AEROSPATIALE PUMA Civil Aircraft Model Details

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General Information of AEROSPATIALE PUMA

Developed Into : Eurocopter AS332 Super Puma; Denel AH-2 Rooivalk

First Flight : 23847

Introduction : 1968

Number Built : 697

Primary Users : French Army; Royal Air Force; Romanian Air Force

Produced : 1968-1987

Role : Utility helicopter

Status : Active service

Variants : IAR 330 ; Atlas Oryx

General characteristics of AEROSPATIALE PUMA

Capacity : 16 passengers

Crew : 3

Disc Area : 177.0 m² (1,905 ft²)

Empty Weight : 3,536 kg (7,795 lb)

Height : 5.14 m (16 ft 10½ in)

Length : 18.15 m (59 ft 6½ in)

Max Takeoff Weight : 7,000 kg (15,430 lb)

Powerplant : 2× Turbomeca Turmo IVC turboshafts, 1,175 kW (1,575 hp) each

Rotor Diameter : 15.00 m (49 ft 2½ in)

Performance of AEROSPATIALE PUMA

Cruise Speed : 248 km/h (134 knots, 154 mph) econ cruise

Maximum Speed : 257 km/h (138 knots, 159 mph)

Never Exceed Speed : 273 km/h (147 knots, 169 mph)

Range : 580 km (313 nm, 360 mi)

Rate Of Climb : 7.1 m/s (1,400 ft/min)

Service Ceiling : 4,800 m (15,750 ft)

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