AD 2015-01-02

final rule
Data completeness: 70%

Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

AD Number
2015-01-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2014-0108
FR Citation
80 FR 3164

Applicability

TypeManufacturerModelDetails
aircraft Mitsubishi Heavy Industries Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes
aircraft Aviat Various Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Airplanes

Unsafe Condition

Stress corrosion cracking in the flanges of the airframe at stations 4610 and 5605.

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

Required Actions

Inspect the flanges of the airframe at stations 4610 and 5605 for stress corrosion cracking. Revise the maintenance manual to include instructions for accessing and inspecting these difficult-to-reach areas.

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. Models MU-2B-30, MU-2B-35, MU-2B-36, MU-2B-36A, and MU-2B-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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