# Proposed AD FAA-2016-9299: Bombardier, Inc. Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2017-08-02
- Products: Bombardier
- Product type: Aircraft
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 26, 2016, 81 FR 74360
- Comments due: December 12, 2016
- Became: [AD 2017-08-02](https://openairdocs.org/ad/2017-08-02)
- Docket: FAA-2016-9299 (https://www.regulations.gov/docket/FAA-2016-9299, where comments are filed)
- Project: 2016-NM-119-AD
- FR document: 2016-25664
- Official PDF: https://openairdocs.org/files/sha256/60/9a/609aba6996b6b9124f009a5715ca262adc37695546f66f3ae1452fcefff1d4fe (from https://www.govinfo.gov/content/pkg/FR-2016-10-26/pdf/2016-25664.pdf)
- Federal Register: https://www.federalregister.gov/documents/2016/10/26/2016-25664/airworthiness-directives-bombardier-inc-airplanes
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/296B061176DCABA7862580580049B53D.0001
- Page: https://openairdocs.org/proposed/FAA-2016-9299

## Summary

We propose to adopt a new airworthiness directive (AD) for certain Bombardier Inc. Model DHC-8-102, -103, and -106 airplanes; DHC- 8-200 series airplanes; and Model DHC-8-300 series airplanes. This proposed AD was prompted by reports of incorrect installation of the auto-ignition system due to crossed wires at one of the splices in the auto-relight system. This proposed AD would require inspecting the auto-ignition system for correct wiring, and doing corrective actions if necessary. We are proposing this AD to detect and correct incorrect wiring of the auto-ignition system, which could result in inability to restart the engine in flight and consequent reduced controllability of the airplane.

## Notices in this docket

- Oct 26, 2016: Notice of proposed rulemaking (NPRM). (first notice), FR document 2016-25664, comments due Dec 12, 2016 (https://www.federalregister.gov/documents/2016/10/26/2016-25664/airworthiness-directives-bombardier-inc-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.
