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Max Holste
MH.1521 Broussard



Operational French Army MH.1521M Broussard at Toussus-le-Noble airfield in 1965
Role Six-seat utility monoplane
National origin France
Manufacturer Avions Max Holste
First flight 1952
Introduction 1954
Retired 1993 (French army)
Primary user French Army
Number built 396
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History Avions Max Holste
Max Holste MH.1521 Broussard

Following the end of the Second World War, Avions Max Holste designed and built a new two-seat trainer and tourer aircraft, the Max Holste MH.52, of which only small numbers were built. Holste then responded to a French Army requirement for an artillery spotter aircraft for a lightweight liaison and observation aircraft. The resulting design, the MH.152, had a fuselage based on that of the MH.52 and a high-mounted wing. It was powered by a 220 horsepower (160 kW) Salmson 8 As.04 engine and had an enclosed, fully-glazed cabin seating a pilot and four passengers. A prototype flew on 12 June 1951. While it demonstrated good short-field performance, the French Army's needs had changed, with it now requiring a robust utility aircraft similar to the de Havilland Canada DHC-2 Beaver

The Max Holste MH.1521 Broussard is a 1950s French six-seat utility monoplane designed by Max Holste to meet a French Army requirement.

Variants

Mystère IVA
MH.152
First prototype of the Broussard series, powered by a Salmson 8 As.04 inverted V-8 engine.
MH.1521
Prototypes, five built plus two pre-production aircraft and 19 pre-production military variants.
MH.1521A
Aircraft modified for agricultural use.
MH.1521C
Production for civil or non-French military customers, 36 built.
MH.1521M
Production for French military, 319 built.
MH.1522
Based on MH.1521, with full span leading-edge slats and double-slotted trailing edge flaps to improve stall performance. Prototype, modified from a pre-production aircraft, flown on 11 February 1958, but later converted back to MH.1521 standard.
MH.153
The prototype MH.152 powered by a Turbomeca Astazou turboprop engine. First flew in this form June 1957
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Avions Marcel Dassault-Breguet Aviation

Dassault Aviation Avions Max Holste
Max Holste MH.1521 Broussard

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General Info

    • Crew: 1-2
    • Capacity: 4-5 passengers
    • Length: 8.65 m (28 ft 5 in)
    • Wingspan: 13.75 m (45 ft 1 in)
    • Height: 3.67 m (12 ft 0 in)
    • Wing area: 25.2 m2 (271 sq ft)
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Powerplant

  • Empty weight: 1,650 kg (3,638 lb) equipped
  • Gross weight: 2,700 kg (5,952 lb)
  • Powerplant: 1 × Pratt & Whitney R-985-AN-1 9-cylinder air-cooled radial piston engine, 336 kW (451 hp)
  • Propellers: 2-bladed Hamilton Standard 2.D.30 constant-speed propeller
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Specifications

  • Maximum speed: 259 km/h (161 mph, 140 kn) at 1,000 m (3,300 ft)
  • Cruise speed: 228 km/h (142 mph, 123 kn)
  • Stall speed: 92.6 km/h (57.5 mph, 50.0 kn)
  • Rate of climb: 3.99 m/s (785 ft/min) at sea level
  • Take-off run: 200 m (660 ft)
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Comparable aircraft

Special Links Avions Marcel Dassault-Breguet Aviation

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The Falcon 6X is largely based on the Falcon 5X aerodynamics and systems, validated during its preliminary flight test program, but it is optimized to take advantage of its 58–62 kN (13,000–14,000 lbf) PW812D engines for a longer cabin and a greater 5,500 nmi (10,200 km) range, a Mach 0.90 top speed and a Mach 0.85 cruise. Its cabin is 12.3 m (40 ft) long, is 1.98 m (78 in) high by 2.58 m (102 in) wide (the largest in a purpose-built business jet), and can accommodate 16 passengers in three zones with 29 windows, including a galley skylight

Avions Max Holste
MH.1521 Broussard

The Falcon 6X was rolled-out on 8 December 2020.[23] The initial flight was on 10 March 2021

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The 6X received both its Federal Aviation Administration and European Union Aviation Safety Agency type certificates in August 2023.The 6X entered service on 30 November 2023

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