Cessna L-19E Specifications
(performance valid only for wheel version)

* Float version

Engine:  Continental O-470-11 6 cylinder, air cooled.
Power:  Military: 213 HP at 2,600 RPM, Normal: 190 HP at 2,300 RPM.

Propeller:  McCauley metal 2-blade, 90 in diameter fixed pitch.

Dimensions

Wingspan:                                36.0 ft
Wing Area:                            174.0 sq ft
Length:                                    25.10 ft
Height:                                      7.4 ft

Empty Weight:                      1,614 lb        * 1,774 lb

Max Gross Weight:               2,400 lb

Fuel Capacity:                       43 gal (US)

Performance

Takeoff Ground Roll:                 380 ft
 
Takeoff Distance
over 50-ft obstacle:                     634 ft

Landing ground roll:                    305 ft

Landing distance
over 50-foot obstacle:                605 ft

Rate of Climb:                         1,230 ft/min     *1,100 ft/min (sea level)

Normal climb IAS:                    80 mph

Best rate of climb IAS:              65 mph


Landing approach IAS:             71 mph

Max cruise:

    TAS:                                  117 mph
    Altitude:                             10,000 ft
    Fuel flow:                            7.8 gph
    Range (no reserves):              491 mi

Max range cruise:

    TAS:                                  105 mph
    Altitude:                             15,000 ft
    Fuel flow:                            6.4 gph
    Range (no reserves):               690 mi

Max glide:

    IAS:                                    75 mph
    Glide ratio:                          7.5 to 1

Never exceed      :                 190 mph            *158 mph

Max IAS (flaps down):          100 mph            *100 mph

Max IAS
front side window open:         120 mph

Max IAS
rear side window open:          145 mph

Maneuvering IAS:                 134 mph            *113 mph

Stall speed (no flaps):              59 mph

Stall speed (full flaps):              54 mph