AD 92-09-07

final rule
Data completeness: 70%

Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. (BHTI) Model 206A and 206B Helicopters

AD Number
92-09-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
91-ASW-33
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron Canada Limited 206A Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. (BHTI) Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. (BHTI) Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. (BHTI) Model 206A and 206B Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B-1 Airworthiness Directives; BELL HELICOPTER TEXTRON, INC. (BHTI) Model 206A and 206B Helicopters

Unsafe Condition

Failure of the vertical fin supports, which could result in loss of the vertical fin and loss of control of the helicopter.

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

Required Actions

Inspect for cracks and modify the vertical fin supports in accordance with Part I of Bell Helicopter Alert Service Bulletin No. 206-91-60. Inspect for gaps between the tailboom and fin mounted inserts and comply with Part II of the same service bulletin if gaps are found. The inspections and modifications must be done per the referenced service bulletin.

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

Compliance Time

within 30 days or 100 hours' time in service, whichever comes first, after the effective date of this AD

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

Affected Aircraft

Bell Helicopter Textron, Inc. Model 206A and 206B helicopters, serial numbers 4 through 1163, equipped with a vertical fin assembly having an external doubler part number 206-020-113-109 on the lefthand side adjacent to the supports.

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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