AD 2006-15-07

final rule
Data completeness: 70%

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

AD Number
2006-15-07
Status
final_rule
Effective Date
Product Category
propeller
Docket
Docket No. FAA-2006-23645
FR Citation
71 FR 41116

Applicability

TypeManufacturerModelDetails
aircraft Mitsubishi Heavy Industries Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition

Improper rigging and/or adjustment of the propeller feathering linkage, which could result in the inability of the linkage to pull the feather valve to function as designed, leading to asymmetric drag and control difficulties outside the operational envelope of the aircraft.

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

Required Actions

Incorporate text from the service information into the Limitations Section of the FAA-approved Airplane Flight Manual (AFM).

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

Mitsubishi Heavy Industries, Ltd. MU-2B series airplanes with Type Certificates A2PC and A10SW, including specific models and serial numbers as listed in the AD.

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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