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SW205 Helicopters

We are pleased to offer, subject unsold or market withdrawal:



SW205 Helicopters



We have available many aircraft that we can offer for upgrade and modernization or standard configuration.



1. SW205 Overhauled with an upgraded 212 Main & Tail Rotor System (5 EA) Lead-time 60-120 days



OR



2. SW205 Overhauled with standard components (4 EA) Immediately



OR



3. SW205 Mid-time with standard components (13 EA) 45-120 days



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



#jb

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