S/N 9069 Flight hours ~ 8,007h Year of Production x Turbomeca Arriel 1E2

Transcription

1 for SALE S/N 9069

2 Aircraft details: Airbus Helicopters BK117C2 MAKE OFFER S/N 9069 Flight hours ~ 8,007h Year of Production 2005 Engine 2x Turbomeca Arriel 1E2 Availability Immediate Highlights: Pilot VFR / IFR Day / Night CAT A EASA-OPS General Equipment Avionics Interior layout Exterior layout Conditional Single IFR Yes Yes Yes EMS Systems and Components Night Scanner Search light System Dual GNS 530/430 Comm Nav System KTS 870 TAS System HD Sky Trac Phone System RDR 2000 WX Radar System HD EMS Configuration 3 Color Paint scheme Solely maintained /operated by one owner

3 S/N 9069 Cockpit view: NVG certified cockpit TTSN: hours Stretchers Interior layout: leather seats

4 Exterior view: Cable cutters TTSN: hours Exterior view: Clamshell doors/windows Exterior view:

5 AIRFRAME Total time: Approx. 5,160 hrs. ENGINE MODEL Arriel 1E2 AVIONICS (1) KRA 405B Rad Alt System KR 21 Marker Beacon System Crew NAT Audio System, Dual AA RDR 2000 WX Radar System VHF/UHF/FM TDFM 6158 System Dual GNS 530/430 Comm Nav System Cabin NAT Audio, AA MAIN FEATURES & EQUIPMENT (1) Night Scanner Search light System, Strobe Lights System. A650 2EA Hover Lights System. 2EA H Tel Tail Light, Cable cutters Medium height skid gears TAS System KTA870 ELT System, Artex C406 Sky Trac ISAT-100, STC SRO 1853NY Transponder System, Dual GTX330 HEGPWS MK-XXI DME System DMS-44A NVG Compatible ASU light System, STC SROI611SE PAINT & INTERIOR Leather interior (grey) 3 colors paint scheme EMERGENCY MEDICAL SYSTEM (1), (2) Medical Floor Stretchers, primary and secondary Storage Box and pockets Overhead Console Vacuum Pump (Qty 2) Air Pump 24V Switching Regulator Medical Outlet Oxygen Storage Cabinet (Transducer, Pressure Gauge, Pressure Transducer, Bottle and Sov) Window bar mount (STC SR09405RC) AND ADDITIONAL EQUIPMENT AFT facing seats, 2 each Cabin/Loading Light Syst Portable Oxygen D-CYL IV Hooks Air Conditioning System, metro STC SH3880SW Tanis Preheat System First Aid kit WSI/FG Flight Bag Provisions AFT Ballast (STC SR09306RC-D) (1) Helidyne FAA Forms 337, dated 10/3, 10/6 or 10/ with DER report or FAA Field approval (2) Keystone Helicopters, EMS interior installed, STC SR01968NY-D

6 AIRFRAME Description Interval Part number Frequency Time remaining Main Rotor Blades RTR B621M ,000 Hrs Hrs (65%) Main Rotor Blades RTR B621M ,000 Hrs 6,183.8 Hrs (52%) Main Rotor Blades RTR B621M ,000 Hrs 6,095.7 Hrs (51%) Main Rotor Blades RTR B621M ,000 Hrs 7,839.3 Hrs (65%) Main Transmission OH B632K ,000 Hrs 1,980.0 Hrs (40%) Main Gearbox Case Assembly RTR B632K ,000 Hrs 3,380.4 Hrs (34%) Main Rotor Shaft RTR ,000 Hrs 24,676.1 Hrs (82%) Main Rotor Head Assembly INSP B622M ,800 Hrs 4,800.0 Hrs (100%) Tension Torsion Straps, 4 ea RTR B622M10T ,950 Cyc 6,362.0 Cyc (53%) Inner Sleeve Assemblies, 4 ea RTRC B622M ,000 Hrs 6,993.4 Hrs (47%) Quad Nuts, Upper/Lower RTR B622M / ,000 Cyc 40,659.0 Cyc (61%) Rotor Star RTR B622M ,200 Hrs 17,193.4 Hrs (68%) Main Servo, Longitudinal OH B673M30A1101 7,500 Hrs 5,925.4 Hrs (79%) Main Servo, Lateral OH B673M30A1301 7,500 Hrs 6,728.2 Hrs (90%) Main Servo, Collective OH B673M30A1203 7,500 Hrs 6,728.2 Hrs (90%) Intermediate Gearbox OH ,500 Hrs 70.7 Hrs (5%) Tail Rotor Transmission OH ,800 Hrs 1,028.2 Hrs (57%) Tail Rotor Blade Assembly RTR B641M ,000 Hrs 3,084.6 Hrs (62%) Tail Rotor Blade Assembly RTR B641M ,000 Hrs Hrs (100%) Laminated Pile Assembly (T/R) RTR B642M ,000 Cyc Hrs (10%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com

7 ENGINE #1 - ARRIEL 1E2 15, May 2017 S/N Total Time: Hrs NG Cycle: 14,236.5 NP Cycle: MO1 Interval On Cond MO1 (Accessory Gearbox) 180 M M (83%) MO2 (Axial Compressor) 7,200 Hrs 5,935.5 Hrs (82%) MO3 (Gas Generator) 3,600 Hrs 2,335.5 Hrs (65%) MO4 (Power Turbine) 7,200 Hrs 5,935.5 Hrs (82%) MO5 (Reduction Gearbox) 3,600 Hrs 2,335.5 Hrs (65%) FCU 3,600 Hrs Hrs (4%) Item Cyc/Hrs Limit On Cond Free Turbin disk 10,000 Cyc Cyc (66%) Free Turbine Blades 12,000 Cyc/ 7,200 Hrs Cyc / Hrs (39%) 1st Stage Turb Disk 10,000 Cyc Cyc (73%) 1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs Cyc/ Hrs (78%) 2nd Stage Turb Disk 10,000 Cyc Cyc (7%) 2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs Cyc / Hrs (7%) Axial Comp Wheel 14,000 Cyc 11,345.5 Cyc (81%) Centrifugal Impeller 14,000 Cyc Cyc (34%) Injector Wheel 10,000 Cyc Cyc (73%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com

8 ENGINE #2 - ARRIEL 1E2 15, May 2017 S/N Total Time: Hrs NG Cycle: 11,625.5 NP Cycle: MO1 Interval On Cond MO1 (Accessory Gearbox) 180 M M (82%) MO2 (Axial Compressor) 7,200 Hrs 1,122.5 Hrs (16%) MO3 (Gas Generator) 3,600 Hrs 3,188.5 Hrs (89%) MO4 (Power Turbine) 7,200 Hrs 1,122.5 Hrs (16%) MO5 (Reduction Gearbox) 3,600 Hrs Hrs (13%) FCU 3,600 Hrs Hrs (28%) Item Cyc/Hrs Limit On Cond Free Turbin disk 10,000 Cyc Cyc (3%) Free Turbin Blades 12,000 Cyc/ 7,200 Hrs Cyc / Hrs (20%) 1st Stage Turb Disk 10,000 Cyc Cyc (91%) 1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs Cyc / Hrs (67%) 2nd Stage Turb Disk 10,000 Cyc Cyc (91%) 2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs Cyc / Hrs (91%) Axial Comp Wheel 22,000 Cyc 10,374.5 Cyc (47%) Centrifugal Impeller 14,000 Cyc 13,137.0 Cyc (94%) Injector Wheel 10,000 Cyc Cyc (91%) For further inquiry: Jeff Donahue Office: ; Mobile: ; jeff.donahue@airbus.com