Koirala v. Thai Airways International, Ltd.

126 F.3d 1205, 1997 WL 590072
CourtCourt of Appeals for the Ninth Circuit
DecidedSeptember 25, 1997
DocketNos. 96-16598, 96-16712
StatusPublished
Cited by2 cases

This text of 126 F.3d 1205 (Koirala v. Thai Airways International, Ltd.) is published on Counsel Stack Legal Research, covering Court of Appeals for the Ninth Circuit primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Koirala v. Thai Airways International, Ltd., 126 F.3d 1205, 1997 WL 590072 (9th Cir. 1997).

Opinion

THOMAS, Circuit Judge:

On July 31, 1992, Thai Airways International (“Thai Airways”) Flight TG-311 crashed into a mountainside while attempting to land at Tribhuvan International Airport in Kathmandu, Nepal, killing all 113 people aboard. In this case, we examine whether the crash was the result of “wilful misconduct” on the part of the flight crew, lifting the Warsaw Convention’s $75,000 cap on damages for personal injury. We agree with the district court that it was.

I

Flight TG-311 was a regularly scheduled flight from Bangkok, Thailand to Kathmandu, Nepal. Tribhuvan International Airport in Kathmandu has the reputation of being one of the most difficult airports in the world in which to land. It is situated in a valley surrounded by very high mountains, requiring a steep approach to land and the full extension of the wing flaps during the entire descent. Kathmandu air traffic control has no radar. Instead, air traffic controllers determine aircraft location and provide instructions to aircraft using air-to-ground and ground-to-air radio communications. Flight TG-311 Captain Preeda Suttimai and First Officer Phunthat Boonyayej (collectively “the flight crew” or “the crew”) were properly licensed and certified, and both had substantial experience flying into Kathmandu.

On the night of the crash, the weather in Kathmandu was cloudy and rainy. The flight crew had little visibility and were entirely dependent upon navigational instruments to fly the aircraft. At 06:46:07 Coordinated Universal Time, Tribhuvan air traffic control authorized the captain to execute a landing approach. The aircraft was at this time flying at heading 022, twenty-two degrees east of due north. When the crew attempted to configure the airplane for landing, they discovered at 06:47:34 that the wing-flaps failed to extend properly, rendering landing too dangerous to attempt. The crew requested permission to divert the aircraft to Calcutta, but before air traffic control responded, the wing flaps extended properly at 06:49:05. By this time, however, the aircraft had traveled too far north and was too high to begin a descent toward the runway.

From 06:49:08 until 06:50:21, the captain asked air traffic control four times for clearance to turn left and fly south to point “Romeo,” a navigational position approximately forty-one miles south of Tribhuvan International Airport from which the aircraft had made its initial approach, to attempt another landing approach. Although a left turn under these circumstances was a reasonable and safe action for the airplane, air traffic control did not respond to the captain’s repeated requests.

At approximately 06:50:50, without requesting or obtaining clearance from air traffic control, the flight crew began a climbing right turn. The first officer notified air traffic control at 06:51:55 of the right turn and the crew’s intention to climb to 18,000 feet and return to point Romeo. Air traffic control ordered the aircraft to descend to 11,500 feet and maintain that altitude, and the flight crew complied with that instruction.

Six separate times from 06:52:06 to 06:59:39, air traffic control authorized the aircraft to head south and return to point Romeo. Instead of turning 180 degrees and heading south on heading 202, as was then-[1208]*1208stated intention, the flight crew mistakenly turned the aircraft full circle, 360 degrees, and unknowingly continued heading north toward the mountains surrounding Kathmandu on heading 022. From the time the aircraft completed the 360 degree turn, at approximately 06:54:41, the flight crew believed they had executed only a 180 degree turn and were heading south, despite the fact that all the navigational instruments on the instrument panel constantly indicated the northerly heading of the aircraft.

The crew had apparently become preoccupied from approximately 06:54:12 with their unsuccessful efforts to input and display the location of point Romeo on the computerized Flight Management System (“FMS”). They were unable to display point Romeo on the FMS because the system was incapable of displaying navigational points located behind the aircraft. As point Romeo was located to the south of the aircraft and the aircraft was heading north, the FMS was unable to display the location of the navigational point. However, the crew believed they were heading south and could not understand why they were unable to display the location of point Romeo on the FMS.

The crew continued to attempt to program the FMS and to operate under the misconception that they were heading south for approximately six minutes, until at least 06:59:56. At 06:59:58, the first officer realized the aircraft was heading north and attempted to communicate this fact to the captain, who did not understand the warning. Twenty-eight seconds later, at 07:00:26, the aircraft crashed into the side of a mountain twenty-three miles north of Kathmandu at an altitude of 11,500 feet and a ground speed of 300 nautical miles per hour, killing all ninety-nine passengers and fourteen crew members on board instantly.

Relatives of seven of the passengers killed in the crash-Santosh Koirala, Chandra Rajlawat, Thomas Hill, Thomas Guta, and Mr. Guta’s three children, Kora Guta, Bo Guta, and Magma Guta-brought an action against Thai Airways pursuant to the Convention for the Unification of Certain Rules Relating to International Transportation by Air, October 12, 1929, 49 Stat. 3000, T.S. No. 876, 137 L.N.T.S. 11, reprinted in 49 U.S.C. § 40105 note (1997) (the “Warsaw Convention” or the “Convention”). Relatives of another passenger, Kandaswamy Ramachandran, also brought an action which was eventually consolidated with the previously filed action.

The parties agreed to bifurcate the trial into liability and damages phases. Before either phase commenced, Thai Airways filed a motion to determine the substantive law governing liability and the availability of damages. Relying in substantial part on the Second Circuit’s opinion in Zicherman v. Korean Air Lines Co., 43 F.3d 18 (2d Cir.1994), the district court held in an order dated October 11, 1995 that U.S. maritime law would govern the dispute.1 The court also held, among other things, that only a decedent’s spouse and dependents could maintain a wrongful death action.

The case was then tried before the district court without a jury, as required by the Foreign Sovereign Immunities Act, 28 U.S.C. §§ 1330, 1602-1611 (“FSIA”), pursuant to which the district court exercised subject matter jurisdiction.2 See 28 U.S.C. § 1330(a). In the liability phase, applying U.S. federal law interpreting the term “wilful misconduct” under the Warsaw Convention, the court found that the crash of Flight TG-311 was the result of the crew’s “wilful misconduct” in failing to monitor their navigational instruments which displayed a norther[1209]*1209ly course for the entire six minutes after the 360-degree turn and before impact.

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126 F.3d 1205, 1997 WL 590072, Counsel Stack Legal Research, https://law.counselstack.com/opinion/koirala-v-thai-airways-international-ltd-ca9-1997.