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Proposed Advisory Circular; Turbine Rotor Strength Requirements

---
identifier: "/us/fr/03-15402"
source: "fr"
legal_status: "authoritative_unofficial"
title: "Proposed Advisory Circular; Turbine Rotor Strength Requirements"
title_number: 0
title_name: "Federal Register"
section_number: "03-15402"
section_name: "Proposed Advisory Circular; Turbine Rotor Strength Requirements"
positive_law: false
currency: "2003-06-18"
last_updated: "2003-06-18"
format_version: "1.1.0"
generator: "[email protected]"
agency: "Transportation Department"
document_number: "03-15402"
document_type: "notice"
publication_date: "2003-06-18"
agencies:
  - "Transportation Department"
  - "Federal Aviation Administration"
fr_citation: "68 FR 36623"
fr_volume: 68
comments_close_date: "2003-08-01"
fr_action: "Notice of availability of proposed advisory circular and request for comments."
---

#  Proposed Advisory Circular; Turbine Rotor Strength Requirements

**AGENCY:**

Federal Aviation Administration, DOT.

**ACTION:**

Notice of availability of proposed advisory circular and request for comments.

**SUMMARY:**

The Federal Aviation Administration (FAA) announces the availability of proposed advisory circular (AC) Number 33.27-1, Turbine Rotor Strength Requirements of 14 CFR 33.27.

**DATES:**

Comments must be received on or before August 1, 2003.

**ADDRESSES:**

Send all comments on the proposed AC to the Federal Aviation Administration, Attn: Tim Mouzakis, Engine and Propeller Standards Staff, ANE-110, 12 New England Executive Park, Burlington, MA 01803-5299.

**FOR FURTHER INFORMATION CONTACT:**

Tim Mouzakis, Engine and Propeller Standards Staff, ANE-110, at the above address; telephone: (781) 238-7114; fax: (781) 238-7199; e-mail: *[email protected].*

**SUPPLEMENTARY INFORMATION:**

**Comments Invited**

A copy of the subject AC may be obtained by contacting the person named under *FOR FURTHER INFORMATION CONTACT* or by donwloading the proposed AC from the following Internet Web site: *http://www.airweb.faa.gov/rgl.* The FAA invites interested parties to comment on the proposed AC. Comments should identify the subject of the AC and be submitted to the individual identified under *FOR FURTHER INFORMATION CONTACT* . The FAA will consider all communications received by the closing date before issuing the final AC.

**Background**

This AC provides guidance and acceptable methods, but not the only methods, for demonstrating compliance with the rotor strength (overspeed) requirements of § 33.27 of title 14 of the Code of Federal Regulations (14 CFR 33.27).

(Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.)

Issued in Burlington, Massachusetts, on June 11, 2003.

Peter A. White,

Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service.