Common use of FUSELAGE, WINDOWS AND DOORS Clause in Contracts

FUSELAGE, WINDOWS AND DOORS. (a) The fuselage and doors will be free of major dents and abrasions, loose or pulled or missing rivets in excess of maintenance manual limits and all repairs are Permanent Repairs. (b) Windows will be free of major delamination, blemishes and crazing in excess of maintenance manual limits allowing continued in service operation without special inspection or other action and will be properly sealed. (c) Doors will be free moving, correctly rigged and be fitted with serviceable seals. (d) All external repairs for the pressurised fuselage shall have been reviewed in accordance with the latest revision of the Manufacturer’s repair assessment programme (if issued, and otherwise in accordance with the Manufacturer’s published guidelines) applicable at the time of repair and supported by certified documentation evidencing accomplishment in accordance with EASA or FAA approved data (that is, the Manufacturer’s structural repair manual or the Manufacturer’s service bulletin or the Manufacturer’s written approval or FAA/EASA STC (Supplemental Type Certificate) or FAA Form 8110- 3/8100-9 approval or otherwise approved by the EASA or FAA.

FUSELAGE, WINDOWS AND DOORS. (a) The fuselage and doors will be free of major dents and abrasions, loose or pulled or missing rivets in excess of maintenance manual limits and all repairs are Permanent Repairs.; (b) Windows will be free of major delamination, blemishes and crazing in excess of maintenance manual limits allowing continued in service operation without special inspection or other action and will be properly sealed.; (c) Doors will be free moving, correctly rigged and be fitted with serviceable seals.; and (d) All external repairs for the pressurised fuselage shall have been reviewed in accordance with the latest revision of the Manufacturer’s repair assessment programme (if issued, and otherwise in accordance with the Manufacturer’s published guidelines) applicable at the time of repair and supported by certified documentation evidencing accomplishment in accordance with EASA or FAA approved data (that is, the Manufacturer’s structural repair manual or the Manufacturer’s service bulletin or the Manufacturer’s written approval or FAA/EASA STC (Supplemental Type Certificate) or FAA Form 8110- 3/8100-9 approval or otherwise approved by the EASA or FAA.