Houghton v. McDonnell Douglas Corp.

413 F. Supp. 1230, 14 Fair Empl. Prac. Cas. (BNA) 1586
CourtDistrict Court, E.D. Missouri
DecidedMay 14, 1976
Docket73 C 14(3)
StatusPublished
Cited by9 cases

This text of 413 F. Supp. 1230 (Houghton v. McDonnell Douglas Corp.) is published on Counsel Stack Legal Research, covering District Court, E.D. Missouri primary law. Counsel Stack provides free access to over 12 million legal documents including statutes, case law, regulations, and constitutions.

Bluebook
Houghton v. McDonnell Douglas Corp., 413 F. Supp. 1230, 14 Fair Empl. Prac. Cas. (BNA) 1586 (E.D. Mo. 1976).

Opinion

413 F.Supp. 1230 (1976)

Phillip W. HOUGHTON, Plaintiff,
and
W. J. Usery, Jr., Secretary of Labor, United States Department of Labor, Intervenor-Plaintiff,
v.
McDONNELL DOUGLAS CORPORATION, Defendant.

No. 73 C 14(3).

United States District Court, E. D. Missouri, Eastern Division.

May 14, 1976.

*1231 John J. Schlueter, Rooney, Webbe, Davidson & Schlueter, St. Louis, Mo., for plaintiff.

Gilbert Drucker, Alan M. Serwer, U. S. Dept. of Labor, Chicago, Ill., Donald J. Stohr, U. S. Atty., Joseph B. Moore, Asst. U. S. Atty., St. Louis, Mo., for intervenor-plaintiff.

Veryl L. Riddle, Bryan, Cave, McPheeters & McRoberts, St. Louis, Mo., for defendant.

MEMORANDUM

WANGELIN, District Judge.

This matter is before the Court for a decision on the merits after a trial to the Court sitting without a jury. The case at bar was brought pursuant to the Age Discrimination and Employment Act, 29 U.S.C. § 621, et seq., (hereinafter ADEA). The Court being fully advised of the premises hereby makes the following findings of fact and conclusions of law.

Findings of Fact

1. Plaintiff, Phillip W. Houghton, was born October 1, 1919, and now resides in St. Louis County, Missouri.

2. The Intervenor-Plaintiff is the Secretary of Labor, of Washington, D. C.

3. Defendant, McDonnell Douglas Corporation, (hereinafter McDonnell) is a corporation, organized and existing under the laws of Maryland, having its principal office and place of business in the State of Missouri. At all relevant times, defendant has had twenty or more employees for each working day and each of twenty or more calendar weeks.

4. Defendant McDonnell is engaged in the manufacture and sale of high performance military aircraft to the government of the United States and other foreign states.

5. The high performance aircraft produced by McDonnell include the F-4 Phantom, which is a military fighter aircraft. *1232 This aircraft has been produced by defendant in various models since 1958. During the period since 1960 the F-4 Phantom was almost exclusively the only high performance aircraft in production by the defendant.

6. The F-4 is still in production by the defendant and has the capability, at certain altitudes, of reaching speeds in excess of twice the speed of sound (Mach 2), and is generally flown by a single pilot with a radar observer/weapons officer in the rear seat.

7. Defendant McDonnell also presently produces the F-15 Eagle, which is also a military fighter aircraft similar to the F-4. The F-15 is a single seat high altitude interceptor. The design and technology of the F-15 represents a significant advance over the design and technology employed in the production of the F-4.

8. The F-4 has the following characteristics of performance:

a. It accelerates from zero miles per hour to one hundred seventy (170) miles per hour take-off speed in ten (10) seconds using seventeen hundred (1700) feet of runway, and after gear and flap retraction it can accelerate at a rate of seven hundred eighty (780) miles per hour per minute.

b. It climbs from sea level to an altitude of thirty five thousand (35,000) feet in two and one-half minutes from brake release.

c. In level flight, depending on the altitude and temperature, the aircraft speed may exceed twice the speed of sound (Mach 2), or over two thousand (2,000) feet per second.

d. At maximum level flight speed enclosing on another object on a collision course, the rate of closing speed is one thousand four hundred and forty (1440) miles per hour, or two thousand eighty (2,080) feet per second, or a similar aircraft on a head-on collision course, the closing speed would effectively be two thousand eight hundred and eighty (2,880) miles per hour, or four thousand one hundred and sixty (4,160) feet per second.

e. The aircraft's landing speed is approximately one hundred eighty (180) miles per hour.

9. Defendant McDonnell employs three categories of test pilots: Experimental, Engineering and Production. As of January 1, 1972, defendant listed fifteen test pilots on its test pilot roster, including plaintiff Houghton. Of these pilots, nine were Experimental test pilots, four were Engineering test pilots, one was a Production test pilot, and the last, Houghton, was Chief Production test pilot.

10. Of the three categories of test pilots, the duties of an Experimental test pilot are the most demanding. An Experimental test pilot must be qualified to perform experimental and production testing and must be able to use engineering abilities while performing a series of prescribed tests and maneuvers on new types or research models of aircraft on their initial flights, including:

a. Flights evaluating aircraft performance.

b. Development flights expanding the limits of the aircraft flight or design envelope,[1] or weapons system.

c. High risk flights demonstrating structural integrity, control system modifications, maneuverability, missile/gun firing, etc.

11. An Engineering test pilot is required to pilot test aircraft through a series of prescribed test and maneuver in order to determine compliance with engineering specifications during subsystem development tests such as auto-pilot, flight control, radar and electronic navigation, weapons systems tests, engine tests, and other development flights.

12. A Production test pilot is expected to use engineering abilities while piloting recently assembled production aircraft through a series of prescribed tests and maneuvers in order to functionally evaluate *1233 items such as the air frame, navigation and radar systems, power plant and other items, for final company acceptance before delivery to the customer.

13. A typical production test flight consists of take-off, flight to the testing area and return to the St. Louis airport within a time of approximately one hour and fifteen minutes.

14. In many instances the plane being flown has never been flown before the production test flight.

15. The test pilot flies the aircraft without a co-pilot or other person capable of flying or landing the aircraft.

16. Portions of the flight commonly occur in the vicinity of a major city with the attendant dangers to the general population in the event of an accident or crash.

17. In beginning and ending a production test flight, pilots fly over heavily populated areas of the City and County of St. Louis.

18. During a production test flight, the pilot is required to undergo a brief two to three second acceleration of approximately 5 "Gs"[2] pull up to check the structural integrity of the aircraft, plus one brief pull-up of approximately 4 "Gs" to observe the disengagement of the auto-pilot system.

19. The production test flight also includes in addition to the acceleration tests, a level speed run approaching twice the speed of sound (Mach 2) to verify the integrity of the air frame and proper operation of the engines at supersonic speeds.

20. The Production test pilot is also expected to conduct a radar intercept test which consists of closing upon a friendly target at a rate in excess of one thousand miles per hour. The Production test pilot must also be able to fly over rolling terrain and attempt to maintain a constant altitude of two hundred fifty (250) feet above the earth at speeds up to five hundred fifty (550) miles per hour or eight hundred (800) feet per second.

21.

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413 F. Supp. 1230, 14 Fair Empl. Prac. Cas. (BNA) 1586, Counsel Stack Legal Research, https://law.counselstack.com/opinion/houghton-v-mcdonnell-douglas-corp-moed-1976.