AD 2006-17-01

final rule
Data completeness: 70%

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

AD Number
2006-17-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2006-23883
FR Citation
71 FR 47699

Applicability

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

Unsafe Condition

Torque transducers that are out of calibration could result in degraded performance and poor handling qualities, leading to loss of control in certain situations.

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

Required Actions

Incorporate power assurance charts into the Limitations Section of the Airplane Flight Manual (AFM), inspect the engine torque indication system, and recalibrate the torque pressure transducers as required.

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

Compliance Time

Within 50 flight hours after the effective date of this AD.

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

Affected Aircraft

Mitsubishi Heavy Industries MU-2B series airplanes, including models MU-2B, MU-2B-10, MU-2B-15, MU-2B-20, MU-2B-25, MU-2B-26, MU-2B-30, MU-2B-35, MU-2B-36, MU-2B-25, MU-2B-26, MU-2B-26A, and MU-2B-40, with specific serial number ranges.

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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