# Proposed AD 95-NM-164-AD: Fokker Model F28 Mark 0100 Series Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 96-12-19
- Action: Notice of proposed rulemaking (NPRM).
- Published: January 19, 1996, 61 FR 1294
- Comments due: February 21, 1996
- Became: [AD 96-12-19](https://openairdocs.org/ad/96-12-19)
- Docket: 95-NM-164-AD
- FR document: 96-492
- Official PDF: https://openairdocs.org/files/sha256/b7/a4/b7a45d6e49d01843b36e012e2d10256ff7cd7efb2113720fdface492bb78abb9 (from https://www.govinfo.gov/content/pkg/FR-1996-01-19/pdf/96-492.pdf)
- Federal Register: https://www.federalregister.gov/documents/1996/01/19/96-492/airworthiness-directives-fokker-model-f28-mark-0100-series-airplanes
- Page: https://openairdocs.org/proposed/95-NM-164-AD

## Summary

This document proposes the adoption of a new airworthiness directive (AD) that is applicable to certain Fokker Model F28 Mark 0100 series airplanes. This proposal would require installation of reinforcement plates under each hook latch fitting on the frame of each large cargo door. For some airplanes, this proposal would require inspection to detect cracking in the area around each hook latch fitting, and repair, if necessary. This proposal is prompted by the results of stress analyses and destructive tests which revealed that fatigue-related cracking may develop in the vicinity of the hook latch fittings on the frame of the large cargo doors. The actions specified by the proposed AD are intended to prevent reduced structural integrity of the frames of the cargo door due to fatigue cracking, which may lead to the cargo door(s) opening while the airplane is in flight.

## Notices in this docket

- Jan 19, 1996: Notice of proposed rulemaking (NPRM). (first notice), FR document 96-492, comments due Feb 21, 1996 (https://www.federalregister.gov/documents/1996/01/19/96-492/airworthiness-directives-fokker-model-f28-mark-0100-series-airplanes)

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