Airworthiness Directive

AD 2000-22-16 65 FR 66927 Active

Federal Aviation Administration · 14 CFR part 39

FR document
00-28232
Amendment
39-11963
Published
2000-11-08
Effective
2000-12-13
Models covered
1
Last live check
2026-10-03
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AD

2000-22-16

FR doc 00-28232 · 65 FR 66927

AD 2000-22-16Published 2000-11-08Effective 2000-12-13

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 check of the rudder pedals to ensure full and free movement at all rudder pedal positions, and modification of the forward rudder pedal boxes.

Full official abstract

This amendment adopts a new airworthiness directive (AD), applicable to all British Aerospace (Jetstream) Model 4101 airplanes, that requires a functional check of the rudder pedals to ensure full and free movement at all rudder pedal positions, and modification of the forward rudder pedal boxes. The actions specified by this AD are intended to prevent restricted movement of the rudder pedals due to structural interference, which could result in reduced controllability of the airplane. This action is intended to address the identified unsafe condition.

More directives for British Aerospace Jetstream 41

  1. AD 2009-16-01 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2009-08-05
  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
  5. AD 2008-17-04 Airworthiness Directives; BAE Systems (Operations) Limited (Jetstream) M... 2008-08-19

All British Aerospace Jetstream 41 directives

Applies to 1 model in our index