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AD 56-16-04 ACTIVE

Landing Gear Torque Knees
Key Information
AD Number 56-16-04 Status Active
Effective Date Not specified Issue Date Not specified
Docket Number Unknown Amendment N/A
Product Type ["Aircraft"] Product Subtype ["Small Airplane"]
CFR Part --- - Part 39 CFR Section N/A
Citation This information is not available.
Applicability
Manufacturer(s) Swift Museum Foundation, Inc.
Model(s) GC-1A GC-1B
Regulatory Text

56-16-04 UNIVERSAL (Globe): Applies to Models GC-1A and GC-1B Aircraft.

To be accomplished as soon as possible but not later than September 15, 1956.

It has been reported that the landing gear was replaced with an E.L.I. type gear (air-oil) on a Globe Model GC-1B airplane with a serial number higher than 196. A subsequent failure of one of the aluminum alloy torque knees resulted in the loss of the left landing gear and damage to the airplane. It is probable that the Adel aluminum alloy knee was substituted for the regular P/N 64A40 forged steel knee. The Adel aluminum alloy knee is not a suitable replacement on the E.L.I. gear assembly, since it does not provide for the extension stop, P/N 64A31.

To preclude similar occurrences, all aircraft not equipped with Adel main landing gear struts must replace the aluminum alloy torque knees with forged steel knees.

1. On aircraft equipped with Adel struts, the Adel forged aluminum torque knee assembly is satisfactory and may be retained.

2. Forged steel knees, E.L.I. P/N 64A40 are suitable as replacements on all types of landing gear units.

This supersedes AD 46-33-01.