Crash of an ATR72-500 in Magong: 48 killed

Date & Time: Jul 23, 2014 at 1906 LT
Type of aircraft:
Operator:
Registration:
B-22810
Survivors:
Yes
Site:
Schedule:
Kaohsiung – Magong
MSN:
642
YOM:
2000
Flight number:
GE222
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
54
Pax fatalities:
Other fatalities:
Total fatalities:
48
Captain / Total flying hours:
22994
Captain / Total hours on type:
19069.00
Copilot / Total flying hours:
2392
Copilot / Total hours on type:
2083
Aircraft flight hours:
27039
Aircraft flight cycles:
40387
Circumstances:
The aircraft was being operated on an instrument flight rules (IFR) regular public transport service from Kaohsiung to Magong in the Penghu archipelago. At 1906 Taipei Local Time, the aircraft impacted terrain approximately 850 meters northeast of the threshold of runway 20 at Magong Airport and then collided with a residential area on the outskirts of Xixi village approximately 200 meters to the southeast of the initial impact zone. At the time of the occurrence, the crew was conducting a very high frequency omni-directional radio range (VOR) non-precision approach to runway 20. The aircraft was destroyed by impact forces and a post-impact fire. Ten passengers survived the occurrence and five residents on the ground sustained minor injuries. The occurrence was the result of controlled flight into terrain, that is, an airworthy aircraft under the control of the flight crew was flown unintentionally into terrain with limited awareness by the crew of the aircraft’s proximity to terrain. The crew continued the approach below the minimum descent altitude (MDA) when they were not visual with the runway environment contrary to standard operating procedures. The investigation report identified a range of contributing and other safety factors relating to the flight crew of the aircraft, TransAsia’s flight operations and safety management processes, the communication of weather information to the flight crew, coordination issues at civil/military joint-use airport, and the regulatory oversight of TransAsia by the Civil Aeronautics Administration (CAA).
Probable cause:
- The flight crew did not comply with the published runway 20 VOR non-precision instrument approach procedures at Magong Airport with respect to the minimum descent altitude (MDA). The captain, as the pilot flying, intentionally descended the aircraft below the published MDA of 330 feet in the instrument meteorological conditions (IMC) without obtaining the required visual references.
- The aircraft maintained an altitude between 168 and 192 feet before and just after overflying the missed approach point (MAPt). Both pilots spent about 13 seconds attempting to visually locate the runway environment, rather than commencing a missed approach at or prior to the MAPt as required by the published procedures.
- As the aircraft descended below the minimum descent altitude (MDA), it diverted to the left of the inbound instrument approach track and its rate of descent increased as a result of the flying pilot’s control inputs and meteorological conditions. The aircraft’s hazardous flight path was not detected and corrected by the crew in due time to avoid the collision with the terrain, suggesting that the crew lost situational awareness about the aircraft’s position during the latter stages of the approach.
- During the final approach, the heavy rain and associated thunderstorm activity intensified producing a maximum rainfall of 1.8 mm per minute. The runway visual range (RVR) subsequently reduced to approximately 500 meters. The degraded visibility significantly reduced the likelihood that the flight crew could have acquired the visual references to the runway environment during the approach.
- Flight crew coordination, communication, and threat and error management were less than effective. That compromised the safety of the flight. The first officer did not comment about or challenge the fact that the captain had intentionally descended the aircraft below the published minimum descent altitude (MDA). Rather, the first officer collaborated with the captain’s intentional descent below the MDA. In addition, the first officer did not detect the aircraft had deviated from the published inbound instrument approach track or identify that those factors increased the risk of a controlled flight into terrain (CFIT) event.
- None of the flight crew recognized the need for a missed approach until the aircraft reached the point (72 feet, 0.5 nautical mile beyond the missed approach point) where collision with the terrain became unavoidable.
- The aircraft was under the control of the flight crew when it collided with foliage 850 meters northeast of the runway 20 threshold, two seconds after the go around decision had been made. The aircraft sustained significant damage and subsequently collided with buildings in a residential area. Due to the high impact forces and post-impact fire, the crew and most passengers perished.
- According to the flight recorders data, non-compliance with standard operating procedures (SOP's) was a repeated practice during the occurrence flight. The crew’s recurring non-compliance with SOP's constituted an operating culture in which high risk practices were routine and considered normal.
- The non-compliance with standard operating procedures (SOP's) breached the obstacle clearances of the published procedure, bypassed the safety criteria and risk controls considered in the design of the published procedures, and increased the risk of a controlled flight into terrain (CFIT) event.
Final Report:

Crash of a Saab 340 off Hsinchu: 13 killed

Date & Time: Mar 18, 1998 at 1932 LT
Type of aircraft:
Operator:
Registration:
B-12255
Flight Phase:
Survivors:
No
Schedule:
Hsinchu - Kaohsiung
MSN:
337
YOM:
1993
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
13
Aircraft flight hours:
8076
Circumstances:
When the crew boarded the aircraft in Hsinchu for the flight to Kaohsiung it had been a long and demanding day for the captain who was to fly the aircraft. He had been on duty more than 11 hours and performed nine flights. The accident flight, which was planned to be his last flight of the day, was to take place in darkness. The weather was above minima but IMC. During the pre-flight check the crew noted a failure in the RH Main Bus. This caused a number of systems to be unavailable, a.o.: the autopilot, the left hand EFIS, LH/RH Flight Director, LH RMI, EFIS Comparators, and the no. 2 engine anti-ice start bleed valve being open (as a result of this, the ITT on this engine was approximately 15°C higher than normal at selected power on this engine). Despite the fact that, according to the Minimum Equipment List (MEL), taking off for a flight with any of the Main Buses inoperative was not allowed, the captain decided to continue. During taxi to runway 05 the aircraft was cleared for a Chunan One (CN1) departure. The aircraft took off at 19:29:09. Because of the autopilot was not available, the captain now had to fly manually. In addition, the flying had to be performed without support from the yaw-damper that was also inoperative as a result of the RH Main Bus failure. This means that more active rudder control was required, while the DFDR-data shows that such input was not made. The more than 30°C ITT-split between the engines, of which approximately 15°C was caused by the RH Engine Anti-ice Start Bleed Valve being open, did have little effect on the behavior of the aircraft in the initial start-sequence. But when the crew, 30 seconds after lift off, disengaged CTOT and started to manually adjust the RH PLA downwards, possibly to get equal ITT in the engines, this ended up in a torque-split of more than 13% between the engines, with the RH engine being lower in torque. This asymmetry tended to yaw and roll the aircraft to the right and required higher aileron input than normal to the left in order to keep the aircraft at a constant bank angle. Normally the flaps are retracted at around 1,000 feet during initial climb. In this flight the flap retraction was not initiated until the first officer was reading the Climb Check List in which the flap position should be checked and verified. Flap retraction was done just prior to the aircraft reaching VFE15 (175 KIAS, which is the maximum allowed speed with flaps extended). When the climb power was set, a symmetric PLA change was made. However, due to the earlier RH Power Lever Angle (PLA) pull in combination with the normal backlash in the power lever cables between the PLA and the HMU, the RH engine torque was decreased while the LH engine torque remained unchanged. Hence, a torque split occurred. This resulted in an increased aerodynamic asymmetry giving a force tending to yaw and bank the aircraft to the right. Consequently, still more aileron input was required in order to maintain a correct bank angle. Because the behavior of the aircraft was very different from what the captain was used to, the need for continuous manual flying under IMC-conditions may have totally occupied his capacity. This could also explain why, during this phase of flight, he did not observe the aircraft starting a turn to the right 78 seconds after take off instead of continuing the left turn for a heading of 260. At about this same time, and for no obvious reasons, the positive rate of climb decreased and the aircraft leveled out at approximately 2,000 feet for a short time instead of continuing the climb to its assigned altitude of 3,000 feet. The captain's actions could be interpreted as signs that he might have been suffering from fatigue or spatial disorientation. It is difficult to determine if the F/O was aware of the captain's deviation from the cleared departure route. All indications point to the fact that he was not aware or that he out of respect for the captain did not report of the deviations. For example, the F/O transmitted back to Taipei Approach 114 seconds after takeoff, "Left 230, Bravo 12255," while at the same time the aircraft was in a right turn with a 21 degree right bank, passing through a heading of 312 degrees. In fact, his primary means for monitoring the flight were very limited due to dark, IMC-conditions since his EFIS instruments were black or flagged. This could also explain why the captain did not receive any support from the F/O about the flight becoming more and more uncontrolled. Not until 124 seconds after takeoff and 37 seconds prior to the last DFDR-recording did the captain state that he was having a problem with the heading and asked for help with the magnetic compass. At that time the aircraft was in a 24° right bank and 10° pitch up position and had a heading and roll rate by one degree per second. From that moment a continuous decrease in pitch angle was recorded down to -65,4° just prior to the impact. Just 19 seconds before the last DFDR-recording, with a heading of 022 and a bank angle of 36° to the right, the captain said "Ask for a radar vector." At this moment, he also initiates a short aileron input to the right, further increasing the bank angle. The other crewmembers did not answer or give any notable response to the captain's request for help with the magnetic compass. The reason might be that they also were very confused about the situation and unable to take any relevant action. When the captain, 14 seconds before the last DFDR-recording, said "Wah Sei!!! Everything is wrong." the aircraft was in a 8,4° pitch down and the right bank angle was 47,5°. Finally, only 10 seconds before the last data point was recorded, the first officer responds by asking "Sir, shall we look at this one? ". Pitch down was then 15,8° and the right roll angle 71,7°. In the last part of the flight the pitch and bank angles were at extreme values not to be experienced in normal operation. At this stage of the flight, the control inputs recorded are rapid aileron inputs to the right that further increased the adverse attitudes. The aircraft was then totally uncontrolled and the airspeed and sink rate increased dramatically. Four seconds before impact the Vmo warning started. The aircraft then crashed into the sea.
Probable cause:
The following factors were identified:
- The flight crew's failure to maintain the situational awareness resulting in the loss of aircraft control,
- The failure of R/H main electrical bus resulting in the malfunction of R/H navigation system and flight instruments,
- Flight crew did not comply with MEL,
- Night time and IMC resulted in no or limited visual reference for the flight crew,
- The captain conducted the flight in a fatigue and spatial disorientation condition,
- Flight crew did not comply with standard operation procedures.

Crash of a Grumman S-2 Tracker near Kaohsiung: 4 killed

Date & Time: May 25, 1996
Type of aircraft:
Operator:
Registration:
2219
Flight Phase:
Flight Type:
Survivors:
No
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
4
Circumstances:
Crashed in unknown circumstances near Kaohsiung. All four occupants were killed, two pilots and two officers.

Crash of a McDonnell Douglas MD-82 in Kaohsiung

Date & Time: Oct 25, 1993 at 1159 LT
Type of aircraft:
Operator:
Registration:
B-28003
Survivors:
Yes
Schedule:
Kaohsiung - Taipei
MSN:
53065
YOM:
1991
Flight number:
FE118
Country:
Region:
Crew on board:
8
Crew fatalities:
Pax on board:
152
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After takeoff from Kaohsiung-Hsiao Kang Airport, while climbing to a height of 600 feet, the left engine failed. The crew declared an emergency and was cleared to return. On approach, the aircraft was unstable and too high on the glide. It landed too far down the runway, about 4,000 feet past the runway threshold. Unable to stop within the remaining distance, the aircraft overran, collided with a drainage ditch, lost its undercarriage and eventually came to rest against a concrete wall. All 160 occupants were evacuated, among them four passengers were slightly injured.
Probable cause:
The fan cowl on the left engine separated during initial climb.

Crash of a Cessna 404 Titan II in Kaohsiung: 13 killed

Date & Time: Jun 27, 1989 at 0906 LT
Type of aircraft:
Operator:
Registration:
B-12206
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Kaohsiung – Wangan
MSN:
404-0418
YOM:
1978
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
Shortly after takeoff from Kaohsiung Airport, while in initial climb, the crew encountered engine troubles. The airplane stalled and crashed in a residential area near the airport, bursting into flames. A passenger was injured while 12 other occupants were killed as well as one people on the ground.
Probable cause:
Engine trouble for unknown reasons.

Crash of a Boeing 737-281 off Magong: 13 killed

Date & Time: Feb 16, 1986 at 1850 LT
Type of aircraft:
Operator:
Registration:
B-1870
Survivors:
No
Schedule:
Kaohsiung - Magong
MSN:
20226
YOM:
1969
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
6
Pax fatalities:
Other fatalities:
Total fatalities:
13
Circumstances:
On final approach to Magong Airport by night, the crew apparently encountered problems with the nose gear. The captain decided to initiate a go-around procedure. Few minutes later, while climbing, the airplane entered an uncontrolled descent and crashed in the sea. On March 10, the wreckage was found in a depth of 58 meters about 19 km north of the airport. All 13 occupants were killed.

Crash of a Boeing 737-222 in Sanyi: 110 killed

Date & Time: Aug 22, 1981 at 1000 LT
Type of aircraft:
Operator:
Registration:
B-2603
Flight Phase:
Survivors:
No
Schedule:
Taipei - Kaohsiung
MSN:
19939
YOM:
1969
Flight number:
FE103
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
104
Pax fatalities:
Other fatalities:
Total fatalities:
110
Aircraft flight cycles:
33313
Circumstances:
The airplane departed Taipei-Songshan Airport bound for Kaohsiung. Fourteen minutes later, while cruising at FL220, radar contact was lost with the airplane and the crew did not send any distress message. The airplane entered an uncontrolled descent, suffered an explosive cabin decompression, partially disintegrated in the air and crashed in Sanyi, in the Miaoli County. Debris scattered on a large area (10 km2) and all 110 occupants were killed, among them the Japanese writer Kuniko Mukōda.
Probable cause:
Extensive corrosion damage in the lower fuselage structures, and at a number of locations there were corrosion penetrated through pits, holes and cracks due to intergranular corrosion and skin thinning exfoliation corrosion, and in addition, the possible existence of undetected cracks because of the great number of pressurization cycles of the aircraft (a total of 33,313 landings), interaction of these defects and the damage had so deteriorated that rapid fracture occurred at a certain flight altitude and pressure differential resulting rapid decompression and sudden break of passenger compartment floor beams and connecting frames, cutting control cables and electrical wiring. And eventually loss of power, loss of control, midair disintegration.

Crash of a Britten-Norman BN-2A-8 Islander in Lanyu

Date & Time: Sep 9, 1979
Type of aircraft:
Operator:
Registration:
B-11107
Flight Phase:
Survivors:
Yes
Schedule:
Lanyu - Kaohsiung
MSN:
335
YOM:
1973
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was cleared for takeoff from runway 13/31 and increased engine power. Few seconds prior to rotation, the twin engine airplane collided with a Yung Shing Airlines Cessna 404 registered B-12204 that entered the runway without permission. Both aircraft came to rest on runway and all 16 occupants in both aircraft were injured.
Probable cause:
It was determined that the crew of the Cessna 404 engaged on runway without permission while the Islander was taking off.

Crash of a Dornier DO.28B-1 in Kaohsiung

Date & Time: Dec 27, 1974
Type of aircraft:
Registration:
B-125
Flight Phase:
Flight Type:
MSN:
3103
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Crashed in unknown circumstances while flying on behalf of the Civil Aviation Authority of Taiwan.

Crash of a Handley Page HPR-7 Dart Herald 201 near Tainan: 36 killed

Date & Time: Feb 24, 1969 at 1200 LT
Operator:
Registration:
B-2009
Flight Phase:
Survivors:
No
Schedule:
Kaohsiung - Taipei
MSN:
157
YOM:
1962
Flight number:
FE104
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
36
Circumstances:
After takeoff from Kaohsiung Airport, while climbing, the crew encountered technical problems with the right engine. The captain informed ground about his situation and was cleared to return for a safe landing. He quickly realized he could not make it so he reduced his altitude and attempted and emergency landing. While flying a low height over a dense wooded area, the airplane went out of control and eventually crashed in flames in an open field located near Tainan. The aircraft was totally destroyed and all 36 occupants were killed. The aircraft crashed 12 minutes after its takeoff from Kaohsiung Airport, bound for Taipei-Songshan Airport.
Probable cause:
It is believed that the right engine failed in flight. For undetermined reason, the crew was unable to feather the propeller that was windmilling, causing high drag and the loss of control.