Source: http://www.law.cornell.edu/cfr/text/14/29.85
Timestamp: 2014-11-27 09:46:35
Document Index: 529095465

Matched Legal Cases: ['art 29', '§ 29', '§ 29', '§ 29', 'art 29', 'arts 27', 'arts 27', 'arts 27', 'arts 27']

14 CFR 29.85 - Balked landing: Category A. | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 29 › Subpart B › Section 29.85 14 CFR 29.85 - Balked landing: Category A.
There is 1 rule appearing in the Federal Register for 14 CFR 29. View below or at eCFR (GPOAccess)
§ 29.85
Balked landing: Category A.
For Category A rotorcraft, the balked landing path with the critical engine inoperative must be established so that—
The transition from each stage of the maneuver to the next stage can be made smoothly and safely;
From the LDP on the approach path selected by the applicant, a safe climbout can be made at speeds allowing compliance with the climb requirements of § 29.67(a)(1) and (2); and
The rotorcraft does not descend below 15 feet above the landing surface. For elevated heliport operations, descent may be below the level of the landing surface provided the deck edge clearance of § 29.60 is maintained and the descent (loss of height) below the landing surface is determined.
[Doc. No. 24802, 64 FR 45338, Aug. 19, 1999]
Title 14 published on 2014-01-01The 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.2014-09-15; vol. 79 # 178 - Monday, September 15, 201479 FR 54889 - Special Conditions: AgustaWestland, AW189; Use of 30-Minute All Engines Operating (AEO) Power Rating
typeregulations.gov FR Doc.2014-21794 RIN Docket No.FAA-2014-0697 Special Conditions No.29-034-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is September 4, 2014. We must receive your comments by October 30, 2014. 14 CFR Part 29 SummaryThese special conditions are issued for the AgustaWestland Model AW189 helicopter. This model helicopter will have the novel or unusual design feature of a 30-minute all engines operating (AEO) 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.
Title 14 published on 2014-01-01The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 29 after this date.2014-09-15; vol. 79 # 178 - Monday, September 15, 201479 FR 54889 - Special Conditions: AgustaWestland, AW189; Use of 30-Minute All Engines Operating (AEO) Power Rating
2014-07-31; vol. 79 # 147 - Thursday, July 31, 201479 FR 44320 - Interest in Restructure of Rotorcraft Airworthiness Standards
typeregulations.gov FR Doc.2014-16999 RIN DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of Disposition of Comments. The docket is terminated as of July 31, 2014. 14 CFR Parts 27 and 29 SummaryThis notice disposes of public comments received by the Federal Aviation Administration (FAA) in response to a Federal Register notice published on February 22, 2013, requesting comments on a potential restructuring of the rotorcraft airworthiness standards of Title 14 of the Code of Federal Regulations (14 CFR) parts 27 (normal category rotorcraft) and 29 (transport category rotorcraft). Specifically, the agency sought comments on the necessity of updates to parts 27 and 29, including whether to change the existing weight- and seat-based applicability standards for normal and transport rotorcraft. Based on the comments received, the FAA is terminating this docket. Commenters indicated a substantial interest in revising or restructuring the certification standards for parts 27 and 29, and the FAA&apos;s Rotorcraft Directorate will begin establishing the appropriate forums to involve interested parties.