2006 Cessna Citation Bravo Jet Aircraft (SOLD)

Low Time, Two Owners Since New, No Known Damage History, European Based, Primus 1000 Integrated Avionics System.

Type:
Airplane (Jet Aircraft)
Manufacturer:
Cessna
Model:
Citation Bravo
Year:
2006
Serial Number:
550B-1130
Reg. Number:
G-JHEX
Total Time:
1,604 Hours
Seats:
7
Price:
Price upon request

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Description

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