Zone

Crash of an ATR72-500 in Rome

Date & Time: Feb 2, 2013 at 2032 LT
Type of aircraft:
Operator:
Registration:
YR-ATS
Survivors:
Yes
Schedule:
Pisa - Rome
MSN:
533
YOM:
1997
Flight number:
AZ1670
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
46
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
18552
Captain / Total hours on type:
3351.00
Copilot / Total flying hours:
624
Copilot / Total hours on type:
14
Aircraft flight hours:
24088
Circumstances:
The Rome-Fiumicino Airport Runway 25 was closed to trafic due to work in progress so the crew was vectored and cleared for a landing on runway 16L. The approach was completed in good visibility with strong crosswinds from 250° at 28 knots gusting to 41 knots and windshear. On the last segment, the aircraft lost height and impacted ground 567 metres short of runway 16L threshold. The aircraft bounced three times, lost its right main gear, slid for few dozen metres and came to rest in a grassy area some 1,780 metres past the runway threshold. All 50 occupants were rescued, among them seven were slightly injured. The aircraft was damaged beyond repair.
Probable cause:
The accident is due to the human factor. In particular, it was caused by an improper conduct of the aircraft by the PF (commander) during landing, not consistent with the provisions of the operator's manuals, in an environmental context characterized by the presence of significant criticality (presence of crosswind with values at the limit/excess those allowed for the ATR 72) and in the absence of an effective CRM.
The following factors may have contributed to the event:
- The failure to carry out the landing briefing, which, in addition to being required by company regulations, would have been an important moment of pooling and acceptance of information fundamental to the safety of operations.
- The maintenance of a V APP significantly higher than expected.
- The conviction of the commander (PF), deriving from his considerable general and specific experience on the aircraft in question, to be able to conduct a safe landing in spite of the presence of critical wind conditions for the type of aircraft.
- The considerable difference in experience between the commander and the first officer, which has reasonably prevented the latter from showing his critical capacity, thus rendering CRM techniques ineffective.
Final Report:

Crash of an Airbus A319-132 in Palermo

Date & Time: Sep 24, 2010 at 2007 LT
Type of aircraft:
Operator:
Registration:
EI-EDM
Survivors:
Yes
Schedule:
Rome - Palermo
MSN:
2424
YOM:
2005
Flight number:
JET243
Country:
Region:
Crew on board:
5
Crew fatalities:
Pax on board:
124
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
13860
Captain / Total hours on type:
2918.00
Copilot / Total flying hours:
1182
Copilot / Total hours on type:
937
Aircraft flight hours:
15763
Aircraft flight cycles:
8936
Circumstances:
Following an uneventful flight from Rome-Fiumicino Airport, the crew started a night approach to Palermo-Punta Raisi Airport in poor weather conditions with heavy rain falls, thunderstorm activity and reduced visibility. During the descent, weather information was transmitted to the crew, indicating a visibility of 4 km with few CB's at 1,800 feet and a windshear warning for runway 20. On final approach, at an altitude of 810 feet (100 feet above MDA), following the 'minimum' call, the captain instructed the copilot to continue the approach despite the copilot did not establish a visual contact with the runway. At an altitude of 240 feet, the copilot reported the runway in sight but informed the captain that all four PAPI's lights were red. The captain took over control and continued the approach after the airplane deviated from the descent profile. With an excessive rate of descent of 1,360 feet per minute, the aircraft impacted ground 367 metres short of runway 07 threshold and collided with the runway 25 localizer antenna. Upon impact, both main landing gear were partially torn off. The aircraft slid for about 850 metres before coming to rest on the left of the runway. All 129 occupants were rescued, among them 35 were injured. The aircraft was damaged beyond repair.
Probable cause:
The event is classified as short landing accident and the cause is mainly due to human factors. The fact that the aircraft contacted the ground took place about 367 meters short of the runway threshold was due to the crew's decision to continue the instrument approach without a declared shared acquisition of the necessary visual references for the completion of the non-precision procedure and of the landing maneuver. The investigation revealed no elements to consider that the incident occurred due to technical factors inherent in the aircraft.
The following contributing factors were identified:
- The poor attitude of those present in the cockpit to use of basics of CRM, particularly with regard to interpersonal and cognitive abilities of each and, overwhelmingly, the commander.
- Deliberate failure to comply with SOP in place which provided, reaching the MDA, to apply the missed approach procedure where adequate visual reference of the runway in use had not been in sight of both pilots.
- Failure to apply, by those present in the cockpit, the operators rules, concerning in particular: the concept of "sterile cockpit"; to do the descent briefing; to make callouts on final approach.
- The routine with the crew, carrying out approaches to Palermo-Punta Raisi Airport, from which the complacency to favor the personalization of the standards set by operator, and by law. The complacency is one of the most insidious aspects in the context of the human factor, as it creeps in individual self-satisfaction of a condition, which generates a lowering of situational awareness, however bringing them to believe they had found the best formula to operate.
- The existence of adverse weather conditions, characterized by the presence of an extreme rainfall, which significantly reduced the overall visibility.
- The "black hole approach" phenomenon, due to adverse weather conditions together with an approach carried out at night, the sea, to a coast characterized by few dimly lit urban settlements.
This created the illusion in the PF of "feeling high" compared to what he saw and believed to be the threshold, with the result to get him to abandon the ideal descent profile, hitherto maintained, to make a correction and the subsequent short landing.
- The decrease of performance of the light beam produced by SLTH in extreme rain conditions; The only bright horizontal reference for the crew consisted of the crossbar of the SALS, probably mistaken for the threshold lights.
Final Report:

Ground accident of a McDonnell Douglas MD-82 in Trieste

Date & Time: Apr 20, 2004 at 1038 LT
Type of aircraft:
Operator:
Registration:
I-DAWR
Survivors:
Yes
Schedule:
Rome – Trieste
MSN:
49208/1190
YOM:
1985
Flight number:
AZ1357
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
92
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7988
Captain / Total hours on type:
3800.00
Copilot / Total flying hours:
5724
Aircraft flight hours:
41745
Aircraft flight cycles:
34235
Circumstances:
Following an uneventful flight from Rome-Ciampino Airport and a normal landing at Trieste-Ronchi dei Legionari Airport runway 09, the crew vacated the runway and continued via taxiway Bravo to the apron. The copilot was the pilot-in-command and he was facing sun while approaching the ramp. At the last moment, the captain noticed a dump truck on the right side of the taxiway. He took over controls and elected to turn to the left but the aircraft collided with the truck. The outer part of the right wing was torn off for about 3,5 metres and the fuselage was bent. Also, a fuel tank ruptured, causing a spill on the taxiway. The captain immediately stopped the airplane and all 96 occupants evacuated safely. It appeared that construction works were in progress near the taxiway Bravo. A Notam was not issued about this and the tower controller had not informed the crew either.
Probable cause:
The analysis of the technical, operational and organizational context in which the event took place (impact of the end of the right wing of the aircraft, during taxiing, against the rear body of a truck that was parked for work within the protection area of the taxiway that leads from the Bravo connection to the parking area) has allowed to determine the following causes, which are attributable to human and environmental factors.
- Failure to close the Bravo taxiway with the issue of the relative NOTAM of the works in progress.
- Failure of the Torre control to provide the pilots with essential information on the condition of the airport, as provided for by ICAO in ICAO Doc. 4444 PANS-ATM.
- Vertical and horizontal ground signs do not correspond to those specified in ICAO Annex 14.
- Failure to comply with the ENAC circular (APT-11), applicable for the type of work in progress at the airport.
- Insufficient surveillance of the airport area affected by the works by ENAC and the airport management company Aeroporto FVG.
- Lack of an airport Safety Management System .
- Inadequate surveillance of the external space during taxiing by the flight crew, resulting in incorrect assessment of the position of the aircraft with respect to the obstacle.
Final Report:

Ground accident of an ATR42-300 in Rome

Date & Time: Mar 6, 2003 at 2050 LT
Type of aircraft:
Operator:
Registration:
I-ATRF
Flight Phase:
Survivors:
Yes
Schedule:
Rome - Rimini
MSN:
034
YOM:
1986
Flight number:
MTC403
Country:
Region:
Crew on board:
3
Crew fatalities:
Pax on board:
42
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
7685
Captain / Total hours on type:
1159.00
Copilot / Total flying hours:
740
Copilot / Total hours on type:
232
Aircraft flight hours:
27472
Aircraft flight cycles:
28492
Circumstances:
Following a normal taxi procedure at Rome-Fiumicino Airport, the crew was at the holding point of runway 25, ready for departure. On board were 42 passengers and a crew of three. Both engines were turning at 70% torque. When the crew released the brakes, the swinging lever of the left main gear failed. The aircraft sank on its belly and stopped. All 45 occupants evacuated safely and there were no injuries. The aircraft was damaged beyond repair.
Probable cause:
Failure of the swinging lever of the left main gear due to the presence of fatigue cracks.
Final Report:

Crash of a Douglas DC-9-32 in Warsaw

Date & Time: Dec 17, 1991 at 1749 LT
Type of aircraft:
Operator:
Registration:
I-RIBN
Survivors:
Yes
Schedule:
Rome - Warsaw
MSN:
47339
YOM:
1969
Flight number:
AZ552
Country:
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
90
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
While descending to Warsaw-Okecie Airport, the crew encountered poor weather conditions with thunderstorm activity. On final approach, the copilot suggested the captain to abandon the landing procedure and to initiate a go-around maneuver. The captain dismissed the copilot's suggestion, disengaged the autopilot system and continued the approach when visual contact with the ground was established at an altitude of 400 feet. In a nose-down attitude and at an excessive speed of 155 knots (about 25-30 knots above the recommended speed), the aircraft struck the runway 33 surface nose gear first. The aircraft bounced then veered off runway to the left, rolled on soft ground for about 860 metres and lost its nose gear before coming to rest. All 96 occupants were evacuated, among them three passengers were slightly injured. The aircraft was damaged beyond repair.
Probable cause:
Wrong approach configuration on part of the flying crew who decided to continue the descent while the aircraft was unstable and misaligned with the runway. The following contributing factors were reported:
- Failure of the crew to initiate a go-around procedure,
- Unstabilized approach,
- Excessive approach speed,
- Touchdown completed in a nose-down attitude,
- Poor crew coordination,
- Poor weather conditions with thunderstorm activity.