Crash of a Lockheed C-130H Hercules in Eindhoven: 34 killed

Date & Time: Jul 15, 1996 at 1802 LT
Type of aircraft:
Operator:
Registration:
CH-06
Flight Type:
Survivors:
Yes
Schedule:
Rimini - Eindhoven
MSN:
4473
YOM:
1972
Flight number:
610
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
37
Pax fatalities:
Other fatalities:
Total fatalities:
34
Captain / Total flying hours:
2102
Captain / Total hours on type:
1436.00
Copilot / Total flying hours:
582
Copilot / Total hours on type:
138
Aircraft flight hours:
10914
Circumstances:
The aircraft was chartered by the Dutch Air Force (Koninklijke Luchtmacht) to fly the Dutch Air Force's brass band from Italy back to the Netherlands. The transport plane arrived at Verona-Villafranca at 13:33. Forty passengers boarded the plane and at 15:04 the Hercules took off from Villafranca for a short flight to Rimini, where it landed at 15:31. Three passengers deplaned at Rimini and the Hercules was back in the air at 15:55 heading for Eindhoven. The Hercules descended into Eindhoven and contacted Eindhoven Tower at 18:00. Eindhoven Tower cleared the flight for the approach: "Okay, you may continue descent for 1000, as number one in traffic, for a direct final course runway 04, QNH 1027." After reported the runway in sight, the Hercules was cleared to land: "610 is cleared to land runway 04, the wind from 360° 10 knots." Possibly as a result of the presence of a large number of birds near the runway, the copilot initiated a go around. Birds were ingested by both left hand engines (n°1 and 2), causing both engines to lose power. For reasons unknown the crew shut down engine n°3 and feathered the propeller. The plane then turned left and crashed off the left side of the runway. Within seconds a fire erupted which was fed by the oxygen from the airplane's oxygen system. Some emergency exits in the main cabin were unreachable because of the fire while other exits could not be opened because of twisting of the fuselage. The fact that there were a large number of passengers on board the plane was not immediately clear tot the fire fighters. It took some 23 minutes before passengers were noted in the main cabin.
Probable cause:
The accident was initiated, most probably as a reaction to observing birds, by the go-around which was made at a low altitude during which a flock of birds could no longer be evaded.
The accident became inevitable when:
- Bird ingestion in the two left engines occurred due to which the power of these two engines was lost,
- As a result of power loss, the aircraft became uncontrollable at a very low altitude and crashed.
The relative low experience of the crew was a contributing factor.

Crash of a Lockheed C-130H Hercules in Tandil

Date & Time: May 16, 1996 at 1200 LT
Type of aircraft:
Operator:
Registration:
TC-67
Flight Type:
Survivors:
Yes
MSN:
4576
YOM:
1975
Country:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances while landing at Tandil Airport. There were no casualties.

Crash of a Lockheed C-130H Hercules near Khartoum: 91 killed

Date & Time: Feb 26, 1996 at 1855 LT
Type of aircraft:
Operator:
Flight Type:
Survivors:
No
Schedule:
El Obeid - Khartoum
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
85
Pax fatalities:
Other fatalities:
Total fatalities:
91
Circumstances:
While descending to Khartoum Airport, the crew declared an emergency due to in-flight fire. Shortly later, the aircraft entered an uncontrolled descent and crashed 40 km from Khartoum Airport. The aircraft disintegrated on impact and all 91 occupants were killed.

Crash of a Lockheed C-130E Hercules near Bliss: 6 killed

Date & Time: May 13, 1995
Type of aircraft:
Operator:
Registration:
62-1838
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Boise - Colorado Springs
MSN:
3801
YOM:
1963
Flight number:
Sumit 38
Location:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
After departure from Boise-Gowen Field, en route to Peterson AFB in Colorado Springs, the crew encountered technical problems with the engine n°2. The crew declared an emergency and elected to divert to Mountain Home AFB. About 20 minutes into the flight, the engine n°2 compressor disintegrated. The aircraft entered an uncontrolled descent and crashed 12 miles north of Bliss. All six crew members were killed.
Crew:
Lt Col Robert Buckout, Commander
1st Lt Lance Daugherty, pilot,
Cpt Geoffery Boyd, navigator,
CMSgt Jimmy Vail, flight engineer,
M/Sgt Jay Kemp, loadmaster,
S/Sgt Michael Scheideman, loadmaster.
Probable cause:
The cause of the crash was that the number 2 (inside left wing) engine had a buggy undertemp sensor, causing the crew to enrich the fuel mixture, leading to an actual engine overtemp. One of the fuel lines ruptured or melted, causing the fire, and one of the crewmen hit the fire carts, but the fire re-erupted moments later, and there were no more extinguishers available for that engine. One of the pins that was supposed to melt in an engine fire, releasing the engine from the AC, failed to release the engine properly, while another worked properly. Still half connected to the wing hard point, the engine torqued at an awkward angle, causing severe wing and fuselage damage, which led to the crash.

Crash of a Lockheed C-130B Hercules in Trinidad

Date & Time: Dec 31, 1994
Type of aircraft:
Operator:
Registration:
TAM-67
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Trinidad - Trinidad
MSN:
3581
YOM:
1960
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a local training at Trinidad-Jorge Heinrich Arauz Airport. Upon takeoff, the aircraft lost height and crash landed by the runway. All four occupants escaped uninjured while the aircraft was damaged beyond repair. It is believed that the loss of control occurred at liftoff while the crew was attempting a 3-engine takeoff.

Crash of a Lockheed RC-130E Hercules in Formosa de Rio Preto: 21 killed

Date & Time: Oct 14, 1994 at 1900 LT
Type of aircraft:
Operator:
Registration:
2460
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Rio de Janeiro - Belém
MSN:
4293
YOM:
1968
Country:
Crew on board:
6
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
21
Circumstances:
The four engine aircraft departed Rio de Janeiro-Galeão Airport at 1600LT on a flight to Belém, carrying 15 passengers and a crew of six. About three hours into the flight, while in cruising altitude, a fire erupted on board. The crew lost control of the aircraft that entered a dive and crashed in an open field located in Formosa de Rio Preto. The aircraft was totally destroyed and all 21 occupants were killed.
Probable cause:
It was determined that a fire of unknown origin erupted in flight, followed by several explosions. A that time, a load of ammunition was stored in several boxes in the cargo compartment.

Crash of a Lockheed L-382G-43C Hercules in Hong Kong: 6 killed

Date & Time: Sep 23, 1994 at 1915 LT
Type of aircraft:
Operator:
Registration:
PK-PLV
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Hong Kong - Djakarta
MSN:
4826
YOM:
1979
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
6
Captain / Total flying hours:
11781
Captain / Total hours on type:
3949.00
Copilot / Total flying hours:
9064
Copilot / Total hours on type:
2570
Aircraft flight hours:
15223
Circumstances:
Following a normal takeoff roll, the pilot-in-command started the rotation. During initial climb, at a height of about 100 feet and at a speed of 122 knots, the engine n°4 went into Beta range and lost power. The crew elected to regain control but the aircraft rolled to the right, causing the right wing to struck the grassy area along runway 13. Out of control, the aircraft plunged in the Kowloon Bay and came to rest 500 metres offshore. Six occupants were rescued while six others were killed.
Probable cause:
The accident was the consequence of the following factors:
- The n°4 propeller went into Beta range shortly after rotation because the cable of the speed lever failed,
- The crew were unable to maintain control of the aircraft following this occurrence.

Crash of a Lockheed C-130A Hercules near Pearblossom: 3 killed

Date & Time: Aug 13, 1994 at 1331 LT
Type of aircraft:
Operator:
Registration:
N135FF
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Hemet - Hemet
MSN:
3148
YOM:
1957
Flight number:
Tanker 82
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
11000
Captain / Total hours on type:
2000.00
Aircraft flight hours:
20300
Circumstances:
While in level flight, the airplane's right wing separated and, during the separation sequence, wing fuel ignited. Subsequent laboratory examination of right-side, center-wing fragments revealed two fatigue cracks that propagated to overstress fractures. One of the cracks was within the underside wing skin below a doubler, and the other was within the doubler itself. The total size and origin of the fatigue regions could not be determined due to damage to fracture surfaces and a lack of available material. The airplane was delivered new to the U.S. Air Force in December 1957 and was retired from military service in 1986. In May 1990, the FAA issued a restricted-category special airworthiness certificate authorizing the airplane to dispense aerial fire retardant. At the time of the accident, the airplane had a total of 20,289 flight hours, 19,547 of which were acquired during its military service. The inspection and maintenance programs used by the operator, which were based on military standards, included general visual inspections for cracks but did not include enhanced or focused inspections of highly stressed areas, such as the wing sections, where the fatigue cracks that led to those accidents were located. The operator did not possess the engineering expertise necessary to conduct studies and engineering analysis to define the stresses associated with the firefighting operating environment and to predict the effects of those stresses on the operational life of the airplanes.
Probable cause:
The inflight failure of the right wing due to fatigue cracking in the underside right wing skin and overlying doubler. A factor contributing to the accident was inadequate maintenance procedures to detect fatigue cracking.
Final Report:

Crash of a Lockheed L-382G-35C Hercules in Malanje

Date & Time: Apr 7, 1994
Type of aircraft:
Operator:
Registration:
D2-THC
Flight Type:
Survivors:
Yes
MSN:
4679
YOM:
1976
Location:
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing at Malanje Airport, the crew encountered technical problems with the brakes. The aircraft came to rest on the runway, bursting into flames. All five crew members escaped uninjured while the aircraft was destroyed by fire.
Probable cause:
Brakes overheated after landing for unknown reasons.

Crash of a Lockheed C-130H Hercules in Stepanakert: 32 killed

Date & Time: Mar 17, 1994 at 2230 LT
Type of aircraft:
Operator:
Registration:
5-8521
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Moscow - Tehran
MSN:
4432
YOM:
1971
Country:
Region:
Crew on board:
13
Crew fatalities:
Pax on board:
19
Pax fatalities:
Other fatalities:
Total fatalities:
32
Circumstances:
En route from Moscow to Tehran, while in cruising altitude over Armenia by night, the aircraft was shot down by a surface-to-air missile and crashed 3 km north of Stepanakert Airport. All 32 occupants were killed. According to Iranian authorities, all passengers were employees of the Iranian embassy in Moscow flying back home with family members.
Probable cause:
Shot down by a surface-to-air missile.