C-27J Spartan Tactical military transport aircraft

C-27J Spartan Tactical military transport aircraft. First flight: 1999 © Konstantinos Panitsidis
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C-27J Spartan Military Aviation Capacity Aircraft Developed by the LMATTS Consortium (Lockheed Martin Alenia Tactical Transport Systems) based on the G222 / C-27 Spartan.

The deployment program took place in the mid-1990s, although it was based on the mechanical parts of the G222, many of which were improved to accommodate the new ROLLS-ROYCE AE 2100D2 propulsion system, as well as up-to-date electronic equipment, complete with modern cockpit analogue to the C-130J Hercules II. Its first flight took place in September 1999.

Technical description: Cockpit

The aircraft has a full glass cockpit and is equipped with five color LCDs to reduce crew workload. 

 

C-27J Spartan Cockpit © Κων/νος Πανιτσίδης
C-27J Spartan Cockpit.



The C-27J cockpit is fully compatible with AN / AVS-9 third generation night vision systems and HUD (optional).

Each pilot is provided with a Flight Management System and throw of cargo by inserting the required coordinates of the area while being provided by a flight management unit.

Electronic equipment includes dual digital automatic pilot and APN 241 low power meteorological radar capable of mapping, weather detection and Wind Shear.

Internal configuration:

For heavy cargo transportation the aircraft has reinforced flooring. The landing system can adjust the height of the spindle to facilitate unloading of the airplane. The maximum payload is 11.500 kg.



Cabin interior dimensions
C-27J Spartan
C-27J Spartan:  Length 8.58 m, Width 2.45 m, Height 2.25 m

 

On a typical mission the aircraft can carry equipment as follows:


C-27J Spartan © Konstantinos Panitsidis
2xHMMWV vehicles. 1xPanhard AML-90. 2xPanhard M3. 3xHowitzer cannons of 105 mm.

 

C-27J Spartan © Konstantinos Panitsidis

To drop the cargo the aircraft, can transport up to 3xΗCU-6/E  and 1xHCU-12/E or 7xHCU-12/E or 12xA22 CDS.

 


C-27J Spartan © Konstantinos Panitsidis

1 Bell 206 helicopter with rotors, main rotor mast and vertical tail fin in removed. Up to 3 AE2100 engines or two F-16, Mirage 2000 and C-130 Hercules engines.

 

The aircraft carries up to 46 soldiers or 36 paratroopers in missions. In freight forwarding missions it can transport 36 stretchers (injured) including 6 nurses.

It takes about 15 minutes to perform a freight forwarding mission, and within 35 minutes of its destination it can carry out a throw loads.

 

Power Plant:

 

Rolls-Royce AE 2100D2 turboprop engine © Konstantinos Panitsidis
Rolls-Royce AE 2100D2 turboprop engine

 

The Spartan is powered by two Rolls-Royce AE 2100 D2 motors with a maximum power of 3.460 kW (4.640 h.p.) each in take-off with outdoor ambient temperatures of up to 39,4o C.

 

In addition to the two engines, the aircraft also has a backup power unit that is capable of operating the engines in both air and ground. 

 

Propeller R391 type Dowty R391 Aircraft C-27 Spartan
Manufacturer: Dowty Aerospace Propellers. Country of origin: United Kingdom. Prototype manufacture date: 1999. Type: Constant speed, variable pitch. Number of blades: Έξι (6). Diameter: 4,11 m. Weight: 315 kg. 

 

Export:

2003 - Hellenic Air Force signs first contract for purchase of 12 C-27J Spartan with option to purchase 3 more aircraft.
2001/2002-Italian Air Force, 12 C-27J Spartan, 8-Bulgaria, 54 Army and 24-USAF purchase contracts, with prospective users include Australia, Saudi Arabia, Portugal, Finland, Malaysia, Taiwan .

 

Patches

354 Tactical Transportation Squadron

354 Tactical Transportation Squadron





Three-view drawing

C-27J Spartan





Technical specifications

DESIGNER
Lockheed Martin Alenia Tactical Transport Systems
COUNTRY
USA, Italy
TYPE
Tactical military transport aircraft
CREW
2
POWER-PLANT
Two Allison AE 2100D2 (3) turboprop engines
Power, h.p.
2x5.000
DIMENSIONS
 
Length, m
22,70
Height, m
10,57
Wing span, m
28,70
Wing area m2
82,00
WEIGHT  
Maximum take-off, kg 30.000
Normal take-off, kg 25.800
Empty aircraft, kg 16.103
Internal fuel, kg 9.400
Payload, kg 9.000
- soldiers 46
- paratroops 48
- passengers 30
- stretcher 24
PERFORMANCE
 
Maximum speed, km/h
580
Cruising speed, km/h
556
Maximum overload, g
-
Rate of climb, m/min
-
Service ceiling, m 8.380
Range, km
3.500
Combat range, km -
ARMAMENT Doesn't have (defensive).





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