1979 Lear 35A

Aircraft Information
Year: 1979
Make: Lear
Model: 35A
Serial #: 35A-0258
Airframe Hrs. Total Time: 10,251
Landings: 9,162
Price: Make Offer
Contact Number: 1-847-726-5000
Description

2005 has brought new changes to business jet travel.  The FAA has mandated several avionics upgrades that can cost up to $300,000.00.  This Learjet 35A is one of the few that is 100% compliant with all these FAA mandates including RVSM & TAWS.  This aircraft has just undergone a fresh 12 year inspection and web sheer mod.  This Lear 35A features a stunning 2004 new interior in neutral colors.  This is truly a turn-key, no excuses airplane.  Currently operating on a 135 Charter Certificate and maintained to the highest standards.

Exterior

The exterior of this Learjet is overall white with gray and blue stripes.  The paint was completed in 1995.

Interior

The fireblocked interior of this 35A features four individual seats, a three-place rear divan and a left hand side-facing seat with toilet provisions. Seats are completed in Chambray leather with silver/gray wool carpeting and light gray headliner. Cabinetry is located mid-cabin, also this interior features an Airshow 400. The Lear's interior was completed by Cameron Aircraft in December 2003.

Interior 2

The fireblocked interior of this 35A features four individual seats, a three-place rear divan and a left hand side-facing seat with toilet provisions.  Seats are completed in Chambray leather with silver/gray wool carpeting and light gray headliner.  Cabinetry is located mid-cabin, also this interior features an Airshow 400.  The Lear's interior was completed by Cameron Aircraft in December 2003.

 

Engines
RightLeft
Model: TFE-731-2-2BTFE-731-2-2B
Serial #: P74722P74716
Engine Program: MSP GoldMSP Gold
Hrs. Total Time: 9,92610,047
Cycles Since New: 8,8178,878
Hrs. CZI: 1793,618
Hrs. MPI: 303779
Avionics
Autopilot: Jet FCS-200
ELT: Artex G406-1 (installed 11/03)
CVR: Fairchild A100
Global Positioning System: Bendix King KLN 900
COMMS: Dual Collins VHF-20
Flight Director System: Collins FD109 & FD108
NAVS: Dual Collins VIR-30
ADF: Dual Collin ADF-60
Transponder: Dual Collins TDR-90
High Frequency: Bendix King KHF-950
Radar: Honeywell Primus 400-Color
Flight Phone: Wulfsburg VI
DME: Collins DME-40
Enhanced Ground Proximity Warning System: Sandel TAWS
Additional Features
  • Executive Door
  • Aeronca Thrust Reversers
  • RVSM
Maintenance
  • Emergency Air Bottle Hydrostatic Inspection complied with May 2005
  • On CAMS Reporting System
  • Capacity Check the PS-823 completed May 2005
  • 25 Month Wing Fuel Flapper Valve Inspection complied with May 2005
  • Left Engine 800 Hour Inspection complied with May 2005
  • Capacity Check Main Aircraft Batteries completed May 2005
  • Phase A complied with August 2003
  • Phase B - D complied with August 2002
  • 12 Year complied with January 2004 @ 9707 Hrs.
  • Sheer web inspection complied with March 2004
  • 300 Hour Airframe Inspection complied with May 2005
  • Accomplished AD82-01-05 (Stall Warning Accel Check)
  • Weight Check the Engine Fire Bottles completed May 2005
  • 1,500 Hour Hydraulic Hose Replacement completed May 2005