AD 47-06-02

final rule
Data completeness: 60%

Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft

AD Number
47-06-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Swift Museum Foundation, Inc. GC-1A Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft
aircraft Swift Museum Foundation, Inc. GC-1B Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft

Unsafe Condition

Failure to crank the landing gear emergency extension crank back to the full up position before retraction could damage the retraction system.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Replace the landing gear emergency extension crank warning placard with Globe P/N 11-532-3735, which includes the instruction to crank back to the full up position before the next retraction. Complete rewinding is necessary to prevent damage.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

prior to April 1, 1947

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Globe Models GC-1A and GC-1B Aircraft with serial numbers 3 to 408 Inclusive; 1004 to 1319 Inclusive; and 2001 to 2239 Inclusive.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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