14 CFR 29, Subpart E - Powerplant
- — General
- § 29.901 — Installation.
- § 29.903 — Engines.
- § 29.907 — Engine vibration.
- § 29.908 — Cooling fans.
- — Rotor Drive System
- § 29.917 — Design.
- § 29.921 — Rotor brake.
- § 29.923 — Rotor drive system and control mechanism tests.
- § 29.927 — Additional tests.
- § 29.931 — Shafting critical speed.
- § 29.935 — Shafting joints.
- § 29.939 — Turbine engine operating characteristics.
- — Fuel System
- § 29.951 — General.
- § 29.952 — Fuel system crash resistance.
- § 29.953 — Fuel system independence.
- § 29.954 — Fuel system lightning protection.
- § 29.955 — Fuel flow.
- § 29.957 — Flow between interconnected tanks.
- § 29.959 — Unusable fuel supply.
- § 29.961 — Fuel system hot weather operation.
- § 29.963 — Fuel tanks: general.
- § 29.965 — Fuel tank tests.
- § 29.967 — Fuel tank installation.
- § 29.969 — Fuel tank expansion space.
- § 29.971 — Fuel tank sump.
- § 29.973 — Fuel tank filler connection.
- § 29.975 — Fuel tank vents and carburetor vapor vents.
- § 29.977 — Fuel tank outlet.
- § 29.979 — Pressure refueling and fueling provisions below fuel level.
- — Fuel System Components
- § 29.991 — Fuel pumps.
- § 29.993 — Fuel system lines and fittings.
- § 29.995 — Fuel valves.
- § 29.997 — Fuel strainer or filter.
- § 29.999 — Fuel system drains.
- § 29.1001 — Fuel jettisoning.
- — Oil System
- § 29.1011 — Engines: general.
- § 29.1013 — Oil tanks.
- § 29.1015 — Oil tank tests.
- § 29.1017 — Oil lines and fittings.
- § 29.1019 — Oil strainer or filter.
- § 29.1021 — Oil system drains.
- § 29.1023 — Oil radiators.
- § 29.1025 — Oil valves.
- § 29.1027 — Transmission and gearboxes: general.
- — Cooling
- § 29.1041 — General.
- § 29.1043 — Cooling tests.
- § 29.1045 — Climb cooling test procedures.
- § 29.1047 — Takeoff cooling test procedures.
- § 29.1049 — Hovering cooling test procedures.
- — Induction System
- § 29.1091 — Air induction.
- § 29.1093 — Induction system icing protection.
- § 29.1101 — Carburetor air preheater design.
- § 29.1103 — Induction systems ducts and air duct systems.
- § 29.1105 — Induction system screens.
- § 29.1107 — Inter-coolers and after-coolers.
- § 29.1109 — Carburetor air cooling.
- — Exhaust System
- § 29.1121 — General.
- § 29.1123 — Exhaust piping.
- § 29.1125 — Exhaust heat exchangers.
- — Powerplant Controls and Accessories
- § 29.1141 — Powerplant controls: general.
- § 29.1142 — Auxiliary power unit controls.
- § 29.1143 — Engine controls.
- § 29.1145 — Ignition switches.
- § 29.1147 — Mixture controls.
- § 29.1151 — Rotor brake controls.
- § 29.1157 — Carburetor air temperature controls.
- § 29.1159 — Supercharger controls.
- § 29.1163 — Powerplant accessories.
- § 29.1165 — Engine ignition systems.
- — Powerplant Fire Protection
- § 29.1181 — Designated fire zones: regions included.
- § 29.1183 — Lines, fittings, and components.
- § 29.1185 — Flammable fluids.
- § 29.1187 — Drainage and ventilation of fire zones.
- § 29.1189 — Shutoff means.
- § 29.1191 — Firewalls.
- § 29.1193 — Cowling and engine compartment covering.
- § 29.1194 — Other surfaces.
- § 29.1195 — Fire extinguishing systems.
- § 29.1197 — Fire extinguishing agents.
- § 29.1199 — Extinguishing agent containers.
- § 29.1201 — Fire extinguishing system materials.
- § 29.1203 — Fire detector systems.
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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-20684 RIN 2120-AJ51 Docket No. FAA-2009-0413 Amdt. No. 29-55 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule; OMB approval of information collection. The rule published on December 2, 2011, and became effective on January 31, 2012. However, at the time of publication, the new information collection requirements imposed by 14 CFR 29.571, lacked OMB approval. This document announces receipt of OMB's June 28, 2012 approval. 14 CFR Part 29 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, “Fatigue Tolerance Evaluation of Metallic Structures,” which was published on December 2, 2011.
GPO FDSys XML | Text 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 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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-18199 RIN Docket No. FAA-2012-0785 Special Conditions No. 29-027-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is July 18, 2012. We must receive your comments by September 25, 2012. 14 CFR Part 29 These special conditions are issued for the Agusta S.p.A. (Agusta) Model AW139 and AB139 helicopters. These model helicopters, as modified by Agusta, will have novel or unusual design features associated with installing an optional SAR AFCS. The applicable airworthiness standards do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers necessary to show a level of safety equivalent to that established by the existing airworthiness standards.
GPO FDSys XML | Text 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 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].
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§ 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 29 after this date.
GPO FDSys XML | Text 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 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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-24676 RIN Docket No. SW022 Special Conditions No. 29-022A-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Amended final special conditions. Effective Date: The effective date of these special conditions is November 5, 2012. 14 CFR Part 29 These special conditions amend and supersede those final special conditions No. 29-022-SC, for the ECF model EC225LP helicopter, which were published in the Federal Register on November 6, 2008 (73 FR 65968). A notice proposing this amendment was published December 20, 2010 (75 FR 79312). This amendment modifies the original final special conditions to address comments received and to clarify the intent of some of the requirements. This helicopter, as modified by ECF, will have novel or unusual design features associated with installing an optional SAR AFCS. 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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-20684 RIN 2120-AJ51 Docket No. FAA-2009-0413 Amdt. No. 29-55 DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final rule; OMB approval of information collection. The rule published on December 2, 2011, and became effective on January 31, 2012. However, at the time of publication, the new information collection requirements imposed by 14 CFR 29.571, lacked OMB approval. This document announces receipt of OMB's June 28, 2012 approval. 14 CFR Part 29 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, “Fatigue Tolerance Evaluation of Metallic Structures,” which was published on December 2, 2011.
GPO FDSys XML | Text 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 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.
GPO FDSys XML | Text type regulations.gov FR Doc. 2012-18199 RIN Docket No. FAA-2012-0785 Special Conditions No. 29-027-SC DEPARTMENT OF TRANSPORTATION, Federal Aviation Administration Final special conditions; request for comments. The effective date of these special conditions is July 18, 2012. We must receive your comments by September 25, 2012. 14 CFR Part 29 These special conditions are issued for the Agusta S.p.A. (Agusta) Model AW139 and AB139 helicopters. These model helicopters, as modified by Agusta, will have novel or unusual design features associated with installing an optional SAR AFCS. The applicable airworthiness standards do not contain adequate or appropriate safety standards for this design feature. These special conditions contain the additional safety standards the Administrator considers necessary to show a level of safety equivalent to that established by the existing airworthiness standards.
GPO FDSys XML | Text 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 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.