Recent Transactions

2003 Bombardier Learjet 45 #227

Airframe:

2700 Hours
2680 Cycles
Certificate of Airworthiness – September 2002
XR Engine Upgrade

Engines:

Left & Right
Description Honeywell TFE731-20BR-1B (BR Engines)
Serial Number P-116454 P-116455
Engine Total Time 2700 Hours 2630 Hours
Engine Cycles 2680 2596
Thrust 3,500 lbs. each
Program Coverage MSP Gold

APU:

Description Honeywell RE100 (LJ)
Serial Number P-125
APU Total Time 980 Hours

Avionics:

The Bombardier Learjet 45 business jet is equipped with a Honeywell Primus 1000 avionics system, including an Electronic Flight Instrument System (EFIS), equipped with an Engine Instrumentation and Crew Alerting System (EICAS), for unparalleled new levels of systems management. The EICAS integrates the multitude of electromechanical instruments that previously were required to display critical engine parameters, offering significant safety and operational benefits. The EFIS, which employs four large displays, presents vital information to the crew in an uncluttered format, simplifying cockpit scan and thereby reducing pilot workload and fatigue. The Primus 1000 is Category II approach capable. Standard features include:

  • EFIS with four 8 x 7 inch (20.3 x 17.8 cm) displays
  • “Dark Cockpit” methodology presents vital information on a “need-to-know” basis, suppressing extraneous data
  • Dual Data Acquisition Units (DAU)
  • Dual Micro Air Data Computers (MADC)
  • Color Weather Radar with rain echo attenuation compensation
  • EICAS provides systems and status information
  • Primus 660 Weather Radar
  • Radio Altimeter & Standby Altimeter
  • Display and Guidance Computers (DGC) integrated with autopilot, flight director, EFIS and EICAS processors
  • Dual Attitude and Heading Reference System (AHRS) Fiber Optic Gyros
  • Dual Honeywell Primus II Integrated Comm/Nav Radios
  • Traffic Collision Avoidance System (TCAS 2000) w/ Upper and Lower Antenna
  • Enhanced Ground Proximity Warning System (EGPWS)
  • Emergency Locator Transmitter (C406-2)
  • Cockpit Voice Recorder (30 Min)
 

Avionics Options:

  • Dual UNS-1C Flight Management System
  • Dual Integrated Comm Unit RCZ-833K (8.33 KHz and Mode S w/Enhanced Surveillance)
  • Data Transfer Unit
  • Single KHF-950 HF Communication with SELCAL
  • Magnastar C2000 Satellite Telephone with 2 handsets
  • Flight Data Recorder (provisions only)

Additional Equipment Options:

  • Airshow 400
  • CD/DVD Player
  • Cabin Audio System
  • Aircraft locking package
  • Exterior Lighting Package
  • Concorde Battery
  • 12.1 Forward and Aft Cabin Monitors
  • Wood Veneer Package, High Gloss Finish
  • 110 Volt Cabin Power System
  • Tail Illumination Package
  • Pulsating Recognition Lights
 

Exterior:

Split Base Paint with Oyster White on the Top and Las Vegas Gold on the Bottom, Platinum and Gold accent stripes in Excellent Condition

Interior:

The Bombardier Learjet 45 cabin has 410 cubic feet (11.6 m3) of volume and 19.75 ft (6.02 m) of length, making it particularly spacious. This translates into more head, shoulder and leg room and an unprecedented level of comfort for eight passengers. This Learjet 45XR features double-club seating for eight (8) passengers and four 20-inch (51-cm) executive tables. The aft lavatory is belted for a ninth (9) passenger seat.

Interior Selections:

  • Wood Veneer – Quarter Striped Sapelle (High Gloss)
  • Carpet – Tan Wool and Mushroom Silk
  • Dado Panel – Townsend Leather Sable
  • Cabin Seats – Townsend Leather; Two Tone Mocha and Sable Leather
  • Headliner – Ultraleather; Milkweed
  • Plating – Satin Nickel

Aft Lavatory:

  • Externally Serviced Flushing Toilet
  • Sink with Tepid Water
  • Toilet Paper Dispenser
  • Belted Toilet Seat Certified for Takeoff & Landing
  • Solid Closing Panel Doors
  • Coat Rod
  • Storage Retention Net
  • Lighted Vanity Mirror
 

Baggage Area:

The Aircraft is equipped with an internal storage area (15 cubic feet, 150 lb) and an external baggage compartment (50 cubic feet, 500 lb).

Maintenance:

Inspection Last Compliance Next Due
Phase A1-A6 6-30-2010 at 2393 ACTT 6-30-2011 or 2693 ACTT
Phase B1-B6 6-30-2010 at 2393 ACTT 6-30-2012 or 2993 ACTT
Phase C1-C6 12-18-2008 at 1862 ACTT 12-18-2012 or 3062 ACTT
Phase D1-D6 6-30-2010 at 2393 ACTT 6-30-2018 or 4800 ACTT
Gear Overhaul New 10,000 Cycles

Weights:

Maximum Ramp Weight 21,250 lb
Maximum Takeoff Weight 21,000 lb
Maximum Landing Weight 19,200 lb
Maximum Zero Fuel Weight 16,500 lb
Basic Operating Weight 14,128 lb
Approximate Fuel Capacity 6,062 lb