# Proposed AD FAA-2009-0198: Fokker Model F.28 Mark 0100 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2009-13-02
- Products: Fokker Services B.V.
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: March 6, 2009, 74 FR 9774
- Comments due: April 6, 2009
- Became: [AD 2009-13-02](https://openairdocs.org/ad/2009-13-02)
- Docket: FAA-2009-0198 (https://www.regulations.gov/docket/FAA-2009-0198, where comments are filed)
- Project: 2008-NM-129-AD
- FR document: E9-4731
- Official PDF: https://openairdocs.org/files/sha256/3d/fd/3dfdba2328dd783ddc5c7f731a44910289135e6910f3990b799089925f056c37 (from https://www.govinfo.gov/content/pkg/FR-2009-03-06/pdf/E9-4731.pdf)
- Federal Register: https://www.federalregister.gov/documents/2009/03/06/E9-4731/airworthiness-directives-fokker-model-f28-mark-0100-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DE3B1D6CB01DE3C586257571004DF999.0001
- Page: https://openairdocs.org/proposed/FAA-2009-0198

## Summary

The FAA proposes to supersede an existing airworthiness directive (AD) that applies to certain Fokker Model F.28 Mark 0100 airplanes. The existing AD currently requires revisions to the airplane flight manual (AFM) to include procedures to prohibit use of reverse engine thrust power settings between idle and emergency maximum and to prohibit stabilized engine operation in a certain engine speed range on the ground. This proposed AD would continue to require revising the AFM to include certain procedures. This proposed AD would also require removing the normal maximum (second) detent for the reverse-thrust control. In addition, this proposed AD would require revising the AFM to prohibit use of reverse thrust in flight and to limit operation of Max Reverse thrust. This proposed AD results from issuance of mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product.We are proposing this AD to prevent inadvertent operation in the prohibited stabilized engine speed range on the ground, which could result in uncontained engine fan blade failure due to high cycle fatigue cracking.

## Notices in this docket

- Mar 6, 2009: Notice of proposed rulemaking (NPRM). (first notice), FR document E9-4731, comments due Apr 6, 2009 (https://www.federalregister.gov/documents/2009/03/06/E9-4731/airworthiness-directives-fokker-model-f28-mark-0100-airplanes)

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