NPRM 93-CE-61-AD

Became AD 95-20-07

Proposed airworthiness directive · Airworthiness Directives; Piper Aircraft Corporation PA24, PA28R, PA30, PA32R, PA32RT, PA34-200, PA34-200T, PA39, and PA44 Series Airplanes

Published
February 22, 1995 · 60 FR 9799
Comments due
May 5, 1995
Action
Notice of proposed rulemaking (NPRM)
Docket
93-CE-61-AD
FR document
95-4251

A proposal is not in force. If adopted, it becomes an AD, usually with changes. Only the Federal Register edition is official.

Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Piper Aircraft Corporation (Piper) PA24, PA28R, PA30, PA32R, PA32RT, PA34-200, PA34-200T, PA39, and PA44 series airplanes. The proposed action would require repetitively inspecting the main gear side brace studs for cracks and replacing any cracked main gear side brace stud. Several reports of main gear side brace stud cracks on the affected airplanes, including seven incidents where the main landing gear (MLG) collapsed, prompted the proposed AD. The actions specified by the proposed AD are intended to prevent a MLG collapse caused by main gear side brace stud cracks, which, if not detected and corrected, could result in loss of control of the airplane during landing operations.

The resulting AD

Notices in this docket · 1