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Piper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640

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Complete illustrated Piper parts catalog 761-640 for the PA-32RT-300 Lance II and PA-32RT-300T Turbo Lance II – every figure, part number, index and serial-number application across all fourteen sections of the aircraft.

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Description

Piper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640

This is the Piper Parts Catalog covering the PA-32RT-300 Lance II and the turbocharged PA-32RT-300T, published under document number 761-640. It was originally issued on October 28, 1977 and consolidated through the January 1983 revision, giving you the accumulated parts breakdown for both normally aspirated and turbocharged Lance II airframes. Every replacement part in the catalog carries a Piper part number, a figure-and-index reference tying it back to its illustration, and where applicable a serial-number range showing which aircraft the part fits.

File Details

  • Manual type: Illustrated Parts Catalog (Aerofiche format)
  • Brand: Piper Aircraft Corporation
  • Models covered: PA-32RT-300 Lance II, PA-32RT-300T Turbo Lance II
  • Document number: 761-640
  • Original issue date: October 28, 1977
  • Revisions incorporated: September 1978, May 1979, April 1980, April 1981, January 1983
  • Aerofiche set: Two cards (card 1 of 2 and card 2 of 2)
  • Language: English
  • Format: PDF

Chapters Covered

The catalog is organised into fourteen major sections. Each section is further divided into illustrated sub-groups, and every sub-group carries its own parts listing.

  • Section I – Wing Group: Wing Installation; Leading Edge Assembly; Trailing Edge Assembly; Aileron Assembly; Flap Assembly
  • Section II – Fuselage Group: Fuselage Assembly Complete; Upper Forward, Center and Aft Cockpit Assemblies; Lower Forward and Aft Cockpit Assemblies; Aft Section; Forward Cabin Door; Aft Cabin Door; Forward Baggage Door; Aft Cargo Door; Enclosure Installation
  • Section III – Tail Surfaces Group: Tail Surfaces Installation; Stabilator Assembly; Fin Assembly; Rudder Assembly
  • Section IV – Landing Gear Group: Nose Gear Installation and Assembly; Cleveland and McCauley Nose Wheels; Main Gear Installation and Assembly; Main Wheel Assembly; Brake Assembly; Landing Gear Doors (PA-32RT-300 and PA-32RT-300T); Hand Brake Installation; Toe Brake Installation; Toe Brake Master Cylinder Assembly
  • Section V – Cabin Equipment Group: Cockpit Finishing Installation; Window Curtain Installation; Carpet Installation; Headliner and Forward Air Duct Installation; Seats Installation; Vertically Adjustable Front Seat Assembly; 7th Seat Installation; Aft Facing Center Seat Assembly; Club Seating Installation
  • Section VI – Instruments Group: Instrument Panel Installation; Vacuum System Installation; Pitot Static System Installation
  • Section VII – Power Plant Group: Power Plant Installation (PA-32RT-300 and PA-32RT-300T); Engine Instrument Lines; Engine Exhaust System; Engine Baffle Installation; Engine Cowl Assembly; Propeller Assembly; Engine Controls Installation
  • Section VIII – Fuel System Group: Forward Fuel System Installation; Aft Fuel System Installation; Fuel Tank Assemblies
  • Section IX – Control System Group: Control System Installation; Flap Control Installation; Stabilator Trim Installation; Rudder Trim Mechanism Installation; Control Wheel Installation; Rudder Pedal Installation
  • Section X – Hydraulic System Group: Hydraulic System Installation
  • Section XI – Environmental Group: Cabin Heat and Defroster System; Aft Fresh Air Duct Installation; Air Conditioning Compressor, Refrigerant Lines and Alternator Installation; Air Conditioning Duct and Evaporator Installation; Air Conditioning Condenser Installation
  • Section XII – Electrical System Group: Electrical System Installation; Instrument Panel Electrical Installation; Air Conditioning Electrical Installation; Battery Box Installation; External Power Supply Installation; Standard Alternator Assembly (Chrysler); Air Conditioning Alternator Assembly (Prestolite)
  • Section XIII – Electronics Group: Electric Trim Installation; AutoFlite II Installation; AutoControl III B Installation; AltiMatic III C Installation; King KFC-200 AutoPilot Installation; Piper Automatic Locator (ELT) Installations; Radar Altimeter Installation; Encoder Installation; Radio, Antenna System and Static Wicks Installation; Audio Selector Assembly; Radar System Installation; Radio Installation Drawings
  • Section XIV – Miscellaneous Group: Placards and Exterior Stencils; Optional Equipment Kits and Repair Kits
  • Standard Paint Chart: Acrylic Lacquer and Polyurethane Enamel exterior finish references

Complete PDF Bookmark Tree

Complete Bookmarks

The complete bookmarks in the β€œPiper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640” are as follows:

761-640 – LANCE II PARTS CATALOG – PA-32RT-300, PA-32RT-300Tp. 1
AEROFICHE EXPLANATIONp. 2
INTRODUCTIONp. 3
TABLE OF CONTENTSp. 8
FIGURE 1. COMPLETE AIRPLANEp. 12
SECTION I – WING GROUPp. 13
FIGURE 2. WING INSTALLATIONp. 13
FIGURE 3. WING LEADING EDGE ASSEMBLYp. 17
FIGURE 4. WING TRAILING EDGE ASSEMBLYp. 20
FIGURE 5. AILERON ASSEMBLYp. 25
FIGURE 6. FLAP ASSEMBLYp. 28
SECTION II – FUSELAGE GROUPp. 31
FIGURE 7. FUSELAGE ASSEMBLY – COMPLETEp. 31
FIGURE 8. FUSELAGE UPPER FORWARD COCKPIT ASSEMBLYp. 35
FIGURE 9. FUSELAGE UPPER CENTER COCKPIT ASSEMBLYp. 39
FIGURE 10. FUSELAGE UPPER AFT COCKPIT ASSEMBLYp. 43
FIGURE 11. FUSELAGE LOWER FORWARD COCKPIT ASSEMBLYp. 47
FIGURE 12. FUSELAGE LOWER AFT COCKPIT ASSEMBLYp. 51
FIGURE 13. FUSELAGE AFT SECTIONp. 55
FIGURE 14. FORWARD FUSELAGE CABIN DOORp. 59
FIGURE 15. FUSELAGE AFT CABIN DOORp. 63
FIGURE 16. FUSELAGE FORWARD BAGGAGE DOORp. 67
FIGURE 17. FUSELAGE AFT CARGO DOORp. 71
FIGURE 18. FUSELAGE ENCLOSURE INSTALLATIONp. 74
SECTION III – TAIL SURFACES GROUPp. 78
FIGURE 19. TAIL SURFACES INSTALLATIONp. 78
FIGURE 20. STABILATOR ASSEMBLYp. 81
FIGURE 21. FIN ASSEMBLYp. 85
FIGURE 22. RUDDER ASSEMBLYp. 88
SECTION IV – LANDING GEAR GROUPp. 92
FIGURE 23. NOSE GEAR INSTALLATIONp. 92
FIGURE 24. NOSE GEAR ASSEMBLYp. 97
FIGURE 25. NOSE WHEEL ASSEMBLY (CLEVELAND)p. 101
FIGURE 26. NOSE WHEEL ASSEMBLY (MCCAULEY)p. 104
FIGURE 27. MAIN GEAR INSTALLATIONp. 107
FIGURE 28. MAIN GEAR ASSEMBLYp. 111
FIGURE 29. MAIN WHEEL ASSEMBLYp. 116
FIGURE 30. BRAKE ASSEMBLYp. 119
FIGURE 31. LANDING GEAR DOOR INSTALLATION (PA-32RT-300)p. 122
FIGURE 31A. LANDING GEAR DOOR INSTALLATION (PA-32RT-300T)p. 125
FIGURE 32. HAND BRAKE INSTALLATIONp. 129
FIGURE 33. TOE BRAKE INSTALLATIONp. 133
FIGURE 34. TOE BRAKE MASTER CYLINDER ASSEMBLYp. 136
SECTION V – CABIN EQUIPMENT GROUPp. 140
FIGURE 35. COCKPIT FINISHING INSTALLATIONp. 140
FIGURE 36. WINDOW CURTAINS INSTALLATIONp. 145
FIGURE 37. CARPET INSTALLATIONp. 148
FIGURE 38. HEADLINER AND FORWARD FRESH AIR DUCT INSTALLATIONp. 153
FIGURE 39. SEATS INSTALLATIONp. 156
FIGURE 40. VERTICALLY ADJUSTABLE FRONT SEAT ASSEMBLYp. 162
FIGURE 41. 7TH SEAT INSTALLATIONp. 166
FIGURE 42. AFT FACING SEAT ASSEMBLY – CENTERp. 169
FIGURE 43. CLUB SEATING INSTALLATIONp. 172
SECTION VI – INSTRUMENTS GROUPp. 176
FIGURE 44. INSTRUMENT PANEL INSTALLATIONp. 176
FIGURE 45. VACUUM SYSTEM INSTALLATIONp. 181
FIGURE 46. PITOT STATIC SYSTEM INSTALLATIONp. 184
SECTION VII – POWER PLANT GROUPp. 187
FIGURE 47. POWER PLANT INSTALLATION (PA-32RT-300)p. 187
FIGURE 47A. POWER PLANT INSTALLATION (PA-32RT-300T)p. 191
FIGURE 47B. ENGINE INSTRUMENT LINES INSTALLATION (PA-32RT-300T)p. 195
FIGURE 48. ENGINE EXHAUST SYSTEM INSTALLATION (PA-32RT-300)p. 198
FIGURE 49. ENGINE BAFFLE INSTALLATION (PA-32RT-300)p. 201
FIGURE 49A. ENGINE BAFFLE INSTALLATION (PA-32RT-300T)p. 204
FIGURE 50. ENGINE COWL ASSEMBLY (PA-32RT-300)p. 208
FIGURE 50A. ENGINE COWL ASSEMBLY (PA-32RT-300T)p. 211
FIGURE 51. PROPELLER ASSEMBLY (PA-32RT-300)p. 215
FIGURE 51A. PROPELLER ASSEMBLY (PA-32RT-300T)p. 218
FIGURE 52. ENGINE CONTROLS INSTALLATION (PA-32RT-300)p. 221
FIGURE 52A. ENGINE CONTROLS INSTALLATION (PA-32RT-300T)p. 226
SECTION VIII – FUEL SYSTEM GROUPp. 231
FIGURE 53. FORWARD FUEL SYSTEM INSTALLATION (PA-32RT-300)p. 231
FIGURE 53A. FORWARD FUEL SYSTEM INSTALLATION (PA-32RT-300T)p. 234
FIGURE 54. AFT FUEL SYSTEM INSTALLATION (PA-32RT-300)p. 237
FIGURE 54A. AFT FUEL SYSTEM INSTALLATION (PA-32RT-300T)p. 241
FIGURE 55. FUEL TANK ASSEMBLIESp. 245
SECTION IX – CONTROL SYSTEM GROUPp. 253
FIGURE 56. CONTROL SYSTEM INSTALLATIONp. 253
FIGURE 57. FLAP CONTROL INSTALLATIONp. 258
FIGURE 58. STABILATOR TRIM INSTALLATIONp. 262
FIGURE 59. RUDDER TRIM MECHANISM INSTALLATIONp. 266
FIGURE 60. CONTROL WHEEL INSTALLATIONp. 269
FIGURE 61. RUDDER PEDAL INSTALLATIONp. 273
SECTION X – HYDRAULICS SYSTEM GROUPp. 276
FIGURE 62. HYDRAULIC SYSTEM INSTALLATIONp. 276
SECTION XI – ENVIRONMENTAL GROUPp. 280
FIGURE 63. CABIN HEAT AND DEFROSTER SYSTEMp. 280
FIGURE 64. AFT FRESH AIR DUCT INSTALLATIONp. 284
FIGURE 65. AIR CONDITIONING COMPRESSOR REFRIGERANT LINES AND ALTERNATOR INSTALLATIONp. 287
FIGURE 66. AIR CONDITIONING DUCT AND EVAPORATOR INSTALLATIONp. 291
FIGURE 67. AIR CONDITIONING CONDENSER INSTALLATIONp. 294
SECTION XII – ELECTRICAL SYSTEM GROUPp. 297
FIGURE 68. ELECTRICAL SYSTEM INSTALLATIONp. 297
FIGURE 69. INSTRUMENT PANEL ELECTRICAL INSTALLATIONp. 301
FIGURE 70. AIR CONDITIONING ELECTRICAL INSTALLATIONp. 305
FIGURE 71. BATTERY BOX INSTALLATIONp. 308
FIGURE 72. EXTERNAL POWER SUPPLY INSTALLATIONp. 311
FIGURE 73. ALTERNATOR ASSEMBLY AND INSTALLATION (CHRYSLER)p. 314
FIGURE 74. ALTERNATOR ASSEMBLY (PRESTOLITE)p. 318
SECTION XIII – ELECTRONICS GROUPp. 321
FIGURE 75. ELECTRIC TRIM INSTALLATIONp. 321
FIGURE 76. AUTOFLITE II INSTALLATIONp. 324
FIGURE 77. AUTOCONTROL III B INSTALLATIONp. 327
FIGURE 78. ALTIMATIC III C INSTALLATIONp. 330
FIGURE 78A. KING KFC-200 AUTOPILOT INSTALLATIONp. 334
FIGURE 79. PIPER AUTOMATIC LOCATOR (ELT) INSTALLATION (COMMUNICATIONS COMPONENT CORP)p. 337
FIGURE 79A. PIPER AUTOMATIC LOCATOR (ELT) INSTALLATION (NARCO AVIONICS)p. 340
FIGURE 80. RADAR ALTIMETER INSTALLATIONp. 344
FIGURE 81. ENCODER INSTALLATION (NARCO – AR 500 AND UNITED – 5125-P3)p. 347
FIGURE 82. RADIO ANTENNA SYSTEM AND STATIC WICKS INSTALLATIONp. 350
FIGURE 83. AUDIO SELECTOR ASSEMBLYp. 353
FIGURE 84. RADAR SYSTEM INSTALLATION (PA-32RT-300) (PA-32RT-300T)p. 356
RADIO INSTALLATION DRAWINGSp. 359
SECTION XIV – MISCELLANEOUS GROUPp. 362
FIGURE 85. PLACARDS AND EXTERIOR STENCILSp. 362
OPTIONAL EQUIPMENT KITS AND REPAIR KITSp. 366
NUMERICAL INDEXp. 368

What separates this catalog from a generic service book is the way every part is anchored. The “Figure and Index Number” column ties each listing back to a numbered callout on the matching exploded illustration, so you can look at a drawing of the stabilator, find callout 23, and read straight across to the part number, description and quantity required. Indented listings show assembly hierarchy – order the parent assembly and you receive the components listed beneath it, or order the sub-component on its own. The “No. Req.” column tells you whether the quantity is per figure or per assembly, and the “AR” symbol flags parts used as required. The “Serial Numbers Affected” column is particularly valuable on a twin-variant catalog like this one, because so many Lance II parts were changed between the 1978 and 1979 production runs, or between the normally aspirated and turbocharged airframes. Codes throughout the listings direct parts with a “W” suffix to the Lock Haven spares department and everything else to Vero Beach, so you know which supply channel a part belongs to before you place an order.

The document also carries Piper’s own ordering and identification guidance – how to trace a part from its location on the aircraft, how to read the indent structure in the nomenclature column, and what information to supply when ordering. A complete table of contents at the start of each card lets you move directly to the figure you need instead of scanning hundreds of pages.

What This Lance II Parts Catalog Lets You Do

Whether you are maintaining a 1978 PA-32RT-300, a 1979 Turbo Lance II, or any aircraft in the covered serial ranges, this catalog gives you the identification layer that repair work depends on. You can trace a worn or damaged component from its position on the airframe diagram to its correct Piper part number, confirm whether that number applies to your specific serial number, and see exactly how many are required and what it attaches to.

That matters most when parts have been superseded. The catalog’s revision history runs through January 1983, and the code explanations scattered through the figures call out the differences directly – for example, stabilator trim barrel changes by serial number break, or landing gear door hardware that differs between the PA-32RT-300 and the PA-32RT-300T. Ordering the wrong variant of a small bracket or a trim cable is an expensive mistake, and the serial-number column is what prevents it.

Because the coverage spans wings, fuselage structure, tail surfaces, landing gear, brakes, cabin interior, instruments, power plant, exhaust, baffles, cowl, propeller, fuel system, flight controls, hydraulics, environmental systems, electrical system and the full electronics/avionics group, one document handles nearly every identification question that comes up on these aircraft. Airframe shops, avionics installers, interior refurbishers and owner-maintainers all work from the same reference.

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Piper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640 β€” PDF page 13 preview
Piper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640 β€” PDF page 39 preview
Piper PA-32RT-300 & PA-32RT-300T Lance II Illustrated Parts Catalog 761-640 β€” PDF page 198 preview

Delivered as an instant PDF download – no shipping, no waiting, and no physical binder to keep track of. Open it on a workshop laptop, a tablet at the aircraft, or a phone in the hangar. Print just the figures you need for the job in front of you, whether that is a single page or the whole wing group.

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