C-FNCG - 1990 DEHAVILLAND DHC 8 102

1990

DEHAVILLAND

DHC-8-102

211

Used

C-FNCG

Owner: North Cariboo Air Base: Calgary, AB Canada Specification Date: August 18, 2010 Utilization Program: Low Utilization 37 Seats, Standard deHavilland Galley, Forward Lavatory. Fresh C-Check.

33717.0

Total Hours Since New: 33,717 Total Cycles Since New: 43,610 Last "A" Check: 33,423 Last "C" Check: 33,570 Last "60 Month" Check: April 22, 2010 Last Major Cycle Inspection: 40K Completed Jan 27, 2005

Pratt & Whitney PW120A Operator Approved TBO: On Condition Left Engine SN: 120111 Hours Since New: 42,695 Cycles Since New: 48,005 Hours Since Last Shop Visit: 7,585 Hours Since HSI: 7,585 Cycles to First Limiter: 3,251 Right Engine SN: 121158 Hours Since New: 26,650 Cycles Since New: 32,516 Hours Since Last Shop Visit: 2,993 Hours Since HSI: 2,993 Cycles to First Limiter: 863

Hamilton Standard 14SF-7 Operator Approved TBO: 10,500 hrs., 10 Years Left Prop Assembly SN: 870150 Prop Hub: 292 TSOH (Aug. 6, 2009) Actuator: 409 TSOH (March 3, 2009) Blade #1: 292 TSOH (July 24, 2009 Blade #2: 290 TSOH (Aug. 14, 2009) Blade #3: 1987 TSOH (Jan. 12, 2007) Blade #4: 290 TSOH (Aug. 14, 2009) Right Prop Assembly SN: 881012 Prop Hub: 284 TSOH (Sept. 17, 2009) Actuator: 4872 TSOH (March 19, 2004) Blade #1: 4449 TSOH (Nov. 25, 2003) Blade #2: 2965 TSOH (Oct. 5, 2005) Blade #3: 4872 TSOH (Mar. 9, 2004) Blade #4: 315 TSOH (Sept. 2, 2009)

Communications Radio: 2 King KTR-908 Navigation Radio: 2 King KNR-634 GPS IFR Approach: 1 Garmin 165 ADF: 2 King KDF-806 DME: 2 King KDM-708A Transponder: 1 Bendix KXP-756 Transponder Mode S: 1 Honeywell TPR-720 Radar: 1 Sperry 800 Radio Altimeter: 1 Sperry RT-300 GPWS: 1 Honeywell Mk VII TCAS: 1 Honeywell TCASII Air Data Computer: 2 Sperry AZ-800 AHARS: 2 Sperry FZ-800 SAHS: 1 Sperry C14A, 1 Sperry VG14 Audio Controller: 2 Avtech 5061-1 Flight Data Recorder: 1 Sundstrand 980-4100 Cockpit Voice Recorder: 1 Sundstrand AV557C ELT: 1 Kannad 406AF-C Passenger Briefing: 1 Autoflight

Ballistic Door With Remote Entry Dual Main Batteries - Concorde RG380E/44 NOSE LANDING GEAR Shock Strut Life Cycles Left: 20,212 Cycles Since Overhaul: 10,531 Date of Overhaul: March 3, 2001 Drag Strut Life Cycles Left: 29,830 Cycles Since Overhaul: 10,536 Date of Overhaul: March 3, 2001 MAIN LANDING GEAR Shock Strut Life Cycles Left: 16,498 (Left), 15,161 (Right) Cycles Since Overhaul: 8,555 (Left), 11,702(Right) Date of Overhaul: 5-Oct-01 (Left), 27-Oct-00 (Right) Drag Strut Life Cycles Left: 4,509 (Left), 17,950 (Right) Cycles Since Overhaul: 640 (Left), 8,702 (Right) Date of Overhaul: 18-Nov-08 (Left), 21-Sep-00 (Right) Lower Cavity Cycles Since Overhaul: 640 (Left), N/A (Right) Date of Overhaul: 18-Nov-08 (Left) Yoke Assy. Life Cycles Left: 21,403 (Left), 10,296 (Right) Cycles Since Overhaul: 8,555 (Left), 23,484 (Right) Date of Overhaul: 5-Oct-01 (Left), 24-Aug-95 (Right) Stabilizer Stay Life Cycles Left: 15,835 (Left), 17,902 (Right) Cycles Since Overhaul: 8,555 (Left), 8,702 (Right) Date of Overhaul: 5-Oct-01 (Left), 28-Sept-00 (Right) WEIGHTS Max Take-Off Weight: 34,500 lbs. Max Landing Weight: 33,500 lbs. Max Zero Fuel Weight: 31,000 lbs. Empty Operating Weight: 23,356 lbs. Payload: 11,165 lbs.

CABIN CONFIGURATION 37 Seats Standard deHavilland Galley Forward Lavatory Aircraft Specifications Subject To Verification

Fresh C-Check