N543AE - 2012 EUROCOPTER EC145
Aircraft Summary
General
Year
2012
Manufacturer
EUROCOPTER
Model
EC145
Serial Number
9514
Registration #
N543AE
Condition
Used
FlightRules
IFR
Based at
KGPM
Description
Aka BK117C2. 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 standard 8-Pax .
Airframe
Total Time
2670
Complete Logs
Yes
Airframe Notes
See Sales Brochure under Service Logs Drop down Menu.
Total Time Since New: ≈2,670 hours Projected Time at Delivery: Not To Exceed 2,700 Hours Dedicated Mission: Basic Utility Delivery: As Is/Where Is, Location: FOB Grand Prairie, TX Training, at AHI: 1 Pilot Transition/1 Technician.
Rotor
Main Rotor Blade Time Remaining
22387
Main Rotor Hub Time Remaining
4760
Main Rotor Gearbox Time Remaining
2330
Anti-Torque System
Tail Rotor
Tail Rotor Blade Time Remaining
6654
Tail Rotor Gearbox Time Remaining
680
Rotor Notes
Tail Rotor and Intermediate Gearboxes can be extended by 300 hours.
Intermediate Gearbox has 334 hours remaining before overhaul; may be extended to 634 hours TBO.
T/R Gearbox has 680 hours remaining before overhaul; may be extended to 980 hours TBO.
Modifications/Conversions
Modifications/Conversions
See Sales Brochure under Service Log Drop down Menu.
CENTRAL PANEL
• Central Panel Display System (CPDS) consisting of two
LCD displays
• Cautions and Advisories Display (CAD) with digital indication of:
Caution and advisory information
Fuel quantity indication
• Vehicle and Engine Multifunction Display (VEMD) with
digital indication of:
Engine parameters (engine oil pressure, engine oil
temperature)
FLI (First Limit Indicator) for TQ, TOT,rN1 as analogue display
Main gear box parameters (oil pressure, oil temperature)
Dual amp meter for generator; ampere meter for battery
Dual voltmeter
Outside Air Temperature (OAT)
Mast moment indicator
• Back-up conventional instruments (2”)
• Clock
• Stand-by-horizon
• Triple (rotor and engines) RPM-indicator
• Warning unit
• Engine fire warning with fuel emergency shut-off
• Warning lights
• Aural warning (for each warning, rotor RPM, fire warning)
• Fire extinguishing system warning
• Master caution light
• Main switch panel
• DC power control
• VARTOMS control
• Start switches
• Magnetic compass
AIR DATA
• Dual pitot static system (electrically heated pitot tube and static port)
• 2 ADC MEGHAS sensors
STANDARD INSTRUMENTS (SINGLE PILOT)
• Air speed indicator (3”)
• Vertical speed indicator (3”)
• Encoding altimeter (3”)
• Artificial horizon (4”)
• Gyro magnetic heading with horizontal situation ind. (3”)
Avionics
ADS-B Equipped
Yes
Artificial Horizon
Yes
Radar Altimeter
Yes
Single Pilot Operation
Yes
Auto Pilot
Yes
Wire Strike Protection System
Yes
Avionics/Radios
See Sales Brochure under Service Logs Drop down Menu.
Garmin GTX 330 Transponder
Dual Garmin 430 GPS/COMM/NAV
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
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.
Additional Equipment
Dual Controls
Yes
Cargo Hook
Yes
A/C
Yes
Heater
Yes
Baggage Compartment
Yes
Additional Equipment
See Sales Brochure under Service Logs Drop down Menu
Standard Gear with Full Length Steps
Standby Attitude Gyro
Engine Fire Detection and Extinguishing System
Fuel Flow Display
Cargo Sling System Fixed Provisions
Fixed Provisions Hoist, Right Side
Cable Cutter System (Wire Strike)
Rotor Brake System
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)
Exterior
Year Painted
2012
Door Type
Hinged and Sliding
Exterior Notes
Very Good Condition
Interior
Year Interior
2012
Configuration
Passenger / Utility
Interior Notes
See Sales Brochure under Service Logs Drop down Menu
Pilot & Copilot Energy Absorbing Height Adjustable BAE Seats (STC SR01938LA).
8-Passengers Standard Energy Absorbing Seats that can be configured from One to Eight independent seating arrangements.
Alternate Nine (9) Passenger Utility BAE Troop Seats (can 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)
Inspection Status
Inspection Status
CURRENTLY IN WORK and At 2650 hours total time:
(1) Airframe 4800 hour/6 year Main rotor head inspection;
(2) Airframe 800 hour/36 month Periodical completed;
(3) Main Rotor Blades refurbished and processed through AHI Blade Shop.
Airworthy
Yes
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