2014 bombardier learjet 75 -...

4 Dominion Drive IBuilding 3, Suite 200 ISan Antonio, TX 78257ITel 210-687-1828 IFax 210-687-1826 Iwww.ExpressJets.com

2014 Bombardier Learjet 75 Serial Number 485, Registration No. N752R


2014 Bombardier Learjet 75 Serial Number 485, Registration N752R

About the Aircraft Flying faster and further with a full passenger and fuel capacity than any of its nearest competitors, the Learjet 75 has just raised the bar. It’s impressive 2,040 nautical mile range carries you 200 nautical miles further than the nearest competitor, and does so with the lower direct operating costs in its class.

Based in Memphis, Tennessee, this beautifully appointed aircraft features Vision Flight Deck and Garmin G5000 Avionics, WiFi, XM Weather and Radio and Airshow Lite. Cabin seats track, swivel, recline, and allow for the longest seated length of any competitor in the light jet category.

Airframe 859 Total Airframe Hours 624 Total Airframe Landings

Engines

Honeywell TFE731-40BR Enrolled on Honeywell MSP ($276.63 Per Hour/Eng) 859 Hours Since New 624 Cycles Since New

APU Honeywell RE100 (LJ) Enrolled on MSP ($81.36 Per Hour) 398.3 Hours Since New 682 Cycles Since New

Specificationsaresubjecttoverificationuponinspection. Aircraftsubjecttopriorsaleorremovalfrommarket. Thespecificationsarefor introductorypurposesonly, the information is innowayawarranty fromExpress Jetsor theownerof theaircrafton thevalidityof the information. Buyer should relyon theirowninspectionandverificationsoftheabovelistedinformation.



Avionics Bombardier Vision Flight Deck w/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) Emergency Locator Transmitter (ELT) Dual 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) Flight Information System Synthetic Vision Systems (SVS)

(continued) Standby Instrument System GWX 70 Weather Radar Dual VHF Navigation Receivers Rockwell Collins DME 4000 Dual 24 Channel GPS WAAS Receivers Dual GTX 3000 Transponders Garmin GTS 8000 TCAS II with Change 7 Rockwell Collins ALT 4000 Rad Altimeter Terrain Awareness and Warning System (TAWS) Dual Air Data Computers Garmin SATCOM L-3 FA2100 (120 Minute) CVR Artex C406 ELT ESIS GH-3900




Additional Equipment & Options ATG 5000 Broadband WiFi XM Weather & Radio Airshow Lite TOLD Performance Database

Interior Fireblocked interior is a double club configuration certified for nine passengers for takeoff and landing. Elegantly appointed interior features light beige seating with dark beige accents, light beige headliner and sidewalls and darker patterned carpet. High gloss woodwork through cabin, including forward refreshment center, fold out tables and drink rails. Recessed floor, under seat storage, forward bulkhead monitor, individual monitor receptacles, aft belted lavatory.

Exterior Overall white fuselage with accents in varying shades of gray.

Maintenance Status Delivery Date: December 22, 2014 RVSM Compliance FM Immunity / 8.33 COM Compliance MNPS/RNP5/RNP10 Compliance Avtrak Electronic Maintenance Tracking




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 Range at 4 Pax with 2 Crew…………..2,040 nm (3,778 km)

Weights Max Ramp Weight…………………………….….21,750 lb Maximum Take-Off Weight………………………21,500 lb Maximum Landing Weight…………………….….19,200 lb Maximum Zero Fuel Weight………………….…...16,000 lb Basic Operating Weight……………………..……..14,274 lb Maximum Fuel Weight…………………………..….6,062 lb



Cockpit


Forward Galley


Forward Jumpseat


Interior


Aft Lavatory


Exterior



A) Manufacturer warrants to Buyer that at Delivery Time, the Aircraft shall be free from: (i) defects in material, (ii) defects in manufacture, and (iii) defects in design, having regard to the state-of-the-art as of the time of the design of the Aircraft (collectively, the “Warranty”). Manufacturer ’s sole obligation and liability (and Buyer’s sole and exclusive remedy) under this Warranty is expressly limited to correction by repair, replacement or rework of the defective part by Manufacturer at a Manufacturer owned service facility or at a service facility authorized by Manufacturer to perform warranty repairs on Learjet 75 aircraft. For the sake of clarity, the Warranty covers the cost of the replacement part and the labor to perform the repair, replacement or rework, provided the labor hours do not exceed the applicable flat rates established by the Manufacturer from time to time, and in the event no flat rates have been established, the labor hours shall not exceed the usual Manufacturer removal times. Manufacturer ’s obligations under the Warranty are subject to Buyer giving notice to Manufacturer of a claim under this Warranty within the earlier of (i) 90 days of discovery of the defect or (ii) the expiration of the applicable Warranty period specified below.

All costs and expenses associated with repositioning the Aircraft for repairs under the Warranty, and all costs and expenses associated with the return of a defective part covered by this Warranty, shall be at Buyer’s expense. For the full Warranty to apply, Manufacturer must receive defective components within the period specified in the Parts Logistics Price Catalog. B) Subject to the terms in this Addendum 1, the Warranty offered by Manufacturer for the Aircraft (excluding the Engines and APU) shall be for sixty (60) months or 5,000 flight hours, whichever first occurs, from the date title to the Aircraft is transferred from Manufacturer to Buyer, except that:

i.  the Warranty with respect to the Completion Work shall be for twenty-four (24) months or 1,000 flight hours, whichever first occurs, from the date title to the Aircraft is transferred from Manufacturer to Buyer; and

Addendum 1: Warranty Information



ii.  the Warranty with respect to the windshield shall be for sixty (60) months or 2,500 flight hours, whichever first occurs, from the date title to the Aircraft is transferred from Manufacturer to Buyer; and iii. the warranty with respect to the cabinets, excluding veneer and finish, shall be sixty (60) months or 2500 flight hours, whichever first occurs, from the date title to the Aircraft is transferred from Manufacturer to Buyer.

For Warranty purposes, Completion Work is hereby defined as: (i) the exterior paint, (ii) all interior systems, components, parts, and furnishings, including but not limited to those installed in the Aircraft from the cockpit curtain back to the aft baggage bay wall (excluding cabinets), (iii) all vendor components that support the aforementioned items and (iv) cabinet veneer and finishes. The Warranty with respect to emergency batteries will be for twelve (12) months or 500 flight hours, whichever first occurs, from the date title to the Aircraft is transferred from Manufacturer to Buyer.

C)  Buyer shall be entitled to claim a repair, replacement or rework pursuant to this Warranty for a defective part provided:

i.  The Aircraft has been operated and maintained in accordance with Manufacturer ’s approved Flight Manual, Maintenance Manual and Service Bulletins, as each may be amended from time to time by Manufacturer; and

ii.  An installation, repair, alteration or modification to or of the Aircraft made by Buyer or a third party other than Manufacturer is not the cause or a contributing cause of the defect; and

iii.  The Aircraft has not been subject to misuse, abuse, damage or accident, and has not been improperly stored or protected against the elements when not in use.

D) Notwithstanding any other provisions to the contrary, the Warranty shall not apply to the engines or the APU installed on the Aircraft. The engine and APU warranties are provided directly by the engine and APU manufacturers to Buyer, shall be the sole responsibility of the manufacturers, and the rights of Buyer with respect to the engines and APU shall be a matter as between the engine or APU manufacturer and Buyer. Buyer agrees that Manufacturer




shall have no obligation or liability for the engines or the APU including, without limitation, the warranty for the engines or APU, service bulletins for the engines and APU, and/or any lack of performance, reliability or maintainability of the Aircraft as a result of the engines or APU. The Warranty takes into account usage on life- limited and time tracked parts. Life-limited and/or time tracked components (e.g. batteries, brakes, starter generators, landing gear, stabilizer actuators, etc. as referenced in Chapter 5 of the aircraft maintenance manual), will be covered under this Warranty on a pro-rata basis, with Buyer paying for the consumed portion of the parts and labor, and the Manufacturer paying the unused portion at the time of replacement. i.  This Warranty also excludes the following:

Scheduled maintenance and scheduled inspections; all fuel, landing fees, applicable taxes, tariffs, duties, freight, crew expenses and insurance; rental exchanges or the labor associated with rental exchanges, including tooling and/or test equipment provided as a rental; Ground Support Equipment including engine, pitot/static covers; rigging or calibration of any system requiring adjustments after 300 hrs time in service; abuse, accidents, or acts of God; missing parts (parts lost or misplaced after delivery of the Aircraft).

Supplies necessary for airplane cleaning, servicing and replenishment of toilet supplies, fuel, oil, hydraulic fluids, liquid deicing systems, windshield rain repellant, oxygen system, sealant of any type, bonding wires, jumper wires, bonding straps, and other consumables; items or components, which experience normal wear and tear, corrosion, or erosion caused by operational use of the Aircraft, or exposure to environmental elements, regardless of time in service; windshield crazing; silk covered items, metallic paint color matching, or interior plating (other than satin nickel plating); light bulbs, lamps, LED’s, light strips, diverter strips, fuses and current limiters, lenses, filters, gaskets, seals (such as door, panel or fairing seals), o-rings, back-up rings, static wicks, fasteners, nut plates, dome nuts, rivets, placards, bearings, bushings, tires, and other consumables and expendables; loose equipment (smoke goggles, maintenance runners, etc.); Schrader valves used on systems requiring regular servicing such as oxygen and nitrogen; any accessory, equipment or part incorporated in the Aircraft, which is not furnished pursuant to this Agreement.

ii.




Vendor-issued service bulletins unless the service bulletin is part of a Bombardier-issued service bulletin; Airworthiness Directives (AD’s), and Advisory Wire(s), unless linked to a Bombardier- issued service bulletin. Foreign object damage (FOD); upgrades to components or software upgrades; preventative maintenance or components changed as a precaution; maintenance errors or improper maintenance; Mobile Repair Party (MRP) travel time and expenses; overtime or premium time labor charges; hangar storage; engineering expense (unless directly associated with a warrantable repair); customer requests for modifications or replacements; flight test expense associated with recertifying and trouble shooting an aircraft, including crew expense; any defect that is discovered after the expiration of the warranty, per paragraph B above; engines or APU, per paragraph D above.

G) Any repair, replacement or rework under the Warranty shall be covered to the extent of the un- expired portion of the applicable Warranty period set forth in this Addendum 1 remaining at the time of such repair, replacement or rework.

H) All costs resulting from the removal of non-defective items (No Fault Found), other than by Manufacturer or Manufacturer’s representatives, shall be paid by Buyer. I) Buyer shall maintain reasonably complete records of operations and maintenance of the Aircraft and shall make such records available to Manufacturer as Manufacturer may reasonably require. If Buyer fails to maintain such records Manufacturer shall be relieved of its Warranty obligations to the extent that such failure affects Manufacturer ’s obligations under this Warranty provision. J) The Warranty is accessory to the Aircraft and follows the rights to the Aircraft without requirement of Manufacturer ’s approval for transfer. The Warranty is for the benefit of Buyer, its successors and all persons to whom title to the Aircraft may be transferred during the Warranty periods set forth herein, provided that any successor or owner shall remain subject to the applicable terms of the Warranty to the same extent as the Buyer.

iv.

iii.


2014 bombardier learjet 75 -...

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