Crash of a Martin P5M-2 Marlin off Sangley Point AFB: 10 killed

Date & Time: Jan 6, 1967
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Sangley Point - Sangley Point
Country:
Region:
Crew on board:
10
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
10
Circumstances:
The crew was completing a training mission when a rocket fixed to the bottom of the right wing exploded while being ignited in flight. Out of control, the Marlin crashed into the sea off Sangley Point AFB, killing all 10 crew members.

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 DC-3A in Legazpi: 2 killed

Date & Time: Dec 16, 1965 at 1722 LT
Type of aircraft:
Operator:
Registration:
PI-C856
Survivors:
Yes
Schedule:
Manila – Legazpi
Flight number:
AM101
Location:
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
18
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1957
Captain / Total hours on type:
1256.00
Copilot / Total flying hours:
2596
Copilot / Total hours on type:
709
Circumstances:
Flight AM101 was a scheduled domestic flight from Manila to Legaspi. It took off from Manila International Airport at 1505 hours. At 1640 hours it established initial contact with Legaspi Radio, reported 7 minutes north-west of the field and requested weather and landing information. Legaspi Radio transmitted the following information: 1600H surface wind 0400/8 kt, visibility 5 km clouds 6 oktas 450 metres, 8 oktas 2,100 metres; temperature 24°, dewpoint 24°, runway in use 06 QNH 29.81 inches. At 1707 hours the flight requested information regarding the traffic in the circuit and was informed that there was none. At 1715 hours the sound of an aircraft, presumably AM101, was heard south of the airport but the aircraft was hardly visible. At 1716 hours the flight inquired again about the present weather and the 1700 hours weather observation was passed to the aircraft. Subsequent inquiry about present visibility, wind direction and speed was made by the flight which was advised that the wind was 040 18 kt and the visibility approximately 4 km. At 1718 hours the flight was seen turning for a landing on Runway 24. The landing roll was described by witnesses as unusually fast after the aircraft made a two-wheel touchdown, tail wheel high approximately 300 m after the threshold of Runway 24. Before the tail wheel came into contact with the runway full power was applied and the aircraft was observed airborne. At approximately 200 ft altitude, it initiated a tight left turn, collided with the top of a tree and then hit a building located two miles southwest of Legaspi Airport. Both pilots were killed while all other occupants were injured.
Probable cause:
The Board determined that the probable cause of this accident was a power stall during a tight turn manoeuvre at too low an altitude from which successful recovery was impossible.
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:

Crash of a Douglas DC-3A-197 on Mt Kantakan: 10 killed

Date & Time: Sep 11, 1965 at 1625 LT
Type of aircraft:
Operator:
Registration:
PI-C942
Flight Phase:
Survivors:
No
Site:
Schedule:
Cebu City – Bacolod
MSN:
1926
YOM:
1937
Flight number:
FE060
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
7
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
2427
Captain / Total hours on type:
495.00
Copilot / Total flying hours:
1345
Copilot / Total hours on type:
715
Aircraft flight hours:
74853
Circumstances:
Flight 60 was a scheduled domestic flight from Lahug Airport, Cebu City, to Bacolod Airport, Negros Occidental. It departed Lahug Airport at 1519 hours on a VFR flight plan and six minutes later it made contact with Cebu Control Tower giving its ETA at Bacolod as 1555 hours. Nothing further was heard from the flight. The estimated time en route was 45 minutes. At 1700 hours the flight was declared in distress and a communication search was started. It was subsequently found that the flight had run into some tree tops on the side of Mt. Kanlaon and had crashed at Mt. Kantakan, La Carlota, Negros Occidental, at approximately 1625 hours. The wreckage was found a week later and all 10 occupants have been killed.
Probable cause:
The Board determined that the probable cause of this accident was an error of judgment on the part of the pilot to fly VFR into an instrument meteorological condition resulting in a collision with the terrain.
Final Report:

Crash of a Douglas C-47A near Libacao: 37 killed

Date & Time: Jul 25, 1965 at 0740 LT
Operator:
Registration:
777
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Nichols - San Jose Buenavista
MSN:
20243
YOM:
1944
Location:
Country:
Region:
Crew on board:
7
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
37
Circumstances:
The airplane departed Nichols AFB in the early morning, bound for San Jose Buenavista with 7 crew members and 30 passengers, among them civilians. While cruising at an altitude of 6,000 feet in poor weather conditions, the airplane struck the slope of Mt Madiac located 95 km northeast of San Jose Buenavista. SAR operations were conducted and the wreckage was found three days later in an isolated area, about 300 meters below the summit. The aircraft was destroyed and all 37 occupants have been killed. At the time of the accident, weather conditions were poor with low clouds and a visibility limited to few hundred meters. There were some gusty winds up to 40 knots at the time of the accident, which caused the aircraft to deviate from the prescribed route.
Probable cause:
Controlled flight into terrain.

Crash of a Douglas DC-6B in Cebu City

Date & Time: Jun 6, 1965
Type of aircraft:
Operator:
Registration:
PI-C950
Flight Phase:
Survivors:
Yes
MSN:
43820
YOM:
1952
Location:
Country:
Region:
Crew on board:
0
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll at Cebu Airport, one the undercarriage failed. The airplane sank on runway and slid for several yards before coming to rest. There were no casualties but the aircraft was written off.
Probable cause:
Undercarriage failure during takeoff.

Crash of a Douglas C-47 at Clark AFB: 5 killed

Date & Time: Mar 25, 1965
Operator:
Flight Type:
Survivors:
No
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
5
Circumstances:
On final approach to Clark AFB, the twin engine airplane collided with a USAF Rockwell T-39A Sabreliner registered 62-4458. The jet was carrying a crew of two who was completing a local training flight. Both airplane crash 1,5 km east of the airfield and all seven occupants on both aircraft were killed.

Crash of a Rockwell T-39A Sabreliner at Clark AFB: 2 killed

Date & Time: Mar 25, 1965
Type of aircraft:
Operator:
Registration:
62-4458
Flight Type:
Survivors:
No
Schedule:
Clark - Clark
MSN:
276-11
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
The crew was completing a local training flight at Clark AFB. On final approach, the Sabreliner collided with a USAF C-47 carrying a crew of five. Both airplane went out of control and crashed 1,5 km east of the airbase. All seven crew members on both aircraft were killed.

Crash of a Douglas DC-3A near Libmanan: 10 killed

Date & Time: Mar 8, 1965 at 1030 LT
Type of aircraft:
Operator:
Registration:
PI-C948
Survivors:
Yes
Site:
Schedule:
Manila – Naga
MSN:
4892
YOM:
1942
Flight number:
FE043
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
4454
Captain / Total hours on type:
3646.00
Copilot / Total flying hours:
1462
Copilot / Total hours on type:
761
Aircraft flight hours:
31929
Circumstances:
Flight 43 was a non-scheduled domestic flight from Manila International Airport to Naga-Pili Airport. It took off from Manila at 0943 hours, Philippine local time, on a DVFR flight plan at 7,500 ft. Estimated time en route was 1:10 hours. At 1010 hours the flight reported over Alabat at 5 500 ft, estimating arrival at Pili Airport at 1045 hours. No difficulties were reported by the crew. This was the first and last message from the flight. At 1515 hours a communication search was initiated. Alert phase and distress phase were respectively declared at 1350 and 1455 hours, then an aerial search was initiated which continued up to the receipt of the information from the two survivors that the aircraft had crashed and burned on the steep and thickly forested slope of Mt. Tangcong Vaca (height: 2,480 ft). The site of the accident was 19 NM north-west of Pili Airport, at approximately 1500 ft AMSL. The accident occurred at approximately 1030 hours.
Probable cause:
The probable cause of this accident was VFR flight into instrument meteorological conditions resulting in collision with the rising terrain.
Final Report: