True Blue Air Services

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Catalog #: 142788
Catagory: Aircraft -->Rotor (Helicopters)

Price: CONTACT US
Date Added: February 19, 2022

We are pleased to offer, subject unsold or market withdrawal: Fully refurbished Helicopter Bell UH-1H to the SW205 Standard SW205 HP HELICOPTER WITH T53-L-703 ENGINE Aircraft Model: SW205 Certification: DR Standard Transport Category Airworthiness Certificate Production Certificate: HI-101 TCDS: H6SO Engine Model: T53-L-703 Engine Hours: TBO: 3500 TSO: 0.0 NEW: Soundproofing, Battery (Lead Acid), Seat Covers, Seat Belts, Fire Extinguisher, Windows MID-TIME: 212 Main Rotor Blades & 212 Tail Rotor Blades OVERHAULED: Power-train components ALL current applicable A.D.’s, complied with Current Annual Inspection Transponder Vertical Fin Spar Kit VHF/NAV Radio New Single Stage Paint Dual Flight Controls Utility Seating Configuration Wire Strike Kit Door Struts KAFLEX Main Driveshaft Dual Hydraulics 6000 lbs. On-board Cargo Hook Kit 212 Stabilizer Bar Tubes 212 Transmission, 42° Gearbox, Nose GPS Standard Aircraft Exterior Dimensions: Length, fuselage, ft (m) 42.39 (12.92) Width, fuselage, ft (m) 8.00 (2.44) Length, T/R turning, ft (m) 42.39 (12.92) Width, widest point, ft (m) 8.00 (2.44) Length, both turning, ft (m) 42.39 (12.92) Width, landing gear, ft (m) 8.00 (2.44) Height, top, rotor hub, ft (m) 14.39 (4.390) Gr clearance, fuselage, ft (m) 1.18 (0.36) Height, top, T/R arc, ft (m) 14.39 (4.390) Gr clearance, T/R, ft (m) NA (NA) Standard Aircraft Interior Dimensions: Cabin Cabin Length, max, ft (m) 7.67 (2.33) Width 8.00 (2.44) Height, max, ft (m) 4.33 (1.32) Volume, ft3 (m3) 200.00 (6.32) Standard Aircraft Weights: (Typical) Max gross, lbs (kg) 11,200 (5080) Empty, std acft, lbs (kg) 4,840 (2200) Useful load, lbs (kg) 5,660 (2573) Useful, with full fuel, lbs (kg) 4,220 (1918) External load, lbs (kg) 6,000 (2727) Gross with ext load, lbs (kg) 11,200 (5080) SW205HP WITH T53-L-703 ENGINE TAKEOFF AND LANDING GROSS WEIGHT VERSUS AMBIENT AIR TEMPERATURE AND PRESSURE ALTITUDE AMBIENT AIR TEMPERATURE- °C WEIGHT– ALTITUDE– TEMPERATURE LIMITATIONS FOR TAKEOFF AND LANDING

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