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Aircraft Location:Cleveland, Ohio, USA
Seller Information
View Seller InformationGeneral
Year
2006
Manufacturer
Model
Serial Number
2060
Registration #
N133VS
Condition
Used
Description
HIGHLIGHTS
U.S. Registered & Based
Honeywell Primus1000/Primus II Avionics
UNS-1Ew Flight Management System
WAAS/LPV
Engines Enrolled on Honeywell MSP
ADS-B Out
Honeywell TCAS 2000
Honeywell Mark V EGPWS
Honeywell Primus 660 Weather Radar
Airshow 410
Forward and Aft Cabin 10.4” Video Monitors
Cabin Audio / Video System & DVD Player
110 Volt Cabin Outlets
Airframe
Total Time
4,417.9
Total Landings
3,324
Maintenance Tracking
Camp
Airframe
Certification Date August 29, 2006
In-Service Date September 28, 2006
Enrolled on CAMP Maintenance Tracking System
Engine Program
Engine 1 Maintenance Program
MSP
Engine 1
Engine 1 Make/Model
HONEYWELL TFE731-20BR-1B
Engine 1 Serial Number
P-116753C
Engine 1 Time
4,417.9 SNEW
Engine 1 Cycles Since Overhaul
3,324
Engine 2
Engine 2 Make/Model
HONEYWELL TFE731-20BR
Engine 2 Serial Number
P-116752C
Engine 2 Time
4,417.9 SNEW
Engine 2 Cycles Since Overhaul
3,324
Avionics
Flight Deck Manufacturer/Model
HONEYWELL PRIMUS 1000
ADS-B Equipped
Yes
WAAS
Yes
LPV
Yes
Avionics/Radios
Honeywell Primus 1000/Primus II Avionics Suite
Honeywell 4-Tube 7” X 8” EFIS DU-870
Universal UNS-1Ew Flight Management System
Universal LPV Monitor
Dual Honeywell IC-600 Autopilot Computers
Honeywell GC-550 Flight Guidance Control
Dual Honeywell AHZ-800 AHRS
Dual Honeywell DA-800 Digital Acquisition Units
Dual Honeywell RNZ-851/851B NAV (Single ADF)
Dual Honeywell AZ-950 Air Data Computers
Dual Honeywell DC-550 EFIS Control Units
Honeywell LSZ-860 Lightning Sensor System
Dual Honeywell RCZ-833M Comm./Transponders
Dual Honeywell RM-855 Radio Management Units
Honeywell KHF-950 HF Comm System
Dual Honeywell AV-850A Audio Control Panels
Honeywell TCAS-2000 TCAS II
Honeywell RT-300 Radio Altimeter System Transceiver
Honeywell Mark V Enhanced Ground Proximity System
Honeywell Primus WU-660 Weather Radar
Honeywell Cockpit Voice Recorder SSCVR
Artex C406-2 Emergency Locator Transmitter
AVIONICS UPGRADES / CERTIFICATIONS / CAPABILITIES
RVSM Compliant
Class A TAWS
TCAS II
Mode S Enhanced Surveillance
ADS-B Out
VHF Comm. 8.33 MHz Spacing
WAAS/LPV Equipped
Windshear Detection
Additional Equipment
Additional Equipment
Dual Concorde Lead Acid Main Batteries
Flight Deck Rosen Sun Visor System
Keith Products Vapor Cycle Air Conditioning System
Nordam Thrust Reverser Control Box Upgrade
Forward Cabin Bulkhead Galley Rest Seat
KGS SS120C Cabin Inverter
Lighted Control Wheel Chart Holders
Dual Galley Heated Refreshment Dispensers
Lavatory Baggage Cargo Net & Coat Rod
Dual Galley Ice Drawers
External Serviceable Lavatory
Galley Pull Out Work Surface
Single Point Refueling
Cabin Dual Cupholders
Exterior
Exterior
CUSTOM PAINT
White Base
Blue / Bronze / Titanium Stripes
Interior
Number of Seats
7
Interior
INTERIOR CONFIGURATION
Seven Passenger Executive Interior
Seventh Passenger Belted Lavatory Seat
Forward Cabin Four Place Executive Club Seats
Forward Club Seating Executive Tables
Dual Aft Cabin Forward Facing Executive Seats
Aft Cabin Slimline Executive Tables
Forward Galley
Aft Lavatory with Belted Flushing Potty
Lavatory Vanity & Sink
Aft Lavatory Baggage Area
Lavatory Lighted Mirror
Cabin/Lavatory Pocket Doors
Aft External Baggage
ENTERTAINMENT / CONNECTIVITY
Rockwell Collins ICG ePhone SATCOM Phone System
Flight Deck Handset & Cabin Wireless Handset
Audio International DVD Player
Cabin 110 Volt AC Power Outlets
Forward & Aft Cabin Audio International 10.4” Video Monitors
Airshow 410 Cabin Flight Display System
Cabin Audio/Video Touch Screen Controls
Cabin Audio System w/Subwoofer
Inspection Status
Inspection Status
MAINTENANCE STATUS
Phase A (300 Hr): Completed 6/2025 @ 4,227 hrs • Next Due 4,527 hrs
Phase B (600 Hr): Completed 9/2024 @ 4,026 hrs • Next Due 4,626 hrs
Phase C (1,200 Hr): Completed 10/2022 @ 3,518 hrs • Next Due 4,718 hrs
Phase D (2,400 Hr): Completed 10/2022 @ 3,518 hrs • Next Due 5,918 hrs
4,800 Hour Checks: Due at 4,800 hrs
9,600 Hour Checks: Due at 9,600 hrs
Perform Major Landing Gear Inspection 10,000 Hours
L&R Main Landing Gear Strut Assembly-Special Detailed Inspection - 96 Month 10/22 @ 3518 Hrs 10/2030
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