Airworthiness Directive

AD 2002-12-01 67 FR 39843 Active

Federal Aviation Administration · 14 CFR part 39

FR document
02-14410
Amendment
39-12773
Published
2002-06-11
Effective
2002-07-16
Models covered
1
Last live check
2026-10-03
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AD

2002-12-01

FR doc 02-14410 · 67 FR 39843

AD 2002-12-01Published 2002-06-11Effective 2002-07-16

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

Requires a functional test of the shortening mechanism of the nose landing gear for free movement of the capsule in the upper and lower bearings, and corrective action, if necessary.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain BAE Systems (Operations) Limited (Jetstream) Model 4101 airplanes, that requires a functional test of the shortening mechanism of the nose landing gear for free movement of the capsule in the upper and lower bearings, and corrective action, if necessary. This action is necessary to prevent damage to the capsule, which could result in inability to extend the nose landing gear in normal or emergency situations, and consequent injury to passengers and flight crew. This action is intended to address the identified unsafe condition.

More directives for British Aerospace Jetstream 41

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  2. AD 2009-10-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-05-07
  3. AD 2009-02-07 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-26
  4. AD 2008-18-02 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-02-20
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All British Aerospace Jetstream 41 directives

Applies to 1 model in our index