Crash of a Cessna 404 Titan off Olcott: 1 killed

Date & Time: Dec 22, 1977 at 0924 LT
Type of aircraft:
Registration:
N404SA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Oshawa – Buffalo
MSN:
404-0025
YOM:
1976
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4700
Captain / Total hours on type:
51.00
Circumstances:
En route from Oshawa to Buffalo on a cargo flight, the twin engine airplane crashed in unknown circumstances into Lake Ontario off Olcott, New York. Few debris were sighted in heavy seas but no trace of the pilot.
Probable cause:
Due to lack of evidences, the exact cause of the accident could not be determined.
Final Report:

Crash of a Piper PA-31-310 Navajo in Rochester: 1 killed

Date & Time: Jul 20, 1977 at 2152 LT
Type of aircraft:
Operator:
Registration:
N406CA
Flight Type:
Survivors:
No
Schedule:
Buffalo - Rochester
MSN:
31-637
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
8300
Captain / Total hours on type:
7735.00
Circumstances:
While on approach to Rochester-Greater Rochester Airport, the pilot lost control of the airplane that entered a dive and crashed in flames in the Cheektowaga County. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Uncontrolled descent on final approach due to improper operation of flight controls. The following contributing factors were reported:
- Physical impairment,
- Hypertensive hemorrhage of left basal ganglia.
Final Report:

Crash of a Mitsubishi MU-2B-30 Marquise in New York: 7 killed

Date & Time: Apr 5, 1977 at 1431 LT
Type of aircraft:
Registration:
N888RJ
Flight Type:
Survivors:
Yes
Schedule:
Somerset - LaGuardia
MSN:
542
YOM:
1971
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
7
Captain / Total flying hours:
13500
Circumstances:
While approaching LaGuardia Airport in poor weather conditions (low ceiling and fog), both engines failed. The pilot lost control of the airplane that crashed at Pelham Bay Park, Bronx, about five miles north of the airport. A passenger was seriously injured while seven other occupants were killed.
Probable cause:
Double engine failure on approach due to fuel exhaustion. The following contributing factors were reported:
- Inadequate preflight preparation,
- Mismanagement of fuel,
- Fuel exhaustion,
- Low ceiling,
- Fog,
- Fuel quantity gauge - erratic.
Final Report:

Crash of a Piper PA-31-350 Navajo Chieftain off Grand View-On-Hudson: 3 killed

Date & Time: Dec 4, 1976 at 1205 LT
Operator:
Registration:
N59825
Flight Phase:
Survivors:
No
Schedule:
Philadelphia - White Plains
MSN:
31-7652076
YOM:
1976
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3000
Circumstances:
En route from Philadelphia to White Plains with three people on board, the twin engine airplane collided with a Cessna 172 operated by Teterboro Flight Service, registered N75604 and carrying two people. Following the collision, both aircraft went out of control and crashed into the Hudson River near the Tappan Zee Bridge. Both aircraft were destroyed and all five occupants have been killed.
Probable cause:
In-flight collision after the pilot failed to see and avoid other aircraft. The following contributing factors were reported:
- Not under radar contact,
- No control zone,
- Fresh scuff marks on leading edge of deicing boot of vertical stabilizer.
Final Report:

Crash of a Beechcraft 99A Airliner in Poughkeepsie

Date & Time: Mar 16, 1976 at 1630 LT
Type of aircraft:
Operator:
Registration:
N7997R
Flight Phase:
Survivors:
Yes
Schedule:
Poughkeepsie - New York
MSN:
U-119
YOM:
1969
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14159
Captain / Total hours on type:
3343.00
Circumstances:
Just after liftoff from an ice/slush covered runway, the airplane shuddered then rolled left and right, causing the wings to drop. The airplane leveled, crash landed and came to rest in flames. All seven passengers and a pilot were evacuated to safety while a pilot was seriously injured.
Probable cause:
Stall during initial climb after the crew exercised poor judgment. The following contributing factors were reported:
- Inadequate preflight preparation,
- Initiated flight in adverse weather conditions,
- Failed to abort takeoff,
- Failed to maintain flying speed,
- Airport conditions: ice/slush on runway,
- Snow,
- Icing conditions including sleet and freezing rain,
- Visibility 1/2 mile or less,
- Fog,
- Aircraft approximately 368 lbs over gross weight.
Final Report:

Crash of a Mitsubishi MU-2B-20 in Argyle: 1 killed

Date & Time: Feb 18, 1976 at 1520 LT
Type of aircraft:
Operator:
Registration:
N531MA
Flight Phase:
Survivors:
No
Schedule:
Manchester - Bennington
MSN:
130
YOM:
1968
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2897
Captain / Total hours on type:
45.00
Circumstances:
While in initial approach to Bennington-William H. Morse State Airport, the twin engine airplane lost height, stalled and crashed in flames in Argyle, about 26 miles northwest of Bennington Airport. The aircraft was destroyed and the pilot, sole on board, was killed.
Probable cause:
Loss of control after the pilot failed to maintain flying speed. The following contributing factors were reported:
- Lack of familiarity with aircraft,
- Attempted operation beyond experience/ability level,
- Icing conditions including sleet, freezing rain,
- Fog,
- After four day checkout in an aircraft, instructor told the student pilot not to attempt IFR flight until he attended formal school.
Final Report:

Crash of a Rockwell Aero Commander 560 in Skaneateles: 1 killed

Date & Time: Jan 12, 1976 at 1236 LT
Operator:
Registration:
N2692B
Flight Phase:
Survivors:
No
Schedule:
Skaneateles – Salisbury – Wilmington
MSN:
560-192
YOM:
1955
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
11200
Captain / Total hours on type:
3300.00
Circumstances:
Just after liftoff at Skaneateles Airstrip, the twin engine airplane touched the runway and drifted to the left, causing the left main gear to struck a snowbank. The takeoff was continued when the airplane went out of control and rolled inverted. The pilot, sole on board, was killed.
Probable cause:
Ground loop during takeoff run after the pilot diverted attention from operation of aircraft. The following contributing factors were reported:
- Failed to maintain directional control,
- Failed to abort takeoff,
- Failed to follow approved procedures,
- Airport conditions.
Final Report:

Crash of a Douglas DC-10-30C in New York

Date & Time: Nov 12, 1975 at 1310 LT
Type of aircraft:
Operator:
Registration:
N1032F
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
New York - Frankfurt - Jeddah
MSN:
46826
YOM:
1974
Flight number:
OV032
Crew on board:
11
Crew fatalities:
Pax on board:
128
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
25000
Captain / Total hours on type:
2000.00
Copilot / Total flying hours:
14500
Copilot / Total hours on type:
450
Aircraft flight hours:
8193
Circumstances:
The airplane was engaged in a positioning flight from New York to Jeddah via Frankfurt, carrying ONA employees only. The aircraft taxied to runway 13R and commenced takeoff at 13:10. Shortly after accelerating through 100 knots, but before reaching the V1 speed, a flock of birds were seen to rise from the runway. The aircraft struck many birds and the takeoff was rejected. Bird strikes had damaged the no. 3 engine's fan blades, causing rotor imbalance. Fan-booster stage blades began rubbing on the epoxy micro balloon shroud material; pulverized material then entered into the engine's HPC area, ignited and caused the compressor case to separate. A fire erupted in the right wing and no. 3 engine pylon. The aircraft couldn't be stopped on the runway. The pilot-in-command steered the aircraft off the runway onto taxiway Z at a 40 knots speed. The main undercarriage collapsed and the aircraft came to rest against the shoulder of the taxiway. The successful evacuation may be partially attributed to the fact that nearly all passengers were trained crew members.
Probable cause:
The disintegration and subsequent fire in the No.3 engine when it ingested a large number of seagulls. Following the disintegration of the engine, the aircraft failed to decelerate effectively because:
- The n°3 hydraulic system was inoperative, which caused the loss of the n°2 brake system and braking torque to be reduced 50%,
- The n°3 engine thrust reversers were inoperative,
- At least three tyres disintegrated,
- The n°3 system spoiler panels on each wing could not deploy,
- The runway surface was wet.
The following factors contributed to the accident:
- The bird-control program at John F. Kennedy airport did not effectively control the bird hazard on the airport,
- The FAA and the General Electric Company failed to consider the effects of rotor imbalance on the abradable epoxy shroud material when the engine was tested for certification.
Final Report:

Crash of a Boeing 727-225 in New York: 113 killed

Date & Time: Jun 24, 1975 at 1605 LT
Type of aircraft:
Operator:
Registration:
N8845E
Survivors:
Yes
Schedule:
New Orleans - New York
MSN:
20443/837
YOM:
1970
Flight number:
EA066
Crew on board:
8
Crew fatalities:
Pax on board:
116
Pax fatalities:
Other fatalities:
Total fatalities:
113
Captain / Total flying hours:
17381
Captain / Total hours on type:
2813.00
Copilot / Total flying hours:
5063
Copilot / Total hours on type:
4327
Aircraft flight hours:
12206
Circumstances:
Eastern Air Lines Flight 66, a Boeing 727-225 operated as a scheduled passenger flight from New Orleans to New York-JFK. The flight departed New Orleans about 13:19. It proceeded on an IFR flight plan. Eastern 66 arrived in the New York City terminal area without reported difficulty, and, beginning at 15:35:11, Kennedy approach control provided radar vectors to sequence the flight with other traffic and to position it for an ILS approach to runway 22L at the Kennedy airport. The automatic terminal information service (ATIS) reported: "Kennedy weather, VFR, sky partially obscured, estimated ceiling 4,000 broken, 5 miles with haze... wind 210° at 10, altimeter 30.15, Expect vectors to an ILS runway 22L, landing runway 22L, departures are off 22R... " At 15:52:43, the controller transmitted, "All aircraft this frequency, we just went IFR with 2 miles very light rain showers and haze. The runway visual range is---not available, and Eastern 66 descend and maintain four thousand, Kennedy radar one three two four." Eastern 66 acknowledged the transmission. At 15:53:22, the flight contacted the Kennedy final vector controller, who continued to provide radar vectors around thunderstorms in the area, to sequence the flight with other traffic, and to position the flight on the localizer course. The flight crew then discussed the problems associated with carrying minimum fuel loads when confronted with delays in terminal areas. One of the crewmembers stated that he was going to check the weather at the alternate airport, which was LaGuardia Airport (LGA). Less than a minute later, one of the crewmembers remarked, "... one more hour and we'd come down whether we wanted to or not." At 15:59:19, the final vector controller transmitted a message to all aircraft on his frequency that "a severe wind shift" had been reported on the final approach and that he would report more information shortly. Eastern Air Lines Flight 902, a Lockheed L-1011 TriStar, had abandoned its approach to runway 22L earlier. At 15:59:40, Eastern 902 re-established radio communications with the Kennedy final vector controller, and the flight crew reported, "... we had... a pretty good shear pulling us to the right and... down and visibility was nil, nil out over the marker... correction... at 200 feet it was... nothing." The final vector controller responded, "Okay, the shear you say pulled you right and down?" Eastern 902 replied, "Yeah, we were on course and down to about 250 feet. The airspeed dropped to about 10 knots below the bug and our rate of descent was up to 1,500 feet a minute, so we put takeoff power on and we went around at a hundred feet." While Eastern 902 was making this report, the captain of Eastern 66, said, "You know this is asinine." An unidentified crewmember responded, "I wonder if they're covering for themselves." The final vector controller asked Eastern 66 if they had heard Eastern 902's report. Eastern 66 replied, "...affirmative." The controller then established the flight's position as being 5 miles from the outer marker (OM) and cleared the flight for an ILS approach to runway 22L. Eastern 66 acknowledged the clearance at 16:00:54, "Okay, we'll let you know about the conditions." One minute later, the first officer, who was flying the aircraft, called for completion of the final checklist. While the final checklist items were being completed, the captain stated that the radar was, "Up and off... standby." At 16:02:20, the captain said, "...I have the radar on standby in case I need it, I can get it off later." At 16:02:42, the final vector controller asked Eastern 902, "..would you classify that as severe wind shift, correction, shear?" The flight responded, "Affirmative." The first officer of Eastern 66 then said, "Gonna keep a pretty healthy margin on this one. An unidentified crewmember said, "I...would suggest that you do" the first officer responded, "In case he's right." At 16:02:58, Eastern 66 reported over the OM, and the final vector controller cleared the flight to contact the Kennedy tower. The first officer requested 30° of flaps and the aircraft continued to bracket the glideslope with the airspeed oscillating between 140 and 145 knots. At 1603:12, the flight established communications with Kennedy tower local controller and reported that they were, "outer marker, inbound." The Kennedy tower local controller cleared Eastern 66 to land. The captain acknowledged the clearance and asked, "Got any reports on braking action...?" The local controller did not respond until the query was repeated. The local controller replied, "No,none, approach end of runway is wet... but I'd say about the first half is wet--we've had no adverse reports." At 1603:57.7, the flight engineer called, "1000 feet" and at 1604:25, the sound of rain was recorded. The flight was nearly centered on the glideslope when the flight engineer called, "500 feet." The airspeed was oscillating between 140 and 148 knots and the sound of heavy rain could be heard as the aircraft descended below 500 feet. The windshield wipers were switched to high speed. At 16:04:40, the captain said, "Stay on the gauges." The first officer responded, "Oh, yes. I'm right with it." The flight engineer reported, "Three greens, 30 degrees, final checklist," and the captain responded, "Right." At 16:04:52, the captain said, "I have approach lights," and the first officer said, "Okay." The captain then again said, "Stay on the gauges," and the first officer replied, "I'm with it." N8845E then was passing through 400 feet, and its rate of descent increased from an average of about 675 fpm to 1,500 fpm. The aircraft rapidly began to deviate below the glideslope, and 4 seconds later, the airspeed decreased from 138 kts to 123 kts in 2.5 seconds. The Boeing 727 continued to deviate further below the glideslope, and at 16:05:06.2, when the aircraft was at 150 feet, the captain said, "runway in sight." Less than a second later, the first officer said, "I got it." The captain replied, "got it?" and a second later, at 16:05:10, an unintelligible exclamation was recorded, and the first officer commanded, "Takeoff thrust." The airplane contacted the top of the No. 7 approach light tower at an elevation of 27 feet above the mean low-water level and 2,400 feet from the threshold of runway 22L. The aircraft continued and struck towers 8 and 9. The aircraft’s left wing was damaged severely by impact with these towers--the outboard section was severed. The aircraft then rolled into a steep left bank, well in excess of 90°. It contacted the ground and the fuselage struck five other towers. The aircraft then continued to Rockaway Boulevard, where it came to rest. The approach light towers and large boulders along the latter portion of the path caused the fuselage to collapse and disintegrate. A fire had erupted after the left wing failed.
Probable cause:
The aircraft's encounter with adverse winds associated with a very strong thunderstorm located astride the ILS localizer course, which resulted in high descent rate into the non-frangible approach light towers. The flight crew's delayed recognition and correction of the high descent rate were probably associated with their reliance upon visual cues rather than on flight instrument reference. However, the adverse winds might have been too severe for a successful approach and landing even had they relied upon and responded rapidly to the indications of the flight instruments. Contributing to the accident was the continued use of runway 22L when it should have become evident to both air traffic control personnel and the flight crew that a severe weather hazard existed along the approach path.
Final Report:

Crash of a Boeing 727-251 near Thiells: 3 killed

Date & Time: Dec 1, 1974 at 1926 LT
Type of aircraft:
Operator:
Registration:
N274US
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
New York - Buffalo
MSN:
20296/777
YOM:
1969
Flight number:
NW6231
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
7434
Captain / Total hours on type:
1973.00
Copilot / Total flying hours:
1938
Copilot / Total hours on type:
1611
Aircraft flight hours:
10289
Circumstances:
Flight NW6231 departed New York-JFK at 19:14 for a ferry flight to Buffalo and was cleared by departure control to climb to FL140. At 19:21 the flight was cleared to climb to FL310. The aircraft began to climb 2,500 fpm at an airspeed of 305 knots. As the aircraft climbed through FL160, both the airspeed and the rate of climb began to increase. Reaching FL230, the airspeed had reached 405 knots and the rate of climb had exceeded 6,500 fpm. The overspeed warning horn sounded a little later, followed 10 seconds later by a stick shaker stall warning. The aircraft then leveled at 24800 feet with a speed of 420 knots until it turned rapidly to the right, 13 seconds later. The airplane started to descend out of control, reaching a vertical acceleration of +5g until it struck the ground in a slightly nose down and right wing-down attitude. The aircraft had descended from 24000 feet to 1090 feet in 83 seconds.
Probable cause:
The loss of control of the aircraft because the flight crew failed to recognize and correct the aircraft's high-angle-of-attack, low-speed stall and its descending spiral. The stall was precipitated by the flight crew's improper reaction to erroneous airspeed and Mach indications which had resulted from a blockage of the pitot heads by atmospheric icing. Contrary to standard operational procedures, the flight crew had not activated the pitot head heaters.
Final Report: