CTHIn ForceLegislation
AD/J4100/23 - Nose Landing Gear Wheel Outer Cone
BAe Systems (Operations) Jetstream 4100 BAe Systems (Operations) Jetstream 4100 Series Aeroplanes
Start here
Get a plain-English read of BAe Systems (Operations) Jetstream 4100
Turn the raw legal text into a practical explanation grounded in AD/J4100/23 - Nose Landing Gear Wheel Outer Cone.
BAe Systems (Operations) Jetstream 4100 Series Aeroplanes
| AD/J4100/23 | Nose Landing Gear Wheel Outer Cone | 4/2008 |
|---|
| Applicability: | All Model Jetstream Series 4100 aircraft, all serial numbers. |
|---|---|
| Requirement: | Action in accordance with the requirements of EASA AD 2008-0036.Note: BAE SYSTEMS (Operations) Limited Service Bulletin J41-32-086 original issue, or later EASA approved revision, refers. |
| Compliance: | As specified in the Requirement document, with a revised effective date of10 April 2008. |
| This Airworthiness Directive becomes effective on 10 April 2008. | |
| Background: | A failure mode has been identified following the examination of parts from a Jetstream 4100 Series aircraft, that can lead to the loss of a nose wheel. A combination of excessive wear and/or adverse tolerances on the axle inner cone, outer cone or wheel hub splined sleeve cones results in the loss of the critical gap between the inner flange face of the wheel outer cone and the axle end face. This condition, if not corrected, can cause the wheel nut lock plate to break, leading to the wheel retention nut unscrewing and subsequent separation of the nose wheel from the NLG axle. |
Image unavailable in extracted text
David Villiers
Delegate of the Civil Aviation Safety Authority
28 February 2008