Crash of a Boeing 707-351C in Karm Umran: 9 killed

Date & Time: Dec 14, 1988 at 2150 LT
Type of aircraft:
Operator:
Registration:
5N-AYJ
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Dar es-Salaam - Cairo - Brussels
MSN:
19168
YOM:
1966
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
9
Circumstances:
During a night approach to Cairo-Intl Airport, the crew initiated a go-around as the visibility was too low (400 meters). A second attempt to land few minutes later was also abandoned. The crew decided to divert to Luxor Airport where weather conditions were better. While approaching Luxor from the north, the crew declared an emergency due to low fuel when the aircraft lost height and crashed onto several houses located in the city of Karm Umran, about 45 km north of Luxor Airport runway 20 threshold. The aircraft was destroyed and all eight occupants were killed as well as one people on the ground.
Probable cause:
It is believed that the crew was forced to attempt an emergency landing due to fuel exhaustion.

Crash of an Ilyushin II-14P in Linfen: 46 killed

Date & Time: Oct 7, 1988 at 1321 LT
Type of aircraft:
Registration:
B-4218
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Linfen - Linfen
MSN:
6 34 14 06
YOM:
1956
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
44
Pax fatalities:
Other fatalities:
Total fatalities:
46
Circumstances:
The aircraft was chartered to carry 44 employees of a local knitting factory for a 15 minutes sightseeing flight over the Linfen Area. Shortly after takeoff, while in initial climb, the left engine failed. The aircraft lost height, causing the left wing to struck a building. Upon impact, the left wing was partially torn off. The aircraft then collided with eight poplars and eventually crashed on an hotel. Four passengers were rescued while 44 others occupants as well as two people on the ground were killed.
Probable cause:
It was determined that the left engine had failed following a fatigue fracture in the engine's oil pump drive shaft.

Crash of a Douglas B-26B Invader in Bogotá

Date & Time: Sep 21, 1988
Type of aircraft:
Operator:
Registration:
HK-1247P
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
Schedule:
Bogotá - Bogotá
MSN:
27829
YOM:
1944
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
One pilot and one engineer took off from Bogotá-El Dorado Airport on a post maintenance check flight. After takeoff, while completing a left turn, the pilot lost control of the airplane that crashed near residential area in Bogotá. Fortunately, both occupants were rescued and no one on ground was injured.

Crash of an IAI Arava 201 in La Carlota: 4 killed

Date & Time: Sep 5, 1988
Type of aircraft:
Operator:
Registration:
GN-7952
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
049
YOM:
1978
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Shortly after takeoff from La Carlota-General Francisco de Miranda AFB, the airplane lots height and crashed on a textile mill, bursting into flames. All three crew members as well as one people on the ground were killed.

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

Date & Time: Aug 25, 1988 at 1530 LT
Registration:
N6069W
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
61-0676-7963318
YOM:
1979
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
3000
Captain / Total hours on type:
50.00
Circumstances:
Witnesses stated that the aircraft used almost the entire length of the runway during the ground run. After rotation and gear retraction, it continued to climb in a nose high attitude to approximately 100-150 feet, then it started an approximately 20° bank to the right until it hit power lines and crashed into the top of a printing shop about 3/4 mile from the airport. Witnesses employed at the airport stated that the aircraft had been having undetermined problems with the right engine for a few weeks prior to the accident, but was still being flown and the right engine running extremely rough. All three occupants were killed.
Probable cause:
Occurrence #1: loss of engine power
Phase of operation: takeoff - initial climb
Findings
1. (c) engine assembly - undetermined
2. (c) operation with known deficiencies in equipment - attempted - pilot in command
3. Propeller feathering - performed
----------
Occurrence #2: forced landing
Phase of operation: descent - emergency
----------
Occurrence #3: in flight collision with object
Phase of operation: maneuvering - turn to landing area (emergency)
Findings
4. (f) object - wire, transmission
5. (f) object - building (nonresidential)
Final Report:

Crash of a Cessna 404 Titan in Aurora

Date & Time: Jun 10, 1988 at 1604 LT
Type of aircraft:
Operator:
Registration:
N8827K
Flight Type:
Survivors:
Yes
Site:
Schedule:
Greeley - Denver
MSN:
404-0424
YOM:
1978
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
1400
Captain / Total hours on type:
400.00
Aircraft flight hours:
3486
Circumstances:
The pilot was on a flight from Greeley to Denver, Colorado to obtain minor maintenance on a cargo door. As the aircraft was being vectored on final approach, the pilot reported that he believed the aircraft had fuel starvation. Subsequently, the aircraft was observed to make a complete roll and crash in a residential area. Only about 1.5 gallon of fuel was found in the right wing tank. The left wing and fuel tank were destroyed, but no odor of fuel was noted on the ground around the left wing. Also, a lack of fuel was noted in the fuel lines. The aircraft had not been refueled after the previous flight. The pilot that had flown the aircraft on a previous flight estimated there was 100 lbs of fuel remaining in each tank after his flight.
Probable cause:
Occurrence #1: loss of engine power (total) - nonmechanical
Phase of operation: approach - vfr pattern - final approach
Findings
1. 1 engine
2. (f) aircraft preflight - improper - pilot in command
3. (f) refueling - not performed - pilot in command
4. (f) in-flight planning/decision - improper - pilot in command
5. (f) fluid, fuel - starvation
6. (f) fuel supply - inadequate - pilot in command
----------
Occurrence #2: loss of control - in flight
Phase of operation: approach - vfr pattern - final approach
Findings
7. (c) airspeed (vmc) - not maintained - pilot in command
8. (c) aircraft control - not maintained - pilot in command
----------
Occurrence #3: in flight collision with terrain/water
Phase of operation: descent - uncontrolled
Final Report:

Crash of a Beechcraft E18S in Detroit: 3 killed

Date & Time: Mar 10, 1988 at 0026 LT
Type of aircraft:
Registration:
N900WP
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Detroit - Fort Wayne
MSN:
BA-298
YOM:
1957
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
1764
Captain / Total hours on type:
375.00
Circumstances:
The flight was an air taxi cargo flight carrying truck parts. After takeoff, the tower asked the pilot if he was in difficulty and the pilot replied 'roger' and requested a change of flight plan. The aircraft was seen flying erratically just above the tree tops. The aircraft descended almost vertically into a residential area. The rear of one home was ignited by the impact and 2 occupants of the house were fatally burned. Post accident investigation revealed no engine malfunction but there were discrepancies in the load manifest and the aircraft weight and balance. Before takeoff a company employee watched the pilot secure the cargo with ropes nets and clips but did not help because he 'didn't know what the pilot was doing. 'Impact' damage precluded determination of the original placement and security of the cargo and any possible shifting prior to impact. The net weight on the cargo manifest did not include the weight of the trays to hold the parts. This was an omission of 150 lbs. Company personnel said no weight and balance information was left with them when the aircraft departed.
Probable cause:
Occurrence #1: loss of control - in flight
Phase of operation: takeoff - initial climb
Findings
1. (f) dispatch procedures - inadequate - company/operator management
2. (c) aircraft weight and balance - not performed - pilot in command
3. (c) aircraft weight and balance - improper
4. (c) aircraft performance, climb capability - inadequate
5. (c) aircraft control - not maintained - pilot in command
6. (f) supervision - poor - company/operator management
Final Report:

Crash of an Antonov AN-12B near Charbatia AFB: 17 killed

Date & Time: Mar 8, 1988
Type of aircraft:
Operator:
Registration:
L2174
Flight Phase:
Flight Type:
Survivors:
Yes
Site:
MSN:
6 3 438 06
YOM:
1965
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
After takeoff from Charbatia AFB, while in initial climb, the crew declared an emergency after an engine caught fire. After being cleared to return, the captain initiated a turn while the fire spread to the nacelle and the wing. The aircraft entered an uncontrolled descent and crashed in the district of Paikarapur. The aircraft and few houses were totally destroyed. All nine occupants as well as eight people on the ground were killed. 10 other people on the ground were injured.
Probable cause:
The exact cause of the engine fire could not be determined with certainty. However, it was reported that the fire extinguishing systems were inoperative.

Crash of a Lockheed L-382G-35C Hercules in Cancao: 8 killed

Date & Time: Oct 14, 1987 at 0705 LT
Type of aircraft:
Operator:
Registration:
HB-ILF
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Kuito - Benguela
MSN:
4701
YOM:
1976
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
8
Captain / Total flying hours:
11198
Captain / Total hours on type:
10526.00
Copilot / Total flying hours:
4682
Copilot / Total hours on type:
1628
Aircraft flight hours:
8772
Aircraft flight cycles:
5708
Circumstances:
The four engine aircraft was dispatched in Angola on behalf of the International Red Cross. En route from Kuito to Benguela, while climbing to an altitude of 12,000 feet, the aircraft was hit by a surface-to-air missile that struck the engine n°3. The aircraft entered a dive and crashed on the village of Cancao located about 40 km west of Kuito. The aircraft disintegrated on impact and at least eight houses were destroyed. All six occupants were killed as well as two other people on the ground.
Probable cause:
Shot down by a surface-to-air missile. The exact type of missile and its origin remain unknown.
Final Report:

Crash of a Beechcraft 200 Super King Air in Southend: 1 killed

Date & Time: Sep 12, 1987 at 0535 LT
Registration:
G-WSJE
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Southend - Bergamo
MSN:
BB-484
YOM:
1979
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
4320
Captain / Total hours on type:
50.00
Circumstances:
The twin engine aircraft departed Southend Airport on a cargo flight to Bergamo, carrying newspapers and magazines. Two minutes and 30 seconds after liftoff, while climbing in limited visibility due to the night and low clouds, the airplane entered a dive and crashed on a garage, bursting into flames. The pilot, sole on board, was killed.
Probable cause:
Examination of the propeller assemblies indicated that, although the right-hand propeller appeared to have been at fine pitch and rotating at high revolutions at impact, the left-hand propeller had been rotating much more slowly and appeared to have been at, or close to, its fully feathered position. The firewall shut-off fuel valve for the left-hand engine was found in its closed position, consistent with the action of shutting down this engine at some point prior to the impact. A strip examination of the left-hand engine was conducted and showed no evidence of damage to its rotating assemblies prior to the impact with the garage. The only damage identified on this engine as not being consistent with the impact was a ruptured diaphragm within the low-pressure compressor bleed valve. This rolling diaphragm is designed to hold the compressor bleed valve closed a high power settings and to provide smooth opening of the compressor bleed valve with reduction of compressor discharge pressure.
Final Report: