Modification in the leading edge slat and trailing edge flap configurations and installation of an external mixer nozzle to each engine.
Modification in the leading edge slat and trailing edge flap configurations and installation of an external mixer nozzle to each engine.
Please contact modification supplier for further details.
STC Status: Amended
STC Date: 16/11/99
Responsible Office: Seattle Aircraft Certification Office (ANM-100S), Tel: (425) 917-6400
Boeing Company, The