A quick summary:
US government auditors monitoring the F-35 Joint Strike Fighter programme have warned that Lockheed Martin expects delays of aircraft deliveries will continue for at least another year. The Defense Contracts Management Agency (DCMA) also has expressed fears Lockheed Martin will never fully recover, citing parts shortage trends indicating the F-35 assembly line in Fort Worth, Texas, "will not be able to achieve or sustain [full] rate production".The reports show Lockheed's biggest manufacturing problem is the F-35's wing, a fact the company has long acknowledged. Here's more from the story.
Severe shortages of parts have forced Lockheed to send incomplete wings to a mating fixture, which joins the four major wing structures to the fuselage. Even after the missing parts arrive, finishing the wings inside the mating fixture is more difficult, which extends the delay.The reports are a wealth of data. Here are some highlights, including several points that didn't fit inside the news story.
Lockheed has previously said that many of the parts shortages were caused by the 2004 redesign. As part of an effort to save up to 1,360kg (3,000lb), Lockheed introduced stricter manufacturing tolerances knowing many suppliers would need several years to achieve them.
- July 2007: Five potential suppliers rejected Lockheed's design for the F-35A gun port access panel, each calling Lockheed's design too complex to manufacture.
- July 2007: The Honeywell integrated power pack failed on the test stand, even as the AA-1 flight test article was already grounded. The DCMA noted these examples, along with "risks associated with concurrent development, elevate concerns and jeopardize [redacted] the flight test program schedule."
- August 2007: DCMA found that Lockheed "is not following, nor consistently applying [earned value management system, or EVMS] guidelines". The report adds: "The utility of EVMS has declined to a level where it does not serve its intended purpose and the government is not obtaining useful program performance data to anticipate and mitigate program risks."
- December 2007: "There is a high risk of not meeting the 400hr system level mean-time-between-failure requirement by the end of [system development and demonstration, or SDD]. As risk mitigation, [redacted] had budgeted methods of 'growing' reliability earlier than originally planned, but cost constraints resulted in LM Aero canceling the Reliability Growth Tests. These tests were the primary vehicle for improving MTBF during SDD."
- December 2008: "Seat anomalies were observed in the ejection sequence during an escape system sled test on 20 Nov 08, with two successive failures occurring during subsequent qualification testing. An investigation revealed that the ejection seat sequencer failed to function properly and the ejection seat operated in back-up mode. Data indicates a communications fault during sequencer power-up -- bench testing has shown that the sequencer is fully functional following the communications fault."
- December 2008: DCMA raised concerns about Lockheed's monthly spending rate, projecting the SDD budget will be depleted by Fiscal 2011.
- April 2009: "Present supplier delivery data/trends indicate LM Aero will not be able to achieve or sustain rate production of F-35 aircraft assembly, manufacturing sequence or DD-250 delivery dates."
- July 2009: "The Program has surpassed one year since the revised Program Master Schedule (6.1), which established an Over Target Baseline for cost and schedule, was implemented. An initial improvement in overall SDD planned versus actual activity completion performance was observed in May 2008 when MS 6.1 was implemented into the schedule. Over the last seven months, performance has averaged an approximate 40% completion rate. ... MS 6.1 does not appear to be achievable - there is a strong probability of Master Schedule realignment (MS 6.2?) currently under consideration."
- September 2009: "The volume of major [change requests, or CRs] is projected to continue. While much of this volume was anticipated within the program, the number of major changes and the disruption to the floor were not anticipated. ... Change as a result of design errors, assembly issues and integration issues were not anticipated as they have been seen."