Rahul Sharma (Editor)

CASA C 101

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Top speed
  
770 km/h

Length
  
12 m

First flight
  
June 29, 1977

Number of seats
  
2

Wingspan
  
11 m

Engine type
  
Garrett TFE731

Manufacturer
  
EADS CASA

CASA C-101 CASA C101 Aviojet Trainer and Light Attack Aircraft Military

The CASA C-101 Aviojet is a low-wing single engine jet-powered advanced trainer and light attack aircraft. It remains in service in the Spanish Air Force and some other countries; it is also flown by the Patrulla Aguila aerobatics team.

Contents

CASA C-101 CASA C101 Aviojet Images

It was designed to replace the already outdated Hispano Saeta. Spanish aircraft maker CASA began work on the C-101 in 1975. Germany's MBB and the USA's Northrop helped with the development, and the first four prototypes flew in June 1977. The design followed that of other jet trainers such as the BAE Hawk and the Alpha Jet, but was less aerodynamically sophisticated, with an unswept wing, and it had limited weapons capability.

CASA C-101 Cassa101

First look dcs casa c 101 aviojet


Design and development

CASA C-101 CASA C101 Aviojet CombatAircraftcom

The aircraft was designed in response to a Spanish Air Force requirement in 1975 for a jet trainer to replace its aging fleet of Hispano HA-200s and Ha.220s. Like many European jet trainers, it was also to have a limited attack capability. CASA sought technical assistance from Messerschmitt-Bölkow-Blohm (MBB) and Northrop, the latter designing the wings. A design along largely conventional lines was the result, the only surprising feature being a large internal weapons bay beneath the rear cockpit, allowing for a wider variety of armament to be carried than the underwing pylons alone would allow. Alternatively, this bay can be used to carry reconnaissance equipment. The aircraft is designed in a modular fashion to ease manufacturing and maintenance, and enjoys a great range since its initial requirement called for autodeployment to the Canary Islands from the Spanish mainland.

CASA C-101 FileEADS CASA C101 ILA2002jpg Wikimedia Commons

Although the first flight took place on 27 June 1977, test flights did not begin until 17 April 1978. Performance was found to be better than anticipated by the designers. An initial Spanish Air Force order for 88 machines was placed, a dedicated trainer version designated C-101EB-01 by CASA and E.25 Mirlo ("Blackbird") by the air force. The first aircraft entered service on 17 March 1980.

CASA C-101 httpsuploadwikimediaorgwikipediacommonsthu

This was followed in production by a combination attack/trainer with an uprated engine designated C-101BB-02 bought by Honduras, which bought four, and Chile, which bought four aircraft and parts for another eight to be assembled locally by ENAER. All Chilean BB-02s are designated T-36 Halcón.

CASA C-101 CASA C101 Wikipedia

In 1983, CASA flew a dedicated attack version, the C-101CC-02, which was again ordered by Chile. This time, only the prototype was built in Spain, with the remaining 22 machines built by ENAER. This variant features yet another engine upgrade and increased fuel capacity and is designated A-36 Halcón ("Falcon").

Sixteen similar aircraft, the C-101CC-04 were sold to Jordan.

CASA C-101 FileCasac101aviojetpatrullaaguilaarpjpg Wikimedia Commons

The final version of the C-101, the C-101DD was demonstrated by CASA in 1985, featuring vastly improved avionics and the capability to carry the AGM-65 Maverick air-to-ground missile, but failed to attract any orders.

In the 1990s the armament system was modernized.

Operators

 Chile
  • Chilean Air Force (35 -12 C-101BB and 23 C-101CC-)
  •  Honduras
  • Honduran Air Force (4 C-101BB) These aircraft scored several kills against drug smuggling aircraft
  •  Jordan
  • Jordanian Air Force (16 C-101CC)
  •  Spain
  • Spanish Air Force (88 C-101EB)
  • Specifications (CASA C-101EB)

    Data from {name of first source}

    General characteristics

  • Crew: Two (student and instructor)
  • Length: 12.25 m (40 ft 2 in)
  • Wingspan: 10.60 m (34 ft 9 in)
  • Height: 4.25 m (13 ft 11 in)
  • Wing area: 20.0 m² (215 ft²)
  • Empty weight: 3,800 kg (8,380 lb)
  • Loaded weight: 5,000 kg (11,000 lb)
  • Max. takeoff weight: 5,600 kg (12,300 lb)
  • Powerplant: 1 × Garrett TFE731-2-2J turbofan engine, 15.8 kN (3,550 lbf)
  • Performance

  • Maximum speed: 770 km/h (417 knots, 480 mph)
  • Range: 4000 km (2160 nm, 2485 mi)
  • Service ceiling: 12,500 m (41,000 ft)
  • Rate of climb: 1,490 m/min (4,900 ft/min)
  • Wing loading: 250 kg/m² (52 lb/ft²)
  • Thrust/weight: 1:3.2 (3.16 N/kg)
  • Maximum G: +7.5 -3.9
  • Armament

  • 1 - 30 mm DEFA cannon or 2 - 12.7 mm (.50 cal) M3 machine guns in detachable pods underneath the forward fuselage
  • Up to 2,220 kg (4,890 lb) disposable stores on 6 underwing pylons
  • 2 - Rafael Shafrir (A-36 "Toqui") air-to-air missiles
  • References

    CASA C-101 Wikipedia


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