AD 2001-03-12

Recurring final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

AD Number
2001-03-12
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-224-AD
FR Citation
66 FR 10953

Applicability

TypeManufacturerModelDetails
aircraft British Aerospace (Jetstream) Model 4101 Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

Unsafe Condition

Elevator cable tension regulators becoming detached from the splined shaft of the assembly, which could result in difficulty adjusting the elevators, leading to reduced controllability of the airplane.

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

Required Actions

Inspect the elevator cable tension regulator lever assembly to detect discrepancies, including looseness and migration along the splines, within 7 weeks after February 1, 2000. Repeat inspections at intervals not exceeding 1,500 flight hours until the modification is completed. Modify the elevator cable tension regulators in accordance with Jetstream Service Bulletin J41-27-059 within 12 months after the effective date of this AD.

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

Compliance Time

Within 12 months after the effective date of this AD.

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

Affected Aircraft

All British Aerospace (Jetstream) Model 4101 airplanes, certificated in any category.

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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