Crash of an Embraer EMB-110P1 Bandeirante in Germiston: 17 killed

Date & Time: Mar 1, 1988 at 1728 LT
Operator:
Registration:
ZS-LGP
Survivors:
No
Schedule:
Phalaborwa – Johannesburg
MSN:
110-402
YOM:
1982
Flight number:
MN206
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
On approach to Johannesburg-Jan Smuts Airport, the twin engine aircraft suffered an in-flight explosion, broke in two and crashed in a industrial area located in Germiston, about 13 km southwest from the airport. The cockpit was found about 250 meters from the main wreckage and all 17 occupants were killed.
Probable cause:
It was determined that the accident was the consequence of an in-flight explosion caused by the detonation of a bomb. A mineworker encountering marital and financial problems boarded the plane at Phalaborwa Airport with a bomb consisting of nitroglycerin and ammonium nitrate. He recently contracted an important life insurance.

Crash of an Embraer EMB-110P Bandeirante in Vilhena

Date & Time: Jan 21, 1988
Operator:
Registration:
PT-GJQ
Survivors:
Yes
MSN:
110-084
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Vilhena Airport, the crew was completing a last turn to join the approach path when the aircraft stalled and crashed about 2 km short of runway threshold. All 13 occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
It was determined that the aircraft's speed was too low during the last sharp turn, causing the aircraft to stall and crash.

Crash of an Embraer EMB-110P Bandeirante in Santo Ângelo

Date & Time: Jul 25, 1987
Operator:
Registration:
PT-GKT
Survivors:
Yes
MSN:
110-130
YOM:
1976
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Santo Ângelo Airport, the crew encountered crosswinds up to 35 knots gusting. The airplane floated and eventually landed too far down the runway 29. After touchdown, the crew initiated the braking maneuver but the aircraft was unable to stop within the remaining distance, overran and came to rest into a ravine. All 13 occupants were rescued while the aircraft was damaged beyond repair. As the landing procedure was incorrect, the crew should initiate a go-around.

Crash of an Embraer EMB-110P2 Bandeirante off Hoskins: 14 killed

Date & Time: Feb 6, 1987
Operator:
Registration:
P2-RDM
Survivors:
Yes
Schedule:
Rabaul - Hoskins
MSN:
110-262
YOM:
1980
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
14
Circumstances:
While descending to Hoskins Airport, the crew encountered poor weather conditions with thunderstorm activity and severe turbulences. Control was lost and the aircraft crashed in the sea few km offshore. Three passengers were rescued while 14 other occupants were killed.
Probable cause:
Loss of control due to severe atmospheric turbulences.

Crash of an Embraer EMB-110P1 Bandeirante in Alpena: 3 killed

Date & Time: Mar 13, 1986 at 2200 LT
Operator:
Registration:
N1356P
Survivors:
Yes
Schedule:
Detroit - Alpena - Saulte Sainte Marie
MSN:
110-370
YOM:
1981
Flight number:
MQ1746
Crew on board:
2
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3384
Captain / Total hours on type:
574.00
Copilot / Total flying hours:
6271
Copilot / Total hours on type:
21
Aircraft flight hours:
9698
Aircraft flight cycles:
16767
Circumstances:
About 2050 on March 13, 1986, Simmons Airlines flight 1746, an Embraer Bandeirante, EMB-110P1, operating as a regularly scheduled flight, departed the Detroit Metropolitan Airport en route to Sault Ste Marie, Michigan, with a stop in Alpena, Michigan. The en route portion of the flight to Alpena was uneventful. However, due to the prevailing instrument meteorological conditions, the crew was unable to complete the instrument landing system (ILS) approach and land and they declared a missed approach at 2142. At 2153, the flight was cleared for a second ILS approach to Alpena. At 2156, the crew acknowledged that radar services were being terminated. This was the last transmission from the airplane. About 2215, a motorist reported that the airplane had
crashed. The airplane was found in a wooded area about 300 feet to the left of the extended centerline, and 1 1/2 miles short of the threshold of runway 01 at Alpena. The airplane was destroyed and two of the seven passengers and one of the two crewmembers onboard were killed.
Probable cause:
The National Transportation Safety Board determines that the probable cause of this accident was the flightcrew’s continued descent of the airplane below the glideslope and through the published decision height without obtaining visual reference of the runway for undetermined reasons. Contributing to the accident was the inefficient system used to disseminate weather-related information to the crew.
Final Report:

Crash of an Embraer EMB-110C Bandeirante in Vitória da Conquista: 2 killed

Date & Time: Oct 9, 1985 at 1900 LT
Operator:
Registration:
PT-GKA
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Vitória da Conquista – Salvador
MSN:
110-090
YOM:
1976
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Shortly after takeoff from Vitória da Conquista Airport, the twin engine airplane encountered difficulties to gain sufficient height. During initial climb, it stalled and crashed about 2 km from the runway end. Both pilots were killed.
Probable cause:
The exact cause of the accident could not be determined. However, it is believed that the captain elected to make a low pass over the house of a friend when he lost control of the aircraft.

Crash of an Embraer EMB-110P1 Bandeirante in Villagarzón

Date & Time: Aug 4, 1985
Operator:
Registration:
HK-2593
Flight Phase:
Survivors:
Yes
Schedule:
Villa Garzón - Puerto Asís
MSN:
110-302
YOM:
1980
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll, the right engine failed and exploded. The crew abandoned the takeoff procedure when the aircraft went out of control. It veered off runway and collided with trees located about 1,600 meters from the end of the runway. The aircraft was destroyed while all 16 occupants were rescued, among them five were injured.
Probable cause:
Failure and explosion of the right engine during takeoff for unknown reasons.

Crash of an Embraer EMB-110P Bandeirante in Juara: 17 killed

Date & Time: Jun 23, 1985
Operator:
Registration:
PT-GJN
Survivors:
No
Schedule:
Juara - Cuiabá
MSN:
110-063
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
After takeoff from Juara Airport, while climbing, the crew declared an emergency after the failure of the left engine. The crew was cleared to return and the rescue teams were dispatched at the airport. On final approach, during the last segment, the aircraft went out of control and struck the ground. It veered off runway and collided with an emergency vehicle (fire bombers truck) before coming to rest in flames. All 17 occupants were killed while no one on the ground was injured.
Probable cause:
A left engine faulty fuel injection nozzle caused a blow torch effect, damaging compressor turbine vane ring and causing thermal fatigue and loss of one of the turbine blades. The resulting imbalance ruptured the starting control bypass fuel return.

Crash of an Embraer EMB-110P1 Bandeirante near Buga: 17 killed

Date & Time: Jan 23, 1985 at 1030 LT
Operator:
Registration:
HK-2638
Flight Phase:
Survivors:
No
Site:
Schedule:
Florencia – Neiva – Cali
MSN:
110-341
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
After passing over the Tuluá VOR at an altitude of 10,500 feet, the crew was cleared to start the descent when the aircraft struck the slope of a mountain located 16 km southeast from Buga. The aircraft disintegrated on impact and all 17 occupants were killed. The wreckage was found at an altitude of 8,600 feet. At the time of the accident, the visibility was reduced due mist and intermittent rain falls.
Probable cause:
Controlled flight into terrain after the crew decided to continue under VFR mode in IMC conditions.

Crash of an Embraer EMB-110P1 Bandeirante in Jacksonville: 13 killed

Date & Time: Dec 6, 1984 at 1814 LT
Operator:
Registration:
N96PB
Flight Phase:
Survivors:
No
Schedule:
Jacksonville - Tampa
MSN:
110-365
YOM:
1981
Flight number:
PT1039
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
13
Captain / Total flying hours:
10000
Captain / Total hours on type:
400.00
Copilot / Total flying hours:
3000
Copilot / Total hours on type:
500
Aircraft flight hours:
5662
Aircraft flight cycles:
7858
Circumstances:
At 18:12, flight 1039 was cleared for takeoff from runway 31. At 18:13, while over the departure end of the runway and climbing through 600 feet, the crew acknowledged a frequency change. Thirty seconds later, the airplane was seen in a steep a descent near the extended centerline of the runway. The Bandeirante struck the ground 7,800 feet beyond the departure end of runway 31 and 85 feet to the right of the extended runway centerline in an inverted nose down attitude, after which it caught fire and burned. Before ground impact, the horizontal stabilizer, including bulkhead No. 36, had separated from the fuselage. Both elevators and elevator tips, the tail cone assembly, and the aft portion of the ventral fin also had separated in flight. All 13 occupants were killed.
Probable cause:
A malfunction of either the elevator control system or elevator trim system, which resulted in an airplane pitch control problem. The reaction of the flight crew to correct the pitch control problem overstressed the left elevator control rod, which resulted in asymmetrical elevator deflection and overstress failure of the horizontal stabilizer attachment structure. The Safety Board was not able to determine the precise problem with the pitch control system.
Final Report: