Nord 2500 Noratlas Civil Aircraft Model Details

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General Information of Nord 2500 Noratlas

Designer : Jean Calvy

First Flight : 18151

Introduction : 19522

Manufacturer : Nord Aviation

National Origin : France

Number Built : 425

Primary Users : France; Germany; Greece; Israel

Retired : 1989, France

Role : Military Transport

Status : Retired

General characteristics of Nord 2500 Noratlas

Capacity : 45 soldiers, 36 paratroopers, 18 patients with medics, or cargo

Crew : 42465

Empty Weight : 29,327 lb (13,302 kg)

Height : 19 ft 8 in (6.0 m)

Length : 72 ft 1 in (21.96 m)

Max Takeoff Weight : 45,423 lb (20,603 kg)

Powerplant : 2 × SNECMA-manufactured Bristol Hercules 738/739 radial engine, 2,090 hp (1,558 kW) each

Useful Load : 18,647 lb (8,458 kg)

Wing Area : 1,089 ft² (101.2 m²)

Wingspan : 106 ft 8 in (32.5 m)

Performance of Nord 2500 Noratlas

Cruise Speed : 199 mph (320 km/h) at 1,500 meters

Maximum Speed : 273 mph/251 mph (440 km/h/405 km/h) maximum/under full load

Range : 1,550 mi (2,500 km)

Rate Of Climb : 1,080 ft/min (5.5 m/s)

Service Ceiling : 23,300 ft (7,100 m)

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