Manila-Ninoy Aquino

The flight was bound for Manila with one pilot, one aircraft mechanic, and two passengers on board. The aircraft was reported missing after it took off from Bicol International Airport (RPLK) at Daraga, Albay. The aircraft is being operated by the Energy Development Corporation (EDC) and was on a routine general aviation flight. All aircraft occupants were fatally injured in this accident. The pilot submitted a VFR to IRF flight plan that will utilize standard departure on RWY 05 of RPLK. According to the flight plan, it will be transitioning to IFR and intercepting NAGA VOR. It will further continue W9 airway and proceed to ALABAT for the arrival procedure in Manila. The flight departed from RWY 05, made a procedural right upwind turn, and crossed the final approach of RWY 05. At 0647LT, ATC established contact with the aircraft while passing 2,600 ft. The ATC inquired if the flight had already passed Camalig by-pass, and the pilot responded "We're passing Camalig by-pass now". The pilot was instructed by ATC to continue climbing and report twenty nautical miles out of RPLK, which was acknowledged by the pilot. At 0650LT, no position report was received from the aircraft. The ATC initiated contact with the aircraft several times, but no response was received. The duty ATC contacted the Manila Area Control Center (MACC) for any signatures of the aircraft that they might have picked up. The MACC informed the ATC that there was an initial signature contact that later disappeared on the radar monitor. At about 0900LT, the Philippine Aeronautical Rescue Coordinating Center (PARCC) elevated the alert to a DETRESFA on the missing aircraft. On the next day, February 19, 2023, the operator launched their own search operation using an AW139 helicopter, which was able to locate the missing aircraft at about 6,300 feet on the south-west slope of Mt Mayon Volcano with grid coordinates of 13°14'56.45 N and 123°40'57.79 E. An aerial reconnaissance by CAAP-AAIIB investigators and EDC using a helicopter was conducted on 20 February 2023. The general impact area shows the scattered wreckage of aircraft debris and signs of post-impact fire. All four occupants were killed.

An IAI Westwind II 1124A type of aircraft with registry number RP-C5880, was destroyed following a runway excursion while taking-off at RWY 06, Ninoy Aquino International Airport (NAIA), Manila Philippines. All eight (8) occupants (six (6) Filipino, one (1) Canadian and one (1) American citizen are fatally injured. The aircraft is being operated by Lionair Inc. and was bound for Haneda, Japan on a medical evacuation flight. While the aircraft was on take-off roll before reaching taxiway R2, sparks were noted at the runway, it continued until the aircraft came to complete stop and engulfed by fire. Chunks of rubber and metal debris were present on the runway. Scrape marks coming from the right hand (RH) wheel hub were also visible. Tire marks followed by scrape marks on the runway coming from the LH tire and wheel hub were also seen after taxiway H1 intersection. Large portion of the remaining LH tire was recovered from the grassy portion near taxiway H1. After exiting from the asphalted portion of runway safety area, the aircraft initially run over two (2) runway edge lights then impacted into a concrete electric junction box and came to a complete stop at the runway secondary fence. The aircraft settled almost 172 meters away from the end of RWY 06, in an upright position at 14°30'53.50"N; 121°1'48.48"E and heading of 170 degrees. The flight was on Instrument Flight Rules (IFR) condition. A Notice to Airmen (NOTAM) of NAIA RWY 06/24 closure for aircraft operation was declared at 2000H and opened for operation at 0420H, March 30, 2020.

The airplane encountered a loss of control in flight while approaching Manila and crashed into a private resort located in Barangay Pansol, Calamba, Laguna, Philippines. It lost radar contact with Manila Approach after being cleared to descent from 9,000 feet for 5,000 feet tracking-in radial 170, 25 DME to Ninoy Aquino International Airport (RPLL). The aircraft wreckage was found in a private resort with coordinates of 14°10’33.62” N and 121°11’34” E and heading approximately 228° with most its fuselage totally burned. All the nine (9) occupants were fatally injured and two (2) other persons on the ground sustained serious injuries. The aircraft took off from Dipolog Principal Airport (RPMG), Dipolog City, Zamboanga del Norte bound for Manila (RPLL) on a MEDEVAC flight. Instrument Metrological Condition (lMC) prevailed at the time of the accident.

On August 16, 2018, about 1555UTC/2355H local time, a Boeing 737-800 type of aircraft with Registry No. B-5498 operating as flight CXA 8667 sustained substantial damage following a runway excursion after second approach while landing on Runway 24 of Ninoy Aquino International Airport (NAIA), Manila, Philippines. The flight was a scheduled commercial passenger from Xiamen, China and operated by Xiamen Airlines. The one hundred fifty-seven (157) passengers and two (2) pilots together with the five (5) cabin crew and one air security officer did not sustain any injuries while the aircraft was substantially damaged. An instrument flight rules flight plan was filed. Instrument Meteorological Conditions (IMC) prevailed at the time of the accident. During the first approach, the Captain who was the pilot flying aborted the landing at 30 feet Radio Altitude (RA) due to insufficient visual reference. A second approach was considered and carried out after briefing the First Officer (FO) of the possibility of another aborted landing should the flight encounter similar conditions. The briefing included a diversion to their planned alternate airfield. The flight was “stabilized” on the second approach with flaps set at 30 degrees landing position, all landing gears extended and speed brake lever appropriately set in the ARM position. On passing 1,002 feet Radio Altitude (RA), the autopilot was disengaged; followed by the disengagement of the auto-throttle, three (3) seconds later. The ILS localizer lateral path and Glide slope vertical path were accurately tracked and no deviations were recorded. The “reference” landing speed for flaps 30 for the expected aircraft gross weight at the time of landing was 145 knots and a target speed of 150 knots was set on the Mode Control Panel (MCP). The vertical descent rate recorded during the approach was commensurate with the recommended descent rate for the profile angle and ground speed; and was maintained throughout the approach passing through the Decision Altitude (DA) of 375 feet down to 50 feet radio altitude (RA). As the aircraft passed over the threshold, the localizer deviation was established around zero dot but indicated the airplane began to drift to the left of the centerline followed by the First Officer (FO) making a call out of “Go-Around” but was answered by the Captain “No”. The throttle levers for both engines were started to be reduced to idle position at 30 feet RA and became fully idle while passing five (5) feet RA. At this point, the aircraft was in de-crab position prior to flare. At 13 feet RA, the aircraft was rolling left and continuously drifting left of the runway center line. At 10 feet RA another call for go-around was made by the FO but was again answered by the Captain with “No” and “It’s Okay”. At this point, computed airspeed was approximately 6 knots above MCP selected speed and RA was approaching zero feet. Just prior to touchdown, computed airspeed decreased by 4 knots and the airplane touched down at 151 knots (VREF+6). The wind was recorded at 274.7 degrees at 8.5 knots. Data from the aircraft’s flight data recorder showed that the aircraft touched down almost on both main gears, to the left of the runway centerline, about 741 meters from the threshold of runway 24. Deployment of the speed brakes was recorded and auto brakes engagement was also recorded. The auto brakes subsequently disengaged but the cause was undetermined. Upon touchdown, the aircraft continued on its left-wards trajectory while the aircraft heading was held almost constant at 241 degrees. After the aircraft departed the left edge of the runway, all landing gears collided with several concrete electric junction boxes that were erected parallel outside the confines of the runway pavement. The aircraft was travelling at about 147 knots as it exited the paved surface of the runway and came to rest at approximately 1,500 meters from the threshold of Runway 24, with a geographical position of 14°30’23.7” N; 121°0’59.1” E and a heading of 120 degrees. Throughout the above sequence of events from touchdown until the aircraft came to a full stop, the CVR recorded 2 more calls of “GO-AROUND” made by the FO. Throughout the landing sequence, the thrust reversers for both engines were not deployed. Throttle Lever Position (TLP) were recorded and there was no evidence of reverse thrust being selected or deployment of reversers. After the aircraft came to a complete stop, the pilots carried out all memory items and the refence items in the evacuation non-normal checklist, which includes extending the flaps to a 40 degrees position. The aircraft suffered total loss of communication and a failure in passenger address system possibly due to the damage caused by the nose gear collapsing rearwards and damaging the equipment in the E/E compartment or the E-buss wires connecting the Very High Frequency (VHF) 1 radio directly to the battery was broken. The Captain then directed the FO to go out of the cockpit to announce the emergency evacuation. The cabin crew started the evacuation of the passengers utilizing the emergency slides of the left and right forward doors. There were no reported injuries sustained by the passengers, cabin crew, flight crew or the security officer.

On or about 1000H January 17, 2015, the Holy Father “Pope Francis” visited the typhoon-devastated province of Leyte and utilized an Airbus 320 aircraft for Tacloban airport, and Bombardier Global 5000 RP-C9363 aircraft was part of the Papal entourage with passengers on board. The weather condition was worsening and the visit of the Pope had to cut short due to approaching tropical storm code named “AMANG”, with strong winds of up to 130km/h(80mph) according to PAGASA and moderate rain as signal n°2 was already forecasted at the province of Leyte. At 1304H, the Global 5000 RP-C9363 was given start up clearance by tower controller and subsequently a taxi clearance at 1308H to exit via south taxiway next to the departing Airbus320 PAL8010. At 1306H, the First Airbus 320 PAL8010 aircraft carrying the Papal entourage took-off utilizing RWY 36 with prevailing wind condition of 290̊/18 knots crosswind and temperature of 24°. At 1311H, RP-C 9363 was not allowed to move from present position to proceed to the active runway via south taxiway by the military ground marshaller. At 1322H, the 2nd Airbus 320 PAL8191 took-off with prevailing wind conditions of 290°/23 kts crosswind. The separation time between the Global 5000 to the first and second aircraft were 29 minutes and 13 minutes respectively. At 1335H, finally RP-C9363 Global 5000 was cleared for take-off at runway 36 bound for Ninoy Aquino International Airport (RPLL) with two (2) pilots and 14 passengers on board. The wind condition at that time was 300°/18 kts with gustiness and temperature of 24°. The aircrew performed rolling take-off and the acceleration was normal, the pilot nonflying (NPF) called for air speed alive, 80 knots, V1 and Rotate. Before approaching south taxiway abeam the terminal building, the aircraft started to veer to the left side of the runway centerline. The aircraft continued to roll veering to the left side of the runway and the left hand main landing gear was already out of the runway after the north taxiway. The aircraft underwent runway excursion and sustained substantial damage after simultaneous collision with the concrete bases of runway edge lights and to the concrete culvert before it came to a complete stop at approximately 1500 meters from the take-off point. Immediate evacuation was performed to all passengers. The crash and fire rescue personnel arrived at the area and assisted the passengers and aircrew.

The aircraft was performing a charter flight from Manila to Balesin, carrying tourists en route to the Balesin Island Club. The approach and landing were completed in poor weather conditions with heavy rain falls. After landing, the four engine aircraft was unable to stop within the remaining distance. It overran, lost its nose gear and came to rest in the Lamon Bay, few dozen metres offshore. All 75 occupants escaped uninjured while the aircraft was damaged beyond repair.

On December 10, 2011, BE-65-80QA (Queen Air) with Registry RP-C824 took off from RWY 13, Manila Domestic Airport on/or about 0610 UTC (1410H) southbound for San Jose, Mindoro. There were three (3) persons on board, the PIC and two (2) other persons; one was seated at the right-hand cockpit seat and the other one at the passenger seat. After airborne, the ATC gave instructions to the pilot o turn right and report five (5) miles out. After performing the right turn, the pilot requested for a reland which was duly acknowledged but the ATC with instructions to cross behind traffic on short final Rwy 06 (a perpendicular international runway) and to confirm if experiencing difficulty. However, there was no more response from the pilot. From a level flight southward at about 200 feet AGL, three (3) loud sputtering/burst sounds coming from the aircraft were heard (by people on the ground) then the aircraft was observed making a left turn that progressed into a steep bank and roll-over on a dive. After about one complete roll on a dive the aircraft hit ground at point of impact (Coordinates 14.48848 N 121.025811 E), a confined area beside a creek surrounded by shaties where several people were in a huddle. Upon impact, the aircraft exploded and fire immediately spread to surrounding shanties and a nearby elementary school building. The aircraft was almost burned into ashes and several shanties were severely burned by post-crash fire. A total of thirteen (13) persons were fatality injured composed of: the 3 aircraft occupants who died due to non survivable impact and charred by post-crash fire, and ten (10) other persons on the ground, all residents at vicinity of impact point, incurred non-fatal injuries and were rushed to a nearby hospital for medical treatment. About 20 houses near the impact point were completely burnt and the adjacent Elementary School building was severely affected by fire.

Cebu Pacific Air flight 5J509, an ATR 72-500, took off from Tuguegarao Airport, Philippines, bound for Manila-Ninoy Aquino International Airport. The first officer was the Pilot Flying (PF) while the captain was the Pilot Not Flying (PNF). Approaching Manila, the flight was under radar vector for a VOR/DME approach to runway 24. At 7 miles on finals the approach was stabilized. A sudden tailwind was experienced by the crew at 500 feet radio altitude (RA) which resulted in an increase in airspeed and vertical speed. The captain took over the controls and continued the approach. Suddenly, the visibility went to zero and consequently the aircraft experienced a bounced landing three times, before a go-around was initiated. During climb out the crew noticed cockpit instruments were affected including both transponders and landing gears. They requested for a priority landing and were vectored and cleared to land on runway 13. After landing the aircraft was taxied to F4 where normal deplaning was carried out. No injuries were reported on the crew and passengers.

On October 17, 2009at about 12:04 pm, RP-C550 a DC-3type of aircraft took off from Manila Domestic airport bound for Puerto Princesa, Palawan. Approximately 5 mins after airborne, the Pilot-in-Command (PIC) informed Manila Tower that they were turning back due to technical problem. The PIC was asked by the air controller whether he was declaring an “emergency” and the response was negative. The PIC was directed to proceed South Mall and wait for further instruction (a standard procedures for VFR arrivals for runway 13). At South Mall, RP-C550 was cleared to cross the end of runway 06, still without declaring an emergency. The tower controller sensed that something was wrong with the aircraft due to its very low altitude, immediately granted clearance to land runway 06. However, the aircraft was not able to make it to runway 06. At about 12:14, RP-C550 crashed at an abandoned warehouse in Villa Fidela Subd., Brgy. Elias Aldana Las Piñas City about 4 kms. from the threshold of runway 06. As a result, the aircraft was totally destroyed and all aboard suffered fatal injuries due to impact and post crash fire.

Following an uneventful flight from Manila, the crew started the descent to Caticlan Airport and was informed that runway 06 was in use due to the wind component. For unknown reasons, the captain decided to land on runway 24. The approach was too long and the aircraft landed too far down the runway, about 950 metres past the runway threshold. Unable to stop within the remaining distance, it overran and came to rest in a grassy area against the perimeter fence. All 59 occupants escaped uninjured while the aircraft was damaged beyond repair.