Maroto MA-4
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Maroto MA-4 | |
---|---|
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.
Contents
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
Specifications
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