AD 2004-12-10

final rule
Data completeness: 70%

Airworthiness Directives; Hamilton Sundstrand Corporation (Formerly Hamilton Standard Division) Model 568F Propellers

AD Number
2004-12-10
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. 2003-NE-48-AD
FR Citation
69 FR 32855

Unsafe Condition

Reports of propeller blades found at inspection with random areas of missing adhesive under the compression wrap, which exposed the steel tulip part of the blade, leading to potential corrosion-induced fatigue and blade separation.

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

Required Actions

Remove propeller blades, part numbers R815505-3 and R815505-4, with serial numbers FR1699 through FR2625 and FR20010610 through FR20021010, from service and replace them with serviceable blades according to the specified schedule.

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

Compliance Time

Within the compliance times specified in Table 1 of the AD, with some blades due by December 31, 2007.

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

Affected Aircraft

Hamilton Sundstrand Corporation (formerly Hamilton Standard Division) Model 568F propellers with propeller blades, part numbers R815505-3 and R815505-4, serial numbers FR1699 through FR2625 and FR20010610 through FR20021010, installed on, but not limited to, Aerospatiale ATR42-400, ATR42-500, ATR72-212, and ATR72-500 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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