Crash of a Lockheed L-188A Electra in Kinshasa

Date & Time: Mar 13, 1995
Type of aircraft:
Operator:
Registration:
9Q-CDG
Flight Type:
Survivors:
Yes
Schedule:
Matadi - Kinshasa
MSN:
1119
YOM:
1960
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On final approach to Kinshasa-N'Djili Airport, the four engine aircraft was too low and descending at an insufficient speed when it collided with power cables, stalled and crashed in an open field. All occupants were rescued while the aircraft was destroyed.

Crash of a Lockheed L-188A Electra in Kinshasa

Date & Time: Jan 21, 1994
Type of aircraft:
Registration:
9Q-CCV
Flight Type:
Survivors:
Yes
MSN:
1126
YOM:
1960
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing, the nose gear collapsed. The aircraft slid on its belly and eventually came to rest on the runway. There were no casualties but the aircraft was damaged beyond repair.
Probable cause:
The nose gear collapsed on landing for unknown reasons.

Crash of a Lockheed L-188CF Electra in Oranjestad

Date & Time: Jul 14, 1990 at 1627 LT
Type of aircraft:
Registration:
N4465F
Flight Type:
Survivors:
Yes
Schedule:
Oranjestad – Panama City
MSN:
1096
YOM:
1959
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6060
Captain / Total hours on type:
3150.00
Aircraft flight hours:
31829
Circumstances:
While in climb at 18,000 feet the crew heard and explosion and lost n°3 and 4 engines. They visually noted that the propellers and portions of the gearboxes were also missing. They then shut down no 2 engine due to erratic indications. They declared an emergency and landed. The gear boxes and propellers were not recovered from the caribbean sea.
Probable cause:
The inflight loss of the n°3 and 4 propellers and gearboxes for undetermined reasons. The failed components were not recovered from the Caribbean Sea.
Final Report:

Crash of a Lockheed L-188CF Electra in Tegucigalpa: 3 killed

Date & Time: Mar 21, 1990
Type of aircraft:
Operator:
Registration:
HR-TNL
Flight Type:
Survivors:
No
Site:
Schedule:
San Pedro Sula - Tegucigalpa
MSN:
1134
YOM:
1960
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
While approaching Tegucigalpa-Toncontin Airport in poor weather conditions, the crew failed to realize his altitude was too low when the aircraft struck the south slope of Cerro de Hula (1,600 meters high) located 14 km from runway 01 threshold. The aircraft was destroyed and all three crew members were killed.

Crash of a Lockheed L-188PF Electra in Trelew

Date & Time: Sep 23, 1989 at 1205 LT
Type of aircraft:
Operator:
Registration:
0789/6-P-101
Flight Type:
Survivors:
Yes
Schedule:
Buenos Aires - Trelew
MSN:
1123
YOM:
1960
Flight number:
FAA789
Location:
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Trelew-Almirante Zar Airport runway 06, the aircraft collided with a truck that was parked at the side of the runway. The left main gear collapsed and the aircraft came to rest. All 23 occupants evacuated safely while the aircraft was damaged beyond repair.

Crash of a Lockheed L-188C Electra in Taura

Date & Time: Sep 4, 1989 at 1654 LT
Type of aircraft:
Operator:
Registration:
HC-AZJ
Survivors:
Yes
Schedule:
Quito - Tulcán
MSN:
2004
YOM:
1959
Location:
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
92
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Quito-Mariscal Sucre Airport, while climbing, the left main gear warning light remained on. The captain decided to divert to Taura AFB for an emergency landing. The aircraft belly landed and slid for few dozen meters before coming to rest. All 99 occupants escaped uninjured while the aircraft was damaged beyond repair.
Probable cause:
The bolts on the front gear doors were stuck because of a stuck support rod.

Crash of a Lockheed L-188A Electra in Lago Agrio: 7 killed

Date & Time: Sep 12, 1988 at 1429 LT
Type of aircraft:
Operator:
Registration:
HC-AZY
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Lago Agrio - Quito
MSN:
1052
YOM:
1959
Country:
Crew on board:
7
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
7
Circumstances:
The engine n°2 was inoperative due to technical problems and the crew decided to takeoff on a positioning flight to Quito with only three engines. Shortly after takeoff from Lago Agrio Airport, while in initial climb, the engine n°1 caught fire and exploded. The crew lost control of the aircraft that banked left and crashed, bursting into flames. All seven occupants were killed.
Probable cause:
Failure and explosion of the engine n°1 at takeoff for unknown reasons.

Crash of a Lockheed L-188AF Electra near Kasongo-Lunda: 2 killed

Date & Time: Feb 5, 1986
Type of aircraft:
Operator:
Registration:
9Q-CWT
Flight Phase:
Survivors:
Yes
Schedule:
Kasongo-Lunda – Kinshasa
MSN:
1045
YOM:
1959
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
10
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Few minutes after takeoff from Kasongo-Lunda, en route to Kinshasa, the crew encountered engine problems. He completed an emergency landing in the bush about 80 km north of Kasongo-Lunda. The aircraft crash landed and was damaged beyond repair. Two passengers were killed while 12 other occupants were injured.

Crash of a Lockheed L-188C Electra in Medan

Date & Time: Nov 30, 1985
Type of aircraft:
Operator:
Registration:
PK-RLG
Survivors:
Yes
Schedule:
Jakarta - Padang
MSN:
2008
YOM:
1959
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Padang-Tabing Airport, both wheels on the right main gear detached and fell on a watch manufacture located in the approach path. The captain decided to divert to Medan-Polonia Airport more suitable for an emergency landing. Following a normal approach, the four engine aircraft belly landed and slid for few dozen meters before coming to rest. All 45 occupants evacuated safely while the aircraft was damaged beyond repair.
Probable cause:
Loss of both right wheels for unknown reasons.

Crash of a Lockheed L-188CF Electra at Dobbins AFB

Date & Time: Jan 29, 1985 at 0936 LT
Type of aircraft:
Operator:
Registration:
N854U
Flight Type:
Survivors:
Yes
Schedule:
Philadelphia - Charlotte
MSN:
2009
YOM:
1959
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6900
Captain / Total hours on type:
303.00
Aircraft flight hours:
47765
Circumstances:
During gear retraction after takeoff, the right main gear became jammed in a partially retracted position and the respective in-transit gear light would not extinguish. Attempts to recycle the gear were unsuccessful. The flight crew diverted to Atlanta, GA; then decided to land at Dobbins AFB, where there was a long, wide runway that could be foamed. Foam was applied to approximately 300 feet of runway 29. The aircraft was landed with the nose and left main gear extended and the right main gear partially retracted. Subsequently, the aircraft veered to the right and stopped with the nose gear approximately 70 feet off the runway. Fire erupted in the area of the right main gear; however, the fire was quickly extinguished by fire dept personnel. An investigation revealed the clearance between the main landing gear door hook, pn 803845-1, and the strut roller was excessive. The reason for the improper clearance was not determined. Lockheed service bulletin 88/sb-558 warned that excessive clearance combined with a drop in hydraulic pressure, gust or maneuver could result in the gear jamming. All three crew members were uninjured.
Probable cause:
Occurrence #1: airframe/component/system failure/malfunction
Phase of operation: takeoff - initial climb
Findings
1. Door, landing gear - assembly
2. (c) door, landing gear - clearance
3. (c) door, landing gear - exceeded
4. (c) landing gear, normal retraction/extension assembly - jammed
5. (c) landing gear, main gear - movement restricted
6. Gear down and locked - not possible
----------
Occurrence #2: dragged wing, rotor, pod, float or tail/skid
Phase of operation: landing - roll
----------
Occurrence #3: loss of control - on ground/water
Phase of operation: landing
Findings
7. Directional control - not possible
8. Ground loop/swerve - uncontrolled
Final Report: