Airbus Helicopters, Inc. Presentation Template · PC343CE and Conforms to Type Certificate Data...
Transcript of Airbus Helicopters, Inc. Presentation Template · PC343CE and Conforms to Type Certificate Data...
This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
BK117C2
(EC145T1)
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
BK117C2
Model: BK117C2 (EC145T1)
Twin Engine: Turbomeca Arriel 1E2
Serial Number: 9514
Registration Number: N543AE (USA)
Sales Price: $4,210,000
Available: Immediate
Manufacture Year: 2012
Total Time Since New: ≈1,485 hours
Projected Time at Delivery: Not To Exceed 1,550 Hours
Dedicated Mission: Basic Utility
Delivery: As Is/Where Is,
Location: FOB Grand Prairie, TX
Training, at AHI: 1 Pilot Transition/1 Technician
18 July 2016
General Overview
Aircraft Manufactured in the USA under Production Certificate
PC343CE and Conforms to Type Certificate Data Sheet
EASA.R.101 and FAA H13EU R12. Airbus Helicopters Maintained
and Operated. Dual Pilot IFR (Not WAAS Certified), Utility
Configured with Standard Production Release Avionics. Cabin
interior adapted to BAE Crew and Cabin High Density Style Seating.
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
BK117C2 General Equipment
• Standard Gear with Full Length Steps
• Standby Attitude Gyro
• Engine Fire Detection and Extinguishing System
• Fuel Flow Display
• Cargo Sling System, Onboard
• Bambi Bucket, Fixed Provisions
• Hoist, RH Fixed Provisions
• Cable Cutter System (Wire Strike)
• Rotor Brake System
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• 3 Axis Autopilot with Yaw SAS
• Controllable Landing/Search Light, 200W/400W
• External Lashing Points, 60 Knots
• Anti Collision LED Light (STC SR09303RC-D)
• Position LED Lights (STC SR09302RC-D)
• 44 AH Lead Acid Battery (STC SR09298RC-D)
• Dual Windshield Wiper System
• Carbide Skid Protectors, Brauer (STC SR03936AT)
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
BK117C2 Avionics
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• Garmin GTX 330 Transponder
• Dual Garmin 430 GPS/COMM/NAV
• ARTEX C406 ELT
• DME, CDM-451
• *Wulfsberg C5000 V/UHF AM/FM System
• *Dual Wulfsberg UHF-FM P2000 System (STC
SR00036MC-D)
• Marker Beacon Installation, KR 21
• 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
NOTE: Items Marked with “*” may be ITAR
Restricted if Aircraft is to be Sold outside USA.
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
18 July 2016
BK117C2 Interior
• Pilot & Copilot Energy Absorbing Height
Adjustable BAE Seats (STC SR01938LA)
• Utility BAE Troop Seats, Aft & Forward Facing
Only – 6 Passengers (STC SR01906LA)
• Alternate Six (6) Passenger Seats (to be
negotiated)
• Loincoin Cabin Flooring
• Tinted Overhead Sunshades
• Slant and XL Center Consoles
• Freon Air Conditioning, Air Comm
(STCSR00601DE)
• Dual Controls
• Cockpit Ventilation and Cabin Heat
• Crew & Cabin Door Window Vents (STC
SR09308RC-D)
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
AIRFRAME COMPONENTS
Description Interval Part number Frequency Time remaining
Main Rotor Blades, 4 ea RTR B621M1002104 12,000 Hrs 11,370 Hrs (95%)
Main Gearbox Assembly OH B632K1001051 3,600 Hrs 2,115 Hrs (59%)
Main Gearbox Case Assembly RTR B632K1020101 10,000 Hrs 8,515 Hrs (85%)
Main Rotor Shaft RTR 4639205027 30,000 Hrs 28,515 Hrs (95%)
Main Rotor Head Assembly INSP B622M1002101 4,800 Hrs 3,015 Hrs (63%)
Tension Torsion Straps, 4 ea RTR B622M10T1001 12,000 Cyc 2,394 Cyc (20%)
Inner Sleeve Assemblies, 4 ea RTR B622M1009201 15,000 Hrs 13,515 Hrs (90%)
Quad Nuts, Upper/Lower RTR B622M1004201/5201 67,000 Cyc 57,394 Cyc (86%)
Rotor Star RTR B622M1001201 25,200 Hrs 23,315 Hrs (93%)
Main Servo, Longitudinal OH B673M30A1101 7,500 Hrs 6,,015 Hrs (80%)
Main Servo, Lateral OH B673M30A1301 7,500 Hrs 6,,015 Hrs (80%)
Main Servo, Collective OH B673M30A1203 7,500 Hrs 6,,015 Hrs (80%)
Intermediate Gearbox OH 4639002009 1,500 Hrs 1,500 Hrs (100%)
Tail Rotor Transmission OH 4639003009 1,800 Hrs 315 Hrs (18%)
Tail Rotor Blade Assembly, 2 ea RTR B641M1001101 5,000 Hrs 3,519 Hrs (70%)
Laminated Pile Assembly (T/R) RTR B642M1005101 13,000 Cyc 8,977 Cyc (69%0
Airframe Components Time Remaining
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
ENGINE 1 - ARRIEL 1E2
Serial Number 48321TEC
Item Interval Remaining Life
MO1 On Condition N/A
MO2 7,200 Hrs 5,715 Hrs (79%)
MO3 3,600 Hrs 2,115 Hrs (59%)
MO4 7,200 Hrs 5,715 Hrs (79%)
MO5 3,600 Hrs 2,115 Hrs (59%)
FCU 3,000 Hrs 1,515 Hrs (51%)
Service Life Limits
Item Cyc/Hrs Limit Remaining
Free Turbine Disk 10,000 Cyc 8538 Cyc (85%)
Free Turbine Blades 12,000 Cyc 10,538 (88%)
1st Stage Turb Disk 10,000 Cyc 8,014 Cyc (80%)
1st Stg Turb Blades 12,000 Cyc/6,000 Hrs 10,014 Cyc/4,515 Hrs (75%)
2nd Stage Turb Disk 10,000 Cyc 8,014 Cyc (80%)
2nd Stg Turb Blades 10,000 Cyc/6,000 Hrs 8,014 Cyc/4,515 Hrs (75%)
Axial Comp Wheel 14,000 Cyc 12,014 Cyc (86%)
Centrifugal Impeller 14,000 Cyc 12,014 (86%)
Injector Wheel 10,000 Cyc 8,014 Cyc (80%)
Engine Components Time Remaining
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ENGINE 2 - ARRIEL 1E2
Serial Number 48323TEC
Item Interval Remaining Life
MO1 On Condition N/A
MO2 7,200 Hrs 5,715 Hrs (79%)
MO3 3,600 Hrs 2,115 Hrs (59%)
MO4 7,200 Hrs 5,715 Hrs (79%)
MO5 3,600 Hrs 2,115 Hrs (59%)
FCU 3,000 Hrs 1,515 Hrs (51%)
Service Life Limits
Item Cyc/Hrs Limit Remaining
Free Turbine Disk 10,000 Cyc 8535 Cyc (85%)
Free Turbine Blades 12,000 Cyc 10,535 (88%)
1st Stage Turb Disk 10,000 Cyc 7,914 Cyc (79%)
1st Stg Turb Blades 12,000 Cyc/6,000 Hrs 9,914 Cyc/4,515 Hrs (75%)
2nd Stage Turb Disk 10,000 Cyc 7,914 Cyc (79%)
2nd Stg Turb Blades 10,000 Cyc/6,000 Hrs 7,914 Cyc/4,515 Hrs (75%)
Axial Comp Wheel 14,000 Cyc 11,914 Cyc (85%)
Centrifugal Impeller 14,000 Cyc 11,914 (85%)
Injector Wheel 10,000 Cyc 7,914 Cyc (79%)
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This document contains proprietary data or other confidential information of Airbus Helicopters, Inc. (“AHI”) or its affiliates, which shall not
be disclosed to any third party or reproduced, in whole or in part, without AHI’s prior written consent.
Inspections, Primary
14, July 2016
For further inquiry:
Jeff Donahue
Office: (972) 641-3735 Mobile: (972) 955-6177 Email: [email protected]
AIRFRAME INSPECTIONS*
Description Frequency Time remaining
Airframe, Supplemental 300 Hrs 280 Hrs (93%)
Airframe, Intermediate 400 Hrs 121 Hrs (30%)
Airframe, Periodic 800 Hrs 521 Hrs (65%)
Engine 800 Hrs 695 (87%)
Engine 1,200 Hrs 914 (76%)
*Aircraft and Engine Status Runs will be supplied upon Request.