47-06-02: Landing Gear Retraction Placard
FAA order 47-06-02 is an airworthiness directive. The FAA's subject line: Landing Gear Retraction Placard. System: landing gear.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Swift Museum Foundation, Inc.
- Models
- GC-1A, GC-1B
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 (632 characters)
47-06-02 GLOBE: (Was Mandatory Note 5 of AD-766-5.) Applies to Models GC-1A and GC-1B Aircraft Serial Numbers 3 to 408 Inclusive; 1004 to 1319 Inclusive; and 2001 to 2239 Inclusive.
Compliance required prior to April 1, 1947.
Replace the warning placard located at the landing gear emergency extension crank with a revised placard, Globe P/N 11-532-3735, having the added instruction: "Crank back to the full up position before the next retraction of the landing gear". Complete rewinding is necessary to prevent damage to the retraction system.
(Globe Customer Service Maintenance Bulletin No. 6 covers this same subject.)
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/47-06-02.json · aircraft systems.
