Airframe
- Total Time: 2083
- Landings: 1629
Airframe, Engines & APU
- Entered into service in June 2002.
- Aircraft not involved in operational incidents or major repairs.
- CAMP Maintenance Programme Management enrolled.
- Engines: PWCA 305A
Left engine Hours / Cycles: 2083 / 1629
Left engine Hours / Cycles: 1984 / 1539
- APU: T-20G-10C3A
Hours / Cycles: 1095 / 2383
Certification
Aircraft full compliant:
- EU-OPS1
- Part 21
- Eurocontrol
- Airworthiness Review Certificate issued, next due July 30th 2011
Operational Approvals
- RVSM
- B-RNAV
Floorplan
Cabin layout arrangement for 8 passengers:
- One Single Seat forward-facing in the forward left side of the cabin
- One two-place side-facing Divan in the forward right side of the cabin
- Four Executive Single Seats in Club arrangement in the aft part of the cabin
- Certified Toilet for take-off and landing
INTERIOR EQUIPMENT
- Completion in 2001.
- Fireblocked; Eight (8) passenger seating including a belted lavatory seat.
- Executive interior features a fwd two-place divan on the right side, opposite a
fwd facing seat with a foldout table.
- Seats are covered in classic cow, tan, townsend leather.
- Carpet is off white colored wool.
- The aft cabin features a four-place club arrangement with two foldout executive
tables.
- Fwd right hand galley cabinet and aft private lavatory.
- 15.1” forward bulkhead monitor.
EXTERIOR PAINTING SCHEME
- Paint Color “A” - DeSoto, i1050, Matterhorn White.
- Paint Color “B” - DeSoto, IM902, Titanium.
- Paint Color “C” - DeSoto, i6033, Royal Blue.
Avionics
Collins Pro Line 4 EFIS/Avionics system including:- Four BF Goodrich Tube EFD/MFD with 8” x 7” Displays.
- Single Collins RTA-844 Radar.
- Dual Collins FCC-4006 Autopilot.
- Dual Collins FCC-850A Flight Control Computer
- Dual Collins FMC - 851C Flight Management Computer.
- Dual Collins FMC - 852C (Navigation Computer)
- Dual Collins VIR-432 NAV Receivers w/FM Immunity.
- Dual Collins DME-442.
- Single ALT-4000 Radio Altimeter.
- Single Universal Avionics CVR-30 Cockpit Voice Recorder.
- Single Fairchild F1000 Flight Data Recorder
- Single ARTEX ELT 110-406.
- Dual Collins VHF-422C Comms w/ 8.33 Spacing.
- Dual TDR-94D Mode-S Enhanced Surveillance Transponders.
- Collins TTR-4000 TCAS II with Change 7.
- Dual Collins RTU-870T (Radio Tunning Units).
- Single Collins RAC - 870 Radio Altimeter Converter.
- Single Freeflight Systems SELCAL JetCall 2.
- Dual Collins AAP - 851 Altitude Awareness Panel.
- Single CHP - 850 Course/Heading Panel.
- Single ICC - 851A IAPS Card Cage.
- Four IOC-851A I/O Processor.
- Four PWR-851A IAPS Power Supply.
- Single Collins SDD - 640A Sensor Display Driver.
- Single Collins SDU - 640B Sensor Display Unit.
- Dual ADC-850D Air Data Computer.
- Dual Collins ARP-851 Air Data Reference Panel.
- Dual Colllins SIA-850 Signal Interface Adapter.
- Single Horizon Aerospace Standby Altimeter (2”).
- Dual Collins ADF-462 ADF
- Single Bendix King KHF-950 HF COMM (w/Selcal)
- Dual Collins AHC-85E AHRS
- Single Universal CVR-120 Cockpit Voice Recorder
- Dual Universal UNS-1C Flight Management with GPS
- Single Allied Signal EGPWS w/ Wind Shear
Additional Features
- Airshow 400 Inflight Information System
- Galley has a Warming Oven, 2 Hot Liquid Containers and 2 Ice Drawers.
- Entertainment: 10 Disc CD and Single DVD Player
- Illuminated Chart Holders.
- Baker Passenger Audio Amplifier.
- Single UASC Aero-M Digital Airbone Telephone System.
- Passenger Briefing System.
- 115 Volt Outlet in Fwd R/H Cabinet and in club seating area Seat #1.
EMERGENCY EQUIPMENT
- Two (2) Smoke Goggles
- One (1) Protective Breathing Equipment
- One (1) Crash axe
- One (1) JAR-OPS 1 first aid kid
- Two (2) Cockpit Flashlights (one behind pilot and co-pilot)
- Three (3) fire extinguishers (two in cockpit, one in cabin)
- Life Vests located in every Seat
- One (1) Portable Oxygen Bottle
SCHEDULED MAINTENANCE STATUS
Packages next due are as follows:- Phase A1-A6: April 30th, 2011 or 2272 FH
- Phase B1-B6: November 17th, 2011 or 2506 FH
- Phase C1-C6: November 24th, 2013 or 3106 FH
- Phase D1-D6: October 31st, 2017 or 4306 FH
- 3000 Landing Inspection: 3000 FC
- Major Landing Inspection: 6000 FC
- 12 Years Airframe Inspection: Oct. 31st, 2013 or 6000 FC
- 12000 FH Airframe Inspection: 12000 FH
- Engines Hot Section Inspection: 3600 EH
- Engines Overhaul: 7200 EH
- Stage 1 Turbine Disc: 3100 EC
Weights
Weight & Balance performed on April 29st, 2010.Next Weight & Balance due on April 2014.
- Max Ramp Weight: 23,750 lbs
- Take Off Weight: 23,500 lbs
- Landing Weight: 19,500 lbs
- Max Zero Fuel Weight: 17,000 lbs
- Basic Empty Weight: 14,707 lbs
- Max Fuel Weight (usable): 7,910 lbs
- Payload with Full Fuel: 734 lbs
- Max Payload: 1,894 lbs