# Proposed AD FAA-2006-23646: Air Tractor, Inc., Models AT-400, AT- 401, AT-401B, AT-402, AT-402A, and AT-402B Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2006-08-08
- Products: Air Tractor
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: December 10, 2008, 73 FR 74999
- Comments due: February 9, 2009
- Became: [AD 2006-08-08](https://openairdocs.org/ad/2006-08-08)
- Docket: FAA-2006-23646 (https://www.regulations.gov/docket/FAA-2006-23646, where comments are filed)
- Project: 2006-CE-005-AD
- FR document: E8-29165
- Official PDF: https://openairdocs.org/files/sha256/75/dc/75dcc55b0ac37d6534f3cd3b25b7e9ce15f814cd16b3526112ff45364d69bf53 (from https://www.govinfo.gov/content/pkg/FR-2008-12-10/pdf/E8-29165.pdf)
- Federal Register: https://www.federalregister.gov/documents/2008/12/10/E8-29165/airworthiness-directives-air-tractor-inc-models-at-400-at-401-at-401b-at-402-at-402a-and-at-402b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/60991EB6E7BAB2B28625751D006EF095.0001
- Page: https://openairdocs.org/proposed/FAA-2006-23646

## Summary

We propose to revise Airworthiness Directive (AD) 2006-08-08, which applies to certain Air Tractor, Inc. (Air Tractor), Models AT- 400, AT-401, AT-401B, AT-402, AT-402A, and AT-402B airplanes. AD 2006- 08-08 currently requires you to repetitively eddy current inspect the wing lower spar cap in order to reach the safe life and, for certain Models AT-402A and AT-402B airplanes and those that incorporate or have incorporated Marburger Enterprises, Inc. (Marburger), winglets, lowers the safe life for the wing lower spar cap. Since we issued AD 2006-08- 08, we have received information to update inspection intervals for the Models AT-401B, AT-402A, and AT-402B airplanes based on a revised damage tolerance analysis. Consequently, this proposed AD would not only retain the actions of AD 2006-08-08, but would reduce the number of repetitive inspections for all affected Model AT-401B airplanes and certain Models AT-402A and AT-402B airplanes. We are proposing this AD to prevent fatiguecracks from occurring in the wing lower spar cap before the originally established safe life is reached. Fatigue cracks in the wing lower spar cap, if not detected and corrected, could result in wing separation and loss of control of the airplane.

## Notices in this docket

- Dec 10, 2008: Notice of proposed rulemaking (NPRM). (first notice), FR document E8-29165, comments due Feb 9, 2009 (https://www.federalregister.gov/documents/2008/12/10/E8-29165/airworthiness-directives-air-tractor-inc-models-at-400-at-401-at-401b-at-402-at-402a-and-at-402b)

---
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.