PZL M-24 Dromader Super
# PZL M-24 Dromader Super

The PZL M-24 Dromader Super (a.k.a. Super Dromedary) is a single engine agricultural aircraft, developed in the 1980s by the WSK-Mielec (later PZL-Mielec) from the PZL-Mielec M-18 Dromader. It did not progress beyond the prototyping stage.

## Development

The plane was developed as a bigger and more capable variant of the successful agricultural plane PZL-Mielec M-18 Dromader. Some components of the M-18 were used it its construction, but it is generally bigger and stronger, with a more powerful engine. The wings were fitted with a new central section of a larger span.

The first prototype of the M-24 flew on July 20, 1987, and was powered with a 736 kW (987 hp) Shvetsov ASh-62IR radial engine. The second prototype, designated M-24B, was powered by the Polish-designed 890 kW (1,200 hp) PZL-Kalisz K-9AA radial engine and first flew in 1988. The third prototype, M-24T, was powered by the Pratt & Whitney PT6A-45AG turboprop engine. Four prototypes were built, but the type did not enter production.

The experience with the M-24 was utilised in creating the M-18B variant of the M-18, powered with the PZL K-9 engine, first flown in 1993.

## Design

The aircraft is a metal low-wing cantilever monoplane, conventional in layout. It has a monocoque fuselage, covered with duralumin. The wings are composed of three parts, fitted with flaps and slats. There is a two-seat cabin (pilot and optional passenger or mechanic, in tandem), placed high. The single radial engine has a four blade propeller. Behind the engine is an internal 2,700-litre (590 imp gal; 710 US gal) tank for chemicals or water. A fuel tank holds 1,400 litres (310 imp gal; 370 US gal).

The plane has exchangeable sets of equipment for spraying, cropdusting or fire extinguishing. It has conventional fixed landing gear with a tail wheel.

## Specifications (M-24B)

Data from Jane's all the World's Aircraft 1989–90

General characteristics

* Crew: 1, pilot
* Capacity: 1 passenger and 2,700 L (710 US gal; 590 imp gal) / 2,000 kg (4,400 lb) of chemicals
* Length: 10.8 m (35 ft 5 in)
* Wingspan: 19.9 m (65 ft 3 in)
* Height: 4.3 m (14 ft 1 in) in rigging position

             3.78 m (12.4 ft) tail down
* Wing area: 45 $m^2$ (480 sq ft)
* Aspect ratio: 8.8
* Empty weight: 2,870 kg (6,327 lb)
* Max takeoff weight: 5,000 kg (11,023 lb) and Max landing weight

             5,500 kg (12,100 lb) (restricted)
* Powerplant: 1 × PZL ASz-62IR 9-cylinder air-cooled radial piston engine, 750 kW (1,000 hp)
* Propellers: 4-bladed PZL constant-speed propeller

Performance

* Cruise speed: 220 km/h (140 mph, 120 kn)
* Stall speed: 110 km/h (68 mph, 59 kn) flaps down
* Service ceiling: 4,000 m (13,000 ft)
* g limits: +3.5 -1.4
* Rate of climb: 5 m/s (980 ft/min) clean

             3 m/s (590 ft/min) with agricultural equipment
* Wing loading: 111.1 $kg/m^2$ (22.8 lb/sq ft) (normal)

             122.2 $kg/m^2$ (25.0 lb/sq ft) (restricted)
* Power/mass: 0.149 kW/kg (0.091 hp/lb) (normal)

             0.1355 kW/kg (0.0824 hp/lb) (restricted)
* Take-off to 50 m (160 ft): 340 m (1,120 ft)
* Landing from 50 m (160 ft): 470 m (1,540 ft)
