AD 2001-26-05

final rule
Data completeness: 70%

Airworthiness Directives; Hamilton Sundstrand Model 247F Propellers

AD Number
2001-26-05
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. 2001-NE-40-AD
FR Citation
66 FR 67074

Unsafe Condition

Partial slippage at the bond joint between the blade tulip and the composite blade airfoil interface due to debonding.

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

Required Actions

Remove all four existing propeller blades (P/N's R810640-1, R810640-2, and R810640-3) from service, replace them with serviceable propeller blades, and mark the propeller with a new part number.

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Compliance Time

Within 30 days of the effective date of this AD.

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Affected Aircraft

Hamilton Sundstrand Model 247F propellers, part numbers 810610-1 and 815550-1, installed on, but not limited to, Aerospatiale ATR-72 and Xian MA-60 airplanes.

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

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