Engines Enrolled on Rolls Royce Corporate Care
APU Enrolled on JSSI
HUD & EVS
Synthetic Vision System
Batch 3.4 FMS Upgrade
KA-Band Internet
Increased MTOW 99,500 LBS
Certification Date March 2010
Primus Elite DU-875 Avionics Upgrade including ADS-B, FANS 1A, & WAAS
EFIS (Electronic Flight Instrument System): Six Tube Honeywell DU-875 Color Displays w/ Jeppesen Charts & Maps
FMS (Flight Management System): Triple Honeywell CD-820
FLT DIR (Flight Director): Primus 2000XP IFCS w/ Triple IC-800
GPS (Global Positioning Device): Dual Honeywell HG-2021
EFB (Electronic Flight Bag): Dual Class II
Navigation Radio: Dual Honeywell RNZ-851
SVS (Synthetic Vision System): Dual Honeywell
EVS (Enhanced Vision System): GT546-001-7
HUD (Heads-Up Display): GT546-001-7
Autopilot: Dual Honeywell IC-800
VHF Com (Very High Frequency Communication): Triple Honeywell RCZ-833M
HF Com (High Frequency Communication): Dual Rockwell Collins HF-9031A w/ SELCAL CSD-714
ELT (Emergency Locator Transmitter): Artex 406 ELT
Radar: Honeywell Primus WU-880
EGPWS (Enhanced Ground Proximity Warning System): Honeywell
TCAS (Traffic Collision Avoidance System): ACSS TCAS-2000 w/ Change 7.1
LSS (Lighting Sensor System): Honeywell LP-860
CVR (Cockpit Voice Recorder): Honeywell 980-6022-001
FDR (Flight Data Recorder): Honeywell 980-4700-041
New Soft Goods – May 2021
Thirteen Passengers (13)
Spacious Forward Galley Area
Adjacent Crew Rest Area
Forward and Aft Lavatory
Forward Cabin with Four-Person Club Seat with Ledge Pull-Out Tables on Each Side
Mid- Cabin Four-Person Conference Area with Opposite Credenza
Aft Cabin Two Club Seats
Aft Cabin Three-Person Divan (two seats certified for take-off and landing)
In-Flight Accessible Baggage Compartment
New Paint – October 2020
Matterhorn White with Medium Gray and Granite Accents
MAINTENANCE STATUS:
Batch 3.4 FMS Upgrade
Engines enrolled on Rolls Royce Corporate Care
APU enrolled on Honeywell JSSI
Maintenance tracked by CAMP
15-Month Next Due June 2025
30-Month Next Due August 2025
60-Month Next Due October 2025
120-Month Next Due August 2030
180-Month Next Due August 2025
240-Month Next Due August 2030
500 Hour Check Next Due at 5202 Hours
750 Hour Check Next Due at 5575 Hours
1000 Hour Check Next Due at 5683 Hours
1500 Hour Check Next Due at 3233 Hours
2250 Hour Check Next Due at 5983 Hours
3000 Hour Check Next Due at 5969 Hours
4500 Hour Check Next Due at 8991 Hours
WEIGHTS:
Max Take Off Weight: 99,500 lbs.
Max Landing Weight: 78,600 lbs.
Basic Operating Weight: 52,653 lbs.
Max Fuel Weight: 44,716 lbs.
Payload at Max Fuel: 2,408 lbs.
ADS-B Out: Automatic Dependent Surveillance – Broadcast Out
CPDLC: Controller Pilot Data Link Communications
FANS 1/A: Future Air Navigation System
WAAS: Wide Area Augmentation System
MNPS: Minimum Navigation Performance Specifications
RNP 4: Require Navigation Performance 4
RVSM: Reduced Vertical Separation Minimum
