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BÜCKER Bu 131 JUNGMANN



Type: Primary Trainer; later, night ground attack
Origin: Bucker Flugzeugbau GmbH
Models: A, B and export versions
First Flight (Prototype): April 27, 1934
First Delivery (Luftsportverband): Late 1934
First Delivery (Luftwaffe): 1935


Engine:
(A) Hirth HM 60R inverted in-line four
(B) Hirth HM 504A-2 inverted in-line four
Horsepower: (A) 80 hp; (B) 105 hp
Propeller Unit: N/A
Diameter: N/A


Dimensions:
Wing span: 7.40m (24 ft. 3½ in.)
Wing Surface Area: N/A
Length: (B) 6.62m (21 ft. 8½ in.)
Height: 2.25m (7 ft. 4½ in.)
Stabilizer Span: N/A
Wheel Track: N/A
  Weights:
Empty: 390kg (860 lbs.)
Loaded: 680kg (1,499 lbs.)

Performance:
Maximum Speed: (B) 114 mph (183 kph)
Landing Speed: 51 mph (82 kph)

Range (Fully Loaded): 650 km (404 miles)

Initial Climb: N/A
Endurance: N/A
Service Ceiling: N/A

Armament:
None


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