Crash of a Boeing 707-323C in Kinshasa

Date & Time: Nov 1, 1997
Type of aircraft:
Operator:
Registration:
9Q-CKK
Survivors:
Yes
MSN:
19577
YOM:
1968
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Kinshasa-N'Djili Airport, the crew informed ATC that the nose gear was stuck in its wheel well and could not be lowered, even manually. The aircraft landed on its nose and slid on the runway before coming to rest. There were no casualties but the aircraft was damaged beyond repair.

Crash of a Yakovlev Yak-40 in Jalalabad: 2 killed

Date & Time: Oct 29, 1997
Type of aircraft:
Operator:
Registration:
YA-KAE
Survivors:
Yes
MSN:
9 44 10 37
YOM:
1974
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
20
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
Crashed on landing in unknown circumstances. A crew member and a passenger were killed.

Crash of a Douglas DC-9-32 in Mexico City

Date & Time: Oct 15, 1997 at 2030 LT
Type of aircraft:
Operator:
Registration:
XA-DEJ
Survivors:
Yes
MSN:
47594
YOM:
1973
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
67
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The base of the empennage struck the runway surface upon landing at Mexico City-Benito Juárez Airport. The aircraft was stopped on the runway and all 72 occupants evacuated safely. The aircraft was written off.

Crash of an Avro 748-401-2B in Yogyakarta

Date & Time: Oct 13, 1997
Type of aircraft:
Operator:
Registration:
PK-IHO
Survivors:
Yes
MSN:
1774
YOM:
1980
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For unknown reasons, the twin engine airplane landed very hard at Yogyakarta-Adisutjipto Airport. All 10 occupants were uninjured while the aircraft was damaged beyond repair following irreparable structural damages.

Crash of a Douglas DC-9-32 near Nuevo Berlin: 74 killed

Date & Time: Oct 10, 1997 at 2210 LT
Type of aircraft:
Operator:
Registration:
LV-WEG
Flight Phase:
Survivors:
No
Schedule:
Posadas - Buenos Aires
MSN:
47446
YOM:
1969
Flight number:
AU2553
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
69
Pax fatalities:
Other fatalities:
Total fatalities:
74
Captain / Total flying hours:
9238
Captain / Total hours on type:
177.00
Copilot / Total flying hours:
2910
Copilot / Total hours on type:
1384
Aircraft flight hours:
56854
Aircraft flight cycles:
54800
Circumstances:
The aircraft departed Posadas-Libertador General José de San Martín Airport at 2118LT on a regular scheduled flight to Buenos Aires, carrying 69 passengers and five crew members. While cruising at an altitude of 35,000 feet, weather conditions deteriorated with cumulonimbus reported till 49,000 feet, stormy weather, icing conditions and severe turbulences with winds up to 80 km/h and an OAT of -59° C. The crew modified his route and entered the Montevideo FIR without contacting Montevideo ATC. At 2204LT, the aircraft entered an area with severe icing conditions and three minutes later, the copilot (pilot-in-command) initiated a descent without prior permission. Meanwhile, the captain contacted Ezeiza Control, requesting permission to descend. Ezeiza Control radioed that the flight was over Uruguay territory and that they needed to contact Montevideo Control for permission. At 2209:17, Montevideo ATC cleared the crew to descend to FL257, an altitude reached at 2210:25. During the descent the first officer complained that his airspeed indicator did not seem to be working correctly. Descending through FL300, the first officer extended the slats. The pilots were trained to extend slats when recovering from approach to stall situations at 10,000 - 12,000 feet. However, the actual airspeed at the time of extension was higher than permitted. This exceeded the design limit, causing an asymmetry. The aircraft entered an uncontrolled descent and crashed in a near vertical attitude in an open field located about 21 km east of Nuevo Berlin. The aircraft disintegrated on impact and all 74 occupants were killed. At the point of impact, a cratere of 10 metres deep by 30 metres wide was found. The accident was not survivable. It was reported that that the airspeed suddenly increased from 200 knots to 450 knots in four seconds, probably after the Pitot tubes got iced.
Probable cause:
The immediate cause of the accident was likely that at an altitude of 30,000 feet, the first officer, who was the pilot-in-command, found himself in flight conditions which induced him to extend the slats. This manoeuvre was completed at a speed much higher than the limit of the structural design of the slats, and their extension caused an asymmetry and a subsequent loss of control from which a recovery was not possible. The copilot's interpretation as to the need to extend the slats would have been a result of erroneous indications of low speed (IAS), caused by blockage of the Pitot tubes which resulted from icing conditions while cruising in clouds with an extreme OAT of -59° C. It was not possible to determine if the obstruction was caused by the crew by not activating the heating system via the selector switch, or failure of that system.
The following contributing factors were identified:
a) No indication of Mach number on the speed indicators installed in the accident aircraft within its flight envelope, with air speeds below 250 KIAS.
b) Lack of crew training in flight instrument failures and upset recovery.
c) Lack of crew training in the recovery of approach to stall in the DC-9 aircraft in "clean configuration" in accordance with the procedures specified in the FCOM, section 5, 10-0-0, code 30.
d) Lack of instruction and pilot training in crew resource management (CRM).
e) Absence of a warning light Pitot/Stall-Heater OFF on the annunciator panel.
f) Deficiency in operational procedures.
Final Report:

Crash of a Let L-410UVP in Khabarovsk

Date & Time: Sep 26, 1997 at 2100 LT
Type of aircraft:
Operator:
Registration:
RA-67474
Survivors:
Yes
MSN:
84 12 39
YOM:
1984
Flight number:
Dh228
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While descending to Khabarovsk-Novy Airport by night, both engine stopped simultaneously. The crew attempted an emergency landing when the aircraft crash landed in a field located 11 km from Khabarovsk Airport. All seven occupants were injured and the aircraft was damaged beyond repair.
Probable cause:
Failure of both engines on approach following a fuel exhaustion.

Crash of an Airbus A300B4-600 in Medan: 234 killed

Date & Time: Sep 26, 1997 at 1334 LT
Type of aircraft:
Operator:
Registration:
PK-GAI
Survivors:
No
Site:
Schedule:
Jakarta - Medan
MSN:
214
YOM:
1982
Flight number:
GA152
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
222
Pax fatalities:
Other fatalities:
Total fatalities:
234
Captain / Total flying hours:
11978
Captain / Total hours on type:
782.00
Copilot / Total flying hours:
709
Copilot / Total hours on type:
709
Aircraft flight hours:
27095
Aircraft flight cycles:
16593
Circumstances:
On 26 September 1997 the Garuda Indonesia Flight GA 152, PK-GAI Airbus A300-B4 departed from the Jakarta Soekarno-Hatta International Airport at 04:41 UTC. The aircraft was on a regular scheduled passengers flight to Polonia International Airport of Medan, North Sumatera with estimated time of arrival 06:41 UTC. Flight GA 152 was flying under Instrument Flight Rules during daylight. Before the flight, the flight crew reported to Garuda Indonesia Flight Operations office to receive flight briefings, including Notice to Airmen (NOTAM), weather conditions and forecast en-route, at destination and alternate airports, as well as the flight plan. The NOTAM stated that the MDN VOR was overdue for maintenance and advised to use the facility ‘with caution', although the Medan VOR has been calibrated with both ground and flight calibration on 14 June 1997 and valid until 14 December 1997, the use of Medan VOR was classified as “restricted due to radial course alignment at 270 degrees radial”. At the time of flight-planning, the visibility from Medan TAFOR (26 September 1997, 00.00 UTC – 24.00 UTC) was 1000 meters in smoke. The dispatcher stated that he received information through company channel that the actual visibility at Medan was 400 meters in smoke, which was below the minimum required visibility for runway 05 ILS of 800 meters. At 06:12:51 GA 152 requested a descend clearance to Medan Control. Medan Control cleared the aircraft to descend to FL 150. On passing FL 150, GA 152 was informed that the aircraft was in radar contact, at a distance of 43 nautical miles from MDN VOR/DME. The crew was then instructed to descend to 3000 ft for a landing on Runway 05 and to reduce the speed to 220 knots to allow Bouraq flight BO 683 to takeoff from Runway 23 at 06:20:47. GA152 requested a speed of 250 knots below 10000 feet which was approved. At 6:27:12, Medan Approach instructed GA 152 to maintain altitude on heading to Medan VOR/DME. GA 152 confirmed this instruction at 6:27:21. At 06:27:50 Medan Approach transmitted an instruction “Merpati one five two you er .. turn left heading two four zero vectoring for intercept ILS runway zero five from the right side traffic now er.. rolling”. There was no response by any aircraft to this transmission. At 06:28:06 Medan Approach enquired “Indonesia one five two do you read”. GA 152 asked the ATC to repeat the message. At 06:28:13 Medan Approach instructed GA 152 to “Turn left heading er.. two four zero two three five now vectoring for intercept ILS runway zero five”. This instruction was acknowledged by GA 152. At 06:28:52 the PIC asked the Medan Approach whether the aircraft was clear from the mountainous area northwest from Medan. This was confirmed by Medan Approach, and GA 152 was instructed to continue turning left on heading 215°M. At 06:29:41, GA 152 was instructed to descend to 2000 ft and the crew acknowledged it. Recorded FDR information indicates the aircraft is essentially wings level, heading approx 225M° and passing through 3000 feet on descent. Then at 06:30:04 GA 152 was instructed to turn right heading 046 degrees, and to report when established on the localizer. This was acknowledged by GA 152, but misread the heading “Turn right heading zero four zero Indonesia one five two check established”. Meanwhile recorded FDR information indicates the aircraft commences a roll to the left, heading reducing indicating a left turn and passing through 2600 feet on descent. At 6:30:33, while turning left, First Officer reminded the Captain to turn right. Two seconds later GA 152 queried Medan Approach whether the turn is to the left or to the right onto heading 046 degrees. At 6:30:39 Medan Approach replied “Turning right Sir”, which was acknowledged by GA 152. FDR data shows that the aircraft began to roll to wings level. At 06:30:51 Medan Approach asked whether GA 152 was making a left turn or a right turn. Recorded FDR information indicates the aircraft was wings level and rolling to the right, heading approximately 135°M and increasing, at 2035 feet pressure altitude on descent. GA 152 responded “We are turning right now”. At 06:31:05 Medan Approach instructed GA 152 to continue turning left. Recorded FDR information showed that at this point the aircraft had passed the assigned 2000 ft altitude and continued descending. GA 152 replied “Err...confirm turning left we are starting to turn right now”. During the interview, the controller stated that it was around this time that he recognized that the aircraft went below the required altitude (1800 ft and descending). Recorded FDR information indicates the aircraft reduced right roll from approx 24.3º to 10.2° and then rolled right again to approx 25°, while heading was increasing indicated a right turn was being maintained and the aircraft continued descending. At 06:31:32 the sound of tree impact is recorded. The elevation of the initial impact with the trees was at about 1550 ft above sea level. The final impact on the bottom of a ravine approximately 600 meters from the first tree impact destroyed the aircraft, and 234 people on board of the aircraft perished. There were no ground casualties.
Probable cause:
There was confusion regarding turning direction of left turn instead of right turn at critical position during radar vectoring that reduced the flight crew’s vertical awareness while they were concentrating on the aircraft’s lateral changes. These caused the aircraft to continue descending below the assigned altitude of 2,000 feet and hit treetops at 1,550 feet above mean sea level.
Final Report:

Crash of a De Havilland Dash-8-301 in Pereira

Date & Time: Sep 14, 1997 at 2000 LT
Operator:
Registration:
HK-4062X
Survivors:
Yes
Schedule:
San Andrés – Bogotá – Pereira
MSN:
196
YOM:
1990
Country:
Crew on board:
5
Crew fatalities:
Pax on board:
39
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following a normal approach and landing, the crew started the braking procedure. After a course of about 700 metres, the undercarriage slowly retracted. The aircraft came to rest on its belly and was damaged beyond repair. All 44 occupants escaped uninjured.

Crash of a Dornier DO228-212 near Miri: 10 killed

Date & Time: Sep 6, 1997 at 1942 LT
Type of aircraft:
Operator:
Registration:
9M-MIA
Survivors:
No
Site:
Schedule:
Labuan – Bandar Seri Begawan – Miri
MSN:
8217
YOM:
1993
Flight number:
BI238
Location:
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The twin engine aircraft departed Bandar Seri Begawan Airport at 1903LT on a regular schedule flight to Miri, Sarawak. At 1936LT, the crew was cleared for an approach to runway 02 but failed to acknowledge. Six minutes later, while descending by night, the aircraft struck the slope of Mt Lambir (500 metres high) located 13,7 km from the airport. The wreckage was found the next morning at 0710LT. All 10 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew descended below the minimum safe altitude for unknown reasons.

Crash of a Boeing 737-268A in Najran

Date & Time: Sep 6, 1997 at 0945 LT
Type of aircraft:
Operator:
Registration:
HZ-AGM
Flight Phase:
Survivors:
Yes
Schedule:
Riyadh – Najran – Sharurah
MSN:
21282
YOM:
1976
Flight number:
SV1861
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
79
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll from Najran Airport runway 06/24, at a speed of 95 knots, the right engine thrust suddenly increased. Few seconds later, at a speed of 120 knots, the exhaust gas temperature warning came on in the cockpit panel. The captain decided to abort and initiated an emergency landing procedure. Speed brakes were deployed but the thrust reversers could not be activated. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and right engine before coming to rest. All 85 occupants evacuated safely.