Hawaiian Airlines, Ltd. v. United States

139 F. Supp. 942, 134 Ct. Cl. 675, 1956 U.S. Ct. Cl. LEXIS 94
CourtUnited States Court of Claims
DecidedApril 3, 1956
DocketNo. 144-52
StatusPublished

This text of 139 F. Supp. 942 (Hawaiian Airlines, Ltd. 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
Hawaiian Airlines, Ltd. v. United States, 139 F. Supp. 942, 134 Ct. Cl. 675, 1956 U.S. Ct. Cl. LEXIS 94 (cc 1956).

Opinion

Jones, Chief Judge,

delivered the opinion of the court:

This case is before the court under a special act, the text of which is set out in finding 1.

It authorizes the court to hear, determine and render judgment on a claim for damages to a Douglas DC-3 airplane owned by plaintiff on June 16,1942, caused by a United States Army plane during a takeoff while the Douglas plane was lawfully parked at the John Kodgers Airport in the Territory of Hawaii. Liability is to be determined “upon the same principles and measures of liability as in like cases between private parties.”

Following the attack on Pearl Harbor on December 6,1941, the Governor of Hawaii issued a proclamation placing all territorial airports under the control of the United States Armed Forces. Commercial airlines were permitted to continue operations to a restricted degree under the supervision of the Armed Forces.

The plaintiff had been operating as an inter-island air carrier since 1929, using the John Rodgers Airport as its starting point. Before the proclamation the airport had been operated and maintained by the Department of Public Works of the Territory.

During the year 1942, the Army constructed a runway the first section of which was some 2,800 feet long, with a rock base, covered with sand rolled with an oil binder. None of it was paved. It had also added at the west end of the first section a 700- or 800-foot extension, made of coral and dirt fill. The use of the extension was restricted to military aircraft. Plaintiff’s planes were permitted the use of only the first section.

The area in which plaintiff’s DC-3 was parked at the time of the collision had been used continuously by the Hawaiian Airlines as a passenger-loading area since 1929. The nearby passenger terminal was a building owned by plaintiff. The building was separated from the loading area by a fence with a gate through which passengers could walk to the waiting aircraft.

[677]*677Lines had been painted on the pavement to designate the proper parking position. Plaintiff’s plane was within the designated area. It was not on or near the runway. Planes taking off on the runway and. using the extension would miss the waiting plane by 200 to 300 feet. Fortunately loading had not started on plaintiff’s plane at the time of the collision although it was scheduled to leave within a few minutes.

At about 8: 00 a. m. on June 16, 1942, the army plane involved began its takeoff with a pilot, a copilot and several passengers who were a part of the Army or civilian employees of the Army. They were to be flown to another part of the same island. The army plane was a C-33. The corresponding commercial plane of the same type was DC-2.

After proceeding for about 800 feet in the line of the takeoff the left wheel of the airplane apparently struck a shallow pool of rainwater, collected on the runway. The airplane started turning to the left off the runway and toward the Hawaiian Airlines’ passenger station and loading area where plaintiff’s DC-3 was parked. At the time the army plane started to turn left the distance to where plaintiff’s DC-3 was parked was still 900 to 1,000 feet, a distance greater than the plane had traveled after the beginning of the takeoff. The collision could have been avoided by immediately discontinuing the takeoff which would have enabled the plane to stop before reaching the DC-3.

Evidently the pilot’s emphasis was on regaining the runway so as to continue his takeoff without interruption rather than stopping the plane and starting the takeoff anew. He increased the speed to about 75 miles and by applying full right brakes and rudder, advancing the left throttle and retarding the right throttle, attempted to control the plane and get it back on the runway. He did not succeed.

Soon after becoming airborne the landing gear and underside of the army plane hit the nose section of the DC-3 demolishing the cockpit and forward part of the fuselage and knocking the engine on the right side of the DC-3 from its mountings. The impact caused the army plane to crash to the cement pavement about 100 feet beyond the DC-3 in the direction of a building known as Hangar No. 2, the wing tip hitting an ambulance that was parked between the DC-3 and [678]*678the hangar. Fire broke out immediately which resulted in the destruction of the army airplane. All the occupants succeeded in escaping without serious injury. The army plane probably would have crashed into the hangar if it had not been forced to the ground as a result of the collision.

At the time the wind was very light, being from the southeast at about 3 miles per hour, which is practically no wind. Under such conditions the pilot may choose his takeoff direction. The weather was good with no obstruction to visibility or to the army pilot’s ability to observe the presence of plaintiff’s DC-3 parked in front of the airline’s passenger terminal. It had rained during the night and there were shallow puddles of water standing in various places along the surface of the runway and parking areas, which was normal after a rain. It was customary and not regarded as unsafe to conduct operations with such puddles on the runway. Neither the pilot nor the copilot in the written statements which they prepared on the day of the accident referred to the presence of the puddles or as to the condition of the runway having caused or contributed to the accident. The pilot’s subsequent statement to the Army Accident Classification Committee referred to the puddles without specifically assigning that condition as the cause of the accident. The pilot, however, at the hearing before the trial commissioner attributed the accident to the shallow puddle of water. The copilot did not do so.

Both the pilot and the copilot were second lieutenants, the pilot having had a total of 600 hours flying time, and the copilot about 400 hours. The copilot, however, had never flown a 2-engine aircraft.

The army pilot had authority, if he believed the takeoff could not be safely accomplished, to discontinue or abandon it, or he could have obtained permission to make the takeoff without using the runway extension.

The Army Accident Classification Committee made a report in which they absolved the pilot from any blame. For some reason at the time the investigation was made the Committee did not talk to nor secure the evidence of the officer who was in charge of the field.

[679]*679The facts as disclosed by the record as a whole preclude any other reasonable conclusion than that the damages to the plaintiff’s plane were the proximate result of the negligence of the defendant, its agents and servants.

The evidence justifies the conclusion that had the pilot exercised the care that an ordinarily prudent person would have exercised under the same or similar circumstances he could and would have stopped the plane within less than the 900 to 1,000 feet which still lay between him and plaintiff’s plane at the time when the plane he was operating became diverted from the runway and when it was traveling at not more than 40 miles per hour; and that his failure to do so constituted negligence which was the direct and proximate cause of the injury.

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Related

§ 2516
28 U.S.C. § 2516

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Bluebook (online)
139 F. Supp. 942, 134 Ct. Cl. 675, 1956 U.S. Ct. Cl. LEXIS 94, Counsel Stack Legal Research, https://law.counselstack.com/opinion/hawaiian-airlines-ltd-v-united-states-cc-1956.