTALLATIONp. 500
FIGURE 51A. TRIM TAB INTERCONNECT SYSTEM INSTALLATIONp. 506
SECTION X – ELECTRONICS GROUPp. 513
FIGURE 52. COLLINS AND ARC RADIO INSTALLATIONp. 513
FIGURE 53. RADIO JUNCTION BOXES (PA-23-235/250/250(6))p. 517
FIGURE 54. RADIO JUNCTION BOXES (PA-23-250(6))p. 521
FIGURE 54A. RADIO JUNCTION BOXES (14-VOLT) (PA-23-250(6))p. 523
FIGURE 54B. RADIO JUNCTION BOXES (28-VOLT) (PA-23-250(6))p. 525
FIGURE 55. ALL WEATHER ANTENNA INSTALLATIONp. 527
FIGURE 55A. PIPER AUTOMATIC LOCATOR (ELT) INSTALLATION (GARRETT MFG. LTD)p. 529
FIGURE 55B. PIPER AUTOMATIC LOCATOR (ELT) INSTALLATION (COMMUNICATIONS COMPONENTS CORP)p. 531
FIGURE 55C. PIPER AUTOMATIC LOCATOR (ELT) INSTALLATION (NARCO AVIONICS)p. 533
FIGURE 56. PIPER PM-1 MARKER BEACON INSTALLATION (PA-23-250(6))p. 535
FIGURE 57. AUTOCONTROL I INSTALLATIONp. 538
FIGURE 58. AUTOCONTROL II INSTALLATIONp. 541
FIGURE 59. AUTOCONTROL III INSTALLATION (PA-23-250(6))p. 544
FIGURE 59A. AUTOCONTROL III B INSTALLATION (PA-23-250(6))p. 546
FIGURE 60. ALTIMATIC PILOT I INSTALLATIONp. 548
FIGURE 61. ALTIMATIC PILOT II INSTALLATIONp. 551
FIGURE 61A. ALTIMATIC PILOT III AND III B INSTALLATIONp. 556
FIGURE 62. ALTIMATIC PILOT II B-1 INSTALLATIONp. 560
FIGURE 63. ALTIMATIC PILOT III C INSTALLATION (PA-23-250(6))p. 563
FIGURE 64. ALTIMATIC X F/D AUTOPILOT INSTALLATION (PA-23-250(6))p. 567
FIGURE 65. ALTIMATIC X AUTOPILOT INSTALLATION (PA-23-250(6))p. 570
FIGURE 66. ALTIMATIC V F/D AND V F/D-1 AUTOPILOT INSTALLATION (PA-23-250(6))p. 573
FIGURE 67. ALTIMATIC V AND V-1 AUTOPILOT INSTALLATION (PA-23-250(6))p. 579
FIGURE 68. AUTOPILOT/FLIGHT DIRECTOR INSTALLATION (BENDIX FCS-810) (PA-23-250(6))p. 583
FIGURE 69. AUTOPILOT INSTALLATION (BENDIX FCS-810) (PA-23-250(6))p. 586
FIGURE 69A. KING AUTOPILOT (KAP-200) AND KING AUTOPILOT F/D (KFC-200) INSTALLATIONp. 589
FIGURE 70 .RADAR ALTIMETER INSTALLATION (PA-23-250(6))p. 591
FIGURE 71. GLIDE SLOPE COUPLER INSTALLATION (PA-23-250(6))p. 593
FIGURE 72. RADIO MAGNETIC INDICATOR INSTALLATION (PA-23-250(6))p. 595
FIGURE 73. KING RADAR INSTALLATION (KWX-40) (PA-23-250(6))p. 597
FIGURE 74. BENDIX RADAR INSTALLATION (RDR-150) (PA-23-250(6))p. 599
FIGURE 75. ENCODING ALTIMETER INSTALLATION (PA-23-250(6))p. 602
RADIO INSTALLATION AND WIRING DIAGRAM DRAWINGSp. 604
SECTION XI – MISCELLANEOUS GROUPp. 613
OPTIONAL EQUIPMENT KITS, REPAIR KITS AND SPECIAL TOOLSp. 613
DECALSp. 619
NUMERICAL INDEXp. 627

Powerplant and Related Hardware Called Out in the Lists

Power Plant Group listings name the engines and turbocharger packages that change part effectivity. Engines called out include Lycoming O-540-A1B5 250 H.P., Lycoming O-540-A1D5 250 H.P., Lycoming IO-540-C4B5, Lycoming IO-540-J4A5, and Lycoming TIO-540-C1A. Separate figures cover AiResearch turbocharger installation, Lycoming turbocharger installation, early and late propellers, propeller synchronizer and synchrophaser hardware, baffles, exhaust collectors, and the distinct nacelle used with the Lycoming turbocharger. Fuel-system figures split carbureted installations, fuel-injection installations from serial 27-2322 through 27-2504, later six-place fuel systems, fuel cells through serial 27-4815 versus 27-4816 and up, and wing-tip tanks from serial 27-7654001 and up.

Airframe, Landing Gear, and Cabin Hardware

Wing Group figures identify left and right wing panel assemblies that change across Apache, early Aztec, and six-place production, plus spar straps, shims, root fairings, tie-down rings, ailerons, flaps, and wing tips. Fuselage Group figures run from the complete shell through serial-specific instrument panels, dual pitot-static hardware, seats, doors, oxygen bottles and regulators, Stewart Warner and Janitrol heaters, and ventilating ducting. Chassis Group figures cover nose and main gear struts, wheels, and single or dual brake installations. Tail figures separate the stabilator used through serial 27-7554168 and 27-8054001 and up from the stabilator used on serials 27-7654001 through 27-7954121, plus rudder and fin.

Electrical, Hydraulic, Ice Protection, and Paint

Electrical listings distinguish 14-volt and 28-volt battery boxes, with a further 28-volt split at serial 27-7954098. External power, taxi lights, strobes, propeller deicers, and pneumatic deicer boots from B.F. Goodrich and Airborne/Goodyear appear in their own figures. Hydraulic figures cover the early combined system, the later split fuselage and wing systems, powerpak internals, the anti-retraction valve, and the emergency gear extender through serial 27-7954121. A standard paint chart lists exterior enamel, acrylic lacquer, and Titanine polyurethane colors with quart and gallon Piper numbers, plus interior thermoplastic-trim aerosol colors.

Ordering From This Catalog

When you work from the Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522, specify model and serial number on every order, then the part number and the nomenclature exactly as printed. Shortages must be claimed within three days of receipt. Returned goods require prior written permission and prepaid freight. Damage in transit is a carrier claim. Those administrative notes sit in the front matter alongside the grid-numbering explanation left over from the Aerofiche card set.

What This Catalog Lets You Do

With the Piper PA-23-250 Aztec and PA-23-235 Apache Illustrated Parts Catalog 753 522 you can identify wing panels, flaps, ailerons, fuselage skins and frames, instrument panels, seats, doors, oxygen and heater components, landing-gear and brake parts, tail surfaces, engines and turbocharger hardware, propellers, fuel cells and selector boxes, electrical boxes and lighting, hydraulic powerpak pieces, flight-control cables and trim hardware, and the radios and autopilots that the catalog still illustrates for earlier serials. Matching the printed serial range and letter code to the airplane on the ramp keeps you from ordering a six-place-only panel for an Apache or a pre-4816 fuel cell for a later wing. Instant PDF delivery after payment means you can open the figures on any device and print the pages you need in the hangar—no shipping wait.

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