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Beechcraft King Air C90GTx |
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¸Å¿ö | ÀàÐÍ: | ÎÐÂÖÂÝÐý½°·É»ú | Æ·ÅÆ: | Beechcraft | ÐͺŠ1: | King Air C90GTx | ÖÆÔìÄê: | 2010 | ×¢²áºÅ: | EASA-reg. | ϵÁкÅ: | tbs | ÊôÐÔ: | ±»IFR¼ø¶¨µÄ ±»IFR×°±¸µÄ ʼÖÕ£¨Ò»Ö±£©Í£ÁôÔÚ»ú¿â | µØµã: | Ó¢¹ú | ʱ¼ä×ܼÆ: | 1395 h | ¼Û¸ñ: | ѯ¼Û | Å·ÃËÔöֵ˰: | ÊÇµÄ | Ôöֵ˰¹æ¶¨: | ¶Ô | ϸ½Ú |
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TAS TOP-A-SERVICES LTD (UK) Alf Kuenzl Richmond House, Walkern Road Sales Office Austria - see phone Herts SG1 3QP Stevenage Ó¢¹ú
µç»°: +447492912111 ´«Õæ: +43 699-31169215 ÒÆ¶¯µç»°: +43 699-11169215 |
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¸Å¿ö | ÀàÐÍ: | ÎÐÂÖÂÝÐý½°·É»ú | Æ·ÅÆ: | Beechcraft | ÐͺŠ1: | King Air C90GTx | ÖÆÔìÄê: | 2010 | ×¢²áºÅ: | EASA-reg. | ϵÁкÅ: | tbs | ÊôÐÔ: | ±»IFR¼ø¶¨µÄ ±»IFR×°±¸µÄ ʼÖÕ£¨Ò»Ö±£©Í£ÁôÔÚ»ú¿â | µØµã: | Ó¢¹ú | ʱ¼ä×ܼÆ: | 1395 h | ¼Û¸ñ: | ѯ¼Û | Å·ÃËÔöֵ˰: | ÊÇµÄ | Ôöֵ˰¹æ¶¨: | ¶Ô | ³Ë¿ÍÊýÁ¿: | 5 | µÇ½: | 1200 |
·¢¶¯»ú£¨¶à¸ö£© | ·¢¶¯»úÊýÁ¿: | 2 | Æ·ÅÆ/ÐͺÅ: | P&WC PT6A-135 | P&WC PT6A-135 | ¹¦ÂÊ: | 550 PS | 550 PS | ×Üʱ¼ä: | 1395 h | 740 h | Time Between Overhaul ???
´óÐÞ¼ä¸ôʱ¼ä (hours): | 3600 h | 3600 h | SNEW: | 1395 h | 1395 h | ÂÝÐý½° Æ·ÅÆ/ÐͺÅ: | Hartzell 4-bladed | Hartzell 4-bladed | ÂÝÐý½°Ê±¼ä 1: | 1395 h SNEW | 1395 h SNEW | ÂÝÐý½°×Üʱ¼ä: | - | 1395 h |
·¢¶¯»úÃèÊö/ϸ½Ú | Engines running fine
Under Engine Maintenance Program ! |
º½¿Õµç×Óѧ | • Two AFD-3010 and one AFD-3010E adaptive flight display (pilot’s PFD, MFD and copilot’s PFD); incorporates an Engine Indicating (EI) system.
• 2 Rockwell Collins VHF-4000 transceivers (118.000 to 136.975 MHz with 8.33 KHz increments), tuning through CDU or Rockwell Collins RTU-4200.
• Rockwell Collins NAV-4000 VOR/LOC/GLS/ADF/Marker Beacon receiver, tuning through CDU or RTU.
• Rockwell Collins NAV-4500 VOR/LOC/GLS/Marker Beacon receiver, tuning through CDU or RTU.
• AHRS – Dual Rockwell Collins AHC-3000 attitude heading reference system including dual FDU-3000 flux detector units, slaved and DG heading modes are provided.
• GPS – Rockwell Collins GPS-4000S Global Positioning System. DBU-5000 data base unit for all database loading. ADC – Dual Rockwell Collins ADC-3010 air data computers. ADF – Rockwell Collins NAV-4000 with ADF, including antenna.
• Transponders – Dual Rockwell Collins (Mode S) TDR-94D ‘Diversity’ transponders with enhanced surveillance and Flight ID, controlled through CDU or RTU. Transponder ATC Ident button on pilot’s and copilot’s control wheels.
• DME – Rockwell Collins DME-4000 with DME information displayed on PFD’s.
• CVR – L3 Communications FA2100-1020-00 cockpit voice recorder with 120 minute recording time.
• Flight Guidance System – dual Rockwell Collins FGC-3000 flight guidance computers, single autopilot system with yaw damper.
• FMS – Rockwell Collins FMS-3000 with single CDU-3000 and navigational inputs from GPS receivers,
•Navigation receivers, and DME. FMS 4.0 software provides LPV approach capability,
• IFIS – Rockwell Collins with IFIS 6.0 software provides enhanced map features to traditional displays (e.g.
rivers, lakes, national boundaries, airway and airspace depictions). A File Server Unit (FSU) is connected to an
Ethernet capable MFD and provides the control interface using a Cursor Control Panel (CCP).
• Rockwell Collins ECH-5000 Electronic Charts software depicting NOTAMS, airport diagrams with aircraft location and approach charts (GPS/ILS). The charts are integrated into IFIS and preloads the electronic charts to match the FMS flight plan.
• SFDS – Meggitt Mark II provides back-up attitude, heading, airspeed, altitude, and Nav with backup battery.
• Rockwell Collins TWR-850 Turbulence Weather Radar incorporates the Doppler principle of frequency shift to detect and display precipitation-related turbulence (up to a 50 nm range). It also features an auto-tilt function target alert mode.
• Rockwell Collins ALT-4000 radio altimeter, measures altitude up to 2,500 feet AGL, displayed on PFD.
• Rockwell Collins MDC- 3110 maintenance diagnostics computer, displays maintenance information on MFD and downloads through the DBU-5000 to memory stick.
• TAWS – ACSS TAWS+ system provides a Class A terrain awareness and warning system display on the MFD in normal mode or PFD in reversionary mode.
• TCAS 1 – (level 1) using L3 Communications Skywatch HP displayed on MFD in normal mode, PFD in reversionary mode. |
×°±¸ | • Checklist display capability – normal and emergency checklists displayed on the MFD.
• Cabin paging – cockpit to cabin paging with four cabin speakers.
• Ground comm switch tied to comm 1 and pilot’s and copilot’s audio.
• Dual hand held microphones.
• Microphone key button on pilot’s and copilot’s control wheels.
• Static wicks.
• Emergency Locator Transmitter Artex ELT C406-2 with cockpit switch.
• White lighting. Avionics master switch. Lighted panels.
• COLLINS ALT-55B RAz
• Audio system – dual dB 700/dB 800 systems. |
ÄÚ²¿ | excellent and clean - like new |
Inspection Status | up-to-date |
ÆäËû | • Very low time
• One owner since new
• Remaining Beechcraft warranty
• Outstanding interior,
• No damage history
Also can offer a model ea. 2011, 2012, 2014, 2017 - inquire. |
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