Delco Electronics Corp. v. United States

35 Cont. Cas. Fed. 75,679, 17 Cl. Ct. 302, 1989 U.S. Claims LEXIS 120, 1989 WL 68472
United States Court of Claims·Decided June 23, 1989·No. No. 97-86C·Published·Cited by 28 cases

Opinion

OPINION

MARGOLIS, Judge.

Plaintiff Delco Electronics Corporation seeks to recover $31.5 million as a total equitable adjustment on behalf of itself and three subcontractors under a contract with the Air Force. The defendant agrees that plaintiff is entitled to an equitable adjustment, but seeks to limit the amount to approximately $7.9 million. On May 22, 1987, .the court ruled that the plaintiff’s recovery was not limited to a not-to-exceed (NTE) offer of $14.2 million, a sum which the government has already paid, because the court determined that the government failed to accept plaintiff’s NTE offer. That decision is reported at 12 Cl.Ct. 367.

A seven-day trial was held in Washington D.C. from September 14, 1988 until September 23, 1988. The parties introduced nearly 500 exhibits and provided over 1300 pages of transcribed testimony. After review of the entire record, the court finds that the weight of the evidence presented supports the plaintiff’s claims. The court finds that the plaintiff is entitled to a total equitable adjustment of $28,324,284. The plaintiff was already paid $14,219,000 of this amount. Accordingly, judgment will be entered in favor of the plaintiff for $14,105,284 plus interest.

' FACTS

A. The FSA/CAS Contract

On December 14, 1981, the Air Force awarded General Motors Corporation con[305] tract F34601-82-C-0180 for design and production of a Fuel Savings Advisory and Cockpit Avionics System for KC-135 and other -135 aircraft (the FSA/CAS contract). The contract was subsequently transferred to Delco Electronics Corporation, a division of General Motors. One of the principal components of the system to be provided by Delco under the FSA/CAS contract was the Integrated Fuel Management and Center of Gravity System (IFM/CGS) referred to herein as the “fuel panel.”

Delco subcontracted portions of the work to be performed under the FSA/CAS contract. Delco entered into a subcontract with Gull, Inc. (Gull) to design and manufacture the fuel panel, as well as the Tank Interface Unit (TIU) and the Remote Display Unit (RDU). Delco entered into a subcontract with Electrospace Systems, Inc. (ESI) to provide the “Group A” kits which consisted of the wiring, cables, brackets, and installation and mounting hardware, necessary for installation of the FSA/CAS equipment into various configurations of aircraft. Delco entered into a subcontract with Rockwell International Corporation-Collins Government Avionics Division (Collins) to design and manufacture the Integrated Control and Display Unit (ICDU) and the Bus System Interface Unit (BSIU).

Delco itself designed and manufactured the Fuel Savings Advisory System computer (FSAS computer). Delco also designed and manufactured test equipment, reviewed and supervised the work of its subcontractors, and acted as the system integrator. Delco’s efforts were carried out at its facilities in both Milwaukee, Wisconsin and Santa Barbara, California.

B. The Initial Fuel Panel Change

At a system design review in January 1982 (less than one month after award of the contract), the Air Force advised Delco that it had decided to relocate a radar scope to the area of the cockpit that was to have been occupied by the fuel panel, and to provide space for a second ICDU. This change resulted in a reduction in the space available for the fuel panel and necessitated a major redesign of the fuel panel. The Air Force requested that Delco provide a proposal to perform the required redesign of the fuel panel for a NTE price. On March 5,1982, the Air Force issued Modification (Mod) P00002. Mod P00002 was an acceptance of Delco’s offer to perform the change for a NTE price, and provided that the definitized price for the fuel panel change would not exceed $4,612,606 for the current contract quantity and $5,763,410 for the quantities of Option II and Option III, which were not yet exercised.

Mod P00002 authorized Delco to perform the complete fuel panel change including engineering design, procurement of parts, and production of the redesigned fuel panel, and committed the Air Force to pay Delco for the changed work up to the NTE price. Mod P00002 added $2,968,343 in funds to the contract and eliminated certain other contract requirements in the amount of $1,644,263, thereby providing that $4,612,606 was available to pay Delco for the fuel panel changes up to the NTE price for the then current quantity. Pursuant to Mod P00002, Delco and its subcontractors began design and engineering work on a modified fuel panel. From April 27, 1982 through May 4, 1982, Delco and the Air Force conducted a preliminary design review (PDR) of the entire FSA/CAS program. As part of the PDR, Gull presented the preliminary designs for the fuel panel as changed by Mod P00002.

The fuel panel to be provided under the FSA/CAS contract as originally awarded consisted of a single Line Replaceable Unit (LRU). This original single LRU fuel panel was a derivation of fuel quantity gauging units sold commercially by Gull for McDonnell Douglas DC-8 and MD-80 airliners. The original fuel panel contained a single microprocessor for computation of the aircraft center of gravity. The fuel management functions were not microprocessor controlled. Instead, the original fuel panel contained ten identical discrete circuit cards, each of which controlled the fuel management functions and information display for a single fuel tank on the aircraft. The reduced space in the cockpit pedestal [306] resulting from the relocation of the radar scope required that the microprocessor and associated circuitry needed for computation of the aircraft center of gravity be relocated to a second LRU denominated the Center of Gravity Control Unit (CGCU). Delco and the Air Force agreed that the CGCU would be located in the nose wheel well of the aircraft.

C. The Revised Fuel Panel Change

In July 1982, it was determined that a further reduction in the size of the fuel panel was required in order to accommodate the wider throttle quadrant in the KC-135E version of the -135 aircraft. This change, among other things, required the relocation of equipment and the installation of additional sophisticated data transmission circuits. At a meeting on July 14, 1982, the Air Force selected a new layout for the Integrated Fuel Management Panel (IFMP) to accommodate the wider throttle quadrant. This second redesign has been referred to as the “revised fuel panel change.”

As a result of the discovery of the wider throttle quadrant, the Air Force and Delco agreed that Mod P00002 would be deleted and a new modification issued encompassing all of the changes to the fuel panel. By telegram dated July 16, 1982, Delco proposed that Mod P00002 be cancelled and that a new unpriced modification to cover the revised fuel panel be issued for a total NTE price of $17,746,000.

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Delco Electronics Corp. v. United States, 35 Cont. Cas. Fed. 75,679, 17 Cl. Ct. 302, 1989 U.S. Claims LEXIS 120, 1989 WL 68472 (cc 1989).

35 Cont. Cas. Fed. 75,679 (Delco Electronics Corp. v. United States) — published by Counsel Stack Legal Research, free access to 12M+ legal documents.

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