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SW204 HP HELICOPTER WITH T53-L-703 ENGINE



Aircraft Model: SW204HP



Certification: DR Standard Transport Category Airworthiness Certificate



Production Certificate: HI-101



T.C.D.S: Dominican Republic H6SO



Engine Model: T53-L-13B



Engine Hours: TBO: 2400 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 Paint

Dual Flight Controls

Utility Seating Configuration

Wire Strike Kit

Door Struts

KAFLEX Main Driveshaft

Standard Aircraft Exterior Dimensions:



Length, fuselage, ft (m) 40.38 (12.31) Width, fuselage, ft (m) 8.00 (2.44)

Length, T/R turning, ft (m) 44.65 (13.61) Width, widest point, ft (m) 9.33 (2.84)

Length, both turning, ft (m) 57.10 (17.40) Width, landing gear, ft (m) 8.37 (2.55)

Height, top, rotor hub, ft (m) 12.40 (3.78) Gr clearance, fuselage, ft (m) N/A (N/A)

Height, top, T/R arc, ft (m) 14.60 (4.45) Gr clearance, T/R, ft (m) 6.10 (1.86)



Standard Aircraft Interior Dimensions:



Cabin Cabin



Length, max, ft (m) 5.00 (1.52) Width 7.67 (2.34)

Height, max, ft (m) 4.67 (1.42) Volume, ft3 (m3) 140.00 (3.96)



Standard Aircraft Weights: (Typical)



Max gross, lbs (kg) 8,501 (3856) Empty, std acft, lbs (kg) 4,799 (2177)

Useful load, lbs (kg) 3,702 (1679) Useful, with full fuel, lbs (kg) 2,081 (944)

External load, lbs (kg) 4,000 (1814) Gross with ext load, lbs (kg) 9,500 (4309)



SW204HP 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



Specification and photos are not contractual and are subject to verification upon inspection



#jb

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