Source: http://www.law.cornell.edu/cfr/text/14/23.1589
Timestamp: 2013-05-25 07:51:13
Document Index: 384754882

Matched Legal Cases: ['§ 23', '§ 23', '§ 23', '§ 23', 'art 23', 'art 23', '§ 106', '§ 40113', '§ 44701', '§ 44702', '§ 44704', 'art 23']

14 CFR 23.1589 - Loading information. | Title 14 - Aeronautics and Space | Code of Federal Regulations | LII / Legal Information Institute
14 CFR 23.1589 - Loading information.
There are 4 Updates appearing in the Federal Register for 14 CFR 23. Select the tab below to view, or View eCFR (GPOAccess)
§ 23.1589
The following loading information must be furnished:
(a) The weight and location of each item of equipment that can be easily removed, relocated, or replaced and that is installed when the airplane was weighed under the requirement of § 23.25.
(b) Appropriate loading instructions for each possible loading condition between the maximum and minimum weights established under § 23.25, to facilitate the center of gravity remaining within the limits established under § 23.23.
[Doc. No. 4080, 29 FR 17955, Dec. 18, 1964, as amended by Amdt. 23-45, 58 FR 42167, Aug. 6, 1993; Amdt. 23-50, 61 FR 5195, Feb. 9, 1996]
Title 14 published on 2012-01-01The 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.2013-02-13; vol. 78 # 30 - Wednesday, February 13, 201378 FR 10055 - Special Conditions: Tamarack Aerospace Group, Cirrus Model SR22; Active Technology Load Alleviation System (ATLAS)
2012-03-26; vol. 77 # 58 - Monday, March 26, 201277 FR 17323 - Special Conditions: XtremeAir GmbH, XA42; Acrobatic Category Aerodynamic Stability
typeregulations.gov FR Doc.2012-6837 RIN Docket No.FAA-2011-1387 Special Conditions No.23-256-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions. Effective Date: April 25, 2012. 14 CFR Part 23 SummaryThese special conditions are issued for the XtremeAir GmbH XA42 airplane. The XA42 airplane has a novel or unusual design feature associated with its static stability. This airplane can perform at the highest level of aerobatic competition. To be competitive, the aircraft was designed with positive and, at some points, neutral stability within its flight envelope. Its lateral and directional axes are also decoupled from each other providing more precise maneuvering. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for these design features. 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. These special conditions are only applicable to aircraft certified solely in the acrobatic category.
2012-03-23; vol. 77 # 57 - Friday, March 23, 201277 FR 16907 - Special Conditions: Embraer S.A., Model EMB 505; Inflatable Side-Facing Seat Three-Point Restraint Safety Belt With an Integrated Airbag Device in the Side-Facing Divan Aft Position
typeregulations.gov FR Doc.2012-6956 RIN Docket No.FAA-2012-0315 Special Conditions No.23-257-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is March 16, 2012. Comments must be received on or before April 23, 2012. 14 CFR Part 23 SummaryThese special conditions are issued for the installation of an inflatable three-point restraint safety belt with an integrated airbag device at the aft position in two-place side-facing divan seats on the Embraer S.A. aircraft model EMB-505. These airplanes, as modified by the installation of these inflatable safety belts, will have novel and unusual design features associated with the upper-torso restraint portions of the three-point safety belts, which contain an integrated airbag device. 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.
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 CodeUSC : 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 2012-01-01The following are ALL rules, proposed rules, and notices (chronologically) published in the Federal Register relating to 14 CFR 23 after this date.2013-02-13; vol. 78 # 30 - Wednesday, February 13, 201378 FR 10055 - Special Conditions: Tamarack Aerospace Group, Cirrus Model SR22; Active Technology Load Alleviation System (ATLAS)
2012-05-15; vol. 77 # 94 - Tuesday, May 15, 201277 FR 28530 - Special Conditions: Tamarack Aerospace Group, Cirrus Model SR22; Active Technology Load Alleviation System (ATLAS)
typeregulations.gov FR Doc.2012-11214 RIN Docket No.FAA-2012-0485 Notice No.23-12-01-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Notice of proposed special conditions. Send your comments on or before June 14, 2012. 14 CFR Part 23 SummaryThis action proposes special conditions for the Tamarack Aerospace Group&apos;s modification to the Cirrus Model SR22 airplane. This airplane as modified by Tamarack will have a novel or unusual design feature(s) associated with Tamarack Aerospace Group&apos;s modification. The design change will install winglets and an Active Technology Load Alleviation System (ATLAS). The addition of the ATLAS mitigates the negative effects of the winglets by effectively aerodynamically turning off the winglet under limit gust and maneuver loads. This is accomplished by measuring the aircraft loading and moving a small aileron-like device called a Tamarack Active Control Surface (TACS). The TACS movement reduces lift at the tip of the wing, resulting in the wing center of pressure moving inboard, thus reducing bending stresses along the wing span. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. These proposed 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.