AD 62-06-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Brantly International, Inc. | B-2 | Airworthiness Directives; BRANTLY Model B-2 Helicopters |
| aircraft | Brantly International, Inc. | B-2A | Airworthiness Directives; BRANTLY Model B-2 Helicopters |
| aircraft | Brantly International, Inc. | B-2B | Airworthiness Directives; BRANTLY Model B-2 Helicopters |
Unsafe Condition
Sudden movement of the seat backs to the full aft adjustment position due to the seat back adjustment wire P/N B2-334-32.
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Required Actions
Remove the seat back adjustment wire P/N B2-334-32 from the left and right seat backs.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 10 hours' time in service after the effective date of this AD
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Affected Aircraft
Brantly International, Inc. Model B-2 Helicopters equipped with seat back adjustment wire P/N B2-334-32.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Seat Back Adjustment
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_62-06-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 62-06-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRANTLY Model B-2 Helicopters Subject: Seat Back Adjustment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/23/1962 Make: Brantly International, Inc. Model: B-2 | B-2A | B-2B Product Type: Aircraft Product Subtype: Rotorcraft Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 62-06-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 62-06-01 SUBJECT HEADING: Airworthiness Directives; BRANTLY Model B-2 Helicopters ACTION: SUMMARY: DATES: Effective March 23, 1962. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 62-06-01 BRANTLY: Amdt. 410 Part 507 Federal Register March 16, 1962. Applies to All Model B-2 Helicopters Equipped With Seat Back Adjustment Wire P/N B2-334-32. Compliance required within the next 10 hours' time in service after the effective date of this AD. To prevent the sudden movement of the seat backs to the full aft adjustment position, the following must be accomplished: Remove the seat back adjustment wire P/N B2-334-32 from the left and right seat backs. This directive effective March 23, 1962. FOOTER:
Document Text
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AD Final Rules - DRS_62-06-01.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 62-06-01 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; BRANTLY Model B-2 Helicopters Subject: Seat Back Adjustment Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 03/23/1962 Make: Brantly International, Inc. Model: B-2 | B-2A | B-2B Product Type: Aircraft Product Subtype: Rotorcraft Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 62-06-01 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: AD NUMBER: 62-06-01 SUBJECT HEADING: Airworthiness Directives; BRANTLY Model B-2 Helicopters ACTION: SUMMARY: DATES: Effective March 23, 1962. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 62-06-01 BRANTLY: Amdt. 410 Part 507 Federal Register March 16, 1962. Applies to All Model B-2 Helicopters Equipped With Seat Back Adjustment Wire P/N B2-334-32. Compliance required within the next 10 hours' time in service after the effective date of this AD. To prevent the sudden movement of the seat backs to the full aft adjustment position, the following must be accomplished: Remove the seat back adjustment wire P/N B2-334-32 from the left and right seat backs. This directive effective March 23, 1962. FOOTER:
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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