Date of Manufacture (CofA): October 2001
Entry into Service: February 2003
Rolls-Royce BR700-710A2-20 On Condition (Task Oriented)
Left (#1): S/N: 12317 5,972 Hours 3,110 Cycles
Right (#2): S/N: 12316 5,972 Hours 3,110 Cycles
Honeywell RE220-GX S/N: P-208 4,850 Hours 5,855 Cycles
Major Aircraft Enhancements & Upgrades
- IAC BATCH 3.4 Software Upgrade (SB 700-31-030): FMS 6.1, RNP 0.3, Vertical Glide Path (VGP) mode (LNAV/VNAV), FANS 1/A+/CPDLC, WAAS(SBAS)/LPV & RNP 4 30/30.
- FANS 1/A+ / RNP 4 30/30 (SB 700-34-053).
- WAAS(SBAS)/LPV (SB 700-34-054).
- ADS-B Out (SB 700-34-062 Rev 3) (v2 / DO-260B).
- TCAS 7.1 (AD 2012-02-08).
- Aircell ATG-5000 Gogo Biz® Hi-Speed Broadband Internet & Wi-Fi System w/ Provisions for Swift Broadband.
Avionics and Equipment
Honeywell Primus 2000XP 6-Tube EFIS Integrated Avionics Suite with Primus Elite DU-875AF Flight Deck Upgrade (STC#: ST00299BO).
Primus Elite DU-875AF Flight Deck includes:
- Six LCD 8″ x 7″ DU-875 Color EFIS Displays (2 PFD / 2 EICAS / 2 MFD).
- Electronic Moving Map of the World.
- Paperless Jeppesen Charts.
- Video Display to include EVS & Airshow Images.
Four Honeywell DA-810 Data Acquisition Units Honeywell DL-1000 Data Loader
Triple NZ-2000 Integrated FMS w/ CD-820 Displays, 6.1 Software & & WAAS(SBAS)/LPV
Dual 12 Channel Honeywell GPS 550 GPS
Triple Honeywell LASEREF IV Inertial Reference Units (IRU)
Integrated Electronic Standby Indicator (IESI)
Dual Honeywell Primus II NAV/COM/ADF/DME w/ 3rd VHF Transceivers w/ 8.33 Spacing, FM Immunity, RVSM
Dual Collins ALT-4000 Radio Altimeters
Dual Collins HF-9031A HF Comm System w/ Coltech CSD-714 SELCAL System
Triple Honeywell AZ-840 Micro Air Data Computers
Triple IC-800 Integrated Avionics Computers (IAC)
Engine Indication/Crew Alerting System (EICAS)
Honeywell Primus WU-880 Color Weather Radar w/ Dual Control
Synthetic Vision System (SVS)
Thales/Sextant Heads-Up Flight Display System for CAT II Operations (HUD)
AirCell Axxess 2-Channel Iridium SATCOM
Honeywell MCS-7000 Inmarsat SATCOM
Honeywell LSZ-860 Lightning Sensor System
Dual Honeywell RCZ-833K Enhanced Mode S Transponders w/ ADS-B Out v2
Honeywell Mark VII EGPWS w/ Wind Shear & Rwy Awareness & Advisory Sys (RAAS)
Jump Seat Audio Panel & Full-Face O2 Mask
Honeywell RT-950 TCAS II w/ Change 7.1
Dual Honeywell Autopilots w/ Autothrottles
Honeywell Cockpit Voice Recorder (SSCVR)
Honeywell Flight Data Recorder (SSFDR)
Teledyne TL-806 Airborne Datalink System (ADLS)
Dual Primus II RM-855 Radio Management Units
Artex 406Hz Satellite ELT System
2nd Refuel/Defuel Control Panel
Honeywell VHF/SAT AFIS
Dual Honeywell RNZ-851 Integrated NAV Units w/ VOR/ILS/MKR/ADF/DME
Full Authority Digital Eng Control System (FADEC)
Central Aircraft Information Maintenance System Version 7.1 (CAIMS)
Pilot & Copilot Emergency Vision Assurance System (EVAS)
Pulse & Logo Lights
MNPS, RNP-5 / RNP-10
1A (500hr) – 3A (1500hr) 9A (4500hr) – 1C (15mo) – 2C (30mo) – 4C (60mo) – 8C (120mo) – 12C (180mo) Tasks & Landing Gear Restoration Completed September 2012 at 4,388.6 Hrs. by Jet Aviation – St. Louis, MO.
4C (60mo) Tasks Completed August 2017 at 5,556.7 Hrs. by Bombardier – Hartford, CT.
On Factory-Recommended Maintenance Program per FAR 91.409(f)(3)
Engines are “On Condition”
Maintenance Tracked on Flightdocs Computerized Maintenance Program
Periodic Inspections Last Completed Next Due (Date/Hours)
750 Hour Check 07/2018 @ 5,749 Hrs 6,499 Hrs
1000 Hour Check 07/2018 @ 5,749 Hrs 6,749 Hrs
2250 Hour Check 09/2012 @ 4,389 Hrs 6,689 Hrs
3000 Hour Check 07/2018 @ 5,749 Hrs 8,749 Hrs
4500 Hour Check 09/2012 @ 4,389 Hrs 8,939 Hrs
15 Month Check 06/2019 @ 5,972 Hrs 09/2020
30 Month Check 07/2018 @ 5,749 Hrs 01/2021
60 Month Check 08/2017 @ 5,557 Hrs 08/2022
120 Month Check (8C) 09/2012 @ 4,389 Hrs 12/2022
180 Month Check (12C) 09/2012 @ 4,389 Hrs 12/2027
240 Month Check (16C) N/A 12/2021
Last Weighed April 2016
Max Ramp Weight: 96,250 lbs.
Max Takeoff Weight: 96,000 lbs.
Max Landing Weight: 78,600 lbs.
Max Zero Fuel Weight: 56,000 lbs.
Basic Empty Weight: 49,643 lbs.
Soft Goods Refurbishment September 2012 @ Jet Aviation – St. Louis, MO
The thirteen (13) passenger fire-blocked interior with crew jump seat features a forward left-side crew rest area, forward right-side main galley, forward right-side crew chemical lavatory, spacious aft main vacuum lavatory with vanity and wardrobe closet, and in-flight accessible aft baggage compartment. The Forward Cabin features a four-place club grouping with executive pull-out tables. The Mid Cabin features a left-side 4-place conference group with hi-low conference table opposite a wood credenza followed by a bulkhead with manual pocket door. The private Aft Cabin features a left-side two-place club with executive foldout table and right-side 3-place berthable divan (3-passenger take-off & land with right-side bulkhead removed). Club chairs are covered in light tan leather and the divan in coordinating tan fabric. The Baker Cabin Management System includes one (1) 20” monitor mounted on left-side forward cabin bulkhead and one (1) 20″ monitor mounted on left-side aft cabin bulkhead. The cabin is equipped with Airshow and DVD/CD/VHS players. NOTE: The transition from Baker to Honeywell Ovation HD CMS is in progress with the 1st of 3 phases complete – galley touchscreen panel and associated wiring and software have been upgraded. The Forward Right-Side Full-Service Galley includes a TIA convection oven, microwave oven, dual-compartment chiller/tray storage, coffee/espresso maker, potable hot and cold water, ice drawer, 2 pullout work surfaces, ample storage for glassware, china, catering trays and additional supplies, and 10.4” touch-screen control panel.
Painted September 2012 @ Jet Aviation – St. Louis, MO
Matterhorn White Upper Fuselage and Light Gray Lower Fuselage with Single Medium Gray Stripe.
Aircraft is Hangared at Waterbury–Oxford Airport (OXC) in Oxford, CT, USA.