AD 98-20-39

final rule
Data completeness: 70%

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

AD Number
98-20-39
Status
final_rule
Effective Date
Product Category
aircraft
Docket
98-CE-39-AD
FR Citation
Federal Register: October 01, 1998 (Volume 63, Number 190)

Applicability

TypeManufacturerModelDetails
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-10 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-15 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-20 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-25 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-26 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-26A Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-30 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-35 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes
aircraft Mitsubishi Heavy Industries, Ltd. MU-2B-36 Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. MU-2B Series Airplanes

Unsafe Condition

The wing tip tank may separate from the airplane because of an incorrect bolt corroding, which could result in loss of control of the airplane.

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

Required Actions

Inspect each forward attachment fitting bolt of the wing tip tanks to determine if any incorrect bolt is installed. Replace any incorrect bolt with P/N 017A-12887-5 or P/N 017A-12887-7 bolts prior to further flight. Identify P/N 017A-12887 or P/N 017A-12887-3 bolts with the letters 'SPL'.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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