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USA provides Afghanistan new helicopters

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Afghan Air Force gets five more MD 530F attack helicopters
Franz J Marty, Kabul - IHS Jane's Defence Weekly
20 June 2016

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The Afghan Air Force received five new MD-530F Cayuse Warrior helicopters on 17 June, according to the USAF. Source: DVIDS
Five additional MD 530F Cayuse Warrior light attack helicopters arrived in Kabul on 17 June to boost the Afghan Air Force's (AAF's) capability to support Afghan National Army ground operations.

The latest delivery raises the number of such airframes provided by the United States to the AAF from 13 to 18. A further nine aircraft are scheduled for delivery by the end of August 2016, which would increase the number of the AAF's MD 530Fs to a pre-arranged total of 27.

"These five latest [MD 530Fs] have the capability to fire rockets or .50 calibre machine guns, and sighting systems that are not on the previously delivered helicopters," said Lieutenant Colonel Bill Ashford, commander of the US Air Force's (USAF's) 438th Air Expeditionary Advisory Squadron.

While earlier reports indicated that previously fielded MD 530Fs were equipped not only with FN Herstal 12.7 mm (.50 cal) heavy machine gun pods but also with seven-tube M260 launchers for 70 mm (2.75 inch) rockets, Lt Col Ashford said the newly arrived MD 530Fs are the first ones fitted with rockets.

Rocket-firing capabilities are set to be added to the previously delivered 13 MD 530Fs over the course of 2016, according to a report by the US Department of Defense.

There is sometimes some confusion regarding the exact number of MD 530Fs fielded with the AAF, as some of the helicopters already delivered were returned to the United States for weapon upgrades before being re-delivered to Afghanistan.
 
Afghanistan is not particularly happy with these helos.It seems low range and service ceiling are one of the major reasons.
 
Afghanistan is not particularly happy with these helos.It seems low range and service ceiling are one of the major reasons.
Are they paying or getting free?

they need OV-10D

faster,more endurance, and more deadly.
They will need someone to fly those machines also
 
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USA is bearing its cost.But what is the use of a machine if it doesn't fit for intended role?

Afghanistan is particularly happy with Russian MI-35.
Well money makes the mare go....If they can afford, they can buy from Agustawestland too. But I think it is okay for their needs, for internal operations.
 
So USD 20 mln for 36 is not that expensive but it is not a heli...cannot hover like a helicopter.

Actually,they should provide these...

A-10_Thunderbolt_II_In-flight-2.jpg


Nothing suits better.
Why don't you sponser them...why should we waste our tax money on them.
 
So USD 20 mln for 36 is not that expensive but it is not a heli...cannot hover like a helicopter.


Why don't you sponser them...why should we waste our tax money on them.


$20 million each so $720 million, add another $200 million for weapons,spares, and training.


OV-10D doesn't need to hover when it can orbit which is just as good :D

AC130techniques.jpg
 
Afghanistan is not particularly happy with these helos.It seems low range and service ceiling are one of the major reasons.
The successful Hughes 500/MD 500 series began life in response to a U.S. Army requirement for a light observation helicopter (OH). Jst because the MD-500 series can carry a veriety of weapons, that does not make it an Attack Helicopter.

Low range, maybe. But it is a very small helicopter.
Low ceiling, not likely: the 530F is the hot and high version of the 500E, powered by an Allison 250-C30B rated at 650 shp (485 kW), certified in 1985.

The MD 530F® is engineered to meet your requirements for hot-day, high-altitude operation
http://www.mdhelicopters.com/v2/md_530f.php

MD 530F
Data from The International Directory of Civil Aircraft

General characteristics
Performance
https://en.wikipedia.org/wiki/MD_Helicopters_MD_500#MD_530F

Armament
  • four TOW anti-tank missiles, or
  • two 7.62mm General Electric M134 Miniguns plus ammunition, or
  • four General Dynamics Stinger air-to-air missile, or
  • two seven-shot rocket pods

Comparable helicopters

Specifications (SA 341) Gazelle

General characteristics



    • Crew: 2
    • Capacity: 3 Passengers
    • Length: 11.97 m (39 ft 0 in)
    • Main rotor diameter: 10.5 m (34 ft 6 in)
    • Height: 3.15 m (10 ft 3 in)
    • Main rotor area: 86.5 m2 (931 ft2)
    • Empty weight: 908 kg (2,002 lb)
    • Gross weight: 1,800 kg (3,970 lb)
Performance



    • Maximum speed: 310 km/h (193 mph)
    • Cruising speed: 264 km/h (164 mph)
    • Range: 670 km (416 miles)
    • Service ceiling: 5,000 m (16,405 ft)
    • Rate of climb: 9 m/s (1,770 ft/min)
https://en.wikipedia.org/wiki/Aérospatiale_Gazelle#Specifications_.28SA_341.29


Specifications (SA 316B) aka Alouette III, Hal Chetak


General characteristics

  • Crew: 2
  • Capacity: 5 passengers
  • Length: 10.03 m (32 ft 10¾ in)
  • Main rotor diameter: 11.02 m (36 ft 1¾ in)
  • Height: 3.00 m (9 ft 10 in)
  • Main rotor area: 95.38 m2 (1026 ft2)
  • Empty weight: 1,143 kg (2,520 lb)
  • Gross weight: 2,200 kg (4,850 lb)
  • Powerplant: 1 × Turbomeca Artouste IIIB turboshaft, 649 kW (870 shp) derated to 425 kW (570 hp)
Performance

  • Maximum speed: 210 km/h (130[61] mph)
  • Cruising speed: 185 km/h (115 mph)
  • Range: 540 km (335 miles)
  • Service ceiling: 3,200 m (10,500 ft)
  • Rate of climb: 4.3 m/s (850 ft/min)
https://en.wikipedia.org/wiki/Aérospatiale_Alouette_III#Specifications_.28SA_316B.29

Specifications (as550 c3) Fennec

Data from Jane's All The World's Aircraft 2003–2004

General characteristics

  • Crew: 2
  • Capacity: 4 passengers
  • Length: 10.93 m (35 ft 10 in) (fuselage length), 12.94 m (42 ft 6 in) (overall length, rotors turning)
  • Height: 3.34 m (10 ft 11 in)
  • Empty weight: 1,220 kg (2,690 lb)
  • Max takeoff weight: 2,250 kg (4,960 lb)
  • Fuel capacity: 540 L (143 US Gal)
  • Powerplant: 1 × Turbomeca Arriel 2B turboshaft, 632 kW (847 shp) (limited to 500 kW (671 shp for take-off)
  • Main rotor diameter: 10.69 m (35 ft 1 in)
  • Main rotor area: 89.75 m2 (966.1 sq ft)
Performance
  • Maximum speed: 246 km/h (153 mph; 133 kn) (max cruise)
  • Never exceed speed: 287 km/h (178 mph; 155 kn)
  • Range: 648 km (403 mi; 350 nmi)
  • Service ceiling: 5,280 m (17,323 ft)
  • Rate of climb: 10.30 m/s (2,028 ft/min)
Armament
https://en.wikipedia.org/wiki/Eurocopter_Fennec
 
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Specifications (EC120 B)

General characteristics
Performance
https://en.wikipedia.org/wiki/Eurocopter_EC120_Colibri#Specifications_.28EC120_B.29
 

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