# Proposed AD FAA-2006-25391: Fokker Model F.28 Mark 0070 and 0100 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2007-04-23
- Products: Fokker Services B.V.
- Product type: Aircraft
- Action: Supplemental notice of proposed rulemaking (NPRM); reopening of comment period.
- Published: December 28, 2006, 71 FR 78107
- Comments due: January 22, 2007
- Became: [AD 2007-04-23](https://openairdocs.org/ad/2007-04-23)
- Docket: FAA-2006-25391 (https://www.regulations.gov/docket/FAA-2006-25391, where comments are filed)
- Project: 2006-NM-097-AD
- FR document: E6-22279
- Official PDF: https://openairdocs.org/files/sha256/0d/0b/0d0bad5681af9bd27c7f8751d8033b356b7098d77f83220cb7f4f04afcbf0184 (from https://www.govinfo.gov/content/pkg/FR-2006-12-28/pdf/E6-22279.pdf)
- Federal Register: https://www.federalregister.gov/documents/2006/12/28/E6-22279/airworthiness-directives-fokker-model-f28-mark-0070-and-0100-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EE0E7371E6C6B4A0862572520059D9C2.0001
- Page: https://openairdocs.org/proposed/FAA-2006-25391

## Summary

The FAA is revising an earlier NPRM for an airworthiness directive (AD) that applies to certain Fokker Model F.28 Mark 0070 and 0100 airplanes. The original NPRM would have superseded an existing AD that currently requires a one-time inspection of the sliding members in the main landing gear (MLG) for cracking and replacement of the sliding members with serviceable parts if necessary. The original NPRM proposed to require repetitive magnetic particle inspections of the sliding members of the MLG for cracking and corrective actions as necessary. The original NPRM resulted from inspection findings that have shown repetitive inspections are needed to establish fleet safety. This new action revises the original NPRM by correcting a certain part number in the applicability. We are proposing this supplemental NPRM to detect and correct fatigue cracking of the sliding member, which could result in possible separation of the MLG from the airplane and consequent reduced controllabilityof the airplane upon landing and possible injury to passengers.

## Notices in this docket

- Jul 19, 2006: Notice of proposed rulemaking (NPRM). (first notice), FR document E6-11416, comments due Aug 18, 2006 (https://www.federalregister.gov/documents/2006/07/19/E6-11416/airworthiness-directives-fokker-model-f28-mark-0070-and-0100-airplanes)
- Dec 28, 2006: Supplemental notice of proposed rulemaking (NPRM); reopening of comment period., FR document E6-22279, comments due Jan 22, 2007 (https://www.federalregister.gov/documents/2006/12/28/E6-22279/airworthiness-directives-fokker-model-f28-mark-0070-and-0100-airplanes)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.
