Difference between revisions of "Maroto Botín MB-6"

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(Created page with "{|{{Infobox aircraft begin | name = Maroto Botín MB-6 | image = OO-GER DC-6A-B Belgian Intl Air Svcs LPL 11JUL68 (5575539472).jpg | alt =...")
 
 
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{{distinguish|text=the [[Maroto B-6]]}}
 
{|{{Infobox aircraft begin
 
{|{{Infobox aircraft begin
 
  | name            = Maroto Botín MB-6
 
  | name            = Maroto Botín MB-6
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  | manufacturer    = [[Maroto Botín|Maroto Botín Aerospace Corporation]]
 
  | manufacturer    = [[Maroto Botín|Maroto Botín Aerospace Corporation]]
 
  | designer        =  
 
  | designer        =  
  | first flight    = 1952
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  | first flight    = 9 July 1952
  | introduction    = 1952
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  | introduction    = 12 December 1952
 
  | retired        =  
 
  | retired        =  
 
  | status          = In limited service
 
  | status          = In limited service
  | primary user    = [[Creeperian Airlines]]
+
  | primary user    = [[Creeperian Airlines]] (historical)
  | more users      = [[Creeperian Air Force]]
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  | more users      = [[Creeperian Air Force]] (historical)<br />[[Sequoyah National Airways]]
 
  | produced        = 1952–1962
 
  | produced        = 1952–1962
 
  | number built    = 458
 
  | number built    = 458
 
  | developed from  = [[Maroto MA-4]]
 
  | developed from  = [[Maroto MA-4]]
 
  | variants with their own articles =  
 
  | variants with their own articles =  
  | developed into  =  
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  | developed into  = [[Maroto Botín MB-7]]
 
}}
 
}}
 
|}
 
|}
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* [[Creeperian Air Force]]
 
* [[Creeperian Air Force]]
 
* [[Creeperian Airlines]]
 
* [[Creeperian Airlines]]
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{{flag|Kivu}}
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* [[Air Kivu]]
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{{flag|Lurjize}}
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* [[Lurjize Airlines]]
 +
{{flag|Sequoyah}}
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* [[Sequoyah National Airways]]
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{{flag|Uulgadzar}}
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* [[Uulgadzan Army]]
  
 
== Specifications ==
 
== Specifications ==
  
 
[[File:Douglas DC-6 3 view.svg|thumb|right|250px|The design of the Maroto Botín MB-6.]]
 
[[File:Douglas DC-6 3 view.svg|thumb|right|250px|The design of the Maroto Botín MB-6.]]
 +
[[File:Douglas DC-6A-B, Air Atlantique AN0495861.jpg|thumb|right|225px|The cockpit of the Maroto Botín MB-6.]]
  
 
{{Aircraft specs
 
{{Aircraft specs

Latest revision as of 19:18, 12 July 2023

Maroto Botín MB-6
OO-GER DC-6A-B Belgian Intl Air Svcs LPL 11JUL68 (5575539472).jpg
A Maroto Botín MB-6 in 1986.
Role
Troop transporter/passenger airliner
National origin
 Creeperopolis
Manufacturer
Maroto Botín Aerospace Corporation
First flight
9 July 1952
Introduction
12 December 1952
Status
In limited service
Primary users
Creeperian Airlines (historical)
Creeperian Air Force (historical)
Sequoyah National Airways
Produced
1952–1962
Number built
458
Developed from
Maroto MA-4
Developed into
Maroto Botín MB-7

The Maroto Botín MB-6 is a Creeperian four-engine piston aircraft built by the Maroto Botín Aerospace Corporation.

History

The Maroto MA-6 was developed by the Maroto Botín Aerospace Corporation. The aircraft was developed from the Maroto MA-4 after a request from National Imperial Airways, the national airline of Creeperopolis, after it rejected the proposed Maroto Botín MB-5 for being too short-range.

The MB-6 first flew in 1952 and entered service with both National Imperial Airways and the Creeperian Air Force that same year. The aircraft continues to be in limited service.

Operators

 Creeperopolis

 Kivu

 Lurjize

 Sequoyah

 Uulgadzar

Specifications

The design of the Maroto Botín MB-6.
The cockpit of the Maroto Botín MB-6.

General characteristics

  • Crew: 3
  • Capacity: 48–68 passengers
  • Length: 100 ft 7 in (30.66 m)
  • Wingspan: 117 ft 7 in (35.84 m)
  • Height: 28 ft 5 in (8.66 m)
  • Wing area: 1,463 sq ft (135.9 m2)
  • Empty weight: 52,567 lb (23,844 kg)
  • Max takeoff weight: 97,200 lb (44,089 kg)
  • Fuel capacity: ~4,260 US gal (3,550 imp gal; 16,100 l)
  • Powerplant: 4 × Reyes Ribelles M-MB6 9-cylinder air-cooled radial piston engine, 2,400 hp (1,800 kW) each at 2,300 rpm and 6,700 ft (2,000 m)
  • Propellers: 3-bladed

Performance

  • Cruise speed: 311 mph (501 km/h, 270 kn) 65% power at 15,000 ft (4,600 m)
  • Range: 3,983 mi (6,410 km, 3,461 nmi) maximum
  • Service ceiling: 25,000 ft (7,600 m)
  • Rate of climb: 1,070 ft/min (5.4 m/s)
  • Wing loading: 24.3 lb/sq ft (119 kg/m2)
  • Power/mass: 0.11 hp/lb (0.18 kW/kg)

See also