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Crash of an Airbus A320-214 in Butuan

Date & Time: Oct 26, 2007 at 0645 LT
Type of aircraft:
Operator:
Registration:
RP-C3224
Survivors:
Yes
Schedule:
Manila - Butuan
MSN:
753
YOM:
1997
Flight number:
PR475
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
148
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Following an uneventful flight from Manila-Ninoy Aquino Airport, the crew started the approach to Butuan Airport in good weather conditions. After landing on runway 12/30 which is 1,965 metres long, the aircraft was unable to stop within the remaining distance. It overran, went down an embankment and came to rest in a coconut grove. The cockpit was partially destroyed and both pilots were seriously injured while 32 passengers escaped with minor injuries. 120 other occupants were unhurt and the aircraft was damaged beyond repair.
Probable cause:
It is believed that the aircraft landed too far down the runway, reducing the landing distance available.

Crash of an Airbus A320-214 in Bacolod: 3 killed

Date & Time: Mar 22, 1998 at 1941 LT
Type of aircraft:
Operator:
Registration:
RP-C3222
Survivors:
Yes
Schedule:
Manila - Bacolod
MSN:
708
YOM:
1997
Flight number:
PR137
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
124
Pax fatalities:
Other fatalities:
Total fatalities:
3
Captain / Total flying hours:
5048
Captain / Total hours on type:
74.00
Copilot / Total flying hours:
2886
Copilot / Total hours on type:
147
Aircraft flight hours:
1240
Aircraft flight cycles:
1070
Circumstances:
Flight PR137 was a regular scheduled passenger flight and departed Manila for Bacolod at 18:40. The airplane departed with the thrust reverser of engine n°1 inoperative. At 19:20, PR137 called Bacolod Approach Control and reported passing FL260 and 55 DME to Bacolod . The crew then requested landing instructions and was instructed to descend to FL90 after passing Iloilo and descend to 3,000 feet for a VOR runway 04 approach. Wind was 030° at 08 kts, altimeter 1014 mbs, transition level at FL60 and temperature at 28°C. At 19:28, the flight requested to intercept the final approach to runway 04 and Approach Control replied "PR 137 visual approach on final". At 19:37, Bacolod Tower cleared the flight to land at runway 04 and the clearance was acknowledged by the pilot. The approach was flown with the Autothrust system was engaged in SPEED mode. The thrust lever of engine no.1 was left in Climb detent. Upon touchdown the first officer called out "no spoilers, no reverse, no decel". Engine no.2 was set to full reverse thrust after touchdown, but the engine no .1 thrust lever was not retarded to idle and remained in the climb power position. Consequently, the spoilers did not deploy. Because one engine was set to reverse, the autothrust system automatically disengaged. With the autothrust disengaged, no. 1 engine thrust increased to climb thrust. Due to the asymmetrical thrust condition, the A320 ran off the right side of the runway. At this speed, rudder and nosewheel steering are ineffective. Engine no.2 was moved out of reverse up to more than 70 percent N1 and the airplane swerved back onto the runway. The A320 continued past the runway end. The aircraft hit the airport perimeter fence and then jumped over a small river. It continued to slice through a hallow block fence where it went through several clusters of shanties and trees. No fire ensued after the crash.
Probable cause:
The probable cause of this accident was the inability of the pilot flying to assess properly the situational condition of the aircraft immediately upon touch down with n°1 engine reverse inoperative, thereby causing an adverse flight condition of extreme differential power application during the landing roll resulting in runway excursion and finally an overshoot. Contributory to this accident is the apparent lack of technical systems knowledge and lack of appreciation of the disastrous effects of misinterpreting provisions and requirements of a Minimum Equipment List (MEL).
Final Report: