Crash of a Mitsubishi MU-2B-60 Marquise near Burlington: 1 killed

Date & Time: Apr 19, 1984 at 2022 LT
Type of aircraft:
Registration:
N466MA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Burlington - Windsor Locks
MSN:
1540
YOM:
1981
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5700
Captain / Total hours on type:
3200.00
Aircraft flight hours:
7890
Circumstances:
The aircraft was flown earlier in the day for a sales demonstration. On the return flight, when the landing gear were lowered, the pilot thought he heard a noise emitting from the gear, although cockpit indications were normal. The aircraft landed at Johnny Cake Airport and was refueled for a flight to Bradley Field where it is hangared. The pilot stated he intended to make the 22 miles flight with the gear down as a precaution. He also stated his intention to fly below the overcast because of delays of up to 45 minutes in obtaining IFR clearances. Moments after takeoff the aircraft collided with trees east of the airport. About one mile east of the airport is a north-south ridge. Another pilot, who departed 15-20 mins earlier, reported entering the overcast between 400 and 700 feet agl. Ground witnesses one mile southeast of the airport who heard the crash described the weather as heavy fog and mist. One witness estimated the ceiling as 100 feet agl. The pilot, sole on board, was killed.
Probable cause:
Occurrence #1: in flight encounter with weather
Phase of operation: cruise
Findings
1. (f) weather condition - low ceiling
2. (c) VFR flight into imc - initiated - pilot in command
----------
Occurrence #2: in flight collision with object
Phase of operation: cruise
Findings
3. (f) object - tree(s)
4. (c) altitude - inadequate - pilot in command
5. (f) light condition - dark night
Final Report:

Crash of a Beechcraft E18S in Windsor Locks: 1 killed

Date & Time: Sep 19, 1979 at 0404 LT
Type of aircraft:
Operator:
Registration:
N705M
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Windsor Locks – Baltimore
MSN:
BA-353
YOM:
1958
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
6425
Captain / Total hours on type:
125.00
Circumstances:
Shortly after a night takeoff from Windsor Locks-Bradley Airport, while on a cargo flight to Baltimore, the twin engine airplane stalled and crashed in flames. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Uncontrolled collision with ground during initial climb following an inadequate preflight preparation. The following contributing factors were reported:
- Cargo shifted after rotation,
- Improperly loaded aircraft,
- Tie-down snaps, rings found disconnected,
- Aircraft 682 pounds over max gross weight.
Final Report:

Crash of a Beechcraft E18S in Albany

Date & Time: Sep 1, 1978 at 2046 LT
Type of aircraft:
Operator:
Registration:
N58H
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Albany – Windsor Locks
MSN:
BA-250
YOM:
1957
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4618
Captain / Total hours on type:
214.00
Circumstances:
After takeoff from Albany Airport, while in initial climb, the left engine failed. The airplane lost height then struck the ground and crashed near the airport. The pilot, sole on board, was slightly injured and the aircraft was destroyed.
Probable cause:
Engine failure during initial climb for undetermined reasons. The following contributing factors were reported:
- Failed to follow approved procedures,
- Improper emergency procedures,
- Forced landing off airport on land,
- Failed engine not feathered.
Final Report:

Crash of a Mitsubishi MU-2B-26A near Manchester: 2 killed

Date & Time: Aug 28, 1978 at 1317 LT
Type of aircraft:
Registration:
N765MA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Manchester - Windsor Locks
MSN:
372
YOM:
1978
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
15679
Captain / Total hours on type:
50.00
Circumstances:
Shortly after takeoff from Manchester Airport, while climbing, the crew reported compass problem when the airplane entered an uncontrolled descent and crashed in Bedford, about four miles west of the airport. The aircraft was destroyed and both occupants were killed.
Probable cause:
Uncontrolled descent and subsequent crash after the crew diverted attention from operation of aircraft. The following contributing factors were reported:
- Flight and navigation instruments: other,
- Low ceiling,
- Visibility 4 miles or less.
Final Report:

Crash of a Beechcraft D18 in Windsor Locks

Date & Time: Jun 19, 1978 at 2030 LT
Type of aircraft:
Registration:
N10VT
Flight Type:
Survivors:
Yes
Schedule:
Albany – Windsor Locks
MSN:
A-699
YOM:
1952
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3496
Captain / Total hours on type:
1003.00
Circumstances:
On final approach to Windsor Locks-Bradley Airport, the left engine lost power and the right engine failed. The crew attempted an emergency landing when the airplane struck trees and crashed in flames. Both occupants were slightly injured and the aircraft was destroyed.
Probable cause:
Engine failure or malfunction on final approach caused by the following factors:
- Compressor assembly: bearing, rotor shaft,
- Lack of lubrication-specific part, not system,
- Overheated,
- Turbine assembly: blade, turbine wheel,
- Fatigue fracture,
- High obstruction,
- N° 2 bearing on left engine failed,
- Right engine power turbine blade failed.
Final Report:

Crash of a Douglas DC-9-31 in Philadelphia

Date & Time: Jun 23, 1976 at 1712 LT
Type of aircraft:
Operator:
Registration:
N994VJ
Survivors:
Yes
Schedule:
Providence – Windsor Locks – Philadelphia – Nashville – Memphis
MSN:
47333/481
YOM:
1969
Flight number:
AL121
Crew on board:
4
Crew fatalities:
Pax on board:
102
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
25000
Captain / Total hours on type:
6000.00
Copilot / Total flying hours:
11000
Copilot / Total hours on type:
6000
Aircraft flight hours:
21320
Circumstances:
Allegheny Airlines Flight 121, a Douglas DC-9-31, suffered a landing accident on the Philadelphia International Airport, Pennsylvania. Of the 106 persons onboard, 86 persons were injured; there were no fatalities. The captain of Flight 121 had conducted an instrument approach to runway 27R in visual conditions as a thunderstorm passed over the airport in a north-northeasterly direction. When near the threshold the captain initiated a go-around from a low altitude and entered rain of increasing intensity. Shortly thereafter the aircraft was seen descending in a nose-up attitude with the landing gear retracted. After striking tail first on a taxiway about 4,000 feet beyond the threshold of runway 27, the aircraft slid about 2,000 feet and stopped. The wreckage came to rest about 6,000 feet beyond the threshold and about 350 feet to the right of the centerline of runway 27R.
Probable cause:
The aircraft's encounter with severe horizontal and vertical wind shears near the ground as a result of the captain's continued approach into a clearly marginal severe weather condition. The aircraft's ability to cope under these conditions was borderline when flown according to standard operating procedures; however, if the aircraft's full aerodynamic and power capability had been used, the wind shear could probably have been flown through successfully. Contributing to the accident was the tower controller's failure to provide timely below-minimum RVR information.
Final Report:

Crash of a Douglas C-47B-10-DK in Windsor Locks

Date & Time: Jul 16, 1971 at 1521 LT
Operator:
Registration:
N74844
Flight Type:
Survivors:
Yes
Schedule:
Windsor Locks - Beverly
MSN:
15013/26458
YOM:
1944
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
8194
Captain / Total hours on type:
570.00
Circumstances:
The crew departed Windsor Locks-Bradley Airport on a ferry flight to Beverly for a maintenance check. Shortly after takeoff, while climbing, one of the engine lost power and the crew was cleared to return for an emergency landing. On approach, the airplane crash landed few dozen yards short of runway and came to rest in flames. The airplane was damaged beyond repair and all three occupants escaped uninjured.
Probable cause:
Inadequate preflight preparation. The following factors were reported:
- Water in fuel,
- The crew failed to maintain flying speed,
- Lack of familiarity with aircraft,
- Partial loss of power on one engine,
- The aircraft had not flown for about 10 months,
- The pilot was not rated on type, last flew DC-3 in 1967.
Final Report:

Crash of a Douglas DC-4-1009 in Boston: 3 killed

Date & Time: Mar 10, 1964 at 0822 LT
Type of aircraft:
Operator:
Registration:
N384
Flight Type:
Survivors:
No
Schedule:
New York – Windsor Locks – Boston
MSN:
18379
YOM:
1944
Flight number:
SL012
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
6000
Captain / Total hours on type:
814.00
Copilot / Total flying hours:
5824
Copilot / Total hours on type:
4340
Aircraft flight hours:
40233
Circumstances:
Slick Airways Flight 12, a Douglas C-54B-DC, N384, operating as a scheduled cargo flight from John F. Kennedy International Airport, New York, New York, to Logan International Airport, Boston, Massachusetts, with a stop at Bradley Field, Windsor Locks, Connecticut, crashed at 0821:35, March 10, 1964, while making an instrument approach to Runway 4R at Logan International Airport. The aircraft crashed in a lumberyard approximately 7,000 feet from the displaced threshold of Runway 4R and on the extended centerline of that runway. Boston weather at the time was: scattered clouds at 400 feet, overcast at 700 feet, surface visibility 1-1/2 miles in moderate sleet and fog, wind 050 degrees (.JPG">), 22 knots, gusts to 28 knots, temperature 32 degrees, dewpoint 32 degrees. The captain, first officer, and freight handler, the only occupants, were killed. The aircraft was demolished by impact forces and the ensuing fire.
Probable cause:
The Board determines the probable cause of this accident was loss of balancing forces on the horizontal surface of the aircraft's empennage, due to ice accretion, causing the aircraft to pitch nose down at an altitude too low to effect recovery.
Final Report:

Crash of a Curtiss C-46F-1-CU Commando in Windsor Locks: 2 killed

Date & Time: Mar 4, 1953 at 0150 LT
Type of aircraft:
Operator:
Registration:
N4717N
Flight Type:
Survivors:
No
Schedule:
New York – Windsor Locks – Philadelphia – Cleveland – Detroit – Chicago
MSN:
22400
YOM:
1945
Flight number:
SL1623
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
7742
Captain / Total hours on type:
5092.00
Copilot / Total flying hours:
4074
Copilot / Total hours on type:
1958
Aircraft flight hours:
43310
Circumstances:
At 0139 the pilot advised Bradley Approach Control that the aircraft was over Hartford at 0138 and that he would maintain 3,000 feet to the Bradley Field outer marker. The controller in the Bradley Field tower, who was handling all three radio positions, acknowledged the Hartford position report, gave the flight a time check (0139), and cleared it for an instrument approach with advice that No. 6 was the runway in use. Weather information was also given to the flight: "Wind indicating northeast calm," and Bradley Field 0128 weather conditions - ceiling indefinite 500 feet, obscurement, visibility one and one-half miles, light rain and fog, altimeter 30.01 inches. The pilot was then requested to report over the outer marker when inbound and was advised that the Bradley Field glide path was inoperative until further notice. The glide path had been decommissioned for some time owing to extension of Runway 6; this had been duly published in "Notices to Airmen." At approximately 0141, the pilot asked if the Bradley Field ILS localiser was also inoperative. He was told that the monitoring panel indicated normal operation of all components except the glide path. The pilot replied, "I believe my ILS is cut momentary and I will continue to make an ADF let-down." The flight reported over the outer marker at 0144. The controller acknowledged and asked the pilot if the flight was inbound. The pilot replied "Roger" and the aircraft was cleared to land. The controller advised that the high intensity lights were on intensity 5 (maximum brilliance) and requested the pilot to let the tower know when he wished the intensity lowered, The pilot again acknowledged with "Roger." This was the lest contact with the aircraft. At approximately 0149, the controller requested the pilot to give the aircraft's position. Receiving no response, he then transmitted the following advisory: "If you are experiencing transmitter difficulties and have missed your approach you are cleared to reverse course, climb to 2,500 feet to the outer marker for another approach 2 Several other efforts were made to contact the flight, but to no avail. Following the last contact with the tower, the aircraft was seen and heard flying low to the southwest of Bradley Field just before it struck the trees. The aircraft was destroyed by impact forces and both pilots were killed.
Crew:
Jefferson R. Elliott, pilot,
John Bielak, copilot.
Probable cause:
The Board determines that the probable cause of this accident was that after missing his first approach to the airport, the pilot displayed poor judgment in attempting a circle under the overcast in rain and at night, rather than execute a standard instrument approach. The following findings were pointed out:
- The controller did not receive any information from the pilot that he had missed the first approach, was conducting a missed approach procedure, was circling with visual contact, nor was any request received for clearance to conducts second approach,
- The pilot did not cancel his IFR flight plan at any time,
- There was no evidence of mechanical failure or malfunction of either the aircraft or engines.
Final Report:

Crash of a Lockheed RA-29-LO Hudson near Windsor Locks: 6 killed

Date & Time: Feb 11, 1942 at 1555 LT
Type of aircraft:
Operator:
Registration:
41-23340
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Windsor Locks - Windsor Locks
MSN:
414-6157
YOM:
1941
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The crew departed Windsor Locks-Bradley Airport on an aerial photography on behalf of the 1st Mapping Squadron. While cruising at an altitude of 28,000 feet over the area of Windsor Locks, the airplane suffered a catastrophic failure, apparently lost its tail, entered a dive and crashed near East Granby, west of the airport. All six crew members were killed.
Crew (1st Mapping Squadron):
1st Lt Melvin W. Schoephoester, pilot,
2nd Lt Walter C. Boyle,
S/Sgt Michael M. Kaufman,
Sgt Gordon Johnson,
Sgt Thomas F. Quinn,
Sgt John T. Howey Jr.
Probable cause:
The exact cause of the accident could not be determined because the airplane was totally destroyed by impact forces. Nevertheless, it is possible that the accident was caused by a failure of the automatic pilot system. The following elements were identified:
- Both engine switches were cut, the throttles to the right engine were completely closed, while the throttles to the left engine were completely open, and the fuel selector valve for the right engine was turned off;
- The right propeller appeared to have been feathered, and experts concluded that it was feathered at the time of impact;
- The committee has found no evidence to indicate failure of the wings, it is more likely that the tail break away in flight.