AD 66-30-05

final rule
Data completeness: 70%

Airworthiness Directives; Fairchild Hiller Model FH-1100 Helicopters

AD Number
66-30-05
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft FH1100 Manufacturing Corporation FH-1100 Airworthiness Directives; Fairchild Hiller Model FH-1100 Helicopters

Unsafe Condition

Failure of the Bendix main engine drive shaft, which occurred with less than 15 hours total time on the shaft.

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

Required Actions

Remove the Bendix main engine drive shaft P/N 19E49-4 and install Bendix shaft P/N 19E49X3 or 19E49-3 or an equivalent approved by the Chief, Aircraft Engineering Division, FAA Western Region, Los Angeles, California.

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

Fairchild Hiller Model FH-1100 Helicopters with Bendix main engine drive shaft P/N 19E49-4.

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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