Airport (less than 10 km from airport)

Crashed on approach to Bahía Blanca-Comandante Espora Airport after the crew attempted an emergency landing for unknown reasons. All three crew members were killed.
Crew:
Lt Javier Diamante,
Lt José Gahn,
Cpl Gustavo Marquez.

On final approach to Almaty Airport, the crew decided to initiate a go-around for unknown reasons when the aircraft lost height and crashed. All eight occupants were killed. There were low clouds and rain falls at the time of the accident.

The pilot was approaching Atlantic City Airport by night and poor weather conditions when the twin engine aircraft struck the ground and crashed few miles short of runway. The aircraft was destroyed and the pilot, sole on board, was killed.

On final approach to Koh Samui Airport runway 35, the aircraft entered an area of heavy rain falls. As the crew was unable to locate the runway, the captain decided to initiate a go-around procedure. With flaps fully extended, the crew increased power and started to gain height when the aircraft rolled to the left to an angle of 75° then entered an uncontrolled descent and crashed at a speed of 147 knots about 5 km short of runway threshold. The aircraft disintegrated on impact and all 38 occupants were killed.

Following an uneventful flight from Moscow-Domodedovo Airport, the crew started the approach to Yakutsk-Intl Airport. Due to poor weather conditions and a visibility below minima, the crew diverted to Magan Airport. The aircraft overflew the runway threshold at a height of 22 meters and a speed of 297 km/h. It 'floated' for 22 seconds and eventually landed 1,647 meters past the runway threshold. For unknown reasons, the captain maintained the aircraft in a nose-up attitude and the nose gear landed nine seconds after the first touchdown only. Reverse thrust were not activated and the spoilers were finally deployed but too late. At a distance of 47 meters from the runway end, the captain shut down all four engine when the aircraft overran at a speed of 167 km/h. It went down an embankment, lost its undercarriage and came 538 meters past the runway end, 3,978 meters from the runway threshold and 2,331 meters from the touchdown point. Four passengers were injured and 185 other occupants were evacuated safely. The aircraft was damaged beyond repair.

The aircraft was completing a special flight on behalf of the Libyan Red Crescent. On approach, the crew was instructed to follow a holding circuit of 40 minutes because a landing was not possible due to poor weather conditions. When the circuit was completed, the crew initiated the approach but the visibility was still poor as the weather did not improve. The aircraft landed hard, causing the left main gear to collapse. The left wing struck the ground and was torn off till the engine. Out of control, the aircraft veered off runway to the left and came to rest, bursting into flames. All five occupants were injured and the aircraft was destroyed.

On the 14th November 1990 ALITALIA flight 404, aircraft type DC-9-32 registration I-ATJA, took off from runway 36R at LIN bound for ZRH. The flight was a scheduled commercial flight. The clearance was to the destination airport Zürich, via a CANNE IC departure to Flight Level 120, the transponder code 0302. The PIC assumed the duties of assisting pilot and dealt with the radio-telephony. The First Officer was the handling pilot. The take-off was at 1836 hrs. The standard climb via CANNE towards Airway A9 to the cruising flight level of 200 was trouble free. About 2 minutes after reaching Flight Level 200 the crew listened to Zürich VOLMET. From this they gathered that the surface wind at Zürich was 240/08 kt. This led the PIC forsee a landing on runway 28. Having heard from the ATIS that the landing runway was 14, the crew still discussed a right hand circling approach for a landing on runway 28. The discussion continued considering a left hand circling to runway 28. At 1852.53 hrs, from a QNH of 1019 hPa the crew worked out a QFE of 970 hPa. During the descent, the crew discussed the approach procédure for runway 14, where the Copilot mentioned the Outer Marker height for runway 16. After the discussion about the setting of the navigation aids, they also discussed the procédure to be followed in the event of a communications failure. The crew were instructed that following radar vectors they should fly an ILS approach to runway 14. At 1900.01 hrs the Copilot said "We perform a CAT JJ (approach)". The PIC was in agreement because the navigation equipment had to be checked. Whilst verifying the décision height, it transpired that the Copilot was still Consulting the approach chart for runway 16. Further lengthy discussions about the setting of the required navigation aids followed. As the aircraft passed abeam Zürich descending to Flight Level 90, the PIC noted: "We are by KLOTEN, FL 90. He is bringing us in high". Clearance to descend to Flight Level 60 followed at 1902.28 hrs. At 1902.50 hrs ALITALIA 404 was instructed to fly heading 325. VHF NAV 1 was tuned to Trasadingen VOR (TRA), VHF NAV 2 to Kloten VOR (KLO). To define the fix at EKRON, the course 068 was also set. At 1904.32 hrs the PIC repeated "The outer marker is at 1200 ft (QFE), it can be verified by 3.8 [NM] from Kloten. Rhein (RHI NDB) 5.6 [NM]...". At 1905.15 hrs a new heading was required which the PIC confirmed. The identification of the ILS - 14 was registered on the CVR at 1905.32 hrs. At 1906.20 hrs, together with the approach clearance to runway 14, a new heading of 110, descent to 4000 ft and the QNH of 1019 hPa was given. The PIC confirmed this clearance, however the heading was read back as 120. The incorrect readback of the clearance by the PIC caused the Copilot some uncertainty of the required heading to be flown. The PIC confirmed the approach clearance and the cleared altitude 4000 ft to the COPI, whereby the COPI ordered "RADIO APPROACH...". At this point an altitude of about 5000 ft (QNH) was passed. One of the pilots asked the other whether he had a Glide Path indication. The aircraft position was just before interception of the Localiser passing an altitude of about 4700 ft (QNH) (according to radar and DFDR). It was already about 1300 ft below the Glide Path. Answering the question about the Glide Path, the other pilot replied (hardly understandable) "On 1...I don't have...." Consequently the PIC said: "Good, so let's do it on 1". The COPI then ordered "RADIO 1". The flaps were probably set to 15°. In the meantime, the aircraft had passed through the localiser and was now slightly east of it. About the same time as the PIC said "Capture LOC capture glide path capture - so we are on the localiser, a little off track but..." (translated from Italian) the aircraft descended through 4000 ft (QNH) (about 11.5 NM from the threshold runway 14). It was thus about 1200 ft below the glide path. The QFE 970 hPa was also set by the COPI. About 5 seconds later the Altitude Exit Alert was heard (Descent through 3700 ft [QNH]). The PIC cancelled the warning by setting 5000 ft (Go Around Altitude) on the Altitude Preselect. The PIC said to the COPI: "There is another one (Finnair 863) in front quite close. You can reduce even further to 150 (kt) otherwise we'll end up with a "go around". A discussion followed about possible icing. After this the flaps were set to 25 during which no Landing Gear horn was heard. At this point the aircraft was established on the localiser. The altitude was about 3000 ft QNH - ca. 1200 feet below the glide path. The PIC: "Outer Marker check is at 1250 ft [QFE]". The height was now about 1600 ft QFE. 10 seconds after Flaps 25, the flaps were set to 50. The Outer Marker height of 1250 ft QFE was now passed. The PIC said "Bravo" followed by sounds of switching. At 8 NM final the PIC mentioned "3.8 almost 4 miles". At about 7 NM final, (15 seconds after the PIC's words "Almost 4 miles") the COPI asked "... haven't we passed it?". After a further 12 seconds the COPI asked once again "Didn't we pass the outer marker?" The height was now 670 ft QFE. The PIC's answer was "No no it hasn't changed yet. At 6.6 NM final the PIC said "Oh it shows 7 The crew was now ordered by Zürich ARR to change frequency to Zürich TWR. At 6.25 NM final the pilots conversed as follows: "... That doesn't make sense to me "Nor to me ...". 2 seconds after this conversation the PIC called out "Pull, pull, pull, pull! ". Simultaneously autopilot disconnection could be heard. The position was now about 500 ft AGL overhead Weiach - about 350 ft QFE. 2 seconds later the COPI called out "GO AROUND" the PIC responded with "No no no no ... catch the glide". At this point the DFDR shows a pitch change from -2° [AND] to +5.4° [ANU]. At the same time the thrust was increased from 1.3 to 1.7 EPR. The sink rate decreased from 1100 ft/min. to 190 ft/min. After 11 seconds (the pitch oscillated at +1° [ANU]) the PIC asked "Can you hold it?" to which the COPI replied "Yes". One second after the COPI's answer the Radio Altimeter warning (pip pip pip) indicating 200 ft/AGL could be heard. During this, the PIC said "Hold on let's try to At 1911.18 hrs the aircraft Struck the north em slope of the Stadlerberg at a altitude of 1660 ft QNH. All 46 occupants were killed.

The pic/cfi was conducting a public use instructional flight with two military rated student pilots. The airplane was observed at about 60 to 80 feet agl south of the approach end of an active runway. It yawed to the right, and back to the left, colliding with the terrain in a 45° leftwing-low attitude, and disappeared from view. He flight had been in the pattern making touch-and-go's, and had earlier reported a single engine approach. This landing was to be a full-stop. All three occupants were killed.

Shortly after takeoff from runway 15, while in initial climb, the aircraft banked right and crashed about 300 meters from the apron, bursting into flames. A crew member was injured while nine other occupants were killed.

The crew (one instructor and one pilot under training) departed Blantyre-Chileka Airport on a local training flight. Few minutes after takeoff, the instructor shut down the right engine to simulate a failure and the crew continued the flight when, shortly later, the left engine lost power and failed. The crew elected to restart the right engine but without success. In a such situation, the pilots decided to return to Blantyre Airport when, on final approach, the aircraft stalled and crashed 1,300 meters short of runway. One pilot was killed while the second occupant was seriously injured.