S/N 9053 ~ 5,160h (not to exceed 5,300 hrs) Year of Production x Turbomeca Arriel 1E2 Availability August 2017

Transcription

1 for SALE S/N 9053

2 Aircraft details: Airbus Helicopters BK117C2 Make Offer S/N 9053 Flight hours ~ 5,160h (not to exceed 5,300 hrs) Year of Production 2004 Engine 2x Turbomeca Arriel 1E2 Availability August 2017 Highlights: Pilot VFR / IFR Day / Night CAT A General Equipment Avionics Interior layout Exterior layout Conditional Dual IFR Yes Yes Utility Configuration Controllable Landing/Search Light Dual Garmin 430 GPS/COMM/NAV Garmin GTX 330 Transponder Radar Altimeter, KRA405B NVG/NVIS Lighting System (STC SR09303RC-D) Loincoin Cabin Flooring 2 Color Paint scheme Solely maintained./operated by one owner

3 Cockpit view: TTSN: hours Interior view Interior layout: seats

4 Exterior view: TTSN: hours Exterior view: Clamshell door windows Exterior view:

5 AIRFRAME Total time: Approx. 5,160 hrs. ENGINE MODEL Arriel 1E2 AVIONICS Dual Garmin 430 GPS/COMM/NAV VHF Comm CD-402 Garmin GTX 330 Transponder ARTEX C406N ELT DME, DM-411B Wulfsberg C5000 V/UHF AM/FM System (1) Dual Wulfsberg UHF-FM P2000 System (1) Marker Beacon Installation, KR 21 (1) May be ITAR restricted if aircraft is to be sold outside USA Radar Altimeter, KRA405B Nav/ILS/LPV Approach Switching for SMD 45 Displays Thales (4x) SMD 45 Displays Pilot, Copilot,and Rear Station Becker ACU 6100 Audio Controls NVG/NVIS Lighting System (STC SR09303RC-D), Aircraft NVG Radios/Instrumentation (1) MAIN FEATURES & EQUIPMENT Standard Gear with Full Length Steps Standby Attitude Gyro Engine Fire Detection and Extinguishing System Cargo Sling Siren System Fixed Provisions Cargo Sling Mirror Fixed Provisions Rescue Hoist, LH Fixed Provisions Rotor Brake System Fuzz Burner System, Engine and Gearboxes Windshield Wiper Blade System ADDITIONAL EQUIPMENT PAINT & INTERIOR Pilot & Copilot Height Adjustable BAE Seats (STC SR01938LA) Alternate Passenger Seating is available as a post sale installation. Slant and Center Consoles Clamshell Door Windows Dual Controls Emergency Floats, Fixed Provisions 3 Axis Autopilot with Yaw SAS Controllable Landing/Search Light, 200W/400W Engine Compressor Wash Device Anti Collision LED Light (STC SR09303RC-D) Lt/Rt Position LED Lights (STC SR09302RC-D) 40 AH Saft Nicad Battery Carbide Skid Protectors, Brauer (STC SR03936AT) Engine Cowling MI-15 Internal Heat Coating

6 AIRFRAME Description Interval Part number Frequency Time remaining Main Rotor Blades, 4ea RTR B621M ,000 Hrs 11,287 Hrs (94%) Main Transmission OH B632K ,000 Hrs 4,844 Hrs (96%) Main Gearbox Case Assembly RTR B632K ,000 Hrs 9,844 Hrs (98%) Main Rotor Shaft RTR ,000 Hrs 29,844 Hrs (99%) Main Rotor Head Assembly INSP B622M ,800 Hrs 2,246 Hrs (47%) Tension Torsion Straps, 4 ea RTR B622M10T ,000 Cyc 7,141 Cyc (59%) Inner Sleeve Assemblies, 4 ea RTRC B622M ,000 Hrs 12,446 Hrs (82%) Quad Nuts, Upper/Lower RTR B622M / ,000 Cyc 62,141 Cyc (92%) Rotor Star RTR B622M ,200 Hrs 22,646 Hrs (89%) Main Servo, Longitudinal OH B673M30A1101 7,500 Hrs 4,923 Hrs (65%) Main Servo, Lateral OH B673M30A1301 7,500 Hrs 4,923 Hrs (65%) Main Servo, Collective OH B673M30A1203 7,500 Hrs 4,923 Hrs (65%) Intermediate Gearbox OH ,500 Hrs 300 Hrs (20%) Tail Rotor Transmission OH ,800 Hrs 330 Hrs (18%) Tail Rotor Blade Assembly RTR B641M ,000 Hrs 2,602 Hrs (52%) Laminated Pile Assembly (T/R) RTR B642M ,000 Cyc 12,324 Hrs (94%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com

7 ENGINE #1 - ARRIEL 1E2 S/N Total Time: 2,701.4Hrs NG Cycle: 4, NP Cycle: 3, MO1 Interval On Cond MO1 (Accessory Gearbox) 180 M 64 M (36%) MO2 (Axial Compressor) 7,200 Hrs 4,731 Hrs (65%) MO3 (Gas Generator) 3,600 Hrs 987 Hrs (27%) MO4 (Power Turbine) 7,200 Hrs 4,731 Hrs (65%) MO5 (Reduction Gearbox) 3,600 Hrs 1,131 Hrs (31%) FCU 3,600 Hrs 1,291 Hrs (35%) Item Cyc/Hrs Limit On Cond Free Turbin disk 10,000 Cyc 6,811 Cyc (68%) Free Turbine Blades 12,000 Cyc/ 7,200 Hrs 8,812 Cyc / 4,731 Hrs (65%) 1st Stage Turb Disk 10,000 Cyc 5,582 Cyc (55%) 1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 7,582 Cyc/ 3,387 Hrs (56%) 2nd Stage Turb Disk 10,000 Cyc 5,582 Cyc (55%) 2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 5,582 Cyc / 3,387 Hrs (56%) Axial Comp Wheel 22,000 Cyc 17,915 Cyc (81%) Centrifugal Impeller 14,000 Cyc 9,915 Cyc (70%) Injector Wheel 10,000 Cyc 5,581 Cyc (55%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com

8 ENGINE #2 - ARRIEL 1E2 S/N Total Time: 2,296.1 hrs NG Cycle: 3,628.4 NP Cycle: 2, MO1 Interval On Cond MO1 (Accessory Gearbox) 180 M 70 M (39%) MO2 (Axial Compressor) 7,200 Hrs 4,891 Hrs (67%) MO3 (Gas Generator) 3,600 Hrs 1,291 Hrs (35%) MO4 (Power Turbine) 7,200 Hrs 5,025 Hrs (69%) MO5 (Reduction Gearbox) 3,600 Hrs 1,425 Hrs (39%) FCU 3,600 Hrs 1,292 Hrs (35%) Item Cyc/Hrs Limit On Cond Free Turbin disk 10,000 Cyc 8,516 Cyc (85%) Free Turbin Blades 12,000 Cyc/ 7,200 Hrs 9,686 Cyc / 5,025 Hrs (69%) 1st Stage Turb Disk 10,000 Cyc 6,372 Cyc (63%) 1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 8,372 Cyc /841 Hrs (14%) 2nd Stage Turb Disk 10,000 Cyc 6,372 Cyc (63%) 2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 6,372 Cyc / 3,691Hrs (61%) Axial Comp Wheel 22,000 Cyc 18,372 Cyc (83%) Centrifugal Impeller 14,000 Cyc 10,372 Cyc (74%) Injector Wheel 10,000 Cyc 6,372 Cyc (63%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com