CASA C-212 Aviocar
Notes: This is a
Spanish transport for both military and civilian uses, in use by a large amount
of countries all over the world.
The basic version is the C-212, and they get progressively bigger and more
capable. First flight was in March 1971, and the Aviocar was designed initially
to replace the outmoded Junkers Ju-52s and Douglas C-47s the Spanish Air Force
was using in the late 1960s. The Aviocar entered Spanish Air Force service in
1974, and first civilian examples were delivered in 1975. Construction began in
Spain by CASA, but in 1975 IPTN in Indonesia negotiated a license to produce the
Aviocar, and by 2006, IPTN became the only source of parts and new Aviocars.
(Indonesian C-212s are designated NC-212.) The C-212-200 is in use by US SOCOM
as the C-41A; the C-41A was also in use in Iraq and Afghanistan by PMC
Blackwater. The C-212 is popular with skydivers and smoke jumpers due to its
rear ramp which can be opened in flight. The C-212 is currently used by some 35
military operators.
The C-212 is a
turboprop-powered STOL cargo aircraft which also has civilian airline versions.
It is characterized by its boxy fuselage with a high-mounted wing and tall tail.
The rear fuselage has side doors for paratroopers and a rear ramp, a rarity in
such a small cargo aircraft; there is also a door for crew entry on the front
left side. The fuselage is not pressurized, limiting its service ceiling. The
Aviocar has been designed for austere environments without a lot of ground
support or hardened runways. The engines are self-starting with a small onboard
APU. The wings are narrow but wide, and are fitted with high-lift devices such
as double slotted flaps and leading-edge slats.
The base model is the
C-212A (also known as the C-212-100); this model has a pair of Honeywell
TPE331-5-251C turboprop engines developing 840 horsepower each. The C-212-200 is
stretched and is powered by a pair of TPE331-10R-511C turboprop engines
developing 900 horsepower each. The C-212-300 has further upgraded
TPE331-10R-513C engines, also with an output of 900 horsepower each. The
vertical stabilizer was also slightly enlarged, and winglets were added to the
tips of the wings. The nose is stretched and more aerodynamic, and houses a
cargo compartment. Avionics have been upgraded, including the addition of an
autopilot. The C-212-400 is powered by TPE331-12JR-701C engines developing 925
horsepower each. The nose houses
upgraded avionics instead of cargo. The NC212i is an improved Indonesian
C-212-400, with uprated engines developing 970 horsepower each. The SH-89 is an
antisubmarine version of the C-212-200, with an extended nose for search radar,
sonar, ECM, and SIGINT gear. It is used primarily by the Swedish Air Force (the
base C-212-200 is designated the Tp 89 by the Swedish), but also built by the
Indonesians as the NC-212-200 MPA (Maritime Patrol Aircraft).
The C-212 may
carry a 1000-liter auxiliary fuel tank in the fuselage or a pair of 750-liter
auxiliary fuel tanks. The wings have a pair of hardpoints, but these may only be
occupied by 500-liter fuel tanks.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
C-212-100 |
$2,333,789 |
JP5 |
2.82 tons |
8 tons |
3+18 or 16 paratroopers or 8 stretchers |
15 |
None |
Enclosed |
|
C-212-200 |
$3,002,054 |
JP5 |
3.16 tons |
9 tons |
3+28 or 24 paratroopers or 14 stretchers |
15 |
None |
Enclosed |
|
C-212-300 |
$12,409,474 |
JP5 |
3.26 tons |
9.19 tons |
3+28 or 24 paratroopers or 14 stretchers |
17 |
Radar (74 km), FLIR (30 km) |
Enclosed |
|
C-212-400 |
$12,409,474 |
JP5 |
3.95 tons |
11.14 tons |
3+28 or 24 paratroopers or 14 stretchers |
17 |
Radar (74 km) |
Enclosed |
|
NC212i |
$12,456,444 |
JP5 |
3.95 tons |
11.14 tons |
3+28 or 24 paratroopers or 14 stretchers |
17 |
Radar (74 km) |
Enclosed |
|
SH-89 |
$18,057,013 |
JP5 |
3 tons |
8.7 tons |
5 |
20 |
Radar (74 km), SLAR (50 km), FLIR (30
km), Sonar (2 km) |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
C-212-100 |
1216 |
338 (110) |
NA
92 4/2
40/20 |
2040 |
752 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
C-212-200 |
1152 |
320 (110) |
NA
86 4/2
40/20 |
2040 |
800 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
C-212-300 |
1128 |
313 (110) |
NA
85 4/2
40/20 |
2040 |
800 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
C-212-400 |
963 |
267 (110) |
NA
72 4/2
40/20 |
2040 |
824 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
NC212i |
1010 |
281 (110) |
NA
76 4/2
40/20 |
2040 |
866 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
SH-89 |
1189 |
330 (110) |
NA
89 4/2
40/20 |
2040 |
800 |
7500 |
FF4
CF4 RF3
W4 T3 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
C-212-100/200 |
None |
600/500m Primitive Runway |
None |
2 Hardpoints (Fuel Tanks Only) |
None |
|
C-212-300/400/NC212i |
Flare/Chaff Dispensers (30/20) |
600/500m Primitive Runway |
None |
2 Hardpoints (Fuel Tanks Only) |
None |
|
SH-89 |
ECM 2, ELINT 3, Secure Radios, Sonobuoys
(60) |
600/500m Primitive Runway |
None |
2 Hardpoints |
None |
CASA C-295
Notes: The CASA
C-295 (now Airbus C295) is an improved version of the CN-235 listed in
International Cargo Aircraft. It
was developed by CASA in the 1990s, and the launch customer was the Spanish Air
Force in 1999. Currently, Egypt is currently the largest user of the C-295, with
21 in their air force, though India currently has eight and plans to add 12 per
year for a few years. License
production is undertaken in Indonesia by IPTN and India by Tata. The C-295 has
seen combat service in Kosovo, Iraq, and Afghanistan. The C-295 has a modular
cargo bay and can be rapidly reconfigured for passengers, paratroops, medevac,
or cargo. Ground crew and equipment requirements are minimal and the C-295 is at
home in austere environments. The C-295 is in use by military forces, civilian
airlines and cargo companies, and by relief organizations.
The C-295 is a
stretched version of the CN-235 with more powerful engines. The fuselage is long
and slender and the wingspan likewise long.
The wings also have several STOL and low speed refinements such as double
slotted flaps and leading-edge slats. It can move 50% more cargo with the same
range as the CN-235, and can go a little faster and higher as well. The landing
gear has an autoreverse capability, and is able to turn 180 degrees on the
ground on a runway as narrow as 12 meters. The landing gear can take the stress
of operating from soft, grassy fields as well as hardened runways. The avionics
are advanced, including an autopilot, weather radar, and the HIAS (Highly
Integrated Avionics System). The avionics allow the aircraft to function within
civil aviation rules as well as military rules. The C-295 is powered by a pair
of Pratt & Whitney Canada PW127G turboprop engines, delivering 2645 horsepower
each. These engines are coupled to six-bladed propellers with composite
scimitar-shaped blades. The engines have a modular design easing maintenance and
upkeep. The wings have hardpoints, and have been integrated with a wide variety
of air-to-ground ordnance.
There are a
number of variants and projected variants of the C-295. The AEW&C variant is a
relatively inexpensive AWACS-type aircraft incorporating a 360-degree radar in
an external saucer dome on the roof of the fuselage, and allows functions
similar to that of the E-2 Hawkeye carrier-borne early warning aircraft. The
SIGINT (Signals Intelligence) variant conducts radio and radar surveillance and
electronic reconnaissance. The MPA variant (Maritime Patrol/Antisubmarine) is a
reconnaissance patrol and antishipping/antisubmarine aircraft with devices to
hunt and kill enemy shipping and submarines. It has been tested with several
antishipping missiles, including the Harpoon, Exocet, and Marte, as well as
bombs, rockets, torpedoes, and depth charges.
For a short time in the early 2000s, the C-295 was studied for possible
conversion to a gunship, similar to the AC-235. Indian C-295s have extra EW
equipment. The C-295 ISR variant is equipped with machineguns, antitank
missiles, and bombs and rockets on its hardpoints. The KC-295 is an aerial
refueling tanker variant; it will not be further detailed here.
|
Vehicle |
Price |
Fuel Type |
Load |
Veh Wt |
Crew |
Mnt |
Night Vision |
Radiological |
|
C-295 |
$54,106,036 |
JP5 |
9 tons |
23.2 tons |
4+71 or 48 paratroopers or 24 stretchers |
25 |
Radar (200 km) |
Enclosed |
|
C-295 (Indian) |
$61,080,036 |
JP5 |
9 tons |
23.24 tons |
4+71 or 48 paratroopers or 24 stretchers |
26 |
Radar (200 km) |
Enclosed |
|
C-295 AEW&C |
$107,051,249 |
JP5 |
1 ton |
24.5 tons |
7 |
50 |
Radar (400 km) |
Enclosed |
|
C-295 SIGINT |
$58,281,893 |
JP5 |
2 tons |
23.42 tons |
7 |
27 |
Radar (200 km) |
Enclosed |
|
C-295 MPA |
$84,826,506 |
JP5 |
6 tons |
23.4 tons |
5 |
28 |
Radar (300 km), Thermal Imaging (30 km),
MAD (1.2 km) |
Enclosed |
|
C-295 ISR |
$56,555,653 |
JP5 |
3.5 tons |
23.5 tons |
4 |
27 |
Radar (200 km), FLIR (30 km) |
Enclosed |
|
AC-295 |
$75,426,600 |
JP5 |
3 tons |
23.9 tons |
8 |
28 |
Radar (200 km), SAR (45 km), FLIR (30
km) |
Enclosed |
|
Vehicle |
Tr Mov |
Com Mov |
Mnvr/Acc Agl/Turn |
Fuel Cap |
Fuel Cons |
Ceiling |
Armor |
|
C-295 |
1315 |
365 (95) |
NA
99 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
C-295 (Indian) |
1313 |
365 (95) |
NA
99 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
C-295 AEW&C |
1247 |
346 (95) |
NA
93 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
C-295 SIGINT |
1303 |
362 (95) |
NA
98 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
C-295 MPA |
1304 |
362 (95) |
NA
98 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
C-295 ISR |
1299 |
361 (95) |
NA
97 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
AC-295 |
1278 |
355 (95) |
NA
96 4/2
40/20 |
7500 |
2366 |
9145 |
FF7
CF7 RF7
T6 W7 |
|
Vehicle |
Combat Equipment |
Minimum Landing/Takeoff
Zone |
RF |
Armament |
Ammo |
|
C-295 |
RWR, Flare/Chaff Dispensers (30/30),
All-Weather Flight, Secure Radios |
320/670m Primitive Runway |
+1 |
6 Hardpoints |
None |
|
C-295 (Indian) |
RWR, Flare/Chaff Dispensers (30/30),
All-Weather Flight, Secure Radios, ECM 1, IRCM 1 |
320/670m Primitive Runway |
+1 |
6 Hardpoints |
None |
|
C-295 AEW&C |
Advanced IFF, RWR, ECM 2, Short-Range
Radio Jamming (10 km), Track While Scan, Target ID, ELINT 3, Look-Down
Radar, Secure Radios, Auto Track, GPS, Satcom Gear, Flare/Chaff
Dispensers (30/30) |
320/670m Primitive Runway |
Nil |
None |
None |
|
C-295 SIGINT |
RWR, Flare/Chaff Dispensers (30/30),
All-Weather Flight, Secure Radios, ELINT 3, Radio/Radar Detectors, ECM 1 |
320/670m Primitive Runway |
+1 |
6 Hardpoints |
None |
|
C-295 MPA |
RWR, Flare/Chaff Dispensers (40/40),
Look-Down Radar, ECM 2, IRCM 1, EW Suite, Sonobuoys (40) |
320/670m Primitive Runway |
+3 |
6 Hardpoints |
None |
|
C-295 ISR |
RWR, Flare/Chaff Dispensers (30/30),
All-Weather Flight, Secure Radios, Laser Designator (30 km) |
320/670m Primitive Runway |
+2 |
6 Hardpoints |
None |
|
AC-295 |
RWR, Flare/Chaff Dispensers (30/30),
All-Weather Flight, Secure Radios, Laser Designator (30 km) |
320/670m Primitive Runway |
+4 |
30mm M230LF Autocannon (LS), M134D
Minigun (LS), 6 Hardpoints |
750x30mm, 2000x7.62mm |