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Thomas G.
DOTY
Disintegrating force of a dynamite explosion resulting in
destruction of the aircraft
Flight 11 departed O'Hare at 8:35 p.m. The flight
was routine until just before the Mississippi River, when it deviated
from its filed flight plan to the north to avoid a line of
thunderstorms. In the vicinity of Centerville, Iowa, the radar image
of the aircraft disappeared from the scope of the Waverly, Iowa,
Flight Following Service. At approximately 9:17 p.m. an explosion
occurred in the right rear lavatory, resulting in separation of the
tail section from the fuselage. The aircraft broke up and the main
part of the fuselage struck the ground about six miles north-northwest
of Unionville, Missouri.
Witnesses in and around both Cincinnati, Iowa and
Unionville reported hearing loud and unusual noises at around 9:20
p.m., and two more saw a big flash or ball of fire in the sky. A B-47
Stratojet bomber out of Forbes Air Force Base in Topeka, Kansas, was
flying at the altitude of 26,500 feet in the vicinity of Kirksville,
Missouri. The aircraft commander saw a bright flash in the sky forward
of and above his aircraft's position. After referring to his
navigation logs he estimated the flash to have occurred at 9:22 p.m.
near the location where the last radar target of Flight 11 had been
seen. Most of the fuselage was found near Unionville, but the engines
and parts of the tail section and left wing were found up to six miles
away from the main wreckage.
Of the 45 individuals on board, 44 were dead when
rescuers reached the crash site. One passenger, 27-year old Takehiko
Nakano of Evanston, Illinois, was alive when rescuers found him in the
wreckage, but he died of internal injuries at Saint Joseph Mercy
Hospital in Centerville, Iowa, an hour and a half after being rescued.
Another of the victims was passenger Fred P. Herman, a recipient of
the United States Medal of Freedom.
FBI agents discovered that one of the passengers,
Thomas G. Doty, a married man with a five-year-old daughter, had
purchased a life insurance policy from Mutual of Omaha for $150,000,
the maximum available; his death would also bring in another $150,000
in additional insurance (some purchased at the airport) and death
benefits. Doty had recently been arrested for armed robbery and was to
soon face a preliminary hearing in the matter. Investigators
determined that Doty had purchased six sticks of dynamite for 29 cents
each, shortly before the crash, and were able to deduce that a bomb
had been placed in the used towel bin of the right rear lavatory.
Author Arthur Hailey based a subplot of his 1968
novel Airport on the Flight 11 bombing.
Notably, until 2009 Continental Airlines still used
Flight 11, on the Paris-Houston route; flight numbers in the USA
involved in fatal accidents are more commonly retired. Effective
October 25, 2009 Flight 11 was replaced on the Paris-Houston route by
flight 33.
In July 2010, a memorial was erected near the crash
site in Unionville, Missouri on the anniversary of the crash.
CIVIL AERONAUTICS BOARD
AIRCRAFT ACCIDENT REPORT
RELEASED: August 1, 1962
CONTINENTAL AIR LINES, INC., BOEING 707-124, N 70775,
NEAR UNIONVILLE, MISSOURI, MAY 22, 1962
SYNOPSIS
On the night of May 22, 1962, a Continental Air Lines Boeing
707-124, N 70775, operating as Flight 11 en route from OHare Airport,
Chicago, Illinois, to Kansas City, Missouri, was flying via Jet Route
26V at an altitude of 39,000 feet. A few minutes after Flight 11 had
made a northerly deviation from course to circumnavigate a
thunderstorm, in the vicinity of Centerville, Iowa, the radar image of
the aircraft disappeared from the scope of the Waverly, Iowa, Flight
Following Service. At approximately 2117 an explosion occurred in the
right rear lavatory resulting in separation of the tail section from
the fuselage. The aircraft broke up and the main part of the fuselage
struck the ground about 6 miles north-northwest of Unionville,
Missouri. All 37 passengers and crew of 8 sustained fatal injuries.
The aircraft was totally destroyed.
The Board determines that the probable cause of this accident was
the disintegrating force of a dynamite explosion which occurred in the
right rear lavatory, resulting in destruction of the aircraft.
Investigation
Aircraft N 70775, a Boeing 707-124, arrived at OHare International
Airport, Chicago, Illinois, from Los Angeles, California, as
Continental Air Lines Flight 10 at approximately 1900 1 on May 22,
1962. At OHare the aircraft received routine servicing and a
turnaround inspection in preparation for scheduled departure to Los
Angeles as Flight 11 with an intermediate stop at Kansas City.
The crew of Flight 11 had flown into OHare from Los Angeles as the
crew of CAL Flight 4, a Boeing 720, landing there at 1913. The crew
consisted of Captain Fred R. Gray, First Officer Edward J. Sullivan,
Second Officer Roger D. Allen, Director of Passenger Services, David
E. Olssen, and Stewardesses Marilyn Bloomquist, Mary McGrath, Martha
Rush, and Stella Berry. Flight dispatch was accomplished by the
dispatcher at the carriers headquarters in Denver through the customer
service agent in Chicago in accordance with company policy and
procedure. The dispatchers proposed flight plan cruising altitude of
28,000 feet from Chicago to Kansas City was changed to 39,000 feet by
the captain because he had knowledge of thunderstorm activity west of
Chicago. An en route time of 1:01 hours from Chicago to Kansas City
was shown on the flight plan. Flight 11 was released from OHare with a
takeoff gross weight and a center of gravity well within prescribed
limits.
U. S. Weather Bureau forecasts indicated heavy thunderstorm activity
associated with an active cold front and prefrontal squall lines
between Chicago and Kansas City. A severe weather warning was in
effect for an area which lay across part of the proposed route of
Flight 11, predicting heavy thunderstorms, maximum tops of 50,000 feet,
with severe to extreme turbulence and possibility of tornadoes.
Flight 11 reported off OHare Airport at 2035 and was vectored by
departure control to Bradford, Illinois, reporting over Bradford at
39,000 feet on Jet Route 26 Victor at 2052. Just east of the
Mississippi River, at approximately 2101, Flight 11 asked Chicago Air
Route Traffic Control Center if it had a radar picture of the squall
line just ahead of the flight. The reply was negative and the center
handed the flight over to the Flight Following Radar Site at Waverly,
Iowa, one minute later. At about 2102, Flight 11 requested information
regarding penetration of the storm area, and the Waverly controller
suggested a southerly circumnavigation of a thunderstorm lying across
the aircrafts flightpath.
Additional discussion between Flight 11 and the controller developed
the fact that the thunderstorm could be circumnavigated either to the
south or to the north. The nature of this discussion indicated that
the aircraft's radar was operating satisfactorily, and Flight 11
elected to pass to the north around the storm cell. After the aircraft
passed around the storm, the controller informed the flight that a
direct course to Kirksville from its present position should avoid all
inclement weather. The crew then replied that they were starting a
turn, and requested clearance direct to Kansas City. The Waverly
controller approved this request and informed the flight that descent
clearance was being processed.
For several minutes Waverly attempted to contact Kansas City Center
without success and so informed the flight, whereupon Flight 11
replied Okay, we can probably reach them on your radio, do you want to
send us over? This was the last transmission heard from Flight 11 and
is believed, by the controller, to have occurred at approximately
2114. Within approximately -one minute of this transmission, however,
the Waverly controller established contact with Kansas City Center and
attempted to effect a radar handoff of Flight II. At the same time
Waverly tried unsuccessfully to contact Flight 11 to request that they
establish communications with Kansas City on 133.95 mcs. Waverly also
attempted to identify to the Kansas City Center the radar target
location of Flight 11 as about 10 miles south of the intersection of
Airways J45V and J64V, and moving in a southerly direction. The Kansas
City controller momentarily observed an indistinct target at this
approximate position but this target disappeared after two or three
sweeps of the antenna and was never useable for radar handoff purposes.
The Waverly controller stated that at approximately 2115, one minute
after Flight 11s last transmission, he observed the aircraft's
transponder return and subsequently the primary target begin to fade
from the radar scope. It was later determined that the aircraft had
crashed 6 miles north-northwest of Unionville, Missouri.
Numerous people in the vicinity of the accident site were contacted
during a search for eyewitnesses to the accident, but none could be
found who could positively correlate what they saw with the
Continental aircraft. Several persons in the vicinity of Cincinnati,
Iowa, and Unionville, Missouri heard loud and unusual noises. Two
witnesses saw a big flash or ball of fire of short duration in the sky.
The times at which these phenomena occurred were estimated by
witnesses as between 2110 and 2130. All witnesses stated that the
weather was clear at the time.
A B-47 from Forbes AFB, Topeka, Kansas, was flying in the vicinity
of Kirksville, Missouri, at the approximate time of the accident and
was headed in a northerly direction at 26,500 feet. The aircraft
commander later reported that he saw a bright flash in the sky forward
of and above his position. After referring to his navigation logs he
estimated the flash to have occurred at 2122, near the location where
the last radar target of Flight 11 had been seen by Waverly. He
further stated that weather in the area at the time was clear with
little or no turbulence.
The foil magazine removed from N 70775s flight recorder showed
little damage, but there was extensive denting of the recorder case,
severe distortion of the mounting bracket, arid considerable damage to
the internal mechanism. All of the parameter values recorded on the
foil were readable and showed a normal operation of the aircraft.
These values closely coincided with the aircrafts reported flight
profile from liftoff at OHare Airport until 42 minutes later, when the
vertical acceleration trace indicated extremely large excursions and
all other traces became unreliable. The recorder indicated that the
aircraft had encountered moderate turbulence at several intervals
throughout the flight, but that for about five minutes prior to the
last normal trace the air was smooth. Correlation of the flight
recorder readings with the reported takeoff time indicates that at
2111, on encountering the last appreciable turbulence, the aircraft
turned from a magnetic heading of 270 degrees to a heading of 247
degrees. It held this heading for about 30 seconds, and then turned
further left to 230 degrees, holding within 10 degrees of the latter
heading from approximately 2113 to the point where the traces became
abnormal. The pressure altitude trace indicated a normal descent, from
39,000 feet, was begun at approximately 2115 and it continued at a
fairly constant rate of 1,000 feet per minute for 2 minutes 7 seconds
to an altitude of 36,800 feet. The indicated airspeed trace during
this same interval of time shows an unsteady increase from 250 to 274
knots. The acceleration trace for this period of time varies little
from 1.0 g except for a five-second interval at about 2116, when it
jumped slightly between 0.78 and 1.23 g. Approximately one minute
later, approximately 42 minutes after liftoff, or at approximately
2117, the flight recorder traces became extremely active.
The fuselage of N 70775, minus the aft 38 feet, and with part of the
left and most of the right wing intact, struck the ground, headed
westerly down a 10-degree slope of an alfalfa field located about 6
miles north-northwest of Unionville, Missouri and 1-1/2 miles west of
State Highway No. 5. The nose of the aircraft dug into the ground at a
20-degree angle, with some telescoping of the fuselage just aft of the
cockpit; however, the remaining fuselage, although badly broken, was
not telescoped. The fuselage and wings struck the ground in a nose-down
attitude and with the lateral axis almost level. There were
indications of rotation about the vertical axis at impact, but the
absence of drag marks down the hill reflected an almost complete lack
of horizontal speed. The landing gear was down and locked; the wing
flaps were up. An emergency checklist was found between the captains
yoke and his instrument panel. Two flight deck clocks had stopped at
2121:15 and 2121:45, respectively.
The engines were found at four separate locations within an area 1/2
mile wide and 3/4 mile long, with the closest engine approximately
1-1/8 miles southwest of the main wreckage. Each engine was partially
buried in the ground on impact from an almost vertical fall.
Inspection of the engines indicated that there was little or no
rotation of compressors or turbines at ground impact.
Four large pieces of the aircraft were scattered in a northeasterly
direction along the aircrafts flightpath 4 to 6-1/2 miles from the
main wreckage. One of these, a 29-foot section of the left wing, was
found about 4 miles away. The outboard panel and tip of the left wing
were located 6-1/2 miles northeast of the main wreckage. The
horizontal stabilizer and elevator assembly was lying in a hayfield
about 1/2 mile north of the 29-foot wing section. About 6 miles
northeast of the main wreckage the vertical fin and rudder assembly,
with about half of the station 1440 and 1507 frames and some top skin
still attached, was found intact having dropped almost vertically into
thick woods. A soot-covered "assist" handle from one of the airplanes
lavatories, a pillow, and some tissue paper were found lodged inside
an aperture between the station 1440 frame and the fin. A small amount
of blood and other human remains were found on the aft surface or this
frame. Numerous abrasion marks and several punctures were found on the
surfaces of the fin. There were also abrasions on the right horizontal
stabilizer with blue smears matching cabin interior components!
Fragments of the airplane were scattered along a narrow path 40
miles long in a northeasterly direction from the main wreckage. Low
density materials such as papers, napkins, pillows, and insulation
were recovered at distances tip to 120 miles away.
Examination of the wreckage showed no evidence of metal fatigue,
structural or systems failure or malfunction, fire in flight, or
collision with another aircraft or foreign object. The condition and
pattern in which the wreckage was found indicated a high altitude
breakup and disintegration of the aircraft in flight.
During the initial stages of the investigation, about 20 feet of the
fuselage between stations 1220 and 1440 could not be found. An
intensified search for the missing wreckage was conducted; all
scattered wreckage, including pieces of the missing section, were
consolidated at one location and two mockups of the aft fuselage area
were constructed. One consisted of the fuselage exterior from about 10
feet forward of the main entrance door to the empennage; the other
mockup, the interior in the same general area. As interior and
exterior pieces of the fuselage were refitted into their original
positions on the two mockups it was found that the pieces became
progressively smaller from all directions toward a focal point inside
the right rear lavatory. Most of the pieces of this compartment were
mere fragments or were entirely missing. Localized bulges and
deformations of aircraft skin; jagged perforations of skin, structure
and equipment from objects propelled at high velocity; concentrations
of gray-black deposits applied under heavy force; aircraft skin pushed
straight out over rivet heads; and other such evidence clearly
revealed that a high-order detonating force had emanated from the
lavatory. The physical evidence further showed that this force had
originated in the waste towel bin underneath the washbasin counter of
the right rear lavatory, and had acted in all directions from this
point.
Thirty-six bodies were recovered from the main wreckage and eight
were found at various points from three-tenths of a mile to almost two
miles back along the flightpath. One passenger in the main wreckage
survived the accident but succumbed to fatal injuries about 1-1/2
hours after his rescue, which occurred several hours after the
accident. The captain, first officer, and second officer were in their
normal crew locations. Three smoke masks in the cockpit were found
with face plates demolished, oxygen hoses broken, and with blood and
tissue, adhered to the inside and outside of each mask. Toxicological
and pathological examinations of the flight crew bodies disclosed no
abnormalities. No indication of burns was found on any of the bodies.
A review of the maintenance records of N 70775 revealed no
significant irregularities prior to the aircrafts departure from OHare
Airport on the night of May 22, 1962.
Analysis and Conclusions
Regarding the operational and maintenance aspects of this accident,
the records show that the flight crew was properly qualified, that the
aircraft was dispatched in accordance with company policies and
procedures, and that the aircraft was airworthy at the time the flight
departed from O'Hare Airport.
Statements made by controller personnel who had the aircraft under
radar surveillance during most of the flight, traces made by the
aircrafts flight recorder, and witness statements regarding local
weather conditions indicate that Flight 11, though having encountered
thunderstorms across its flightpath, had safely circumnavigated them
and was in clear weather conditions with no significant turbulence
when the disaster occurred. It is therefore concluded that weather was
not a factor in this accident.
All available evidence indicates that the aircraft started
disintegrating at an appreciable altitude in the vicinity of
Centerville, Iowa, and at a time determined to be approximately 2117.
This conclusion if supported by the Waverly radar controller, who
observed the aircraft's transponder and primary radar target begin to
fade from his scope at approximately 2115. Groundwitnesses in the
vicinity who heard unusual noises or saw a flash or ball of fire in
the sky placed the time somewhere between 2110 and 2130. The B-47
pilot who saw a flash in the sky estimated the time of the flash as
being 2122. However, the most reliable evidence regarding the time of
the explosion is considered to be that indicated by the aircrafts
flight recorder as being 2117.
The physical evidence showed that the landing gear was down and that
the flight crew was wearing smoke masks at the time of impact. In
addition, the emergency checklist was found between the captains yoke
and his instrument panel. This evidence leads to the belief that upon
experiencing an explosion, which would of course be followed by
explosive decompression, the crew initiated the required emergency
descent procedures. It is also thought that the crew donned smoke
masks due to the dense fog which forms in the cabin immediately after
explosive decompression.
At separation of the tail, the remaining aircraft structure pitched
nose down violently, causing the engines to tear off, after which it
fell in uncontrolled gyrations. After separation from the aircraft the
engines assumed a trajectory which allowed sufficient time for their
compressors and turbines to coast to a negligible r.p.m. before impact
with the ground.
Reconstruction and examination of the aft fuselage proved
conclusively that the forces which caused the initial disintegration
radiated from a point within the used towel bin underneath the
washbasin in the right rear lavatory. The violence of the explosion
was clearly shown by the pattern of breakup and projection of
fragments emanating from this focal point. Such evidence was in sharp
contrast to the damage caused by an explosion resulting from any
combustible material or source connected with the operation of the
aircraft, its systems or components. The Federal Bureau of
Investigation laboratory analyses of residues collected on material
from the right rear lavatory and surrounding structure established
that the explosive used was dynamite.
Evaluation of all the evidence leads logically to the conclusion
that a dynamite device was placed in the used towel bin of the right
rear lavatory with the express intent to destroy the aircraft.
During the early stages of the investigation, when the first clues
of such a possibility were found, the Federal Bureau of Investigation
was apprised of all such evidence so that the apparent criminal
aspects of the accident could be properly pursued. The FBI immediately
initiated a full-scale investigation.
Probable Cause
The Board determines that the probable cause of this accident was
the disintegrating force of a dynamite explosion which occurred in the
right rear lavatory resulting in destruction of the aircraft.