Small Airplanes
Amendment | Effective Date | Subject |
---|---|---|
Part 3 (N) | November 1, 1949 | Reissue of Part 03 with all amendments incorporated |
3-1 | December 7, 1949 | Required fireproof identification plate, location of data plate. |
3-2 | February 6, 1950 | Required safety belts for airplanes manufactured after January 1, 1951, and that belts must be approved. |
3-3 | October 11, 1950 | Eliminated all references to restricted airplanes and adopted a new part, Part 8. |
3-4 | January 15, 1951 | Amended approximate 30 sections of the code dealing with: Service tests, flight tests, performance, stalls, spins, seats, propeller vibration, fuel systems, oil systems, construction, fire protection, position lights. |
3-5 | April 30, 1951 | Amended stall characteristics requirements, stalling demonstration. |
3-6 | June 4, 1951 | Amended stall characteristics requirements, required flight manual entry of altitude losses in excess of 100 feet or any pitch in excess of 30 degrees below level flight |
3-7 | March 4, 1952 | Aerobatic spin requirements, instrument power, simplified structural design criteria, showing of structural integrity by flight tests. |
3-8 | June 23, 1952 | Fuel tank sump requirements. |
3-9 | December 15, 1952 | Correction of References. |
3-10 | May 16, 1953 | Part 3 limited to airplanes of 12,500 pounds or less, equipment, placards, induction system icing, equipment, AFM. |
3-11 | May 17, 1954 | Position lights requirements. |
3-12 | December 18, 1962 | Applicable requirements, type certificate, fire precautions. |
3-13 | August 25, 1955 | Items of mass, fuel oil ratio, placards, weight, gust loads, automatic pilot systems. |
3-14 | March 13, 1956 | Annual Airworthiness Review of 1955, incorporation of results; firewall, fire protection, design weight, seats, berths, position lights, fuel system, placards. |
R-391 | May 1, 1953 | Application of Transport performance requirements to the C-46 airplane. |
Last updated: Wednesday, June 22, 2022