58-22-03: Goodrich G-3-787 Wheel Assembly
FAA order 58-22-03 is an airworthiness directive published December 16, 1958. The FAA's subject line: Goodrich G-3-787 Wheel Assembly. It names Piper PA-23 Apache and Aztec: about 1,315 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: landing gear.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Piper Aircraft Inc.
- Models
- PA-23
- On this site
- Piper PA-23 Apache and Aztec 1,315 registered
Dates and paperwork
- Published
- December 16, 1958
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (1,274 characters)
58-22-03 PIPER: Applies to All Model PA-23 Aircraft Equipped With Goodrich G-3-787 Main Wheel Assemblies.
Compliance required as indicated.
Failures of the Goodrich G-3-787 wheel assembly are being reported. These wheels may be continued in service subject to inspection as specified below, or replaced with Goodrich G-3-880 wheel assembly or Cleveland Aircraft Products wheel assembly Model 3060 or 3080A and brake assembly Model 3000-500 or another equivalent approved type wheel and brake combination.
1. Remove wheels and tires and inspect wheels at each one hundred hours of operation or at each tire change, whichever occurs first.
2. Inspect the flange area of both wheel halves by means of Dy-Check or Zyglo, whichever is available. Cracks may appear on either the inside or outside surface of the flange.
3. If cracks are present in the flange area, remove the defective wheel half from service and replace as indicated above.
4. To detect possible flange failures during preflight inspection, look for outward deformation of flanges. A wheel with a flange failure will appear to wobble when rotated.
(Goodrich Service Bulletin No. 102, dated July 25, 1956, and Piper Service Letter No. 291, dated June 5, 1957, covers this same subject.)
Related safety bulletins advice on the same designs, not orders
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2017-02-21CE-17-08 · Main Landing Gear Drag Link Bolt
2012-09-17CE-12-44 · Exhaust systems
2008-01-09CE-08-11 · Landing Gear
2005-07-07CE-05-67 ·
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of November 6, 2026. Connections as data: /graph/directive/58-22-03.json · aircraft systems.
