2006 CESSNA Citation Bravo SOLD

AIRFRAME Total time: 1604 hrs Total landings: 1563 ENGINES Model: Pratt Whitney Canada PW530A Serial Number: PCE-DA0679 (L), PCE-DA0678 (R) Total Time: 1604hrs (L), 1604hrs (R) Cycles Since New: 1563 (L), 1563 (R) Next OH due in: 2396 hrs (4000hr TBO) Next HSI due: 1175 (2000hr MPI / Borescope) MAINTENANCE INSPECTIONS Phase 1-4 c/out 21st Oct 2022 at 1511.0 hrs / 1499 Ldgs – next due 1811.0 (1811:00) Hours or 31st October 2024 Phase 5 c/out 15th Nov 2021 at 906:42 hrs / 984 Ldgs – next due 2106.7 (2106:42) hours or 30th Sept 2024 Engine ‘Minor’ Inspections, plus Oil Filter replacements carried out recently. AVIONICS CONNECTIVITY Primus 1000 Integrated Avionics System Primus 660 Weather Radar Honeywell Mark Vii Enhanced Ground Proximity Warning System (EGPWS) Dual Garmin GTX 3000 (Mode S) TCAS II With Software Change 7.1 Universal UNS-1L Flight Management System Garmin GTN625Xi Avidyne EX 500 Multi-Function Display Flight Data Recorder Cockpit Voice Recorder Artex C406-2 Three Frequency ELT With Navigation Interface Safe Flight N1 Computer Pulselight System 2401 With TCAS II Interface Ground Dispatch Power Switch Cockpit Speaker Mute Switch 500W/115VAC Inverter located outside pressure vessel EQUIPMENT OPTIONS Locking Fuel Caps, Ski Tube, Tail Flood Lights. ADDITIONAL EQUIPMENT INFORMATION Permanent Data Transfer Unit – Universal Mark VII Enhanced Ground Proximity Warning System (EGPWS) – Honeywell KHF – 950 Provisions Only – Honeywell Cockpit Speaker Mute Switch UNS-1L (Exchange) – Universal JAA Flight Data Recorder (Provisions Only) – Honeywell Teledyne Controls C406-2 three frequency ELT with Navigation Interface (Exchange) – Artex N1 Computer – Safe Flight Panel Layout Bravo 550-MSPEC-1-02 TCAS II With Software Change 7 Pulselight system 2401 with TCAS II Interface Provisions only for Garmin GPS-400, coupled switched with #1 FMS GPS-400 to have primary means Oceanic/Remote Operations capability. Locate TCAS processor JAA FDR provisions (with ski tube installed) in the tailcone. Mode S Diversity Transponders with enhanced surveillance in lieu of optional transponders installed with TCAS II Light – Tail Flood Refrigerant Type Supplemental Cooling Locking Fuel Caps (Exchange) Install Encode ski tube. 500W/115VAC Inverter located outside the pressure vessel Interior/Exterior Aircraft Specification Revision Basic Ground Dispatch Power Switch Modifications: CAS 67B TCAS II System (Change 7.1) Avidyne EX 500 Multi-Function Display