Fuselage a. Window and windshield frame structure, but excluding the windows and windshield. Exterior skins, doublers, circumferential frames but excluding all systems, fairings, insulation, lining and decorative clips and brackets.
b. Engine mount support box structure and machined pylon attachment fittings. Primary structure frames around body openings for passenger door, baggage door, avionics door, flying control access door, APU access door and emergency exits.
c. Nose landing gear well structure, including wheel well walls, ceiling, pressure bulkheads and pressure floor structural components at fuselage wing cutout.
Fuselage. (1) Dents, corrosion and abrasions, or any loose, pulled or missing rivets shall be within the limits of Lessee's maintenance manual. External patches shall be of a type consistent with industry standards and approved by Lessee's maintenance manual. Each repair will have proper documentation of structural repair manual reference and/or engineering repair drawings or documentation as applicable.
(2) Windows shall be serviceable in accordance with Lessee's maintenance manual. Visibility through windows will meet standard industry standards.
(3) Doors shall be free moving, correctly rigged and be fitted with serviceable seals, in accordance with Lessee's maintenance manual limits.
(4) Exterior logos will be removed pursuant to Exhibit E hereto, by stripping or sanding off the present logo, and repainting to blend with existing exterior paint in accordance with standard industry practices.
(5) Unpainted metal surfaces shall be clean and buffed.
Fuselage. External surface skins and doublers, stringers, circumferential frames between forward pressure bulkhead and aft pressure dome, excluding all systems, insulation, lining and decorative clips and brackets.
Fuselage. 3.1 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 doubters, 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 Sxxxx 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. Frames, plating, stringers and pressure bulkheads, but excluding all non-load carrying access doors.
Fuselage. (1) Dents, corrosion and abrasions, or any loose, pulled or missing rivets shall be within the limits of Lessor's (upon delivery) and Lessee's (upon return) maintenance manual. External patches shall be of a type consistent with industry standards and approved by Lessor's (upon delivery) and Lessee's (upon return) maintenance manual. Each repair shall have proper documentation of structural repair manual reference and/or engineering repair drawings or documentation as applicable.
(2) Windows shall be serviceable in accordance with Lessor's (upon delivery) and Lessee's (upon return) maintenance manual. Visibility through windows will comply with industry standards.
(3) Doors shall be free moving, correctly rigged and be fitted with serviceable seals, in accordance with Lessor's (upon delivery) and Lessee's (upon return) maintenance manual limits.
(4) Exterior logos will be removed pursuant to Exhibit F hereto, by stripping the present logo, and repainting to blend with existing exterior paint in accordance with Lessor's (upon delivery) and Lessee's (upon return) standard maintenance manual practices.
(5) Unpainted metal surfaces shall be clean and buffed.
Fuselage. (a) External surface skins and doublers, stringers, circumferential frames between forward pressure bulkhead and aft pressure dome, excluding all systems, insulation, lining and decorative clips and brackets;
(b) Window and windshield structure but excluding the windows and windshields;
(c) Primary structure frames around body openings for passenger doors, cargo/baggage doors and emergency exits;
(d) Nose gear support structure;
(e) Floor beams and supporting structure in the flight compartment and cabin including the lavatory, excluding seat tracks in both areas;
(f) Forward pressure bulkhead and aft pressure dome; and
(g) Floor beams and supporting structure in the baggage compartment providing same is not damaged through abusive handling of baggage or cargo.
Fuselage. Windows and Doors. The fuselage shall be free of major dents and abrasions, scab patches and loose or pulled or missing rivets. Paint will be touched up. Windows shall be free of delamination, blemishes, crazing and shall be properly sealed. Doors shall be free moving, correctly rigged and be fitted with serviceable seals.
Fuselage. Window and windshield frame structure, but excluding the windows and windshield. Exterior skins, doublers, circum-ferential frames but excluding all systems, fairings, insulation, lining and decorative clips and brackets.
Fuselage
