Crash of a Fairchild C-123B Provider at Santa Bernardina AFB: 17 killed

Date & Time: Apr 30, 1970 at 1230 LT
Type of aircraft:
Operator:
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Santa Bernardina - Santa Bernardina
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
13
Pax fatalities:
Other fatalities:
Total fatalities:
17
Circumstances:
The airplane arrived in the morning from Montevideo-Carrasco and its crew already completed several sortie in the morning. Around noon, 13 officers of the Uruguayan Army embarked the airplane and the crew was supposed to make a demonstration flight, proving the manoeuvrability of the airplane. While flying at low height, the airplane struck a tree and crashed in a huge explosion near the runway 27 threshold. A passenger was seriously injured (burned) while 16 other occupants were killed. Few hours later, the only survivor died from his injuries. Among the passengers was Col Américo Gonzalez, Chief of the Santa Bernardina Airbase.
Crew:
Maj William Kern, pilot,
Cpt Richard Morris, copilot,
S/Sgt José Rivera,
Sgt Alfred Ford.
Passengers:
Col Américo Gonzalez,
Maj Roberto Dego,
Maj Ibes Tinetti,
Cpt Heráclio Abelleira,
1st lt Manuel Villamil,
2nd Lt Rolando Paller,
2nd Lt Dámaso Sosa,
2nd Lt Mario Scarzella,
Ens Ricardo Rodríguez,
Ens Héctor Angellini,
Ens Rubén Spinelli,
Ens José Suárez,
Ens Rubén Feria.

Crash of a Britten-Norman BN-2A Islander in Rawalpindi

Date & Time: Apr 7, 1970
Type of aircraft:
Operator:
Registration:
G-AXRJ
Flight Type:
Survivors:
Yes
MSN:
123
YOM:
1970
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The crew was completing a demo flight on behalf of the British manufacturer Britten-Norman. On final approach, during the last segment, the twin engine aircraft hit an obstacle located near the runway threshold and crashed. Both crew members were injured and the aircraft was destroyed.

Crash of a Pilatus PC-6/C-H2 Turbo Porter in Asunción: 2 killed

Date & Time: May 8, 1969 at 1100 LT
Operator:
Registration:
N356F
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Asunción - Asunción
MSN:
2014
YOM:
1967
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
2
Circumstances:
While taking part to a military airshow, the aircraft was engaged in a demonstration flight at Asunción-Presidente Stroessner Airport. Shortly after liftoff, the single engine airplane deviated from the climb path then stalled and crashed in flames on the apron before colliding with a parked Lineas Aéreas Paraguayas Convair CV-240 registered ZP-CDN. The Porter was totally destroyed and two of its occupants, among them the pilot, were killed. The CV-240 was partially destroyed and later considered as damaged beyond repair.
Crew:
Ernesto Vicnoli, pilot. †
Passengers:
Gen Andrés Rodríguez y Adrián Jara,
Doctor Luis Migone, †
Lt Juan Félix León.

Crash of a Breguet Bre.1150 Atlantic in Farnborough: 6 killed

Date & Time: Sep 20, 1968 at 1513 LT
Type of aircraft:
Operator:
Registration:
43/F-XCVX
Flight Type:
Survivors:
No
Schedule:
Farnborough - Farnborough
MSN:
43
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Registered 43 (F-XCVX), the aircraft was engaged in a demo flight at the annual Farnborough Airshow and was carrying five officers of the flottille 22F based at Nîmes-Garons Naval Air Station, France. Following several circuits, the crew decided to make a new low pass in front of the spectators with the left engine shut down and its propeller feathered. On final, while at an altitude of 300 feet and a speed of 140 knots with the flaps down to 10°, the aircraft stalled and crashed in a huge explosion on a parking located few hundred yards short of runway. Upon impact, the empennage was torn off and crashed on the roof of the staff mess of the British Air Force Aeronautical Research Center. All five crew members were killed as well one man on the ground.
Crew:
Cpt Jean-Yves Saint-M'Leux,
OE1 G. Durand,
EV C. Lemaire,
QM R. Bequier,
S/Maj A. Goasguen.
Probable cause:
As a result of the undercarriage having been left extended, it is possible that the air speed at the time of unfeathering the port prop was less than normal, and less than intended by the pilot. This in itself would not have resulted in an accident. Possibly because of [a] control jam, the rudder deflection necessary at this speed to balance the asymmetric thrust of the starboard engine and the drag of the unfeathered port propeller, was not applied. This was the most important cause, and allowed yaw, sideslip and roll to develop to the extent that the pilot had inadequate control of the port turn which he had initiated. The aircraft’s height and speed were insufficient to permit recovery by a reduction of power on the starboard engine. Bank therefore increased beyond the point at which level flight could be sustained, and the aircraft stalled in the turn and crashed.

Crash of a Piaggio PD-808 in San Sebastian: 6 killed

Date & Time: Jun 18, 1968 at 1650 LT
Type of aircraft:
Operator:
Registration:
I-PIAI
Flight Type:
Survivors:
No
Site:
Schedule:
Madrid – San Sebastian
MSN:
503
YOM:
1968
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
5
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The airplane was engaged in a demonstration tour within Europe on behalf of the Italian manufacturer Piaggio. On approach to runway 22 in poor weather conditions, the pilot decided to make a go around and initiated a turn to the right when the airplane struck the slope of Mt Jaizkibel located 4 km west of the airport. The wreckage was found about 15 meters below the summit and all six occupants were killed, among them the Italian businessman Lino Zanussi.
Crew/passengers:
Lino Zanussi,
Alfio di Vora,
Giovanni Battista Talotti,
Diego Hurtado de Mendoza,
Sergio Milich,
Davide Albertazzi.
Probable cause:
It was determined that the pilot neglected the published go-around procedures at San Sebastian Airport while initiating a turn to the right as he must turn to the left. The lack of visibility due to poor weather conditions was considered as a contributing factor.

Crash of a Blackburn B-101 Beverley C.1 in Malaysia: 6 killed

Date & Time: Dec 15, 1967
Type of aircraft:
Operator:
Registration:
XL150
Flight Phase:
Flight Type:
Survivors:
No
Site:
MSN:
1036
YOM:
1957
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
The crew took part to a demonstration flight when he encountered poor weather conditions. While cruising at low height, the airplane struck the slope of a mountain located some 144 km north of Johor Bahru. The wreckage was found about 50 meters below the summit and all six crew members were killed.

Crash of a Cessna 421A Golden Eagle I in Findlay

Date & Time: Nov 3, 1967 at 2012 LT
Type of aircraft:
Operator:
Registration:
N4019L
Flight Type:
Survivors:
Yes
MSN:
421A-0019
YOM:
1967
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
21412
Captain / Total hours on type:
52.00
Circumstances:
The pilot was completing a local demonstration flight to potential customers. While on a night approach to Findley Airport, he failed to realize his altitude was insufficient when the airplane struck tree tops and crashed in a wooded area located few miles short of runway. The aircraft was destroyed and all three occupants were injured.
Probable cause:
Improper IFR operation on part of the pilot-in-command who misjudged altitude and misread instruments/altimeter settings.
Final Report:

Crash of a Fokker F27 Friendship 400 in Malaybalay: 19 killed

Date & Time: Apr 27, 1967 at 1710 LT
Type of aircraft:
Operator:
Registration:
PK-PFB
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Malaybalay - Malaybalay
MSN:
10306
YOM:
1966
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
16
Pax fatalities:
Other fatalities:
Total fatalities:
19
Captain / Total flying hours:
4365
Captain / Total hours on type:
2190.00
Aircraft flight hours:
441
Aircraft flight cycles:
337
Circumstances:
The aircraft was under a two week lease from the owner, the Permina Oil Company of Indonesia, to the Royal Netherlands Aircraft Factories - Fokker, for the purpose of a series of demonstration flights in the Philippines. It arrived at Manila on 24 April 1967 and conducted demonstration flights at various airports on 26 and 27 April 1967. On that day the aircraft took off from Mactan at 0816 hours and after having flown to ten different aerodromes it arrived at Davao at 1557 hours where the main fuel tanks and water/ methanol tanks were filled to capacity. At 1635 hours the aircraft took off from Davao and landed at Malaybalay Airport on runway 06 at 1705 hours. It continued its landing roll up to the end of the runway, made a 180° turn and then took off from runway 24. According to ground witnesses the take-off was initiated with both engines at maximum power and the aircraft became airborne at about two-thirds of the runway length. At that time the right hand propeller was starting to slow down and stopped when the aircraft reached a height of about 1 metre above the ground. The aircraft appeared to have difficulty in gaining height and followed a creek between two hills in a right wing low attitude. It struck a tree and some bamboos and crashed on a hill 45 m higher than the runway elevation. The site of the accident was located 1 380 m from the end of runway 04 and 136.5 m to the right of its extended centre line. The accident occurred at 1710 hours. All three crew members and 16 passengers were killed.
Probable cause:
The probable cause of the accident was poor judgement of the pilot in taking off towards the direction where the terrain was unsuitable for single engine performance. Also contributing to the accident were the following:
- The gross take-off weight was more than that allowed to clear the rising terrain along the flight path,
- Inadequate available data regarding Malaybalay Airport.
Final Report:

Crash of a Hawker-Siddeley HS.125-1 off Nice: 2 killed

Date & Time: Jun 5, 1966 at 1712 LT
Type of aircraft:
Operator:
Registration:
F-BKMF
Flight Type:
Survivors:
No
Schedule:
Cannes - Nice
MSN:
25007
YOM:
1964
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
4601
Captain / Total hours on type:
324.00
Copilot / Total flying hours:
2080
Copilot / Total hours on type:
50
Aircraft flight hours:
798
Circumstances:
The airplane departed Cannes at 1645LT bound for Nice and the crew was supposed to perform three low pass over the Airport of Nice-Côte d'Azur during a local Airshow. The first path was performed at low height over the runway. The crew then completed a turn to the right in an attempt to make a second low pass but on the opposite direction. Doing so, the airplane climbed to an altitude of 2,000 feet when control was lost. It went into a dive, caught fire in the air and crashed in flames into the sea some 1,5 km southwest of the airfield. The aircraft was destroyed and both pilots were killed.
Probable cause:
The stresses applied to the airframe of F-BKMF during the manoeuvre carried out in order to return to the Nice runway, exceeded the design limit loads of the wing unit. A rupture was then caused to the wing unit which resulted in the leakage of a large quantity of fuel from the upper surface near the wing root. The aircraft stalled under the high load factor and the pilot was unable to regain control because of the small height margin and the damage to the aircraft structure. In spite of the considerable stick forces which have to be applied in a normally trimmed aircraft in order to carry out such a manoeuvre, the latter may have been attempted by the pilot, who was experienced, skillful and cautious, in view of the following circumstances: "tight" manoeuvre at low altitude in poor visibility; air display atmosphere (type of flying pre-supposing special training different from the training normally required for a chief pilot of the Air Affaires company); possible anxiety to avoid crossing the flight paths of several aircraft in the vicinity during the display.
Final Report:

Crash of a Stinson V-77 Reliant in Boise: 2 killed

Date & Time: Oct 16, 1965 at 1745 LT
Type of aircraft:
Registration:
N60361
Flight Type:
Survivors:
No
Schedule:
Boise - Boise
MSN:
77-43
Location:
Crew on board:
1
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
5000
Captain / Total hours on type:
100.00
Circumstances:
On approach to Boise Airport, the pilot initiated a go-around procedure when the aircraft struck a dirt bank and crashed, bursting into flames. Both occupants, performing a demo flight, were killed.
Probable cause:
The pilot delayed in initiating go-around procedure and seat belt was not fastened.
Final Report: