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Airplane Model Detials


General Data

Manufacturer
Diamond
Model
DA-20 Katana
Comment
Utility
Modified UTC
2020-05-23 15:22:48

Speed

Vne (MAX. BRS DEPLOY)

161 KTS

185 MPH

298 KMH

Va (maneuver IAS)

104 KTS

120 MPH

193 KMH

Vfe (max. flaps extended)

81 KTS

93 KPH

150 KMH

Vno (max. structural cruising)

118 KTS

135 KPH

218 KMH

Do not exceed Vno speed except in smooth air, and then only with caution

 

Take-Off

Climb Speed during normal take-off for 15 m (50 ft) obstacle

60 KTS

68 MPH

110 KMH

Best Rate-of-Climb speed at sea level vy (Wing Flaps T/O)

65 KTS

75 MPH

110 KMH

Best Angle-of-Climb speed at sea level vx (Wing Flaps T/O)

57 KTS

66 KPH

106 KMH


Cruise

Maximum permissible speed in rough air VNO

118 KTS

135 MPH

218 KMH

Maximum permissible speed with full control surface deflections VA

104 KTS

120 MPH

193 KMH

Maximum permissible speed with Wing Flaps extended VFE

81 KTS

93 KPH

150 KMH


Landing

Approach speed for normal landing. Wing Flaps in landing position

57 KTS

66 MPH

106 KMH

Balked landing climb speed, Wing Flaps in landing position

57 KTS

66 MPH

106 KMH

Maximum demonstrated crosswind speed during take-off and landing

15 KTS

17 KPH

27 KMH

 

Propeller RPM (gear ratio 2.2727 : 1)

 

Max T/O Power 5 min

2550 RPM

Max Continuous Power

2420 RPM

 

Apprived Fuel Grades:

AVGAS 100LL

 

Weigth

Maximum permissible weight

1609 lbs (730 Kg)

Max. weight in the trunk

44 lbs (20 Kg)

 

Approved Maneuvers

This airplane is certified in the UTILITY Category in accordance with JAR-VLA.

Permissible Utility Category Maneuvers:

a) All normal flight maneuvers

b) Stalls (except whip stalls)

c) Lazy Eight’s Entry speed: 116 kts (215 km/h)

    Chandelles: Entry speed: 116 kts (215 km/h)

    Steep turns in which the angle of bank does not exceed 60°

d) Spinning (with Wing Flaps UP)

 

G-Factors

at VA

at VNE

with full flaps

Positive

+4.4

+4.4

+2.0

Negative

-2.2

-2.2

0


Data for CG calculation














Seats
Tanks
Trunks

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