# Proposed AD 99-NE-35-AD: MT-Propeller Entwicklung GMBH Models MTV-9-B-C and MTV-3-B-C Propellers

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2002-23-09
- Products: MT-Propeller Entwicklung
- Product type: Propeller
- Action: Notice of proposed rulemaking (NPRM).
- Published: February 27, 2002, 67 FR 8910
- Comments due: April 29, 2002
- Became: [AD 2002-23-09](https://openairdocs.org/ad/2002-23-09)
- Docket: 99-NE-35-AD
- FR document: 02-4587
- Official PDF: https://openairdocs.org/files/sha256/ed/37/ed37f5a0c79007577553187ddc22d87c39b6aecfc8698ee8dc9523d07a47fa5f (from https://www.govinfo.gov/content/pkg/FR-2002-02-27/pdf/02-4587.pdf)
- Federal Register: https://www.federalregister.gov/documents/2002/02/27/02-4587/airworthiness-directives-mt-propeller-entwicklung-gmbh-models-mtv-9-b-c-and-mtv-3-b-c-propellers
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DE9A4814B0E4226586256B6D005C5A33.0001
- Page: https://openairdocs.org/proposed/99-NE-35-AD

## Summary

The Federal Aviation Administration (FAA) proposes to supersede an existing airworthiness directive (AD), applicable to MT-Propeller Entwicklung GMBH models MTV-9-B-C and MTV-3-B-C propellers. That AD currently requires initial and repetitive inspections of Torx head blade root lag screws that are used on certain serial number (SN) propellers and replacing all lag screws on the propeller if any screws are found broken or with insufficient torque. In addition, that AD currently requires replacing certain part number (P/N) Torx head blade root lag screws with improved, hexagonal head blade root lag screws. This proposal would require the expansion of the applicability from certain SN propellers to all propellers with certain SN blades that may contain the suspect Torx head blade root lag screws. This proposal is prompted by FAA awareness that a propeller hub of an affected propeller could be changed, thereby changing the propeller serial number, creating a propeller that is notlisted in the AD and that has affected blades and lag screws. The actions specified by the proposed AD are intended to prevent failure of the blade root lag screw, which could result in propeller blade separation and loss of control of the airplane.

## Notices in this docket

- Feb 27, 2002: Notice of proposed rulemaking (NPRM). (first notice), FR document 02-4587, comments due Apr 29, 2002 (https://www.federalregister.gov/documents/2002/02/27/02-4587/airworthiness-directives-mt-propeller-entwicklung-gmbh-models-mtv-9-b-c-and-mtv-3-b-c-propellers)

---
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.