Richardson v. United States

372 F. Supp. 921, 1974 U.S. Dist. LEXIS 12972
CourtDistrict Court, N.D. California
DecidedJanuary 3, 1974
DocketC-51806 OJC
StatusPublished
Cited by8 cases

This text of 372 F. Supp. 921 (Richardson v. United States) is published on Counsel Stack Legal Research, covering District Court, N.D. California primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Richardson v. United States, 372 F. Supp. 921, 1974 U.S. Dist. LEXIS 12972 (N.D. Cal. 1974).

Opinion

MEMORANDUM FOR JUDGMENT

OLIVER J. CARTER, Chief Judge.

Plaintiffs have brought a civil action against the United States wherein they allege that Federal Aviation Agency (FAA) tower personnel at San Francisco International Airport negligently failed to provide pilot Marshall G. Richardson with an adequate and timely warning regarding an aeronautical phenomenon known as “wake turbulence” or “wing tip vortices.” Richardson was on final approach to the airport and, the plaintiffs allege, as a direct and proximate result of the Tower’s failure to warn of the wake turbulence danger, Richardson’s aircraft crashed into the San Francisco Bay, killing Richardson and causing damage to the plane itself.

Plaintiffs Loma C. Richardson, wife of and as executrix of the estate of Marshall G. Richardson, and Mrs. Lowell H. Ruff and Edward G. Richardson, children of the deceased, are suing as the sole surviving heirs for the wrongful death of Marshall G. Richardson. Plaintiff Newark Insurance Company, the hull insurance carrier on the aircraft, has joined in the action as subrogee of the estate of Marshall G. Richardsqn to recover sums paid in settlement of a claim for damages to the aircraft. Jurisdiction is based upon the Federal Tort Claims Act, 28 U.S.C. § 1346(b), and the law of the State of California is therefore applicable.

FINDINGS OF FACT

On March 6, 1967 at 1:23 p. m. decedent Marshall G. Richardson, flying a single engine Navion, Registration Number N8760H, contacted the San Francisco Airport Traffic Control Tower (hereinafter referred to as Tower) and requested landing instructions. Richardson at that time stated that he was approximately a mile and a half north of Candlestick Park — a normal entry point into the San Francisco International Airport traffic pattern. The Tower acknowledged Richardson’s request and the Navion commenced its downwind approach. At 1:30 p. m. the Tower informed Richardson that he was to follow a TWA Boeing 707 straight in on Runway 28 Right. Decedent acknowledged the Tower’s transmission and stated that “we have him [TWA Boeing 707] in sight.” The Navion’s last transmission occurred at 1:32 p. m. when, in response to the Tower’s query as to “how far out” the Navion was, Richardson indicated that he was a mile and a half behind the Boeing and had passed Coyote Point. Thirty seconds later the TWA jet had completed its landing and began to taxi to the terminal. At 1:33 p. m. the Navion was cleared to land and a wake turbulence advisory was given by the Tower. 1 The Navion did not respond to this transmission.

From the evidence introduced at trial, it appears extremely likely that the Navion Richardson was flying was caught in the wake turbulence generated by the TWA Boeing 707 it was following. As a result of being caught therein, Richard *924 son lost control of the aircraft and was killed when the Navion crashed into San Francisco Bay approximately one half mile from the threshold of Runway 28 Right.

Wake turbulence is a phenomenon about which there existed some controversy in 1967. The aerodynamic characteristics of the phenomenon had not (and apparently still have not) been ascertained to a particularly high degree of certainty. 2 Disputes as to intensity, duration, and causation have been common. 3 However, wake turbulence can be generally described as that force generated by the aircraft’s air foil 4 as it passes through a mass of air and thereby creates lift. Each wing of the aircraft leaves behind the trailing edge a continuous sheet of unstable air. The uneven flow of air (spillage) around the wing tip forces the unstable air to roll into two distinct vortices — i. e., funnel shaped masses of air currents moving in a circular fashion — -trailing behind and below each tip. The vortices rotate in opposite directions and always settle towards the ground. At a height determined by the mass of the aircraft and the length of its wing, the vortices separate laterally and continue to move apart from each other until they strike the ground and are dissipated. The wind can have a great effect on the vortices, assisting movement in one direction, retarding movement in another.

Large aircraft during take-off and landing present the greatest wake turbulence danger since at these points they are creating greater lift foreés while simultaneously traveling at relatively slower speeds. Light aircraft such as the Navion must be particularly alert when landing or taking off in the vicinity of large aircraft such as the TWA Boeing 707.

The Navion conducted its approach at an altitude greatly below the descent path of the preceding Boeing. Flying in such a position placed the Navion squarely within the zone of danger created by wake turbulence since, as noted above, the vortices descend and never ascend. Accordingly, the safest and most effective method of avoiding wake turbulence would have been to maintain an altitude above the descent path of the preceding aircraft and “landing long.” 5 There existed no conditions at the time of the accident that would have prevented the Navion from either maintaining a higher altitude or effecting a long landing. The above-described procedure for avoiding wake turbulence is essential knowledge for any pilot operating around large airports. Richardson knew, or should have known, of the procedure and, had he utilized it, the Navion would not have encountered the wake turbulence generated by the Boeing 707.

The weather at the time of the accident was hazy, with approximately seven miles visibility. Accordingly, the approach was conducted pursuant to Visual Flight Rules (VFR). Under VFR, the pilot is responsible for selecting the altitude, speed, course, and separation 6 of *925 his aircraft. Thus the Tower was responsible for sequencing — i. e., informing the Navion that he was to land after the TWA Boeing 707 — but Richardson himself had the responsibility for selecting the altitude, course, and speed at which he would land his aircraft behind the 707.

The Air Traffic Controller at the time of the accident was Charles E. Henson, an ATC with over thirteen years of experience. Mr. Henson, an employee of the FAA, had no reason to suspect that the Navion was being flown by anyone other than an experienced and competent pilot. At no time during final approach did Henson or other Tower personnel have the Navion visually sighted. A radar scope was utilized by Tower personnel to assist visual control, and although at various times the Tower had a fix on the Navion, the radar was incapable of indicating altitude. Richardson never, during the period he was on final approach, indicated his altitude and, accordingly, the Tower was not aware of the dangerous altitude at which the Navion was flying.

Mr. Henson was aware of the existence of the wake turbulence phenomenon and the procedures available to avoid it.

Free access — add to your briefcase to read the full text and ask questions with AI

Related

Cite This Page — Counsel Stack

Bluebook (online)
372 F. Supp. 921, 1974 U.S. Dist. LEXIS 12972, Counsel Stack Legal Research, https://law.counselstack.com/opinion/richardson-v-united-states-cand-1974.