2014 Bombardier Learjet 75 airframe: 333. 1 Hours Since New landings: 277 Since New engines
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- ADDITIONAL EQUIPMENT OPTIONS
- EXTERIOR
- Aircraft Includes DX (Diagnostics Express) Ground Support Software and Maintenance Computer Interface Adapter (MCIA) MAINTENANCE STATUS
- PERFORMANCE
2014 Bombardier Learjet 75 AIRFRAME: 333.1 Hours Since New LANDINGS: 277 Since New ENGINES: Honeywell TFE731-40BR Engines - Enrolled on MSP 333.1 Hours Since New 277 Cycles Since New
129.1 Hours Since New AVIONICS: Bombardier Vision Flight Deck with Garmin G5000 Avionics Suite Single 3-Axis Automatic Flight Control Systems with Computation for Flight Guidance, Autopilot, Yaw Damper and Pitch Trim Electronic Flight Instrument System (EFIS) Engine Indication and Crew Awareness System (EICAS) Surface Awareness System; Cockpit Voice Recorder (CVR); and Emergency Locator Transmitter (ELT) Two (2) Flight Management Systems (FMS) supporting Required Navigation Performance (RNP) non- AR 0.3 approaches with radius-to-fix (RF) legs and Precision and non-precision approach operations (e.g. LNAV/VNAV and Localizer Performance with Vertical Guidance (LPV) approaches) One (1) Flight Information System One (1) Synthetic Vision Systems (SVS) One (1) Standby Instrument System One (1) Weather Radar Two (2) VHF Navigation Receivers One (1) DME Transceiver Two (2) 24 Channel GPS WAAS Receivers Two (2) Mode S Transponders Capable of ADS-B Out in Accordance AC 20-165A One (1) Traffic Surveillance System Capable of TCAS II Change 7.1 One (1) Radio Altimeter System One (1) Terrain Awareness and Warning System (TAWS) and Two (2) Air Data Computers.
Single HF Communication with SELCAL Structural/Wiring Provisions - Digital Flight Data Recorder (DFDR) Additional 110V Outlets in Cockpit Lighted Control Wheel Chart Holders Smartphone Handsets - Wired Iridium with ATG Broadband System Galley Rest Seat Media Center Equipment/Furnishings - Modification of Galley and Aft Lavatory Trash Container Door Latches Pneumatic - Removal of the Nacelle Anti-Ice Valve Heat Blanket INTERIOR: Interior accommodates seating for two crew and eight passengers. Crew area features sheepskin covers on crew seats, rail mounted sunvisors, electronically-heated foot warmers, map and dome lights, speakers electronically adjustable rudder pedals, and curtain closeout to cockpit. Forward right galley provides single hot liquid container, one ice drawer with two ice compartments and single overboard drain, 4.3-inch Cabin Management System control panel, iPod 30-pin docking station, trash storage and other miscellaneous storage. Seating for eight passengers is a double club configuration with swivel and reclining capability, inboard armrests, three folding tables, one plug-in table, and flat floor throughout the cabin. Cabin further features arm ledge and lower side ledge storage, convenience panel with reading lights, table lights, air vents and oxygen masks, Four 110V 60Hz Universal AC outlets in main cabin, with fifth in aft lavatory. A life vest is provided at each seat, window shades, drink holders and two wine bottle holders. Entertainment features include Audio System consisting of sidewall cabin speakers, audio amplifier and headset jack at each seat location, Video System with Six 7” popup screens at each seat (less emergency exit club seats), two 4.3” touchscreen controllers at emergency exit club seats, one 12.1” high-resolution flat panel screen LCD monitor installed on left-hand forward cabinet, moving map system with worldwide map selection and an HDMI input port located at the VIP seat. Cabin control capability at each seat provides passenger control panel equipped with table and reading light switches, scroll wheel for means of navigation on the passenger touch screen and one USB charger limited to smart phone charging capabilities. Standard aft lavatory area contains externally serviced flushing toilet, sink with tepid water, paper dispenser, miscellaneous storage and storage retention net, coat rod, and lighted vanity mirror. Aft storage area within lavatory are provides 15 cu ft (up to 150 pounds), and external heated baggage compartment of 50 cu ft provides for up to 500 pounds of baggage. EXTERIOR: Overall Matterhorn White Desoto. LOOSE EQUIPMENT: Pitot Covers One Dorsal Inlet Cover Two Engine Covers Three Jack Pads One Tail Stand One Emergency Door Locking Pin Gust Locks Thrust Reverser Locking Pins One Maintenance Runner for Center Aisle One Entryway Throw Rug and Throw Rugs Between Club Seats Keys for Standard Lock
Certified for CAT I Approaches Certified for Flight Into Known Icing RVSM Compliant Engines & APU Enrolled on MSP, Enrolled on Smart Parts Please See Addendum 1: Warranty Information PERFORMANCE: Take-Off Field Length (SL, MTOW) 4,440 ft (1,353 m) Landing Distance (SL, MLW) 2,660 ft (811 m) Long Range Cruise Speed M 075 (432 ktas) Max Certified Operating Altitude 51,000 ft (15,545 m) Initial Cruise Alt. After MTOW Departure 45,000 ft (13,716 m) Range at 4 Pax with 2 Crew 2,040 nm (3,778 km)
Max Ramp Weight: 21,750 lb (9,866 kg) Maximum Take-Off Weight: 21,500 lb (9,752 kg) Maximum Landing Weight: 19,200 lb (8,709 kg) Maximum Zero Fuel Weight: 16,000 lb (7,257 kg) Basic Operating Weight: 13,890 lb (6,300 kg) Maximum Fuel Weight 6,062 lb (2,750 kg) Specifications are subject to verification. Aircraft subject to prior sale or removal from market. The specifications are for introductory purposes only, the information is in no way a warranty from Express Jets or the owner of the aircraft on the validity of the information. Buyer should rely on their inspection and verification of the above listed information.
4 Dominion Drive Building 3, Suite 200 San Antonio, TX 78257 www.expressjets.com Tel: 210-687-1828 * Fax: 210-687-1826 * E-fax: 210-579-7184 Directory: models models -> Quantifying projected impacts under 2°C warming models -> Concepts For Developing Component-based Systems models -> Jump-start Your Thinking models -> Thor able-star photo captions models -> Famous Journalists in American History models -> A comparison of 1/72 Scale Space Shuttle Kits by Jay Chladek models -> Rockets of the world supplement contents by year models -> Simplifying Autonomic Enterprise Java Bean Applications via Model-driven Development: a Case Study models -> Tcss 343 Master Syllabus Version: April 2011 (Approved: 27 May 2011) Catalog Description Download 20.67 Kb. Share with your friends:
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