Crash of a Short SC.7 Skyvan 3 Variant 200 in Pittsburgh

Date & Time: Sep 16, 1996 at 2200 LT
Type of aircraft:
Operator:
Registration:
N10DA
Flight Type:
Survivors:
Yes
Schedule:
Clarksburg - Pittsburgh
MSN:
1873
YOM:
1969
Flight number:
SBX1215
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11000
Captain / Total hours on type:
1100.00
Aircraft flight hours:
18553
Circumstances:
The pilot had flown this route in make and model airplane for nearly 4 years. He calculated 900 pounds of fuel were required for the flight, and saw 956 pounds on the fuel totalizer. The pilot was told by the ground controller of weather delays to his destination that ranged up to 2.5 hours. En route he was issued holding instructions with an EFC of 50 minutes later. After released from holding, 52 minutes after takeoff, the pilot was told that he was being vectored for a 35 mile final approach. The pilot then told the controller that he was fuel critical and the controller vectored him ahead of other airplanes. Ten minutes later, 84 minutes after takeoff, the controller asked his fuel status, and the pilot responded 'pretty low, seems like I'm losing oil pressure.' The pilot then advised the controller, 85 minutes after takeoff, that he shut down the right engine. He then declared an emergency and advised that he was not going to make the airport. Examination of the wreckage revealed the fuel tanks were intact, the fuel caps were secured, and the amount of fuel recovered from both tanks was 1.5 gallons, which was less than the specified unusable quantity. Company records showed that similar flights took about 48 minutes, and the airplane's average fuel flow was 580 pounds per hour.
Probable cause:
The pilot's improper in-flight decision to continue to his destination when known en route delays were encountered which resulted in fuel exhaustion.
Final Report:

Crash of a Piper PA-31P-425 Pressurized Navajo in Lost Creek: 4 killed

Date & Time: Jul 20, 1983 at 1040 LT
Type of aircraft:
Operator:
Registration:
N234LC
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Clarksburg - Lost Creek - Memphis
MSN:
31-7400178
YOM:
1974
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
18900
Captain / Total hours on type:
2400.00
Circumstances:
The aircraft took off with 4 occupants and an estimated 596 lbs of cargo on board. After it took off, the ATC controller noted that it was climbing slower than expected. After climbing to about 4,200 feet msl, the aircrew reported a problem with the left engine and said they did not believe they could make it back to the departure airport. They expressed a desire to continue toward the southwest. ATC proceeded to vector them to the Weston Airport, but informed them that it had no instrument approach. After the reported engine malfunction, ATC personnel noted that the aircraft continued in a gradual left turn. About 8 minutes after takeoff, radio contact was lost. A witness on the ground saw the aircraft come over a hill with the sound of an engine at high power. At about that time, the aircraft collided with a power line cable, then crashed into two trees, impacted the ground and burned. An examination of the wreckage revealed no significant preimpact failures. The aircraft was estimated to be approximately 400 lbs over its max certificated gross weight. All four occupants were killed.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: climb - to cruise
Findings
1. (c) reason for occurrence undetermined
----------
Occurrence #2: forced landing
Phase of operation: approach
Findings
2. (f) aircraft weight and balance - exceeded - pilot in command
----------
Occurrence #3: in flight collision with object
Phase of operation: approach
Findings
3. (f) weather condition - low ceiling
4. (f) weather condition - fog
5. (f) object - wire,transmission
6. (f) object - tree(s)
----------
Occurrence #4: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Nord 262A-36 in Clarksburg: 2 killed

Date & Time: Feb 12, 1979 at 1300 LT
Type of aircraft:
Operator:
Registration:
N29824
Flight Phase:
Survivors:
Yes
Schedule:
Clarksburg – Washington DC
MSN:
48
YOM:
1968
Flight number:
AL561
Crew on board:
3
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
4028
Captain / Total hours on type:
528.00
Copilot / Total flying hours:
7474
Copilot / Total hours on type:
474
Aircraft flight hours:
9140
Circumstances:
On February 12, 1979, Allegheny Airlines Flight 561 (N29824) had originally departed Benedum Airport, Clarksburg, West Virginia, for Morgantown, West Virginia, at 1116, but the pilot decided not to make an approach at Morgantown because the instrument landing system's (ILS) glide slope was out of service, and the visibility was 1/2 mi. Thereafter the flight returned to Benedum Airport and landed at 1146. The aircraft was on the ground for about 1 hr 14 min at Benedum Airport. During that time the aircraft was refueled to 3,000 lbs of Jet-A fuel (1,500 lbs in each wing tank), and all surfaces were deiced with a mixture of unheated ethylene glycol and water. Although the Safety Board could not determine the precise time of deicing, the persons involved stated that it was performed between 1220 and 1235. The persons involved stated that it was performed between 1220 and 1235. The persons who deiced the plane stated that there was no snow or ice on the aircraft when they finished decing it. Flight 561 was rescheduled as a passenger flight from Benedum Airport to National Airport, Washington, D.C. There were 22 passengers and a crew of 3 on board. Before the captain started the engines for taxiing, the station agent asked him if he wanted the aircraft deiced again, since it was still snowing. The captain declined the offer and about 1257 he taxied the aircraft from the parking ramp. According to the station agent, the aircraft had about 1/4 in. of wet snow on all its horizontal surfaces when it left the parking ramp. He said that some of the snow blew off as the aircraft moved toward the departure runway, but some of the snow appeared to stick to the aircraft's horizontal surfaces. Twelve of the passengers recalled that shortly after liftoff, the aircraft rolled to the right, back to the left, and back to the right. After the last roll, the right wingtip struck the ground and impact followed shortly thereafter. The aircraft crashed in an inverted position off the right side of the departure end of runway 21. According to other witnesses, the ground roll appeared normal. The Clarksburg Tower local controller said that he saw Flight 561 taxi to runway 21, and he cleared the flight for takeoff. He saw the aircraft during takeoff until it reached taxiway D, which is about 1,000 ft from the tower, but he did not see the aircraft after that point. He had spoken with the captain by telephone before the takeoff and had given him the 1215 special observation weather. He also radioed the same weather to Flight 561 when it was taxiing for takeoff. He stated that he saw no snow on the aircraft but that moderate snow was falling at the time. The Clarksburg approach controller said that he saw Flight 561 as it turned to line up for takeoff on runway 21. He watched the aircraft through binoculars and saw nothing abnormal as the takeoff roll began. He thought the aircraft was rotated about 1,900 ft down the runway and the liftoff appeared to him to be normal. He lost sight of the aircraft at 50 ft of altitude because of the poor visibility. He recalled that during Flight 561's takeoff, the runway lights were set at their highest intensity. He also stated that he saw no snow blow off the aircraft during its takeoff roll. Shortly after the aircraft disappeared from his view, he heard the sound of an emergency locator transmitter on 121.5 MHz. He asked the Cleveland Center controller if Flight 561 had established contact with him. Since his reply was negative, the approach controller closed the airport and activated the airport emergency plan. The control tower chief observed Flight 561 during takeoff. He lost sight of the aircraft when it was at an altitude of about 20 ft above the runway. At that time the aircraft's attitude appeared to be normal. A pilot in the terminal restaurant said that when the aircraft left the parking ramp, he saw about 1/2 to 1 in. of snow on the wing and tail surfaces of the aircraft. He said that the takeoff appeared normal; but, just before the aircraft disappeared into the overcast, it appeared to pitch up sharply. Another witness who had experience as a pilot was located on taxiway C about 75 ft from the runway. He thought the aircraft lifted off about 200 to 300 ft past taxiway C. Shortly after liftoff, he saw the right wing of the aircraft dip about 45°, then the left wing dipped about the same amount, and the right wing dipped again before the aircraft disappeared from his view about 100 ft above the runway. Shortly thereafter, he heard two separate and distinct sounds of impact. The witness heard no unusual engine noises from the aircraft. The aircraft crashed during daylight hours at an elevation of 1,203 ft ms1. A passenger and a crew member were killed while 23 other occupants were injured, some of them seriously.
Probable cause:
The National Transportation Safety Board determines that the probable cause of the accident was the captain's decision to take off with snow on the aircraft's wing and empennage surfaces which resulted in a loss of lateral control and a loss of lift as the aircraft ascended out of ground effect. The following findings were reported:
- The aircraft had been deiced 20 to 30 min before takeoff; however, about 1/4 in. of wet snow had accumulated on the top of the wings and horizontal stabilizer before the captain taxied the aircraft for takeoff,
- The captain of Flight 561 did not insure that the aircraft's wings, stabilizing surfaces, and control surfaces were clean and free of snow before he began the takeoff roll,
- Shortly after liftoff, the aircraft became laterally unstable; it rolled to the right, then to the left, back to the right, and its right wing struck the runway,
- The snow adhering to the outboard sections of the wing probably caused those sections to stall prematurely,
- The stalling of the outboard sections of the wings caused a loss of lift and significantly reduced the effectiveness of the ailerons, which resulted in lateral control problems and lateral instability,
- The lateral oscillation of the aircraft further decreased lift and caused the aircraft to lose altitude and crash,
- One passenger was fatally injured because her seatbelt was not fastened,
- The accident was marginally survivable for the flight crew because the cockpit structure was crushed inward, which reduced the occupiable space, particularly for the first officer.
Final Report:

Crash of a Douglas C-47A-75-DL in Clarksburg: 3 killed

Date & Time: Jun 22, 1957 at 0750 LT
Operator:
Registration:
N88835
Flight Type:
Survivors:
No
Schedule:
Washington - Washington
MSN:
19448
YOM:
1944
Flight number:
H-3
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
4342
Captain / Total hours on type:
961.00
Copilot / Total flying hours:
6248
Copilot / Total hours on type:
3138
Aircraft flight hours:
14168
Circumstances:
Training flight H-3 was scheduled by Capital (Capital Airlines) flight training department for Captain Carl R. Burke, instructor, and two Copilots, Henry A. Podgurski and Robert K. Thomas. This was the second of a series of six flights being made for the purpose of giving Messrs. Podgurski and Thomas flight instruction to prepare them for upgrading from copilot to captain. The flight was dispatched in accordance with visual flight rules to operate in an area northwest, north, and northeast of Washington, D. C. This area was used by Capital as its local practice area for training flights. The aircraft was fully serviced with 820 gallons of fuel. Its gross takeoff weight was less than the max allowable and the center of gravity was within allowable limits. The weather was clear and was not a factor in thin accident. Takeoff was made at 0625. At 0631 the flight advised the company by radio of the trip number, time of takeoff, fuel aboard, and flight duration. There were no other radio contacts with the flight. At approximately 0745, N88835 was observed in the vicinity of Clarksburg, Maryland, by many people who saw it during several tea of flight and in its plunge to the ground.
Probable cause:
The Board determines that the probable cause of this accident was loss of airspeed while executing maneuvers during a training flight, resulting in a stall followed immediately by a spin from an altitude too low to effect recovery. The following findings were reported:
- No malfunctioning of the aircraft, engines, or control systems was evident from the examination of the wreckage,
- The pilots were executing a "canyon approach" maneuver at an altitude approximately 2,500 feet above the terrain (3,000 feet msl),
- During the abandon-approach phase of this maneuver the aircraft was inadvertently stalled from which it entered a spin and crashed,
- Although rotation had stopped before impact occurred there was insufficient altitude to effect a recovery.
Final Report:

Crash of a Boeing 247D in Charleston

Date & Time: Apr 16, 1941 at 1633 LT
Type of aircraft:
Operator:
Registration:
NC13359
Flight Phase:
Survivors:
Yes
Schedule:
Knoxville – Bristol – Charleston – Clarksburg – Pittsburgh
MSN:
1741
YOM:
1932
Flight number:
PCA143
Crew on board:
3
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
2327
Captain / Total hours on type:
947.00
Copilot / Total flying hours:
1474
Copilot / Total hours on type:
212
Aircraft flight hours:
14866
Circumstances:
Shortly after takeoff from Charleston Airport, while climbing, the right engine failed. The pilot lost control of the airplane that stalled and crashed in a wooded area located near the airport. All nine occupants were injured and the aircraft was destroyed by impact forces. There was no fire.
Crew:
Russell J. Wright, captain,
William H. Riley, first officer,
Irene Coates, flight stewardess.
Probable cause:
Loss of power in the right engine due to causes unknown.
Contributing factors were:
- Failure of PCA to establish adequate procedures to require its pilots to be familiar with the terrain surrounding airports, and failure of Captain Wright to familiarize himself adequately with the terrain surrounding the Charleston Municipal Airport.
- Failure of PCA to inform its pilots of the amount of power which could reasonably be taken from Pratt and Whitney Wasp S1H1-G engines under emergency conditions, and the consequent hesitancy of Captain Wright to exercise his emergency authority and use additional power soon enough to clear the ridge.
Final Report: