VENTURA
TM
Ultralight Aircraft
Pilot’s Operating Handbook
VENTURA-POH-ENG
Rev. 00
SERIAL NUMBER:
YY-MM-62-XXXX-Z
FIRST ISSUE:
04/05/2018
REVISION 00:
04/05/2018
NOT CONTROLLED COPY
PAGE:
37/60
5. PERFORMANCES
This paragraph gives information regarding take-off, climb, cruising and landing performances. All
the speeds shown are indicated on the airspeed (IAS).
WARNING
AIRCRAFT PERFORMANCES ARE INFLUENCED
BY WEATHER CONDITIONS AND ALTITUDE
(TEMPERATURE AND HUMIDITY). ALL DATA
PUBLISHED BELOW, ARE REFERRED TO ISA
(INTERNATIONAL STANDARD ATMOSPHERE).
FOR
ANY
NON-STANDARD
CLIMATIC
CONDITIONS,
APPLY
THE
NECESSARY
CORRECTIONS.
WARNING
RUNWAY SURFACE AND SLOPE, ELEVATION,
TEMPERATURE, TYPE OF PROPELLER, PITCH
SET AND OTHER OPTIONS INSTALLED, SUCH AS
TUNDRA TIRES, DETERMINE VARIATIONS IN
PERFORMANCES.
THE PUBLISHED DATA ARE REFERRED TO A
FLAT ASPHALT RUNWAY AND VENTURA
AIRCRAFT IN STANDARD CONFIGURATION
(ROTAX 912ULS AND DUC FLASH PROPELLER).
5.1. TAKE-OFF AND LANDING DISTANCES (ROTAX 912ULS)
Altitude
Take-off run
(asphalt, Flaps ½)
(990 [Lbs] / 450 [kg])
Take-off run
(asphalt, Flaps ½)
(1320 [Lbs] / 600 [kg])
Sea level
150 ft / 45 m
220 ft / 66 m
3,000 ft / 900 m
208 ft / 65 m
305 ft / 93 m
6,000 ft / 1,800 m
270 ft / 82 m
400 ft / 122 m
To obtain take-off distance on a 15 [m] / 50 [ft] obstacle, practice rule suggests to multiply the take-
off run for 2.5 times.
Weight
Landing Distance
(Asphalt, No Flap)
Landing Distance
Asphalt, Full Flap
990 Lbs / 450 Kg
767 ft / 230 m
310 ft / 95 m
1320 Lbs / 600 Kg
1065 ft / 325 m
440 ft / 135 m
