religare strategic advisory commentary - aircraft procurement - april 2010
TRANSCRIPT
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Development of CapabilityThe IAF has evolved from its humble beginnings in October 1931, when it consisted of
six officers, five pilots and four Westland Wapiti biplanes, into the fourth largest air
force in the world. It has done this through a gradual process of evolution,
modernization and learning from engagement in conflict.
India in 2007 is a vastly different place to the India of 1963, when the MiGs were first
commissioned by the IAF. Modern India needs an air force capable of defending its
borders against terrorists, countering the nuclear threat of potential aggressors and
helping to fulfill its growing role as a world food donor and provider of international
aid. To achieve this goal, the Indian Air Force is undergoing a frantic modernization
process as it attempts to attain world recognition.
This commentary provides a quick round-up of some of the major procurement and
design and development programs underway.
A look at the present
Aircraft procurement,
design and development
initiatives
April 2010 I A Commentary on the Fixed & Rotary Wing Procurement, Design &
Development Programs
Light Combat Aircraft TEJAS
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Program: Light Combat Aircraft (LCA) TEJAS
Proposal finalized in 1983. Initial Development cost: US$ 124 million. Present cost (till date): US$ 2.89 billion Estimated delivery: First squadron to be
delivered to the IAF by 2015
Background: The LCA project was sanctioned
to replace the ageing Mig-21 fleet of the IAF
and to develop the indigenous Defence
industry. Although approval for the
development of the LCA was given in 1983, the
actual design and development did not begin
until June 1993. An entire decade was actually
used to establish the Aerospace infrastructure
that was almost completely non-existent tillthat time. ADA was nominated as the program
manager, while Hal and DRDO were appointed
as principal partners. Phase-1 focused on
"proof of concept" and comprised the design,
development and testing of two technology
demonstrator aircraft (TD-1 and TD-2) and
fabrication of a structural test specimen
airframe. This was followed by the production
of two prototype vehicles (PV-1 and PV-2), and
creation of the necessary basic infrastructure
and test facilities for the aircraft. Phase-2consisted of the manufacturing of three more
prototype vehicles (PV-3 as the production
variant, PV-4 as the naval variant, and PV-5 as
the trainer variant) and a fatigue test specimen.
Phase 1 commenced in 1990 and HAL started
work on the technology demonstrators in mid-
1991; however, a financial crunch resulted in
full-scale funding not being authorized until
April 1993. The first technology demonstrator,
TD-1, was rolled out on 17 November 1995 and
was followed by TD-2 in 1998, but they werekept grounded for several years due to
structural concerns and trouble with the
development of the flight control system. In
the meantime, the development of the Multi-
Mode Radar was started by Hal and LRDE in
1997. LCAs maiden flight was successfully
completed by TD-1, on Jan 4, 2001. The first
supersonic flight of the TEJAS took place in
August, 03. In all 2 technology demonstrators
5 prototype vehicles (PV) and 8 pre-production
aircraft were to be built. The IAF and the Navy
had then projected a total requirement of 220
aircrafts.
Present situation: The TD-1, TD-2, PV-1, PV-2LSP-1, and LSP-2 have completed 1,341 flights
in total. The maximum speed reached has been
1.4 Mach. The manufacture of PV-5, which is
the twin seated trainer version, has been
completed. The IAF is projected to get its firs
squadron of LCA only by 2014-2015. At present
the IAF has only given a confirmed order of 40
aircrafts. The navy has given a confirmed order
of 9 aircrafts that are to be used on the
indigenous aircraft carrier being built at the
Cochin shipyard.PV-4 which was to be the Naval variant has
now become the second production variant
For the navy, 2 separate prototypes are
planned, NP-1 (2 seater) and NP-2 (single
seater). The LS-3 LCA is slated for its first test
flight at the end of April, it will be fitted with an
Elta MMR radar.
The LCA has a maximum take-off weight of
13,500kg. Its internal fuel capacity is 3000 liters
that give it a maximum range of 3000 km. Its
maximum speed is 1.8 Mach and its serviceceiling is 54,000 feet.
The LCA is armed with 1 cannon carrying 220
rounds and 8 hard-points. The exact
combination of missiles is yet to be decided.
The phase wise cost break-up in the
development of the LCA till date is:
Full Scale Engineering DevelopmentPhase-1, which was completed in
March, 2004 US$ 486 million
Full Scale Engineering DevelopmentPhase-2, which is projected for
completion in December, 2012
US$ 550 million
Continuation of Full ScaleEngineering Development til
December, 2018 US$ 1.178 billion
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Development of the naval versionof the LCA US$ 210 million.
In the 3rd week of April 2010, LCA-LSP-3 made
the first flight. The LSP-3 is a quantum jump in
terms of the equipment fit on the aircraft. It is
almost the final configuration including the
new air-data computers, Multi Mode Radar,(MMR) new communication and navigation
equipment and radar-warning receiver.
In its path towards Initial Operational Capability
(IOC), a pair of LCA Tejas fighters -- Prototype
Vehicle-3 (PV3) and Limited Series Production-2
(LSP-2) -- were deployed to Jamnagar for a
period of five weeks for testing by the South
Western Air Command (SWAC). The trials
entailed flight envelope expansion in various
stores configurations, as well as air-to-ground
weapon delivery trials in different modes ofweapon delivery.
A Tejas Mark-2 is currently under development
due to the inability of the Mark-1 to meet the
IAFs requirements and the Navys
requirements for operations from an aircraft
carrier. The IAF is still considering an order of
up to 125 aircraft when a re-designed Mark 2 is
developed. The Mark 2 will have a more
powerful engine, be heavier by 200kgs, have
refined aerodynamics and other vital, yet
undecided parts to be replaced to reduceobsolescence. The Indian Navys Mark 2 version
of the Tejas will be capable of much shorter
take off and landing distance from an aircraft
carrier. A new engine in collaboration with
Snecma is also under development for the
Mark-2 LCA.
Program: FGFA (Fifth Generation Fighter
Aircraft)
First designed by SUKHOI DESIGNBUREAU in 2000
Development cost: Estimated atapproximately US$ 8-10 billion.
Unit price: US$ 100 million
Estimated Delivery: 2015 foRussian version (PAK-FA) and 2017
for Indian version (FGFA).
Detail: Although an Inter-Governmenta
agreement was signed between Russia and
India in 2007, it took more than 24 monthsafter that to freeze the design and other
contractual parameters. Eventually, the
commercial agreement was only verbally
mentioned during Vladimir Putins visit to India
in 2010. The designated parties were ROSS-
TECHNOLOGY and HAL. According to the
proposed agreement a total of 500 aircraft wil
be manufactured. Whereas Russia will take the
delivery of 200 Single seater and 50 Twin seater
aircrafts, India will take the delivery of 200
Twin seater and 50 Single seater aircraft.Sukhoi Design bureau has already designed 3
prototypes and the first test flight took place
on January 29, 2010. The flight trials are to be
completed by 2012.
The aircraft is of the 30 tone category. It will be
powered by the Saturn AL-41F, which provides
17.5 tons of thrust with after-burner. This
enables the aircraft to have a SUPER-CRUISE at
1.5 Mach. The FGFA will be the first non-
american aircraft that will truly belong to the
5th generation and also to have Super CruiseThe Radar Cross section of the FGFA is only
0.5sqm, whereas for the Su30MKI, it is 20sqm
The FGFA will be armed with Indian missiles
such as the ASTRA. The final load is yet to be
determined. The FGFA is supposed to have a
maximum range in excess of 5000km with in
flight refueling.
HAL will contribute 25% towards the design
and development of the FGFA. The fuselage wil
be 25% Titanium and 20% composites. India
will contribute its expertise in aircraftcomposites, developed while designing the
LCA. Hals work share will also include the
Mission computer, navigation systems, cockpit
displays, counter measure dispensing systems
and other critical softwares.
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Program: BASIC TRAINER AIRCRAFT
Development / Commercial of the Shelf
Purchase (COTS) purchase
HTT-40 designed by HAL RFI floated in October 2009.
RFP floated for 75 units in Jan 2010.
Background: The HAL built Hindustan Piston
Trainer-32 (HPT-32) has been in use since 1984.
The HPT-32 has experienced 90 incidents of the
engine switching off in mid-air, leading to 19
deaths and the loss of 17 aircrafts. On July 31 st
2009, in one such incident, 2 senior instructors
had a fatal crash. A court of enquiry, found that
the engine had run dry and as a consequence
the entire fleet of HPT-32s was grounded. The
main reason behind the HPT-32s enginesuddenly going dry is the fact that the aircraft
looses fuel supply if it does an inverted dive
that is greater than 2G in magnitude. The IAF
has now issued a RFP for Ballistic Parachutes,
so that the HPT-32 will harmlessly float back to
the ground in the event of an engine failure.
However at present, due to the grounding of
the fleet, it has lead to a situation where the
IAF is left without a basic trainer.
Present Situation: In January 2009, HAL
offered to the IAF the Hindustan Turbo Trainer-40 (HTT-40). It said that it could deliver the
basic trainer within 6 years. However the IAF
was not quite sure and also it could not afford
to wait for a basic trainer for 6 years.
The IAF issued a RFP in January 2010 for 75
basic trainer aircrafts. Companies in contention
and their respective models are:
o Raytheon- T-6 Texano Finmeccanica- M-311o Pilatus- PC-7 or PC-9o Grob- G-120TPo Korea Aerospace- KT-1o Embraer- Tucanoo EADS PZL (PZL-130-TC-11 orik)
A pre-bidders conference was also held on
February 2nd, 2010. The RFP states that the
manufacturer will have to deliver the first 12
aircraft within 24 months of the contract. The
chosen trainer will remain in the IAF inventory
for at least 30 years and the aircraft should
have been recently certified. The responses to
the RFP were submitted on March 17th 2010.
Program: INTERMEDIATE JET TRAINER (IJT)
HJT-36, SITARA
Development started in 1999 by HAL. Initial Budget: US$ 40 million Initial Delivery: 2006
Background: At present the IAF uses the
Hindustan Jet Trainer (HJT-16) KIRAN for the
stage-2 training. Induction of the Kiran fleet
began in 1968. The aircraft have already
clocked 6000 hours and are almost nearing the
end of their life. There have also been 13 fata
crashes over the last 10 years. The IAF had
ordered 250 aircraft and its fleet strength has
had a steady decline at the rate of 2 to 3
aircraft every year.
Present Situation: The speed of development
of the HJT-36 was very impressive in the initia
stages; from metal cutting to the first flight it
took a span of only 20 months. However afte
that there were several delays due to the
Russian NPO-SATURN AL-551 engine. After
receiving the engine from Russia, it was fitted
on the first prototype PT1 and sent back to
Russia for flight trials and certifications. This
process was delayed in Russia and also the
integration of the engine with other aircraft
systems took longer than anticipated. So theprototypes were now powered by the French
SNECMA LARZAC 04H20.
The first flight with the NPO SATURN Al-551
took place on May 09, 2010 in Bangalore. The
flight lasted 30 min and consisted of only basic
maneuvers. The Initial Operational Clearance is
slated for June 2010 and HAL already has a
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confirmed order of 12 limited series aircrafts.
The total order is expected to be in the region
of 225 aircrafts.
Program: ADVANCE JET TRAINER (AJT) RFI issued in April 2009 for 57 aircrafts.
Background: After negotiating for over two
decades, India in 2004, signed a US$ 1.6 billion
contract for 66 HAWK AJTs with BAE. The IAF
received 24 aircraft in fly-away condition; the
remaining 42 were to be assembled by HAL. Till
the end of 2009, HAL had managed to deliver
only 5 aircrafts as against the stipulated 25. The
contract signed with BAE had an option for 40more aircrafts, however the IAF is not satisfied
with the service level being offered by BAE and
hence it is not exercising this option.
Present Situation: The IAF does not want to be
in a position where it does not have a sufficient
number of AJTs. In April 2009, a RFI was issued
to 6 companies for 57 aircrafts.
The contenders are:
o Alenia- M-346o Korean Aerospace- T-50o Aero Vodochody- L-159o Yak-130o MiG-ATo BAE- Hawk-136
HAL is also pushing its twin engine HJT-39
Combat Aircraft Trainer (CAT), as is DRDO and
ADA with a trainer based on the LCA-TEJAS. The
LCA-TEJAS derivative is very similar to South
Koreas T-50 Golden Eagle.
Program: LIGHT COMBAT HELICOPTER (LCH)
HAL given sanction in October 2006. Initial Budget: US$ 24 million for
building 2 prototypes.
Initial delivery: 2010
Detail: The LCH was first unveiled in 2003. It
was expected to be operational within a period
of 4 years. However the operational clearance
was received from the MoD only in Octobe
2006. HAL was to provide two prototypes by
late 2008 and the Initial Operational Clearance
was expected by November 2010.
The LCH design was frozen in March 2008 and
the first prototype TD-1 was to take flight
within 1 year, followed by TD-2 which would be
fitted with all the weapons and electronic
sensors. By the end of 2009, the IAF was slated
to conduct flight tests on TD-3.
TD-1 finally took flight on March 29, 2010 at
HALs helicopter complex in Bangalore. The LCH
flew for 20min and provided a low speed, low
altitude check of all systems onboard. The
Initial Operational clearance is now slated for
December 2011. HAL at present is trying to
reduce the LCHs weight progressively over the
first three prototypes. A total of 375 kg wouldbe reduced over the 3 technology
demonstrators. However it means that the LCH
could enter production 200 kg heavier than
planned. HAL claims that the IAF has accepted
this extra weight.
The LCH is a 5.5 tone gunship with a narrow
fuselage accommodating a pilot and a
gunner/co-pilot in tandem configuration. It has
a full glass cockpit; helmet mounted targeting
systems and full day and night operationa
capabilities. The twin-engine helicopter ispowered by SHAKTI engines that develop
1200hp each- giving it a maximum air speed of
275km/h. SHAKTI was jointly developed by HAL
and TURBOMECCA of France.
The armament suite comprises a combination
of free flight 60/68mm rockets, MISTRAL AAM
a nose mounted NEXTER 20mm canon and
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other missiles. It will be fitted with the SAAB
aviatronics ECM suite.
To support operations at high altitudes, the
LCH is designed to take off fully loaded at an
altitude of 10,000feet and operate its weapons
up to 16,300feet.
Program: MEDIUM RANGE MARITIME
RECONNAISSANCE AIRCRAFT (MRMR)
6 units for the Navy 6 units for the Coast Guard RFI issued in Jan 2009. Coast Guard expected to conduct trials in
May-June 2010. Estimated price for 6 units for Coast Guard:
US$ 1 billion.
Details: The Indian Navy and Coast Guard
issued a RFI for 6 MRMR aircrafts in January
2009. The expected ranges for the MRMR
aircraft was about 500Nautical miles with an
endurance of 6 hours.
The Indian Navy wanted its MRMR aircrafts to
be fitted with an Airborne Early Warningsystem and these aircraft would replace the
Britten-Norman Islander and the Dornier 228.
The possible contenders for the Navys MRMR
aircraft are:
Modified P8i from Boeing Falcon 9000 from Dassault,
modified by IAI ELTA.
P-99MPA from Embraer ATR-72ASW from EADS and Alenia CN-235MP from EADS-CASA.
The Coast Guard will be conducting trials
shortly. The contenders are the Russian Bereiv
Be-200 and the American Bombardier Q400.
The procurment of these survaillance aircraft
has been fast tracked after the Mumba
attacks.
Program: MEDIUM COMBAT AIRCRAFT (MCA)
First announced in 2006 as a follow upto the LCA.
First design shown at AERO INDIA 2009 Estimated cost: US$ 1.2 billion fo
development of 5 prototypes.
Estimated delivery: 2020, Totaestimated requirement of 250 aircrafts
Details: This aircraft would be Indias first foray
in the 14-15 tonnes category; LCA is in the 10
11 tonnes category and the FGFA is in the 20
tonnes plus category. The MCA is planned as
the replacement aircraft for the Jaguar and the
MiG-27. The project is being undertaken with
the partnership of the ADA, NAL and HAL. At a
later stage, other DRDO laboratories would also
play a role.
The MCA is expected to be a twin seater, fifth
generation fighter aircraft powered by the next
generation KAVERI under co-development with
SNECMA of France, having thrust vectoring and
Super Cruise capabilities. The MCA is expected
to incorporate an indigenous Active Scan rada
and the ASTRA BVR missile. The composites fo
building the MCA is under development at the
Pune and Hyderabad DRDO laboratories, which
are pursuing maximum stealth characteristics
to enable the aircraft to have a very miniscule
radar cross section. The MCA has now been re-
named as the NEXT GENERATION FIGHTER
AIRCARFT (NGFA).
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Program: LIGHT UTILITY HELICOPTER (LUH)
Procurement- Commercial Off The Shelf
Purchase (COTS) / Design & Development
Units: 197 COTS purchase & 187 Design& Developed by HAL.
RFP for procurement issued in June2008; HAL given go-ahead in Feb 2009. Estimated cost: US$ 750 million COTS
purchase.
Offset Clause: 50%
Details: The Indian Army and Navy want to
replace their Chetak and Cheetah helicopters.
An earlier RFP issued in 2006 was retracted in
December 2007, when it was found out that
the EUROCOPTER AS550 that was sent for trials
was actually the civilian version. This previous
RFP also stated that only 60 units were to be
supplied in a fly-away condition with the
remaining 137 units to be licensed
manufactured by HAL.
The fresh RFP stated that all units are to be
supplied in a fly-away condition and the offset
has been enhanced to 50%. Out of the 197helicopters, 133 are for the Army and 64 for
the Navy. The RFP has been issued to:
o Augusta Westlando Bell Helicopterso Eurocoptero Kamovo Sikorsky
BELL has opted out of the competition as it has
stated its inability to comply with the 50%offset clause in the RFP. The trials for the LUH
were slated for August 2009; however the
schedule was yet to be finalized.
HAL has got approval for the design and
development of an indigenous LUH in February
2009. The approval finally came for building
187 units and it was decided that either the
Russians or Eurocopter would partner HAL in
this project. The helicopters would supplement
the 197 helicopters being bought off the shelf
However in March 2010, HAL decided to not
seek any foreign collaboration. The Indigenous
LUH is expected to be of the 3tonnes categoryand have a range of 500 km. It would be
powered by a single HAL/Turbomeca SHAKT
engine and be able to carry a payload of 500
kg. The first flight is scheduled for 2015.
Program: ADVANCED ATTACK HELICOPTER
(AAH)
Units: 22 RFP Issued in MAY 2008/May 2009. Estimated cost: US$ 550 million.
Details: Only 3 companies submitted their bids
by the August 2008 deadline. These were
Eurocopter, AugustaWestland and Kamov.
Boeing had requested for an eight week
extension to submit its bid, which was denied
by the MoD. Bell withdrew from the
participation, because its model on offer was
no longer in production and was available only
through the FMS route.
Eventually the government retracted the RFP
on March 24th, 2009 as none of the 3 bids
conformed with the Staff Qualitative
requirements. The IAF was of the opinion thatthey had not received offers from all the best
available options.
The IAF wants the twin-engine helicopters to
have a turret gun of 20mm or higher caliber
and be able to fire 70mm rockets at a range of
1.2 kilometers. Also required is the ability to
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employ air-to-ground, fire-and-forget missiles
with a range of at least seven km, fitted with
state-of-the-art electronic warfare protection
suite and carry a radar warning receiver
capable of intercepting, identifying and
prioritizing multiple airborne and ground-based
radio frequency emitters. Other requirementsinclude all-weather, all-terrain, and day-and-
night operations capabilities.
A fresh RFP was released in May 2009. The RFP
was issued to:
o AugustaWestland- AW129o Bell- AH-1Z Super Cobrao
Boeing- Apache AH64D Block III
o Eurocopter- Tiger HADo Kamov- Ka-50o Mil- Mi-28NEo HAL- Light Combat Helicopter
Submissions were made by October 2009 and
the first deliveries are expected only by end
2012. The schedule for trials is yet to bedetermined.
Program: HEAVY LIFT HELICOPTER
Units: 15 RFP issued in MAY 2008/ May 2009 Contenders:
o Boeing- CH47F Chinooko Sikorsky- CH-53Ko AugustaWestland- AW101o Mil- Mi-46
Details: The original RFP was divided into 3
parts. 6 helicopters were required to replace
the existing fleet of Mi-26 helicopters. Anothe
16 heavy utility helicopters were to be supplied
for high-altitude aerial logistics and four of the
same model will be configured for high-altitude
combat search-and-rescue. This RFP waswithdrawn in March 2009 and a fresh one fo
15 units was issued in May 2009 when UPA-2
came into power. The responses to the RFP
were submitted in October 2009. The offset
proposals were submitted by January 2010
and further details are awaited.
Program: ANTI SUBMARINE WARFARE
HELICOPTER (ASW)
Units: 16 Estimated price: US$ 600 million RFP issued in late 2005
Details: The Indian Navy wanted to purchase
16 ASW helicopters as replacements for its
losses to its AugustaWestland Seaking fleet.
The Navys requirements included a physica
weight of not more than 10-12 tons; ASW and
search-and-rescue capabilities; a winch
endurance of up to four hours; and an ability to
host state-of-the-art electronic warfare
systems. Responses were received from
Eurocopter- EC725, NH Industries- NH90
Sikorsky- S-70B and Lockheed Martin- MH-60R
After receiving the responses, the NAVY was to
hold trials in late 2006, but no schedule wasdetermined. In April 2007, it seemed that now
the Navy had a change of plans and a fresh RFP
was on its way. More details are awaited.
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Program: MEDIUM LIFT HELICOPTER (MLH)
Total Demand: 350 units
Category: 10-12 tonnes
Design and developed by HAL
Details: HAL has been trying to develop a MLH
since 2004; however it is still stuck in the
design stage. The Navy, Army and Air force
have now requested the MoD to procure the
helicopters from overseas. HAL did try to tie up
with Eurocopter and Mil to help in the design
and development, but had to retract the RFP in
July 2009 as the design parameters were
changed. The production would have extended
for a period of 10-15 years.
Program: MEDIUM RANGE TANKER
TRANSPORT (MRTT)
Units: 6 Estimated cost: US$ 2 billion RFI issued in January 2010. Likely contenders:
o IL-78MKIo EADS- Airbus A330o Boeing- KC-767
Details: The IAF operates a fleet of 6 IL-78MKI
tanker aircrafts. It had wanted 6 more aircrafts
and during a previous competitive bidding the
IL-78 had once again emerged as the most
competitive bidder in June 2009. However the
IAF wanted to purchase the EADS offering
based on the Airbus A330 platform. The
Cabinet Committee on Security over-ruled the
IAF in September 2009and scrapped the entire
bid, terming the EADS offering as too
expensive.
A fresh RFI has now been issued in January
2010. Further details are awaited.
Program: AMPHIBIOUS AIRCRAFT
Units: 6 RFI issued in March 2010.
Details: To keep an eye on uninhabited islands
and carrying out search and rescue missions
over the country's maritime zone, the IAF is
planning to induct 6 amphibious aircrafts in to
its fleet.
The aircrafts are planned to be used for inter
island communication and rapid response
duties during emergencies such as a tsunami or
reaching out to people stranded on islands or
ships in the sea.
The IAF wants an aircraft which should have a
short take-off capability with a range of at least
800 nautical miles so that they can cover a long
range, they added.
Canadian Bombardier and Russian Beriev are
expected to receive the Request for Proposa
(RFP), which is expected to be issued by the IAF
soon.
Program: HEAVY LIFT AIRCRAFT
Unit: 10 Possible contender: Boeing C-17
GLOBEMASTER
Estimated cost: US$ 2.5 billion
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Details: The IAF wants to replace and augment
its fleet of Russian-made AN-32 and IL-76 air
lifters. The C-17 with a payload of around 75-80
tonnes can lift around 200 fully geared troops,
and can be used for carrying armored vehicles,
artillery guns and medium-sized helicopters
from one place to another. It can take-off froma 3000ft runway and its operating range is 2450
nautical miles. The sale will take place through
the FMS route.
P8I- Concluded C-130J- Concluded Mi17 V- Concluded
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