Primus Elite 2000XP Integrated Avionics System – (3) IC-800 Integrated Avionics Computer – (3) AZ-940 Air Data Computer – (2) HF-9031A HF Receiver – (4) DA-810 Data Acquisition Unit – (2) WC-880 Radar Control Panel – HST-2110 High Speed Transceiver – (6) DU-875 LCD Display Unit – (3) ALT-4000 Radio Altimeter Transceiver – SRT-2100 Satcom Transceiver – (3) CD-820 Control Display Unit – (2) RNZ-851 Navigation Receiver – SSFRD Flight Data Recorder – (3) LASEREF IV Inertial Reference Unit – (2) RCZ-833M VHF Comm. Unit – HFR5-V Cockpit Voice Recorder
– HUD/EVS – TCAS 7.1 – CPDLC / FANS 1/A+ – SBAS w/ LPV – Synthetic Vision – Datalink 2000 – EGPWS w/ Windshear Detection and RAAS – Batch 3.4 (SB700-1A11-31-021) – Increased MTOW to 92,500 (SB700-1A11-11-008) – Flap Corrosion & Drainage (SB700-1A11-57-016, -019, -020) – Collins Cabin Electronics System (CES) – FWD RH 24” bulkhead monitor – AFT LH 24” bulkhead monitor – 21” stowable credenza monitor – Gogo Biz AVANCE L5
PAX – 13 Galley – FWD with microwave, oven, and coffee maker FWD – Four club seats AFT – Four place conference group opposite credenza MID – Two club seats opposite three place divan Lav – FWD crew and AFT cabin lavatories
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