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for SALE S/N 9069

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Page 1: for SALE - airbushelicoptersinc.comairbushelicoptersinc.com/images/products/Pre-owned/BK117C2-SN-9069..., no part of it shall be reproduced or transmitted without the express prior

for SALES/N 9069

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S/N 9069

Aircraft details:

Airbus Helicopters BK117C2 $2,950,000

S/N 9069

Flight hours ~ 8,007h

Year of Production 2005

Engine 2x Turbomeca Arriel 1E2

Availability Immediate

Pilot Single

VFR / IFR IFR

Day / Night Yes

CAT A Yes

EASA-OPS Yes

Highlights: General Equipment EMS Systems and Components

Night Scanner Search light System

Avionics Dual GNS 530/430 Comm Nav System

KTS 870 TAS System HD117-30-8017

Sky Trac Phone System

RDR 2000 WX Radar System HD117-30-8013

Interior layout EMS Configuration

Exterior layout 3 Color Paint scheme

Conditional Solely maintained /operated by one owner

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

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TTSN: 428.3 hours

Cockpit view: NVG certified cockpit

Stretchers

Interior layout: leather seats

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

S/N 9069

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TTSN: 428.3 hours

Exterior view: Cable cutters

Exterior view: Clamshell doors/windows

Exterior view:

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

S/N 9069

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AIRFRAME ENGINE MODEL

Total time: Approx. 8,007 hrs. Arriel 1E2

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)

AVIONICS (1)

KRA 405B Rad Alt System KR 21 Marker Beacon System Crew NAT Audio System, Dual AA96-863 RDR 2000 WX Radar System VHF/UHF/FM TDFM 6158 System Dual GNS 530/430 Comm Nav System Cabin NAT Audio, AA95-729

MAIN FEATURES & EQUIPMENT (1)

Night Scanner Search light System, 099-799-100 Strobe Lights System. A650 2EA Hover Lights System. 2EA H0135-62-2001 Tel Tail Light, 13500001-1 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

The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

S/N 9069

ADDITIONAL EQUIPMENT

AFT facing seats, 2 each Cabin/Loading Light Syst Portable Oxygen D-CYL IV Hooks

Air Conditioning System, metro STCSH3880SW

Tanis Preheat System First Aid kit WSI/FG Flight Bag Provisions AFT Ballast 117-84264 (STC SR09306RC-D)

EMERGENCY MEDICAL SYSTEM (1), (2)

(1) Helidyne FAA Forms 337, dated 10/3, 10/6 or 10/7 2005 with DER report or FAA Field approval

(2) Keystone Helicopters , EMS interior installed, STC SR01968NY-D

AND

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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

AIRFRAME

Description Interval Part number Frequency Time remaining

Main Rotor Blades RTR B621M1002104 12,000 Hrs 7818.6 Hrs (65%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 6,183.8 Hrs (52%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 6,095.7 Hrs (51%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 7,839.3 Hrs (65%)

Main Transmission OH B632K1001051 5,000 Hrs 1,980.0 Hrs (40%)

Main Gearbox Case Assembly RTR B632K1020101 10,000 Hrs 3,380.4 Hrs (34%)

Main Rotor Shaft RTR 4639305102 30,000 Hrs 24,676.1 Hrs (82%)

Main Rotor Head Assembly INSP B622M1002101 4,800 Hrs 4,800.0 Hrs (100%)

Tension Torsion Straps, 4 ea RTR B622M10T1001 11,950 Cyc 6,362.0 Cyc (53%)

Inner Sleeve Assemblies, 4 ea RTRC B622M1009201 15,000 Hrs 6,993.4 Hrs (47%)

Quad Nuts, Upper/Lower RTR B622M1004201/5201 67,000 Cyc 40,659.0 Cyc (61%)

Rotor Star RTR B622M1001201 25,200 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 4639002009 1,500 Hrs 70.7 Hrs (5%)

Tail Rotor Transmission OH 4639003011 1,800 Hrs 1,028.2 Hrs (57%)

Tail Rotor Blade Assembly RTR B641M1001101 5,000 Hrs 3,084.6 Hrs (62%)

Tail Rotor Blade Assembly RTR B641M1001101 5,000 Hrs 4997.1 Hrs (100%)

Laminated Pile Assembly (T/R) RTR B642M1005101 13,000 Cyc 1351.0 Hrs (10%)

For further inquiry:

Jeff Donahue

Office: 972-641-3735 ; Mobile: 972-955-6177 ; Email: [email protected]

S/N 9069

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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

For further inquiry:

Jeff Donahue

Office: 972-641-3735 ; Mobile: 972-955-6177 ; Email: [email protected]

S/N 9069

ENGINE #1 - ARRIEL 1E2 15, May 2017 S/N 18743

Total Time: 7437.5 Hrs NG Cycle: 14,236.5 NP Cycle: 7274.0

MO1 Interval On Cond

MO1 (Accessory Gearbox) 180 M 149.0 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 134.1 Hrs (4%)

Item Cyc/Hrs Limit On Cond

Free Turbin disk 10,000 Cyc 6602.0 Cyc (66%)

Free Turbine Blades 12,000 Cyc/ 7,200 Hrs 4726.0 Cyc / 4786.5 Hrs (39%)

1st Stage Turb Disk 10,000 Cyc 7345.5 Cyc (73%)

1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 9345.5 Cyc/ 4735.5 Hrs (78%)

2nd Stage Turb Disk 10,000 Cyc 696.5 Cyc (7%)

2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 696.5 Cyc / 1531.5 Hrs (7%)

Axial Comp Wheel 14,000 Cyc 11,345.5 Cyc (81%)

Centrifugal Impeller 14,000 Cyc 4696.5 Cyc (34%)

Injector Wheel 10,000 Cyc 7345.5 Cyc (73%)

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The data set forth in this document are general in nature and for information purposes only. For performance data and operating limitations, reference must be made to the approved flight manual and all appropriate documents.

This document is property of Airbus Helicopters®, no part of it shall be reproduced or transmitted without the express prior written authorization of Airbus Helicopters® and its contents shall not be disclosed.

©Airbus Helicopters® 2017-- All rights reserved.

For further inquiry:

Jeff Donahue

Office: 972-641-3735 ; Mobile: 972-955-6177 ; Email: [email protected]

S/N 9069

ENGINE #2 - ARRIEL 1E2 15, May 2017 S/N 18696

Total Time: 6078.5 Hrs NG Cycle: 11,625.5 NP Cycle: 9872.0

MO1 Interval On Cond

MO1 (Accessory Gearbox) 180 M 147.5 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 464.5 Hrs (13%)

FCU 3,600 Hrs 994.3 Hrs (28%)

Item Cyc/Hrs Limit On Cond

Free Turbin disk 10,000 Cyc Will Be Replaced Prior to Sale

Free Turbin Blades 12,000 Cyc/ 7,200 Hrs Will Be Replaced Prior to Sale

1st Stage Turb Disk 10,000 Cyc 9137.0 Cyc (91%)

1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 8084.7 Cyc /4188.2 Hrs (67%)

2nd Stage Turb Disk 10,000 Cyc 9137.0 Cyc (91%)

2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 9137.0 Cyc / 5588.5 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 9137.0 Cyc (91%)


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