Fuselage Structure Sample Clauses
The Fuselage Structure clause defines the requirements and standards for the main body of an aircraft, specifying how it must be designed, constructed, and maintained. This clause typically outlines the materials to be used, structural integrity tests, and compliance with relevant aviation regulations. By setting clear expectations for the fuselage's construction and performance, it ensures the safety and reliability of the aircraft, addressing potential risks related to structural failure.
Fuselage Structure. 3.1.1 Fore and aft bulkheads
3.1.2 Pressurized floors and bulkheads surrounding the main and nose gear wheel well and centre wing box
3.1.3 Skins with doublers, stringers and frames from the forward pressure bulkheads to the frame supporting the rear attachment of horizontal stabilizer
3.1.4 Window and windscreen attachment structure but excluding transparencies
3.1.5 Passenger and cargo doors internal structure
3.1.6 ▇▇▇▇▇ excluding scuff plates and upper beams surrounding passenger and cargo door apertures
3.1.7 Cockpit floor structure and passenger cabin floor beams excluding floor panels and seat rails
3.1.8 Keel beam structure
Fuselage Structure. Fore and aft bulkheads
Fuselage Structure. Fore, [ * ] and Aft pressure bulkheads, [ * ]
Fuselage Structure. Fittings
Fuselage Structure. 3.1.1 Fore and aft bulkheads
3.1.2 Pressurized floors and bulkheads surrounding the main and nose gear wheel well and center wing box
3.1.3 Skins with doublers, stringers and frames from the forward pressure bulkheads to the frame supporting the rear attachment of horizontal stabilizer