Price
$5,300,000
Aircraft Information
Make: Learjet
Country: Czech Republic
Model: 60-XR
State/Province: Not provided
Year: 2009
City/Airport: Karlovy Vary (LKKV)
Serial No: 60-369
Registration No: M-MARI
Flight Time: 694 hours
Engine Time: 694 hours
Description
Year of Manufacture: 2009
AFTT: 694
Landings/Cycles: 392
Serial #:60-369
Reg. #: M-MARI
Aircraft Base:LKKV
Engine Model:Pratt & Whitney PW305A
Engine 1: PCE-CA0597
Engine 2: PCE-CA0598
APU INFORMATION:
Make/Model: Sundstrand Gemini T-20G-10C3A
Serial #:SP-E080497
TTSN: 397
Starts: 864
CERTIFICATION INFORMATION: RVSM/B-RNAV/P-RNAV/MNPS/RNP-10
EASA/JAR OPS certified
Airframe Maintenance Tracking Program: CAMP
Maintenance
Inspection/ C/W/ next due
Phase A/26-Jul-2013 at 492:30 hrs /26-Jul-2014 or at 792:30 hrs
Phase B/23-Nov-2012 at 299:46 hrs /23-Nov-2014 or at 899:46 hrs
Phase C/31-Jan-2011 at 77:54 hrs/ 31-Jan-2015 or at 1277:54 hrs
Phase D/—/24-Feb-2017 or at 2400 :00 hrs
Avionics
Processing System (IAPS-3000)
Engine Indication System (EIS)
Dual Collins Flight
Management System (FMS-5000) meeting P- RNAV requirements in European airspace and incorporating two each of:
-CDU-3000 Control Display Units
-GPS-4000A GPS receivers
-FMC-5000
-Flight Management Computers
-Enhanced Ground Proximity Warning System (EGPWS) with Windshear
Traffic Collision Avoidance System (TCAS II) inc. dual Mode S transponders with diversity and and certified to Change 7 (ACAS II in Europe)
Attitude Heading Reference System (AHRS-3000)
EFIS with 4LCD 8×10 inch display units
Dual Air Data System (ADS- 850) dual ADC-850D computers, display control panels (DCP-3000) and signal interface adapters (SIA), supports Chartlink and has capability to display Enhanced Map Overlays Graphical Weather on the MFD’s
Dual Audio Systems
Honeywell Avionics KHF-1050 HF Transceiver
Dual Weather Radar System (WXR-840)
Emergency Locator Transmitter (ELT) transmitting on 121.5, 243.0 and 406.025 MHz frequencies.
Maintenance Diagnostic System (MDS)
Category II and RVSM capable FCS-3000 Flight Guidance System (FGS) with digital autopilot
Dual Radio Sensor System (RSS) digital communication and navigation system, each incorporating:
• Radio Tuning Units (RTU- 4220)
• Distance Measuring Equipment (DME-442)
• VHF NAV Receivers (VIR- 432) with SELCAL and 8.33 kHz spacing
• VHF Comm Transceivers (VHF-422C)
• Radio Altimeter (ALT- 4000)
Interior
Seats: 6
Six passenger Executive interior with seats in black and beige leather and woodwork in high gloss maple veneer.
Exterior Description
The exterior features an overall matterhorn white with Tan and Black Accent Stripes.
Additional Features
Integrated Standby Indicator System (ISIS)
Dual digital clocks
Emergency electrical bus system
Landing gear deployment panel Fuel control and status panel
Anti-skid braking and steering status display
Dual inverters
Master warning/caution system with glare shield annunciator and panel-mounted warning lights
System test switch panel and aural warning system
Dual avionics master switches
Oxygen indication located on pilot’s circuit breaker panel
Fuel quantity indicator Digital pressurization
Pitch, roll, and yaw pedestal- mounted trim control panel
Electrically-heatedtailcone baggage system
Hydraulic, emergency air, and anti-ice system indicators located with the system control switch panels
Auxiliary cockpit foot warmers and cabin heaters
Wing ice detection light
Locking tailcone door and baggage door
P&W engine synchronizer
Chip detector
Gear mute and go-around in throttle
Triple pilot heat system
Tailcone maintenance light