14 CFR 27.1505 - Never-exceed speed. | Title 14 - Aeronautics and Space | Code of Federal Regulations

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§ 27.1505

Never-exceed speed.

(a) The never-exceed speed, VNE, must be established so that it is—

(1) Not less than 40 knots (CAS); and

(2) Not more than the lesser of—

(i) 0.9 times the maximum forward speeds established under § 27.309 ;

(ii) 0.9 times the maximum speed shown under §§ 27.251 and 27.629; or

(iii) 0.9 times the maximum speed substantiated for advancing blade tip mach number effects.

(b) VNE may vary with altitude, r.p.m., temperature, and weight, if—

(1) No more than two of these variables (or no more than two instruments integrating more than one of these variables) are used at one time; and

(2) The ranges of these variables (or of the indications on instruments integrating more than one of these variables) are large enough to allow an operationally practical and safe variation of VNE.

(c) For helicopters, a stabilized power-off VNE denoted as VNE (power-off) may be established at a speed less than VNE established pursuant to paragraph (a) of this section, if the following conditions are met:

(1) VNE (power-off) is not less than a speed midway between the power-on VNE and the speed used in meeting the requirements of—

(i) § 27.65(b) for single engine helicopters; and

(ii) § 27.67 for multiengine helicopters.

(2) VNE (power-off) is—

(i) A constant airspeed;

(ii) A constant amount less than power-on VNE; or

(iii) A constant airspeed for a portion of the altitude range for which certification is requested, and a constant amount less than power-on VNE for the remainder of the altitude range.

(Secs. 313(a), 601, 603, 604, and 605 of the Federal Aviation Act of 1958 ( 49 U.S.C. 1354(a), 1421, 1423, 1424 , and 1425); and sec. 6(c) of the Dept. of Transportation Act ( 49 U.S.C. 1655(c) ))

[Amdt. 27-2, 33 FR 964, Jan. 26, 1968, and Amdt. 27-14, 43 FR 2325, Jan. 16, 1978; Amdt. 27-21, 49 FR 44435, Nov. 6, 1984]

Title 14 published on 2012-01-01

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.

2012-08-22; vol. 77 # 163 - Wednesday, August 22, 2012

77 FR 50576 - Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures; OMB Approval of Information Collection

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-20685
RIN	2120-AJ52
Docket No.	FAA-2009-0660
Amdt. Nos.	27-47, 29-54

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final rule; OMB approval of information collection.

The rule published on December 1, 2011, and became effective on January 30, 2012. However, at the time of publication, the new information collection requirements imposed by 14 CFR 27.573 and 29.573 lacked OMB approval. This document announces receipt of OMB's June 28, 2012 approval.

14 CFR Parts 27 and 29

Summary

This document notifies the public of the Office of Management and Budget's (OMB's) approval of the information collection requirement contained in the FAA's final rule, “Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures,” which was published on December 1, 2011.

2012-08-13; vol. 77 # 156 - Monday, August 13, 2012

77 FR 48058 - Special Conditions: Eurocopter France, EC130T2; Use of 30-Minute Power Rating

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-19444
RIN
Docket No.	FAA-2012-0820
Special Conditions No.	27-028-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special conditions; request for comments.

The effective date of these special conditions is July 30, 2012. We must receive your comments by September 27, 2012.

14 CFR Part 27

Summary

These special conditions are issued for the Eurocopter France Model EC130T2 helicopter. This model helicopter will have the novel or unusual design feature of a 30-minute power rating, generally intended to be used for hovering at increased power for search and rescue missions. 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 Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

2012-02-01; vol. 77 # 21 - Wednesday, February 1, 2012

77 FR 4890 - Damage Tolerance and Fatigue Evaluation for Composite Rotorcraft Structures, and Damage Tolerance and Fatigue Evaluation for Metallic Structures; Correction

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-2170
RIN	2120-AJ52
Docket No.	FAA-2009-0660
Amdt. Nos.	27-47A, 29-54A
and Docket No.	FAA-2009-0413
Amdt. No.	29-55A

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final rule; correction.

This correction is effective February 1, 2012. The “Composite Rotorcraft Structures” final rule becomes effective January 30, 2012. The “Metallic Structures” final rule becomes effective January 31, 2012.

14 CFR Parts 27 and 29

Summary

The FAA is correcting two final rules, “Damage Tolerance and Fatigue Evaluation for Composite Rotorcraft Structures” (76 FR 74655), published December 1, 2011, and “Damage Tolerance and Fatigue Evaluation for Metallic Structures” (76 FR 75435), published December 2, 2011. In the “Composite Rotorcraft Structures” rule, the FAA amended its regulations to require evaluation of fatigue and residual static strength of composite rotorcraft structures using a damage tolerance evaluation, or a fatigue evaluation if the applicant establishes that a damage tolerance evaluation is impractical. In the “Metallic Structures” rule, the FAA amended its regulations to address advances in structural fatigue substantiation technology for metallic structures to provide an increased level of safety by avoiding or reducing the likelihood of the catastrophic fatigue failure of a metallic structure. This document corrects errors in the preamble of those two documents by adding a statement advising that affected parties do not need to comply with the information collection requirements until the Office of Management and Budget (OMB) approves the collections.

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 2012-01-01

The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 27 after this date.

2013-02-22; vol. 78 # 36 - Friday, February 22, 2013

78 FR 12254 - Interest in Restructure of Rotorcraft Airworthiness Standards

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2013-03709
RIN

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Request for comments.

Send your comments to reach us on or before May 23, 2013.

14 CFR Parts 27 and 29

Summary

The Federal Aviation Administration (FAA) is requesting comments and information on the public's interest in restructuring the rotorcraft airworthiness standards of normal category rotorcraft and transport category rotorcraft. Specifically, the agency is seeking comments on whether to change the existing applicability standards for maximum weight and number of passenger seats for either or both types of rotorcraft, or whether to consider other approaches for determining applicability. The FAA is soliciting public input because of some rotorcraft community interest in increasing the 7,000 pound maximum weight limit for the modern normal category rotorcraft and because there may be recommendations for new approaches to make the rotorcraft airworthiness standards more efficient and adaptable to future technology. This action is part of an effort to develop recommendations for possible FAA rulemaking action.

2012-08-22; vol. 77 # 163 - Wednesday, August 22, 2012

77 FR 50576 - Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures; OMB Approval of Information Collection

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-20685
RIN	2120-AJ52
Docket No.	FAA-2009-0660
Amdt. Nos.	27-47, 29-54

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final rule; OMB approval of information collection.

The rule published on December 1, 2011, and became effective on January 30, 2012. However, at the time of publication, the new information collection requirements imposed by 14 CFR 27.573 and 29.573 lacked OMB approval. This document announces receipt of OMB's June 28, 2012 approval.

14 CFR Parts 27 and 29

Summary

This document notifies the public of the Office of Management and Budget's (OMB's) approval of the information collection requirement contained in the FAA's final rule, “Damage Tolerance and Fatigue Evaluation of Composite Rotorcraft Structures,” which was published on December 1, 2011.

2012-08-13; vol. 77 # 156 - Monday, August 13, 2012

77 FR 48058 - Special Conditions: Eurocopter France, EC130T2; Use of 30-Minute Power Rating

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-19444
RIN
Docket No.	FAA-2012-0820
Special Conditions No.	27-028-SC

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final special conditions; request for comments.

The effective date of these special conditions is July 30, 2012. We must receive your comments by September 27, 2012.

14 CFR Part 27

Summary

These special conditions are issued for the Eurocopter France Model EC130T2 helicopter. This model helicopter will have the novel or unusual design feature of a 30-minute power rating, generally intended to be used for hovering at increased power for search and rescue missions. 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 Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.

2012-02-01; vol. 77 # 21 - Wednesday, February 1, 2012

77 FR 4890 - Damage Tolerance and Fatigue Evaluation for Composite Rotorcraft Structures, and Damage Tolerance and Fatigue Evaluation for Metallic Structures; Correction

GPO FDSys XML | Text

Additional Documents

type	regulations.gov
FR Doc.	2012-2170
RIN	2120-AJ52
Docket No.	FAA-2009-0660
Amdt. Nos.	27-47A, 29-54A
and Docket No.	FAA-2009-0413
Amdt. No.	29-55A

DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration

Final rule; correction.

This correction is effective February 1, 2012. The “Composite Rotorcraft Structures” final rule becomes effective January 30, 2012. The “Metallic Structures” final rule becomes effective January 31, 2012.

14 CFR Parts 27 and 29

Summary

The FAA is correcting two final rules, “Damage Tolerance and Fatigue Evaluation for Composite Rotorcraft Structures” (76 FR 74655), published December 1, 2011, and “Damage Tolerance and Fatigue Evaluation for Metallic Structures” (76 FR 75435), published December 2, 2011. In the “Composite Rotorcraft Structures” rule, the FAA amended its regulations to require evaluation of fatigue and residual static strength of composite rotorcraft structures using a damage tolerance evaluation, or a fatigue evaluation if the applicant establishes that a damage tolerance evaluation is impractical. In the “Metallic Structures” rule, the FAA amended its regulations to address advances in structural fatigue substantiation technology for metallic structures to provide an increased level of safety by avoiding or reducing the likelihood of the catastrophic fatigue failure of a metallic structure. This document corrects errors in the preamble of those two documents by adding a statement advising that affected parties do not need to comply with the information collection requirements until the Office of Management and Budget (OMB) approves the collections.

14 CFR 27.1505 - Never-exceed speed.

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