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| Engine Programs | RR Corp Care |
| Landings | 700 |
| Engines | Type: BR700-710A2-20 Plan: Rolls Royce Corporate Care Call for current Times |
| APU | Type: Honeywell RE-220 S/N: P-330 Call for current APU Times |
| Airframe | Weight & Balance: Empty: 51,258 lbs Basic Operating: 52,971 lbs Max Takeoff: 99,500 lbs (SB 700-11-020) Max Landing: 78,600 lbs Max Zero Fuel: 56,000 lbs Full Fuel: 45,050 lbs Max Ramp: 99,750 lbs (SB 700-11-020) |
| Avionics | COM: Dual Honeywell RCZ 833K with optional 3rd RCZ 833 unit installed NAV: Dual Honeywell RNZ 851 FDS: Honeywell Primus 2000XP A/P: Honeywell GP 400 Guidance Panel XPNDR: Dual Honeywell RCZ 833K Mode S with Enhanced Flight ID ADF: Dual Honeywell RNZ 851 DME: Dual Honeywell RNZ 851 ADC: Triple Honeywell AZ 840 MADC FMS: Triple Honeywell NZ 2000 with CDU 820s and 5.8 Software GPS: Dual Honeywell GPS 550 HG2021GD03 AFIS: Teledyne Controls Tele link Unit (ADLU) STCOM: ICS 100 Iridium, Collins SAT 6100 with SRT 2100 High Speed Data HFCOM: Dual Collins HF 9000 (HF9031A) FFONE: ICG Aerocom 3000, 2 cordless handsets and 3 corded handsets EFIS: Six DU 870 Displays (2 PFD, 2 EICAS, 2 MFD) RADAR: Honeywell WU 880 with LSZ 860 Lightning Sensor (SB 700-34-003) SELCAL: Single Coltech CSD 714 TCAS: Honeywell TCAS 2000 RT 950 with Change 7 RADALT: Dual Honeywell ALT 4000 EGPWS: Honeywell Mark V with RAAS (218-218 software) LRNAV: Triple Honeywell Laseref IV (HG2001GD03) FDR: Honeywell SSFDR 980-4700-041 CVR: Honeywell SSCVR 980-6022-001 ELT: Artex B406-4 Audio Panels: Triple Honeywell AV850A |
| Options and Additional Features | RVSM Capable MNPS Capable FM Immunity Compliant 8.33 Spacing Compliant TAWS Compliant Rockwell Collins Cabin Electronic system (CES) version 7 upgrade Thales HFDS Heads-Up Flight Display System (SB 700-34-002) Bombardier Enhanced Vision System BEVS (SB 700-34-033 Rev. 1) Triple Honeywell IC 800 Integrated Avionics Computers (4) Honeywell DA 810 Data Acquisition Units Honeywell 3rd FMS with Cabin Video Feed (SB 700-34-004) Honeywell IAC -009 Software Upgrade (SB700-31-001) Honeywell LSS Lightning Sensor (SB 700-34-030) Honeywell NZ 2000 Upgrade to CD 820 Displays (SB 700-34-047) Honeywell Quick Access Recorder Installation QAR (SB 700-31-026) Teledyne Controls G-624E P7.0G Sky Printer Cockpit Printer EMS Technologies AMT 50 SATCOM Antenna Assembly EVAS Enhanced Vision Assurance Systems Dual APE 4190 Digital Cockpit Clocks Logo Lights System (SB 700-33-001 Rev. 1) CAIMS Central Aircraft Information Maintenance System with PMAT Display Auto Throttle System Maximum Take-Off Weight Increase to 99,500 lbs (SB 700-11-020) Autopilot Emergency Decent Mode (SB 700-22-003) Wiring Provisions for XM Weather System (by 337) Baggage Door Internal T Handle Installation (SB 700-52-033) Addition of Refuel/Defuel Control Panel in Flight Compartment (SB 700-28-002 Rev. 1) Certification for Operations at Airports with Maximum Weight Restrictions (SB 700-11-018) Modifications to Permit Zero Flap Take Off Capability (SB 700-27-059 A, B and C) Pulse Landing lights |
| Interior | This aircraft has a 13 passenger fireblocked interior plus a crew rest area and one crew jump seat. The forward section of the aircraft features a crew rest area adjacent to the galley. The forward cabin features four single chairs in club configuration with two stowing work tables. The mid cabin includes a four place conference group with a two position manual table. The aft cabin includes a 16g divan (three place with bulkhead removed, two place with bulkhead installed) on the right hand side opposite two chairs in club configuration with a stowing work table. The club BEAerospace individual seats and the divan are all berthable. There is a solid swing door from the galley into the forward cabin, a solid electric door from mid to aft cabin and a solid electric door from aft into lav. The forward galley is equipped with a Hi-Temp oven, microwave oven, dual coffee maker, hot cup, sink with swivel and folding faucet, drain switch, chilled storage with removable shelves and soda storage, clean ice and bottle storage with drainage, wine and liquor storage, china, flatware, utensils, linen and dirty dish bin and crystal storage, (4) 115 VAC 60 HZ outlets. The middle tambour door has a microswitch that deactives the water system and the two forward doors have a microswitch that deactivates the galley utility outlets. There is a 10.4” touchscreen in the upper galley that provides control for all galley and cabin systems. The entertainment and cabin systems feature the Rockwell Collins Cabin Electronic system (CES) version 7 upgrade, (2) units of dual DVD players (4 total DVD players), (1) VCP, (1) CD with MP3 capability and the following Ethernet monitors: (1) 21.3” on left forward bulkhead, (1) 18” (fixed mounted) on the credenza, (1) 24” on right aft bulkhead, (2) fixed mounted in crew rest and galley respectively and (1) portable 10.4” plug in for (4) defined individual seat locations. The entertainment and cabin systems also features the Tailwind 500 Satellite TV System, an Airshow Interactive system, ICS100 Iridium Phone system, Collins SAT 6100 SATCOM with SRT 2100 with (2) 64K HSD data channels and a wireless Ethernet LAN, AEROCOM 3000 with (3) corded handsets and (2) cordless, RJ 45 jacks, 115VAC 60 HZ outlets, fax / printer machine installed in mid cabin credenza, Securaplane CAM-11 and CMX 03-X External camera system with (4) video cameras (2 color and 2 black and white). Forward and Aft fully flushing chemical lavs (8 gallons), externally serviced toilets, each lav includes vanity cabinets with a sink and faucet, soap dispenser, facial tissue dispenser, toilet paper dispenser, concealed power outlet, exhaust fans, storage and switches for both the water heater and floor mat. The aft lav also has a lighted cosmetic mirror. Additional Interior Information: BEAerospace seats all have fold up leg rests, flip up armrests with stowage and electronic controls for lumbar support, flex wing headrests, full swivel capability, full berthing and reclining capability and an audio jack in the lower inboard armrest. The 16g divan has a frame length of 80” take-off and landing certification for 2 with the FWD bulkhead installed and 3 with it removed (it is easily removable by the crew anytime) and it is fully berthable and has (3) shoulder harnesses installed. The double chairs on either side of the 4-place conference group fully recline and each seat has lumbar support. The credenza in main cabin includes a small cold storage/ Ice drawer which is both removable and insulated. Interior Coverings: Chairs are tan leather with fabric inserts Headliner is biscuit Divan is a fabric in a Sapphire color Wood is Fig Walnut Gloss Metal finish is Smoke Nickel Satin Counter tops are a Blue Pearl Tiled Granite Cabin sidewalls were recovered by Bombardier Dallas on 2/1/2008 |
| Exterior | Overall Jet Glo White with Charcoal Gray Metallic and Evening Sky Stripes. Stripes repainted on 6/7/2011 by Westar Aviation. |
| Maintenance | On CAMP maintenance tracking program 1A Check complied with 8/17/10 @ 1,456 hours, next due 12/12/11 or 2,000 hours 2A Check complied with 6/12/09 @ 1,006 hours, next due @ 2,000 hours 3A Check complied with 8/17/10 @ 1,465 hours, next due @ 3,000 hours 450 Landing Check complied with 10/21/09 @ 450 landings, next due @ 900 landings 6A Check due @ 3,000 hours 900 Landing Check due @ 900 landings 9A Check due at 4,500 hours 1C Check complied with 3/31/11 @ 1,663 hours, next due 6/15/12 2C Check complied with 1/6/10 @ 1,160 hours, next due 6/15/12 4C Check due 6/16/12 8C Check due 6/15/17 |
| Additional Description | Remaining Warranty Dates: Airframe & Airframe systems (excluding completion) until June 15, 2012 or 5,000 hrs Aircraft Primary Metal Structures until June 15, 2027 or 20,000 hrs Green Aircraft Avionics until June 15, 2012 or 5,000 hrs BMW Rolls-Royce Engines until June 15, 2012 or 2,500 hrs or cycles APU Parts until June 15, 2013 or 3,000 hrs APU Labor until June 15, 2012 or 5,000 hrs |
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