STATE-OF-THE-ART DESIGN
• Seat design merges the essentiality of an economy class with comfort of a business class
• Seat platform can be fitted into Airbus and Boeing long range aircraft
• High number of options to satisfy the majority of customizations, typical of long range cabin application
• Maximum optimization of passenger living space
• Increased passenger comfort by means of improved cushions foams and ergonomic backrest shape
• Major IFE and In-Seat Power systems can be accommodated with a backrest monitor up to 13” and in-arm monitor up to 11”
• The seat electronic boxes are stowed into the central console to provide free space to stretch the passenger legs
• High strength aluminium alloy primary structure optimized by FEM analysis
• Structure and mechanism validated by dynamic, static, cyclic and abuse testing
STANDARDS FEATURES
- Leather or fabric covers
- Polycarbonate rear backrest shell
- Backrest integrated literature and amenity pockets
- Central console with lateral amenity pockets
- Cocktail table
- Bottles holder
- In-arm table single leaf 17” x 9.5”
- Polyurethane foam cushion with fire blocking core
- Injection moulded bumper
- Die-casted armrest, coated with powdered paint
- Polyurethane armcaps
- Quick release track fittings
- Anti-rattle device on front fitting
- Auto-aligning seat belt attachments
- Life vest pocket made by fabric with red pull strap
- Mechanically controlled backrest recline up to 8”
- Antimacassar Velcro
OPTIONAL FEATURES
• Customized trim & finish
• Rear footrest three ratchet positions
• Coat hook integrated in the backrest side
• Customized antimacassar
• Customer logo (on backrest cover, antimacassar and seat belts)
• In-arm table with PED holder
• Four ways headrest with foldable ears
• Life vest pocket made by soft plastic material with transparent inspection windows and sealable door
QUALIFICATIONS
– ETSO/TSO C127a
– CS/FAR 25 Appendix F part I, II and V
– CS/FAR 25.853 (a) and (c)
– 14CFR part 25 Appendix F parts IV and V / CS 25.853(d) (heat release and smoke emission)
– FAR 121.311 (j) Amendment 121-315 (Full 16g compliance)
– ABD 0031 issue F
– RTCA DO-160E “Environmental Conditions and Test”
