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Testimony before the Subcommittees on Air and Land Forces, and Seapower 
and Expeditionary Forces, Committee on Armed Services, House of 
Representatives: 

United States Government Accountability Office: 

GAO: 

For Release on Delivery Expected at 2:00 p.m. EDT: 

Thursday, March 22, 2007: 

Defense Acquisitions: 

Analysis of Costs for the Joint Strike Fighter Engine Program: 

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

GAO-07-656T: 

GAO Highlights: 

Highlights of GAO-07-656T, a testimony before the Subcommittees on Air 
and Land Forces, and Seapower and Expeditionary Forces, Committee on 
Armed Services, House of Representatives 

Why GAO Did This Study: 

The Joint Strike Fighter (JSF) is the linchpin of future Department of 
Defense (DOD) tactical aircraft modernization efforts because of the 
sheer size of the program and its envisioned role as the replacement 
for hundreds of aircraft that perform a wide variety of missions in the 
Air Force, Navy, and Marine Corps. DOD implemented the JSF alternate 
engine development program in 1996 to provide competition between two 
engine manufacturers in an effort to achieve cost savings, improve 
performance, and gain other benefits. This testimony focuses on GAO’s 
cost analysis performed in response to Section 211 of the John Warner 
National Defense Authorization Act for Fiscal Year 2007. We examined 
the following areas: (1) sole-source and competitive scenarios for 
development, production, and sustainment of the JSF engine, (2) results 
of past engine programs and their related strategies, and (3) impact on 
the industrial base in the event of the complete cancellation of the 
JSF alternate engine program. DOD did not provide comments on our 
findings. 

What GAO Found: 

* Continuing the alternate engine program for the Joint Strike Fighter 
would cost significantly more than a sole-source program but could, in 
the long run, reduce costs and bring other benefits. The current 
estimated life cycle cost for the JSF engine program under a sole-
source scenario is $53.4 billion. To ensure competition by continuing 
to implement the JSF alternate engine program, an additional investment 
of $3.6 billion to $4.5 billion may be required. However, the 
associated competitive pressures from this strategy could result in 
savings equal to or exceeding that amount. The cost analysis we 
performed suggests that a savings of 10.3 to 12.3 percent would recoup 
that investment, and actual experience from past engine competitions 
suggests that it is reasonable to assume that competition on the JSF 
engine program could yield savings of at least that much. In addition, 
DOD-commissioned reports and other officials have said that 
nonfinancial benefits in terms of better engine performance and 
reliability, improved industrial base stability, and more responsive 
contractors are more likely outcomes under a competitive environment 
than under a sole-source strategy. 

* DOD experience with other aircraft engine programs, including the F-
16 fighter in the 1980s, has shown competitive pressures can generate 
financial benefits of up to 20 percent during the life cycle of an 
engine program and/or improved quality and other benefits. 

* The potential for cost savings and performance improvements, along 
with the impact the engine program could have on the industrial base, 
underscores the importance and long-term implications of DOD decision 
making with regard to the final acquisition strategy solution. 

[Hyperlink, http://www.gao.gov/cgi-bin/getrpt?GAO-07-656T]. 

To view the full product, including the scope and methodology, click on 
the link above. For more information, contact Mike Sullivan at (202) 
512-4841 or sullivanm@gao.gov. 

[End of section] 

Mr. Chairmen and Members of the Subcommittees: 

I am pleased to be here today to discuss the Joint Strike Fighter (JSF) 
engine program. The JSF is the linchpin of future Department of Defense 
(DOD) tactical aircraft modernization efforts because of the program's 
sheer size and envisioned role as the replacement for hundreds of 
aircraft that provide a wide variety of missions in the Air Force, 
Navy, and Marine Corps. DOD implemented the JSF alternate engine 
development program in 1996 to provide competition between two engine 
manufacturers in an effort to achieve cost savings, improve 
performance, and gain other benefits. Today, my testimony focuses on 
our cost analysis performed in response to Section 211 of the John 
Warner National Defense Authorization Act for Fiscal Year 
2007.[Footnote 1] Specifically, it examines the following areas: (1) 
sole-source and competitive scenarios for development, production, and 
sustainment of the JSF engine; (2) results of past engine programs and 
their related strategies; and (3) impact on the industrial base in the 
event of the complete cancellation of the JSF alternate engine program. 
While language in the act instructed GAO to report on additional 
elements related to a firm-fixed-price acquisition strategy and any 
other approach that could improve cost or schedule, this statement 
focuses on the areas above, as we determined those to be the most 
viable options under consideration. Appendix I contains information 
about scope and methodology for the cost analysis on which this 
statement is based. We performed our work from January 2007 to March 
2007 in accordance with generally accepted government auditing 
standards. 

Summary: 

The current estimated remaining life cycle cost for the JSF engine 
program under a sole-source scenario is $53.4 billion. To ensure 
competition by continuing the JSF alternate engine program, an 
additional investment of $3.6 billion to $4.5 billion may be required. 
However, the associated competitive pressures from this strategy could 
result in savings equal to or exceeding that amount across the life 
cycle of the engine. The cost analysis we performed suggests that a 
savings of 10.3 to 12.3 percent would recoup that investment, and 
actual experience from past engine competitions suggests that it is 
reasonable to assume that competition on the JSF engine program could 
yield savings of at least that much. These results are dependent on how 
the government decides to run the competition, the number of aircraft 
that are ultimately purchased, and the exact ratio of engines awarded 
to each contractor. In addition, DOD-commissioned reports and other 
officials have said that non financial benefits in terms of better 
engine performance and reliability, improved industrial base stability, 
and more responsive contractors are more likely outcomes under a 
competitive environment than under a sole-source strategy. DOD 
experience with other aircraft engine programs, including that for the 
F-16 fighter, has shown competitive pressures can generate financial 
benefits of up to 20 percent during the life cycle of an engine program 
and/or the other benefits mentioned. The potential for cost savings and 
performance improvements, along with the impact the engine program 
could have on the industrial base, underscores the importance and long- 
term implications of DOD decision making with regard to the final 
acquisition strategy. DOD chose not to provide comments on this 
statement or the cost analysis on which it is based. The JSF program 
office reviewed our findings and made technical comments which were 
incorporated as appropriate. 

Background: 

The Joint Strike Fighter is DOD's most expensive aircraft acquisition 
program. The number of aircraft engines and spare parts expected to be 
purchased, along with the lifetime support needed to sustain the 
engines, mean the future financial investment will be significant. DOD 
is expected to develop, procure, and maintain 2,443 aircraft at a cost 
of more than $338 billion over the program's life cycle.[Footnote 2] 
The JSF is being developed in three variants for the U.S. military: a 
conventional takeoff and landing aircraft for the Air Force, a carrier- 
capable version for the Navy, and a short takeoff and vertical landing 
variant for the Marine Corps.[Footnote 3] In addition to its size and 
cost, the impact of the JSF program is even greater when combined with 
potential international sales (expected to be between 2,000 and 3,500 
additional aircraft) and the current U.S. aircraft that the JSF will 
either replace or complement to meet mission requirements. 

Congress first expressed concern over the lack of engine competition in 
the JSF program in fiscal year 1996 and in fiscal year 1998 directed 
DOD to ensure that sufficient funding was committed to develop an 
alternate engine. Since that time, DOD has initiated multiple studies 
to determine the advantages and disadvantages of the alternate engine 
program. DOD program management advisory groups conducted studies in 
1998 and again in 2002, both resulting in recommendations to continue 
with the alternate engine program. The advisory groups determined that 
developing an alternate JSF engine had significant benefits in the 
areas of contractor responsiveness, industrial base, aircraft 
readiness, and international participation. They also reported finding 
marginal benefits in the areas of cost savings and the ability to add 
future engine improvements. However, they found no benefit with regard 
to reducing development risk without restructuring the program. The 
advisory groups noted that these recommendations were made independent 
of the services' ability to fund the program--meaning overall 
affordability should be taken into consideration. 

In August 2005, DOD awarded a $2.1 billion contract for alternate 
engine system development and demonstration, of which $699 million has 
been appropriated to date.[Footnote 4] In its fiscal year 2007 budget 
submission, DOD proposed canceling the alternate engine program and 
eliminated funding related to this effort. While Congress restored the 
majority of the funding for that year, DOD again eliminated alternate 
engine funding in its proposed budget for fiscal year 2008. 

DOD decided to cancel the alternate engine program prior to the fiscal 
year budget submission, stating that (1) no net cost benefits or 
savings are to be expected from competition and (2) low operational 
risk exists for the warfighter under a sole-source engine supplier 
strategy. We reported last year that this decision was made without a 
new and comprehensive analysis and focused only on the potential up- 
front savings in engine procurement costs. We stated further that costs 
already sunk were inappropriately included and long-term savings that 
might accrue from competition for providing support for maintenance and 
operations over the life cycle of the engine were excluded from the 
decision justification. Our position was that DOD's decision to cancel 
the program was driven by the need to identify sources of funding in 
order to pay for other, more immediate priorities within the 
department. 

DOD did not change the JSF acquisition strategy to reflect its proposed 
elimination of the alternate engine program, and it continues a dual 
engine approach. The 2007 Defense Authorization Act has now placed 
certain restrictions on DOD modification of the dual engine approach. 
According to current JSF program plans, beginning in fiscal year 2007, 
the program office will award the first of three annual production 
contracts to Pratt & Whitney for its F135 engine. In fiscal years 2010 
and 2011, noncompetitive contracts will be awarded to both Pratt & 
Whitney and to the Fighter Engine Team[Footnote 5] for the F136 engine. 
Beginning in fiscal year 2012, contracts will be awarded on an annual 
basis under a competitive approach for quantities beyond each 
contractor's minimum sustaining rate. Full-rate production for the 
program begins in fiscal year 2014 and is expected to continue through 
fiscal year 2034. The JSF program intends to use a combination of 
competition, performance-based logistics, and contract incentives to 
achieve goals related to affordability, supportability, and safety. 
Through this approach, the JSF program office hopes to achieve 
substantial reductions in engine operating and support costs. 
Traditionally, operating and support costs have accounted for 72 
percent of a program's life cycle costs. 

Our Analysis of Alternatives Suggests Competition Benefits Could 
Outweigh Costs: 

Without competition, the JSF program office estimates that it will 
spend $53.4 billion over the remainder of the F135 engine program. This 
includes cost estimates for the completion of system development, 
procurement of 2,443 engines, production support, and sustainment. 
Additional investment of between $3.6 billion and $4.5 billion may be 
required should the Department decide to continue competition in the 
JSF engine program. This includes additional development, procurement, 
support, and stand-up costs for a second engine provider. While Pratt & 
Whitney design responsibilities and associated costs may be reduced 
under a sole-source contract, our analysis shows that competitive 
pressures may yield enough financial savings to offset the costs of 
competition over the life of the program. These results are dependent 
on how the government decides to run the competition, the number of 
aircraft that are ultimately purchased, and the exact ratio of engines 
awarded to each contractor. Given certain assumptions with regard to 
these factors, the additional costs of having the alternate engine 
could be recouped if competition were to generate approximately 10.3 to 
12.3 percent savings. According to actual Air Force data from past 
engine programs, including for the F-16 aircraft, it is reasonable to 
expect savings of at least that much. Additionally, there are a number 
of non financial benefits that may result from competition, including 
better performance, increased reliability, and improved contractor 
responsiveness. 

Sole-Source Alternative Requires Less Short-term Investment: 

The cost of the Pratt & Whitney F135 engine is estimated to be $53.4 
billion over the remainder of the program. This includes cost estimates 
for the completion of system development, procurement of engines, 
production support, and sustainment. Table 1 shows the costs remaining 
to develop, procure, and support the Pratt & Whitney F135 engine on a 
sole-source basis. 

Table 1: Costs to Complete Pratt & Whitney F135 Engine Program (based 
on 2,443 installed engines and spares): 

Cost element: System development and demonstration costs; 
Cost (FY02$B): $1.0. 

Cost element: Total engine unit recurring flyaway costs; 
Cost (FY02$B): $17.6. 

Cost element: Production support costs (including initial spares, 
training, manpower, and depot stand-up); 
Cost (FY02$B): $3.2. 

Cost element: Sustainment costs of fielded aircraft; 
Cost (FY02$B): $31.6. 

Cost element: Total; 
Cost (FY02$B): $53.4. 

Source: JSF program office data; GAO analysis. 

[End of table] 

Costs remaining for the JSF engine program can be broken down into four 
categories: 

* remaining system development and demonstration contract costs; 

* engine unit recurring flyaway costs--per unit cost for aircraft, 
based on rate of learning; 

* production support costs related to production spares, training 
personnel and equipment, manpower, and depot facilities; and: 

* sustainment costs to maintain fielded aircraft based on engine flight 
hour costs and usage rates. 

Stable requirements and funding, a well-defined acquisition strategy, 
an appropriately structured contract, and adequate oversight are keys 
to ensuring the contractor is motivated to perform, especially under a 
sole-source contract where competitive pressure does not exist. In a 
sole-source environment, the primary benefit comes from the improved 
rate of progress, or "learning," achieved by the contractor based on 
having all production activity.[Footnote 6] In other words, the greater 
volume of business given to a single contactor is expected to translate 
into efficiency in production in a shorter time, thereby lowering 
associated costs. Learning curves must be established in a manner so 
that the contractor is not only intent on meeting that curve, but also 
incentivized to exceed the curve in order to achieve cost reductions. 
Through analysis of program information and in conversations with Pratt 
& Whitney and JSF program office personnel, we found examples of 
initiatives aimed at improving the F135 learning curve. Pratt & Whitney 
has ongoing and planned activities in areas such as supply chain 
optimization, technology development, and manufacturing efficiency that 
it hopes will reduce unit costs through the first 5 years of F135 
production. 

Having Pratt & Whitney as the single engine manufacturer may also 
provide benefits in terms of simpler design and integration 
responsibilities. Currently, in addition to development of the F135 
engine design, Pratt & Whitney has responsibility for design and 
development of common components that will go on all JSF aircraft, 
regardless of which contractor provides the engine core. Examples of 
common components include the lift fan and roll posts for the Marine 
Corps variant, the exhaust nozzles, and ducts. This responsibility 
supports the overall F-35 program requirement that the engine be 
interchangeable--either engine can be used in any aircraft variant, 
either during initial installation or when replacement is required. In 
the event that Pratt & Whitney is made the sole-source engine provider, 
future configuration changes to the aircraft and common components 
could be optimized for the F135 engine, instead of potentially 
compromised design solutions or additional costs needed to support both 
F135 and F136. 

JSF Engine Competition Could Result in Future Savings: 

In testimony last year, the Under Secretary of Defense for Acquisition, 
Technology, and Logistics reported that DOD preferred a sole-source 
engine strategy for the JSF program. He noted that maintaining two 
engine suppliers for the program would cost, at that time, an 
additional $1.8 billion for the development phase which was not the 
most efficient use of Department resources. In fact, when considering 
the costs of competition over the full life cycle of the F136 program, 
the additional costs are even greater. The government's ability to 
recoup the additional investments required to support competition 
depends largely on (1) the number of aircraft produced[Footnote 7], (2) 
the ratio that each contractor wins out of that total, and (3) the 
savings rate that competitive pressures drive. We estimated costs under 
two competitive scenarios; one in which contractors are each awarded 50 
percent of the total engine purchases (50/50 split) and one in which 
there is a 70/30 percent award split of total engine purchases to 
either contractor, beginning in fiscal year 2012. Without consideration 
of potential savings, the additional costs of competition total $4.5 
billion under the first scenario and $3.6 billion under the second 
scenario. Table 2 shows the additional cost associated with competition 
under these two scenarios. 

Table 2: Additional Costs for Competition in JSF Engine Program (based 
on 2,443 installed engines and spares): 

Additional costs (FY02$B): System development and demonstration costs; 
50/50 Aircraft award split: $1.4; 
70/30 Aircraft award split: $1.4. 

Additional costs (FY02$B): Total engine unit recurring fly-away costs; 
50/50 Aircraft award split: $3.0; 
70/30 Aircraft award split: $2.1. 

Additional costs (FY02$B): Production support costs (including initial 
spares, training, manpower, and depot standup); 
50/50 Aircraft award split: $.13; 
70/30 Aircraft award split: $.13. 

Additional costs (FY02$B): Sustainment costs of fielded aircraft[A]; 
50/50 Aircraft award split: N/A; 
70/30 Aircraft award split: N/A. 

Additional costs (FY02$B): Total; 
50/50 Aircraft award split: $4.5; 
70/ 30 Aircraft award split: $3.6. 

Source: JSF program office data; GAO analysis. 

[A] No additional sustainment costs were considered because the number 
of aircraft and cost per flight hour would be the same under either 
scenario. 

[End of table] 

The disparity in costs between the two competitive scenarios reflects 
the loss of learning resulting from lower production volumes that is 
accounted for in the projected unit recurring flyaway costs used to 
construct each estimate. The other costs include approximately $1.4 
billion in remaining F136 development costs and $127 million in 
additional stand-up costs, which would be the same under either 
competitive scenario. 

DOD implemented the JSF alternate engine development program to provide 
competition between two engine manufacturers in an effort to achieve 
cost savings, improve performance, and gain other benefits. For 
example, competition may incentivize the contractors to achieve more 
aggressive production learning curves, produce more reliable engines 
that are less costly to maintain, and invest additional corporate money 
in technological improvements to remain competitive. To reflect these 
and other potential factors, we applied a 10 to 20 percent range of 
potential cost savings to our estimates, where pertinent to a 
competitive environment.[Footnote 8] Further, when comparing life cycle 
costs, it is important to consider that many of the additional 
investments associated with competition are often made earlier in the 
program's life cycle, though much of the expected savings do not accrue 
for decades. Therefore, a net present value calculation (time value of 
money) must be included in the analysis and, once applied, provides for 
a better estimate of program rate of return. Figure 1 shows the results 
of our analysis under different scenarios and accounting for the time 
value of money. 

Figure 1: Net Present Value of JSF Engine Competition: 

[See PDF for image] 

Source: JSF program office data; GAO analysis. 

Note: Net present value calculated based on fiscal year 2002. 

[End of figure] 

When we assumed overall savings due to competition, our analysis 
indicated that recoupment of those initial investment costs would occur 
at somewhere between 10.3 and 12.3 percent, depending on the number of 
engines awarded to each contractor. A competitive scenario where one of 
the contractors receives 70 percent of the annual production aircraft, 
while the other receives only 30 percent reaches the breakeven point at 
10.3 percent savings. A competitive scenario where both contractors 
receive 50 percent of the production aircraft reaches this point at 
12.3 percent savings.[Footnote 9] We believe it is reasonable to assume 
at least this much savings in the long run based on analysis of actual 
data from the F-16 engine competition. 

Competition Offers Potential Benefits beyond Financial Savings: 

Competition may also provide benefits that do not result in immediate 
financial savings, but may result in reduced costs or other positive 
outcomes to the program over time. DOD and others have performed 
studies and have widespread concurrence as to these other benefits, 
including better engine performance, increased reliability, and 
improved contractor responsiveness. In fact, in 1998 and 2002, DOD 
program management advisory groups assessed the JSF alternate engine 
program and found the potential for significant benefits in these and 
other areas. Table 3 summarizes the benefits determined by those 
groups. 

Table 3: 1998 and 2002 Program Management Advisory Group Study Findings 
on the Benefits of an Alternate Engine Program: 

Factor assessed: Costs; 
Beneficial: 1998: [Empty]; 
Beneficial: 2002: [Empty]; 
Marginal: 1998: X; 
Marginal: 2002: X; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: Development risk reduction; 
Beneficial: 1998: [Empty]; 
Beneficial: 2002: [Empty]; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: X; 
No value: 2002: X. 

Factor assessed: Engine growth potential; 
Beneficial: 1998: [Empty]; 
Beneficial: 2002: [Empty]; 
Marginal: 1998: X; 
Marginal: 2002: X; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: Fleet readiness; 
Beneficial: 1998: X; 
Beneficial: 2002: X; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: Industrial base; 
Beneficial: 1998: X; 
Beneficial: 2002: X; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: International implications; 
Beneficial: 1998: X; 
Beneficial: 2002: X; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: Other considerations[A]; 
Beneficial: 1998: X; 
Beneficial: 2002: X; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Factor assessed: Overall; 
Beneficial: 1998: X; 
Beneficial: 2002: X; 
Marginal: 1998: [Empty]; 
Marginal: 2002: [Empty]; 
No value: 1998: [Empty]; 
No value: 2002: [Empty]. 

Source: DOD data; GAO analysis and presentation. 

[A] Other considerations include contractor responsiveness, improved 
design solutions, and competition at the engine subsystem level. 

[End of table] 

While the benefits highlighted may be more difficult to quantify, they 
are no less important, and ultimately were strongly considered in 
recommending continuation of the alternate engine program. These 
studies concluded that the program would: 

* maintain the industrial base for fighter engine technology, 

* enhance readiness, 

* instill contractor incentives for better performance, 

* ensure an operational alternative if the current engine developed 
problems, and: 

* enhance international participation. 

We spoke with government officials from various organizations who 
widely concurred with our analysis of the potential benefits of engine 
competition. Many of these were important benefits realized by past 
competitions such as that for the Air Force F-16 aircraft engines. 
Discussions with the Air Force engine manager who co led both advisory 
group studies explained that these benefits are valuable when trying to 
manage significant numbers of fighter-type engines to ensure combat 
readiness. He told us that problems are magnified when trying to manage 
a single engine system, which can require substantial manpower and 
extra hours to keep aircraft flying when engine problems occur. In his 
opinion, the benefits of a dual-source engine would outweigh the costs. 
He stated that he had not seen anything that would change this 
conclusion since the last advisory group study was conducted. 

The ability of competition to deliver such benefits is important for 
the JSF program. In addition to considering engine price, the program 
office has identified a range of potential criteria for competition 
during the production and support phases of the program, which could 
include other costs, reliability, and sustainability. It is reasonable 
to assume that competition under these criteria may drive better engine 
performance and reliability over the life of the program. Such 
improvements can positively affect fleet readiness and schedule 
outcomes while avoiding costs in various other areas for the JSF 
program. 

Another potential benefit of having an alternate engine program, and 
one also supported by the program advisory group studies, is to reduce 
the risk that a single point, systemic failure in the engine design 
could substantially affect the fighter aircraft fleet. Though current 
performance data indicate it is unlikely that engine problems would 
lead to fleet wide groundings in modern aircraft, having two engine 
sources for the single-engine JSF further reduces this risk as it is 
more unlikely that such a problem would occur to both engine types at 
the same time. Because the JSF is expected to be the primary fighter 
aircraft in the U.S. inventory, and Pratt & Whitney will also be the 
sole-source provider of F119 engines for the F-22A aircraft,[Footnote 
10] DOD is faced with the potential scenario where almost the entire 
fleet could be dependent on similar engine cores, produced by the same 
contractor in a sole-source environment. 

Past Engine Programs Show Potential Benefits from Competition: 

Results from past competitions provide evidence of potential financial 
and non financial savings that can be derived from engine programs. One 
relevant case study to consider is the "Great Engine War" of the 1980s-
-the competition between Pratt & Whitney and General Electric to supply 
military engines for the F-16 and other fighter aircraft programs. At 
that time all engines for the F-14 and F-15 aircraft were being 
produced on a sole-source basis by Pratt & Whitney, which was 
criticized for increased procurement and maintenance costs, along with 
a general lack of responsiveness with regard to government concerns 
about those programs. For example, safety issues on the single-engine F-
16 aircraft were seen as having greater consequences than the twin- 
engine F-14 or F-15 aircraft. To address concerns, the Air Force began 
to fund the development and testing of an alternate engine to be 
produced by General Electric; the Air Force also supported the advent 
of an improved derivative of the Pratt & Whitney engine. Beginning in 
1983, the Air Force initiated a competition that Air Force 
documentation suggests resulted in significant cost savings in the 
program. For example, in the first 4 years of the competition, when 
actual costs are compared to the program's baseline estimate, results 
included: 

* nearly 30 percent cumulative savings for acquisition costs, 

* roughly 16 percent cumulative savings for operations and support 
costs, and: 

* total savings of about 21 percent in overall life cycle costs. 

While sole-source competitions have been the general rule for engine 
program strategies, evidence shows that when competition was utilized 
for even part of those programs, positive outcomes were often realized. 
Other than the Great Engine War, there have been a number of U.S. 
competitions for modern fighter engines, including those for the F-15, 
F/A-18, and F-22A fighter aircraft. During the course of this review, 
government and contractor personnel told us that the difference between 
these programs and the F-16 was that competition was limited to only 
one phase of the program (i.e., program initiation or production 
phase). For example, the General Electric F404 engine, which today 
powers the Navy F/A-18 aircraft and the Air Force F-117A aircraft, was 
competed in the mid-1980s. In that case, the Navy had decided to 
upgrade the A-6 aircraft to the A-6F model with two F404 engines, 
thereby increasing the number of F404 engines in the fleet. The Navy 
leadership recommended a second source for that engine, and Pratt & 
Whitney was awarded a "build-to-print" contract, which meant it would 
produce additional F404 engines according to the General Electric 
design. While this competition did provide some improvements in 
contractor responsiveness, government and contractor officials told us 
this was not an optimum competitive environment as it provided no 
design competition. 

The Great Engine War was able to generate significant benefits because 
competition incentivized contractors to improve designs and reduce 
costs during production and sustainment. Competitive pressure continues 
today as the F-15 and F-16 aircraft are still being sold 
internationally. While the other competitions resulted in some level of 
benefits, especially with regard to contractor responsiveness, they did 
not see the same levels of success absent continued competitive 
pressures. 

JSF Program Could Have Long-term Impact on Industrial Base: 

The economic stakes in the JSF engine program are likely to be high 
given the size of the program, international participation, and the 
expected supplier base. Participation in the development, production, 
and support of the JSF engine program will position Pratt & Whitney, 
the Fighter Engine Team, and their respective supplier base to compete 
for future military development and acquisition programs. According to 
government officials, Pratt & Whitney faces a decline in the area of 
large commercial engines, which could result in a shift of workforce 
and overhead costs to military programs. While it is the sole-source 
provider of the engine for the Air Force F-22A aircraft, production 
will likely end in 2012 for that program. Pratt & Whitney will at a 
minimum provide at least some of the engines for the JSF program, the 
extent to which is to be determined by whether or not the Fighter 
Engine Team remains a competitor and, if so, the amount of contract 
awards that company can win. Should the JSF program suffer substantial 
schedule slips beyond 2011 or 2012, the gap between the end of F-22A 
production and the onset of JSF production could grow, resulting in 
workforce disruptions or other negative effects. 

General Electric is a significant entity in the market for large 
commercial engines. However, the company faces declining production 
within its other fighter engine programs, such as the Navy's F/A-18E/F, 
which could result in erosion of specialized skills should the company 
not continue as a participant in the JSF program. While the overall 
health of the company is very strong, business decisions as to where to 
invest company resources could favor the commercial side, should 
military business decline substantially. 

Due to the size of the JSF program, the industrial base implications 
reach far beyond Pratt & Whitney and the Fighter Engine Team. With JSF 
contracts awarded to suppliers within both the U.S. and international 
partner countries, JSF propulsion production and support business will 
contribute to the global engine industrial base for almost 60 years. 
While companies that participate are likely to see increased business 
opportunities, if the JSF comes to dominate the market for tactical 
aircraft, as DOD expects, companies that are not part of the program 
could see tactical aircraft business decline. 

Concluding Observations: 

DOD officials noted in 2006 that canceling the F136 engine program 
would save DOD $1.8 billion in needed investments over the remaining 7 
years of development, which could be used to fund higher-priority 
programs. According to our analysis that figure is now $1.4 billion; 
and does not include the approximately $2.2 billion to $3.1 billion of 
additional investments for procurement, production support, and stand- 
up investments necessary for competition. However, our analysis 
indicates that this investment may be recouped under a competitive 
approach if it generates savings of 10.3 to 12.3 percent. Historical 
data indicate that it is reasonable to assume savings of that much and 
more. Choices made today will ripple forward and influence additional, 
and perhaps even more challenging, decisions in the future. The JSF 
engine acquisition strategy is one such choice facing DOD today. The 
results of our work indicate that with the proper structure and 
attention, and the up-front investments, the alternate engine can 
ultimately recover those investments and potentially provide additional 
benefits to the program. Prior engine programs and more recent DOD 
studies and analyses also suggest these outcomes to be reasonable. DOD 
is now faced with prioritizing its short-term needs against potential 
long-term payoffs through competition for JSF engine development, 
procurement, and sustainment. 

Mr. Chairmen, this concludes my prepared statement. I will be happy to 
answer any questions you or other members of the subcommittee may have. 

Contacts and Acknowledgments: 

For future questions regarding this testimony, please contact Michael 
J. Sullivan, (202) 512-4841. Individuals making key contributions to 
this testimony include Brian Mullins, Assistant Director; J. Kristopher 
Keener; Daniel Novillo; Greg Campbell; Charles Perdue; and Adam 
Vodraska. 

GAO Related Products: 

Joint Strike Fighter: Progress Made and Challenges Remain, GAO-07-360. 
Washington, D.C.: Mar. 15, 2007. 

Tactical Aircraft: DOD's Cancellation of the Joint Strike Fighter 
Alternate Engine Program Was Not Based on a Comprehensive Analysis, GAO-
06-717R. Washington, D.C: May 22, 2006. 

Recapitalization Goals Are Not Supported By Knowledge-Based F-22A and 
JSF Business Cases, GAO-06-487T. Washington, D.C.: Mar. 16, 2006. 

Joint Strike Fighter: DOD Plans to Enter Production before Testing 
Demonstrates Acceptable Performance, GAO-06-356. Washington, D.C.: Mar. 
15, 2006. 

Tactical Aircraft: F/A-22 and JSF Acquisition Plans and Implications 
for Tactical Aircraft Modernization, GAO-05-519T. Washington, D.C.: 
Apr. 6, 2005. 

Defense Acquisitions: Assessments of Selected Major Weapon Programs, 
GAO-05-301.Washington, D.C.: Mar. 31, 2005. 

Tactical Aircraft: Opportunity to Reduce Risks in the Joint Strike 
Fighter Program with Different Acquisition Strategy, GAO-05-271. 
Washington D.C.: Mar. 15, 2005. 

Tactical Aircraft: Status of F/A-22 and JSF Acquisition Programs and 
Implications for Tactical Aircraft Modernization, GAO-05-390T. 
Washington, D.C.: Mar. 3, 2005. 

Joint Strike Fighter Acquisition: Observations on the Supplier Base, 
GAO-04-554. Washington, D.C.: May 3, 2004. 

Joint Strike Fighter Acquisition: Managing Competing Pressures Is 
Critical to Achieving Program Goals, GAO-03-1012T. Washington, D.C.: 
July 21, 2003. 

[End of section] 

Appendix I: Scope and Methodology: 

In conducting our analysis of costs for the Joint Strike Fighter (JSF) 
engine program, we relied primarily on program office data. We did not 
develop our own source data for development, production, or sustainment 
costs. In assessing the reliability of data from the program office, we 
compared that data to contractor data and spoke with agency and other 
officials and determined that the data were sufficiently reliable for 
our review. 

Other base assumptions for the review are as follows: 

* Unit recurring flyaway cost includes the costs associated with 
procuring one engine and certain nonrecurring production costs; it does 
not include sunk costs, such as development and test, and other costs 
to the whole system, including logistical support and construction. 

* Engine procurement costs reflect only U.S. costs, but assumes the 
quantity benefits of the 646 aircraft currently anticipated for foreign 
partner procurement. 

* Competition, and the associated savings anticipated, begins in fiscal 
year 2012. 

* Engine maturity, defined as 200,000 flight hours with at least 50,000 
hours in each variant, is reached in fiscal year 2012. 

* Two years are needed for delivery of aircraft. 

* Aircraft life equals 30 years at 300 flight hours per year. 

For the sole-source Pratt & Whitney F135 engine scenario, we calculated 
costs as follows: 

Development: 

* Relied on JSF program office data on the remaining cost of the Pratt 
& Whitney development contract. We considered all costs for development 
through fiscal year 2007 to be sunk costs and did not factor them into 
analysis. 

Production: 

* For cost of installed engine quantities, we multiplied planned JSF 
engine quantities for U.S. aircraft by unit recurring flyaway costs 
specific to each year as derived from cost targets and a learning curve 
developed by the JSF program office. 

* For the cost of production support, we relied on JSF program office 
cost estimates for initial spares, training, support equipment, depot 
stand-up, and manpower related to propulsion. Because the JSF program 
office calculates those numbers to reflect two contractors, we applied 
a cost reduction factor in the areas of training and manpower to 
reflect the lower cost to support only one engine type. 

Sustainment: 

* For sustainment costs, we multiplied the planned number of U.S. 
fielded aircraft by the estimated number of flight hours for each year 
to arrive at an annual fleet total. We then multiplied this total by 
JSF program office estimated cost per engine flight hour specific to 
each aircraft variant. 

* Sustainment costs do not include a calculation of the cost of engine 
reliability or technology improvement programs. 

For a competitive scenario between the Pratt & Whitney F135 engine and 
the Fighter Engine Team (General Electric and Rolls-Royce), we 
calculated costs as follows: 

Development: 

* We used current JSF program office estimates of remaining development 
costs for both contractors and considered all costs for development 
through fiscal year 2007 to be sunk costs. 

Production: 

* We used JSF program office data for engine buy profiles, learning 
curves, and unit recurring flyaway costs to arrive at a cost for 
installed engine quantities on U.S. aircraft. We performed calculations 
for competitive production quantities under 70/30 and 50/50 production 
quantity award scenarios. 

* We used JSF program office cost estimates for production support 
under two contractors. We assumed no change in support costs based on 
specific numbers of aircraft awarded under competition, as each 
contractor would still need to support some number of installed engines 
and provide some number of initial spares. 

Sustainment: 

* We used the same methodology and assumptions to perform the 
calculation for sustainment costs in a competition as in the sole- 
source scenario. 

Savings: 

* We analyzed actual cost information from past aircraft propulsion 
programs, especially that of the F-16 aircraft engine, in order to 
derive the expected benefits of competition and determine a reasonable 
range of potential savings. 

* We applied this range of savings to the engine life cycle, including 
recurring flyaway costs, production support, and sustainment. We 
assumed costs to the government could decrease in any or all of these 
areas as a result of competitive pressures. 

* We did not apply any savings to the system development and 
demonstration phase or the first five production lots because they are 
not fully competitive. However, we recognize that some savings may 
accrue as contractors prepare for competition. 

In response to the request to present our cost analyses in constant 
dollars, then year dollars, and using net present value, we: 

* calculated all costs using constant fiscal year 2002 dollars, 

* used separate JSF program office and Office of the Secretary of 
Defense inflation indices for development, production, production 
support, and sustainment to derive then year dollars; when necessary 
for the out years, we extrapolated the growth of escalation factors 
linearly; and: 

* utilized accepted GAO methodologies for calculating discount rates in 
the net present value analysis. 

No cost analysis was performed for the scenario where a fixed-price 
contract would be awarded in fiscal year 2008 for the entire life of 
the engine program because neither the contractor nor the Department of 
Defense calculates the necessary cost data. During our discussions with 
both DOD officials and contractor representatives, it was determined 
that neither viewed a fixed-price contract as a viable option for which 
they could quantify a risk premium. 

We did not perform cost analyses of alternative strategies, as we 
determined no other alternative could be implemented without disruption 
to the JSF program's cost and schedule. 

Our analysis of the industrial base does not independently verify the 
relative health of either contractors' suppliers or workload. 

FOOTNOTES 

[1] Pub. L. No. 109-364, 120 Stat. 2083, 2117-2119 (2006). 

[2] Unless otherwise noted, all dollars in this report are fiscal year 
2002 dollars. 

[3] Eight allied nations are also participating in the JSF program: 
United Kingdom, Norway, Denmark, the Netherlands, Canada, Italy, 
Turkey, and Australia. 

[4] Prior to this contract, DOD had invested $722 million in the 
alternate engine program. 

[5] The Fighter Engine Team is a single company, created in July 2002 
by General Electric and Rolls-Royce, and formed for the development, 
deployment, and support of the F136 engine for the JSF program. 

[6] A learning curve represents the relationship between the unit cost 
of an item and the cumulative production quantity of that item. 

[7] In conducting our cost analysis of the alternate engine program, we 
presented the cost of only the U.S. aircraft currently expected for 
production (2,443). These costs assume the quantity benefits of the 646 
aircraft currently anticipated for foreign partner procurement. 

[8] Our review of DOD data as well as discussions with defense and 
industry experts, confirmed this as a reasonable range of potential 
savings to consider. 

[9] These savings amounts reflect net present value calculations that 
discount costs and savings for both inflation and the time value of 
money. 

[10] The F135 engine is a derivative of the F119 engine, which means 
many of the same or similar parts and processes are used to manufacture 
both engines. It also means that the F135 can benefit from lessons 
learned or be susceptible to any systemic problems associated with the 
F119. 

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