Crash of a Boeing KC-135A-BN Stratotanker in Greenwood: 27 killed

Date & Time: Mar 19, 1982 at 2110 LT
Type of aircraft:
Operator:
Registration:
58-0031
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sawyer - Chicago
MSN:
17776/246
YOM:
1959
Crew on board:
4
Crew fatalities:
Pax on board:
23
Pax fatalities:
Other fatalities:
Total fatalities:
27
Aircraft flight hours:
9249
Circumstances:
The four engine airplane departed Kenneth Ingalls Sawyer AFB on a flight to Chicago-O'Hare Airport, carrying 23 passengers and a crew of four. After being cleared to descend from 22,000 feet to 8,000 feet, the crew reduced his speed when at an altitude of 13,700 feet, at a speed of 313 knots, the airplane suffered an in-flight explosion. Both wings detached, all four engines separated as well as the stabs and out of control, the airplane dove into the ground and crashed in an open field located in Greenwood, about 37 miles northwest of Chicago Airport. The aircraft was totally destroyed and all 27 occupants were killed.
Probable cause:
The exact cause of the accident could not be determined with certainty. Considered as 'most probable' was an over-pressurization under the cargo floor, an area that houses fuel and other potential sources of ignition. An explosion caused by the ignition of accumulated combustible vapors occurring in that area could, in fact, rapidly propagate to adjacent areas where fuel is present. There was also 'strong evidence' of explosive over-pressures in the forward, aft and upper fuel tank areas. Significantly, investigation showed that were the walls or fittings of the rubber bladder cells containing the volatile liquid to fail, fuel or vapor could be released into the tank cavity and in turn migrate to other part of the aircraft.

Crash of a Cessna 340 in Saint Charles: 2 killed

Date & Time: Jul 18, 1981 at 2102 LT
Type of aircraft:
Registration:
N5416J
Flight Type:
Survivors:
Yes
Schedule:
Sioux Center - DuPage
MSN:
340-0106
YOM:
1972
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1503
Captain / Total hours on type:
452.00
Circumstances:
During initial approach to DuPage Airport while on flight from Sioux Center, Iowa, the twin engine airplane stalled and crashed in St Charles, few miles from the airfield. The pilot and a passenger were killed while three other passengers were seriously injured.
Probable cause:
Stall during initial approach after the pilot failed to maintain flying speed. The following contributing factors were reported:
- The pilot failed to follow approved procedures,
- Propeller controls not advanced.
Final Report:

Crash of a Cessna 340A in Aurora

Date & Time: Jan 21, 1981 at 1107 LT
Type of aircraft:
Registration:
N26711
Flight Type:
Survivors:
Yes
Schedule:
Aurora - Aurora
MSN:
340A-0748
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5498
Captain / Total hours on type:
69.00
Circumstances:
The crew (one engineer and two pilots) departed Aurora-Sugar Grove for a local post maintenance test flight. While approaching the airport in poor weather conditions with limited visibility due to freezing fog, both engines lost power as the induction systems were iced. The crew attempted an emergency landing when the airplane crashed. All three occupants were seriously injured.
Probable cause:
Controlled collision with ground on final approach due to improper operation of powerplant and powerplant controls. The following contributing factors were reported:
- Improper operation of the anti-icing/deicing equipment or failed to use it,
- Ice induction,
- Airframe ice,
- Icing conditions including sleet and freezing rain,
- Conditions conducive to carburetor/induction system icing,
- Forced landing on airport,
- Airframe buffet,
- Adverse/unfavorable weather,
- Visibility one mile or less,
- Fog,
- Test flight check of radios and pressurization,
- 233 lbs over max weight at takeoff, within limits at the time of the accident.
Final Report:

Crash of a Rockwell Grand Commander 680FL in Chicago: 1 killed

Date & Time: Sep 3, 1980 at 0453 LT
Operator:
Registration:
N4700E
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Chicago - Peoria - Bloomington
MSN:
680-1779-148
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2079
Captain / Total hours on type:
10.00
Circumstances:
After takeoff from Chicago-Midway Airport, on a cargo flight to Bloomington via Peoria, the pilot encountered a loss of power on the left engine. The pilot attempted to return for an emergency landing when the airplane entered a tight turn, lost height, struck trees and crashed in a wooded area, bursting into flames. The pilot, sole on board, was killed.
Probable cause:
Engine failure due to valve assemblies material failure. The following contributing factors were reported:
- The pilot failed to follow approved procedures,
- Forced landing off airport on land,
- N°5 exhaust valve seat in left engine came out of recession,
- Witness observed aircraft in tight turn back to airport.
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 Douglas DC-10-10 in Chicago: 273 killed

Date & Time: May 25, 1979 at 1504 LT
Type of aircraft:
Operator:
Registration:
N110AA
Flight Phase:
Survivors:
No
Schedule:
Chicago - Los Angeles
MSN:
46510/22
YOM:
1971
Flight number:
AA191
Crew on board:
13
Crew fatalities:
Pax on board:
258
Pax fatalities:
Other fatalities:
Total fatalities:
273
Captain / Total flying hours:
22500
Captain / Total hours on type:
3000.00
Copilot / Total flying hours:
9275
Copilot / Total hours on type:
1200
Aircraft flight hours:
19871
Circumstances:
American Airlines Flight 191, a McDonnell-Douglas DC-10-10, crashed on takeoff from Chicago-O'Hare International Airport, Illinois, USA. The aircraft was destroyed and all 271 occupants were killed. Additionally, two persons on the ground sustained fatal injuries. At 14:59 hours local time Flight 191 taxied from the gate at O'Hare Airport. The flight was bound for Los Angeles, California, with 258 passengers and 13 crew members on board. Maintenance personnel who monitored the flight's engine start, push-back, and start of taxi did not observe anything out of the ordinary. The weather at the time of departure was clear, and the reported surface wind was 020° at 22 kts. Flight 191 was cleared to taxi to runway 32R for takeoff. The company's Takeoff Data Card showed that the stabilizer trim setting was 5° aircraft nose up, the takeoff flap setting was 10°, and the takeoff gross weight was 379,000 lbs. The target low pressure compressor (N1) rpm setting was 99.4 percent, critical engine failure speed (V1) was 139 kts indicated airspeed (KIAS), rotation speed (VR) was 145 KIAS, and takeoff safety speed (V2) was 153 KIAS. Flight 191 was cleared to taxi into position on runway 32R and hold. At 15:02:38, the flight was cleared for takeoff, and at 15:02:46 the captain acknowledged, "American one ninety-one under way." The takeoff roll was normal until just before rotation at which time sections of the No.1 (left) engine pylon structure came off the aircraft. Witnesses saw white smoke or vapor coming from the vicinity of the No. 1 engine pylon. During rotation the entire No. 1 engine and pylon separated from the aircraft, went over the top of the wing, and fell to the runway. Flight 191 lifted off about 6,000 ft down runway 32R, climbed out in a wings-level attitude. About nine seconds after liftoff, the airplane had accelerated to 172 knots and reached 140 feet of altitude. As the climb continued, the airplane began to decelerate at a rate of about one knot per second, and at 20 seconds after liftoff, and an altitude of 325 feet, airspeed had been reduced to 159 knots. At this point, the airplane began to roll to the left, countered by rudder and aileron inputs. The airplane continued to roll until impact, 31 seconds after liftoff, and in a 112-degree left roll, and 21-degree nose down pitch attitude. At 15:04 Flight 191 crashed in an open field and trailer park about 4,600 ft northwest of the departure end of runway 32R. The aircraft was demolished during the impact, explosion, and ground fire. The No.1 engine pylon failure during takeoff was determined to have been caused by unintended structural damage which occurred during engine/pylon reinstallation using a forklift. The engine/pylon removal and reinstallation were being conducted to implement two DC-10 Service Bulletins. Both required that the pylons be removed, and recommended that this be accomplished with the engines removed. The Service Bulletin instructions assumed that engines and pylons would be removed separately, and did not provide instructions to remove the engine and pylon as a unit. Additionally, removal of the engines and pylons as a unit was not an approved Maintenance Manual procedure. The lack of precision associated with the use of the forklift, essentially an inability to perform the fine manipulations necessary to accomplish reinstallation of the engine/strut assembly, in combination with the tight clearances between the pylon flange and the wing clevis resulted in damage to the same part that had just been inspected. Inspections of other DC-10 pylon mounts following the accident resulted in nine additional cracked mounts being identified.
Probable cause:
The asymmetrical stall and the ensuing roll of the aircraft because of the uncommanded retraction of the left wing outboard leading edge slats and the loss of stall warning and slat disagreement indication systems resulting from maintenance-induced damage leading to the separation of the no.1 engine and pylon assembly procedures which led to failure of the pylon structure. Contributing to the cause of the accident were the vulnerability of the design of the pylon attach points to maintenance damage; the vulnerability of the design of the leading edge slat system to the damage which produced asymmetry; deficiencies in FAA surveillance and reporting systems which failed to detect and prevent the use of improper maintenance procedures; deficiencies in the practices and communications among the operators, the manufacturer, and the FAA which failed to determine and disseminate the particulars regarding previous maintenance damage incidents; and the intolerance of prescribed operational procedures to this unique emergency.
Final Report:

Crash of a Beechcraft E18 in Chicago

Date & Time: Apr 3, 1979 at 0439 LT
Type of aircraft:
Operator:
Registration:
N1234G
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Chicago - Indianapolis
MSN:
BA-21
YOM:
1954
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15700
Captain / Total hours on type:
3060.00
Circumstances:
At liftoff, the twin engine airplane stalled and crashed in flames. The pilot, sole on board, was injured. He was en route to Indianapolis.
Probable cause:
Uncontrolled collision with ground during initial climb due to vortex turbulence. The pilot failed to follow approved procedures.
Final Report:

Crash of a Beechcraft 65-80 Queen Air in Palwaukee: 1 killed

Date & Time: Mar 29, 1979 at 1745 LT
Type of aircraft:
Operator:
Registration:
N723Q
Survivors:
No
Schedule:
Wheeling - Chicago
MSN:
LD-112
YOM:
1963
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8000
Circumstances:
After takeoff from Wheeling-Palwaukee Airport, while climbing, the pilot declared an emergency after an explosion on the left engine. He was cleared to return for an emergency landing and continued the approach when, upon touchdown, the airplane went out of control and crashed in flames. The pilot, sole on board, was killed.
Probable cause:
Failure of the left engine during climb due to master and connecting rods failure. The following contributing factors were reported:
- Fire and explosion in flight,
- Material failure,
- Leak,
- Fire in engine,
- Complete engine failure,
- N°5 connecting rod,
- Hole in oil sump,
- Left wing and left main gear failed on landing.
Final Report:

Crash of a Piper PA-31-310 Navajo in Savoy: 6 killed

Date & Time: Sep 9, 1978 at 1826 LT
Type of aircraft:
Operator:
Registration:
N26AN
Flight Phase:
Survivors:
No
Schedule:
Savoy - Cleveland
MSN:
31-57
YOM:
1968
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
1502
Captain / Total hours on type:
49.00
Circumstances:
Shortly after takeoff from Savoy-Willard Airport, while climbing, the airplane suffered an engine failure. The pilot lost control of the airplane that crashed in an open field located near Champaign. The aircraft was totally destroyed and all six occupants were killed.
Probable cause:
Engine failure during initial climb due to master and connecting rods failure. The following contributing factors were reported:
- Material failure,
- Improper in-flight decisions,
- Improper emergency procedures,
- Failed to maintain flying speed,
- Connecting rod bolt or nut failure for undetermined reasons,
- Pilot FAA check not completed.
Final Report: