ELECTRONIC CODE OF FEDERAL REGULATIONS Title 14: Aeronautics and Space PART 25—AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES Contents Special Federal Aviation Regulation No. 13 Special Federal Aviation Regulation No. 109 Subpart A—General § 25.1 Applicability. § 25.2 Special retroactive ...
FAA FAR Part 25 (AIRWORTHINESS STANDARDS: TRANSPORT CATEGORY AIRPLANES) / EASA CS 25 (Certification Specifications Large Aeroplanes)Abu HanifahAbu Hanifah Haji AbdullahPeng Pc
• AC 20-136, Protection of Aircraft Electrical/Electronic System Against the Indirect Effects of Lightning, March 5, 1990 5/22/00 AC 25-23 Page 3 • AC 20-138, Airworthiness Approval of Global Positioning System (GPS) Navigation Equipment for Use as a VFR and IFR Supplemental Navigation...
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摘要: Reports on the US Federal Aviation Administration's (FAA) proposed revision of structural load design requirements for transport-category airplanes in order to eliminate the differences with corresponding requirements for aircraft certificated under Europe's Joint Aviation Authorities (JAA)....
Production: Assembly is performed at BAe's Woodford plant. Twenty RJs were delivered in 1998, and production continues at a rate of 20-25 aircraft per year. Ordered: 154 Delivered: 131 RJX In February BAe Regional Aircraft gained authority to offer an upgraded, re-engined version of the Avro...
Certification basis (LSA, Part 23, Part 25, Military). • Ease of manufacturing (how will it be produced). • Maintainability (tools, labor, and methods required to maintain the aircraft). • Initial cost estimation. • Evaluation of marketability. ...
The aircraft offers up to 25% reduction in fuel consumption and emissions and can fly 7,200 nm or 13,300 km non-stop. Seating capacity for the Group’s A330neo will consist of 300 seats within two cabin classes (Business and Economy). Ewen McDonald,...
(ARINC) document 610, Guidance for Design and Integration of Aircraft Avionics Equipment in Simulators (as amended). End Information 2. Applicability (§§60.1 and 60.2) Begin Information No additional regulatory or informational material applies to §60.1, Applicability, or to §60.2, Applicability ...
able aircraft transfer function and attenu- ation curves. Testing must cover the fre- quency band of 10 kHz to 8 GHz. (e) Equipment HIRF Test Level 3. (1) From 10 kHz to 400 MHz, use conducted susceptibility tests, starting at a minimum of 0.15 mA at 10 kHz, increasing 20 ...