AD 43-07-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Fairchild Hiller Corporation | M-62A | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62A-3 | Airworthiness Directives; Fairchild M-62 Series Aircraft |
| aircraft | Fairchild Hiller Corporation | M-62B | Airworthiness Directives; Fairchild M-62 Series Aircraft |
Unsafe Condition
Wood deterioration and weakened glue joints due to moisture accumulation in the wing center-section front and rear spars.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
At each periodic inspection, examine the wing center-section front and rear spars for wood deterioration and weakened glue joints. Follow Fairchild Service Maintenance Bulletin 45-62-1, dated March 10, 1945, for inspection methods and repairs if needed.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
At each periodic inspection
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Fairchild Hiller Corporation M-62A, M-62A-3, M-62B aircraft
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Wing Center Section Spars
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_43-07-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 43-07-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Fairchild M-62 Series Aircraft Subject: Wing Center Section Spars Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Fairchild Hiller Corporation Model: M-62A | M-62A-3 | M-62B Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 43-07-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 43-07-01 SUBJECT HEADING: Airworthiness Directives; Fairchild M-62 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 43-07-01 FAIRCHILD: (Was Service Note 2 of AD-724-2.) Applies to M-62 Series Aircraft. At each periodic inspection, examine the wing center-section front and rear spars for wood deterioration and weakened glue joints due to moisture accumulation. (Method of inspection and repair, if necessary, are covered in Fairchild Service Maintenance Bulletin 45-62- 1, dated March 10, 1945.) FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_43-07-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 43-07-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Fairchild M-62 Series Aircraft Subject: Wing Center Section Spars Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: Make: Fairchild Hiller Corporation Model: M-62A | M-62A-3 | M-62B 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: Updated RGL applicability to match AD applicability; CAR C-11-185 AIRWORTHINESS DIRECTIVES FINAL RULES: 43-07-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 43-07-01 SUBJECT HEADING: Airworthiness Directives; Fairchild M-62 Series Aircraft ACTION: SUMMARY: DATES: ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 43-07-01 FAIRCHILD: (Was Service Note 2 of AD-724-2.) Applies to M-62 Series Aircraft. At each periodic inspection, examine the wing center-section front and rear spars for wood deterioration and weakened glue joints due to moisture accumulation. (Method of inspection and repair, if necessary, are covered in Fairchild Service Maintenance Bulletin 45-62- 1, dated March 10, 1945.) 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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