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Bücker Bü 131 Jungmann

1st Flight 1934

The Bücker Bü 131 Jungmann, a German basic training aircraft, was predominantly utilised by the Luftwaffe during World War II.

As Bücker Flugzeugbau’s inaugural production model, the Bü 131A also holds the distinction of being the last biplane constructed in Germany.

Featuring tandem open cockpits and fixed landing gear, its fuselage was a steel tube structure sheathed in fabric and metal, while the wings were made of wood and fabric.

The aircraft’s maiden flight was powered by an 80 hp (60 kW) Hirth HM60R engine.

In 1936, it was succeeded by the Bü 131B, equipped with a more powerful 105 hp (78 kW) Hirth 504A-2 engine.

Aero in Prague carried out the majority of the Luftwaffe’s wartime production.

Variants

Bü 131A

A two-seat primary trainer biplane, the initial production model.

Bü 131B

Enhanced model, equipped with the more robust Hirth HM 504A-2 piston engine.

Bü 131C

An experimental version was equipped with a 90 hp (67 kW) Cirrus Minor piston engine.

Only one was constructed.

Nippon Kokusai Ki-86A Army Type 4 Primary Trainer

The Japanese production model for the Imperial Japanese Army Air Service was powered by a Hitachi Ha47 engine.

Nippon Kokusai Ki-86B Army Type 4 Primary Trainer

A wooden airframe design can alleviate the shortage of strategic materials.

Kyushu K9W1 Momiji Navy Type 2 Trainer Model 11

The Japanese production model for the Imperial Japanese Navy was powered by the Hitachi GK4A Hatsukaze 11 engine.

Tatra T.131

Czechoslovakia engaged in pre-war licenced production at Tatra in Kopřivnice.

Aero C-4

Mass-produced at the Aero factory in occupied Czechoslovakia during the war, the aircraft retained the original Bücker Bü 131B designation and, post-war, continued to use the original Hirth engine.

Aero C-104

The Czechoslovak post-war development featured the Walter Minor 4-III engine, with a total of 260 units constructed.

CASA 1.131

The Spanish license-built versions were equipped with either a Hirth HM 504 or a 125 hp (93 kW) ENMA Tigre G-IVA engine.

BP 131

Licence-built version

SSH T-131P

The pre-production Polish variant was equipped with a 78 kW (105 hp) Walter Minor 4-III engine.

A total of four aircraft were constructed in the year 1994.

SSH T-131PA

The Polish production model, equipped with a 103 kW (138 hp) LOM M332AK engine, first took flight in 1995.

Specifications

Crew

2

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

Empty weight

380 kg (838 lb)

Gross weight

670 kg (1,477 lb)

Powerplant

1 × Hirth HM 504

4-cylinder inverted air-cooled inline piston engine,

75 kW (100 hp)

Propellers

2-bladed fixed-pitch propeller

Performance

Maximum speed

183 km/h (114 mph, 99 kn)

Cruise speed

170 km/h (110 mph, 92 kn)

Landing speed

82 km/h (51 mph; 44 kn)

Range

650 km (400 mi, 350 nmi)

Service ceiling

4,300 m (14,100 ft)

Wing loading

46.3 kg/m2 (9.5 lb/sq ft)

Power/mass

0.11957 kW/kg (0.07273 hp/lb)

Sources

Profile Publications No. 222: Bucker Bu 131 Jungmann.

CASA 1.131 Jungmann / Bücker Bü 131 Aircraft Instruction Manual.

Flugzeug Profile 027-Bucker Bu-131.

Luftwaffe Fledglings, 1935-1945, Luftwaffe Training Units & Their Aircraft-Barry Ketley & Mark Rolfe.

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