14 CFR 33, Subpart G - Special Requirements: Turbine Aircraft Engines | Title 14 - Aeronautics and Space | Code of Federal Regulations

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§ 33.201 — Design and test requirements for Early ETOPS eligibility.

Title 14 published on 2013-01-01

The following are only the Rules published in the Federal Register after the published date of Title 14.

For a complete list of all Rules, Proposed Rules, and Notices view the Rulemaking tab.

2013-04-03; vol. 78 # 64 - Wednesday, April 3, 2013

78 FR 19982 - Special Conditions: Turbomeca Ardiden 3K Turboshaft Engine

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2013-07662
RIN
EDocket No.	FAA-2012-1085
Special Conditions No.	33-013-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special condition.

The effective date of these special conditions is May 3, 2013.

14 CFR Part 33

Summary

We are issuing these special conditions for the Turbomeca Ardiden 3K model engines. This engine model will have a novel or unusual design feature that is a 30-minute all engines operating (AEO) power rating for hovering at increased power (HIP). This rating is primarily intended for high-power hovering operations that are normal mission functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the FAA considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

2013-03-12; vol. 78 # 48 - Tuesday, March 12, 2013

78 FR 15597 - Special Conditions: GE Aviation CT7-2E1 Turboshaft Engine Model

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2013-05676
RIN
Docket No.	FAA-2012-0745
Special Condition No.	33-012-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special conditions.

The effective date of these special conditions is April 11, 2013.

14 CFR Part 33

Summary

These final special conditions are issued for the General Electric Aviation (GE) CT7-2E1 engine model. This engine model will have a novel or unusual design feature, which is a combination of two existing ratings into a new rating called “flat 30-second and 2-minute OEI” rating. This rating is intended for the continuation of flight of a multi-engine rotorcraft after one engine becomes inoperative. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These final special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

This is a list of United States Code sections, Statutes at Large, Public Laws, and Presidential Documents, which provide rulemaking authority for this CFR Part.

This list is taken from the Parallel Table of Authorities and Rules provided by GPO [Government Printing Office].

It is not guaranteed to be accurate or up-to-date, though we do refresh the database weekly. More limitations on accuracy are described at the GPO site.

United States Code

USC : Title 49 - TRANSPORTATION

§ 106 - Federal Aviation Administration

§ 40113 - Administrative

§ 44701 - General requirements

§ 44702 - Issuance of certificates

§ 44704 - Type certificates, production certificates, airworthiness certificates, and design organization certificates

Title 14 published on 2013-01-01

The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 33 after this date.

2013-04-03; vol. 78 # 64 - Wednesday, April 3, 2013

78 FR 19982 - Special Conditions: Turbomeca Ardiden 3K Turboshaft Engine

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2013-07662
RIN
EDocket No.	FAA-2012-1085
Special Conditions No.	33-013-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special condition.

The effective date of these special conditions is May 3, 2013.

14 CFR Part 33

Summary

We are issuing these special conditions for the Turbomeca Ardiden 3K model engines. This engine model will have a novel or unusual design feature that is a 30-minute all engines operating (AEO) power rating for hovering at increased power (HIP). This rating is primarily intended for high-power hovering operations that are normal mission functions. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards that the FAA considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

2013-03-12; vol. 78 # 48 - Tuesday, March 12, 2013

78 FR 15597 - Special Conditions: GE Aviation CT7-2E1 Turboshaft Engine Model

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2013-05676
RIN
Docket No.	FAA-2012-0745
Special Condition No.	33-012-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special conditions.

The effective date of these special conditions is April 11, 2013.

14 CFR Part 33

Summary

These final special conditions are issued for the General Electric Aviation (GE) CT7-2E1 engine model. This engine model will have a novel or unusual design feature, which is a combination of two existing ratings into a new rating called “flat 30-second and 2-minute OEI” rating. This rating is intended for the continuation of flight of a multi-engine rotorcraft after one engine becomes inoperative. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These final special conditions contain the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

14 CFR 33, Subpart G - Special Requirements: Turbine Aircraft Engines

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