EADS CASA C-295M

Unit cost was $28 million in 2013

Portuguese Air Force CASA C 295M 1 1
photo: airwolfhound

The Airbus / EADS CASA C-295M is a twin-engine, medium-range, multi-purpose transport aircraft that boasts short take-off and landing capability and a strong landing gear that makes it able to operate even in stern locations. It is also designed to support low-level flights for tactical missions.

Manufacturer:
Airbus
Country:
France
Manufactured:
1997 to: Present
ICAO:
C295
Price:
US$28 million (2013)

Specifications

Avionics:
Honeywell RDR-1400C weather radar
Engine:
2x Pratt & Whitney Canada PW127G
turboprop
Power:
2,644 horsepower
Max Cruise Speed:
260 knots
482 Km/h
Approach Speed (Vref):
175 knots
Travel range:
2,600 Nautical Miles
4,815 Kilometers
Fuel Economy:
Service Ceiling:
25,000 feet
Rate of Climb:
2000 feet / minute
10.16metre / second
Take Off Distance:
844 metre - 2,769.00 feet
Landing Distance:
420 metre - 1,377.94 feet
Max Take Off Weight:
23,200 Kg
51,147 lbs
Max Landing Weight:
20,700 Kg
45,635 lbs
Max Payload:
9,250 Kg
20,393 lbs
Fuel Tank Capacity:
2,020 gallon
7,647 litre
Baggage Volume:
57 m3 / 2,013 ft3
Seats - Economy / General:
71 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
1.9 metre - 6.23 feet
Cabin Width:
2.7 metre - 8.86 feet
Cabin Length:
12.7 metre - 41.67 feet
Exterior Length:
24.46 metre - 80.25 feet
Tail height:
8.66 metre - 28.41 feet
Fuselage Diameter:
3.1 metre - 10.17 feet
Wing Span / Rotor Diameter:
25.81 metre - 84.68 feet
Wing Tips:
no winglets
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Description

Production

Construcciones Aeronauticas SA (CASA)- a Spanish aircraft manufacturer that is now part of Airbus Defence produced this versatile and efficient twin-turboprop tactical military transport aircraft known as C-295M. Production took place in the Airbus Military Facility in Seville Spain. Derived from a transport aircraft CN-235, this aircraft has a stretched fuselage, and a high-wing, rear-loader design.

The aircraft made its announcement in June 1997 at the Paris Air Show and took its maiden flight after a year, in 1998. C-295 received certification for operations in 1999.

Orders and Deliveries

As of December 2018, there are 208 C-295 aircraft that have been ordered by 28 countries; 168 units have been dispatched and 166 are being used in operation.

Primary users are Spanish Air Force, Polish Air Force, Brazilian Air Force, Egyptian Air Force, Swiss Air Force, Philippine Air Force, Mexican Air force, Algerian Air Force, Finnish Air Force, UAE Navy, Royal Jordanian Air Force, Mali Air Force, and Kazakhstan Air Defense Force, Bangladesh, Canada, Colombia, Chile, Czech Republic, Ecuador, Ghana, Ivory Coast, Indonesia, Mexico, Oman, Portugal, Saudi Arabia, Spain, Uzbekistan, and Vietnam.

Cockpit

The glass cockpit of C-295M is designed with digital TopDeck Avionics Suite produced by Thales. It has four large active matrix liquid crystal displays that suit night vision goggles.

There are two to three UHF/VHF radios, a single or dual HF radio, and an audio control system inside the communication suite. The aircraft has a Cockpit Voice Recorder, Flight Data Recorder, Identification Friend or Foe, and an Emergency Locator Transponder. Two Multi-Mode Receivers, two Distance Measuring Equipment, two Automatic Direction Finders, and one Direction Finder is included in the navigation equipment.

The advanced system in avionics of C-295M is designed to suit operational requirements for both civil and military purposes.

Cabin

The main cabin with dimension of 12.7 x 2.7 x 1.9 meter has the longest cabin which can accommodate up to 71 seats; or 48 fully equipped paratroops or up to 75 troops. Two paratroop doors are attached side by side on the rear part of the cabin. It can also be arranged for medevac missions, cargo operations, and passenger transport. For easy cargo access, there is a roller loading system installed, and a wide door and cargo ramp in the upswept rear fuselage.

Engine and Performance

Powered by two Pratt & Whitney Canada PW127G turboprop engines, C295M has a maximum thrust of 2,644 hp and 2,919 hp with auto power reserve. Driven by six-bladed composite propellers type HS-568F, the engine blades have auto-feathering and propeller synchrophasing.

Maximum take-off and landing weight are 23,200 kg and 20,700 kg respectively, with a fuel tank capacity of 2,020 US Gal.

Incidents

There are several recorded incidents from 2008 to 2012 involving C-295. January 23 2008 is the Mirosławiec Air Accident where a Polish Air Force C-295 crashed during its approach that caused death of 20 people. After the incident, all Polish C-295 were grounded. On October 31 2011 the Czech Army grounded four C-295M because of an in-flight equipment failure on board one aircraft. One of the two engines stopped working upon landing, also a cockpit display and equipment failed. On November 9, 2012, while flying from Paris to Algeria, Algerian Air Force C-295 crashed in the southern part of France which killed all six people on board.