Military Aircraft Parts

Armed Services Board of Contract Appeals·Decided May 31, 2016·No. ASBCA No. 60009·Published

Opinion

ARMED SERVICES BOARD OF CONTRACT APPEALS

Appeal of -- ) ) Military Aircraft Parts ) ASBCA No. 60009 ) Under Contract No. SPM4A7-l l-M-Dl 11 )

APPEARANCE FOR THE APPELLANT: Mr. Robert E. Marin President

APPEARANCES FOR THE GOVERNMENT: Daniel K. Poling, Esq. DLA Chief Trial Attorney Edward R. Murray, Esq. Jason D. Morgan, Esq. Trial Attorneys DLA Aviation Richmond, VA

OPINION BY ADMINISTRATIVE JUDGE O'SULLIVAN

Military Aircraft Parts (MAP) appeals from a contracting officer's final decision denying its claim for breach of contract. The parties have submitted the appeal for decision on the written record pursuant to Board Rule 11. 1 Both entitlement and quantum are at issue. We have jurisdiction pursuant to the Contract Disputes Act of 1978 (CDA), 41 U.S.C. §§ 7101-7109. We sustain the appeal in part.

FINDINGS OF FACT

1. Purchase Order No. SPM4A7-l l-M-Dl 11 (the contract) was issued by the Defense Logistics Agency Aviation (DLA Aviation) field office, Richmond, Virginia, to MAP on 18 November 2010 (R4 tab 1). The government sought to acquire one first article and six production units of a steel flap track liner for the A-10 aircraft (id. at 3, 8-10). The contract identifies this part as a Critical Application Item (id. at 4 ). The total price of the contract, for first article manufacture and testing and six production parts, was $7,550.00 (id. at 1). Section B of the contract contains first article testing instructions, which provide in pertinent part:

5. MATERIAL PROCESSING, INCLUDING FINISH REQUIREMENTS (PLATING, CASTING, FORGING,

1 MAP originally elected to proceed under Board Rule 12.2, small claims expedited procedure. MAP subsequently elected to remove the appeal from the Board's Rule 12 docket in order to extend the time available for discovery. HEAT TREATMENT, WELDING, INSPECTION, ANODIZE, PAINTING, ETC.) UTILIZED IN THE MANUFACTURE OF FIRST ARTICLE ITEMS SHALL BE IDENTIFIED AND CERTIFIED ALONG WITH A COPY OF MATERIAL PURCHASE REQUESTS AS CONFIRMING TO APPLICABLE DATA REQUIREMENTS. A COPY OF THE PURCHASE ORDER CERTIFYING THE PROCESS ACCOMPLISHED AT OTHER THAN CONTRACTOR FACILITY SHALL BE INCLUDED.

(Id. at 3) The applicable drawings specify the application of cadmium plating and epoxy-polyamide primer as part of the manufacturing process (R4, tab 19 at 7).

2. The contract contained the Federal Acquisition Regulation (FAR) 52.209-4, FIRST ARTICLE APPROVAL-GOVERNMENT TESTING (SEP 1989) clause, with its AL TERNA TE I (JAN 1997). The clause provides in pertinent part:

(b) Within 120 calendar days after the Government receives the first article, the Contracting Officer shall notify the Contractor, in writing, of the conditional approval, approval, or disapproval of the first article. The notice of conditional approval or approval shall not relieve the Contractor from complying with all requirements of the specifications and all other terms and conditions of this contract. A notice of conditional approval shall state any further action required of the Contractor. A notice of disapproval shall cite reasons for the disapproval.

(c) If the first article is disapproved, the Contractor, upon Government request, shall submit an additional first article for testing. After each request, the Contractor shall make any necessary changes, modifications, or repairs to the first article or select another first article for testing. All costs related to these tests are to be borne by the Contractor, including any and all costs for additional tests following a disapproval. The Contractor shall furnish any additional first article to the Government under the terms and conditions and within the time specified by the Government. ...

(d) If the Contractor fails to deliver any first article on time, or the Contracting Officer disapproves any first article, the Contractor shall be deemed to have failed to

2 make delivery within the meaning of the Default clause of this contract.

(h) Before first article approval, the acquisition of materials or components for, or the commencement of production of, the balance of the contract quantity is at the sole risk of the Contractor. Before first article approval, the costs thereof shall not be allocable to this contract for (1) progress payments, or (2) termination settlements if the contract is terminated for the convenience of the Government.

(R4, tab 1 at 14)2 The contract also contains a DLA clause with additional requirements, 52.209-9018, FIRST ARTICLE - GOVERNMENT TEST-ADDITIONAL REQUIREMENTS (SEP 2008) DLAD (id.).

3. The contract required delivery of the first article to the government for testing by 17 May 2011, 180 days after award (R4, tab 1 at 2). It is undisputed that MAP did not deliver the first article by this date; the first article was delivered to the government for testing on 30 January 2012 (R4, tab 37). 3 Government testing of MAP's first article resulted in a discrepancy report that was attached to a notice provided by the contracting officer to MAP on 15 May 2012 that its first article was disapproved (R4, tabs 4, 5). The only discrepancy noted after testing and inspection was with respect to the holes drilled in the part to facilitate its attachment to the flap track-the contract called for the holes to be .190" to .194" in diameter, but the report stated that the actual diameter was ".195 - .196 [in] twelve places" (id.). 4

4. The government's structures engineer who replaced the engineer responsible for reviewing the first article submitted by MAP is familiar with the A-10 wing flap system and provided the following general information about the holes in the flap liner. Aircraft mechanics use the 12 holes to mount the liner, with fasteners, to an underlying aluminum section which is traversed by the roller that extends and retracts the wing flaps of the aircraft. If the liner were not securely fastened and were to detach from the mating section below, the roller would be likely to damage that section and potentially cause the wing flap not to operate correctly. In addition, if the

2 FAR 52.209-4 is not set forth in full text in the contract document. 3 The record before us does not indicate that the government took any action with respect to the missed delivery date. There is no indication that a new delivery date was ever established. 4 A second discrepancy with respect to the certification package was corrected on 14 May 2012 (id.). 3 liner holes are too large, the mechanic attaching the liner may not be able to use it as a template for drilling holes in the mating part and may not be able to use the specified fasteners. (Gov't br., ex. A, Casey Thurber decl. (Thurber decl.) iii! 1-4) However, the government has presented no evidence that the nonconforming holes in MAP's first article were large enough to actually present the potential problems described.

5. At MAP's request, quality assurance representatives (QARs) Randall Fritz and Greg Keeler from the Defense Contract Management Agency (DCMA) visited MAP's facility on 20 June 2012 to witness an inspection of the returned part (gov't br., ex. C, Randall Fritz decl. (Fritz decl.) iii! 2, 3). Contrary to the discrepancy report, only 3 (out of 12 total) holes were found to be out oftolerance-i.e., measuring .195" to .196" in diameter (R4, tab 6). The remainder measured .190" to .194" in diameter (R4, tab 40). At the time, Mr. Marin of MAP pointed out that the out-of-tolerance holes were missing paint, and stated that this condition could have been caused by forcing gauge pins 5 through the holes, thereby removing the paint and enlarging the holes (Fritz decl. ii 5). Mr. Fritz responded that Mr.

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