Repairs assessment for pressurized fuselages.

CFR · 2024-01-01 · US · Title 14

(a) No certificate holder may operate an Airbus Model A300 (excluding the -600 series), British Aerospace Model BAC 1-11, Boeing Model 707, 720, 727, 737, or 747, McDonnell Douglas Model DC-8, DC-9/MD-80 or DC-10, Fokker Model F28, or Lockheed Model L-1011 (1) For the Airbus Model A300 (excluding the -600 series), the flight cycle implementation time is: (i) Model B2: 36,000 flights. (ii) Model B4-100 (including Model B4-2C): 30,000 flights above the window line, and 36,000 flights below the window line. (iii) Model B4-200: 25,500 flights above the window line, and 34,000 flights below the window line. (2) For all models of the British Aerospace BAC 1-11, the flight cycle implementation time is 60,000 flights. (3) For all models of the Boeing 707, the flight cycle implementation time is 15,000 flights. (4) For all models of the Boeing 720, the flight cycle implementation time is 23,000 flights. (5) For all models of the Boeing 727, the flight cycle implementation time is 45,000 flights. (6) For all models of the Boeing 737, the flight cycle implementation time is 60,000 flights. (7) For all models of the Boeing 747, the flight cycle implementation time is 15,000 flights. (8) For all models of the McDonnell Douglas DC-8, the flight cycle implementation time is 30,000 flights. (9) For all models of the McDonnell Douglas DC-9/MD-80, the flight cycle implementation time is 60,000 flights. (10) For all models of the McDonnell Douglas DC-10, the flight cycle implementation time is

official document · source cfr-2024 · id 14:§ 121.1107