1984 Lear 55

Aircraft Information
Year: 1984
Make: Lear
Model: 55
Serial #: 55-0101
Registration #: N112WQ
Airframe Hrs. Total Time: 9,153.8
Landings: 7,349
Price: Make Offer
Contact Number: 1-847-726-5000
Description

Interior:
Seven passenger interior completed in Tan leather, consisting of four place club seating area and aft three place couch. The interior is complimented by Cherry Satin laminate cabinetry, Satin Nickel hardware, Tan small closed-loop carpet and Off-White Ultra Leather headliner. Forward refreshment center is on the left hand side, forward of the entry door. There is a double door and large closet/baggage area on the right hand side. The two fold-open doors lock in the open position and con­tains a pull out lavatory. The cockpit, forward baggage compartment and aft interior storage areas were last redone in May 1998. The cabin seats, carpet and drink rail leather were last redone in Au­gust 1999. The window revels, PSU and headliner were redone in 2003 with Ultra Leather. The wood laminate was redone in December 2004.

Exterior:
Upper fuselage completed in Matterhorn White, lower fuselage and wings completed in Aristo Blue.  Forward and aft stripes completed in Aristo Blue and Gold.

Engines
LeftRight
Make: HoneywellHoneywell
Model: TFE731-3CTFE731-3C
Engine Program: On MSPOn MSP
Hrs. Total Time: 9,145.89,145.8
Cycles Since New: 7,3407,340
Hrs. CZI: 914.8914.8
Hrs. MPI: 914.8914.8
Avionics
Traffic Collision Avoidance System: Honeywell TCAS II with Change 7
Autopilot: J.E.T. 550
CVR: CVR-30
COMMS: Dual Collins VHF-22B
Electronic Flight Instrument System: 5-Tube Collins EFIS-85
Flight Director System: Dual Collins FDS-85
Flight Management System: Dual Universal UNS-1D w/Version 603
NAVS: Dual Collins VIR-32
ADF: Dual Collins ADF-60
Transponder: Dual Collins TDR-90
High Frequency: King KHF-950
Radar: Honeywell P400SL
Flight Phone: MagnaStar C-2000
DME: Dual Bendix DME-42
Radar Altimeter: Collins ALT-55
Enhanced Ground Proximity Warning System: Honeywell Mark VIII
Additional Features
  • IS&S Dual Air Data Display Unit
  • Aerosonic Stand-by Altimeter
  • IDC SAT/TAS
  • J.E.T. AI 804 Stand-by Altitude Indicator
  • Phase I & IA
  • Dual Davtron Clocks
  • Engines Upgraded with 3C Mod
  • 21,500 lb. Max Take Off Weight
  • Thrust Reversers
  • Dual Concord Batteries
  • Digital Electronic Engine Controls
  • APR/Auto Spoilers
  • Single Point Refueling with Fuel Heaters
  • Long Range Fuel 7,707 lbs.
  • Motorola NA-135 SELCAL
  • Universal UL-601 Unilink
Maintenance
  • On CAMP
  • 3,000 Landing Inspection due at 8,921 Landings
  • 6,000 Landing Inspection due at 11,921 Landings