Palma de Mallorca

Flight SWT704, a cargo flight from Palma de Mallorca to Barcelona, was to be used by the crew as an instruction flight. The co-pilot, who that day was flying for the first time since 20th March 1998, and who was sitting in the left-hand seat, would thus carry out a refresher flight as "First officer under supervision", in accordance with the operator's procedures. At first, it had been planned that the aircraft should carry out a missed approach with one engine on its arrival at Barcelona Airport. However, for a runway 25 approach this was very difficult and the captain decided to postpone this manoeuvre. It was then decided to carry out a standard approach leaving the glide path a little above and then stopping the engine. They would then raise the landing gear and flaps by increments. The captain added: "As soon as we're without control, we'll restore it" (the engine). The approach to runway 25 was also normal. At 00:47:10 they contacted the Barcelona control tower, which indicated that they were number 1, that they should continue and that they should notify "established in final". Afterwards, they extended the landing gear and flaps. At 22:49:55 h, the captain notified the control tower that they were established in final. The tower indicated that they should continue, that a flight was leaving runway 25 and that it would call them immediately. At that moment, the Metro was at a height of some 1400 feet, at some 6 nm (about 3 minutes at 120 kt) from the runway threshold. At 22:50:03 h, with gear and flaps down, the instructor said "Well, engine stop" to which the copilot replied: "Come on, landing gear up". Contrary to normal practice, the right engine was shut down completely and the prop was feathered. It's usual practice to retard the throttles to idle to simulate zero thrust for that engine. When the co-pilot pushed the wrong pedal, the plane deviated to the right. The captain then tried to start the engine again. This failed however because due to the seizing of the guide rod bushing of the propeller pitch change mechanism, the pitch varying mechanism did not take the blades to the necessary pitch for start-up. The captain then said: "Well, I am taking out the engine again. I've raised the flap for you. Now flap by increments...". A few moments later the copilot asked "I continue with the approach, don't I?" to which the captain replied in the affirmative and added that they had been authorized to land and that they were going to land with one engine. At 22:51:09 he again confirmed "Well, just continue with one engine" and appeared to give general instructions on how to carry out a missed approach or what to do when near the runway. At 22:52:01, the captain said "landing gear", the co-pilot said "landing gear now" and the captain then confirmed "coming down". The stall warning then began to sound. The aircraft turned off to the right of the ILS localizer and adopted a position of almost 90° of roll to the left, then a position of 90° of roll to the right whilst continuing to lose height and then again took up a position of 90° of roll to the left. Finally, the left wing struck the ground and then the aircraft crashed first into the outside barrier of highway B-203 which runs round the edge of the Airport and then the perimeter fence, finally coming to a halt at some 250 m from the threshold of runway 25 and some 100 metres to the right of the runway axis. The wreckage of the aircraft burst into flames.

Learjet 25B EC-CKR arrived near Northolt following a flight from Palma de Mallorca. Due to the presence of priority traffic which was due to depart Northolt at that time, the flight was extended down wind to a distance of 10 nm before the crew received vectors and descent instructions for the final approach to runway 25. At 3.5nm short of the runway the pilot was asked to confirm that his landing gear was down and locked as is normal procedure at Northolt. After some rephrasing of this question, the landing gear was confirmed down, however during this exchange the aircraft was seen to deviate above the glidepath. At 2.5 nm, landing clearance was confirmed and the aircraft was advised of the surface wind and the fact that there was a 4 kt tailwind. The aircraft was also advised that it was above the glide path. At the decision altitude which was at approximately half a mile from the runway the aircraft was still above the glidepath although seen to be correcting to it. On arrival at the runway the aircraft was observed to land some distance beyond the normal touchdown point. Towards the end of the landing roll it veered to the right and then swerved to the left and overran the end of the runway. It collided with three lighting stanchions and continued in a south-westerly direction towards the airfield boundary which is marked by a high chain-link fence. After bursting through the boundary fence the aircraft ran onto the A40 trunk road and was almost immediately in collision with a Ford Transit van on the east bound carriageway, and seriously injuring its driver. The aircraft came to rest in the left hand lane of the road with the van embedded in the right side of the fuselage immediately forward of the right wing.

Following an uneventful cargo flight from Palma de Mallorca, the crew started a night approach to Madrid-Barajas Airport. On final, the crew forgot to lower the gear and the aircraft landed on its belly and slid for few dozen metres before coming to rest. Both pilots escaped uninjured and the aircraft was damaged beyond repair.

Shortly after takeoff, while in initial climb, the left engine failed. The aircraft lost height and crashed on the apron, near hangars. Both pilots were killed.

After takeoff from Barcelona-El Prat Airport, while climbing to a height of about 200 feet, the aircraft banked left, lost speed and altitude. The crew attempted an emergency landing when the aircraft crash landed in a field. All three occupants escaped uninjured while the aircraft was damaged beyond repair.

During the takeoff roll at Palma Airport, the crew lost control of the aircraft that veered off runway to the left, lost its undercarriage and came to rest. Both pilots escaped uninjured and the aircraft was damages beyond repair.

The approach to Mahón Airport was completed by night and poor weather conditions. On final, the crew lost visual contact with the runway and the captain instructed the pilot to initiate a go-around. In a certain confusion, the aircraft continued its approach until it struck the runway surface with a positive acceleration of 3,56 G. The captain took over control, initiated a go-around and decided to return to Palma de Mallorca where a safe landing wa completed. All 89 occupants evacuated safely while the aircraft was considered as damaged beyond repair due to severe structural damages.

Upon landing, the right main gear collapsed. The aircraft veered off runway and came to rest. Both pilots escaped uninjured while the aircraft was damaged beyond repair.

The aircraft departed Palma de Mallorca Airport on a combined flight to Sigonella NAS with a second USN Grumman C-1A Trader registered 136772. While in cruising altitude some 150 miles east of the Balearic Islands, both aircraft collided in unknown circumstances and crashed in the Mediterranean Sea. Some debris were found floating on water but no trace of the seven crew members (four in 136753 and three on board 136772) was found.

The aircraft departed Palma de Mallorca Airport on a combined flight to Sigonella NAS with a second USN Grumman C-1A Trader registered 136772. While in cruising altitude some 150 miles east of the Balearic Islands, both aircraft collided in unknown circumstances and crashed in the Mediterranean Sea. Some debris were found floating on water but no trace of the seven crew members (four in 136753 and three on board 136772) was found.