Philippines

The four engine aircraft departed Manila-Ninoy Aquino Airport at 1536LT on a schedule flight to Caticlan with 45 passengers and four crew members. On approach to Caticlan, the crew encountered technical problems with the hydraulic system and could not lowered the right main gear that remained stuck in its wheel well. The captain decided to return to Manila and followed a holding pattern to burn fuel. After touchdown on runway 24, the aircraft went out of control, veered off runway to the right and came to rest in a grassy area. All 49 occupants evacuated safely and the aircraft was damaged beyond repair.

The twin engine aircraft departed Taytay-Sandoval-Cesar Lim Rodriguez Airport on a charter flight to Manila, carrying one passenger and two pilots. While approaching Manila, the left engine failed. The crew informed ATC about his situation and continued the descent to Manila when, shortly later, the right engine lost power. Unable to maintain the assigned altitude, the crew attempted to ditch the aircraft in the bay of Manila, about 3 km offshore. The aircraft floated for few minutes, allowing all three occupants to evacuate the cabin. Few minutes later, the aircraft sank and all three occupants were rescued. The wreckage was not recovered.

Few minutes after takeoff from Cagayancillo Airport, the pilot reported engine problems and was cleared to return for an emergency landing. On final approach, the aircraft was not properly aligned so the captain increased engine power and initiated a go-around. The aircraft lost height and crashed in the sea about 2 km offshore. A passenger was rescued while 14 other occupants were killed, among them General Santiago Madrid, Chief of the southwestern military command.

The aircraft was being flown as a route check for for a captain. Another captain was acting as Pilot Monitoring on the flight. The en route part of the flight was uneventful. The aircraft was conducting an ILS approach to runway 05 and the controller reported that they would be behind Philippine Airlines flight 809, an Airbus A319. As the Boeing 737 broke out of clouds, the A319 was observed on runway 05. The Pilot Flying informed ATC of his intention to perform a 360° maneuver, but the Pilot Monitoring advised ATC of the opposite, stating that the aircraft would turn right instead of following the missed approach procedure, which called for a left hand turn to a 020° heading. The aircraft re-entered clouds and attempted to fly visually at a lower altitude in instrument conditions when in fact it should have climbed to 4,000 feet. The flight continued over Samal Island and the flight requested a VOR/DME approach and landing in the opposite direction (runway 23), which was approved by the controller. After having aligned with the runway heading, the aircraft descended below the normal glide path for this approach. It continued down to 570 feet at a point where the aircraft should have been at 1,500 feet. The aircraft crashed into a coconut plantation on a hillside in Barangay San Isidro, disintegrated and caught fire. All 131 occupants were killed.

The twin engine aircraft departed Manila-Ninoy Aquino Airport at 0834LT and was supposed to arrive at Cauayan Airport at 0940LT. At 0919LT, the crew reported his position 96 km from the destination. As he encountered favorable winds, the captain informed ATC about an ETA three minutes earlier at 0937LT. At 0930LT, while flying in clouds, the aircraft struck the slope of a mountain located near Kasibu, about 77 km southwest of Cauayan Airport. The aircraft was destroyed upon impact and all 17 occupants were killed.

The aircraft departed Shanghai-Hongqiao Airport at 2116LT on a cargo flight to Subic Bay with a load of electronics and garments. Weather conditions at Subic Bay Airport was at follow: scattered at 1,800 feet and 7,000 feet, light rain, wind calm and visibility six km. At 2315LT, the aircraft landed on runway 07 (2,400 metres long). Unable to stop within the remaining distance (the runway was wet), the aircraft overran and plunged in the Subic Bay. Both pilots were injured and the aircraft was totally destroyed.

The aircraft departed Lipa City Airport on a flight to Manila and should be delivered to Crown Cargo Express for several missions. On approach to Ninoy Aquino Airport, the crew informed ATC about engine problems. The captain attempted an emergency landing when the aircraft struck power cables and crashed in a rice paddy field located in Santa Rosa, about 25 km south of the airport. All nine occupants escaped uninjured while the aircraft was damaged beyond repair.

While descending to Mankayan Airport on a flight from Poro Point, the crew encountered poor weather conditions with rain falls and limited visibility. The crew just requested the last weather bulletin for Mankayan when the aircraft struck the slope of a mountain and crashed about 20 km from Mankayan. All eight occupants were killed.

Crashed in unknown circumstances in the sea off Coron. The pilot, sole on board, was killed.

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.