AD 2008-13-28

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers

AD Number
2008-13-28
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2008-0254
FR Citation
73 FR 37791

Applicability

TypeManufacturerModelDetails
aircraft Piper Aircraft Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers
aircraft Beechcraft Corporation Model 76 Duchess Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers
engine Lycoming Engines LIO-360 series and LO-360 series reciprocating Airworthiness Directives; Hartzell Propeller Inc. ( )HC-( )(2,3)Y(K,R)-2 Two- and Three-Bladed Compact Series Propellers

Unsafe Condition

Propeller hub cracks initiating from the lubrication holes, leading to blade separation and potential loss of control of the airplane.

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

Required Actions

Perform initial and repetitive eddy current inspections (ECI) of the area around the lubrication holes of the hub blade sockets. Use the procedures described in Hartzell Propeller Inc. Alert Service Bulletin (ASB) No. HC-ASB-61-297, Revision 1.

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

Compliance Time

Within 50 hours time-in-service (TIS) or 12 months after the effective date of the AD, whichever occurs first, for initial ECI. Repetitive ECIs must be performed within 50-hour TIS intervals or within 12 months from the previous ECI, whichever occurs first.

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

Affected Aircraft

Hartzell Propeller Inc. left-hand rotating ( )HC-( )(2,3)Y(K,R)-2 two- and three-bladed, aluminum hub, 'compact' series propellers, with hubs having a non-suffix serial number and lubrication holes located on the shoulder of the hub blade socket. These propellers are installed on Lycoming Engines LIO-360 series and LO-360 series reciprocating engines, installed on Piper Aircraft, Inc. Seneca PA-34-200 and Seminole PA-44-180, and Hawker Beechcraft Corporation Model 76 Duchess airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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