LUFTWAFFE RESOURCE CENTER > TRAINERS > PREVIOUS PAGE

The Bücker Bü 131 "Jungmann" (Young man) was a German 1930s basic training aircraft which was used by the Luftwaffe during World War II.

DESIGN & DEVELOPMENT
After serving in the Kaiserliche Marine in World War I, Carl Bücker moved to Sweden where he became managing director of Svenska Aero AB (Not to be confused with Svenska Aeroplan AB, SAAB). He later returned to Germany with Anders J Andersson, a young designer from SAAB. Bücker Flugzeugbau GmbH was founded in Berlin-Johannisthal, in 1932, with the first aircraft to see production being the Bü 131 Jungmann.

While it was Bücker Flugzeugbau's first production type, the Bü 131A was the last biplane built in Germany. It had two open cockpits in tandem and fixed landing gear. The fuselage was steel tube, covered in fabric and metal, the wings wood and fabric. It first flew on the 80 hp (60 kW) Hirth HM60R.

In 1936, it was followed by the Bü 131B, with a 105 hp Hirth 504A-2.

Most wartime production for the Luftwaffe was by Aero in Prague.

OPERATIONAL HISTORY
Sturdy and agile, the Bü 131A was first delivered to the Deutscher Luftsportverband (DLV). The Bü 131B was selected as the primary basic trainer for the German Luftwaffe, and it served with "virtually all" the Luftwaffe's primary flying schools during the war, as well as with night harassment units such as Nachtschlacht Gruppen (NSGr) 2, 11, and 12. Yugoslavia was the main prewar export customer; "as many as 400 may have found their way" there. She was joined by Bulgaria with 15 and Romania with 40.

Production licenses were granted to Switzerland (using 94, 88 built under licence to Dornier), Spain (building about 530), Hungary (which operated 315), Czechoslovakia (10, as the Tatra T 131, before war began), and Japan, the last of which built 1,037 for Army with Hatsukaze power as the Kokusai Ki-86 and 339 for the Imperial Japanese Navy Air Service (IJNAS) as the Kyushu K9W. In Spain, production continued at CASA until the early 1960s. The Jungmann was retained as the Spanish Air Force's primary basic trainer until 1968.

In the 1960s and early 70s the Spanish, Swiss and Czech governments sold their Jungmanns to private owners many being exported to the United States. About 200 Jungmanns survive to this day, many having been fitted with modern Lycoming O-320 (150 hp) or O-360 (180 hp) four cylinder engins with inverted fuel and oil systems for aerobatic flight.

Current owners and pilots prize the Jungmann for its outstanding handling characteristics when compared to other antique bi-planes and even more modern aerobatic types. Upkeep and maintenance for the Jungmann is comparable to other antique aircraft and is superior when fitted with the Lycoming engines. Airframe parts are available from several sources both in the United States and Europe.

In 1994, the Bü 131 was restored to production briefly using CASA jigs by Bücker Prado in Spain, with 21 aircraft constructed as the BP 131, while SSH Janusz Karasiewicz in Poland also started production of a version of the Jungmann based on Czech plans in 1994. After the death of Janusz Karasiewicz, the Polish company Air Res Aviation continued the production of the Bücker Jungmann. 20 were manufactured in Poland between 1994 and 2000.

VARIANTS:
Bü 131A
Two-seat primary trainer biplane. Initial production version.

Bü 131B
Improved version, powered by the more powerful Hirth HM 504A-2 piston engine.

Bü 131C
Experimental version, fitted with 67 kW (90 hp) Cirrus Minor piston engine. One built.

Nippon Kokusai Ki-86A Army Type 4 Primary Trainer
Japanese production version for the Imperial Japanese Army Air Service. Powered by a Hitachi Ha47

Nippon Kokusai Ki-86B Army Type 4 Primary Trainer
Wooden airframe version to relieve scarce supplies of strategic materials.

Kyushu K9W1 Momiji Navy Type 2 Trainer Model 11
Japanese production version for the Imperial Japanese Navy. Powered by the Hitachi GK4A Hatsukaze 11

Tatra T.131
Czechoslovakia, pre-war licence production in Tatra Kopřivnice.

Aero C-4
Mass-produced in Aero factory in occupied Czechoslovakia during wartime under original Bücker Bü 131B designation, used postwar with original Hirth engine.

Aero C-104
Czechoslovakia, postwar development with a Walter Minor 4-III engine, 260 built.

CASA 1.131
Spanish license-built versions

BP 131
modern license-built version

SSH T-131P
Pre-production modern Polish version, powered by 78 kW (105 hp) Walter Minor 4-III engine. Four built from 1994.

SSH T-131PA
Main Polish production version, with 103 kW (138 hp) LOM M332AK engine. First flew 1995.

OPERATORS:

• Bulgarian Air Force
• Czechoslovak Air Force
• Czechoslovakian National Security Guard
• Hellenic Air Force
• Imperial Japanese Army Air Service
• Imperial Japanese Navy Air Service
• Independent State of Croatia
• Luftwaffe
• Polish Air Force
• Romanian Air Force
• Royal Hungarian Air Force
• Royal Netherlands Air Force
• Royal Romanian Air Force
• SFR Yugoslav Air Force
• Slovak Air Force (1939–45)
• South African Air Force
• Spanish Air Force
• Swiss Air Force
• Yugoslav Royal Air Force

---

SPECIFICATIONS:
Type: Primary Trainer
Origin: Bücker Flugzeugbau
Deigner: Carl Bücker
Crew: Two
Models: See Variants
First Flight: April 27, 1934
Service Delivery: 1935
Final Delivery: 1945
Total Production: ~5,000

POWERPLANT:
  Model: Hirth HM 504
  Type: 4-cylinder invertead air-cooled in-line piston engine
  Number: One
  Horsepower: 100 hp
  Propellers: 2-bladed fixed-pich propeller

DIMENSIONS:
  Length: 6.62 m (21 ft 9 in)
  Wingspan: 7.4 m (24 ft 3 in)
  Height: 2.25 m (7 ft 5 in)
  Wing area: 13.5 m2 (145 sq ft)
  Airfoil: NACA 3410.5

WEIGHTS:
  Empty weight: 380 kg (838 lb)
  Gross weight: 670 kg (1,477 lb)

PERFORMANCE:
  Maximum speed: 183 km/h (114 mph)
  Cruise speed: 170 km/h (110 mph)
  Landing speed: 82 km/h (51 mph)
  Range: 650 km (400 mi)
  Service ceiling: 4,300 m (14,100 ft)
  Time to altitude:

• 1,000 m (3,281 ft) in 5 minutes 12 seconds
• 2,000 m (6,562 ft) in 12 minutes
• 3,000 m (9,843 ft) in 23 minutes
• 4,000 m (13,123 ft) in 45 minutes

  Wing loading: 46.3 kg/m2 (9.5 lb/sq ft)
  Power/mass: 0.11957 kW/kg (0.07273 hp/lb)

LUFTWAFFE RESOURCE CENTER > TRAINERS > PREVIOUS PAGE