The 42nd Air Assault Regiment Arma2 Realism Unit

Welcome to the hanger

Take a look around. The aircraft you see here are the main battle craft of the 42nd Air Assault Regimen. These are the only approved air vehicles we use on our custom operations. If you are in aviation or infantry and would like to see your support or air transportation this is the place to check out...Training accidents have been un-included 

AH-6 "little bird"

 

General characteristics

  • Crew: 2
  • Length: 30 ft 10 in - 32 ft 2 in (9.4 m - 9.8 m)
  • Rotor diameter: 27 ft. 4 in (8.33 m)
  • Height: 8 ft 6 in - 11 ft 2 in (2.6 m - 3.4 m)
  • Empty weight: 1,975 lbs (896 kg)
  • Max takeoff weight: 3,549 lbs (1,610 kg)
  • Powerplant: 1× One Allison T63-A-5A or T63-A-700 turboshaft, 317 hp (236 kW)

Performance

Armament

 

ah-64 apache "king of battle"

 

 

 

 

General characteristics

  • Crew: 2: pilot, CPG (co-pilot/gunner)
  • Length: 58.17 ft (17.73 m) (with both rotors turning)
  • Rotor diameter: 48 ft 0 in (14.63 m)
  • Height: 12.7 ft (3.87 m)
  • Disc area: 1,809.5 ft² (168.11 m²)
  • Empty weight: 11,387 lb (5,165 kg)
  • Loaded weight: 17,650 lb (8,000 kg)
  • Max takeoff weight: 23,000 lb (10,433 kg)
  • Powerplant:General Electric T700-GE-701 and later upgraded to T700-GE-701C (1990-present) & T700-GE-701D (AH-64D block III) turboshafts, -701: 1,690 shp, -701C: 1,890 shp, -701D: 2,000 shp (-701: 1,260 kW, -701C: 1,490 kW, -701D: 1,490 kW) each
  • Fuselage length: 49 ft 5 in (15.06 m)
  • Rotor systems: 4 blade main rotor, 4 blade tail rotor in non-orthogonal alignment[51]

Performance

Armament

c130-j "super hercules"


"

General characteristics

  • Crew: 3 (two pilots, and one loadmaster are minimum crew)
  • Capacity:
  • 92 passengers (128 for C-130J-30) or
  • 64 airborne troops (92 for C-130J-30) or
  • 6 pallets (8 pallets for C-130J-30) or
  • 74 litter patients with 2 medical personnel (97 litters for C-130J-30)
  • 2–3 HMMWVs or an M113 armored personnel carrier
  • Payload: 42,000 lb (19,090 kg) ; for C-130J-30: 44,000 lb/ 19,900 kg
  • Length: 97 ft 9 in, 29.79 m (for C-130J-30: 112 ft, 9 in, 34.69 m)
  • Wingspan: 132 ft 7 in (40.41 m)
  • Height: 38 ft 10 in (11.84 m)
  • Wing area: 1,745 ft² (162.1 m²)
  • Empty weight: 75,562 lb (34,274 kg)
  • Useful load: 72,000 lb (33,000 kg)
  • Max takeoff weight: up to 175,000 lb (79,378 kg); normal 155,000 lb (70,305 kg)
  • Powerplant:Rolls-Royce AE 2100D3 turboprop, 4,637 shp (3,458 kW)) each
  • Propellers: Dowty R391 6-blade composite propeller, 1 per engine

Performance

  • Maximum speed: 362 knots (417 mph, 671 km/h)
  • Cruise speed: 348 kn (400 mph, 643 km/h)
  • Range: 2,835 nmi (3,262 mi, 5,250 km)
  • Service ceiling: 28,000 ft (8,615 m) with 42,000 pounds (19,090 kilograms) payload
  • Takeoff distance: 3,127 ft (953 m) at 155,000 lb (70,300 kg) gross weight

UH-60 "Blackhawk"

General characteristics

  • Crew: 2 pilots (flight crew)
  • Capacity: 2,640 lb of cargo internally, including 14 troops or 6 stretchers, or 8,000 lb (UH-60A) or 9,000 lb (UH-60L) of cargo externally
  • Length: 64 ft 10 in (19.76 m)
  • Fuselage width: 7 ft 9 in (2.36 m)
  • Rotor diameter: 53 ft 8 in (16.36 m)
  • Height: 16 ft 10 in (5.13 m)
  • Disc area: 2,260 ft² (210 m²)
  • Empty weight: 10,624 lb (4,819 kg)
  • Loaded weight: 22,000 lb (9,980 kg)
  • Max takeoff weight: 23,500 lb (10,660 kg)
  • Powerplant:General Electric T700-GE-701C turboshaft, 1,890 hp (1,410 kW) each

Performance

Armament

  • Guns:

mv-22

General characteristics

  • Crew: Four (pilot, copilot and two flight engineers)
  • Capacity: 24 troops (seated), 32 troops (floor loaded) or up to 15,000 lb (6,800 kg) of cargo (dual hook)
  • Length: 57 ft 4 in (17.5 m)
  • Rotor diameter: 38 ft 0 in (11.6 m)
  • Wingspan: 45 ft 10 in (14 m)
  • Width with rotors: 84 ft 7 in (25.8 m)
  • Height: 22 ft 1 in/6.73 m; overall with nacelles vertical (17 ft 11 in/5.5 m; at top of tailfins)
  • Disc area: 2,268 ft² (212 m²)
  • Wing area: 301.4 ft² (28 m²)
  • Empty weight: 33,140 lb (15,032 kg)
  • Loaded weight: 47,500 lb (21,500 kg)
  • Max takeoff weight: 60,500 lb (27,400 kg)
  • Powerplant:Rolls-Royce Allison T406/AE 1107C-Liberty turboshafts, 6,150 hp (4,590 kW) each

Performance

 

av8-b

General characteristics

Performance

Armament

f-35

General characteristics

Performance

Armament