Crash of a Boeing 737-301F in Wamena

Date & Time: Jul 18, 2017 at 1239 LT
Type of aircraft:
Operator:
Registration:
PK-YGG
Flight Type:
Survivors:
Yes
Schedule:
Timika – Wamena
MSN:
23743/1510
YOM:
1988
Flight number:
TMG103
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The aircraft was performing a cargo flight from Timika, carrying five crew members and a load of various goods including constructioin materials. Upon landing on runway 15, the airplane bounced twice. It went out of control and veered off runway to the left. While contacting soft ground, both main landing gear were torn off and the aircraft slid for few dozen metres before coming to rest. All five crew members evacuated safely while the aircraft was damaged beyond repair.

Crash of a Pilatus PC-6/B2-H4 Turbo Porter near Wamena: 5 killed

Date & Time: Jul 5, 2017 at 1110 LT
Operator:
Registration:
PK-RCX
Flight Phase:
Survivors:
No
Site:
Schedule:
Wamena – Derakma
MSN:
922
YOM:
1998
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
The single engine aircraft departed Wamena Airport at 1100LT with three passengers, two pilots and 508 kg of various goods. About 10 minutes later, the airplane struck the slope of a mountain at an altitude of 2,300 metres. It was scheduled to arrive at Derakma at 1125LT. The wreckage was found a day later by the crew of a helicopter. All five occupants were killed. At the time of the accident, VMC conditions prevailed.

Crash of a Lockheed C-130H Hercules in Wamena: 13 killed

Date & Time: Dec 18, 2016 at 0609 LT
Type of aircraft:
Operator:
Registration:
A-1334
Flight Type:
Survivors:
No
Site:
Schedule:
Timika – Wamena
MSN:
4785
YOM:
1978
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
The four engine aircraft departed Timika-Moses Kilangin Airport at 0535LT bound for Wamena. While approaching Wamena, the crew encountered marginal weather conditions and the aircraft descended through several cloud layers when it impaxted a hilly terrain about four minutes before ETA at 0613LT. The aircraft was destroyed by impact forces and a post crash fire and all 13 occupants were killed. The wreckage was found less than 2 km southeast from runway 33 threshold.

Crash of a Boeing 737-347 in Wamena

Date & Time: Sep 13, 2016 at 0733 LT
Type of aircraft:
Operator:
Registration:
PK-YSY
Flight Type:
Survivors:
Yes
Schedule:
Jayapura – Wamena
MSN:
23597/1287
YOM:
1986
Flight number:
TGN7321
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
23823
Captain / Total hours on type:
9627.00
Copilot / Total flying hours:
650
Copilot / Total hours on type:
480
Aircraft flight hours:
59420
Aircraft flight cycles:
48637
Circumstances:
On 13 September 2016, a Boeing 737-300 Freighter, registered PK-YSY was being operated by PT. Trigana Air Service on a scheduled cargo flight from Sentani Airport, Jayapura (WAJJ) to Wamena Airport, Wamena (WAVV), Papua, Indonesia. Approximately 2130 UTC, during the flight preparation, the pilot received weather information which stated that on the right base runway 15 of Wamena Airport, on the area of Mount Pikei, low cloud was observed with the cloud base was increasing from 200 to 1000 feet and the visibility was 3 km. At 2145 UTC, the aircraft departed Sentani Airport with flight number IL 7321 and cruised at altitude 18,000 feet. On board the aircraft was two pilots and one Flight Operation Officer (FOO) acted as loadmaster. The aircraft carried 14,913 kg of cargo. The Pilot in Command (PIC) acted as Pilot Flying (PF) while the Second in Command (SIC) acted as Pilot Monitoring (PM). There was no reported or recorded aircraft system abnormality during the flight until the time of occurrence. After passing point MALIO, the aircraft started to descend. The pilot observed the weather met the criteria of Visual Meteorological Condition (VMC). The pilots able to identify another Trigana flight from Sentani to Wamena in front of them. While passing altitude 13,500 feet, approximately over PASS VALLEY, the Wamena Tower controller instructed the pilot to report position over JIWIKA. When the aircraft position was over point JIWIKA, the Wamena Tower controller informed to the pilot that the flight was on sequence number three for landing and instructed the pilot to make orbit over point X, which located at 8 Nm from runway 15. The pilot made two orbits over Point X to make adequate separation with the aircraft ahead prior to received approach clearance. About 7,000 feet (about 2,000 feet above airport elevation), the pilot could not identify visual checkpoint mount PIKEI and attempted to identify a church which was a check point of right base runway 15. The pilot felt that the aircraft position was on right side of runway centerline. About 6,200 feet (about 1,000 feet above airport elevation), the PF reduced the rate of descend and continued the approach. The PM informed to the PF that runway was not in sight and advised to go around. The PF was confident that the aircraft could be landed safely as the aircraft ahead had landed. Approximately 5,600 feet altitude (about 500 feet above airport elevation) and about 2 Nm from runway threshold the PF was able to see the runway and increased the rate of descend. The pilot noticed that the Enhanced Ground Proximity Warning System (EGPWS) aural warning “SINK RATE” active and the PF reduced the rate of descend. While the aircraft passing threshold, the pilot felt the aircraft sunk and touched down at approximately 125 meters from the beginning runway 15. The Flight Data Recorder recorded the vertical acceleration was 3.25 g on touchdown at 2230 UTC. Both of main landings gear collapsed. The left main landing gear detached and found on runway. The engine and lower fuselage contacted to the runway surface. The aircraft veer to the right and stopped approximately 1,890 meters from the beginning of the runway 15. No one was injured on this occurrence and the aircraft had substantially damage. Both pilots and the load master evacuated the aircraft via the forward left main cargo door used a rope.
Probable cause:
Refer to the previous aircraft that was landed safely, the pilot confidence that a safe landing could be made and disregarding several conditions required for go around.
Final Report:

Crash of a Cessna 208B Grand Caravan EX in Lolat

Date & Time: Jun 14, 2016 at 0758 LT
Type of aircraft:
Operator:
Registration:
PK-RCK
Flight Type:
Survivors:
Yes
Schedule:
Wamena – Lolat
MSN:
208B-5149
YOM:
2014
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
53
Circumstances:
The single engine airplane departed Wamena Airport at 0739LT on a cargo flight to Lolat, carrying two passengers, one pilot and a load of building materials for a total weight of 1,190 kilos. On short final to Lolat Airfield, the aircraft impacted the roof of a wooded house and crashed, bursting into flames. All three occupants of the airplane evacuated safely while three people in the house were injured. The aircraft was totally destroyed by a post crash fire.

Crash of a Boeing 737-3Q8 in Wamena

Date & Time: Aug 28, 2015 at 1547 LT
Type of aircraft:
Operator:
Registration:
PK-BBY
Flight Type:
Survivors:
Yes
Schedule:
Jayapura – Wamena
MSN:
23535/1301
YOM:
1986
Flight number:
8F189
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13880
Captain / Total hours on type:
4877.00
Copilot / Total flying hours:
608
Copilot / Total hours on type:
342
Aircraft flight hours:
54254
Aircraft flight cycles:
38422
Circumstances:
On 28 August 2015 a Boeing 737-300 Freighter, registered PK-BBY was being operated by PT. Cardig Air on a scheduled cargo flight from Sentani Airport (WAJJ) Jayapura to Wamena Airport (WAVV) Papua, Indonesia. At 1234 LT (0334 UTC), the aircraft departed to Wamena and on board the aircraft were two pilots, and 14,610 kg of cargo. The Pilot in Command (PIC) acted as Pilot Flying (PF) while the Second in Command (SIC) who was under line training acted as Pilot Monitoring (PM). There was no reported or recorded aircraft system abnormality during the flight until the time of occurrence. At 0637 UTC, when the aircraft approaching PASS VALLEY, the Wamena Tower controller provided information that the runway in use was runway 15 and the wind was 150°/18 knots, QNH was 1,003 mbs and temperature was 23 °C. At 0639 UTC, the pilot reported position over PASS VALLEY, descended passing FL135. The Wamena Tower controller instructed the pilot to report position over JIWIKA. At 0645 UTC, the pilot reported position over JIWIKA and continued to final runway 15. At 0646 UTC, the pilot reported position on final runway 15 and Wamena Tower controller provided landing clearance with additional information of wind 150°/15 knots and QNH 1,003 mbs. At 0647 UTC, the aircraft touched down about 35 meter before the beginning runway 15 with vertical acceleration of 3.68 G. The left main landing gear collapsed and the left engine contacted to the runway surface. The aircraft stopped at about 1,500 meters from runway threshold. No one was injured on this occurrence.
Probable cause:
According to factual information during the investigation, the Komite Nasional Keselamatan Transportasi determines the findings of the investigation are listed as follows:
1. The pilots held valid licenses and medical certificates.
2. The aircraft had a valid Certificate of Airworthiness (C of A) and Certificate of Registration (C of R), and was operated within the weight and balance envelope.
3. There were no reports of aircraft system abnormalities during the flight.
4. After passed JIWIKA on altitude 10,000 feet, the FDR recorded the engines were on idle, the average rate of descend was approximately 2,000 feet per minute.
5. At altitude approximately 8,000 feet, the flap selected to 40 position and moved to 39.9° one minute 25 seconds later.
6. The BMKG weather report was wind 150°/14-19 knots and the Wamena Tower controller reported to the pilot that the wind was 150°/15 knots. The information of gust wind, which indicated the possibility of windshear, was not reported to the pilot.
7. The EGPWS “CAUTION WINDSHEAR” active on altitude of 5,520 feet.
8. 06:45:43 UTC, the engine power increased when the aircraft altitude was on 5,920 feet prior the EGPWS altitude call “ONE HUNDRED” heard.
9. Started from 06:45:45 UTC, the FDR recorded the CAS increased from 148 knots to 154 knots followed by N1 decreased gradually from 73% to 38%. Three seconds before touched down, the rate of descend was constant on value 1,320 feet per minute followed by EGPWS warning “SINK RATE”.
10. The aircraft touched down at about 35 meters before the beginning runway 15 with the vertical acceleration recorded of 3.68 G.
11. The trunnion link of the left Main Landing Gear (MLG) assembly was found broken and the left main landing gear collapsed.
12. The FDR data contained of 107 flight hours consisted of 170 flight sectors which recorded five times of the vertical acceleration more than 2 G during landing at Wamena. The accumulation of such value of vertical acceleration might lead to landing gear strength degradation.
13. The Visual Approach Slope Indicator (VASI) of runway 15 was not operated after the runway extension.
14. The investigation found several touchdown marks on the pavement before the runway 15.
15. Excessive rubber deposit was found on the surface of runway 15 at about 600 meter started from the runway threshold.
16. The absence of speed correction following the information of headwind of 15 knots and pilot crew briefing after activation of EGPWS caution windshear indicated that the pilot did not aware of the existing windshear, that might be contributed by the absence of gust wind information.
17. The large thrust reduction was not in accordance with the FCOM for windshear precaution and resulted in rapid descend.
18. The accident flight collapsed the landing gear, the FDR recorded the vertical acceleration was 3.683 G which was within the landing gear design limit. This indicated the degradation of landing gear strength.

Contributing Factor:
The large thrust reduction during the windshear resulted in rapid descend and the aircraft touched down with 3.683 G then collapsed the landing gear that had strength degradation.
Final Report:

Crash of a Pacific Aerospace PAC750XL in Ninia: 1 killed

Date & Time: Aug 12, 2015 at 0748 LT
Operator:
Registration:
PK-KIG
Survivors:
Yes
Schedule:
Wamena – Ninia
MSN:
170
YOM:
2010
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
1537
Captain / Total hours on type:
395.00
Aircraft flight hours:
757
Aircraft flight cycles:
1315
Circumstances:
On 12 August 2015, a PAC-750XL aircraft, registered PK-KIG, was being operated by PT. Komala Indonesia on an unscheduled passenger flight from Wamena Airport (WAJW) Papua to Ninia Airstrip , Yahukimo, Papua that was located on radial 127° from Wamena with a distance of approximately 26 Nm. At 0733 LT (2233 UTC), the aircraft departed from Wamena Airport with an estimated time of arrival at Ninia of 2248 UTC. The flight was uneventful until approaching Ninia. On board the aircraft were one pilot, one engineer and 4 passengers. According to the pilot statement, an airspeed indicator malfunction occurred during flight. Video footage taken by a passenger showed that, during the approach at an altitude of approximately 6,500 feet, the airspeed indicators indicated zero and the aural stall warning activated. The aircraft then flew on the left side and parallel to the runway. Thereafter the aircraft climbed, turned left and impacted the ground about 200 meters south-west of the runway. The engineer on board was fatally injured, one passenger had minor injuries and the other occupants, including the pilot, were seriously injured. Two occupants were evacuated to a hospital in Jayapura Airport and four others, including the fatally injured, were evacuated to a hospital in Wamena.
Probable cause:
The following findings were identified:
1. Continuing the flight with both airspeed indicators unserviceable increased the complexity of the flight combined with high-risk aerodrome increased the pilot workload.
2. The improper corrective action at the time of the aural stall warning activating on the final approach, and the aircraft flew to insufficient area for a safe maneuver.
3. The unfamiliarity to the airstrip resulted in inappropriate subsequent escape maneuver and resulted in the aircraft stalling.
4. The pilot was not provided with appropriate training and familiarization to fly into a high-risk airstrip
Final Report:

Crash of a BAe ATP-F in Wamena

Date & Time: Mar 4, 2015 at 1515 LT
Type of aircraft:
Operator:
Registration:
PK-DGB
Flight Type:
Survivors:
Yes
Schedule:
Jayapura – Wamena
MSN:
2029
YOM:
1990
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3912
Captain / Total hours on type:
833.00
Copilot / Total flying hours:
415
Copilot / Total hours on type:
45
Aircraft flight hours:
200845
Aircraft flight cycles:
27921
Circumstances:
On 4 March 2015 a BAe-ATP registration PK-DGB operated by PT. Deraya Air as scheduled cargo flight from Sentani to Wamena Airport. On board of this flight was two pilots while the Pilot in Command (PIC) acted as pilot flying and First Officer (FO) acted as pilot monitoring. The aircraft departed Sentani at 0524 UTC to Wamena airport. The pilot contacted Wamena Tower controller while position on Jiwika way point at altitude 10,000 feet. Wamena Tower controller instructed to use runway 33 and to proceed to left runway 33. At 0602 UTC the pilot requested to proceed to Pyramid waypoint and to descend to 8,000 feet and made holding due to weather. At 0613, a C-130 pilot that was on approach reported making go around runway 33 and ATC instructed to C-130 pilot to proceed to Pyramid waypoint and hold. At 0619 UTC, Wamena Tower controller informed that the weather reported continuous heavy rain, visibility was reported 2 up to 3 km and wind was from 060° with velocity of 6 knots. The PK-DGB aircraft left Pyramid waypoint for approach runway 33. The aircraft proceed to left downwind and descent to 6,500 feet. During turning base leg, the pilot observed runway insight and continued the approach. At 0620 UTC, the aircraft touched down, thereafter veered off to the right of the runway and skid. The aircraft re-entered the runway at approximately 400 meters from beginning runway 33 and stopped near taxiway Delta at approximately 800 meters from beginning runway 33.

Crash of a BAe ATP in Wamena

Date & Time: May 31, 2013 at 0709 LT
Type of aircraft:
Operator:
Registration:
PK-DGI
Flight Type:
Survivors:
Yes
Schedule:
Jayapura - Wamena
MSN:
2027
YOM:
1990
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
3108
Captain / Total hours on type:
1366.00
Copilot / Total flying hours:
5648
Copilot / Total hours on type:
689
Aircraft flight hours:
15755
Aircraft flight cycles:
25431
Circumstances:
On 31 May 2013 aircraft BAe ATP freighter registered PK-DGI operated by PT. Deraya as scheduled cargo/ freight flight from Sentani Airport (WAJJ) to Wamena Airport (WAJW), Papua. On board in this flight were the Pilot in Command (PIC) acted as Pilot Flying (PF) and the Second in Command (SIC) acted as Pilot Monitoring (PM). At 2127 UTC (0627 LT) the aircraft departed from Sentani Airport. The aircraft cruised at 12,000 feet (FL 120)and estimated time of arrival Wamena Airport was 2207 UTC (0707 LT). The first pilot contact with Wamena Tower controller was at 2201 UTC, the aircraft position was approaching Pass Valley point, the controller informed that runway 15 expect to be used and the weather condition was wind calm, visibility 4 Km, low cloud at final area and QNH 1008 mbs. There was no specific of approach and landing briefing by pilot flying to the pilot non flying considering to such weather condition. At 2207 UTC, the pilot reported the position was on final runway 15. The controller requested the information of the flight condition and the pilot reported that the runway has not insight. At 2209 UTC, the pilot reported that the runway was insight and the controller provided the clearance to land and 25 seconds later the aircraft touched down on the centerline. During the landing roll at about 750 meters from the beginning of runway 15 the aircraft veered to the left of the runway shoulder, the pilot recovered by applying the right rudder and asymmetry reverses thrust but the aircraft continued veer to the left and stopped at about 10 meters on the left shoulder of the runway 15. On the landing roll, the FDR recorded that the left engine torque greater then right engine torque. The pilot shutdown both engines normally and evacuated the aircraft safely. The nose landing gear detached and found on the shoulder at about 250 meter from the aircraft final position. The main landing gears broken and all the propellers bent. No injured in this occurrence.
Probable cause:
The following contributing factors were identified:
- The flight did not meet the criteria according to the recommended elements of stabilized approach which required go around.
- The aircraft touched down with 2° misalignment with the runway direction then the aircraft veered off to the left.
- The recovery action was not in accordance to the correct technique according to the ALAR Tool Kit.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 near Wamena: 3 killed

Date & Time: Jun 29, 2009 at 1601 LT
Operator:
Registration:
PK-BRO
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Dekai - Wamena
MSN:
756
YOM:
1981
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
3
Circumstances:
The twin engine aircraft departed Dekai Airport at 1530LT on a cargo flight to Wamena, carrying three crew members and a load of 1,600 kilos of various goods. Between 1554LT and 1600LT, the crew was in contact with Wamena. At 1601LT, while cruising at an altitude of 9,600 feet in limited visibility, the aircraft collided with a mountain slope. The wreckage was found a day later about 19 km southeast from Wamena. The aircraft disintegrated on impact and all three occupants were killed.
Probable cause:
Controlled flight into terrain after the crew was flying under VFR mode in IMC conditions. IFR approach to Wamena are not possible, VFR only.