Cockpit door / Airbus C-295
The Cockpit door is located in the forward part of the aircraft separating the cockpit from the main cabin. It is situated between the civil Lavatory and the Emergency rack FR10.
The Cockpit door includes:
One (1) Full-length center hinge
One (1) Full-length side hinge
One (1) Latch
One (1) Guide pin
One (1) Handle
Two (2) Grids
One (1) Bracket roll assy
It has an appealing and comfortable design, which takes into account ergonomic customization and aesthetic requirements for modern cabin environment, and consideration for the human factors related to its operation. Materials used are of the highest quality and lightest weight consistent with the applicable design requirements. Materials used meet flammability and environmental airworthiness requirements. All metallic materials are adequately protected against corrosion of any origin using only qualified methods and processes.
options
Customized trim & finish
Inserts combination
design
Light weight
Long life and high reliability
Low cost maintenance
Easy maintenance and inspection
Good compactness
Maximum efficiency and safety
Airworthiness compliance
Main equipment
One (1) Full-length center hinge
One (1) Full-length side hinge
One (1) Latch
One (1) Guide pin
One (1) Handle
Two (2) Grids
One (1) Bracket roll assy
certification / qualification
Flammability requirements
according with 14 CFR 25.853 and CS 25.853Environmental requirements
according with RTCA DO-160 ()Static loads requirements
according with CS 25.561 (d)
