N755VT - 1990 LEARJET 55C
Aircraft Summary
General
Year
1990
Manufacturer
LEARJET
Model
55C
Serial Number
55-142
Registration #
N755VT
Condition
Used
Airframe
Total Time
5309.0
Engine Program
Engine Program Notes
TFE731-3AR-3B
Left: 5237.7, CYC: 2869
Right: 5197.7, CYC: 2846
On MSP
Avionics
Avionics/Radios
COMM: DUAL COLLINS VHF-22A
NAV: DUAL COLLINS VIR-32
DME: DUAL COLLINS DME-42
ADF: COLLINS ADF-60
ADC: DUAL COLLINS ADC-85L AIR DATA COMPUTERS
TRANSPONDER: DUAL COLLINS TDR-90 MODE C **STC CERTIFIED FOR RVSM OPERATIONS**
RADAR: COLLINS WXR-350
RADAR ALTIMETER: COLLINS ALT-55B
HF: KING KHF-950
TCAS: ALLIED SIGNAL CAS-66A TCAS 1
LONG RANGE NAV.: DUAL UNS-1D FLIGHT MANAGEMENT SYSTEMS
EGPWS/TAWS: KING KGP 860 ENHANCED GRND PROX. WARNING SYSTEM
AUTOPILOT/FLIGHT DIRECTOR:
COLLINS APS-85 AUTOPILOT WITH AC-585 AUTOPILOT CONTROLLER
COLLINS 85L 5 TUBE EFIS FLIGHT DIRECTOR DISPLAY SUITE
Additional Equipment
Additional Equipment
2 BOTTLE OXYGEN SYSTEM WITH EROS QUICK DON MASKS
ARTEX C406-2 ELT
COLLINS PRE-80L ALTITUDE PRESELECT
SPPR SINGLE POINT REFUELING SYSTEM
AERONCA THRUST REVERSERS
500# BAGGAGE COMPARTMENT
INTERVOX II INTERCOM SYSTEML55-R PASSENGER BRIEFING SYSTEM
SELCAL 5 SELCAL DECODER
CABIN MOUNTED AIRSHOW DISPLAY
FLITEFONE WITH 2 HANDSETS (COCKPIT, CABIN)
MANUALLY ADJUSTABLE WINDOW SHADING SYSTEM
APR AUTOMATIC POWER RESERVE SYSTEM
AUTOSPOILER SYSTEM
Exterior
Exterior Notes
Painted 7/17/2014 WHITE WITH Red, Black, and Grey stripes.
Interior
Interior Notes
Forward Two Place Divan, Tan Leather. Headliner And Sidewalls In Light Tan Leather, With Lower Sidewalls A Combination Of Fabric And Textured Tan Carpet To Floor. Configured For 7 Passenger Seating With 2 Foldout Desks/Workstations Centrally Located. Aft Full Lavatory Area With Privacy Sliding Door. Full Aft Galley Area Containing 2 Drawer Refreshement Center, Portable Coffee Container, Large Drink Cooler. Full Hot/Cold Sink And Vanity Area With Overhead Flourescent Lighting For Vanity And Mirrored Cabinets. 110 Volt Accessory Charging Receptacle Located At Vanity.
Modifications/Conversions
Modifications/Conversions
*AAK 84-6 MODIFICATION:
21,750 MAX RAMP WEIGHT
21,500 MAX TAKEOFF WEIGHT
18,000 MAX LANDING WEIGHT
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