for SALE S/N 9084

S/N 9084

Aircraft details:

Airbus Helicopters BK117C2 MAKE OFFER

S/N 9084

Flight hours ~ 6,283 h

Year of Production 2006

Engine 2x Turbomeca Arriel 1E2

Availability Immediate

Pilot Single

VFR / IFR IFR

Day / Night Yes

CAT A 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.

TTSN: 428.3 hours

Cockpit view: Instrument panel ,

NVG compatible

Interior layout: EMS interior

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 9084

TTSN: 428.3 hours

Interior view: Seating configuration

Exterior view: Clamshell door 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 9084

AIRFRAME ENGINE MODEL

Total time: Approx. 6,282 hrs. Arriel 1E2

Medical Floor with litter attachment Stretchers, primary and secondary Storage Box. Stretcher Overhead Console Vacuum Pump (Qty 2) Air Pump 24V Switching Regulator Medical Outlet, 11 SVAC Window accessory bar, STC SR094405RC Oxygen Storage Cabinet Storage Pockets

ADDITIONAL EQUIPMENT

Attendant seats, RM For and Aft Facing/ LMAFTFacing Portable Oxygen Cyl IV Hooks Cabin/Loading Lights

Air Conditioning System, Metro SH3880SW Tanis Preheat System First Aid kit Flight Bag Provisions, WSI/FG-4000 AFT Ballast Kit, STC SR09306RC-D

AVIONICS (1)

KRA 405B RAD Alt System KR 21 Marker Beacon System Crew NAT Audio System, Pilot/Copilot AA95 RDR 2000 WX Radar System VHF/UHF/FM TDFM 6158 VHF/FM, FFM-30 GNS 530/430 Comm Nav System DMS-44A DME System DMS 44A Cabin Audio, NAT AA95

MAIN FEATURES & EQUIPMENT (1)

Night Scanner Search light System Strobe Lights System Hover Lights System Tel Tail Light Cable Cutter System Medium height skid gears

TAS System KTA 870 ELT System, C406 Sky Trac ISAT-100 Transponder System, Dual GTX 330 HEGPWS, MK XXI NVG Lightning 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.

S/N 9084

EMERGENCY MEDICAL SYSTEM (2), (3), (4)

(1) Helidyne FAA Forms 337’s dated 6/15, 6/18 2006 with FAA 8110 Engineering reports

(2) Metro Aviation STC SRO9403RC

(3) Metro Pallet per form FAA337 dated 02/15/2013

(4) Medseats, Keystone STC SR01968NY-D

AND

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 5,716.9 Hrs (48%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 5,167.4 Hrs (43%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 8,286.1 Hrs (69%)

Main Rotor Blades RTR B621M1002104 12,000 Hrs 10,531.4 Hrs (88%)

Main Transmission OH B632M2001102 5,000 Hrs 2,406.9 Hrs (48%)

Main Gearbox Case Assembly RTR B632K1020101 10,000 Hrs 3,168.9 Hrs (32%)

Main Rotor Shaft RTR 4639305102 30,000 Hrs 23,168.9 Hrs (77%)

Main Rotor Head Assembly INSP B622M1002101 4,800 Hrs 2,842.9 Hrs (59%)

Tension Torsion Straps, 4 ea RTR B622M10T1001 12,000 Cyc 4,253.0 Cyc (36%)

Inner Sleeve Assemblies, 4 ea RTR B622M1009201 15,000 Hrs 8,716.9 Hrs (58%)

Quad Nuts, Upper/Lower RTR B622M1004201/5201 67,000 Cyc 59,303.0 Cyc (89%)

Rotor Star RTR B622M1001201 25,200 Hrs 18,916.9 Hrs (75%)

Main Servo, Longitudinal OH B673M30A1101 7,500 Hrs 1,216.9 Hrs (16%)

Main Servo, Lateral OH B673M30A1301 7,500 Hrs 1,216.9 Hrs (16%)

Main Servo, Collective OH B673M30A1203 7,500 Hrs 1,216.9 Hrs (16%)

Intermediate Gearbox OH 4639002009 1,500 Hrs 813..4 Hrs (54%)

Tail Rotor Transmission OH 4639003011 1,800 Hrs 472.2 Hrs (26%)

Tail Rotor Blade Assembly, 2 ea RTR B641M1001101 5,000 Hrs 4,390.7 Hrs (88%)

Laminated Pile Assembly (T/R) RTR B642M1005101 13,000 Cyc 10,619.0 Cyc (82%)

For further inquiry:

Jeff Donahue

Office: 972-641-3735 ; Mobile: 972-955-6177 ; Email: jeff.donahue@airbus.com

S/N 9084

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: jeff.donahue@airbus.com

S/N 9084

ENGINE #1 - ARRIEL 1E2 15, May 2017

S/N 18811

Total Time: 7079.0 Hrs NG Cycle: 14,285.0 NP Cycle: 10,485.0

MO1 Interval On Cond

MO1 (Accessory Gearbox) 180 M 107.8 M (60%)

MO2 (Axial Compressor) 7,200 Hrs 121.0 Hrs (2%)

MO3 (Gas Generator) 3,600 Hrs 1136.2Hrs (32%)

MO4 (Power Turbine) 7,200 Hrs 2727.6 Hrs (38%)

MO5 (Reduction Gearbox) 3,600 Hrs 3107.3 Hrs (86%)

FCU 3,600 Hrs 298.9 Hrs (8%)

Item Cyc/Hrs Limit On Cond

Free Turbin disk 10,000 Cyc 4507.0 Cyc (45%)

Free Turbine Blades 12,000 Cyc/ 7,200 Hrs 6507.0 Cyc / 5127.7 Hrs (54%)

1st Stage Turb Disk 10,000 Cyc 8457.7 Cyc (85%)

1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 10,457.7 Cyc / 5334.9 Hrs (87%)

2nd Stage Turb Disk 10,000 Cyc 8457.7 Cyc (85%)

2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 8457.7 Cyc / 5334.9 Hrs (85%)

Axial Comp Wheel 22,000 Cyc 7715.0 Cyc (35%)

Centrifugal Impeller 14,000 Cyc 5272.2 Cyc (38%)

Injector Wheel 10,000 Cyc 8457.7 Cyc (85%)

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: jeff.donahue@airbus.com

S/N 9084

ENGINE #2 - ARRIEL 1E2 15, May 2017

S/N 18809

Total Time: 7039.1 Hrs NG Cycle: 14,240.8 NP Cycle: 10,677.0

MO1 Interval On Cond

MO1 (Accessory Gearbox) 180 M 49.1 M (27%)

MO2 (Axial Compressor) 7,200 Hrs 160.9 Hrs (2%)

MO3 (Gas Generator) 3,600 Hrs 1135.2Hrs (32%)

MO4 (Power Turbine) 7,200 Hrs 3160.8 Hrs (44%)

MO5 (Reduction Gearbox) 3,600 Hrs 2989.7 Hrs (83%)

FCU 3,600 Hrs 2989.7 Hrs (83%)

Item Cyc/Hrs Limit On Cond

Free Turbin disk 10,000 Cyc 6049.0 Cyc (60 %)

Free Turbine Blades 12,000 Cyc/ 7,200 Hrs 7417.0 Cyc / 4847.4 Hrs (62%)

1st Stage Turb Disk 10,000 Cyc 4805.2 Cyc (48%)

1st Stage Turb Blades 12,000 Cyc/ 6000 Hrs 6805.2 Cyc / 3535.2 Hrs (57%)

2nd Stage Turb Disk 10,000 Cyc 4805.2 Cyc (48%)

2nd Stage Turb Blades 10,000 Cyc/ 6000 Hrs 4805.2 Cyc / 3535.2 Hrs (48%)

Axial Comp Wheel 22,000 Cyc 7759.2 Cyc (55%)

Centrifugal Impeller 14,000 Cyc 8805.2 Cyc (63%)

Injector Wheel 10,000 Cyc 4805.2 Cyc (48%)