Airworthiness Directive

AD 2003-07-06 68 FR 16195 Active

Federal Aviation Administration · 14 CFR part 39

FR document
03-7746
Amendment
39-13102
Published
2003-04-03
Effective
2003-05-22
Models covered
1
Last live check
2026-09-30
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AD

2003-07-06

FR doc 03-7746 · 68 FR 16195

AD 2003-07-06Published 2003-04-03Effective 2003-05-22

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 you to inspect the steering jack piston rod for cracks and replace if necessary; measure the torque setting of the steering jack piston rod end fitting and stop bolt; and measure the thickness of the tab washers.

Full official abstract

This amendment adopts a new airworthiness directive (AD) that applies to all British Aerospace Model HP.137 Jetstream Mk.1, Jetstream Series 200, Jetstream Series 3101, and Jetstream Model 3201 airplanes. This AD requires you to inspect the steering jack piston rod for cracks and replace if necessary; measure the torque setting of the steering jack piston rod end fitting and stop bolt; and measure the thickness of the tab washers. This AD also requires you to calculate a new safe life limit for the steering jack piston rod based on the results of the inspection and the measurements. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for the United Kingdom. The actions specified by this AD are intended to detect, correct, and prevent cracks in the steering jack piston rod, which could result in failure of the steering jack piston rod. Such failure could lead to loss of steering control of the airplane during takeoff, landing, and taxi operations.

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All British Aerospace Jetstream 31/32 directives

Applies to 1 model in our index