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Testimony: 

Before the Committee on Oversight and Government Reform, House of 
Representatives: 

United States Government Accountability Office: 
GAO: 

For Release on Delivery: 
Expected at 2:00 p.m. EDT:
Wednesday, June 24, 2009: 

V-22 Osprey Aircraft: 

Assessments Needed to Address Operational and Cost Concerns to Define 
Future Investments: 

Statement of Michael J. Sullivan, Director: 
Acquisition and Sourcing Management: 

GAO-09-692T: 

GAO Highlights: 

Highlights of GAO-09-692T, a testimony before the Committee on 
Oversight and Government Reform, House of Representatives. 

Why GAO Did This Study: 

Since the 1980s, the V-22, developed to transport combat troops, 
supplies, and equipment for the U.S. Marine Corps and to support other 
services’ operations, has experienced several fatal crashes, 
demonstrated various deficiencies, and faced virtual cancellation—much 
of which it has overcome. Although recently deployed in Iraq and 
regarded favorably, it has not performed the full range of missions 
anticipated, and how well it can do so is in question. 

Given concerns about the V-22 program, GAO recently reviewed and on May 
11, 2009, reported on MV-22 operations in Iraq; strengths and 
deficiencies in terms of the capabilities expected of the V-22; and 
past, current, and future costs. In that report, GAO recommended that 
the Secretary of Defense require (1) a new alternatives analysis of the 
V-22 and (2) that the Marine Corps develop a prioritized strategy to 
improve system suitability, reduce operational costs, and align future 
budget requests. The Department of Defense (DOD) concurred with the 
second recommendation, but not the first. GAO believes both 
recommendations remain valid. This testimony highlights GAO’s findings 
from that report. 

In speaking of the V-22, we are actually speaking of two variants of 
the same aircraft. The MV-22 is used by the Marine Corps; and the CV-22 
by the Air Force to support special operations. This statement largely 
focuses on the MV-22, but also refers to the V-22 and CV-22. 

What GAO Found: 

As of January 2009, the 12 MV-22s in Iraq successfully completed all 
missions assigned in a low-threat theater of operations—using their 
enhanced speed and range to deliver personnel and internal cargo faster 
and farther than the legacy helicopters being replaced. However, 
challenges to operational effectiveness were noted that raise questions 
about whether the MV-22 is best suited to accomplish the full 
repertoire of missions of the helicopters it is intended to replace. 
Additionally, suitability challenges, such as unreliable component 
parts and supply chain weaknesses, led to low aircraft availability 
rates. 

Additional challenges have been identified with the MV-22’s ability to 
operate in high-threat environments, carry the required number of 
combat troops and transport external cargo, operate from Navy ships, 
and conduct missions in more extreme environments throughout the world. 
While efforts are underway to address these challenges, it is uncertain 
how successful they will be as some of them arise from the inherent 
design of the V-22. 

The V-22’s original program cost estimates have changed significantly. 
From 1986 through 2007, the program’s Research, Development, Test, and 
Evaluation cost increased over 200 percent—from $4.2 to 12.7 billion—
while the cost of procurement increased 24 percent from $34.4 to $42.6 
billion. This increase coincided with significant reductions in the 
number of aircraft being procured—from nearly 1,000 to less than 500—
resulting in a 148 percent increase in cost for each V-22. Operations 
and support costs are expected to rise. An indication is the current 
cost per flying hour, which is over $11,000—more than double the target 
estimate for the MV-22. 

After more than 20 years in development, the MV-22 experience in Iraq 
demonstrated that the Osprey can complete missions assigned in low-
threat environments. Its speed and range were enhancements. However, 
challenges may limit its ability to accomplish the full repertoire of 
missions of the legacy helicopters it is replacing. If so, those tasks 
will need to be fulfilled by some other alternative. Additionally, the 
suitability challenges that lower aircraft availability and affect 
operations and support costs need to be addressed. The V-22 program has 
already received or requested over $29 billion in development and 
procurement funds. The estimated funding required to complete 
development and procure additional V-22s is almost $25 billion (then-
year dollars). In addition, the program continues to face a future of 
high operations and support cost funding needs, currently estimated at 
$75.4 billion for the life cycle of the program. Before committing to 
the full costs of completing production and supporting the V-22, the 
uses, cost, and performance of the V-22 need to be clarified and 
alternatives should be re-considered. 

View [hyperlink, http://www.gao.gov/products/GAO-09-692T] or key 
components. For more information, contact Michael J. Sullivan at 202-
512-4841 or sullivanm@gao.gov. 

[End of section] 

Mr. Chairman and Members of the Committee: 

I am very pleased to be here today to discuss the current status of the 
V-22 Osprey program. Since the V-22 Osprey began development in the mid-
1980s, it has experienced several fatal crashes, demonstrated a variety 
of deficiencies, and faced the virtual cancellation of the program--
much of which it has been able to overcome. There are two variants of 
the V-22 tilt-rotor aircraft currently being used. The MV-22 variant 
for the Marine Corps will replace the CH-46E helicopter as the Marine 
Corps' medium-lift aircraft--to be used along with the heavy-lift CH-
53[Footnote 1]--to fulfill operational requirements such as 
transporting combat troops, supplies, and equipment. The Air Force's CV-
22 variant will augment existing U.S. Special Operations Command 
aircraft. Until recently, the MV-22 was deployed in Iraq. While it 
accomplished assigned missions there, its usage did not encompass the 
full range of tasks anticipated for the aircraft. In addition, 
identified operational challenges raise questions concerning how 
effectively it can perform the full range of anticipated missions. 

My testimony today is based on our recently issued report Defense 
Acquisitions: Assessments Needed to Address V-22 Aircraft Operational 
and Cost Concerns to Define Future Investments.[Footnote 2] In view of 
our past work and others' highlighting concerns about the V-22 program, 
you asked us to determine whether the V-22 will perform as promised, 
and if it will, at what cost. To do this, we reviewed and reported on 
the system from three perspectives: 

* Its operations in Iraq, 

* Its strengths and deficiencies in terms of the capabilities expected 
of it, and: 

* Its past, current, and future costs. 

Our work on both this testimony and the report on which it is based was 
conducted from June 2008 to May 2009 in accordance with generally 
accepted government auditing standards. Those standards require that we 
plan and perform the audit to obtain sufficient, appropriate evidence 
to provide a reasonable basis for our findings and conclusions based on 
our audit objectives. We believe that the evidence obtained provides a 
reasonable basis for our findings and conclusions based on our audit 
objectives. 

Background: 

The V-22 Osprey is a tilt-rotor aircraft--one that operates as a 
helicopter for takeoffs and landings and, once airborne, converts to a 
turboprop aircraft--developed to fulfill medium-lift operations such as 
transporting combat troops, supplies, and equipment for the U.S. Navy, 
Marine Corps, and Air Force special operations. Figure 1 depicts V-22 
aircraft in various aspects of use. 

Figure 1: Views of V-22 Aircraft in Various Aspects of Use: 

[Refer to PDF for image: four photographs] 

Source: U.S. Navy, U.S. Marine Corps. 

[End of figure] 

The Osprey program was started in December 1981 to satisfy mission 
needs for the Army, Navy, and Air Force. Originally headed by the Army, 
the program was transferred to the Navy in 1982 when the Army withdrew 
from the program citing affordability issues. The program was approved 
for full-scale development in 1986, and the first aircraft was flown in 
1989. A month after the first flight, the Secretary of Defense stopped 
requesting funds for the program due to affordability concerns. In 
December 1989, the Department of Defense (DOD) directed the Navy to 
terminate all V-22 contracts because, according to DOD, the V-22 was 
not affordable when compared to helicopter alternatives, and production 
ceased. Congress disagreed with this decision, however, and continued 
to fund the project. In October of 1992 the Navy ordered development to 
continue and awarded a contract to a Bell Helicopter Textron and Boeing 
Helicopters joint venture to begin producing production-representative 
aircraft. 

Low-Rate Initial Production began in 1997. In 2000, the MV-22 variant 
began operational testing, the results of which led the Navy's 
operational testers to conclude that the MV-22 was operationally 
effective and was operationally suitable for land-based operations. 
[Footnote 3] Later evaluations resulted in testers concluding that the 
MV-22 would be operationally suitable on ships as well. Based on the 
same tests, DOD's independent operational testers concluded that the MV-
22 was operationally effective but not operationally suitable, due in 
part to reliability concerns. Despite the mixed test conclusions, a 
Program Decision Meeting was scheduled for December 2000 to determine 
whether the V-22 should progress beyond low-rate initial production 
into full-rate production. Following two fatal crashes that occurred in 
2000 and resulted in 23 deaths, the last one occurring just before the 
full-rate production decision, the V-22 was grounded and, rather than 
proceeding to full-rate production, the program was directed to 
continue research and development while low-rate production continued. 
Before the V-22 resumed flight tests, modifications were made to 
requirements and design changes were made to the aircraft to correct 
safety concerns and problems. A second round of operational testing 
with modified aircraft was conducted in June 2005. Both Navy and DOD 
testers then recommended that the aircraft be declared operationally 
effective and suitable for military use. The Defense Acquisition Board 
approved it for military use as well as full-rate production in 
September 2005. 

Operations in Iraq Demonstrated Effectiveness for Assigned Missions but 
the Aircraft Continues to Experience Challenges: 

The MV-22 deployments in Iraq were considered successful. As of January 
2009, the 12 MV-22s deployed in Iraq and utilized by three separate 
squadrons had successfully completed all missions assigned to them 
including general support--moving people and cargo--in what was 
considered an established, low-threat theater of operations[Footnote 
4]. These deployments confirmed that the MV-22's enhanced speed and 
range enable personnel and internally carried cargo to be transported 
faster and farther than is possible with the legacy helicopters the MV- 
22 is replacing. According to MV-22 users and troop commanders, its 
speed and range "cut the battlefield in half," expanding battlefield 
coverage with decreased asset utilization and enabling it to do two to 
three times as much as legacy helicopters in the same flight time. 
Cited advantages include more rapid delivery of medical care, more 
rapid completion of missions, and more rapid travel by U.S. military 
officials to meetings with Iraqi leaders. The MV-22 also participated 
in a few AeroScout missions and carried a limited number of external 
cargo loads.[Footnote 5] 

However, questions have arisen about whether the MV-22 is the aircraft 
best suited to accomplish the full mission repertoire of the 
helicopters it is intended to replace, and some challenges in 
operational effectiveness have been noted. Also, aircraft suitability 
challenges, such as unreliable parts and supply chain weaknesses, drove 
availability significantly below minimum required levels. 

The aircraft's use in Iraq demonstrated operational challenges. For 
example, the introduction of the MV-22 into Iraq in combination with 
existing helicopters has led to some reconsideration of the appropriate 
role of each. Battlefield commanders and aircraft operators in Iraq 
identified a need to better understand the role the Osprey should play 
in fulfilling warfighter needs. They indicated, for example, that the 
MV-22 may not be best suited for the full range of missions requiring 
medium lift, because the aircraft's speed cannot be exploited over 
shorter distances or in transporting external cargo. These concerns 
were also highlighted in a recent preliminary analysis of the MV-22 by 
the Center for Naval Analysis, which found that the MV-22 may not be 
the optimal platform for those missions. 

Availability challenges also impacted the MV-22. In Iraq, the V-22's 
mission capability (MC) and full-mission capability (FMC) rates fell 
significantly below required levels as well as rates achieved by legacy 
helicopters.[Footnote 6] The V-22 MC minimum requirement is 82 percent, 
with an objective of 87 percent, compared with actual MC rates for the 
three squadrons of 68, 57 and 61 percent. This experience is not unique 
to Iraq deployment, as low MC rates were experienced for all MV-22 
squadrons, in and out of Iraq. In comparison, the Iraq-based legacy 
helicopter MC rates averaged 85 percent or greater during the period of 
October 2007 to June 2008. Similarly, the program originally had a FMC 
requirement of 75 percent; but its actual rate of 6 percent in Iraq 
from October 2007 to April 2008 was significantly short of that, due in 
large part to faults in the V-22's Ice Protection System. In areas 
where icing conditions are more likely to be experienced, such as in 
Afghanistan, this may threaten mission accomplishment. 

Repair parts issues and maintenance challenges affected the 
availability of MV-22s in Iraq. V-22 maintenance squadrons faced 
reliability and maintainability challenges, stemming from an immature 
supply chain not always responsive to the demand for repair parts and 
aircraft and engine parts lasting only a fraction of their projected 
service life. The MV-22 squadrons in Iraq made over 50 percent more 
supply-driven maintenance requests than the average Marine aviation 
squadron in Iraq. A lack of specific repair parts took place despite 
having an inventory intended to support 36 aircraft as opposed to the 
12 aircraft deployed. However, only about 13 percent of those parts 
were actually used in the first deployment. In addition, many parts 
that were used were in particularly high demand, which led to a 
shortage that caused cannibalization of parts from other V-22s, MV-22s 
in the United States, and from the V-22 production line. Thirteen V-22 
components accounted for over half the spare parts unavailable on base 
in Iraq when requested. These 13 lasted, on average, less than 30 
percent of their expected life, and 6 lasted less than 10 percent of 
their expected life. V-22 engines also fell significantly short of 
service life expectancy, lasting less than 400 hours versus the program 
estimated life of 500-600 hours. 

Operational Tests and Training Exercises Have Identified Challenges to 
Accomplishing Full Range of Possible Operations: 

V-22 missions in Iraq represent only a portion of the operations 
envisioned for the aircraft, but operational tests and training 
exercises have identified challenges in the V-22's ability to conduct 
operations in high-threat environments, carry the required number of 
combat troops and transport external cargo, operate from Navy ships, 
and conduct missions operating in more extreme environments throughout 
the world. While efforts are underway to address these challenges, 
success is uncertain since some of them arise from the inherent design 
of the V-22. 

* High-Threat Environments: The Osprey was intended to operate across a 
spectrum of high-threat combat situations, facing a broad range of 
enemy land-and sea-based weapons. However, its ability to do so is not 
yet demonstrated. 

- The V-22 has maneuvering limits that restrict its ability to perform 
defensive maneuvers and it does not have a required integrated 
defensive weapon needed to suppress threats while approaching a landing 
zone, disembarking troops within the landing zone, or while leaving the 
landing zone. Currently, the Marine Corps intends to employ the 
aircraft in a manner that limits its exposure to threats--a change from 
the original intent that the system would be able to operate in such 
environments. 

* Transporting Personnel and External Cargo: Operational tests and 
shipboard training exercises have determined that the capacity of the 
MV-22 to transport troops and external cargo is, in some cases, below 
program requirements. 

- The V-22 cannot carry a full combat load of 24 Marines if equipped as 
intended. The average weight of each Marine fully equipped with 
improved body armor and equipment has risen from 240 to 400 pounds. As 
a result, the aircraft can only transport 20 fully loaded combat troops 
rather than the 24-troop requirement. Troop-carrying capacity may be 
further reduced in other configurations and flight scenarios. 

- Most external cargo loads have not been certified for high-speed 
transport and thus would not enable the V-22's speed to be leveraged. 
Anticipated new and heavier equipment would not be able to be 
transported by the Osprey. A 2007 Center for Naval Analysis study found 
that the MV-22 will not be able to externally transport heavier 
equipment, such as the Joint Light Tactical Vehicle--which is to 
replace the Marine Corps' High-Mobility, Multi-Purpose Wheeled Vehicle 
(HMMWV). As a result, the study concluded that there will be less need 
for MV-22s for external lifting and an increased need for heavier lift 
helicopters. 

- The weight of the MV-22 with added equipment planned as upgrades to 
currently configured aircraft may pose a moderate risk to the program. 
The heavier the aircraft is, the less it can carry. Weight growth as a 
result of planned MV-22 upgrades could reduce the aircraft's 
operational utility transporting loads in higher altitude regions of 
the world, such as Afghanistan. 

* Operating on Navy Ships: Efforts to ready the V-22 for deployment 
onboard Navy ships have identified numerous challenges. 

- Because it is larger than the helicopter it is replacing, ships can 
carry fewer V-22s than the predecessor aircraft. Also, the V-22 cannot 
fully utilize all operational deck spots on ships. The MV-22 is only 
cleared to take off and land from four of the six operational deck 
spots of the LHA-and LHD-class ships usable by CH-46s. 

- The Osprey's large inventory of repair parts also constrains hangar 
deck space essential for maintenance actions on the V-22 and other 
aircraft. The space needed for its repair parts is so large that some 
parts may need to be prepositioned ashore. 

- Safety concerns caused by downwash have been documented. The V-22's 
proprotors create downwash significantly greater than that of the CH-
46s it is replacing. The downwash impacts operations below the 
aircraft, including troop embarkation and debarkation, hooking up 
external loads, and fastroping.[Footnote 7] During shipboard exercises, 
the V-22's downwash dislodged equipment such as life raft container 
securing bands and was so severe in one instance that another person 
was assigned to physically hold in place the sailor acting as the 
landing guide. Recently completed tests on the CV-22 found that the 
significant downwash also had various negative effects on land-based 
missions. 

* Challenges Operating Globally in Extreme Environments: The Osprey's 
ability to conduct worldwide operations in many environments is 
limited. 

- The V-22 had a requirement that its fuselage and cockpit be designed 
to restrict the entry of nuclear, biological, and chemical contaminants 
into the aircraft.[Footnote 8] During initial operational tests 
numerous problems existed with the seals that maintained cabin 
pressure, so the system could not be used. Without it, operational V- 
22s are forced to avoid or exit areas of suspected contamination and 
decontaminate affected aircraft, likely reducing their availability and 
sortie capability. 

- The MV-22 is intended to support diverse mission requirements that 
will require it to fly during the day or at night, in favorable or 
adverse weather, and across a range of altitudes from close to the 
ground to above 10,000 feet above mean sea level. Current V-22 
operating limitations do not support helicopter operations above 10,000 
feet. The MV-22 currently does not have a weather radar and the 
Osprey's Ice Protection System is unreliable, so flying through known 
or forecasted icing conditions is currently prohibited. 

V-22 Costs Rose While Performance Requirements Were Modified: 

The V-22's original program cost estimates have changed significantly 
as research and development, and procurement costs have risen sharply 
above initial projections. Operations and supports costs are just 
beginning and are expected to rise. This has taken place in spite of 
the fact that performance standards and metrics for V-22 were modified 
throughout the development effort. 

V-22 Business Case and Acquisition Strategy Have Eroded as Costs Have 
Increased Significantly and Are Expected to Continue to Rise: 

From initial development in 1986 through the end of 2007, the program's 
Research, Development, Test, and Evaluation cost increased over 200 
percent--from $4.2 to $12.7 billion--while its procurement cost 
increased nearly 24 percent from $34.4 to $42.6 billion.[Footnote 9] 
This increase coincided with significant reductions in the number of 
aircraft being procured--from nearly a thousand to less than 500 (most 
of which will be procured for the Marine Corps)--resulting in a 148 
percent increase in procurement unit cost for each V-22. Operations and 
support (O&S) cost are also expected to rise. Table 1 details key 
aspects of the V-22 program's cost and schedule experience from 
development start to 2007. 

Table 1: V-22 Cost, Quantity and Schedule Changes from Development 
Start to 2007: 

Costs in millions of constant fiscal year 2009 dollars. 

Research & Development; 
1986: $4,211.8; 
2007: $12,682.0; 
Percentage: change: 201%. 

Procurement; 
1986: $34,362.9; 
2007: $42,585.2; 
Percentage: change: 24%. 

Procurement unit cost; 
1986: $37.7; 
2007: $93.4; 
Percentage: change: 148%. 

Average program unit cost (Research, Development, Test, and Evaluation 
plus Procurement costs)/Quantity; 
1986: $42.3; 
2007: $121.2; 
Percentage: change: 186%. 

Procurement quantities; 
1986: 913; 
2007: 456; 
Percentage: change: -50.1%. 

Production years; 
1986: 1990-1999; 
2007: 1997-2018; 
Percentage: change: [Empty]. 

Initial operational capability; 
1986: 1992; 
2007: June 2007; 
Percentage: change: [Empty]. 

Source: GAO analysis of U.S. Navy V-22 Selected Acquisition Reports. 

[End of table] 

O&S costs--typically the largest portion of a weapon system's total 
costs--are currently reported at $75.41 billion for the life cycle of 
the program, but O&S costs for the program are just beginning and are 
expected to rise. One indication they may rise is the current cost per 
flying hour, which is over $11,000--more than double the target 
estimate for the MV-22 as well as 140 percent higher than the cost for 
the CH-46E.[Footnote 10] The Osprey's Iraq experience demonstrated that 
the rise in cost is due in part to unreliable parts, the cost of some 
parts, and required maintenance. 

As illustrated in figure 2, the program's estimated future funding 
needs are approximately $100 billion (then-year dollars)--nearly $25 
billion in procurement and around $75 billion in O&S. 

Figure 2: V-22 Funding Profile (Then-Year Dollars)[Footnote 11] 

[Refer to PDF for image: stacked vertical bar graph] 

Spending category: Research and development; 
Appropriated and requested funds (program start through 2009): $9.6 
billion; 
Estimated future funding: $0.31 billion. 

Spending category: Procurement; 
Appropriated and requested funds (program start through 2009): $19.26 
billion; 
Estimated future funding: $24.78 billion. 

Spending category: Operations and support cost; 
Appropriated and requested funds (program start through 2009): 0; 
Estimated future funding: %75.41 billion. 

Spending category: Total; 
Appropriated and requested funds (program start through 2009): $28.86 
billion; 
Estimated future funding: $100.50 billion. 

Source: V-22 December 2007 Selected Acquisition Report. 

[End of figure] 

According to Marine Corps officials, the presence of unreliable parts 
contributed to reliability and maintainability issues for MV-22 
deployed in Iraq, and a program is in place to address underperforming 
components. However, program management does not consider the current 
reliability and maintainability strategy to be coherent. Problems with 
parts reliability have resulted in more maintenance activity than 
expected, and if there is no improvement, overall cost and maintenance 
hours may remain high. Changes to the current engine sustainment 
contract with Rolls Royce--the V-22's engine manufacturer--could also 
affect the program's already rising O&S costs. 

Key Performance Standards and Other Performance Metrics for MV-22 
Modified: 

Initially, the Marine Corps' proposed performance parameters for the V-
22 were focused on speed, range, and payload. However, the Joint 
Requirements Oversight Council deferred consideration of system 
requirements until completing the 1994 Cost and Operational 
Effectiveness Analysis that validated the V-22 over other alternatives. 
While reports indicate that the MV-22 is meeting all its key 
performance parameters, program officials said modifications were made 
to balance aircraft operational requirements against technical risks 
and program costs. In 2001, for example, modifications consolidated 14 
key performance parameters into 7 for the MV-22 variant. 

While the office of the Director, Operational Test and Evaluation 
(DOT&E) found the MV-22 operationally effective in 2000, it did not 
find it operationally suitable, due in part to reliability concerns. 
Mission capability, one of the metrics used to measure suitability, was 
modified in 2004 such that the mission capability rate does not now 
have to be met until the aircraft reaches system maturity (60,000 
flight hours), whereas the requirement previously specified no minimum 
required number of flight hours. According to Marine Corps Headquarters 
officials, the aircraft currently has over 50,000 hours and may reach 
the 60,000 hour threshold within a year. 

Concerns about V-22 weight increase and how it may affect aircraft 
performance have continued. In 2005, a DOT&E report on the second 
operational test of the MV-22 predicted a drop in performance due to a 
projected weight increase. However, according to Navy operational 
testers who tested the aircraft in 2007, performance did not decrease. 
DOT&E did not report on the 2007 test. The program office is currently 
tracking weight increase in the newest version of the aircraft as a 
potential risk to the achievement of select key performance parameters. 

Concluding Observations: 

After more than 20 years in development and 14 years since the last 
cost and operational effectiveness analysis was developed to reaffirm 
the decision to proceed with the V-22 program, the MV-22 experience in 
Iraq demonstrated that the Osprey can complete missions assigned in low-
threat environments. Its speed and range were enhancements. However, 
challenges may limit its ability to accomplish the full repertoire of 
missions of the legacy helicopters it is replacing. If so, those tasks 
will need to be fulfilled by some other alternative. Viewed more 
broadly, the MV-22 has yet to fully demonstrate that it can achieve the 
original required level of versatility. To be useful to the warfighter 
in a variety of climates and places, its ability to address and resolve 
a range of operational challenges must be re-evaluated. Furthermore, 
suitability challenges that lower aircraft availability and affect the 
operations and support funding that may be required to maintain the 
fleet need to be addressed. Based on the Iraq experience, the cost per 
flight hour is more than double the target estimate. DOD is therefore 
faced with the prospect of directing more money to a program, the 
military utility of which in some areas remains unproven. Now is a good 
time to consider the return on this investment as well as other less 
costly alternatives that may fill the current requirement. 

The V-22 program has already received or requested over $29 billion in 
development and procurement funds. The estimated funding required to 
complete the development and procure additional V-22s is almost $25 
billion (then-year dollars). In addition, the program continues to face 
a future of high operations and support cost funding needs, currently 
estimated at $75.4 billion for the life cycle of the program. Before 
committing to the full costs of completing production and support the V-
22, the uses, cost, and performance of the V-22 need to be clarified 
and alternatives should be reconsidered. Questions to consider include: 
To what degree is the V-22 a suitable and exclusive candidate for the 
operational needs of the Marine Corps and other services? How much will 
it cost? How much can DOD afford to spend? To what degree can a 
strategy be crafted for ensuring control over these future costs? If 
the V-22 is only partially suitable, to what degree can another 
existing aircraft or some mixture of existing aircraft (including V-
22s) or a new aircraft perform all or some of its roles more cost 
effectively? Some consideration should be given to evaluating the roles 
such aircraft play in today's theaters of war and whether their 
performance warrants their cost. 

Failure to re-examine the V-22 program at this point risks the 
expenditure of billions of dollars on an approach that may be less 
effective than alternatives. Furthermore, if the suitability challenges 
facing the program are not adequately addressed, the future cost of the 
program could rise significantly requiring funds that might otherwise 
be made available to satisfy other needs. This is why we recommended in 
our May 11 report that the Secretary of Defense (1) re-examine the V-22 
by requiring a new alternatives analysis and (2) require the Marine 
Corps to develop a prioritized strategy to improve system suitability, 
reduce operational costs, and align future budget requests. DOD 
concurred with our second recommendation, but not the first. In non- 
concurring with our recommendation for a new V-22 alternatives 
analysis, DOD stated that it supports validating required MV-22 
quantities and the proper mix of aircraft, but not by means of a new V- 
22 alternatives analysis. Rather, DOD stated that planning for all 
elements of Marines Corps aviation (including required quantities, 
location, and employment of medium-lift assets) and total force 
affordability are reviewed and updated annually in the Marine Aviation 
Plan. We maintain our recommendation for a new alternatives analysis as 
a means of providing a comparison of a fuller range of alternatives, 
including their costs, operational suitability, and operational 
effectiveness under varying scenarios and threat levels. Furthermore, 
development of a V-22 alternatives analysis could assure congressional 
decision-makers that a reasoned business case exists that supports the 
planned acquisition of an additional 282 V-22s and an expenditure of 
almost $25 billion in procurement funds in fiscal years 2010 and 
beyond. 

Mr. Chairman, this concludes my prepared statement. I would be pleased 
to answer any questions that you or other Members of the Committee may 
have at this time. 

GAO Contact and Staff Acknowledgments: 

For further information about this testimony, please contact Michael J. 
Sullivan at (202) 512-4841 or sullivanm@gao.gov. Individuals making key 
contributions to this testimony include Bruce H. Thomas, Assistant 
Director; Jerry W. Clark; Bonita J.P. Oden; Bob Swierczek; Kathryn E. 
Bolduc; Jonathan R. Stehle; Johanna Ayers; Jason Pogacnik; Hi Tran; 
William Solis; and Marie P. Ahearn. 

[End of section] 

Footnotes: 

[1] CH-53 helicopters are also being used, in part, to conduct medium- 
lift operations for the Marines Corps. 

[2] GAO, Defense Acquisitions: Assessments Needed to Address V-22 
Aircraft Operational and Cost Concerns to Define Future Investments, 
[hyperlink, http://www.gao.gov/products/GAO-09-482] (Washington, D.C.: 
May 11, 2009). 

[3] Operational Effectiveness is the measure of the overall ability of 
a system to accomplish a mission when used by representative personnel 
in the environment planned or expected for operational employment of 
the system. Operational Suitability is the degree to which a system can 
be placed and sustained satisfactorily in field use. 

[4] Low threat includes sporadic small arms fire from random locations 
(maximum caliber 7.62 mm/.30 cal), and automatic weapons (assault 
rifles). Medium threat includes those threats, plus larger caliber 
weapons (.50 cal/12.5 mm and 23mm, but not Anti-Aircraft Artillery 
(AAA)) adapted for anti-aircraft fire, more sophisticated aiming 
devices, and legacy man-portable air-defense systems. High threat 
environment may include mobile and/or stationary surface-to-air 
missiles, early warning radars, integrated AAA fire control systems, 
and interceptor aircraft. 

[5] AeroScout missions were developed for and conducted by legacy 
helicopters. The concept arose prior to the V-22 arriving in Iraq. 
AeroScout missions are made to identify suspicious targets and 
neutralize those threats. 

[6] An aircraft that is mission capable (MC) is one that is in a 
material condition to perform at least one of its designated missions, 
while an aircraft that is fully mission capable (FMC) is in a material 
condition to perform all of its designated missions. The program has 
modified the MC requirement by stating that this threshold should be 
achieved by the time the fleet completes 60,000 flight hours, which 
officials expect to occur sometime near the end of 2009. 

[7] Fastroping is a method used by troops to quickly exit a hovering 
aircraft. 

[8] This requirement has since been dropped. 

[9] Amounts are in constant fiscal year 2009 dollars. 

[10] These data were gathered after the Material Support Date, October 
1, 2008, when the Navy assumed responsibility for all spares and repair 
parts needed to support a new weapons system, subsystem, or support 
equipment end item at Fleet operational sites. 

[11] O&S expenditures to date for the recently fielded MV-22 are not 
reported in the Selected Acquisition Report. O&S funding represents 
past and future funding needs. In fiscal year 2009 dollars, R&D would 
be $12.6 billion in past funds and $0.3 billion in estimated future 
funding; procurement would be $21 billion in past funds and $22.3 
billion estimated future funding, and O&S would be $54.5 billion in 
estimated future funding. 

[End of section] 

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