Spartan Aircraft Co. v. United States

100 F. Supp. 171, 120 Ct. Cl. 327, 1951 U.S. Ct. Cl. LEXIS 79
CourtUnited States Court of Claims
DecidedOctober 2, 1951
Docket48689
StatusPublished
Cited by6 cases

This text of 100 F. Supp. 171 (Spartan Aircraft Co. v. United States) is published on Counsel Stack Legal Research, covering United States Court of Claims primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Spartan Aircraft Co. v. United States, 100 F. Supp. 171, 120 Ct. Cl. 327, 1951 U.S. Ct. Cl. LEXIS 79 (cc 1951).

Opinion

LITTLETON, Judge.

On November 29, 1946, plaintiff and defendant entered into contract Na Ilr-1489. In consideration of prescribed unit prices plaintiff agreed to furnish the labor and materials for the inspection, repair, modification, and conversion of two twin-engine Beechcraft airplanes; referred to in our findings and in this opinion as NC 1064 and NC 1065, owned by the Bureau of Reclamation.

On December 24, 1946, the parties entered into another contract, No. Ur-1491, under which plaintiff agreed to resound-proof and reupholster the two planes for a total consideration of $2,217.04.

Plaintiff has been paid for neither contract and sues here for the contract price for each. There is no issue with respect to contract No. Ur-1491, the resoundproofing and reupholstering contract; defendant admits that plaintiff has fully performed this contract. However, defendant denies performance of contract No. Ilr-1489. Defendant has interposed a counterclaim alleging that as a result of plaintiff’s material breach of its contractual obligations under contract No. Ur-1489 and its failure to use due care and perform in a workmanlike manner, plane NC 1064 was forced to make an emergency landing and was damaged as a result. The counterclaim asks judgment for the amount of the damage.

By March 23, 1947, plaintiff had finished working on NC 1064 and it was redelivered to defendant. Between that date and April •21, 1947, the plane was flown by defendant on thirteen separate days. On April 21, 1947, while en route from Santa Fe to Albuquerque, New Mexico, the engines failed and the plane was forced to make an emergency landing. The details are set out in our findings. The engines’ failure was caused by a stoppage of fuel resulting from a parting during flight of a fuel line'fitting just aft of the firewall in the plane’s right wheel well. We have described this L-shaped fitting and the B-nut which engaged it in our findings. The line broke when the B-nut worked loose from the L-shaped fitting.

Defendant contends that plaintiff failed properly to inspect this fitting-before the plane left its plant. Item 3 of the contract required plaintiff to perform a 100-hour inspection in accordance with an attached check list and to correct all unsatisfactory conditions founU In the section of the check list entitled “Fuel and Oil Systems” was the following: “Fuel Lines: With fuel ‘On’ and pressure built up, inspect fuel lines and connections for leaks, cracks, security of anchorage, chafing, tight *173 ness and condition of hose connections and hose clamps.”

It is our finding that plaintiff followed customary procedure -in performing the “Fuel and Oil Systems” section of the 1 Off-hour inspection.

Defendant has sought to prove that the B-nut was only partially engaged, to the extent of only 3 to 3V4 threads, when plane NC 1064 left plaintiff’s plant, or, alternatively, that the B-nut was fully engaged but liandtight only. A 13-nut is not suitable for operation unless it is wrenchtight. However, it is possible for even a wrenchtight B-nut to vibrate loose from its connection.

We find the evidence insufficient to establish that the B-nut was only partially engaged when the plane left plaintiff’s plant. The wobble pump test and the other tests made of the fuel system, by plaintiff and later by defendant’s pilot and mechanic, negative this possibility. On the other hand, the evidence is not sufficient to enable us to find as a fact that the 13-nut was wrenchtight when the plane left plaintiff’s plant. However, a conclusion that it was wrenchtight at that time is at least as reasonable as a conclusion that it was only liandtight. It is not the practice during a 100-hour inspection to use a wrench on every B-nut in the fuel system. Plaintiff’s employees did not use a wrench to tighten this fitting. There is no evidence that they disconnected or loosened it. However, plaintiff’s inspector felt the nut with his hand, tried to loosen it, and found that he was unable to turn it.

If the B-nut was only partially engaged, or fully engaged but liandtight only, it was up to defendant to prove it. The suit, after all, is on the contract. Plaintiff has shown completion of the work, redelivery of the plane to defendant, acceptance of it by defendant, and use of it thereafter by defendant. This is more than enough to make out a prima facie case of performance. The burden of establishing a breach and the burden of proving that the breach caused the damage to which the counterclaim is addressed were on the Government. Under the circumstances we must hold for plaintiff. See Uncas National Bank v. United States, 18 Ct.Cl. 349; Morrison v. Le Tourncau Co. of Georgia, 5 Cir., 138 F.2d 339. The counterclaim is directed in terms solely to the damage to plane NC 1064; it must be dismissed.

With respect to the other plane, NC 1065, however, defendant has proved four items of faulty performance. On one side of the torque shaft of the lauding gear mechanism one bolt was missing and another was loose. A pump in the anti-icer system was clogged. Plaintiff failed to replace cracked and weathered hose in the oil lines in both wheel wells. The installation of on'e o f the rudder trim tab control cables was faulty. Each of these defects was a violation of Item 3 of the contract which required plaintiff to perform a 100-hour inspection and correct all unsatisfactory conditions found.

While plaintiff denied that these defects existed, it argued that if they were found to have existed, defendant’s allowance therefor should be merely the cost of remedying them. Neither party sought to prove by evidence the cost of remedying any or all of these defects on plane NC 1065. In its exceptions to the Commissioner’s report and in the brief plaintiff contended that the cost would not exceed $100.

Defendant raises the question of whether, the contract being considered indivisible both as to the two planes and as to the fourteen separate items for each plane, the result of the four defects on NC 1065 should not be that plaintiff recovers nothing on contract No. Ilf-1489. We note, however, that defendant concludes its brief with the assertion that it is entitled to judgment in the sum of $24,102 (the alleged cost of repairing the damage to NC 1064) plus $6,191.58 (that part of the contract price allocable to performance of Item 3 on NC 1065), against which defendant would allow plaintiff the contract prices of the two contracts, or $24,430.30 plus $2,217.04.

The severability, or divisibility, of a contract is a vexing problem. See, for example, the annotations at 147 A.L.R. 933; 71 A.L.R. 479; 2 A.L.R. 686; and 2 A.L.R. 643. See also Willision on Contracts (Rev. Ed., 1936) §§ 860A-863. The authorities *174 hold that the question is essentially one of the intention of the parties;- examination of some of the many cases orí the point suggests rather that resolution of the question has more commonly been a matter of the intention of the court.

Contract No. Ilr-1489 obligated plaintiff to — “perform all work and furnish parts required to place the airplanes in as nearly perfect operating condition as is possible.”

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Bluebook (online)
100 F. Supp. 171, 120 Ct. Cl. 327, 1951 U.S. Ct. Cl. LEXIS 79, Counsel Stack Legal Research, https://law.counselstack.com/opinion/spartan-aircraft-co-v-united-states-cc-1951.