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1988 Airbus Helicopters BO-105CBS
| Overview | |
| Listing Status: | Inactive |
| This aircraft has been equipped with several highly sought-after STCs (Supplemental Type Certificates) to enhance operational ease and multi-mission capability. Noteworthy among these are a 10-inch cabin extension, a maximum gross weight increase, and an Environmental Control Unit (ECU) that provides customizable air conditioning and heating for the cabin, ensuring comfort in any season. | |
| Price: | N/A |
| Offered By: | AEROCOR |
| Registration: | N35CR |
| S/N: | S-678 |
| Location: |
Las Vegas, Nevada United States 
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| Airframe | |
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Total Cycles: 35,596.00 MAX SPEED 145 KNOTS MAX ALTITUDE 17,000 FT Component Times (Remaining Times Closest To Retire Or Overhaul) Main Transmission: 629.3 hrs Tail Rotor Gearbox: 790.2 hrs Intermediate Gearbox: 805.4 hrs Starter Generator #1: 817.2 hrs Starter Generator #2: 817.2 hrs |
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| Total Time: | 11,873.4 Hours |
| Avionics | |
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Bendix King KT-76 Transponder (2) Bendix King KY-196 VHF radio Garmin 7 inch display GPSMAP-695/EFB capable Garmin GMA 345c (3 com) audio panel with bluetooth uAvionics Tail Beacon with ADS-B “Out” BFGoodrich Skywatch 497 traffic advisory system |
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| Additional Equipment | |
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Electric gyro system Electric artificial horizon Vertical speed indicator 2 min turn indicator Instrument services clock Electric chip detectors MGB, TGB, INT G/B Shoulder harness inertial lock (pilot/co-pilot) Rotor tie downs and inlet/exhaust covers Aft cabin shoulder harness (3 each) Adjustable co-pilot seat Rear foldable bench seat Pilot/co-pilot door open locks Fire extinguisher Baggage compartment protective floor boards Map reading light Cabin and cargo compartment lights ELT 110 System (Artex) Anti-collision light (Whelen high intensity) Pendulum absorbers (oil lubricated) Reconditioned factory Interior trim Spare fuse box Rear entry clamshell doors Snow shield assembly Baggage door warning light Engine inlet screens Externally mounted mirrors Auxiliary cabin power for RAM iPad mount Max gross weight increase (SB 80-77) Center of gravity increase (Option 48-Forward center of gravity limitation extension) Pulselite lamps, L/H & R/H Pulselite Control (STC SH3319NM) Environmental Control Unit (STC SH1031EA) ECU Cutoff (STC SR08997RC) Lead Acid Battery (STC SR09016RC) Main fuel pump “off” advisory light system (STC SH920NE) Windshield defog system (STC SH7946SW) Manual Engine Anti-ice system (STC SH5847SW) Pulsed Chip Detector (STC SH1260EA) Ten inch cabin extension (STC SH1025EA) Facet oil filter (STC SH479GL) Spare Parts Available For Purchase: Extra fuselage to include: Full set of exterior panels/fairings, rear clamshell doors, rear cabin doors, various windows and fuel tanks Exhaust stacks, control tubes, flight controls, transmission mount and frame Rotor head (serviceable) Tail rotor blades (serviceable) Tail rotor pitch change links Tail rotor hub Technical Specifications: 1 or 2 Pilot with 3 or 4 passenger configuration twin engine helicopter Dual hydraulic system Cruise speed: 120 kts/138 mph Fuel capacity: 150 US gal/570 L Fuel endurance: 2 h 30 min Maximum gross weight: 5,512 lbs/2500 kgs Component Times (Remaining Times Closest To Retire Or Overhaul) |
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| Engines | |
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Make / Model: (2) Rolls Royce 250-C20B Turboshaft engines (420 SHP each) Serial Numbers: #1 Engine: CAE836419 #2 Engine: CAE836333 Total Time: #2 Engine: 9,603.6 SNEW Total Cycles: #1 Engine: 1,123 SNEW #2 Engine: 1,444 SNEW Component Times (Remaining Times Closest To Retire Or Overhaul) #1 Engine: Compressor: 1,255.8 hrs Turbine HMI: 618.6 hrs Bleed Valve: 440.0 hrs 1st Stage Wheel: 642.5 hrs 2nd Stage Wheel: 510.4 hrs Impeller: 1,205.8 hrs #2 Engine: Compressor: 849.4 hrs Turbine HMI: 225.0 hrs Turbine: 478.2 hrs 1st Stage Wheel: 504.5 hrs 2nd Stage Wheel: 250.0 hrs Impeller: 899.4 hrs |
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| Engine Hours: | 8,493.7 SNEW |
| Interior & Exterior | |
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Factory trim interior Configured with five interior seats MAX OCCUPANTS - 5 PEOPLE |
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| Black and yellow PHI paint scheme | |
| Other Info | |
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Inspection Status: This aircraft is great for part 91 operations All mandatory Airworthiness Directives complied with 12 Month Airframe Inspection: Completed Apr 2024 24 Month Transponder/Altimeter Inspection: Due 03/31/2025 12 Month ELT Inspection: Due 11/30/2024 |
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