AD 95-01-08
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | British Aerospace Regional Aircraft | H.P. 137 Jetstream Mk. 1 | Airworthiness Directives; Jetstream Aircraft Limited (formerly British Aerospace, Regional Airlines Limited) HP137 Mk1 and Jetstream Series 200 Airplanes |
| aircraft | British Aerospace Regional Aircraft | Jetstream Series 200 | Airworthiness Directives; Jetstream Aircraft Limited (formerly British Aerospace, Regional Airlines Limited) HP137 Mk1 and Jetstream Series 200 Airplanes |
Unsafe Condition
Cracked rudder pedal adjusting mounting bracket could cause inadvertent rudder movement, resulting in loss of rudder control.
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Required Actions
Within 100 hours time-in-service after the effective date, inspect the rudder pedal adjusting mounting bracket for cracks per SB No. 9/10. If cracks found, replace with improved part P/N 1379111E 1 (Modification No. 5162) before further flight. If no cracks, reinspect at intervals not exceeding 100 hours TIS until Modification No. 5162 is incorporated. By 15,000 hours TIS or within 200 hours TIS after effective date (whichever is later), replace the bracket with P/N 1379111E 1. Incorporating Modification No. 5162 eliminates repetitive inspections.
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Compliance Time
Within the next 100 hours time-in-service after the effective date (for inspection), and within the next 200 hours time-in-service after the effective date or upon accumulation of 15,000 hours time-in-service, whichever occurs later (for replacement).
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Affected Aircraft
Jetstream Aircraft Limited HP137 Mk1 and Jetstream Series 200 airplanes (all serial numbers), 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 8, 2026
Rights: U.S. Government Public Domain
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