SUPER ETENDARD
| Specifications | |
|---|---|
| Country of Origin | France | 
| Builder | DASSAULT-BREGUET | 
| First flight |   May 1958  Etendard IV October 1990 (Upgraded Super Etendard)  | 
| In-service in the French Navy | 
1964  Etendard IV June 1993 (Upgraded Super Etendard)  | 
| Similar Aircraft |  
  | 
| Crew | One | 
| Role | 
  | 
| Span | 31 ft, 6 in / 9.60 meters | 
| Length | 47 ft / 14.31 meters | 
| Height | 3.85 meters | 
| Range | 750-1080 nautical miles | 
| Endurance | 1h45 to 2h15 with réservoir supplémentaire | 
| Speed |  
  | 
| Ceiling | 45,000 feet / 13700 meters | 
| Weight | 11.90 tonnes (6.25 à vide). | 
| In-Flight Refueling | Yes | 
| Internal Fuel | 2612 kg | 
| Payload | 2100 kg w/full int fuel | 
| Power plant / Thrust | SNECMA 8 K50 jet engine / 5 t | 
| Armament | 
  | 
| Systems | 
 
  | 
| Special equipment | 6 Oméra 31 cameras (100, 150, 200 and 600 mm) | 
| Drop Tanks | 
  | 
| Engine | 1 SNECMA 8K50 @ 5 tonnes thrust | 
| Sensors | Agave radar, RWR, ballistic bombsight | 
| User Country | 
  | 
| Number of units produced | 85 (all types of Super Etendard included) | 
| French Navy inventory |  
 52 Super Etendard in two squadrons 5 Etendard IV P  | 
| 
 
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