Airworthiness Directive

AD 95-01-08 60 FR 2493

Federal Aviation Administration · 14 CFR part 39

FR document
95-518
Amendment
39-9119
Published
1995-01-10
Models covered
1
Last live check
2026-08-18
AD

95-01-08

FR doc 95-518 · 60 FR 2493

AD 95-01-08Published 1995-01-10Effective 1995-02-20

Requires repetitively inspecting the rudder pedal adjusting mounting bracket for cracks on Jetstream Aircraft Limited (JAL) HP137 Mk1 and Jetstream Series 200 airplanes, and replacing any cracked bracket.

Full official abstract

This amendment supersedes AD 81-09-03 R1, which currently requires repetitively inspecting the rudder pedal adjusting mounting bracket for cracks on Jetstream Aircraft Limited (JAL) HP137 Mk1 and Jetstream Series 200 airplanes, and replacing any cracked bracket. The Federal Aviation Administration's policy on aging commuter-class aircraft is to eliminate, or in certain instances, reduce the number of repetitions of certain short-interval inspections when improved parts or modifications are available. This action requires replacing the mounting bracket with a new mounting bracket of improved design as terminating action for the repetitive inspections that are currently required by AD 81-09-03 R1. The actions specified by this AD are intended to prevent inadvertent rudder movement caused by a cracked rudder pedal adjusting bracket, which, if not detected and corrected, could result in loss of rudder control.

Applies to 1 model in our index