AD 2000-22-16

final rule
Data completeness: 70%

Airworthiness Directives; British Aerospace (Jetstream) Model 4101 Airplanes

AD Number
2000-22-16
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2000-NM-152-AD
FR Citation
65 FR 66927

Applicability

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

Unsafe Condition

Restricted movement of the rudder pedals due to structural interference, which could result in reduced controllability of the airplane.

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

Required Actions

Perform a functional check of the left and right rudder pedals to ensure full and free movement at all rudder pedal positions. If any restriction is found, modify the forward pedal boxes, including moving the rudder pedals and measuring clearances between the rod attachment bolt and the flange of the floor channel, correcting any incorrect clearances, and repeating the functional check.

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

Compliance Time

Functional check within 60 days after the effective date; modification within 8 months after the effective date.

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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