Dassault Mercure

Airplanes

Length

34.84 m

Flat Wing Span

30.55 m

Height

11.36 m

Flat Wing Area

116 m²

Flat Wing Aspect Ratio

Cruise Speed

926 km/h

Max Speed

704 km/h

Max Mach

0.85 Mach

Max Ceiling

11887.2 m

Number of Engines

Aircraft Engine

First Flight

1971-05-28

Entry Into service

1974-06-04

Number Built

Maximum Take-Off Weight

56.5 t (paragliders: kg)

Total Fuel Capacity

18400

Maximum Range

2084 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Total Fuel Capacity	Maximum Range (km)
Dassault Mercure	56.5	18400	2084

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
737-300	CFM International CFM56	33.4	28.9	126	Compare
Embraer Lineage 1000		36.24	28.72	13	Compare
Antonov An-178	Progress D-436	32.23	30.57	70	Compare
Falcon 10X		33.4	33.6		Compare
737-100	Pratt & Whitney JT8D	30.53	28.35	102	Compare
McDonnell Douglas C-9		36.2712	28.3464	76	Compare

All data (29 fields)

Name: Dassault Mercure
Manufacturer: Dassault Aviation
Description: The Dassault Mercure is a twin-engined narrow-body jet-powered airliner developed and manufactured by French aircraft firm Dassault Aviation.
First Flight: 1971-05-28
Entry Into service: 1974-06-04
Production End: 1975-01-01
Service End: 1995-04-29
Designer: Dassault Aviation
Type: Narrow-body jet airliner
Length (m): 34.84
Height (m): 11.36
Cockpit Crew: 3
Max Speed (km/h): 704
Cruise Speed (km/h): 926
Max Ceiling (m): 11887.2
Rate of Climb (m/s): 16.764
Capacity Description: 162 all-economy
Max Mach (Mach): 0.85
National Origin: France
Number Built: 12
Powerplant Description: 2 × Pratt & Whitney JT8D-15 low bypass turbofan engines
Primary Users: Air Inter
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Dassault_Mercure
Flat Wing Span (m): 30.55
Flat Wing Area (m²): 116
Flat Wing Aspect Ratio: 8
Aircraft Engine: Pratt & Whitney JT8D
Number of Engines: 2