Registration:XA-FRD

Status Date: 17 January 2010
Cycles: 924
Green C of A Date: O ctober 2005
Date Entered Service: April 2006

AIRCRAFT
Maintenance Program & Warranty
• Engines on Honeywell MSP Program, $142/Hr, Contract # 44026121
• APU on Honeywell MSP Program, $0/Hr, Contract # 44026121
• Aiframe on SmartParts $92/Hr, Contract # SP-20078-61

ENGINES
Honeywell AS907-1-1A
#1: TSN: 1,398 Hrs Cycles: 924 SN: P118273
#2: TSN: 1,398 Hrs Cycles: 924 SN: P118274

APU
Honeywell GTC-150 (On MSP Program)
TSN: 1,016 Hrs

AVIONICS
RVSM approved
Collins PROLINE 21 Avionics
• Display tubes: 4 Collins EFIS-4000
• Autopilot: 1 Collins APS-4000 Cat. II
• Weather Radar System: 1 Collins TWR-850
• Air Data System: Dual Collins ADC-850C v.6 with RVSM
• Radio Altimeter: 1 Collins ALT-55B
Collins PROLINE Radios (Arinc 429)
• VHF Comm.: Dual Collins VHF-422A with 8.33 KHS
• VOR /ILS Nav. System: Dual Collins VIR-432
• DME System: Dual Collins DME -442
• ADF System: Dual Collins ADF-462
• Mode S Transponder: Dual Collins TDR -94D
• TCAS II: 1 Collins TCAS 94 Change 7 compliant ACAS II
• Radio Tuning Units: Dual Collins RTU -4020
Other Radios & Equipment
• Flight Management System: Dual Collins 5000
• GPS: Dual Collins GPS 4000 A
• AHR S Compensation Card: 1 PRO LINE 21
• HF Comm.: Dual IRIDIUM KTP-953
• E.L.T.: 1 ARTE X C406-1 MH Z
• IRS: Dual IR 2000
• SELCAL Dual Channel: 1 Coltech SELCAL Decoder
• Digital Clocks: Dual Davtron 811B
• E.G.P.W.S.: 1 Collins MK-VII TAWS
• C.V.R.: 1 FA-2100
• AFIS Allied Signal

INTERIOR
The interior configuration consists of a forward galley and four (4) executive seats arranged in a double club formation. There are two
(2) fold out tables in between. Moving aft there are two (2) executive seats (LH) and opposite a three (3) place divan. The seats are covered in dark and light shades of brown and the divan in checked brown cloth. The rear walkin lavatory has a lighted basin with a belted toilet.

EXTERIOR
The aircraft has a dark blue base followed by two light blue accent stripes aith a red accent stripe above. The top of the fuselage is
finished in matterhorn white. The vertical stabiliser features three large blue accent stripes.

MAINTENANCE
• 2M/400hr Inspection complete 19/04/2007 at Aviación Comercial de America
• 12/24M & 400/800hr Inspection complete 31/01/2008 at Bombardier Tucson service centre
• 12M inspection due in May 2009
• 12/24/48M inspection due in May 2010
• 400hr due at 1,200 TT AF
• 400/800/1200Hr due at 1,600TT AF

WEIGHTS
Max Ramp Weight 39,000 Lbs
Max Take-off Weight 38,850 Lbs
Max Landing Weight 33,750 Lbs
Zero Fuel Weight 27,000 Lbs
Basic Operating Weight 23,500 Lbs
Max Fuel Weight 3,500 Lbs

ADDITIONAL FEATURES
• Life Rafts for 9 pax and crew
• 2 PBE (Protective Breathing Equipment)
• Teleflex Precise Pulse Light Landing System
• Devore Tail Lights
• 2 DME Corp Rechargeable Flash Lights
• KGS Auxiliary 115 VAC 60 HZ. Inverter
• Remote Temperature Control
• Three White Lights strobe System (wing & tail)
• Thrust Reverses
• Wing Ice Detection Lights
• External Baggage & Servicing Lights
• Ladder
• Retractable Tow Bar with Head and Support
• First Aid Kit (MedAir)
• DL-900 Data Loader Unit for Data Base
• Anti Collision Light (Lower)
• FADE C‘s v 6.3
• Airshow 400
• AFIS Allied Signal
• Jump Seat Retractable
• Magnavox Magnastar Airborne Radiotelephone System (4 Handsets) C-2000
• Satcom (Collins SAT-906-4/four channels)
• Fax machine (interfaced)
• Compaq Disc
• VCR HI8/8mm
• Stereo Cabin
• Three Rosen connections for display
• Portable Oxygen Bottle
• L‘Hotellier Smoke Detector System
• Avionics & Galley Master System