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Bücker Bü 181 Bestmann

1st Flight 1937

The Bü 181 was a single-engine, low-wing monoplane with a fixed undercarriage, split flaps, dual controls, and two side-by-side adjustable seats.

The cabin’s fuselage featured a tubular steel frame, while the rear fuselage was encased in wood.

The wings and tail units also boasted a wooden shell structure.

The rudders, elevators, and ailerons were constructed with wooden ribs and fabric covering.

Metallic flaps were characteristic of the B models, and wooden flaps were used on the C models.

A 78 kW (105 hp) Hirth HM 500A or B four-cylinder piston engine powered the Bü 181 Bestmann.

Designed for training, leisure flying, and aerobatics, this aircraft saw extensive use by the Luftwaffe during World War II.

Variants

Bu 181V Prototype

Bü 181 B-0

Pre-production series with Hirth HM 504 A-2 engine

Bü 181 B-1

With Hirth HM 500 A engine

Bü 181 B-2

 As B-1 but no electrics

Bü 181 B-3 (Schlachtflugzeug)

The night harassment variant, created from modified B-1s and C-1s, was equipped with enhanced instrumentation, Revi gunsights, and three ETC 50 bomb racks.

Bomb loads

Either 3 x SC50 or 3 x SD50 or 3 x SD70 or 3 x AB70 droppable clusters.

Maximum bomb load

210 kilograms (463 pounds).

Bü 181 C-1

Enhanced range with a Hirth HM 500B engine.

Bü 181 C-2

As C-1 but no electrics

Bü 181 C-3 (Panzerjäger)

B-2 or C-2 subtype aircraft modified for the anti-tank role are equipped with four Panzerfaust 100 single-use anti-tank grenade launchers, mounted in pairs on each wing.

Post-war licenced construction and developments.

Zlín Z 181

Two-seat primary trainer aircraft. Czech production version of the Bu 181, built by Zlín in Czechoslovakia after the war.

Zlín Z 281

Two-seat primary trainer aircraft, powered by a Toma 4 piston engine.

Zlín Z 381

Two-seat primary trainer aircraft, powered by a 78 kW (105 hp) Walter Minor piston engine.

Czech Air Force Designation C-106.

Gomhouria Mk 1

Two-seat primary trainer aircraft, powered by a Walter Minor piston engine.

Egyptian production version of the Zlín 381, built under licence in Egypt by the Heliopolis Aircraft Works.

Gomhouria Mk 2

Two-seat primary trainer aircraft, powered by a 145 hp (108 kW) Continental C-145 piston engine.

Gomhouria Mk 3

As Mk. 2, but with improved undercarriage.

Gomhouria Mk 4

Increased fuel capacity.

Gomhouria Mk 5

Similar to Mk 1, powered by Walter Minor, but with different engine mounting.

Gomhouria Mk 6

Continental O-300 engine.

Sk 25

Swedish Air Force designation of the licence-built Bestmann.

Specifications

Crew

2

Length

7.85 m (25 ft 9 in)

Wingspan

10.6 m (34 ft 9 in)

Height

2.05 m (6 ft 9 in)

Wing area

13.5 m2 (145 sq ft)

Airfoil

Root

NACA 23017

Tip

NACA 4412

Empty weight

480 kg (1,058 lb)

Max take-off weight

750 kg (1,653 lb)

Powerplant

1 × Hirth HM 500A or 500B 4-cyl,

Inverted air-cooled inline piston engine, 78 kW (105 hp)

Propellers

2-bladed fixed-pitch propeller

Performance

Maximum speed

215 km/h (134 mph, 116 kn) at sea level

Cruise speed

195 km/h (121 mph, 105 kn)

Never exceed speed

440 km/h (270 mph, 240 kn)

Range

800 km (500 mi, 430 nmi)

Service ceiling

5,000 m (16,000 ft).

Sources

Flugzeug Profiles No.30-Bücker Bu 181 “Bestmann”.

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

 

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