AD 84-10-51 R1

final rule
Data completeness: 70%

Airworthiness Directives; BOEING VERTOL COMPANY Model 234 Series Helicopters

AD Number
84-10-51 R1
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft Columbia Helicopters, Inc. 234 Airworthiness Directives; BOEING VERTOL COMPANY Model 234 Series Helicopters

Unsafe Condition

Cracking of the forward main rotor drive shaft could cause possible hazards in flight.

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

Required Actions

Inspect the rotor drive shaft within 70 hours time in service after the effective date or upon 1,600 total hours on the shaft, whichever is later. Subsequent inspections must be done at intervals not exceeding 35 hours time in service. Remove and replace cracked shafts before further flight. Use Service Bulletin 234-63-1009 or equivalent method approved by the FAA.

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

Compliance Time

Within 70 hours time in service after the effective date of this amendment or upon accumulation of 1,600 total hours time in service on the rotor shaft, whichever occurs later, and thereafter at intervals not to exceed 35 hours time in service from the last inspection

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

Affected Aircraft

BOEING VERTOL COMPANY Model 234 series helicopters equipped with forward main rotor drive shaft P/N 114D1245-7

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.