# Proposed AD FAA-2008-1214: BAE Systems (Operations) Limited (Jetstream) Model 4101 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2009-10-02
- Products: BAE Systems
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: November 17, 2008, 73 FR 67817
- Comments due: December 17, 2008
- Became: [AD 2009-10-02](https://openairdocs.org/ad/2009-10-02)
- Docket: FAA-2008-1214 (https://www.regulations.gov/docket/FAA-2008-1214, where comments are filed)
- Project: 2007-NM-259-AD
- FR document: E8-27161
- Official PDF: https://openairdocs.org/files/sha256/49/e0/49e004f7d07084f48ba8d04095aed900abfff61a37db55381c1c5eaae8a5d942 (from https://www.govinfo.gov/content/pkg/FR-2008-11-17/pdf/E8-27161.pdf)
- Federal Register: https://www.federalregister.gov/documents/2008/11/17/E8-27161/airworthiness-directives-bae-systems-operations-limited-jetstream-model-4101-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/FF006A5423DD68C4862575040070D7EA.0001
- Page: https://openairdocs.org/proposed/FAA-2008-1214

## Summary

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to all BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes. The existing AD currently requires operators to determine the number of flight cycles accumulated on each component of the main landing gear (MLG) and the nose landing gear (NLG), and to replace each component that reaches its life limit with a serviceable component. The existing AD also requires operators to revise the Airworthiness Limitations (AWL) section of the Instructions for Continued Airworthiness (ICA) in the aircraft maintenance manual to reflect the new life limits for structurally significant items. This proposed AD would require a new revision of the AWL section of the ICA to incorporate revised life limits for structurally significant items, operational and functional tests of certain systems, and instructions to retain critical ignition source prevention features during configuration changes. This proposedAD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country. We are proposing this AD to prevent failure of certain structurally significant items, including the MLG and the NLG, which could result in reduced structural integrity of the airplane; and to prevent fuel vapor ignition sources, which could result in fuel tank explosion and consequent loss of the airplane.

## Notices in this docket

- Nov 17, 2008: Notice of proposed rulemaking (NPRM). (first notice), FR document E8-27161, comments due Dec 17, 2008 (https://www.federalregister.gov/documents/2008/11/17/E8-27161/airworthiness-directives-bae-systems-operations-limited-jetstream-model-4101-airplanes)

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