Airworthiness Directive

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Federal Aviation Administration

14 CFR Part 39

Amendment 39-4408; AD 82-06-11 R1

Airworthiness Directives; Piper Model PA-28R-201T, PA-28RT-201T, PA-28R-200, PA-28R-201, and PA-28RT-201 Airplanes
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AGENCY: Federal Aviation Administration, DOT

DATES: Effective June 16, 1982.

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82-06-11 R1 PIPER AIRCRAFT CORPORATION: Amendment 39-4349 as amended by Amendment 39-4408. Applies to the following airplanes certificated in any category.
Nose Landing Gear Inspection and Rigging
(Part I of Service Bulletin)

PA-28R-201T Turbo Arrow III28R-7703001 through 28R-7803373
PA-28RT-201T Turbo Arrow IV28R-7931001 through 28R-8131193
Nose Landing Gear Inspection and Modification
(Part II of Service Bulletin)

PA-28R-200 Arrow II28R-7635522 through 28R-7635545
PA-28R-201 Arrow III28R-7737001 through 28R-7837317
PA-28RT-201 Arrow IV28R-7918001 through 28R-8118082

COMPLIANCE: Required as indicated, unless already accomplished.

To prevent the inadvertent retraction of the nose landing gear, accomplish the following:

A) Within the next 100 hours time-in-service after the effective date of this AD, inspect, rig and modify the nose landing gear in accordance with Piper Service Bulletin No. 724A, dated April 20, 1982, Parts I and II as applicable, except dye penetrant must be used for detection of cracks.

B) Record compliance with this AD by an appropriate entry in the airplane maintenance records. This includes those airplanes where the provisions of this AD have already been accomplished.

C) Airplanes may be flown in accordance with FAR 21.197 to a location where this AD may be accomplished.

D) An equivalent method of compliance may be used when approved by the Chief, Aircraft Certification Field Office, FAA, 3400 Norman Berry Drive, East Point, Georgia 30344.

Amendment 39-4349 became effective on March 25, 1982.

This amendment 39-4408 becomes effective on June 16, 1982.