Zone

Crash of a Piper PA-61 Aerostar (Ted Smith 601) in Altoona: 3 killed

Date & Time: Jun 10, 1998 at 1304 LT
Registration:
N60721
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Altoona – Syracuse
MSN:
61-0736-8063360
YOM:
1980
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1100
Circumstances:
Shortly after the airplane took off, a witness about 1 mile from the airport observed the airplane about 150 feet above the ground in a left turn, before it disappeared into the clouds. A witness across from where the airplane crashed stated he was in his shed when he heard the sound of an airplane overhead. When the sound faded and returned, like the airplane had circled above the shed, he stepped outside and looked for the airplane. He saw the airplane exit the clouds in a near vertical position and impact the ground. He described the engine noise as loud and smooth. The airplane impacted in a field about 3/4 miles from the departure airport and was consumed by a post crash fire. Streaks of oil were observed on the leading edge of the right horizontal stabilizer extending to its upper and lower surfaces. Disassembly of both engines did not reveal any pre-impact mechanical malfunctions. A weather observation taken after the accident reported included a visibility of 2 miles with light drizzle and mist, and the ceiling was 400 foot overcast. Witnesses described the weather at the accident site as '...pretty foggy,' and worse than the conditions reported at the airport.
Probable cause:
The pilot's failure to maintain airspeed due to spatial disorientation, which resulted in an inadvertent stall and subsequent collision with terrain. A factor in the accident was the low ceiling.
Final Report:

Crash of a Volpar Turboliner 18 in Cleveland: 1 killed

Date & Time: Dec 15, 1992 at 0912 LT
Type of aircraft:
Registration:
N706M
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Cleveland - Syracuse
MSN:
12360
YOM:
1970
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4768
Captain / Total hours on type:
91.00
Aircraft flight hours:
16115
Circumstances:
After rotation, during the initial climb, the nose of the airplane pitched up to approximately 60° above the horizon. The airplane continued to climb until about 250 feet above the ground, then rolled right, pitched down and descended. The airplane impacted the ground, approximately 45° nose down, 650 feet to the right of the runway. Post accident investigation of the wreckage revealed the elevator jammed in the full up deflection. The upper end of the elevator control rod was found not connected to the elevator, but was found laying aft, wedged between the tail cone and the elevator faring, holding the elevator in the full up position. The control rod connecting bolt was found laying in the bottom of the tail cone undamaged. The washer, nut and cotter pin related to the control rod connecting bolt were not found. The elevator had been removed, recovered and then installed by company maintenance personnel 166 flight hours prior to the accident. The pilot, sole on board, was killed.
Probable cause:
The improper installation of the elevator by company maintenance personnel and the lack of proper inspections by a company certified mechanic/inspector and the faa certified mechanic with inspector authorization. A factor in this accident was an insufficiently defined maintenance procedures that allowed multiple maintenance tasks to be combined into a single line entry.
Final Report:

Crash of a Cessna 208B Super Cargomaster in Plattsburgh: 1 killed

Date & Time: Jan 29, 1990 at 2033 LT
Type of aircraft:
Operator:
Registration:
N854FE
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Plattsburgh - Syracuse
MSN:
208B-0172
YOM:
1989
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4999
Captain / Total hours on type:
1482.00
Aircraft flight hours:
390
Circumstances:
The Cessna 208B made a takeoff with light wet snow falling, at night. The airplane reached an altitude of 700 feet agl prior to making a steep descent, striking trees and impacting inverted. Radar data showed the aircraft lift off point and initial climb rate approached that shown in the flight manual for short field technique. Two other Cessna 208's preceded the accident aircraft from the same airport, one 13 minutes prior and the other 3 minutes prior. Radar data showed they climbed at a slower rate. The accident airplane had come from a hangar and was not deiced prior to departure. A pilot flying a identical airplane with a similar load commented that his climb rate was lower than normal. Another pilot commented that this was the first wet snow of the year and it was sticking to his engine cowling. The pilot, sole on board, was killed.
Probable cause:
Loss of control inflight after the airplane stalled during climbout. The stall resulted from a loss of lift due to a contaminated wing surface. Contributing to the accident was the failure of the pilot to de-ice the aircraft prior to departure.
Final Report:

Crash of a Learjet 23A in Windsor Locks: 3 killed

Date & Time: Jun 4, 1984 at 2341 LT
Type of aircraft:
Registration:
N101PP
Flight Type:
Survivors:
No
Schedule:
Cleveland – Syracuse – Windsor Locks
MSN:
23-085
YOM:
1966
Flight number:
Night Air 4
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
11039
Captain / Total hours on type:
1130.00
Copilot / Total flying hours:
5263
Copilot / Total hours on type:
189
Aircraft flight hours:
8393
Circumstances:
On June 4, 1984, an unmodified Gates Learjet 23A, N101PP, was being operated by Air Continental, Inc., Elyria, Ohio, on a regularly scheduled cargo flight transporting cancelled bank checks under 14 CFR 135. The flight departed Cleveland-Hopkins International Airport, Ohio, as Night Air 4 at 2200 eastern daylight time. After an uneventful flight, Night Air 4 arrived at Syracuse-Hancock International Airport, New York, at 2245. There was routine ground cargo handling at Syracuse; the airplane was not refueled. Night Air 4 departed Syracuse at 2311, was cleared to climb to 17,000 feet, and was handed off to Boston Air Route Traffic Control Center (Boston Center) at 2314. Boston Center cleared Night Air 4 to its requested altitude of FL290 and the en route portion of the flight was uneventful. At 2332, Night Air 4 was handed off at 16,000 feet during its descent to Bradley International Airport, Windsor Locks, Connecticut Approach Control. Approach control identified the airplane, cleared it for a visual approach to runway 33, and at 2336 gave Night Air 4 a turn to position the airplane on final approach at 10 miles from the airport. At 2338:22, Night Air 4 reported that the airplane was on final approach for runway 33, and at 2338:25 the air traffic control tower operator cleared the flight to land. At 2341:18, the control tower operator reported to approach control that there had been an accident at the airport. Fifteen witnesses, who either heard and/or saw the accident, were interviewed, and with the exception of a few minor points, all of the witnesses described basically the same accident sequence. The airplane was on a normal approach to runway 33 with no apparent abnormalities. When the airplane was about 200 feet over the approach lights, an increase in engine thrust was heard and the airplane halted its rate of descent in what two pilot witnesses thought was an apparent attempt to go-around. Immediately afterward, Night Air 4 began what appeared to be a level turn to the right. As the airplane went through about 90° of turn, the wings of the aircraft were nearly vertical to the ground. The airplane's nose dropped below the horizon and the airplane descended into the ground in a nose low attitude. The witnesses stated that they saw an explosion which was followed by intense ground fire. None of the witnesses reported any significant lateral or vertical changes while the aircraft was on short final or during the 90' right turn prior to its descent into the ground. Many witnesses stated that they saw some lights illuminated on the aircraft but none reported seeing the landing lights, located on the landing gear, or the landing gear in the extended position. Witnesses reported no inflight fire, smoke, or airframe separation before the crash. All three occupants were killed.
Crew:
Charles Huffman, pilot,
Ronald Dulay, copilot.
Passenger:
Eldridge Sheetz.
Probable cause:
An uncommanded roll to the right which caused the airplane to roll about 90°and descend into the ground. The cause of the uncommanded roll was an asymmetric retraction of the flight spoilers wherein the left spoiler retracted and the right spoiler did not. The Safety Board could not determine the reason for the right spoiler malfunction.
Final Report:

Crash of a Beechcraft H18 in Morissonville: 1 killed

Date & Time: Mar 19, 1984 at 2058 LT
Type of aircraft:
Operator:
Registration:
N218X
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Plattsburgh – Morrisonville – Syracuse
MSN:
BA-689
YOM:
1964
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
3473
Captain / Total hours on type:
280.00
Aircraft flight hours:
7395
Circumstances:
The pilot landed on the ice and snow covered runway after loading 1,512 lbs of cargo in freezing drizzle conditions, he taxied for takeoff for an IFR departure shortly after rotation, the right wing dropped and the aircraft touched down back on the runway. Visual exam of the aircraft revealed ice accumulations on the leading edges and upper wing surfaces. The pilot attempted to get deice equipment, which was not available. The pilot was offered use of a hangar which he declined. The airport manager was en route to check runway condition for plowing the ice and snow covered runway when the pilot returned to the aircraft. An unsuccessful attempt was made to remove ice from the leading edges by hand. The pilot decided to attempt another takeoff and at this time was almost 1/2 hour beyond his scheduled departure time. Liftoff was approximately 1/5 of way down and after flying at 50 feet agl initiated climb. After attaining an altitude of several hundred feet, the aircraft stalled and descended uncontrolled to impact. The aircraft was destroyed by impact and fire and the pilot was fatally injured.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
1. (f) weather condition - icing conditions
2. (c) ice/frost removal from aircraft - not attained - pilot in command
3. (c) self-induced pressure - pilot in command
4. (f) wing - ice
5. (f) airport snow removal - not performed - airport personnel
6. (f) stabilizer - ice
7. (f) all available runway - not used - pilot in command
8. (f) terrain condition - icy
9. (f) aircraft performance, takeoff capability - deteriorated
----------
Occurrence #2: in flight collision with object
Phase of operation: descent - uncontrolled
Findings
10. (f) object - tree(s)
Final Report:

Crash of a Piper PA-60 Aerostar (Ted Smith Aerostar 600) in Templeton: 2 killed

Date & Time: Jan 11, 1979 at 1110 LT
Registration:
N8022J
Flight Phase:
Survivors:
No
Schedule:
Boston - Syracuse
MSN:
60-0526-170
YOM:
1978
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1600
Circumstances:
While in cruising altitude in good weather conditions, en route from Boston to Syracuse, the twin engine airplane collided with a Piper PA-31-350 Navajo Chieftain owned by the Tamposi-Nash Real Estate Group and registered N33TN. En route from Concord to White Plains, it was carrying two passengers and one pilot. Following the collision, both aircraft entered a dive and crashed near Templeton. Both aircraft were destroyed and all five occupants were killed.
Probable cause:
In-flight collision with another aircraft after the pilot failed to see and avoid other traffic while cruising in an uncontrolled area.
Final Report:

Crash of a Beechcraft E18S in Milford

Date & Time: Jul 29, 1971 at 2215 LT
Type of aircraft:
Operator:
Registration:
N417R
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Syracuse – New York
MSN:
BA-264
YOM:
1957
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3180
Captain / Total hours on type:
247.00
Circumstances:
While cruising by night on a mail flight from Syracuse to New York, the crew encountered technical problems with an engine. It was decided to jettison the cargo as the crew was unable to maintain a safe altitude. Eventually, the airplane struck trees then crashed in Milford, New York. Both crew were injured, one seriously, and the aircraft was destroyed.
Probable cause:
Powerplant failure due to blower, impeller assembly failure. The following factors were reported:
- Lack of lubrication on specific parts,
- Material failure,
- High obstructions,
- Jettisoned load,
- Forced landing off airport on land,
- Damage to impeller and associated parts resulted from impeller bearing failure.
Final Report:

Crash of a Grumman S-2F Tracker off Syracuse: 2 killed

Date & Time: Apr 1, 1969 at 1100 LT
Type of aircraft:
Operator:
Registration:
MM133073
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sigonella - Sigonella
MSN:
44
YOM:
1957
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew departed Sigonella Airbase for a local training mission when the airplane crashed in unknown circumstances into the sea southeast of Syracuse. Both crew members were killed.
Crew:
Lt Claudio Martinelli,
Lt Rino Meini.

Crash of a Grumman S2F-1 Tracker off Syracuse: 3 killed

Date & Time: Apr 27, 1961
Type of aircraft:
Operator:
Registration:
MM144697
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Syracuse - Syracuse
MSN:
658
YOM:
1958
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While conducting a training flight off Syracuse, the aircraft suffered an engine failure and crashed into the Bay of Augusta. All three crew members were killed.
Crew:
Mr. Bacci,
Mr. Ambroso,
Mr. Farina.
Probable cause:
Engine failure.

Crash of a Convair CV-240-0 in Elizabeth: 30 killed

Date & Time: Jan 22, 1952 at 1544 LT
Type of aircraft:
Operator:
Registration:
N94229
Survivors:
No
Site:
Schedule:
Buffalo – Rochester – Syracuse – Newark
MSN:
54
YOM:
1948
Flight number:
AA6780
Crew on board:
5
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
30
Captain / Total flying hours:
7062
Captain / Total hours on type:
2483.00
Copilot / Total flying hours:
2174
Copilot / Total hours on type:
405
Aircraft flight hours:
6633
Circumstances:
The approach to Newark was completed in marginal weather conditions with a ceiling at 400 feet and a 3/4 mile visibility. For unknown reason, the aircraft deviated from the approach path to the left and, in a relative flat attitude, hit an obstacle and eventually crashed in flames on several houses located in the city of Elizabeth, about three miles from runway 06 threshold. All 23 occupants on board the aircraft and seven people in the ground were killed while nine others were injured. Few houses were destroyed.
Probable cause:
The Board determines that there is insufficient evidence available at this time upon which to predicate a probable cause. The following findings were pointed out:
- The flight was routine from Buffalo and was cleared to descend and make an ILS approach, monitored by GCA, to the Newark airport,
- Weather conditions below the 4,000-foot level at Newark were favorable to the formation of carburetor ice,
- The flight reported over Linden, New Jersey, at 1,500 feet inbound to the airport at 1541,
- The Newark weather conditions at 1540 were reported as indefinite ceiling 400 feet, obscurement, visibility 3/4 mile, light rain and fog, altimeter 29 97,
- The aircraft vanished from the GCA screens at a point approximately 900 feet to the right of the glide path and while at an altitude of 400 feet, due to ground interference,
- The weather information indicated lower ceilings and visibilities near the scene of the accident (about three miles southwest of the airport) than were reported at the airport,
- The aircraft was headed in an easterly direction, below the overcast, in a near level attitude, for a distance of approximately 1,300 feet, before it crashed into buildings.
Final Report: