Crash of a Stinson SR-7C Reliant in New Haven: 4 killed

Date & Time: Oct 10, 1965 at 1743 LT
Type of aircraft:
Registration:
N16113
Flight Type:
Survivors:
No
MSN:
9666
YOM:
1936
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
2500
Captain / Total hours on type:
50.00
Circumstances:
On approach to New Haven-Tweed Airport, the engine failed. The pilot lost control of the aircraft that crashed on the ground. All four occupants were killed.
Probable cause:
Loss of engine accessory drive due to excessive wear of splined gear drive. The pilot-in-command failed to maintain flying spee.
Final Report:

Crash of a Convair CV-240-0 at New Haven

Date & Time: Mar 1, 1958 at 1024 LT
Type of aircraft:
Operator:
Registration:
N94213
Flight Phase:
Survivors:
Yes
Schedule:
Boston – New Haven – Bridgeport – New York
MSN:
23
YOM:
1948
Flight number:
AA535
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7453
Captain / Total hours on type:
4660.00
Copilot / Total flying hours:
5300
Copilot / Total hours on type:
3205
Aircraft flight hours:
20857
Circumstances:
This was scheduled passenger flight 535 of March 1 from Boston, Massachusetts, to New York, New York, with stops planned at New Haven and Bridgeport, Connecticut. The crew, consisting of Captain Edward W. Johnson, First Officer Norman A. Paquette, and Stewardess Marian Sullivan, reported to company operations at Boston well ahead of scheduled departure time. Departure from Boston at 0927 was on time and was in accordance with an TFR clearance to cruise at 6,000 feet via airways to New Haven. The flight was routine and on schedule to New Haven. The aircraft was not refueled during the five-minute stop at New Haven, during which time both engines were stopped. The flight departed the terminal with five passengers and 1460 gallons of fuel. Gross weight of the aircraft was well under the maximum allowable and its center of gravity was located within prescribed limits. The wind was calm and runway 14 (4,116 feet), one of two macadam runways, was selected for takeoff. There is no air traffic control tower at New Haven. After completion of the takeoff checklist, the aircraft moved onto the runway and takeoff was initiated from a tan start without delay. This segment of the flight was being flown by First Officer Paquette who occupied the right seat. Captain Johnson, on the left, maintained directional control during the initial acceleration of the aircraft. Before the aircraft reached the intersection of runways 14 and 19, the landing gear was retracted. The aircraft then skidded clown runway 14 near its center and cane to rest 1,050 feet from the far end. Captain Johnson, Stewardess Sullivan, and three passengers left through the right emergency escape hatch over the wing. First Officer Paquette and the two remaining passengers left through the partially opened front entrance door. Fire, around the left engine and the left outboard wing area, caused considerable damage and was extinguished by the local fire department.
Probable cause:
The Board determines that the probable cause of this accident was the improper technique of the captain resulting in the unintentional retraction of the landing gear prior to V 1 speed, which was made possible by a malfunctioning left gear safety switch. A contributing factor was inadequate inspection by the carrier. The following findings were reported:
- The first officer made the takeoff with the captain performing the duties of copilot from his left seat,
- The aircraft operated normally up to 85 knots in the takeoff roll,
- The captain prematurely applied upward pressure on the landing gear selector handle,
- A defective landing gear safety switch allowed the landing gear selector handle to be unlocked during ground operation of the aircraft, and permitted the landing gear to retract,
- Fire did not develop in the left nacelle and fuel tank area until the aircraft skidded to a stop on the runway,
- The company’s inspection of the safety switch was inadequate.
Final Report:

Crash of a Douglas VC-47D in Holyoke: 4 killed

Date & Time: Nov 4, 1955 at 2346 LT
Operator:
Registration:
43-48276
Flight Type:
Survivors:
Yes
Schedule:
Bolling - Westover
MSN:
14092/25537
YOM:
1944
Crew on board:
8
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
While approaching Westover AFB on a flight from Bolling AFB, the crew encountered engine problems. As he lost height, the pilot-in-command elected to make an emergency landing when the airplane crashed into the Connecticut River in Holyoke, about 4 miles from the airbase. Four crew members were rescued while four others were killed.
Probable cause:
It was determined that the engine problems were caused by carburetor incing.

Crash of a Lockheed 18-56-24 LodeStar in Marlborough: 1 killed

Date & Time: Nov 5, 1954 at 1942 LT
Type of aircraft:
Operator:
Registration:
N9201H
Flight Type:
Survivors:
Yes
Schedule:
LaGuardia – Boston
MSN:
2353
YOM:
1943
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8700
Captain / Total hours on type:
200.00
Copilot / Total flying hours:
1600
Copilot / Total hours on type:
600
Aircraft flight hours:
1500
Circumstances:
At approximately 1845, N9201H departed LaGuardia Airport, New York, on a VFR (Visual Flight Rules) flight to Logan Airport, Boston, Massachusetts. The crew consisted of Captain John K. MacKenzie and Copilot Whitney H. Welch. The passengers were Robert W. Mudge, Raymond J. Halloran, both airline pilots, and Mathew C. Abbott, an electrical engineer. Climbing to an altitude of 3,500 feet m. s. l. (mean sea level), the flight proceeded toward Boston. Approximately 12 miles southeast of Hertford, Connecticut, the right engine became very rough and backfired frequently. The captain was unable to correct this condition and later feathered the right propeller when in the vicinity of Willimantic, Connecticut. A wide right turn was made from a northeasterly to a northwesterly heading toward Bradley Field, Windsor Locks, Connecticut. Communication was established with Bradley Field and the flight was cleared for a straight-in approach to runway 33. The aircraft descended to 2,500 feet m. s. l. during the turn and thereafter continued descending on a northwest heading until it struck trees and crashed. Nearby residents quickly reached the scene, gave assistance and notified authorities. The Bradley Field 1930 weather was: Scattered clouds at 4,500 feet, visibility 15 miles plus, temperature 40 degrees, dewpoint 32, wind northwest 6 m. p. h. La Guardia weather at the time of departure was: Ceiling unlimited, visibility 15 miles plus. Conditions en route were clear with excellent visibility. The twin engine airplane was the property of Mr. John Fox.
Probable cause:
The Board determines that the probable cause of this accident was that after failure of the right engine, accepted single-engine procedure was not followed, which resulted in the aircraft losing altitude and striking the ground. The following findings were reported:
- Weather was not a factor in the accident,
- A structural failure occurred in the power section of the right engine that necessitated feathering of the right propeller,
- Failure to attain single-engine performance resulted in loss of altitude,
- Mechanical difficulties in the left engine reduced power but remaining available power was sufficient for single-engine performance.
Final Report:

Crash of a Lockheed L-1049C Super Constellation in Preston City

Date & Time: Aug 3, 1954 at 0840 LT
Operator:
Registration:
F-BGNA
Survivors:
Yes
Schedule:
Paris – Shannon – New York
MSN:
4510
YOM:
1953
Flight number:
AF075
Crew on board:
8
Crew fatalities:
Pax on board:
29
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11959
Captain / Total hours on type:
453.00
Copilot / Total flying hours:
10679
Copilot / Total hours on type:
453
Aircraft flight hours:
2479
Circumstances:
Air France Flight 075 originated at Orly Field, Paris, August 2, 1954, with a crew consisting of Captain Jean Caboche, Copilot Jean Roussean, Navigator Jacques Geffard., First Flight Engineer Albert Grandvaux, Second Flight Engineer Jean-Baptiste *** Stewardess Francine Dono, First Steward Michael Gallet, and Second Steward Jean Capron. The dispatch office had prepared two flight plans - one for a stop at Gander, Newfoundland, the other with a stop at Shannon, Ireland. Owing to marginal weather at Gander with the forecast indicating no improvement, the captain chose the latter plan. The flight departed Paris at 2024 and arrived Shannon at 2247. Fuel tanks were filled and the pilots ware briefed on weather for the nonstop flight to New York. Flight 075 departed Shannon at 0003 the next morning (August 3), estimating 11 hours 49 minutes an route, with fuel for nearly 14 hours. The gross weight at takeoff, 126,100 pounds, was less than the maximum allowable 133,000, and the load was correctly distributed relative to the canter of gravity of the aircraft. The Atlantic crossing was uneventful. Routine position reports were made en route and the flight periodically received weather reports for points along the route and at the destination. Stronger headwinds than had been anticipated were encountered near the North American continent, resulting in lower ground speed and somewhat higher fuel consumption per mile. The flight had approximately 600 gallons of fuel left at 1230 when it reported over Scotland Intersection (15 statute miles southwest of New York International Airport) and received clearance for an ILS approach. It was then 38 minutes behind its original flight plan estimate made at Shannon and had approximately 100 gallons less fuel than anticipated. During the approach, which was being monitored by New York International Airport radar, the flight encountered unexpected heavy turbulence, heavy rain, and a low ceiling, and the captain discontinued the approach at 1237 (0737 e. s. t.) when near his minimum prescribed altitude of 200 feet. The heavy turbulence made control of the aircraft difficult and when the missed approach was made, the captain found himself left of the localizer and below of glide path. The tower, which was immediately advised of the missed approach, told the flight to turn right to 130 degrees (the missed approach course), proceed to Scotland Intersection, and climb to 2,500 feet. Approximately three minutes after the missed approach and while on the 130-degrees course, the flight requested clearance to Boston. Such clearance was issued nine minutes later, as soon as possible consistent with other traffic. Meanwhile, the flight had reported being low on fuel but when asked if an emergency as being declared replied, "Negative, negative, not yet." At the approximate time clearance to Boston was received the flight engineer advised the captain that they had fuel of one more hour of flight. Thirty-three minutes after being cleared to Boston, the flight, at that time in the vicinity of Providence, Rhode Island, called Providence Tower, declared an emergency, and requested weather information. Providence weather, which was marginal, was furnished and the flight was cleared for an approach. However, the pilots found that their navigation kit did not contain an approach plate for Providence Airport and they advised they were not landing there. The captain then descended through a break in the overcast, circled two or three times, and landed with the gear retracted in a field at Preston City, Connecticut. It came to rest in flames in a garden and was destroyed by a post crash fire. All 37 occupants were evacuated safely. Nevertheless, 12 occupants were injured, among them both pilots.
Probable cause:
The Board determines that the probable cause of this accident was inadequate in-flight planning, in that the captain did not make a firm selection of a suitable airport within range of the fuel remaining at the time of the missed approach, necessitating an off-airport landing. The following findings were reported:
- All fuel tanks were filled to capacity during the scheduled stop at Shannon,
- Owing to headwinds the flight had approximately 100 gallons less fuel than anticipated when it arrived over Scotland Intersection, southwest of New York International Airport,
- In the ILS approach to New York International Airport during instrument weather conditions, the flight encountered an unexpected severe local storm with greater turbulence, heavier rain, and a lower ceiling than weather reports had led them to anticipate, and the captain discontinued the approach at 1237,
- The captain decided not to attempt another approach to New York International Airport and instead requested clearance to Boston at 1240 while climbing on the missed approach course,
- The flight was asked by New York International Airport Approach Control if an emergency was being declared, but the copilot replied in the negative,
- An IFR clearance to Boston was issued by New York ARTC at approximately 1249, the flight in the interim having been routed toward Boston via Mitchel range station,
- When the flight reported over Mitchel range station at 1250, the flight engineer advised the captain, upon the latter's request, that there was fuel for one more hour of flight,
- Difficulties with communications after being cleared from ARTC frequency prevented the flight from receiving the dispatcher's suggestion to proceed to Bridgeport or Hartford,
- Testimony of the pilots indicated that the captain intended to land at an intermediate airport between New York and Boston if he could find one with sufficiently good weather conditions,
- There were no language difficulties in conversations with the flight,
- There was sufficient fuel available to fly to Boston or any intermediate airport, but the fuel remaining over Boston, had the flight continued to that point, would have allowed only about 17 minutes of flight thereafter,
- Flight 075 declared an emergency at 1322 (0822 e. a. t.) in its first contact with Providence Tower/INSAC, indicated intention to land at Providence, was cleared for an approach, and then at 1329, advised that they were not landing there,
- The flight descended through a break in the overcast and made an emergency landing at about 1340 (0840 e. s. t. ) in a field and without loss of life.
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 Douglas DC-3-201E in Cheshire: 17 killed

Date & Time: Jan 18, 1946 at 1103 LT
Type of aircraft:
Operator:
Registration:
NC19970
Flight Phase:
Survivors:
No
Schedule:
La Guardia - Boston
MSN:
3254
YOM:
1940
Flight number:
EA105
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
17
Captain / Total flying hours:
7826
Captain / Total hours on type:
3226.00
Copilot / Total flying hours:
2252
Copilot / Total hours on type:
492
Aircraft flight hours:
22028
Circumstances:
About thirty minutes into the flight, a fire erupted in the left engine. The crew was unable to extinguish the fire that spread quickly to the entire engine and nacelle that detached, causing the wing to partially collapse. The aircraft went out of control, dove into the ground and crashed in flames in a field located in Cheshire. All 17 occupants were killed.
Probable cause:
The probable cause of this accident was the failure of the left wing in flight due to an engine fire caused by the failure of a fuel line connection.
Final Report:

Crash of a Douglas C-39 in Bethel: 2 killed

Date & Time: Nov 30, 1942
Type of aircraft:
Operator:
Registration:
38-516
Flight Phase:
Flight Type:
Survivors:
Yes
MSN:
2073
YOM:
1939
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
En route, the crew encountered poor weather conditions with heavy rain falls. Five crew members were able to bail out. While probably attempting an emergency landing, the crew lost control of the aircraft that crashed in a pasture. Both pilots were killed.

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.

Crash of a Stinson SR-10C Reliant in Higganum: 2 killed

Date & Time: Apr 16, 1940 at 1110 LT
Type of aircraft:
Registration:
NC18482
Flight Phase:
Survivors:
Yes
Schedule:
Boston – New Haven
MSN:
3-5811
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
En route from Boston to New Haven, the pilot encountered engine problems. He attempted an emergency landing when the airplane crashed in the Higganum Reservoir State Park, some 35 km northeast of New Haven Airport. Two passengers were killed and two other occupants were injured.
Probable cause:
Emergency landing following an engine failure in flight.