Crash of a Beechcraft 200 Super King Air in Chicago: 3 killed

Date & Time: Nov 11, 1999 at 2020 LT
Operator:
Registration:
N869
Flight Phase:
Survivors:
No
Schedule:
Chicago - South Bend
MSN:
BB-174
YOM:
1976
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
18000
Captain / Total hours on type:
4536.00
Aircraft flight hours:
8636
Circumstances:
Shortly after being cleared for takeoff on runway 18 (3,899 feet by 150 feet, dry concrete) at Merrill C. Meigs Field, Chicago, Illinois, the airplane impacted into Lake Michigan, approximately 300 feet south of the end of the runway. The tower controller said that at the 3/4 field point, the airplane had not rotated. 'All I can see are lights [from the airplane]. At the point where he would have been at the end of the runway, [I] lost the lights.' A witness on the airport said that when the airplane went by, it 'didn't sound like most King Airs do at that point.' There was a pulsating sound, but it was not heavy. The witness said that the airplane was 'bouncing up and down on the [gear] struts, and wasn't coming off the ground.' NTSB Materials examination of the pilot's control yoke showed that there were small distortions in the holes of the column and the rod where the control lock would be inserted. A small crack was observed around 1/4 of the control lock rod hole. The control lock was a substitute for the original airplane equipment. The examination of the control lock showed 'several shiny scratches ... parallel to the length of the pin.' A small deformation was observed near the top of the pin part of the control lock. The company flight department's third pilot said that when they flew the airplane, they always placed the control lock in the pilot's side cockpit wall pocket, along with a car key and a remote hanger door opener. The car key and the door opener were found in the wall pocket during the on-scene investigation. The control lock was
recovered from the lake, 7 days later.
Probable cause:
On ground collision with the lake for undetermined reasons.
Final Report:

Crash of a Cessna 340A in Chicago: 1 killed

Date & Time: Aug 1, 1998 at 2200 LT
Type of aircraft:
Registration:
N5340F
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Chicago - Louisville
MSN:
340A-0667
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1600
Captain / Total hours on type:
500.00
Aircraft flight hours:
3036
Circumstances:
The pilot reported the airplane decelerated during the takeoff roll. He applied the brakes and as he advanced the throttles to full power the airplane accelerated. The airplane cleared the end of the runway then stalled into Lake Michigan, flipped inverted and sank. One passenger reported that it felt as if someone put on the brakes. One passenger drowned. The pilot used 32' of manifold pressure for takeoff versus 37.3' as placarded. The pilot operating handbook lists normal takeoff speed as 91 KIAS, however the airplane was equipped with vortex generators. The pilot reported looking for 105 to 110 KIAS for takeoff. No evidence was found of the pilot having a multi-engine rating. No evidence of a mechanical failure/malfunction was found.
Probable cause:
The pilot's improper use of the throttle in not using full power for takeoff, the pilot's failure to use proper aborted takeoff procedures, and the inadvertent stall/mush. A factor associated with the accident was inadequate preflight/planning by the pilot.
Final Report:

Crash of a Piper PA-60P Aerostar (Ted Smith 602P) in Port Huron

Date & Time: Sep 14, 1994 at 0846 LT
Operator:
Registration:
C-FSMO
Survivors:
Yes
Schedule:
Stratford – Chicago
MSN:
62-0875-8165014
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1174
Captain / Total hours on type:
42.00
Aircraft flight hours:
1841
Circumstances:
As the airplane approached 22,000 feet, the pilot reported that both engines stopped running within seconds of each other. During the emergency landing approach the airplane collided with trees. Onscene investigation revealed no mechanical anomalies with the engines. The fuel system was empty, other than traces of fuel found in the left and right engine's fuel injector servos and flow dividers. Both wing fuel tank caps o-rings were hardened and had flat spots on them. The caps' opening tabs were able to be opened at 8 and 3 lbs of force, respectively. The company holding the airplane's type certificate states an opening force of 16 lbs of force is required. The company's annual inspection checklist requires that the tabs be checked. No record of this being accomplished was found in the airframe logbook. The pilot operating handbook states that the fuel cap tab tension must be checked during the preflight inspection.
Probable cause:
Inadequate preflight by the pilot resulting in fuel exhaustion. Inadequate maintenance and inspection was a factor contributing to the accident.
Final Report:

Crash of a Dassault Falcon 10 in Chicago: 2 killed

Date & Time: Jan 30, 1980 at 1548 LT
Type of aircraft:
Operator:
Registration:
N253K
Flight Phase:
Survivors:
Yes
Schedule:
Chicago - Battle Creek
MSN:
10
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
3453
Captain / Total hours on type:
635.00
Copilot / Total flying hours:
8845
Copilot / Total hours on type:
1163
Aircraft flight hours:
3196
Circumstances:
The airplane was unable to takeoff from Chicago-Merrill C. Meigs Airport runway 18, overran and crashed into Lake Michigan. A pilot and a passenger were killed while four other occupants were seriously injured. The aircraft came to rest in 25 feet of water about 300 feet past the runway end.
Probable cause:
The flightcrew's failure to release the parking brake before the takeoff roll was started, which resulted in significant wheel/brake drag and a nosedown pitching moment that inhibited the aircraft's capability to effect a normal acceleration and rotation for takeoff. Contributing to the accident was the lack of adequate company checklist procedures to insure the timely release of the parking brakes.
Final Report:

Crash of a Beechcraft 99 Airliner off Chicago: 2 killed

Date & Time: Jun 9, 1979 at 1451 LT
Type of aircraft:
Operator:
Registration:
N454SA
Flight Type:
Survivors:
No
Schedule:
Chicago - Chicago
MSN:
U-54
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
2195
Captain / Total hours on type:
300.00
Circumstances:
The pilot was completing a positioning flight to Chicago-Merrill C. Meigs Airport and while descending, he encountered poor weather conditions with low ceiling, fog and limited visibility. He lost control of the airplane that crashed into Lake Michigan. Few debris were found while the main wreckage was not recovered. Both occupants were presumed dead.
Probable cause:
Loss of control on final approach after the pilot suffered a spatial disorientation. The following contributing factors were reported:
- Initiated flight in adverse weather conditions,
- Low ceiling,
- Fog,
- Visibility limited to one mile or less.
Final Report:

Crash of a Rockwell Grand Commander 690 off Chicago: 4 killed

Date & Time: Apr 23, 1977 at 1550 LT
Registration:
N847
Flight Phase:
Survivors:
No
Schedule:
Chicago - Harrisburg
MSN:
690-11140
YOM:
1973
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
6707
Captain / Total hours on type:
1200.00
Circumstances:
After takeoff from Chicago-Merrill C. Meigs Airport, while climbing, the airplane collided with a flock of seagulls. An engine lost power and the airplane lost speed and height. The pilot elected to return when the airplane stalled and crashed into Lake Michigan. The aircraft was destroyed and all four occupants were killed.
Probable cause:
Stall and spin after the airplane collided with a flock of seagulls. The following contributing factors were reported:
- Exercised poor judgment,
- Bird ingestion,
- Failed to maintain flying speed,
- Airport supervisory personnel,
- Improper emergency procedures,
- Pilot advised of seagulls on runway,
- Ineffective bird removal technique,
- Failed to retract flaps.
Final Report:

Crash of a De Havilland DH.104 Dove off Chicago: 1 killed

Date & Time: May 20, 1975 at 1139 LT
Type of aircraft:
Operator:
Registration:
N1536V
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Chicago - Chicago
MSN:
04355
YOM:
1952
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6650
Captain / Total hours on type:
22.00
Circumstances:
After takeoff from Chicago-Merrill C. Meigs, while climbing, both engines failed simultaneously. The pilot lost control of the airplane that stalled and crashed into Lake Michigan. The aircraft was lost and the pilot, sole on board, was killed.
Probable cause:
Complete failure of both engines due to fuel exhaustion. The following contributing factors were reported:
- Inadequate preflight preparation,
- Mismanagement of fuel,
- Fuel exhaustion,
- Failure of both engines,
- Improper operations of flight controls,
- Fuel drained total less than two gallons from each wing,
- Right wing hit first and aircraft cartwheeled.
Final Report:

Crash of a Piper PA-61 Aerostar (Ted Smith 601) off Chicago: 1 killed

Date & Time: Oct 3, 1973 at 0525 LT
Operator:
Registration:
N8MW
Flight Type:
Survivors:
No
Schedule:
Cleveland - Chicago
MSN:
61-0029
YOM:
1969
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
The pilot, sole on board, was completing a cargo flight from Cleveland to Chicago. While he was approaching Chicago-Merrill C. Meigs Airport by night, weather conditions worsened with fog and a limited visibility. The pilot lost control of the airplane that crashed into Lake Michigan about 1,5 mile northeast of the airfield. The aircraft was destroyed and the pilot was killed.
Probable cause:
Uncontrolled descent following improper in-flight decisions. The following factors were reported:
- Continued under VFR mode in adverse weather conditions,
- Spatial disorientation,
- Fog,
- Sighted field cancelled IFR,
- Weather deteriorated with 2 miles visibility in fog.
Final Report:

Crash of an ATECO Westwind II in Peoria: 16 killed

Date & Time: Oct 21, 1971 at 1220 LT
Type of aircraft:
Operator:
Registration:
N51CS
Survivors:
No
Schedule:
Chicago - Peoria
MSN:
BA-211
YOM:
1956
Flight number:
SC804
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
16
Captain / Total flying hours:
16119
Captain / Total hours on type:
133.00
Copilot / Total flying hours:
4690
Copilot / Total hours on type:
43
Aircraft flight hours:
7751
Circumstances:
Chicago & Southern Airlines, Inc., Flight 804, crashed at approximately 1220 central daylight time while it was executing an instrument approach to the Greater Peoria Airport, Peoria, Illinois. The 16 persons on board received fatal injuries. The aircraft made initial contact with powerlines which cross the VOR Runway 12 final of Runway 12 of the Greater Peoria Airport approach course, approximately 2 miles west. Near the point of contact there are two towers, each of which supports four sets of cables. The easterly tower is 681 feet mean sea level. The elevation of the ground at the base of the most contact was made with the lower cables which were 65 feet above ground level. The aircraft thereafter contacted the ground, bounced and slid into the base of a large hedgewood tree 152 feet from the point of initial wire contact, along a wreckage path of 050° magnetic. The major portion of the aircraft structure remained at the base of the tree. An intense fire ensued which almost completely destroyed the cockpit and cabin area of the fuselage. All 16 occupants were killed.
Probable cause:
The National Transportation Safety Board determines that the probable cause of this accident was that the pilot knowingly descended below the Minimum Descent Altitude in an attempt to complete the approach by means of visual reference to ground objects. Because of minimal visibility and low clouds in the approach zone, the aircraft was operated at an altitude too low to provide clearance over the powerlines.
Final Report:

Crash of a Lockheed 18-56-23 LodeStar in Chicago

Date & Time: Nov 17, 1966 at 1652 LT
Type of aircraft:
Operator:
Registration:
N339
Flight Phase:
Survivors:
Yes
Schedule:
Chicago – Pittsburgh
MSN:
2588
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
12811
Captain / Total hours on type:
2365.00
Circumstances:
During the takeoff roll at Chicago-Merrill C. Meigs Airport, prior to V1 speed, a fire warning alarm sounded. The crew decided to abort the takeoff and started an emergency braking procedure. Unable to stop within the remaining distance, the twin engine aircraft overran and plunged into Lake Michigan. All eight occupants were evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Inadequate preflight preparation and/or planning on part of the flying crew. The following findings were reported:
- Inadequate maintenance and inspection on part of the maintenance personnel,
- Parts were missing on the exhaust system: manifolds,
- Despite the takeoff was interrupted prior to V1, the remaining distance was insufficient as the runway was slick and too short,
- False fire warning,
- Airport conditions.
Final Report: