# Proposed AD 98-CE-47-AD: Mooney Aircraft Corporation Models M20J, M20K, M20M, and M20R Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 98-21-26
- Action: Notice of proposed rulemaking (NPRM).
- Published: June 17, 1998, 63 FR 33016
- Comments due: August 21, 1998
- Became: [AD 98-21-26](https://openairdocs.org/ad/98-21-26)
- Docket: 98-CE-47-AD
- FR document: 98-16025
- Official PDF: https://openairdocs.org/files/sha256/e5/48/e548a2c8a83cb1bb5594f66292c3199bc0dcc0692d6a1f1212d21cd7b336e8c6 (from https://www.govinfo.gov/content/pkg/FR-1998-06-17/pdf/98-16025.pdf)
- Federal Register: https://www.federalregister.gov/documents/1998/06/17/98-16025/airworthiness-directives-mooney-aircraft-corporation-models-m20j-m20k-m20m-and-m20r-airplanes
- Page: https://openairdocs.org/proposed/98-CE-47-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to certain Mooney Aircraft Corporation (Mooney) Models M20J, M20K, M20M, and M20R airplanes. The proposed AD would require grinding the surface of the main landing gear (MLG) leg bracket, inspecting this area for cracks, and replacing any cracked MLG leg bracket. The proposed AD is the result of the manufacturing of several of the MLG leg brackets using laser pattern cutting. The brackets, when manufactured using this process, develop minor cracks at the bends, which could propagate over time. The actions specified by the proposed AD are intended to prevent failure of the MLG side brace bolt caused by cracking of the MLG leg bracket, which could result in MLG collapse with consequent loss of control of the airplane during taxi, takeoff, or landing operations.

## Notices in this docket

- Jun 17, 1998: Notice of proposed rulemaking (NPRM). (first notice), FR document 98-16025, comments due Aug 21, 1998 (https://www.federalregister.gov/documents/1998/06/17/98-16025/airworthiness-directives-mooney-aircraft-corporation-models-m20j-m20k-m20m-and-m20r-airplanes)

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