AD 2004-06-51

final rule
Data completeness: 70%

Airworthiness Directives; Boeing Defense and Space Group Model 234 Helicopters

AD Number
2004-06-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2004-SW-09-AD
FR Citation
69 FR 31287

Applicability

TypeManufacturerModelDetails
aircraft Boeing Defense and Space Group Model 234 Airworthiness Directives; Boeing Defense and Space Group Model 234 Helicopters

Unsafe Condition

Crack in the upper shaft extension of the aft vertical shaft assembly, which could result in catastrophic failure of the assembly and subsequent loss of control of the helicopter.

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

Required Actions

Before further flight, inspect the upper shaft extension for a crack and modify the assembly. Thereafter, inspect the upper shaft extension for any crack before the first flight of each day. If any crack is found, replace the assembly with an airworthy assembly before further flight.

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

Compliance Time

Before further flight

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

Affected Aircraft

Boeing Defense and Space Group Model 234 helicopters with aft vertical shaft assembly, part number 234D3300, serial number-181 or lower with a prefix of A, installed, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 6, 2026

Rights: U.S. Government Public Domain

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