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Airplane Model Detials


General Data

Manufacturer
Avions Pierre Robin
Model
DR 400/500
Comment
Type Nr. 45 from 10.03.1998
Modified UTC
2021-08-07 16:50:04

Speed

Vne (NEVER EXCEED)166 kt
308 KMH
Vno (max. cruise)
140 kt
260 KMH
Va (maneuver IAS)116 kt
215 KMH
Vfe (max. speed with extended flaps) 92 kt
170 KMH
Vs0 (stall IAS)
 55 kt
100 KMH

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


Flaps


Vfe (max. speed)Vat (app. speed)
2nd pos.92 kt / 170 KMH70 kt / 130 KMH


Climb Performance


Flaps at T/OFlaps retracted
Vx (best ANGLE of climb)70 kt / 130 KMH73 kt / 135 KMH
Vy (best RATE of climb)
84 kt / 155 KMH
81 kt / 150 KMH


Best glide speed:

Flaps retracted: 92 kt / 170 KMH (no Flaps), glide factor 1:9.3


Stall

Weight 1150 Kg (2535 lbs), Idle


kt / KMH IAS
Bank Angle
30°60°
Flaps retracted
60 kt / 110 KMH
64 kt / 118 KMH
84 kt / 155 KMH
Flaps T/O (pos. 1)
57 kt / 105 KMH
61 kt / 113 KMH
80 kt / 148 KMH
Flaps LND (pos. 2)
55 kt / 100 KMH
58 kt / 107 KMH
76 kt / 141 KMH


Take-Off Performance

Max. weight: 1150 Kg (2535 lbs), dry asphalt, no wind, Flaps T/O, Full Throttle, no incl., cooling open

Take-Off Speed: 59 kt / 110 KMH

IAS in 15 m / 50 ft height: 70 Kt / 130 KMH


Landing Performance

Max. weight: 1150 Kg (2535 lbs), dry asphalt, no wind, Flaps LND, Idle, no incl.

IAS in 15 m / 50 ft height: 70 kt / 130 KMH

Landing Speed: 55 kt / 109 KMH

Cross Wind: max 22 kt / 40 KMH


Engine Performance

 

Max T/O Power 5 min

2700 RPM

Max Continuous Power

2500 RPM

Max. starting time
30 sec
Max. cylinder head temp.
260 C / 500 F


G-Factors for N-Category

max negative

max positive

Flaps retracted

-1.9

+3.8

Flaps extended

0.0

+2.0

Data for CG calculation














Seats
Tanks
Trunks

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