Airworthiness Directive

AD 95-26-10 61 FR 622 Active

Federal Aviation Administration · 14 CFR part 39

FR document
96-269
Published
1996-01-09
Effective
1996-02-08
Models covered
1
Last live check
2026-10-03
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AD

95-26-10

FR doc 96-269 · 61 FR 622

AD 95-26-10Published 1996-01-09Effective 1996-02-08

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 repetitive purging of the hydraulic system and installation of a spoiler actuator that has been previously certified.

Full official abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Jetstream Model 4101 airplanes, that currently requires repetitive purging of the hydraulic system and installation of a spoiler actuator that has been previously certified. That AD was prompted by a report of damage to the locking mechanisms on some pistons of the spoiler actuators. The actions specified by the AD are intended to prevent uncommanded extension of the lift spoiler in the event of loss of hydraulic pressure in the spoiler actuator. This amendment establishes an increased life limit for certain spoiler actuators, and provides an optional terminating action for the requirements of that AD. This amendment also limits the applicability of the rule to fewer airplanes.

More directives for British Aerospace Jetstream 41

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  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