AD 80-18-04 R1

final rule
Data completeness: 70%

Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters

AD Number
80-18-04 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
80-ASW-28
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Bell Helicopter Textron Canada Limited 206A Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206A-1 (OH-58A) Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206B-1 Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206L Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters
aircraft Bell Helicopter Textron Canada Limited 206L-1 Airworthiness Directives; BELL Models 206A, 206B, 206A-1, 206B-1, 206L, and 206L-1 Helicopters

Unsafe Condition

Failure of the main rotor trunnion due to fatigue cracks in parts numbered 206-010-104-3, 206-011-113-001, or 206-011-120-001.

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

Required Actions

Accomplish magnetic particle inspections per Bell Helicopter Textron Alert Service Bulletins 206-80-7/206L-80-9 or FAA-approved equivalent. Inspections must be done within specified intervals based on trunnion time in service: trunnions with <1,100 hours must inspect before 1,200 and 2,400 hours, then every 600 hours. Trunnions with 1,100-1,700 hours or unknown time must inspect within next 100 hours, then every 600 hours. Replace trunnion if cracks found before further flight. Report cracks to FAA as specified.

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

Compliance Time

Compliance required as indicated in the AD, with specific inspection timelines based on trunnion time in service as of the effective date (November 24, 1980).

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

Affected Aircraft

Bell Helicopter Textron Canada Limited Models 206A, 206B, 206A-1, 206B-1, 206L, 206L-1 helicopters equipped with main rotor trunnions P/N 206-010-104-3, 206-011-113-001, or 206-011-120-001.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.