Modification of the aircraft inverter system, reducing the inverter system from three (3) inverters to two (2) inverters due to the reduced aircraft S.C. electrical load.
Modification of the aircraft inverter system, reducing the inverter system from three (3) inverters to two (2) inverters due to the reduced aircraft S.C. electrical load.
Please contact modification supplier for further details.
STC Status: Amended
STC Date: 22/03/02
Responsible Office: Chicago Aircraft Certification Office (ACE-115C), Tel: (847) 294-7358
Dassault-Aviation