AD 98-05-07

final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

AD Number
98-05-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
97-NM-143-AD
FR Citation
Federal Register: March 06, 1998 (Volume 63, Number 44)

Applicability

TypeManufacturerModelDetails
aircraft BAE Systems (Operations) Limited Jetstream Model 4101 Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

Unsafe Condition

The fuselage structure at the stringer joint at station 130 on the left side of the airplane could crack, which could result in rapid decompression of the airplane at the forward fuselage area.

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Required Actions

Replace the stringer joint pieces at four positions at station 130 on the left side of the airplane with new, improved parts in accordance with Jetstream Service Bulletin J41-53-039. An alternative method of compliance may be used if approved by the FAA.

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Compliance Time

Within 6,000 flight hours after the effective date of this AD

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Affected Aircraft

British Aerospace (Jetstream) Model 4101 airplanes, constructors numbers 41081 through 41091 inclusive

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Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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