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63-21-05: Main and Nose Retraction Links

FAA order 63-21-05 is an airworthiness directive. The FAA's subject line: Main and Nose Retraction Links. It names Navion NAVION B, Navion NAVION D, Navion NAVION F, Navion NAVION G, Navion NAVION H: about 150 aircraft on the U.S. register today across them, 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
American Navion Society, LTD.; American Navion Society, LTD.; American Navion Society, LTD.; Fred Garcia; Sierra Hotel Aero, Inc.
Models
D-16, D-16A, 480, Navion (Army L-17A), Navion A (Army L-17B and L-17C), Navion B, Navion D, Navion E, Navion F, Navion G, Navion H
On this site
Navion NAVION B 42 registered
Navion NAVION D 5 registered
Navion NAVION F 6 registered
Navion NAVION G 61 registered
Navion NAVION H 36 registered

Dates and paperwork

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 (1,392 characters)
63-21-05 NAVION and TWIN NAVION: Amdt. 624 Part 507 Federal Register October 2, 1963. Applies to All Navion Serial Numbers NAV-4-2 and up, and all Twin Navion Aircraft, Temco D-16, Temco D-16A, Dauby, Riley, and Camair 480. Compliance required within the next 50 hours' time in service after the effective date of this directive. Service experience indicates that the unsafe condition in the main and nose gear retraction links which prompted the issuance of AD's 61-12-04 and 62-14-04 cannot in all cases be detected by the inspection as required in those AD's. Therefore, the following must be accomplished: (a) Replace the main gear retraction links with revised assembly Navion P/N 143- 33165-20, Temco P/N 57001-9 or FAA approved equivalent having the longer lap welded center section that completely covers the turned down part of the end fitting. (b) Replace the nose gear retraction link with revised assembly Navion P/N 145- 34106-20, Camair P/N 1-6031 or FAA approved equivalent having the longer lap welded center section that completely covers the turned down part of the end fitting. (c) Approval of equivalent parts shall be obtained from an FAA Regional Engineering and Manufacturing Branch or Aircraft Engineering Division, as appropriate. This supersedes AD's 61-12-04 and 62-14-04. This directive effective November 1, 1963. Revised August 25, 1965.

Related safety bulletins advice on the same designs, not orders

2022-05-27AIR-22-13 · Landing Gear Components
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
2007-03-14CE-06-11R1 · Fuel system selector valves

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 October 23, 2026. Connections as data: /graph/directive/63-21-05.json · aircraft systems.