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CASA C-295


C-295MPA Persuader


Overview


C-295M

Spanish air force C-295M tactical transport aircraft.
Source: www.c-295.ca - © copyright lies with original owner

Origin
Spain
Type
Transport aircraft
Entered service
2001
Status
In service
Development
1990's
Developer
Spain - CASA
Production
1997 - present
Producer
Spain - CASA (1997 - 1999)
Spain - EADS CASA (1999 - 2009)
Spain - Airbus Military (2009 - present)
Indonesia - Indonesian Aerospace
India - Tata Advanced Systems
Unit cost
$ 28 million
Number produced
164 by 2017, production continues
Designations
CN-295 (Indonesian production)
T.21 (Spanish service)
C-105A Amazonas (Brazilian service)
CC-295 (Canadian service)
Notable users
Egypt
Poland
Brazil
India
Portugal
Spain

Description


Introduction

The C-295 is a modern transport aircraft of Spanish origin. It was developed in the mid 1990's as a newer, larger and more capable alternative to the successful CN-235. A maritime patrol version has been developed using the same airframe.

Design

The C-295 is based on the earlier CN-235 but has a much longer fuselage. The wings are fitted on top of the fuselage and at there rear there is a large loading ramp. Two Pratt & Whitney PW127G turboprops provide propulsion and are fitted with six blade propellers. A glass cockpit is standard and flares and self-defense systems are fitted.

Firepower

The military transport variant is unarmed. In the maritime patrol version the C-295 is fitted with a wide range of sensors that include radar, optics, sonobuoys and sigint equipment. A range of lightweight torpedoes for use against submarines can be carried under the wings. Anti-ship missiles can be fitted for surface targets.

Cargo capacity

The C-295 may carry up to 9.25 t of cargo, but with maximum load the range is significantly reduced. In troop carrying configuration there are seats for up to 71 passengers. When transporting paratroopers benches are fitted alongside the fuselage for up to 48 soldiers. In the cargo configuration it may carry five large pallets, three Land Rovers or equivalent loads.

Mobility

The C-295 has STOL capability and only needs 320 m runway for landing and 670 m for take-off. The cruise speed is 480 km/h and the ferry range is 5.630 km. The maneuverability is good and 3G turns can be executed at low level.

Users

The first units were delivered to Spain in 2001 and production is expected to continue for many years to come. The C-295 is used by over a dozen air forces and is mainly found in Europe, North Africa, South America and Asia.

Variants


C-295M

Spanish air force C-295M transport aircraft with inflight refueling probe.
Source: Alexander Flühmann - © GNU Attribution - Share Alike license

C-295M
The C-295M is the standard military cargo version of the C-295. It can be configured as troop transport with seats, for paratrooper use with benches and for transport with an empty cargo area.
C-295MPA Persuader
The C-295MPA Persuader is a dedicated maritime patrol version of the C-295. The mission equipment is based on the earlier CN-235MPA and consists of radar, optics, sonobuoys and sigint equipment. The optional six hardpoints allow for a variety of anti-ship missiles, torpedoes, mines, depth charges and recce and jamming pods.
C-295W
Variant of the C-295M with improved performance. The wings feature winglets and the engines are an uprated model. Announced in 2013 and introduced in 2014 or 2015.

Details


Facts C-295M
General
Origin
Spain
Type
Transport aircraft
Crew
2 + 71 (pilot, copilot, 71 passengers)
Dimensions
Length
24.45 m
Wingspan
25.81 m wingspan
10.6 m tailplane
2.7 m fuselage
Height
8.66 m
Wing area
59 m²
Max take-off weight
23.2 t overload
21.0 t normal
Propulsion
Engine setup
Two turboprops with 6-blade propeller
Powerplant
2x Pratt & Whitney PW127G turboprop
Power output
2.645 hp each
Propellers
Hamilton Sundstrand HS-586F-5, 6 blades, 3.94 m diameter
Fuel
7.700 L
Optional in-flight refueling probe
Flight characteristics
Speed
576 km/h maximum
480 km/h cruise
Range
5.630 km empty
4.300 km with 4.5 t payload
1.330 km maximum payload
Ceiling
9.1 km
4.1 km on one engine
Take-off run
670 m minimum
840 - 930 m normal
Landing run
320 m minimum
420 m normal
Thrust-to-weight ratio
0.188 kW/kg at normal load
G limits
+2.5 G
Systems
Sensors
Honeywell RDR-1400C weather radar
Self-defense
Flares
Landing gear
Retractable tricycle, double wheels front, tandem rear
Payload
Cargo
9.25 t maximum
7.0 t normal
Five 2.24 x 2.74 m pallets
3 Land Rovers
Passengers
71 passengers
48 paratroopers
27 stretchers

Media