Crash of a Casa-Nurtanio CN235-100M (IPTN) near Akçadağ: 34 killed

Date & Time: May 16, 2001 at 1315 LT
Operator:
Registration:
086
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Diyarbakir – Ankara
MSN:
C-086
YOM:
1995
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
28
Pax fatalities:
Other fatalities:
Total fatalities:
34
Circumstances:
The airplane departed Diyarbakir Airport at 1250LT on a flight to Ankara, carrying 28 passengers and six crew members on behalf of the 2nd Tactical Aerial Force. About 25 minutes into the flight, while cruising in poor weather conditions, the crew declared an emergency and elected to divert to Malatya-Erhaç Airport. Shortly later, the airplane entered an uncontrolled descent, rolled to the left, completed three successive barrels then crashed in an apricot tree plantation located near Akçadağ. The airplane was totally destroyed and all 34 occupants were killed. The loss of control occurred in poor weather conditions (rain and hail) while the airplane was cruising at an altitude of 17,000 feet and at a speed of 444 km/h.
Crew:
Maj Lütfü Ceylan, pilot,
Lt Murat Erdeveci, pilot,
Lt Yılmaz Tekgül, pilot,
Cpt Hakan Bizrelli,
Lt Mahir Turan, pilot,
Yilmaz Gulhan.
Passengers:
Lt Levent Sahin,
Halil Helvacioğlu,
Ümit Basaran,
Nadir Turkmène,
Mikail Altıntas,
Hasan Ersoy,
Turan Kalin,
Zeki Çınar,
Sudi Doruk,
Mehmet Özden,
Ebubekir Çakıcı,
S/Sgt Yılmaz Aydın,
S/Sgt Mahmut Öner,
Zahit Çelik,
Garçon Saadetin,
Sgt Tuncay Urhan,
Sgt Ferhat Öztürk,
Sgt Ersin Bartan,
Sgt Bulent Haluk Demir,
Sgt Isa Turkmène,
Pvt Halit Güney,
Pvt Erdal Şimşek,
Pvt Aydın Uçar,
Pvt Mutlu Kaymakçı,
Pvt Mehmet Ali Karabudak,
Nedim Akyol,
Şefik Ayaydın,
Pvt Atakan Caran.

Crash of an Avro RJ70 in Siirt

Date & Time: Apr 22, 2000 at 1405 LT
Type of aircraft:
Operator:
Registration:
TC-THL
Survivors:
Yes
Schedule:
Ankara – Siirt
MSN:
E1249
YOM:
1996
Flight number:
TK774
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
42
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
7200
Aircraft flight cycles:
6200
Circumstances:
Following an uneventful flight from Ankara, the aircraft landed at Siirt Airport runway 24/06 which is 1,660 metres long. After touchdown on a wet runway, the aircraft was unable to stop within the remaining distance, overran and came to rest few dozen metres further. All 46 occupants evacuated safely while the aircraft was damaged beyond repair. All conditions were not met for a safe landing and the braking action was moderate to poor. Aquaplaning was suspected.

Crash of a Beechcraft C90 King Air in Bursa: 1 killed

Date & Time: Mar 21, 2000
Type of aircraft:
Operator:
Registration:
TC-LMK
Survivors:
Yes
Schedule:
Ankara - Bursa
MSN:
LJ-1080
YOM:
1984
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
4
Pax fatalities:
Other fatalities:
Total fatalities:
1
Circumstances:
On final approach to Bursa-Yenisehir Airport, the pilot encountered poor weather conditions. Due to low visibility, he was unable to establish a visual contact with the approach and runway lights and initiated a go-around procedure. While completing a circuit, the twin engine aircraft struck the top of a hill located near the airport and crashed. A passenger was killed while four other occupants were injured.

Crash of a Beechcraft 200 Super King Air in Ankara: 6 killed

Date & Time: Feb 17, 1993 at 1222 LT
Operator:
Registration:
10011
Flight Phase:
Flight Type:
Survivors:
No
Site:
Schedule:
Güvercinlik - Diyarbakir
MSN:
BB-1411
YOM:
1991
Country:
Region:
Crew on board:
2
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
6
Circumstances:
Shortly after takeoff from Güvercinlik AFB, while climbing in poor weather conditions, the crew reported engines problems and severe vibrations. He was cleared to divert to Ankara-Esenboğa Airport when the aircraft lost height and crashed on the parking of a post office located in the district of Yenimahalle in Ankara. The aircraft disintegrated on impact and all five occupants were killed as well as one people on the ground, among them General Eşref Turgut Bitlis, Chief of the Turkish Police. At the time of the accident, visibility was limited to 1,500 metres due to snow falls with an OAT of -4° C.
Crew:
Yaşar Erian, pilot,
Yüzbaşı Tuğrul Sezginler, pilot.
Passengers:
Gen Eşref Turgut Bitlis,
Col Fahir Işık,
Sgt-Maj Emin Öner.

Crash of a Fokker F28 Fellowship 1000 near Ankara: 41 killed

Date & Time: Dec 23, 1979
Type of aircraft:
Operator:
Registration:
TC-JAT
Survivors:
Yes
Site:
Schedule:
Samsun - Ankara
MSN:
11071
YOM:
1973
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
41
Pax fatalities:
Other fatalities:
Total fatalities:
41
Aircraft flight hours:
12245
Aircraft flight cycles:
13763
Circumstances:
The crew encountered poor weather conditions and limited visibility due to fog while approaching Ankara-Esenboğa Airport. For unknown reasons, the airplane deviated from the approach path when it struck the slope of Mt Cubuk located about 32 km north from the airport. A crew member and three passengers were seriously injured while 41 other occupants were killed.
Probable cause:
The crew deviated from the approach course for unknown reasons.

Crash of a Douglas DC-10-30CF in Istanbul

Date & Time: Jan 2, 1976 at 0636 LT
Type of aircraft:
Operator:
Registration:
N1031F
Survivors:
Yes
Schedule:
Jeddah - Ankara
MSN:
46825
YOM:
1973
Flight number:
SV5130
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
364
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
9848
Circumstances:
Leased by Saudi Arabian Airlines, the aircraft was completing a charter flight (hajj flight) from Jeddah to Ankara. En route, the crew was informed about poor weather conditions in Ankara (limited visibility due to foggy conditions) and was instructed to divert to Istanbul-Yeşilköy Airport. On approach to runway 24, the copilot informed the captain that one of the VASI's light was red and that their altitude was insufficient. The captain increased engine power but the aircraft continued to descent until it struck the ground eight meters short of the concrete runway. On impact, the left engine (n°1) was torn off and both left main gear and central gear were also torn off when the airplane struck the shoulder of the first runway's concrete block. The aircraft slid on its belly for few hundred meters, veered to the left and came to rest in flames in a grassy area. All 376 occupants were quickly evacuated, among them 10 were slightly injured. The aircraft was damaged beyond repair.
Probable cause:
The crew reported the runway in sight while passing the local NDB about 600 feet below the published minimums. The descent was completed below the glide slope. There were strong evidences that the first officer's altitude callouts were from the radio-altimeter, which was considered as a contributing factor.
Final Report:

Crash of a Douglas DC-7B in Munich

Date & Time: Jan 20, 1968
Type of aircraft:
Operator:
Registration:
SE-ERC
Survivors:
Yes
Schedule:
Ankara - Munich
MSN:
45088/723
YOM:
1956
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
32
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
Upon landing at Munich-Riem Airport, the nose gear collapsed. The airplane slid for several yards before coming to rest. None of the 36 occupants was injured while the aircraft was considered as damaged beyond repair.
Probable cause:
Nose gear collapsed on landing.

Crash of a Douglas C-47A-80-DL in Ankara: 52 killed

Date & Time: Feb 1, 1963 at 1513 LT
Operator:
Registration:
CBK-28
Flight Type:
Survivors:
No
Site:
Schedule:
Ankara - Ankara
MSN:
19668
YOM:
1944
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
52
Captain / Total hours on type:
1452.00
Copilot / Total hours on type:
36
Aircraft flight hours:
2340
Circumstances:
Middle East Airlines flight 265, a Vickers Viscount registered OD-ADE, was descending for Ankara-Esenboğa Airport, Turkey and had been cleared for an approach to runway 03. Last radio contact was at 13:09 hours GMT when the flight reported being over the Ankara NDB at 8000 feet, descending for 6500 feet. The crew would contact Ankara again over the NDB when inbound. Earlier in the day, at 11:22 GMT, a Douglas C-47 transport plane of the Turkish Air Force (CBK-28) had taken off from Ankara's Etimesgut Air Base for an instrument training flight in the southeast region of the Gölbasi beacon. The duration of the flight was planned for 1 hour 30 minutes . In this type of flight the student pilot is normally seated in the left-hand seat, an orange plexiglass panel is placed in front of him on the left half of the windshield, and he wears dark blue glasses. The instructor is in the right-hand seat and is able to maintain a lookout. The training manoeuvres had been completed, and the aircraft was returning to Etimesgut flying under visual flight rules by the time MEA flight 265 was descending for Esenboğa Airport. The Viscount, cruising on a heading of 283°, collided with the C-47 which was flying on a heading of 243° towards Etimesgut. The lower right-hand-side of the Viscount's nose and the starboard wing struck the C-47 from behind at a 40° angle in the door area on its port side. Propeller no. 3 also struck the C-47's left horizontal stabilizer, cutting it off. The blade ends broke off and remained with the tail unit of the C-47 near the base of the left horizontal stabilizer. The blade of propeller no. 4 cut the underside of the tip of the right horizontal stabilizer. Both aircraft flew together for a very short time then separated. The tail unit of the C-47 having been cut off, the C-47 fell vertically immediately thereafter. Prior to being cut off, the left horizontal stabilizer of the C-47 damaged the starboard side skin covering of the Viscount in the vicinity of the passenger cabin windows. This piece of skin covering broke off, and some of the passengers fell out through this hole. The Viscount flew a very short while following the separation of the two aircraft, then nosed down and fell. Both aircraft crashed into a residential area of Ankara, killing 87 people on the ground. 50 others were seriously injured.
Probable cause:
The Viscount aircraft had an IFR flight plan but was cruising under VFR conditions when it hit, with the lower side of the nose and with its starboard wing, the C-47 aircraft of the Turkish Air Force between the door on the port side of the fuselage and the tail group at an angle of forty degrees from the left rear and at an angle of approximately five to ten degrees upward. It cut off, with its starboard inner (No.3) propeller, the port side horizontal stabilizer of the C-47 aircraft. The pilots of the Viscount aircraft did not see the C-47 aircraft cruising below 7000 feet on their right-hand side forward, and the Viscount, having a higher speed, caught up with the C-47 from the left rear. At the last moment the Viscount pilots saw the C-47 and tried to avoid the collision by pulling up, but they did not succeed. The following findings were reported:
- The Viscount pilot made an estimation error of two minutes on the distance between Gölbasi and the Ankara NDB,
- His radiocommunications did not conform to the standard international conversation procedures,
- The C-47 was returning to Etimesgut Airport under visual flight rules (VFR) following an instrument training flight,
- These training flights are scheduled to be carried out below 7 000 ft with the trainee-pilot behind blind flight panels and the instructor-pilot sitting so as to be able to see outside thoroughly, The flights normally last for 1 hour- and 30 minutes, however, the instructor is authorized to extend this period if he deems it necessary,
- The C-47 was subjected to an impact from the port side rear at an angle of 40° and from the bottom to the top upwards at an angle of approximately 5 to 10°. The Viscount's flaps were set at 32° down, and the gear was down and locked. The aircraft collided over the City of Ankara at an altitude less than 7 000 feet.
Final Report:

Crash of a Vickers 754 Viscount in Ankara: 52 killed

Date & Time: Feb 1, 1963 at 1513 LT
Type of aircraft:
Operator:
Registration:
OD-ADE
Survivors:
No
Site:
Schedule:
Beirut – Nicosia – Ankara
MSN:
244
YOM:
1957
Flight number:
ME265
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
11
Pax fatalities:
Other fatalities:
Total fatalities:
52
Captain / Total hours on type:
2925.00
Copilot / Total hours on type:
4200
Circumstances:
Middle East Airlines flight 265, a Vickers Viscount registered OD-ADE, was descending for Ankara-Esenboğa Airport, Turkey and had been cleared for an approach to runway 03. Last radio contact was at 13:09 hours GMT when the flight reported being over the Ankara NDB at 8000 feet, descending for 6500 feet. The crew would contact Ankara again over the NDB when inbound. Earlier in the day, at 11:22 GMT, a Douglas C-47 transport plane of the Turkish Air Force (CBK-28) had taken off from Ankara's Etimesgut Air Base for an instrument training flight in the southeast region of the Gölbasi beacon. The duration of the flight was planned for 1 hour 30 minutes . In this type of flight the student pilot is normally seated in the left-hand seat, an orange plexiglass panel is placed in front of him on the left half of the windshield, and he wears dark blue glasses. The instructor is in the right-hand seat and is able to maintain a lookout. The training manoeuvres had been completed, and the aircraft was returning to Etimesgut flying under visual flight rules by the time MEA flight 265 was descending for Esenboğa Airport. The Viscount, cruising on a heading of 283°, collided with the C-47 which was flying on a heading of 243° towards Etimesgut. The lower right-hand-side of the Viscount's nose and the starboard wing struck the C-47 from behind at a 40° angle in the door area on its port side. Propeller no. 3 also struck the C-47's left horizontal stabilizer, cutting it off. The blade ends broke off and remained with the tail unit of the C-47 near the base of the left horizontal stabilizer. The blade of propeller no. 4 cut the underside of the tip of the right horizontal stabilizer. Both aircraft flew together for a very short time then separated. The tail unit of the C-47 having been cut off, the C-47 fell vertically immediately thereafter. Prior to being cut off, the left horizontal stabilizer of the C-47 damaged the starboard side skin covering of the Viscount in the vicinity of the passenger cabin windows. This piece of skin covering broke off, and some of the passengers fell out through this hole. The Viscount flew a very short while following the separation of the two aircraft, then nosed down and fell. Both aircraft crashed into a residential area of Ankara, killing 87 people on the ground. 50 others were seriously injured.
Probable cause:
The Viscount aircraft had an IFR flight plan but was cruising under VFR conditions when it hit, with the lower side of the nose and with its starboard wing, the C-47 aircraft of the Turkish Air Force between the door on the port side of the fuselage and the tail group at an angle of forty degrees from the left rear and at an angle of approximately five to ten degrees upward. It cut off, with its starboard inner (No.3) propeller, the port side horizontal stabilizer of the C-47 aircraft. The pilots of the Viscount aircraft did not see the C-47 aircraft cruising below 7000 feet on their right-hand side forward, and the Viscount, having a higher speed, caught up with the C-47 from the left rear. At the last moment the Viscount pilots saw the C-47 and tried to avoid the collision by pulling up, but they did not succeed. The following findings were reported:
- The Viscount pilot made an estimation error of two minutes on the distance between Gölbasi and the Ankara NDB,
- His radiocommunications did not conform to the standard international conversation procedures,
- The C-47 was returning to Etimesgut Airport under visual flight rules (VFR) following an instrument training flight,
- These training flights are scheduled to be carried out below 7 000 ft with the trainee-pilot behind blind flight panels and the instructor-pilot sitting so as to be able to see outside thoroughly, The flights normally last for 1 hour- and 30 minutes, however, the instructor is authorized to extend this period if he deems it necessary,
- The C-47 was subjected to an impact from the port side rear at an angle of 40° and from the bottom to the top upwards at an angle of approximately 5 to 10°. The Viscount's flaps were set at 32° down, and the gear was down and locked. The aircraft collided over the City of Ankara at an altitude less than 7 000 feet.
Final Report:

Crash of a Fairchild F27 on Mt Medetsiz: 11 killed

Date & Time: Mar 8, 1962 at 1743 LT
Type of aircraft:
Operator:
Registration:
TC-KOP
Flight Phase:
Survivors:
No
Site:
Schedule:
Istanbul – Ankara – Adana
MSN:
83
YOM:
1960
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
11
Circumstances:
En route, the pilot reported passing Aksaray and estimated to arrive at Adana at 1740LT. At 1728 the pilot reported at FL175 and requested a clearance to approach. At 1740 the flight was cleared to 5,000 feet and was asked to report crossing 8,000 feet and 7,000 feet. Shortly later, at an altitude of 6,800 feet, the airplane struck the slope of Mt Medetsiz located 87 km north of Adana Airport. All 11 occupants were killed.
Probable cause:
According to reports received by the Incirlik tower, the aircraft should have been on the Adana radio range at 1540 hours and at flight level 175. In avoiding cumulus cloud, and associated turbulent conditions, the pilot was not able to keep track of his exact position or to maintain exact altitude.
Final Report: