Maroto MA-4

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Maroto MA-4
Douglas DC-4 CAA NC65 (8575197199).jpg
A Maroto MA-4 in 1948.
Role
Troop transporter/passenger airliner
National origin
 Creeperopolis
Manufacturer
Maroto Aircraft Company
First flight
1945
Introduction
1945
Status
In limited service
Primary users
Creeperian Air Force (historical)
Creeperian Airlines (historical)
Produced
1945–1953
Number built
375
Developed from
Maroto MA-3
Developed into
Maroto Botín MB-5
Maroto Botín MB-6

The Maroto MA-4, sometimes called the Maroto Botín MB-4, is a Creeperian four-engine piston aircraft built by the Maroto Aircraft Company and later the Maroto Botín Aerospace Corporation.

History

The Maroto MA-4 was built by the Maroto Aircraft Company for the Catholic Imperial Restoration Council as a successor for the Maroto MA-3. The aircraft entered service in 1945. After the end of the Creeperian Civil War in 1949, the air force's MA-3s were transferred to National Imperial Airways, the country's national airline. The aircraft remains in limited service.

Operators

 Creeperopolis

 Monsilva

 Uulgadzar

Specifications

The design of the Maroto MA-4.

General characteristics

  • Crew: 4
  • Capacity: 22–86
  • Length: 93 ft 10 in (28.60 m)
  • Wingspan: 117 ft 6 in (35.81 m)
  • Height: 27 ft 6 in (8.38 m)
  • Wing area: 1,460 sq ft (136 m2)
  • Empty weight: 43,300 lb (19,641 kg)
  • Gross weight: 63,500 lb (28,803 kg)
  • Max takeoff weight: 73,000 lb (33,112 kg)
  • Fuel capacity: 2,868 US gal (2,388 imp gal; 10,860 l) normal capacity or 3,592 US gal (2,991 imp gal; 13,600 l) with alternative inner wing tanks
  • Powerplant: 4 × Reyes MA-4 14-cylinder air-cooled radial piston engines, 1,450 hp (1,080 kW) each for take-off
1,100 hp (820 kW) at 14,000 ft (4,300 m)
  • Propellers: 3-bladed, 13 ft 1 in (3.99 m) diameter

Performance

  • Maximum speed: 280 mph (450 km/h, 240 kn) at 14,000 ft (4,300 m)
  • Cruise speed: 227 mph (365 km/h, 197 kn) 60% power at 10,000 ft (3,000 m)
Maximum cruise speed 246 mph (214 kn; 396 km/h) in high blower at 20,800 ft (6,300 m)
  • Range: 3,300 mi (5,300 km, 2,900 nmi) at 10% above max L/D speed
  • Ferry range: 4,250 mi (6,840 km, 3,690 nmi) with inner wing fuel cells
  • Wing loading: 50.1 lb/sq ft (245 kg/m2) at maximum gross weight
  • Power/mass: 0.0787 hp/lb (0.1294 kW/kg) at maximum gross weight with take-off power

See also