Crash of a Fokker F27 Friendship 200 in Chitral

Date & Time: Jun 16, 2004
Type of aircraft:
Operator:
Registration:
AP-AUR
Survivors:
Yes
Schedule:
Peshawar - Chitral
MSN:
10307
YOM:
1966
Flight number:
PK660
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
36
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
After landing on runway 02 at Chitral Airport, the aircraft was unable to stop within the remaining distance. It overran, lost its undercarriage and came to rest in a grassy and sandy area. All 40 occupants evacuated safely and the aircraft was damaged beyond repair.

Crash of an Avro 748-232-2A off Libreville: 19 killed

Date & Time: Jun 8, 2004 at 0938 LT
Type of aircraft:
Operator:
Registration:
TR-LFW
Survivors:
Yes
Schedule:
Libreville – Port Gentil – Franceville
MSN:
1611
YOM:
1967
Flight number:
GBE221
Country:
Region:
Crew on board:
4
Crew fatalities:
Pax on board:
26
Pax fatalities:
Other fatalities:
Total fatalities:
19
Circumstances:
The aircraft departed Libreville-Léon Mba Airport at 0911LT on a flight to Franceville with an intermediate stop in Port Gentil with 26 passengers and four crew members on board. Few minutes after takeoff, the crew informed ATC about technical problem and was cleared to return to Libreville. In excellent weather conditions, the aircraft overflew the runway then crashed in the sea about 100 metres offshore. Eleven occupants were rescued while 19 others were killed, among them one crew member.
Probable cause:
Loss of hydraulic pressure on the right engine forced the crew to shut down this engine and to feather its propeller. On approach, the crew was unable to lower the gears because of the loss of hydraulic pressure.

Crash of an Embraer EMB-120ER Brasília near Manaus: 33 killed

Date & Time: May 14, 2004 at 1835 LT
Type of aircraft:
Operator:
Registration:
PT-WRO
Survivors:
No
Schedule:
São Paulo de Olivença – Tabatinga – Tefé – Manaus
MSN:
120-070
YOM:
1988
Flight number:
RLE4815
Location:
Country:
Crew on board:
3
Crew fatalities:
Pax on board:
30
Pax fatalities:
Other fatalities:
Total fatalities:
33
Captain / Total flying hours:
19069
Captain / Total hours on type:
5819.00
Copilot / Total flying hours:
11927
Copilot / Total hours on type:
4637
Circumstances:
While descending to Manaus-Eduardo Gomes Airport following an uneventful flight from Tefé, the aircraft was correctly established on the ILS when the crew was instructed by ATC to initiate a go-around and to follow a holding pattern as the priority was given to an ambulance flight. The crew made a left turn heading 060° and continued the descent after passing 2,000 feet when the aircraft struck the ground and crashed about 33 km from the airport. The aircraft disintegrated on impact and all 33 occupants were killed.
Probable cause:
Controlled flight into terrain after the crew continued the descent below 2,000 feet until the aircraft impacted ground. The following contributing factors were identified:
- The crew reported his altitude at 2,000 feet while the real altitude of the airplane was 1,300 feet,
- The crew continued the descent until final impact,
- The crew did not react to the GPWS alarm that sounded four times when the aircraft reached the altitude of 400 feet,
- No corrective action was taken by the crew,
- Lack of crew coordination,
- Poor approach planning that led the aircraft descending to a critical altitude,
- Lack of supervision,
- Operational deficiencies.
Final Report:

Crash of an ATR72-212 in San Juan

Date & Time: May 9, 2004 at 1450 LT
Type of aircraft:
Operator:
Registration:
N438AT
Survivors:
Yes
Schedule:
Mayaguez - San Juan
MSN:
438
YOM:
1995
Flight number:
AA5401
Country:
Crew on board:
4
Crew fatalities:
Pax on board:
22
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
6071
Captain / Total hours on type:
3814.00
Copilot / Total flying hours:
2000
Copilot / Total hours on type:
20
Aircraft flight hours:
19276
Aircraft flight cycles:
18086
Circumstances:
Flight 5401 departed Mayagüez, Puerto Rico, for San Juan about 14:15. The captain was the nonflying pilot for the flight, and the first officer was the flying pilot. The takeoff, climb, and en route portions of the flight were uneventful. At 14:37, as the flight approached the San Juan traffic area, the ATIS reported that winds were 060 degrees at 17 knots and gusting at 23 knots. Shortly thereafter, the captain briefed a Vref (the minimum approach airspeed in the landing configuration before the airplane reaches the runway threshold) of 95 knots and told the first officer to "stand by for winds." At 14:43 SJU Terminal Radar Approach Control cautioned the pilots of possible wake turbulence from a preceding Boeing. The captain told the first officer to slow down to about 140 kts. At 14:46, the local controller cleared the airplane to land on runway 08. The first officer turned the airplane left toward runway 08 and transitioned to the visual approach slope indicator. At 14:49, the captain stated, "you better keep that nose down or get some power up because you're gonna balloon." The airplane descended below the glideslope, causing a GPWS "glideslope" alert. The airplane was about 45 feet above ground level and traveling at 110 knots indicated airspeed when it crossed the runway 08 threshold. After the airplane crossed the runway threshold, the captain stated, "power in a little bit, don't pull the nose up, don't pull the nose up." At 14:49:39, the captain stated, "you're ballooning," and the first officer replied, "all right." The airplane touched down for the first time about 14:49:41 and about 1,600 feet beyond the runway 08 threshold with vertical and lateral loads of about 1.3 Gs and -0.10 G, respectively. Upon touchdown the captain stated, "get the power," and, 1 second later, "my aircraft." The first officer responded, "your airplane." The airplane had skipped to an altitude of about 4 feet and touched down again two seconds later about 2,200 feet beyond the runway 08 threshold. The airplane then pitched up to an angle of 9° while climbing to an altitude of 37 feet and the engine torque increased from 10 to 43 percent. About 14:49:49, the pitch angle decreased to -3°, and the engine torque started to decrease to 20 percent with the pitch angle decreasing to -10°. The airplane touched down a third time about 14:49:51 at a bank angle of 7° left wing down and about 3,300 feet beyond the runway 08 threshold and with vertical and lateral loads of about 5 Gs and 0.85 G. The ATR pitched up again to 24 feet and landed a fourth time about 14:49:56 (about 15 seconds after the initial touchdown) and about 4,000 feet beyond the runway 08 threshold. This time the airplane pitched down to -7° and that it was banked 29° left wing down. The airplane came to a complete stop on a grassy area about 217 feet left of the runway centerline and about 4,317 feet beyond the runway threshold.
Probable cause:
The captain’s failure to execute proper techniques to recover from the bounced landings and his subsequent failure to execute a go-around.
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:

Crash of a Cessna 208B Grand Caravan in Lake Manyara

Date & Time: Mar 17, 2004 at 0615 LT
Type of aircraft:
Operator:
Registration:
5H-MUA
Flight Phase:
Survivors:
Yes
Schedule:
Arusha – Lake Manyara – Klein’s Camp – Grumet – Seronera – Lake Manyara – Arusha
MSN:
208B-0487
YOM:
1995
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
8
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
14000
Circumstances:
The aircraft was operating a scheduled flight starting from its base at Arusha. It was to call at Lake Manyara, Klein’s Camp, Grumet and Seronera before returning to Arusha via Lake Manyara. 5H-MUA took off from Arusha at 0530 hours. It was carrying one pilot and 3 passengers. The VFR flight to Lake Manyara was uneventful and the aircraft landed at Lake Manyara at 0555 hours. Five more passengers joined the flight here and 5H-MUA subsequently took off for Klein’s Camp at 0615 hours. During initial climb, the engine failed. The pilot feathered the propeller and attempted an emergency landing on a road. But he was forced to make an evasive manoeuvre because of a truck. The aircraft lost speed and height, collided with a stone wall beside the road and came tor rest. All nine occupants were rescued, among them five were seriously injured.
Probable cause:
Engine failure for undetermined reasons.
Final Report:

Crash of a Dornier DO.28D-2 Skyservant near Guayaquil

Date & Time: Mar 5, 2004 at 1755 LT
Type of aircraft:
Registration:
HC-CBK
Flight Phase:
Survivors:
Yes
Schedule:
Machala – Guayaquil
MSN:
4080
YOM:
1971
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
12
Pax fatalities:
Other fatalities:
Total fatalities:
0
Aircraft flight hours:
2977
Circumstances:
En route from Machala to Guayaquil, while cruising at an altitude of 6,000 feet in rain showers, the left engine lost power. The crew shut down the engine and feathered the propeller then decided to continue at an altitude of 600 feet and a speed of 80 knots. Several attempts to restart the left engine were unsuccessful when the right engine lost power as well. Unable to maintain a safe altitude, the crew attempted an emergency landing when the aircraft crashed in a river, some 23 km south of Guayaquil. All 14 occupants escaped with minor injuries and the aircraft was damaged beyond repair.
Probable cause:
A possible failure of the hydraulic pump on the left engine due to poor maintenance.

Crash of an Airbus A300B4-203 in Jeddah

Date & Time: Mar 1, 2004 at 0140 LT
Type of aircraft:
Operator:
Registration:
AP-BBA
Flight Phase:
Survivors:
Yes
Schedule:
Jeddah - Quetta
MSN:
114
YOM:
1980
Flight number:
PK2002
Country:
Region:
Crew on board:
12
Crew fatalities:
Pax on board:
261
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
During the takeoff roll on runway 34 at Jeddah-King Abdulaziz Airport, ATC informed the crew about a fire on the left main gear. The captain rejected takeoff and was able to stop the aircraft within the remaining distance. All 273 occupants evacuated safely but the aircraft was considered as damaged beyond repair.
Probable cause:
It was determined that both tyres on the left main gear burst during the takeoff roll. Debris punctured a fuel tank in the left wing and other parts were ingested by the left engine.

Crash of a Fokker 50 in Sharjah: 43 killed

Date & Time: Feb 10, 2004 at 1138 LT
Type of aircraft:
Operator:
Registration:
EP-LCA
Survivors:
Yes
Schedule:
Kish Island - Sharjah
MSN:
20273
YOM:
1993
Flight number:
IRK1770
Region:
Crew on board:
6
Crew fatalities:
Pax on board:
40
Pax fatalities:
Other fatalities:
Total fatalities:
43
Captain / Total flying hours:
6440
Captain / Total hours on type:
1516.00
Copilot / Total flying hours:
3978
Copilot / Total hours on type:
517
Aircraft flight hours:
20466
Aircraft flight cycles:
19845
Circumstances:
The aircraft was operating as a scheduled flight from Kish Island, Iran to Sharjah, UAE with the captain initially as the pilot flying (PF). During the cruise and just prior to descent, the captain unexpectedly handed over control of the aircraft to the First Officer prior to the approach to Sharjah. The first officer did not accept this willingly and stated that he was not confident of his ability to conduct a VOR/DME approach into Sharjah. This statement was not consistent with his previous experience and could indicate either a cultural or professional issue. The captain insisted the first officer fly the aircraft and encouraged and instructed him during the approach. At 11:24 hours local time, the aircraft contacted Dubai Arrivals and was cleared from 9000 ft to 5000 ft and instructed to expect a VOR/DME approach to runway 12 at Sharjah International Airport. At 11:29 hours the aircraft was further cleared to 2500 ft and cleared for the approach. The aircraft was under its own navigation and the daylight conditions were fine with excellent visibility. At 11:35 hours the aircraft was instructed to contact Sharjah Tower and the pilot reported that the aircraft was established on the VOR final approach for runway 12. The Tower cleared IRK7170 to land and advised that the wind was calm. At that point the aircraft was slightly above the approach profile. The initial speed for the approach was at least 50 kt high at approximately 190 kt with no flap and no landing gear. The aircraft should have been configured with landing gear down and flap 10° during the approach and stabilized at 130 kt prior to the MDA. Approaching the MDA at flight idle setting, the autopilot was disengaged and the first Officer called for flap 10 at 186 kt (limiting speed of 180 kt) and flap 25 was selected by the Captain, a setting uncalled for by the Pilot Flying at 183 kt (limiting speed of 160 kt), and the landing gear was called for and selected at approximately 185 kt (limiting speed of 170 kt). The captain then took control of the aircraft and shortly afterwards the ground range selectors were heard by Cockpit Voice Recorder to be lifted and the power levers moved from the flight idle stop into the ground control range. The left propeller then went to full reverse whilst the right propeller remained in positive pitch within the ground control range. The aircraft descended in an extreme nose low left bank attitude until impact. The aircraft crashed 2.6 nm from the runway onto an unprepared sandy area adjacent to a road and residential buildings. The aircraft broke apart on impact and a fire started immediately. Three passengers suffered injuries while 43 other occupants were killed.
Probable cause:
During the final approach, the power levers were moved by a pilot from the flight idle position into the ground control range, which led to an irreversible loss of flight control. The following contributing factors were identified:
1. By suddenly insisting the First Officer fly the final approach, the pilot in command created an environment, which led to a breakdown of crew resource management processes, the non observance of the operator’s standard operating procedures and a resultant excessive high approach speed.
2. An attempt to rectify this excessive high approach speed most likely resulted in the non compliance with the Standard Operating Procedures and the movement of the power levers below flight idle.
3. The unmodified version of the Skid Control Unit failed to provide adequate protection at the time of the event.
Final Report:

Crash of a Cessna 208B Grand Caravan off Pelée Island: 10 killed

Date & Time: Jan 17, 2004 at 1638 LT
Type of aircraft:
Operator:
Registration:
C-FAGA
Flight Phase:
Survivors:
No
Schedule:
Pelée Island – Windsor
MSN:
208B-0658
YOM:
1998
Flight number:
GGN125
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
10
Captain / Total flying hours:
3465
Captain / Total hours on type:
957.00
Aircraft flight hours:
7809
Circumstances:
On 17 January 2004, the occurrence pilot started his workday in Toronto, Ontario, reporting for duty at 0445 eastern standard time. In the morning, he completed flights in the Cessna 208B Caravan from Toronto to Windsor, Ontario, Windsor to Pelee Island, Ontario, and then Pelee Island to Windsor where the aircraft landed at 0916. At approximately 1500, the pilot received local weather and passenger information by telephone from the Pelee Island office personnel. The 1430 weather was reported as follows: ceiling 500 feet obscured, visibility two miles. There were eight male passengers for pick up at Pelee Island. One additional passenger was travelling with the pilot. There was no discussion concerning the amount of cargo to be carried or the passenger weights. At 1508, the pilot received a faxed weather package that he had requested from the Flight Information Centre (FIC) in London, Ontario. At 1523, the aircraft was refuelled in preparation for the scheduled 1600 departure to Pelee Island. The passengers were loaded earlier than usual to allow time for aircraft de-icing, as wet snow had accumulated on the fuselage and wings since the previous flight. At 1555, the aircraft was de-iced with Type 1 de-icing fluid, and it departed for Pelee Island at 1605 on an instrument flight rules (IFR) flight plan as Flight GGN125. At 1615, the pilot advised the Cleveland Control Centre, Ohio, United States, that he had Pelee Island in sight, was cancelling IFR, and was descending out of 5000 feet. The pilot also advised Cleveland that he would be departing IFR out of Pelee Island in about 20 minutes as GGN126 and asked if a transponder code could be issued. The Cleveland controller issued a transponder code and requested a call when GGN126 became airborne. The pilot advised that the flight would depart on Runway 27 then turn north. These were the last recorded transmissions from the aircraft. The aircraft landed at 1620. While on the ramp, two individuals voiced concern to the pilot that there was ice on the wing. Freezing precipitation was falling. The pilot was observed to visually check the leading edge of the wing; however, he did not voice any concern and proceeded with loading the passengers and cargo. At approximately 1638, GGN126 departed Pelee Island for Windsor. After using most of the runway length for take-off, the aircraft climbed out at a very shallow angle. No one on the ground observed the aircraft once it turned toward the north; however, witnesses who were not at the airport reported that they heard the sound of a crash, then no engine noise. A normal flight from Pelee Island to Windsor in the Cessna Caravan takes 15 to 20 minutes. Shortly after the aircraft departed, the ticket agent in Windsor received a call from Pelee Island reporting that a crash had been heard. At 1705, when the aircraft had not arrived, the ticket agent called Windsor tower. The pilot had not made contact with any air traffic services (ATS) facility immediately before or after departure, so there was nothing in the ATS system to indicate that the aircraft had taken off. It was, therefore, unaccounted for. There was no signal heard from the emergency locator transmitter (ELT). At 1710, the Windsor tower controller contacted the Rescue Coordination Centre in Trenton, Ontario, and a search was initiated. At 1908, the aircraft empennage and debris were spotted by a United States Coast Guard (USCG) helicopter on the frozen surface of the lake, about 1.6 nautical miles (nm) from the departure end of the runway. There were no survivors. The empennage sank beneath the surface some four hours later. The wreckage recovery was not fully completed until 13 days later.
Probable cause:
Findings as to Causes and Contributing Factors:
1. At take-off, the weight of the aircraft exceeded the maximum allowable gross take-off weight by at least 15 per cent, and the aircraft was contaminated with ice. Therefore, the aircraft was being flown significantly outside the limitations under which it was certified for safe flight.
2. The aircraft stalled, most likely when the flaps were retracted, at an altitude or under flight conditions that precluded recovery before it struck the ice surface of the lake.
3. On this flight, the pilotís lack of appreciation for the known hazards associated with the overweight condition of the aircraft, ice contamination, and the weather conditions was inconsistent with his previous practices. His decision to take off was likely adversely affected by some combination of stress and fatigue.
Findings as to Risk:
1. Despite the abbreviated nature of the September 2001 audit, the next audit of Georgian Express Ltd. was not scheduled until September 2004, at the end of the 36-month window.
2. The internal communications at Transport Canada did not ensure that the principal operations inspector responsible for the air operator was aware of the Pelee Island operation.
3. The standard passenger weights available in the Aeronautical Information Publication at the time of the accident did not reflect the increased average weight of passengers and carry-on baggage resulting from changes in societal-wide lifestyles and in travelling trends.
4. The use of standard passenger weights presents greater risks for aircraft under 12 500 pounds than for larger aircraft due to the smaller sample size (nine passengers or less) and the greater percentage of overall aircraft weight represented by the passengers. The use of standard passenger weights could result in an overweight condition that adversely affects the safety of flight.
5. The Cessna Caravan de-icing boot covers up to a maximum of 5% of the wing chord. Research on this wing has shown that ice accumulation beyond 5% of the chord can result in degradation of aircraft performance.
6. At the Pelee Island Airport, the air operator did not provide the equipment that would allow an adequate inspection of the aircraft for ice during the pre-flight inspection and did not provide adequate equipment for aircraft de-icing.
7. Repetitive charter operators are not considered to be scheduled air operators under current Transport Canada regulations, and, therefore, even though the charter air operator may provide a service with many of the same features as a scheduled service, Transport Canada does not provide the same degree of oversight as it does for a scheduled air operator.
8. A review of the Canadian Aviation Regulations regarding simulator training requirements indicates that there is no requirement to conduct recurrent simulator training if currency and/or pilot proficiency checks do not lapse.
9. Commercial Air Service Standard 723.91(2) does not clearly indicate whether there is a requirement for simulator training following expiration of a pilot proficiency check.
10. Incorrect information on the passenger door placards, an incomplete safety features card, and the fact that the operating mechanisms and operating instructions for the emergency exits were not visible in darkness could have compromised passenger egress in the event of a survivable accident.
11. The dogs being carried on the aircraft were not restrained, creating a hazard for the flight and its occupants.
Final Report: