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Crash of an Avro 748-226-2 in Manila: 33 killed

Date & Time: Feb 3, 1975 at 2310 LT
Type of aircraft:
Operator:
Registration:
RP-C1028
Flight Phase:
Survivors:
Yes
Schedule:
Manila - Iligan
MSN:
1590
YOM:
1966
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
29
Pax fatalities:
Other fatalities:
Total fatalities:
33
Circumstances:
Shortly after takeoff from runway 30, while in initial climb, the crew informed ATC about the failure of the right engine and was cleared to return for an emergency landing. The pilot-in-command initiated a turn to join the runway 06 approach path when the airplane stalled and crashed in flames in a rice paddy field located 4,8 km from the airport. A passenger was seriously injured while 32 other occupants were killed. Few hours later, the only survivor died from his injuries.
Probable cause:
Failure of the right engine during initial climb after three blades located on the high pressure turbine broke away, probably due to the presence of fatigue cracks.

Crash of an Avro 748-2-232 in Bislig

Date & Time: Nov 28, 1972 at 0913 LT
Type of aircraft:
Operator:
Registration:
PI-C1027
Survivors:
Yes
Schedule:
Surigao - Bislig
MSN:
1609
YOM:
1966
Flight number:
PR463
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
24
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
For unknown reason, the twin engine airplane landed hard on runway 23. It bounced twice when the nose gear collapsed. Out of control, the airplane veered off runway to the left then came to rest. While all 28 occupants escaped uninjured, the aircraft was damaged beyond repair.

Crash of a Fokker F27 Friendship 200 in Dumaguete City

Date & Time: Jul 1, 1970
Type of aircraft:
Operator:
Registration:
PI-C504
Survivors:
Yes
MSN:
10209
YOM:
1962
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
19791
Aircraft flight cycles:
15966
Circumstances:
After touchdown, the airplane was unable to stop within the remaining distance. It overran, lost its undercarriage and came to rest with its right wing partially torn off. All 29 occupants escaped uninjured while the aircraft was damaged beyond repair.

Crash of a Fokker F27 Friendship 100 in Iligan: 1 killed

Date & Time: May 9, 1970
Type of aircraft:
Operator:
Registration:
PI-C532
Flight Phase:
Survivors:
Yes
Schedule:
Iligan - Manila
MSN:
10311
YOM:
1966
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
29
Pax fatalities:
Other fatalities:
Total fatalities:
1
Aircraft flight hours:
9646
Aircraft flight cycles:
9049
Circumstances:
The takeoff procedure from Iligan-Maria Christina Airport was attempted by zero visibility due to foggy conditions. For unknown reasons, the airplane was unable to rotate, overran and crashed on sandpile and rockspile. The copilot was killed while several passengers were injured. The aircraft was destroyed.

Crash of an Avro 748-2-209 in Cabanatuan: 36 killed

Date & Time: Apr 21, 1970 at 1130 LT
Type of aircraft:
Operator:
Registration:
PI-C1022
Flight Phase:
Survivors:
No
Schedule:
Cauayan - Manila
MSN:
1643
YOM:
1968
Flight number:
PR215
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
36
Circumstances:
While cruising at an altitude of 10,500 feet, the airplane suffered an explosion. It went out of control, entered a dive and crashed in a field located near Cabanatuan. All 36 occupants have been killed.
Probable cause:
It was determined that an explosion occurred in the rear lavatory during flight. The exact cause of the explosion could not be established.

Crash of a BAc 111-402AP in Manila: 45 killed

Date & Time: Sep 12, 1969
Type of aircraft:
Operator:
Registration:
PI-C1131
Survivors:
Yes
Schedule:
Cebu City - Manila
MSN:
92
YOM:
1966
Flight number:
PR158
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
42
Pax fatalities:
Other fatalities:
Total fatalities:
45
Aircraft flight hours:
7208
Aircraft flight cycles:
6445
Circumstances:
On final approach to Manila Intl Airport, the crew failed to realize his altitude was too low when the airplane struck the ground and crashed in flames some 22 km from the runway 24 threshold. A crew member (steward) and a passenger were rescued while 45 other occupants were killed.

Crash of a Fokker F27 Friendship 100 on Mt Kanlaon: 21 killed

Date & Time: Jul 6, 1967 at 1843 LT
Type of aircraft:
Operator:
Registration:
PI-C527
Flight Phase:
Survivors:
No
Site:
Schedule:
Bacolod - Mactan
MSN:
10285
YOM:
1965
Flight number:
PR385
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
17
Pax fatalities:
Other fatalities:
Total fatalities:
21
Aircraft flight hours:
4228
Aircraft flight cycles:
3684
Circumstances:
The crew departed Bacolod Airport at 1833LT on a flight to Mactan. About ten minutes later, while cruising in poor weather conditions, the airplane struck the slope of Mt Kanlaon located 34 km southeast of Bacolod Airport. The wreckage was found few hours later and all 21 occupants were killed. The crew was flying under VFR mode in IMC conditions when the accident occured.
Probable cause:
It was determined that the crew decided to start the flight under VFR mode while weather conditions were poor with low clouds, necessitating a flight under instruments.

Crash of a Fokker F27 Friendship 100 in Mactan: 12 killed

Date & Time: Feb 28, 1967 at 1918 LT
Type of aircraft:
Operator:
Registration:
PI-C501
Survivors:
Yes
Schedule:
Manila - Mactan
MSN:
10147
YOM:
1960
Flight number:
PR345
Location:
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
15
Pax fatalities:
Other fatalities:
Total fatalities:
12
Captain / Total flying hours:
8000
Captain / Total hours on type:
1180.00
Copilot / Total flying hours:
1758
Copilot / Total hours on type:
1116
Aircraft flight hours:
15956
Aircraft flight cycles:
10195
Circumstances:
Flight 345 was a scheduled domestic flight from Manila to Mactan. It departed Manila at 1720 hours on an IFR clearance direct to Mactan, via Amber 1 at flight level 130. At 1908 hours the flight reported to Mactan Control Approach that it was descending through FL 70. It was cleared to FL 50, given an altimeter setting of 29.81 in Hg and requested to report at FL 60. At 1909 hours the flight requested a visual descent from FL 50 to 30 and at 1913 hours it reported commencing a VOR approach to runway 04. At 1917 hours the flight reported on final and Mactan Approach cleared the flight to land, giving the wind as 330'15 kt. The flight acknowledged the clearance and this was the last communication from the aircraft. Whilst on a long final approach commenced from a height of 1 500 feet approximately 4 miles from the runway threshold, the aircraft suddenly assumed a nose-high attitude and additional power was applied. A crew member then came out of the cockpit and spoke in the direction of a number of supernumerary crew travelling in the passenger compartment instructing them to move forward. Moments later a flight attendant came from the cockpit and instructed everybody to move forward. Before all the passengers could comply, the air- craft started banking alternately to the right and left, descending in a tail low attitude and crashed at approximately 1918 hours 0.9 miles before the threshold of runway 04. At 1919 hours the aerodrome controller observed a fire near-the approach end of runway 04 and alerted the emergency services. All four crew members and eight passengers were killed, seven others survived.
Probable cause:
The Board determined that the probable cause of the accident was a loss of control at a low altitude. The contributory factor was the distribution of load which placed the centre of gravity aft of the rear centre of gravity limit. The following finsings were reported:
- No evidence of malfunction or failure of the aircraft or its engines prior to impact was found. Evidence revealed that the aircraft struck the ground in a left wing low attitude with the landing gear extended and the flaps retracted. The elevator trim tab was found in a full nose-down position,
- The aircraft was loaded in such a way that the centre of gravity was located beyond the aft limit.
Final Report:

Crash of a Douglas C-47A-90-DL near Sablayan: 26 killed

Date & Time: Jun 29, 1966 at 1217 LT
Operator:
Registration:
PI-C17
Flight Phase:
Survivors:
Yes
Site:
Schedule:
Manila – Mamburao – San Jose
MSN:
20573
YOM:
1944
Flight number:
PR785
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
24
Pax fatalities:
Other fatalities:
Total fatalities:
26
Captain / Total flying hours:
4240
Captain / Total hours on type:
244.00
Copilot / Total flying hours:
1777
Copilot / Total hours on type:
396
Circumstances:
Flight 785 was a scheduled domestic VFR flight from Manila to San Jose with an intermediate stop at Mamburao. The aircraft departed Manila at 1030 hours local time and arrived at Mamburao after an uneventful flight. It then took off from Mamburao at 1204 hours. At 1215 hours, the flight requested terminal weather information from San Jose Radio Station. The requested information was transmitted but was not acknowledged. A witness stated that at approximately that same time he had observed an aircraft flying at very low altitude towards the mountain on a heading of approximately 065° and that, soon after, the aircraft disappeared from sight, he heard a loud explosion coming from the mountains east of his position. Subsequent efforts of San Jose Radio Station to contact the flight on both VHF and HF frequencies proved unsuccessful. In the afternoon of 1 July 1966 the wreckage of the aircraft was found at 2,300 feet AMSL in a ravine at the northern slope of Mt Rabangan (altitude 3,500 feet) which is approximately midway between Mamburao and San Jos6 and approximately 10 nautical miles inland. Two passengers were seriously injured while 26 other occupants were killed.
Probable cause:
The Board determined that the probable cause of the accident was misjudgement of the terrain clearance which resulted in the collision with trees. The instrument meteorological conditions en-route accompanied by severe turbulence and strong gusty winds over the crash site were a contributory factor. The weather and the sky condition at the time the airplane as seen over Sablayan was described as low thick dark clouds with strong wind and heavy rain. The actual weather in the vicinity of the crash site was substantially similar to the weather forecast that was conveyed to the pilot by the dispatcher during the weather briefing prior to the flight. Thirteen minutes after take-off the pilot encountered instrument meteorological conditions en-route under a VFR flight clearance.
Final Report:

Crash of a Douglas C-47A-25-DK in Manila: 1 killed

Date & Time: Oct 20, 1965 at 1033 LT
Operator:
Registration:
PI-C144
Flight Phase:
Survivors:
Yes
Schedule:
Manila – Legaspi – Calbayog – Tacloban
MSN:
13403
YOM:
1944
Flight number:
PR741
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
34
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
5146
Copilot / Total flying hours:
2843
Copilot / Total hours on type:
420
Aircraft flight hours:
28139
Circumstances:
Flight 741 was a scheduled domestic flight from Manila to Tacloban with stopovers at Legaspi and Calbayog. The aircraft took off from runway 13 at Manila at 1032 hours Philippines local time with the co-pilot flying the aircraft from the right hand seat. When airborne he ordered the pilot-in-command to raise the landing gear. After having done so the pilot-in-command noticed that the aircraft was veering slightly to the left although the indications of the engine instruments were normal. The co-pilot stated that the right rudder seemed to be jammed. The pilot-in-command then took over the controls. At this time the aircraft was continuously and gradually turning and banking to the left. The pilot-in-command then ordered the co-pilot to check the engine instruments again, and their indications were found to be normal. Both engines were at MET0 power setting and the airspeed was 110 mph. When the aircraft reached 150 ft above the ground, at a heading of 050° and an airspeed of 85 to 90 mph, the left bank and turn were momentarily checked and the right rudder pedal was then forward. The co-pilot attempted to call the control tower, but the transmission was garbled. The aircraft then went back to its left bank attitude in spite of the effort of the pilot-in-command to control the turn. When he noticed that the airspeed had dropped to between 85 to 90 mph he pushed the control yoke to gain airspeed but there was no reaction. At this time the pilot-in- command felt that the left wing had hit something. He tried in vain to control and keep the aircraft in the air. The plane crashed on barracks. A passenger was killed while 10 other people were injured, among them five people on the ground. All other occupants were unhurt.
Probable cause:
The Board determined that the probable cause of this accident was the failure of the pilot to set the rudder trim tab to the proper position before take-off and during the flight. The continuous left turn and bank of the aircraft which resulted in this accident was due to the undetected deflection of the rudder trim tab. The Board further determined that the overload of 68 lb over and above the allowable take-off gross weight of 26 900 lb at Manila was a contributory factor to this accident.
Final Report: