Ka Band with Wi-Fi Batch 3 with FANS 1/A & ADS B (Out) Increased MTOW to 92,500 lbs. Enrolled on Corporate Care APU on JSSI Smart Parts Plus
Airframe: TOTAL TIME: As of February 20, 2019 TOTAL TIME: 2,659 LANDINGS: 1,019 Engine 1ROLLS ROYCE BR700-710A2-20 Engine 1 Time2602 SNEW Engine 1 Cycles998 Engine 1 NotesEnrolled on Rolls Royce Corporate Care Engine 2 Engine 2 ManufacturerROLLS ROYCE Engine 2 Time2602 SNEW Engine 2 Cycles998 Engine 2 NotesEnrolled on Rolls Royce Corporate Care
APU: Allied Signal RE-220 (GX) TOTAL TIME: 2,211 CYCLES: 2,650 SERIAL NUMBER: P-301
AVIONICS: Honeywell Primus 2000 XP Integrated Avionics System AIR DATA COMPUTERS: Triple Honeywell AZ-840 Micro Air Data Computers COCKPIT VOICE RECORDER: Allied Signal Solid State CVR (120 minute) COMMUNICATIONS: Dual VHF Honeywell RCZ-833 Comm Unit DATA ACQUISITION UNIT: Triple Honeywell DA-810 DAUs ELECTRONIC FLIGHT BAG: Dual EMS 100 Electronic Flight Bags ELECTRONIC FLIGHT INSTRUMENT SYSTEM: Six-Tube 8”x7” DU-870 Color EFIS displays EMERGENCY LOCATOR TRANSMITTER: Artex B406-4 ELT with Navigation Interface FLIGHT DATA RECORDER: Allied Signal Solid State Flight Data Recorder (88 parameters) FLIGHT MANAGEMENT SYSTEM: Triple FMS Honeywell NZ-2000 Integrated FMS GLOBAL POSITIONING SYSTEM: Dual Honeywell HG-2021GD04 GPS Sensors HEADS UP FLIGHT DISPLAY SYSTEM: Thales/Sextant HUD HIGH FREQUENCY: Dual Collins HF-9031A HF Communication System INERTIAL REFERENCE UNIT: Triple Honeywell Laseref IV HG-2001GD03 IRUs NAVIGATION: Dual Honeywell RM-855 Radio Management Units RADIO ALTIMETERS: Dual Rockwell Collins ALT-4000 Radio Altimeters SELCAL: Single Coltech CSD-714 SELCAL STANDBY INSTRUMENT: Integrated Electronic Standby Instrument (IESI) TERRAIN AWARENESS AND WARNING: Honeywell Mark V EGPWS TRANSPONDERS: Dual Honeywell Transponders with Enhanced Mode S TRAFFIC COLLISION ALERT AVOIDANCE SYSTEM: Collins TCAS 2000 (Change 7.1) WEATHER RADAR: Primus 880 Color Weather Radar w/Lightning Sensor System and dual control panels
Modifications and Conversions
SB 700-1A11-11-002 – Increase Max takeoff weight to 89,700 lbs – Complied with during completion of aircraft. SB 700-1A11-11-008 – Increase Max Takeoff weight to 92,500 lbs – C/W May 10, 2009 at 810 hours and 335 landings.
(Refurbished in December 2016 by Innotech Montreal, Canada: Re-covered passenger seats, headliner, lower & upper side wall, new carpet and wood re-veneered) The spacious floor plan is certified for takeoff and landing with twelve or thirteen (12/13) passengers. The floor plan features a 4-place club in the forward cabin, a conference table facing a credenza in the mid cabin and 2/3-place divan facing a 2-place club in the aft cabin. The aft divan normally seats 3. For additional privacy in the aft cabin, a removable R/H bulkhead can be installed in minutes. When installed, the divan seats 2 passengers for takeoff and landing. The cabin is equipped with a forward galley, forward and aft lavatories, as well as a jumpseat in the cockpit.
Repainted in December 2016 by Innotech Montreal, Canada Matterhorn White with Gamma Gray and Gloss Blue stripes
120 month inspection due Nov 2026 Gear Overhaul due Nov 2026