# Proposed AD 99-CE-63-AD: Raytheon Aircraft Company Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A, V35B, 36, and A36 Airplanes

- Type: Proposed airworthiness directive (not in force)
- Status: Became AD 2001-08-08
- Action: Notice of proposed rulemaking (NPRM).
- Published: October 18, 2000, 65 FR 62315
- Comments due: December 11, 2000
- Became: [AD 2001-08-08](https://openairdocs.org/ad/2001-08-08)
- Docket: 99-CE-63-AD
- FR document: 00-26712
- Official PDF: https://openairdocs.org/files/sha256/04/57/045748a6b09535b018c29b3635b280551410a67ad2e7252d5e12ed0724e0e39f (from https://www.govinfo.gov/content/pkg/FR-2000-10-18/pdf/00-26712.pdf)
- Federal Register: https://www.federalregister.gov/documents/2000/10/18/00-26712/airworthiness-directives-raytheon-aircraft-company-beech-models-35-c33a-e33a-e33c-f33a-f33c-s35-v35
- Page: https://openairdocs.org/proposed/99-CE-63-AD

## Summary

This document proposes to adopt a new airworthiness directive (AD) that would apply to all Raytheon Aircraft Company (Raytheon) Beech Models 35-C33A, E33A, E33C, F33A, F33C, S35, V35, V35A, V35B, 36, and A36 airplanes that incorporate a certain Teledyne Continental engine configuration. The proposed AD would require you to repetitively replace the existing Aeroquip V-band exhaust clamp. The actions specified by the proposed AD are intended to prevent the exhaust stack from detaching from the turbocharger due to failure of the V-band exhaust clamp. Clamp failure could result in the release of high temperature gases inside the engine compartment with a consequent fire in the engine compartment.

## Notices in this docket

- Oct 18, 2000: Notice of proposed rulemaking (NPRM). (first notice), FR document 00-26712, comments due Dec 11, 2000 (https://www.federalregister.gov/documents/2000/10/18/00-26712/airworthiness-directives-raytheon-aircraft-company-beech-models-35-c33a-e33a-e33c-f33a-f33c-s35-v35)

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