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Crash of a Boeing 737-8GP off Denpasar

Date & Time: Apr 13, 2013 at 1510 LT
Type of aircraft:
Operator:
Registration:
PK-LKS
Survivors:
Yes
Schedule:
Bandung - Denpasar
MSN:
38728/4350
YOM:
2013
Flight number:
LNI904
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
101
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
15000
Captain / Total hours on type:
6173.00
Copilot / Total flying hours:
1200
Copilot / Total hours on type:
923
Aircraft flight hours:
142
Aircraft flight cycles:
104
Circumstances:
On 13 April 2013, a Boeing 737-800 aircraft, registered PK-LKS, was being operated by PT. Lion Mentari Airlines (Lion Air) on a scheduled passenger flight as LNI 904. The aircraft departed from Husein Sastranegara International Airport (WICC) Bandung at 0545 UTC to Ngurah Rai International Airport (WADD), Bali, Indonesia. The flight was the last sector of four legs scheduled for the crew on that day which were Palu (WAML) - Balikpapan (WALL) - Banjarmasin (WAOO) - Bandung (WICC) - Bali (WADD). The aircraft flew at FL 390, while the Second in Command (SIC) was the Pilot Flying (PF) and the Pilot in Command (PIC) was the Pilot Monitoring (PM). There were 2 pilots, 5 flight attendants and 101 passengers comprising 95 adults, 5 children and 1 infant making a total of 108 persons on board. The flight from the departure until start of the approach into Bali was uneventful. At 0648 UTC, the pilot made first communications with the Bali Approach controller (Bali Director) when the aircraft was located 80 Nm from BLI VOR. The pilot received clearance to proceed direct to the TALOT IFR waypoint and descend to 17,000 feet. At 0652 UTC, the Bali Director issued a further clearance for the pilot direct to KUTA point and descent to 8,000 feet. At 0659 UTC, the aircraft was vectored for a VOR DME approach for runway 09 and descent to 3,000 feet. At 0703 UTC, while the aircraft was over KUTA point, the Bali Director transferred communications with the aircraft to Bali Control Tower (Ngurah Tower). At 0704 UTC, the pilot contacted Ngurah Tower controller and advised that the aircraft was leaving KUTA point. The Ngurah Tower controller instructed the pilot to continue the approach and to reduce the aircraft speed to provide sufficient separation distance with another aircraft. At 0707 UTC, the Ngurah Tower issued take-off clearance for a departing aircraft on runway 09. At 0708 UTC, with LKS at approximately 1,600 feet AGL, the Ngurah Tower controller saw the aircraft on final approach and gave a landing clearance with additional information that the wind was from 120° at 05 knots. At 0708:47 UTC, the aircraft Enhance Ground Proximity Warning System (EGPWS) aural alert called “ONE THOUSAND”, the SIC said one thousand, stabilized, continue, prepare for go-around missed approach three thousand. The FDR showed that the pilot flown using LNAV (Lateral Navigation) and VNAV (Vertical Navigation) during the approach until disengagement of the Auto Pilot. The sequence of events during the final approach is based on the recorded CVR and FDR data, and information from crew interviews as follows: At 0708:56 UTC, while the aircraft altitude was approximately 900 feet AGL, the SIC commented that the runway was not in sight, whereas the PIC commented “OK. Approach light in sight, continue”. At 0709:33 UTC, after the EGPWS aural alert “MINIMUM” sounded at an aircraft altitude of approximately 550 feet AGL, the SIC disengaged the autopilot and the auto-throttle and then continued the approach. At 0709:43 UTC, the EGPWS called “THREE HUNDRED”. At 0709:47 UTC, the CVR recorded a sound similar to rain hitting the windshield. At 0709:49 UTC, the EGPWS called “TWO HUNDRED”. At 0709:53 UTC, while the aircraft altitude was approximately 150 feet AGL, the PIC took over control of the aircraft. The SIC handed control to the PIC and stated that he could not see the runway. At 0710:01 UTC, after the EGPWS called “TWENTY”, the PIC commanded for go-around. At 0710:02 UTC, the aircraft impacted the water, short of the runway. The aircraft stopped facing to the north at about 20 meters from the shore or approximately 300 meters south-west of the beginning of runway 09. Between 0724 UTC to 0745 UTC, three other aircraft took-off and six aircraft landed using runway 09. At 0750 UTC, the airport was closed until 0850 UTC. At 0755 UTC, all occupants were completely evacuated, the injured passengers were taken to the nearest hospitals and uninjured occupants to the airport crisis centre.
Probable cause:
The National Transportation Safety Committee initial findings on the accident flight are as follows:
- The aircraft was airworthy prior to impact and has an item on the DMI (deferred maintenance item) category C (right engine oil filter).
- All crew has valid licenses and medical certificates.
- The Second in Command (SIC) acted as Pilot Flying (PF).
- The flight performed a VOR DME approach runway 09, and the published Minimum Descent Altitude (MDA) was 465 ft AGL.
- The approach configuration used was flap 40.
- At 900 ft AGL the PF did not have the runway in sight.
- Upon reaching the MDA the flight profile indicated a constant path.
- The PIC took over control of the aircraft at about 150 ft radio altitude.
- The SIC handed over control to the PIC at about 150 ft and stated that he could not see the runway.
- The final approach phase of the flight profile was outside the envelope of the EGPWS warning, therefore no EGPWS warning was recorded on the CVR.
The NTSC concluded in its final report that the accident was caused by the following factors:
- The aircraft flight path became unstable below minimum descends altitude (MDA) with the rate of descend exceeding 1000 feet per minute and this situation was recognized by both pilots.
- The flight crew loss of situational awareness in regards of visual references once the aircraft entered a rain cloud during the final approach below minimum descends altitude (MDA).
- The PIC decision and execution to go-around was conducted at an altitude which was insufficient for the go-around to be executed successfully.
- The pilots of accident aircraft was not provided with timely and accurate weather condition despite the weather around the airport and particularly on final approach to the airport was changing rapidly.
Final Report:

Crash of a McDonnell Douglas MD-82 in Surabaya

Date & Time: Mar 4, 2006 at 1625 LT
Type of aircraft:
Operator:
Registration:
PK-LMW
Survivors:
Yes
Schedule:
Denpasar – Surabaya
MSN:
49443/1291
YOM:
1986
Flight number:
JT8987
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
138
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Prior to departure from Bali to Surabaya, the crew was informed that the left engine's thrust reverser system was out of service. Following an uneventful flight, the crew completed a normal approach to runway 10 then landed according to procedures. After touchdown, the crew activated the thrust reverser when the airplane deviated to the right. The crew elected to counteract but the aircraft veered off runway, lost its undercarriage and came to rest in a grassy area. All 144 occupants evacuated safely while the aircraft was damaged beyond repair.

Crash of an Airbus A300-622R in Taipei: 203 killed

Date & Time: Feb 16, 1998 at 2006 LT
Type of aircraft:
Operator:
Registration:
B-1814
Survivors:
No
Site:
Schedule:
Denpasar - Taipei
MSN:
578
YOM:
1990
Flight number:
CI676
Country:
Region:
Crew on board:
14
Crew fatalities:
Pax on board:
182
Pax fatalities:
Other fatalities:
Total fatalities:
203
Captain / Total flying hours:
7210
Copilot / Total flying hours:
3530
Aircraft flight hours:
20193
Aircraft flight cycles:
8800
Circumstances:
Following an uneventful flight from Denpasar-Ngurah Rai Airport, the aircraft was approaching Taipei-Taoyuan Airport by night and marginal weather conditions with a limited visibility of 2,400 feet, an RVR of 3,900 feet and 300 feet broken ceiling, 3,000 feet overcast. On final approach to runway 05L in light rain and fog, at the altitude of 1,515 feet, the aircraft was 1,000 feet too high on the glide so the captain decided to initiate a go-around procedure. The automatic pilot system was disconnected but for unknown reasons, the crew failed to correct the pitch up attitude. The aircraft passed the runway threshold at an altitude of 1,475 feet, pitched up go around thrust was applied. The aircraft rapidly pitched up, reaching +35° and climbed through 1,723 feet at an airspeed of 134 knots. The gear had just been raised and the flaps set to 20°. The aircraft continued to climb to 2,751 feet when the speed dropped to 43 knots. At this point, the aircraft stalled, entered an uncontrolled descent (pitched down to 44,65°). The crew was apparently able to regain control when the aircraft rolled to the right at an angle of 20° 2-3 seconds prior to final impact. The aircraft struck the ground 200 feet to the right of the runway 05L centerline and 3,7 km from its threshold and eventually crashed on 12 houses. The aircraft disintegrated on impact and all 196 occupants were killed, among them five US citizens, one Indonesian and one French. On the ground, seven people were killed.
Probable cause:
The following factors were identified:
- Wrong approach configuration as the aircraft was too high on the glide,
- Poor crew coordination,
- The crew failed to comply with published procedures,
- Poor crew training,
- The crew failed to correct the pitch up attitude during the go-around procedure,
- Lack of visibility due to night, rain and fog.

Crash of a Douglas DC-10-30 in Fukuoka: 3 killed

Date & Time: Jun 13, 1996 at 1208 LT
Type of aircraft:
Operator:
Registration:
PK-GIE
Flight Phase:
Survivors:
Yes
Schedule:
Fukuoka – Denpasar – Jakarta
MSN:
46685
YOM:
1979
Flight number:
GA865
Country:
Region:
Crew on board:
15
Crew fatalities:
Pax on board:
260
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
10263
Captain / Total hours on type:
2641.00
Copilot / Total flying hours:
3910
Copilot / Total hours on type:
1437
Aircraft flight hours:
46325
Circumstances:
During the takeoff roll at Fukuoka-Itazuke Airport runway 16, at a speed of 158 knots, the captain started the rotation. During initial climb, at a height of about 3 metres, the right engine suffered a loss of power after a fan blade located on the 1st stage of the high pressure compressor disk separated. The N1 dropped to 23,7% and five seconds later, the flight engineer informed the crew about the failure of the engine n°1. The captain decided to abort the takeoff and landed back on runway. The aircraft contacted ground with a vertical acceleration of 2,1 g then thrust reversers were deployed and ground spoilers were extended. Unable to stop within the remaining distance, the aircraft overran, crossed a road, skidded for about 620 metres before coming to rest in an open field, bursting into flames. Three passengers were killed.
Probable cause:
Although the CAS was well in excess of V1 and the aircraft had already lifted off from the runway, the takeoff was aborted. Consequently the aircraft departed the end of the runway, came to rest and caught fire. It is estimated that contributing to the rejection of the takeoff under this circumstance was the fact that the CAP's judgement in the event of the engine failure was inadequate. Investigation revealed that the turbine blade that failed, had operated for 30913 hours and 6182 cycles. General Electric had advised customers to discard blades after about 6000 cycles.
Final Report:

Crash of a Douglas DC-9-32 in Denpasar

Date & Time: Jun 21, 1993 at 1125 LT
Type of aircraft:
Operator:
Registration:
PK-GNT
Survivors:
Yes
Schedule:
Yogyakarta - Denpasar
MSN:
47790/907
YOM:
1979
Flight number:
GA630
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
72
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
On approach to Denpasar-I Gusti Ngurah Rai Airport, Bali, the aircraft was too high on the glide. The captain made an overcorrection, causing the aircraft to approach the runway with a high rate of descent. In a nose-up attitude, the aircraft struck the runway surface with a positive acceleration of 5 g. After landing, the crew completed the deceleration and braking procedure, vacated the runway and rolled to the gate where all occupants disembarked safely. A complete inspection of the aircraft by technicians revealed that it suffered major fuselage damages and was later declared as damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the flying crew.

Crash of a De Havilland DHC-6 Twin Otter 300 in Labuan Bajo

Date & Time: Apr 3, 1990
Operator:
Registration:
PK-NUQ
Flight Phase:
Survivors:
Yes
Schedule:
Labuan Bajo – Denpasar
MSN:
488
YOM:
1976
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
14
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After liftoff from Labuan Bajo-Mutiara Airport, while in initial climb, the left engine oversped. The crew elected to make an emergency landing when the aircraft struck rocks then crashed in a ravine. All 17 occupants were injured.
Probable cause:
Loss of control during initial climb after the left engine oversped for unknown reasons.

Crash of a Douglas DC-9-32 in Denpasar

Date & Time: Dec 30, 1984
Type of aircraft:
Operator:
Registration:
PK-GNI
Survivors:
Yes
Schedule:
Jakarta - Denpasar
MSN:
47636
YOM:
1974
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
69
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following several errors during the final approach, the aircraft altitude over the runway 09 threshold was too high. The pilot-in-command decided to continue the landing and the touchdown was completed 1,800 meters past the runway threshold. Unable to stop within the remaining distance, the aircraft overran, lost its undercarriage and came to rest in a mangrove, broken in three. All 75 occupants were evacuated, some of them were injured. The aircraft was destroyed.
Probable cause:
Wrong approach configuration on part of the flying crew.

Crash of a Fokker F28 Friendship 1000 on Mt Bromo: 4 killed

Date & Time: Mar 6, 1979 at 1855 LT
Type of aircraft:
Operator:
Registration:
PK-GVP
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Denpasar - Surabaya
MSN:
11094
YOM:
1975
Flight number:
GA553
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Aircraft flight hours:
7676
Aircraft flight cycles:
6707
Circumstances:
The airplane departed Denpasar-Ngurah Rai Airport at 1829LT on a positioning flight to Surabaya, carrying a crew of four. Following a level off at FL165, the crew was cleared to start the descent to Surabaya-Juanda Airport and passed successively FL100 and FL60 when the airplane struck the slope of Mt Bromo (1,890 meters high) located about 33 km southwest of Probolinggo. The aircraft was destroyed upon impact and all four crew members were killed.
Probable cause:
Controlled flight into terrain.

Crash of a Boeing 707-321C near Denpasar: 107 killed

Date & Time: Apr 22, 1974 at 2226 LT
Type of aircraft:
Operator:
Registration:
N446PA
Survivors:
No
Site:
Schedule:
Hong Kong - Denpasar - Sydney - Suva - Honolulu - Los Angeles
MSN:
19268/544
YOM:
1966
Flight number:
PA812
Country:
Region:
Crew on board:
11
Crew fatalities:
Pax on board:
96
Pax fatalities:
Other fatalities:
Total fatalities:
107
Captain / Total flying hours:
18247
Captain / Total hours on type:
7192.00
Copilot / Total flying hours:
6312
Copilot / Total hours on type:
4776
Aircraft flight hours:
27943
Aircraft flight cycles:
9123
Circumstances:
Following an uneventful flight from Hong Kong-Kai Tak, the crew started the descent to Denpasa-Ngurah Rai Airport by night and limited visibility. While descending to runway 09 at an altitude of 4,000 feet, the airplane initiated a turn to 263° when it struck the slope of Mt Masehe located about 68 km from the airport. The wreckage was found few hours later. The aircraft was totally destroyed upon impact and all 107 occupants have been killed.
Probable cause:
The premature execution of a right-hand turn to join the 263 degrees outbound track which was based on the indication given by only one of the ADF's while the other one was still in steady condition.
Final Report: