Executive Interior consists of;

• Deactivation of the L/H rear emergency exit.
• Addition of a new galley in the forward RHS of the passenger cabin.
• Addition of a new storage cabinet in the forward LHS of the passenger cabin, opposite of the galley.
• The forward and mid cabin areas have 4x executive seats each with folding tables between.
• The aft-cabin area has 2 rows of recovered OEM double seats on the R/H side of the cabin and 3 rows of recovered OEM single seats on the L/H side of the cabin.
• Two mid-cabin partitions have been added which include a curtain between and 1 flat panel monitor in each bulkhead facing aft.
• Behind the aft most L/H seat is a new storage closet.
• The existing lavatory is retained with the wall extended to just fwd of the rear passenger service door.
• A ramp is installed to transition from the fwd cabin’s new floor level to the original aircraft’s sunken floor.
• The headliner, side panels and window shades are replaced
• The existing lighting is replaced by new LED units.
• 1 swivel 7” monitor is fitted at each of the 8 single seat locations in the fwd cabin.

Reduction in Maximum Zero Fuel Weight from 28,814 to 28,279 lbs.

Limitations

This modification is eligible to be installed on aircraft equipped with teh type certified 31 passenger cabin layout with aircraft incorporating MOD 10 Maximum Takeoff Weight (MTOW) increase only.

Please contact modification supplier for further details.

STC Status: Issued
STC Date: February 5, 2009
Responsible Office: Southwest Region

Dornier

• 328-300