AD 47-06-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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.
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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
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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.
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Federal Register Abstract
Landing Gear Retraction Placard
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_47-06-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-06-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft Subject: Landing Gear Retraction Placard Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Swift Museum Foundation, Inc. Model: GC-1A | GC-1B Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-06-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-06-02 SUBJECT HEADING: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 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.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_47-06-02.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 47-06-02 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft Subject: Landing Gear Retraction Placard Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Swift Museum Foundation, Inc. Model: GC-1A | GC-1B Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 47-06-02 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 47-06-02 SUBJECT HEADING: Airworthiness Directives; Globe Models GC-1A and GC-1B Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 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.) FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.
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