Udet U-12 Flamingo

Udet U-12 Flamingo type list

a Basic training with Sh 11 engine
b Aerobatic trainer with an improved wing profile
c Advanced trainer with reduced wing area
d Like b but with Sh 12 engine
e c and d combination
w with floats and Sh 12 engine
H Standard Flamingo H = Holz, austrian designation
S Designed by Hämmerle in Austria S = Stahl, steel tube fuselage
o same as S
Hungária I Designed in Hungary , development of U-12.
Hungária II Designed in Hungary , development of U-12.
Hungária III Designed in Hungary , development of U-12.
Hungária IV Designed in Hungary , development of U-12.
Hungária V Designed in Hungary , development of U-12.

Hungária types ( 1 WM licence-built Sh 12 )

Data I II III IV V
Span m 10.0 10.3 10.5 10.3 10.3
Length m 7.4 6.9 7.7 6.9 6.9
Wingarea m2 25.0 26.0 25.0 26.0 26.0
Wingloading kg/m2 33.7 30.0 35.0 32.0 38.0
Weight empty kg 590 547 595 582 587
Weight loaded kg 840 797 845 817 897
Max. speed km/h 150 140 165 150 140
Wing strut formation N N N I N

III also had prop.spinner, Townend-ring and modified landing-gear

As a fighter trainer equipped with 2 8 mm Type 26/31 M Gebauer GKM machineguns

As a bomber trainer carried 10 - 20 kg bombs

Production

Company Number built
Udet Flugzeugbau, Ramersdorf 35 +
Bayerische Flugzeugwerke AG 150
Fliegerwerft Thalerhof 20
Central Repair Workshops ,Hungary 40
Manfred Weiss, Hungary 40
AS. Chr. Backman, Latvia 10
Aviation Regiment Workshop, Latvia 2
Source:
Aircraft Profile No 257 , Armand van Ishoven
Die Flugzeuge der Österreichischen Luftstreikräfte, Haubner
Flugzeug 2/91
U-12 D-1189 towing equipment
Type Two seat trainer
Engine 1 Sh 11 with propeller Ø 2.36 m 1 Sh 5 1 Sh 12
Dimensions  Length 7.47 m, height 2.80, span 9.96 m, wingarea 23.97 m2, ailerons 2.48 m2,
tailplane 1.80 m2, elevator 1.50 m2, fin 0.70 m2, rudder 1.00 m2, main track 1.60 m, mainplane dihedral 3°,
mainplane sweepback 3º
Weights Empty 525 kg, flying weight 800 kg, fuel capacity 96 l, wingload 33,5 kg/m2 Empty 500 kg, flying weight 775 kg, fuel capacity 96 l Empty 550 kg, flying weight 800 kg, fuel capacity 96 l
Performance Max speed 140 km/h, cruising speed 115 km/h, landing speed 75 km/h, climb rate 102 m/min, to 1000 m 7 min. 15 sec., to 3000 m 9 min service ceiling 3350 m Max speed 134 km/h, cruising speed 110 km/h, landing speed 75 km/h, service ceiling 3000 m, range 450 km Max speed 145 km/h, cruising speed 115 km/h, landing speed 75 km/h,  to 1000 m 5 min. 57 sec., service ceiling 3800 m, range 450 km


 

Udet U-12a