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Bücker Bü 131 Jungmann



Type: Advanced aerobatic trainer
Origin: Bucker Flugzeugbau GmbH
Models: B & C
First Flight (Prototype): 1935
First Delivery (Luftsportverband): 1936
First Delivery (Luftwaffe): 1936


Engine:
(B) Hirth HM 506 inverted in-line six
(C) Siemens Sh 14A-4 seven-cylinder radial
Horsepower: (B) 160 hp; (C) 160 hp
Propeller Unit: N/A
Diameter: N/A


Dimensions:
Wing span: 6.60m (21 ft. 7.75 in.)
Wing Surface Area: N/A
Length: (C) 6.02m (19 ft. 9 in.)
Height: 2.20m (7 ft. 2.5 in.)
Stabilizer Span: N/A
Wheel Track: N/A

  Weights:(C Only)
Empty: 425kg (937 lbs.)
Loaded: 585kg (1,290 lbs.)

Performance:
Maximum Speed: (C) 137 mph (220 kph)
Landing Speed: 56 mph (90 kph)

Range (Fully Loaded): 500 km (311 miles)

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

Armament:
None


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