Crash of a Piper PA-31P Pressurized Navajo in São Paulo: 3 killed

Date & Time: Feb 27, 1978
Type of aircraft:
Registration:
PT-DTK
Flight Phase:
Survivors:
No
Site:
MSN:
31-62
YOM:
1968
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
Shortly after takeoff from São Paulo-Congonhas Airport, while climbing, the pilot encountered an unexpected situation and attempted to return for an emergency landing when the airplane went out of control and crashed in flames on a road located near the airport. All three occupants were killed and two people on the ground were injured.

Crash of a Grumman G-21A Goose in Miami Lakes

Date & Time: Dec 13, 1977 at 1315 LT
Type of aircraft:
Registration:
N23DF
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Miami - Miami
MSN:
1133
YOM:
1942
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
4985
Captain / Total hours on type:
935.00
Circumstances:
While completing a local demo flight at Miami-Opa Locka Airport, both engines failed. The pilot lost control of the airplane that crashed onto several houses in Miami Lakes, west of the airfield. The aircraft was destroyed and both occupants were seriously injured.
Probable cause:
Engine failure during traffic pattern/circling and subsequent collision with buildings due to mismanagement of fuel. The following contributing factors were reported:
- Inattentive to fuel supply,
- Fuel starvation,
- Failed to use the checklist,
- Failure of both engines,
- 70 gallons of fuel in right tank,
- Left tank empty.
Final Report:

Crash of an Avro 748-2-232 in Manila: 5 killed

Date & Time: Oct 18, 1977
Type of aircraft:
Operator:
Registration:
PK-RHS
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Manila - Manila
MSN:
1610
YOM:
1967
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The airplane was involved in a local training flight at Manila-Intl Airport, carrying two passengers and a crew of three. While completing a go-around maneuver with one engine out, the pilot-in-command lost control of the airplane that stalled and crashed into several houses located near the airport. Both pilots and three people on the ground were killed while three other occupants were seriously injured. The aircraft was destroyed.
Probable cause:
The crew overestimated aircraft performances and showed overconfidence. At the time of the accident, the aircraft's speed was too low, causing it to stall.

Crash of a Beechcraft G18S in Coraopolis

Date & Time: Aug 17, 1977 at 0541 LT
Type of aircraft:
Registration:
N75FA
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Pittsburgh - Cleveland
MSN:
BA-498
YOM:
1960
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Shortly after takeoff from Pittsburgh-Intl Airport, while climbing, the right engine failed. The pilot-in-command initiated a right turn and attempted to return to the airport when the airplane stalled and crashed in flames in a residential area located in Coraopolis, about three miles northeast of the airport. The aircraft was destroyed and both pilots were seriously injured. There were no injuries on the ground.
Probable cause:
Engine malfunction and stall during initial climb due to powerplant, fuel system, carburetor failure. The following contributing factors were reported:
- Fuel system, carburetor improperly installed, leakage,
- Failed to follow approved procedures,
- Improper operation of powerplant and powerplant controls,
- Attempted operation with known deficiencies in equipment,
- Forced landing off airport on land,
- Right engine not feathered,
- Turned aircraft toward dead engine while returning to airport.
Final Report:

Crash of a Britten-Norman BN-2A-20 Islander in Caracas

Date & Time: Jun 15, 1977
Type of aircraft:
Operator:
Registration:
YV-O-MAR-6
Flight Type:
Survivors:
Yes
Site:
Schedule:
Puerto Cabello - Caracas
MSN:
203
YOM:
1970
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine airplane was performing a flight from Puerto Cabello to Caracas on behalf of the Venezuelan Government. While approaching the Francisco de Miranda AFB, both engines failed simultaneously. The pilot reduced his altitude and attempted an emergency landing on a highway located in La Araña, about nine km west of the airport. Upon landing, the airplane struck few cars and came to rest. Four occupants were injured while four others were unhurt. No one was hurt on the ground.
Probable cause:
Double engine failure on approach caused by a fuel exhaustion.

Crash of a Hawker-Siddeley HS.125-600A in McLean: 4 killed

Date & Time: Apr 28, 1977 at 2038 LT
Type of aircraft:
Registration:
N40PC
Flight Phase:
Survivors:
No
Site:
Schedule:
Washington DC - Birmingham
MSN:
256010
YOM:
1973
Location:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
7807
Captain / Total hours on type:
1900.00
Copilot / Total flying hours:
4049
Copilot / Total hours on type:
114
Aircraft flight hours:
1904
Circumstances:
The airplane departed Washington-National Airport bound for Birmingham, Alabama. Four minutes later, while climbing to an altitude of 9,300 feet, monitoring radar stations lost continuous reception of the aircraft's primary and secondary radar target information. Shortly thereafter, ground witnesses saw an explosion in the sky followed by the wreckage of the aircraft falling to the ground. the sky was overcast and light rain was falling. The four persons aboard were killed and the aircraft was destroyed. One residence and two automobiles were destroyed by impact and fire and several other homes were damaged by falling debris.
Probable cause:
A failure or malfunction of an undetermined nature in the pilot's attitude indicating system which led to a loss of control and overstress of the aircraft structure.
Final Report:

Crash of a Douglas DC-9-31 in New Hope: 72 killed

Date & Time: Apr 4, 1977 at 1619 LT
Type of aircraft:
Operator:
Registration:
N1335U
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Muscle Shoals - Huntsville - Atlanta
MSN:
47393
YOM:
1970
Flight number:
SO242
Crew on board:
4
Crew fatalities:
Pax on board:
81
Pax fatalities:
Other fatalities:
Total fatalities:
72
Captain / Total flying hours:
19380
Captain / Total hours on type:
3205.00
Copilot / Total flying hours:
3878
Copilot / Total hours on type:
235
Aircraft flight hours:
15405
Circumstances:
Southern Airways Flight 242, a DC-9-31, operated as a scheduled passenger flight from Muscle Shoals, Alabama, to Atlanta, Georgia, with an intermediate stop at Huntsville, Alabama. Flight 242 departed Muscle Shoals at 15:21 and landed at Huntsville about 15:44. About 15:54, Flight 242 departed Huntsville on an instrument flight rules (IFR) flight plan for the Hartsfield-Atlanta International Airport; there were 81 passengers and 4 crew members aboard. The flight's route was direct to the Rome VOR and then a Rome runway 26 profile descent to Atlanta. Its estimated time en route was 25 min and its requested en route altitude was 17,000 ft. At 15:56, the controller told Flight 242 that his radarscope was showing heavy precipitation and that the echos were about 5 nmi ahead of the flight. At 15:57:36, the controller said, "...you're in what appears to be about the heaviest part of it now, what are your flight conditions." Flight 242 replied, "...we're getting a little light turbulence and...I'd say moderate rain." At 15:57:47, the controller acknowledged Flight 242's report and told the flight to contact Memphis Center. The Memphis Center controller advised the flight that a SIGMET was current for the area. He then told Flight 242 to contact Atlanta Center. At 16:03:20, Flight 242 switched to another sector of Atlanta Center, established communications on the new frequency and reported being level at FL170. As the aircraft entered an area of rain, the flight crew began discussing the weather depicted on their radar. Based on information from the airborne radar, the captain initially decided that the storms just west of the Rome VOR were too severe to penetrate. Shortly after his initial assessment of the storm system, the captain decided to penetrate the storm area near the Rome VOR. At 16:06:41 Atlanta Center cleared Flight 242 to descend to and maintain 14,000 ft. Shortly afterwards the aircraft entered an area of heavy hail or rain, which continued for at least one minute. The ingestion of intense rain and hail into the engines caused the rotational speed of both engines to decrease below the engine-driven electrical generator operating speeds, and resulted in normal electrical power interruption for 36 seconds. The flight crew likely advanced one or both thrust levers, restoring its generator to operation and provide normal electrical power. After establishing contact with Atlanta Center again, the flight was told to maintain 15,000 ft. At 16:09:15, Flight 242 reported to Atlanta Center, "Okay...we just got our windshield busted and... we'll try to get it back up to 15, we're 14." After reported that the left engine had flamed out, the flight was cleared to descend to 13,000 ft. Meanwhile both engines' high-pressure compressors began to stall severely due to ingestion of massive quantities of water. The severe compressor stalls produced an overpressure surge which deflected the compressor blades forward in the sixth stage of the low-pressure compressors; these blades clashed against the fifth-stage stator vanes and broke pieces from the blades and vanes. Pieces of blades and stator vanes were then ingested into the high-pressure compressors and damaged them severely. Continued high thrust settings following the severe damage to the high-pressure compressors probably caused severe overheating in the turbine sections of both engines, and the engines ceased to function. Shortly before normal electrical power was again, the flight crew radioed that both engines had failed. Atlanta Center told the crew to contact approach control for vectors to Dobbins Air Force Base. Power was then lost for 2 min 4 sec until the APU-driven generator restored electrical power. After establishing contact with Atlanta Approach Control the flight was told they were 20 miles from Dobbins. As the flight was descending, the captain began to doubt their ability to reach Dobbins. Cartersville was closer at 15 miles, so the controller gave vectors for Cartersville. Unable to make it to Cartersville, the crew began looking for a clear field or highway for an emergency landing. At 16:18:02, Flight 242's last transmission to Approach Control was recorded: "... we're putting it on the highway, we're down to nothing." The aircraft's outboard left wing section first contacted two trees near State Spur Highway 92 south-southwest of the community of New Hope. About 0.8 miles farther north-northeast, the left wing again contacted a tree alongside the highway within the community of New Hope. The left and right wings continued to strike trees and utility poles on both sides of the highway, and 570 ft after striking the first tree in New Hope, the aircraft's left main gear contacted the highway to the left of the centerline. Almost simultaneously, the outer structure of the left wing struck an embankment, and the aircraft veered to the left and off the highway. The aircraft traveled another 1,260 ft before it came to rest. As it traveled, the aircraft struck road signs, utility poles, fences, trees, shrubs, gasoline pumps at a gas station-store, five automobiles, and a truck. Of the 85 persons aboard Flight 242, 62 were killed, 21 were seriously injured, and 1 was slightly injured. Additionally, eight persons on the ground were killed. Within a month of the accident, one of the surviving passengers and one person on the ground both died of their injuries.
Probable cause:
Total and unique loss of thrust from both engines while the aircraft was penetrating an area of severe thunderstorms. The loss of thrust was caused by the ingestion of massive amounts of water and hail which, in combination with thrust lever movement, induced severe stalling in and major damage to the engine compressors. Major contributing factors include the failure of the company's dispatching system to provide the flight crew with up-to-date severe weather information pertaining to the aircraft's intended route of flight, the captain's reliance on airborne weather radar for penetration of thunderstorm areas, and limitations in the FAA's ATC system which precluded the timely dissemination of real-time hazardous weather information to the flight crew.
Final Report:

Crash of a Cessna 402 in Brugam: 5 killed

Date & Time: Mar 1, 1977
Type of aircraft:
Operator:
Registration:
P2-GKC
Survivors:
Yes
Site:
Schedule:
Wewak - Brugam
MSN:
402-0144
YOM:
1967
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
On final approach to Brugam Airstrip, the twin engine airplane stalled and crashed on a school building. All nine occupants on board the aircraft were injured while five schoolboy were killed and four others injured.

Crash of a Piper PA-31T Cheyenne in Harrisburg: 9 killed

Date & Time: Feb 24, 1977 at 0924 LT
Type of aircraft:
Registration:
N631PT
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
New Cumberland - Harrisburg - University Park - New Cumberland
MSN:
31-7720001
YOM:
1977
Crew on board:
2
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
9
Captain / Total flying hours:
4469
Captain / Total hours on type:
32.00
Aircraft flight hours:
173
Circumstances:
Shortly after takeoff from Harrisburg-Capital City Airport runway 08, the twin engine aircraft went out of control and crashed in flames onto a house located in a populated area in the town of Bressler, 1,55 statute miles from the departure end of runway 08. The aircraft disintegrated on impact and all eight occupants were killed as well as one people in the house.
Those on board were:
Crew:
David M. Wolf, pilot,
Edward Soisson, copilot.
Passengers:
William Sherlock, State Transportation Secretary,
Richard C. Frame, State GOP Chairman,
William R. Smith, Sherlock's Chief of Staff,
Charles Wilson, PennDOT Public Relations Officer,
Larry G. Pennsyl, PennDOT photographer,
John W. Krebs, PennDOT data processing manager.
Probable cause:
The probable cause of the accident was the flightcrew's failure to insure that the aircraft was loaded properly and that it's center of gravity was within certificated limits. As a result, the aircraft's control characteristics were degraded significantly by a center of gravity well aft of the certificated limits. This imbalance led to the pilot's inability to control a longitudinally unstable aircraft during a climbing turn in instrument meteorological conditions. There was no evidence of engine failure or malfunction, the flight crew was properly certified and the pilots had no medical or psychological problems. The accident was not survivable.
Final Report:

Crash of a Vickers 838 Viscount in Stockholm: 22 killed

Date & Time: Jan 15, 1977 at 0905 LT
Type of aircraft:
Operator:
Registration:
SE-FOZ
Survivors:
No
Site:
Schedule:
Kristianstad – Växjö – Jönköping – Stockholm
MSN:
372
YOM:
1961
Flight number:
OX618
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
22
Aircraft flight hours:
12208
Circumstances:
The aircraft was completing a regular schedule flight from Kristianstad to Stockholm-Bromma with intermediate stop in Växjö and Jönköping, carrying 19 passengers and a crew of three on behalf of Linjeflyg. On approach to Bromma Airport, the crew encountered marginal weather and icing conditions. At an altitude of 1,150 feet and a speed of 137 knots, flaps were deployed at an angle of 40° when control was lost. The airplane entered a nose down attitude and crashed at an angle of 110° and a speed of 210 knots in a parking lot located in the residential area of Kälvesta, about 4,5 km short of runway 12 threshold. The aircraft was totally destroyed by impact forces and a post crash fire and all 22 occupants were killed. At the time of the accident, weather conditions were considered as marginal with icing conditions and a horizontal visibility of 5 km with a cloud base at 700 feet.
Probable cause:
Loss of control on final approach due to an excessive accumulation of ice on the horizontal stabilizers after the crew lower the flaps from 32° to 40°. When control was lost, both right engines n°3 and 4 were not running at full power for undetermined reasons, which caused the deicing system to produce an insufficient temperature.