Program Auxiliary Power Unit (APU) SIN P-I27: 5543 TT (Not enrolled in MSP) Avionics/Radios: Honeywell SPvZ-8500 Cockpit Suite integrated Three Honeywell Flight Management Systems at Software Level 6.0 Third IAC-800 installed for NZ-2000 function FMS CDUs upgraded to CD-820 Dual 12 Channel Global Positioning Satellite Syste

nications System (SDCS), interfaced to the existing Airborne Flight Information System (AFIS). The AFIS system is integrated with the GAC installed Honeywell Flight Management Systems providing complete flight plan and weather information through self-contained VHF COMM data link with the Global Data Center. The SDCS is interface