2013 BELL 407GX

2013

54461

Gebraucht

2x Bell 407GX's For Sale - Contact For Information: Premium Corporate & Utility Helicopter Bell 407GX | Serial Number 54461 | N-Registered An exceptional opportunity to acquire one or both meticulously maintained Bell 407GX with low airframe and engine hours, comprehensive maintenance history, and an extensive list of desirable upgrades. Manufactured in October 2013, this aircraft has had a single previous owner and had been continuously maintained by Bell-authorised service facilities. The helicopter has always been hangared and presents in excellent mechanical and cosmetic condition. AIRCRAFT HIGHLIGHTS: • Bell 407GX with Garmin G1000H Integrated Flight Deck • Airframe Time: 1,620.0 Hours • Rolls-Royce 250-C47B Engine • Engine Time Since New: 1,949.8 Hours • Engine Time Since O/H: Nil Hours • Total Engine Cycles: 2,385 • One Previous Owner since new • Always Hangared • Nil damage History • Original logbooks since New • Compressor 2,000 Hour inspection Completed OPERATIONAL STATUS: The aircraft will be sold on the N-Register and are supported by current records, current maintenance documentation, and a comprehensive component status report available to qualified purchasers. This is a turnkey Bell 407GX offering low hours, outstanding maintenance pedigree, excellent equipment specification, and immediate operational availability.

1,620

AIRFRAME STRUCTURE: Component Remaining Life Spring Pylon Restraints: 3,435 hrs Side Beam Pylons (LH & RH): 3,435 hrs Cyclic Bellcranks: 3,435 hrs Collective Bellcrank: 3,435 hrs Bellcrank Support: 3,435 hrs

MAJOR DYNAMIC COMPONENTS: Component TSN / Remaining Life Transmission: 1,620.2 hrs / 2,880 hrs Main Driveshaft: 1,620.2 hrs / 880 hrs Rotor Brake Disc: 1,620.2 hrs / 1,380 hrs Rotor Brake Calipers (2): 1,620.2 hrs / 1,979 hrs Mast Assembly: 1,620.2 hrs / 880 hrs Mast Pole: 1,620.2 hrs / 4,680 hrs / 95,530 RIN Swashplate & Support: 1,620.2 hrs / 880 hrs Main Rotor Hub: 1,620.2 hrs / 880 hrs Tail Rotor Gearbox: 1,620.2 hrs / 3,380 hrs Tail Rotor Hub: 1,620.2 hrs / 880 hrs Tail Rotor Yoke: 1,620.2 hrs / 3,430 hrs MAIN ROTOR SYSTEM: Component Remaining Life Anti Drive Links: 3,380 hrs Anti Drive Lever: 3,380 hrs Main Rotor Grips (4): 3,380 hrs Upper Plate: 935 hrs Lower Plate: 935 hrs Drive Ring Set: 96,424 RIN Rod End Assemblies (4): 3,435 hrs Main Rotor Clevises (4): 3,435 hrs

ROLLS ROYCE M250-C47B

CAE-848483

1,949.8 SNEW

ENGINE & MAINTENANCE: The Rolls-Royce 250-C47B engine has benefited from recent maintenance and upgrades, including: • Recent Turbine overhaul, inspections and Gearbox upgrades completed by Standard Aero Canada • Engine gearbox oil delivery tube modification completed by Standard Aero • Extensive component life remaining • A comprehensive review of tech bulletins, service installations and commercial engine bulletins as a general review carried out The aircraft has recently undergone significant scheduled maintenance and inspections, including full revision of engine and airframe logbook records ensuring excellent operational readiness and greatly reduced near-term maintenance exposure. Engine Model: Rolls-Royce 250-C47B Serial Number: CAE-484605 Time Since New: 1,949.8 Hours Cycles Since New: 2,385 Recent Work: Turbine overhaul and gearbox upgrades by Standard Aero Canada Upgrade: Engine Gearbox Oil Delivery Tube Modification incorporated ENGINE COMPONENT STATUS: Component Remaining Hours / Cycles 1st Stage Wheel: 2,025 hrs / 3,000 cycles 2nd Stage Wheel: 2,025 hrs / 3,000 cycles 3rd Stage Wheel: 2,600 hrs / 3,615 cycles 4th Stage Wheel: 2,600 hrs / 3,615 cycles Impeller: 5,793 hrs / 13,023 cycles Bleed Valve: 1,025 hrs Fuel Nozzle: 2,000 hrs HMU: 793 hrs

AVIONICS: The aircraft is equipped with the highly regarded Garmin G1000H avionics suite featuring: • Dual Garmin GIA 63H GPS/COM/NAV Units • Garmin GTX 33H Transponder • ADSB compliant • Integrated glass cockpit system • Enhanced situational awareness and operational capability LUBRICANTS: System Lubricant Engine: AeroShell 560 Transmission: AeroShell 555 Main & Tail Rotor Systems: AeroShell 555 Swashplate & Tail Rotor Drive: Mobil 28 Hydraulic System: Fluid 41

INSTALLED EQUIPMENT & STC FACTORY UPGRADES: This Bell 407GX is extensively equipped with operational and comfort-enhancing modifications including: • Inlet Barrier Filter (IBF) System • Improved Hover Performance Kit • Wire Strike Protection System • Vapor Cycle Air Conditioning • Bleed air heating • High Skid Gear • Dual Controls with Tail Rotor Pedal Lockout • Rear View Tail Camera • Rotor Brake • Nicad battery with fresh deep cycle • Ground Handling Wheels • Quick Release Front Doors • Full Rotor Tie-Down Kit • Inlet Plugs and Exhaust Covers • Cabin and boot floor protectors • Maintenance hand holds and steps fitted • Cargo Hook Kit Installed SUPPLEMENTAL TYPE CERTIFICATES & EQUIPMENT: • Inlet Barrier Filter (IBF) System • Dual Controls with Tail Rotor Pedal Lockout • Pre-Flight Step/Handle • Crew Door Opener Kits • Passenger Door Opener Kits • Spacemaker Kit • Folding Maintenance Step • Baggage Door Protector • High Skid Gear • Flitestep Kit • Improved Hover Performance Kit • Wire Strike Protection System • Window and Windshield Kit • Vapour Cycle Air Conditioning System • Cabin Floor Protectors • Boot Floor Protectors • Tail Rotor Camera • LED navigation and landing lights • VIP Interior • Quick Release Front Doors • Artex ELT • Bleed Air Heat • Rotor Brake • Seven Place Intercom System • High Visibility Main Rotor Blade Paint Scheme • Corporate Leather Interior • Cabin Sound Proofing • Main Rotor Frahm • Ground Handling Wheels • Inlet Plugs and Exhaust Covers • Full Rotor Tie-Down Set

PAINT SCHEME: • Primary Colour: Ferrari Red • Accent: Strawberry Pearl • Accent: White Fire Pearl • High visibility Main Rotor paint scheme

EXECUTIVE INTERIOR: Configured for both corporate and utility operations, the aircraft features: • VIP factory Leather Interior • Matching factory carpet to seat color • Sound-Proofed Cabin • Seven-Place Intercom System • Corporate Cabin Finish • Rear cabin interior lighting

MAINTENANCE STATUS: • Nil damage History • One Previous Owner • Always Hangared • Extensive Annual Inspection Completed • All Engine Inspections Completed • A review of TB’s, service installation instructions and CEB’s carried out as a general review • 1,200 Hour Inspection Completed • 24 Month Inspection Completed • 60 Month Inspection Completed • Compressor 2,000 Hour Inspection Completed • Complete log books Available Since New • No Unauthorised Modifications • Documentation Available for Qualified Purchasers Logbooks, maintenance records, component tracking reports and supporting documentation are available upon request for qualified buyers. Technical specifications up to date as of the 17/6/26 and are subject to change depending on customer requirements. Hassle free Worldwide shipping and packaging can be arranged.