Source: https://www.law.cornell.edu/cfr/text/14/appendix-G_to_part_23
Timestamp: 2018-10-19 14:00:35
Document Index: 736038817

Matched Legal Cases: ['art 23', 'art 23', 'art_23', 'art 23', '§ 23', '§ 43']

14 CFR Appendix G to Part 23, Instructions for Continued Airworthiness | US Law | LII / Legal Information Institute
CFR › Title 14 › Chapter I › Subchapter C › Part 23 › Subpart G › Appendix G_to_part_23
14 CFR Appendix G to Part 23, Instructions for Continued Airworthiness
(a) This appendix specifies requirements for the preparation of Instructions for Continued Airworthiness as required by § 23.1529.
G23.2 Format.
(a)Airplane maintenance manual or section.
(b)Maintenance instructions.
G23.4 Airworthiness Limitations section. The Instructions for Continued Airworthiness must contain a section titled Airworthiness Limitations that is segregated and clearly distinguishable from the rest of the document. This section must set forth each mandatory replacement time, structural inspection interval, and related structural inspection procedure required for type certification. If the Instructions for Continued Airworthiness consist of multiple documents, the section required by this paragraph must be included in the principal manual. This section must contain a legible statement in a prominent location that reads: “The Airworthiness Limitations section is FAA approved and specifies maintenance required under §§ 43.16 and 91.403 of the Federal Aviation Regulations unless an alternative program has been FAA approved.”
83 FR 21850 - Accepted Means of Compliance; Airworthiness Standards: Normal Category Airplanes
FR Doc. 2018-09990
83 FR 19427 - Special Conditions: St. Louis Helicopter, LLC; Textron Aviation B300, B300C, B300C (MC-12W), and B300C (UC-12W) Airplanes; Installation of Rechargeable Lithium Batteries
FR Doc. 2018-09350
Docket No. FAA-2018-0374
Special Conditions No. 23-288-SC
The effective date of these special conditions is May 3, 2018. We must receive your comments by June 18, 2018.
83 FR 11634 - Special Conditions: Honda Aircraft Company, Inc., HA-420 Airplane; Single-Place Side-Facing Lavatory Seat Dynamic Test
FR Doc. 2018-05321
Docket No. FAA-2018-0200
Special Conditions No. 23-287-SC
The special conditions are effective March 16, 2018, and are applicable March 7, 2018. We must receive your comments by April 16, 2018.
These special conditions are issued for the Honda Aircraft Company, Inc., HA-420 airplane. This airplane will have a novel or unusual design feature associated with a single-place side-facing seat in the lavatory that can be used as a passenger seat during taxi, takeoff, and landing. 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.
83 FR 9176 - Special Conditions: Textron Aviation, Inc., Model C90A King Air; Installation of Electronic Engine Control System
FR Doc. 2018-04417
Docket No. FAA-2018-0090
Special Conditions No. 23-286-SC
The effective date of these special conditions is March 5, 2018. We must receive your comments by April 4, 2018.
These special conditions are issued for the Textron Aviation, Inc., model C90A King Air airplane. This airplane as modified by Nextant Aerospace will have a novel or unusual design feature associated with installation of an engine that includes an electronic engine control system. 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.
82 FR 40943 - Special Conditions: Game Composites Ltd., GB1 Airplane; Acrobatic Category Aerodynamic Stability
FR Doc. 2017-18324
Docket No. FAA-2017-0651
Special Conditions No. 23-285-SC
These special conditions are effective August 29, 2017 and are applicable on August 22, 2017.
These special conditions are issued for the Game Composites Ltd. GB1 airplane. This airplane will have a novel or unusual design feature(s) associated with static stability. This airplane can perform at the highest level of aerobatic competition. To be competitive, the airplane is designed with its lateral and directional axes being decoupled from each other; providing more precise maneuvering. The applicable airworthiness regulations 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 establish a level of safety equivalent to that established by the existing airworthiness standards.
82 FR 32614 - Special Conditions: Pilatus Aircraft Ltd., PC-24; Pressure Defuel System
FR Doc. 2017-14937
82 FR 32616 - Special Conditions: Pilatus Aircraft Ltd., PC-24; Electronic Engine Control (EEC)
FR Doc. 2017-14936
82 FR 32618 - Special Conditions: Pilatus Aircraft Ltd., PC-24, Autothrust System
FR Doc. 2017-14938
82 FR 30798 - Special Conditions: Game Composites Ltd, GB1 Airplane; Acrobatic Category Aerodynamic Stability
FR Doc. 2017-13991
Notice No. 23-17-02-SC
Send your comments on or before August 2, 2017.
This action proposes special conditions for the Game Composites Ltd. GB1 airplane. This airplane will have a novel or unusual design feature(s) associated with static stability. This airplane can perform at the highest level of aerobatic competition. To be competitive, the airplane is designed with its lateral and directional axes being decoupled from each other; providing more precise maneuvering. 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 the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.
82 FR 25509 - Special Conditions: Pilatus Aircraft Limited Models PC-12, PC-12/45, PC-12/47; Autothrust System
FR Doc. 2017-11347
Special Conditions No. 23-281-SC
This special condition is effective June 2, 2017 and is applicable beginning May 24, 2017.
This special condition is for the Pilatus Aircraft Limited PC-12, PC-12/45, and PC-12/47 airplanes. These airplanes, as modified by Innovative Solutions & Support, Inc., will have a novel or unusual design feature associated with the use of an autothrust system. The applicable airworthiness regulations do not contain adequate or appropriate safety standards for this design feature. This special condition contains the additional safety standards the Administrator considers necessary to establish a level of safety equivalent to that established by the existing airworthiness standards.