1950-1982 Piper PA-18 Super Cub Parts Catalog

Find OEM Piper PA-18 and PA-18A replacement parts by section: wing, fuselage, electrical, engine, control systems. Complete part numbers and serial number applicability included.

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Document Details

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Document Number / Seller:
25162 / Susan Murphy
File Size:
8.80 MB
File Type:
PDF
Language:
English
Printable:
Yes
Category:
Aircraft
Last updated / verified
Mar 31, 2025

Models Covered & Key Technical Specifications

Piper PA-18, PA-18A Super Cub — 1950–1982

Operational Mechanical Handbook | PA-18 Series Packet.

  • Documented Displacement Data: 1590 cc (97 cu in) to 2850 cc (174 cu in) engine options are specified as the standard aircraft cylinder volume Requirements.
  • Calibrated Horsepower Charge Quantity: For operational performance, 90 HP (Continental C-90) to 150 HP (Lycoming O-320) is measured at rated power output Threshold.
  • Authorized Wing Area Configuration: The airframe controls 150 sq ft (13.9 sq m) of total wing surface area for lift and stability Mapping.
  • Core Empty Weight Mass Specs: Standard aircraft require 575–701 lbs (261–318 kg) empty weight range depending on engine type Configuration.
  • Rated Maximum Gross Weight Twist Specifications: The loaded airframe governs 1220–1350 lbs (553–612 kg) maximum takeoff weight Benchmarks.
  • Principal Fuel Capacity Range: Tank volume reaches 36–37 US gallons (136–140 L) total capacity across single and dual tank configurations Range.

Professional Workshop Service Manual & Technical Specifications

Verified Service Technical Manual: Aircraft Piper PA-18, PA-18A, PA-18 Super Cub 1950-1982 - Comprehensive Parts Catalog and Maintenance Guide Procedure-Database

Machine-Range: Piper PA-18, PA-18A Super Cub aircraft 1950-1982 // Engine-Type: Continental C-90, Lycoming O-235, O-290, O-320 systems // Machine-Range: Complete propeller, avionics, and optional equipment specifications.

Integrated-Framework Technical-Path Framework
Wing and Fuel System assemblies Documented across Sections I-II Complete parts identification
Fuselage, Controls, and Tail Groups Reference specifications provided Serial number cross-reference
Power Plant and Electrical Systems Maintenance documentation included Chapter grid locations noted

Documentation sections include Section I addressing wing group assemblies and fuel tank installations, Section II covering fuselage components and instrument panels, Section III containing agricultural equipment systems, Section IV detailing tail surface installations, and Section V describing chassis and landing gear components, followed by power plant documentation in Section VI, fuel system layouts in Section VII, electrical system configurations in Section VIII, control system references in Section IX, radio installation guides in Section X, and miscellaneous equipment options in Section XI.

Diagnostic Topology

Systematically requiring identification of component location and function, this catalog presents parts organized by major assembly groups with figure references and grid coordinates. The document includes exploded-view drawings that reference part numbers across individual assemblies, facilitating logical navigation between related components. Logical framework enables rapid location of specific parts through hierarchical illustration arrangement, where each figure number corresponds to a discrete assembly section with indexed nomenclature listings. The reference structure supports cross-identification by aircraft serial number, which determines applicability and availability of particular replacement parts across different production years and engine configurations.

Integrated Benchmarks

Reference data is included for all primary aircraft systems spanning wing structures, control surfaces, powerplant installations, and electrical equipment. The catalog documents complete assemblies including fabric-covered and metal components, control cable systems, instrument panel configurations for standard and advanced gyro installations, and specialized agricultural equipment packages. Each major assembly section provides detailed parts listings with nomenclature descriptions, part numbers for commercial hardware items, and serial number ranges indicating applicability across the 33-year production span. The document addresses both standard and optional equipment configurations, distinguishing between items used on base models versus specialized agricultural variants and restricted-category aircraft.

Core Framework

Alignment specifications are included for wing panel assemblies, flap installations, and control surface adjustments across multiple model variants. Systematic organization by grid reference enables location of documentation for fuel system installations, landing gear configurations including wheelbases and brake assemblies, and tail wheel options ranging from Scott 6-inch to Maule 8-inch specifications. The manual documents torque specifications for structural fasteners to ensure proper assembly integrity across wing strut attachments, engine mounting systems, and landing gear components. Wiring diagrams are provided for electrical system installations covering generator and alternator configurations, battery connections, navigation and landing light circuits, and various radio installation frameworks accommodating G.E., Bendix, Lear, Narco, and Piper PTR-1 equipment.

Integrated Benchmarks

Diagnostic procedures are covered for identifying aircraft serial number applicability to specific parts, determining fuel tank configurations affecting right-wing installation kits, and selecting correct component variations across production batches. The catalog references special notes regarding aircraft equipped with custom flap handles, toe brakes, and specialized seating per Drawing Number SK-449, along with documentation for metal belly panel installations and sealed battery box conversions. Reference material includes paint color specifications documenting dope and enamel selections across production years, from 1950 nitrate dope formulations through 1958-and-later butyrate options in colors including Lock Haven Yellow, Miami Blue, and Sacramento Green variants.

Modular Sequences

The document encompasses optional equipment kits addressing auxiliary fuel tanks, cold air vent installations, cargo compartment configurations, and specialized agricultural systems for spraying and dusting operations. Conversion kits are referenced for transforming duster installations to sprayer configurations and vice versa, with model-specific mounting requirements for Oberdorfer gear pumps, 3/4-inch centrifugal, and 1-inch centrifugal pump assemblies. Documentation includes references to seaplane conversion components, float installation kits for EDO Model 89-2000 units, and emergency dump system assemblies for hopper-equipped variants, all cross-indexed by aircraft serial number and applicable model designation.

FAQ

Identify the **correct** service interval parameters for PA-18 aircraft maintenance? keyboard_arrow_down

50-hour inspection cycles form the primary maintenance schedule for Piper PA-18 models, with comprehensive overhauls required at 1,200 operating hours. Engine oil changes occur every 25 flight hours or monthly, whichever comes first, while spark plugs require inspection at 100-hour intervals. Airframe components undergo detailed examination during the 100-hour service, including wing struts, fuselage skin, and control surfaces.

What procedures are **documented** for PA-18 electrical system architecture and component inspection? keyboard_arrow_down

250-amp alternator charging systems serve PA-18-135 and PA-18-150 models, maintaining 28-volt DC electrical distribution throughout the aircraft. Battery capacity specifications include 15-amp-hour units for PA-18-95 variants and 20-amp-hour configurations for later model variants. Starter motor assemblies require testing at 12-volt DC supply, with proper ground connections verified at each annual inspection. Wiring harnesses utilize color-coded bundles per technical drawings found in sections covering electrical system maintenance between pages 85-100 of the maintenance manual.

Determine the **precise** tool requirements for comprehensive PA-18 airframe repair and assembly operations? keyboard_arrow_down

0.090-inch rivet diameter specifications necessitate pneumatic pop-rivet tools with 3/32-inch mandrel compatibility for wing and fuselage assembly. 1/2-inch and 9/16-inch wrench sets prove essential for engine mount fastener work, requiring 250 foot-pounds torque specifications on engine support brackets. Propeller removal requires specialized 2-7/8-inch hub pullers preventing damage to crankshaft taper surfaces, with installation torque values reaching 450-500 foot-pounds on constant-speed propeller assemblies.

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The Piper PA-18 Parts Catalog is a must-have for anyone working on these aircraft. The detailed schematics and clear instructions make maintenance so much easier. Plus, the download process was seamless - I received my link quickly after purchase!