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JURCA MJ-2 Tempete

From SKYbrary Wiki

Name MJ-2 Tempete
Manufacturer JURCA
Body Narrow
Wing Fixed Wing
WTC Light
Type code L1P
Engine Piston
Engine count Single
Mass group 1

Manufacturered as:

JURCA MJ-22 Tempete
JURCA MJ-2 Tempete
JURCA Tempete
JURCA MJ-20 Tempete
SIRAVIA MJ-22 Tempete

JURCA MJ-2 Tempete

JURCA MJ-2 Tempete


The Jurca MJ-2 Tempête (French: "Tempest") is a single-seat sport aircraft designed in France in the mid 1950s and marketed for homebuilding.

Technical Data

Wing span 6.00 m19.685 ft <br />
Length 5.85 m19.193 ft <br />
Height 2.40 m7.874 ft <br />
Powerplant 1 x Continental A-65-8, 48.5 kW (75 hp)
Engine model Continental O-170

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
(to FL100)
Descent (FL100
& below)
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 88 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance 250 m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance 250 m
MTOW 550550 kg <br />0.55 tonnes <br /> kg Ceiling FL110 ROD ft/min APC A
WTC L Range 300300 nm <br />555,600 m <br />555.6 km <br />1,822,834.647 ft <br /> NM

Accidents & Serious Incidents involving MJ2

None on SKYbrary