Crash of a Swearingen SA227AC Metro III off Montevideo: 2 killed

Date & Time: Jun 6, 2012 at 1955 LT
Type of aircraft:
Operator:
Registration:
CX-LAS
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Montevideo - Buenos Aires
MSN:
AC-482
YOM:
1982
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
16177
Copilot / Total flying hours:
406
Aircraft flight hours:
26158
Circumstances:
The crew was performing a cargo flight from Montevideo to Buenos Aires on behalf of DHL. The aircraft departed runway 24 at Montevideo-Carrasco Airport at 1945LT and the crew was cleared to climb to FL080. While reaching a height of 4,500 feet, the aircraft entered an uncontrolled descent and crashed in the sea at a speed of 570 knots which caused its disintegration off Flores Island. Few debris were found the following day floating on water but the main wreckage was localized two weeks later about one NM south of Flores Island. The CVR was found on 02AUG2012 but was unreadable as the content was concerning the last 30 minutes of the precedent flight. On 11FEB2013, fishermen found the cargo door in their fishnet. No trace of the cargo nor the crew was ever found.
Probable cause:
Investigations determined that both engines were running normally at impact, that no propeller blades were lost during descent, that fuel was not contaminated and that no problems occurred on the on electrical system. Meteorological Office confirmed that severe icing conditions prevailed at the time of the accident between FL010 and FL150. The loss of control was the consequence of erroneous indications of the flight instruments, associated with the possible formation of crystalline ice on the aircraft' structure, causing a loss of situational awareness of the crew.
Final Report:

Crash of a De Havilland DHC-2 Beaver in Lillabelle Lake: 2 killed

Date & Time: May 25, 2012 at 1408 LT
Type of aircraft:
Operator:
Registration:
C-FGBF
Survivors:
Yes
Schedule:
Edgar Lake - Lillabelle Lake
MSN:
168
YOM:
1952
Country:
Crew on board:
1
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
1100
Captain / Total hours on type:
300.00
Aircraft flight hours:
22000
Circumstances:
The Cochrane Air Service de Havilland DHC-2 Mk.1 Beaver floatplane (registration C-FGBF, serial number 168) departed Edgar Lake, Ontario, with 2 passengers and 300 pounds of cargo on board. The aircraft was destined for the company’s main base located on Lillabelle Lake, Ontario, approximately 77 miles to the south. On arrival, a southwest-bound landing was attempted across the narrow width of the lake, as the winds favoured this direction. The pilot was unable to land the aircraft in the distance available and executed a go-around. At 1408, Eastern Daylight Time, shortly after full power application, the aircraft rolled quickly to the left and struck the water in a partially inverted attitude. The aircraft came to rest on the muddy lake bottom, partially suspended by the undamaged floats. The passenger in the front seat was able to exit the aircraft and was subsequently rescued. The pilot and rear-seat passenger were not able to exit and drowned. The emergency locator transmitter activated on impact.
Probable cause:
Findings as to Causes and Contributing Factors:
1. On the windward side of the landing surface, there was significant mechanical turbulence and associated wind shear caused by the passage of strong gusty winds over surface obstructions.
2. During the attempted overshoot, the rapid application of full power caused the aircraft to yaw to the left, and a left roll quickly developed. This movement, in combination with a high angle of attack and low airspeed, likely caused the aircraft to stall. The altitude available to regain control before striking the water was insufficient.
3. The pilot survived the impact, but was unable to exit the aircraft, possibly due to difficulties finding or opening an exit. The pilot subsequently drowned.
4. The rear-seat passenger did not have a shoulder harness and was critically injured. The passenger’s head struck the pilot’s seat in front; this passenger did not exit the aircraft and drowned.
Findings as to Risk:
1. Without a full passenger safety briefing, there is increased risk that passengers may not use the available safety equipment or be able to perform necessary emergency functions in a timely manner to avoid injury or death.
2. Not wearing a shoulder harness can increase the risk of injury or death in an accident.
3. Not having a stall warning system increases the risk that the pilot may not be aware of an impending aerodynamic stall.
4. Commercial seaplane pilots who do not receive underwater egress training are at increased risk of being unable to exit the aircraft following a survivable impact with water.
Final Report:

Crash of a Rockwell Shrike Commander 500S off El Loa: 2 killed

Date & Time: May 18, 2012 at 0150 LT
Operator:
Registration:
CC-CGX
Flight Phase:
Survivors:
No
Schedule:
Iquique - Iquique
MSN:
500-3306
YOM:
1978
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
20183
Captain / Total hours on type:
10000.00
Copilot / Total flying hours:
3755
Copilot / Total hours on type:
2137
Aircraft flight hours:
16308
Circumstances:
The twin engine aircraft departed Iquique-General Diego Aracena Airport at 2115LT on May 17 on a fishing survey and prospection mission over the Pacific Ocean, carrying two pilots. There was sufficient fuel on board for a 7,5-hour flight. While cruising by night, the aircraft entered an uncontrolled descent and crashed in the sea about 30 km northwest of El Loa. Few debris were found floating on water the following morning. Both occupants were killed.
Probable cause:
A loss of control in flight for unknown reasons.
Final Report:

Crash of a Piper PA-42-720 Cheyenne III off Grand Case: 4 killed

Date & Time: May 5, 2012 at 0240 LT
Type of aircraft:
Registration:
F-GXES
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Grand Case - Fort-de-France
MSN:
42-8001043
YOM:
1980
Flight number:
TIF520
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
3
Pax fatalities:
Other fatalities:
Total fatalities:
4
Captain / Total flying hours:
3950
Captain / Total hours on type:
513.00
Aircraft flight hours:
7593
Aircraft flight cycles:
7830
Circumstances:
The twin engine aircraft was engaged in an ambulance flight between Grand Case and Fort-de-France and was carrying a pilot, a nurse, a doctor and a patient, a Greek citizen in honeymoon in Saint Martin who suffered a heart attack. He normally should be transferred to Fort-de-France from Saint Martin-Princess Juliana Airport with another Operator but the aircraft suffered technical problem prior to departure and the patient was transferred to Grand Case Airport. Piper PA-42 left Grand Case-L'Espérance runway 12 at 02H39. One minute later, during initial climb, it lost height and crashed into the Caribbean Sea, some three NM off the airport, off Tintamarre Island. Around 1000LT in the morning, a wheel and some others debris were found floating in water and no trace of the four occupants was found. They were later considered as deceased.
Probable cause:
The French BEA said in its final report that no technical anomaly to affect significantly the performance of the airplane or its pitch control could be demonstrated. It appears that the pilot had consumed alcohol before the flight and was awake since 0630LT and did not sleep over 20 hours, which could affect his capabilities. In conclusion, the investigation did not determine the cause of the accident, but the following factors may have contributed:
- aircraft's operation with one pilot only,
- absence of regulation does not allow the Civil Aviation Authority to ensure the adequacy of the operational objectives of an operator and its capacity to maintain its activity. This failure could not ensure that the pilot was able to conduct the flight.
- the presence of a flight recorder would probably help to understand the circumstances of the accident with more precision. Important data failed to the investigation, which was not able to identify all possible measures to avoid a similar accident in the future.
Final Report:

Crash of a Cessna 421C Golden Eagle III in the Gulf of Mexico: 1 killed

Date & Time: Apr 19, 2012 at 1208 LT
Operator:
Registration:
N48DL
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
Slidell - Sarasota
MSN:
421C-0511
YOM:
1978
Country:
Region:
Crew on board:
1
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
1
Captain / Total flying hours:
2350
Aircraft flight hours:
4659
Circumstances:
According to a statement provided by the Jacksonville Center air traffic control (ATC) facility, the pilot contacted ATC while at flight level 270. About 25 minutes later, the airplane began to deviate from the ATC-assigned altitude and route. The controller’s attempts to contact the pilot were unsuccessful. The North American Aerospace Defense Command launched military fighter aircraft to intercept the airplane. The military pilots reported that the airplane was circling in a left turn at a high altitude and low airspeed and that its windows were partially frosted over. They also reported that the pilot was slumped over in the cockpit and not moving. They fired flares, and the pilot continued to be unresponsive. The airplane circled for about 3 hours before it descended into the Gulf of Mexico and sank. The pilot and airplane were not recovered. Review of the pilot’s Federal Aviation Administration medical records did not reveal any recent medical conditions that would have deemed him unfit to fly.
Probable cause:
Pilot incapacitation, which resulted in the pilot’s inability to maintain airplane control and the airplane’s subsequent ocean impact.
Final Report:

Crash of a Beechcraft C90GTi King Air off Oranjestad

Date & Time: Apr 3, 2012 at 0920 LT
Type of aircraft:
Operator:
Registration:
N8116L
Flight Phase:
Flight Type:
Survivors:
Yes
Schedule:
Wichita - Fort Lauderdale - Willemstad - Belo Horizonte
MSN:
LJ-2042
YOM:
2011
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
11700
Captain / Total hours on type:
2600.00
Copilot / Total flying hours:
3649
Copilot / Total hours on type:
33
Aircraft flight hours:
14
Circumstances:
On April 3, 2012, about 0920 atlantic standard time (ast), a Hawker Beechcraft C90GTx, N8116L, operated by Lider Taxi Aereo, was substantially damaged after ditching in the waters of the Caribbean Sea, 17 miles north of Aruba, following a dual loss of engine power during cruise. The flight departed Fort Lauderdale Executive Airport (FXE), Fort Lauderdale, Florida, and was destined for Hato International Airport (TNCC), Willemstad, Curacao. The airline transport pilot and the pilot rated passenger were uninjured. Visual meteorological conditions prevailed, and an instrument flight plan was filed for the delivery flight conducted under 14 Code of Federal Regulations Part 91. The Amsterdam arrived at the ditching location at 1120. The airplane was partially submerged. The crew of the Amsterdam attempted to prevent the airplane from sinking by placing a cable around it and hoisting it onboard. However during the attempted recovery, the fuselage broke in half and the airplane sank.
Probable cause:
Review of the fuel ticket revealed that the misspelled words; "Top Neclles" was handwritten on it. It was also signed by the pilot. Further review revealed that only 25 gallons had been uploaded to the airplane, and this number had been entered in the box labeled "TOTAL GALLONS DELIVERED". Review of the start reading and end reading from the truck meter also concurred with this amount. Furthermore, It was discovered that the "134 gallons" that the pilot believed had been uploaded to the airplane was in fact the employee number of the fueler that had topped off the nacelle tanks and had entered his employee number on the "FUEL DEL BY:" line. Utilizing the information contained on the fuel ticket, it was determined that the airplane had departed with only 261 gallons of fuel on-board. Review of performance data in the POH/AFM revealed that in order to complete the flight the airplane would have needed to depart with 328 gallons on-board.
Final Report:

Crash of a Convair CV-440-38 in San Juan: 2 killed

Date & Time: Mar 15, 2012 at 0738 LT
Operator:
Registration:
N153JR
Flight Phase:
Flight Type:
Survivors:
No
Schedule:
San Juan - Sint Marteen
MSN:
117
YOM:
1953
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
0
Pax fatalities:
Other fatalities:
Total fatalities:
2
Captain / Total flying hours:
22586
Captain / Total hours on type:
9000.00
Copilot / Total flying hours:
2716
Copilot / Total hours on type:
700
Circumstances:
The airplane, operated by Fresh Air, Inc., crashed into a lagoon about 1 mile east of the departure end of runway 10 at Luis Muñoz Marín International Airport (SJU), San Juan, Puerto Rico. The two pilots died, and the airplane was destroyed by impact forces. The airplane was operated under the provisions of 14 Code of Federal Regulations (CFR) Part 1251 as a cargo flight. Visual meteorological conditions prevailed at the time of the accident, and a visual flight rules flight plan was filed. The flight had departed from runway 10 at SJU destined for Princess Juliana International Airport, St. Maarten. Shortly after takeoff, the first officer declared an emergency, and then the captain requested a left turn back to SJU and asked the local air traffic controllers if they could see smoke coming from the airplane (the two tower controllers noted in postaccident interviews that they did not see more smoke than usual coming from the airplane). The controllers cleared the flight to land on runway 28, but as the airplane began to align with the runway, it crashed into a nearby lagoon (Laguna La Torrecilla). Radar data shows that the airplane was heading south at an altitude of about 520 ft when it began a descending turn to the right to line up with runway 28. The airplane continued to bank to the right until radar contact was lost. The estimated airspeed at this point was only 88 knots, 9 knots below the published stall speed for level flight and close to the 87-knot air minimum control speed. However, minimum control speeds increase substantially for a turn into the inoperative engine as the accident crew did in the final seconds of the flight. As a result, the airplane was operating close to both stall and controllability limits when radar contact was lost. Pilots flying multiengine aircraft are generally trained to shut down the engine experiencing a problem and feather that propeller; thus, the flight crew likely intended to shut down the right engine by bringing the mixture control lever to the IDLE CUTOFF position and feathering the right propeller, as called out in the Engine Fire In Flight Checklist. This would have left the flight crew with the left engine operative to return to the airport. However, postaccident examinations revealed that the left propeller was found feathered at impact, with the left engine settings consistent with the engine at takeoff or climb setting. The right engine settings were generally consistent with the engine being shut down; however, the right propeller’s pitch was consistent with a high rotation/takeoff power setting. The accident airplane was not equipped with a flight data recorder or a cockpit voice recorder (nor was it required to be so equipped); hence, the investigation was unable to determine at what point in the accident sequence the flight crew shut down the right engine and at what point they feathered the left propeller, or why they would have done so. Post accident examination of the airplane revealed fire and thermal damage to the airframe on the airplane’s right wing rear spar, nacelle aft of the power section, and in the vicinity of the junction between the augmentor assemblies and the exhaust muffler assembly. While the investigation was unable to determine the exact location of the ignition source, it appears to have been aft of the engine in the vicinity of the junction between the augmentor assemblies and exhaust muffler assembly. The investigation identified no indication of a fire in the engine proper and no mechanical failures that would have prevented the normal operation of either engine.
Probable cause:
The flight crew's failure to maintain adequate airspeed after shutting down the right engine due to an in-flight fire in one of the right augmentors. The failure to maintain airspeed resulted in either an aerodynamic stall or a loss of directional control.
Final Report:

Crash of a De Havilland DHC-6 Twin Otter 300 off in Caballococha

Date & Time: Mar 9, 2012 at 1130 LT
Operator:
Registration:
FAP-317
Flight Type:
Survivors:
Yes
Schedule:
Iquitos - Caballococha
MSN:
324
YOM:
1971
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
9
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The seaplane landed hard in the Caballococha's Laguna. Upon landing on water, the right float was torn off, the aircraft overturned and sank. All 11 occupants were rescued and the aircraft was damaged beyond repair. It was performing a flight from Iquitos on behalf of the 42nd Group of the Peruvian Air Force.

Crash of a Cessna 402B off Punto Fijo

Date & Time: Feb 9, 2012 at 1200 LT
Type of aircraft:
Operator:
Registration:
YV2663
Flight Type:
Survivors:
Yes
Schedule:
Valera - Punto Fijo
MSN:
402B-1024
YOM:
1975
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
1
Pax fatalities:
Other fatalities:
Total fatalities:
0
Circumstances:
The twin engine aircraft was performing a cargo flight from Valera-Dr. Antonio Nicolás Briceño Airport to Punto Fijo, carrying one passenger, two pilots and a load consisting of valuables. On approach to Punto Fijo-Josefa Camejo Airport, the crew encountered technical problems and ditched the aircraft off the Amuay refinery. The aircraft sank in shallow water and all three occupants took refuge on the roof of the airplane before being rescued few minutes later.
Probable cause:
The failure of the seal of the balance tube on the left engine intake manifold, causing a loss of manifold pressure and then a loss of engine power.
Contributing Factor:
- Discrepancies found with the quality control of the maintenance services performed on the aircraft,
- The non-assertive decisions taken during the flight when the emergency occurred.

Crash of a Beechcraft F90 King Air off Belém

Date & Time: Feb 8, 2012 at 2244 LT
Type of aircraft:
Operator:
Registration:
PT-OFD
Survivors:
Yes
Schedule:
São Paulo – Belém
MSN:
LA-118
YOM:
1981
Country:
Crew on board:
2
Crew fatalities:
Pax on board:
2
Pax fatalities:
Other fatalities:
Total fatalities:
0
Captain / Total flying hours:
5500
Captain / Total hours on type:
70.00
Copilot / Total flying hours:
6750
Copilot / Total hours on type:
7
Circumstances:
The aircraft departed São Paulo-Congonhas Airport at 1630LT on a flight to Belém, carrying two passengers and two pilots. During the approach to Belém-Val de Cans-Júlio Cezar Ribeiro Airport runway 06 by night, one of the engine flamed out. Few seconds later, the second engine failed as well. The crew ditched the aircraft in the Bay of Guajará, about 1,2 km short of runway 06 threshold. All four occupants were rescued by servicemen of the Naval Base who were on duty at the time of the accident. A pilot was slightly injured while three other occupants escaped uninjured. The aircraft sank and the wreckage was recovered 12 days later.
Probable cause:
The following findings were identified:
a) The pilots had valid aeronautical medical certificates;
b) The pilots had valid technical qualification certificates;
c) The aircraft captain had qualification and enough experience for the flight in question;
d) The copilot was under training;
e) The aircraft had a valid airworthiness certificate;
f) The planning of the flight from SBSP to SBBE was done by the pilot in command, who took in consideration an aircraft with a full load of fuel;
g) The flight plan read that the fuel endurance was 7 hours and 30 minutes of flight, for an estimated elapse time of 5 hours and 40 minutes at FL230;
h) When the aircraft was passing over the city of Palmas, State of Tocantins, the pilots decided, in conjunction, to proceed non-stop to the destination, discarding the need to make an intermediate landing for refueling;
i) The aircraft was registered in the passenger transport category (TPP) and was engaged in the transport of a sick person;
j) The fuel quantity indicators and the fuel flow indicators of the aircraft were not showing dependable information;
k) The flight plan for the leg betwren SBSP and SBBE contained information of sick person transportation, but there was no sick person on board;
l) The aircraft made a ditching near the banks of Guajará Bay, at a distance of approximately 1,200 meters from the threshold of runway 06 of SBBE;
m) The passengers and crew were rescued by Brazilian Navy servicemen on duty on the Naval Base of Val de Cans;
n) One of the pilots and both passengers got out uninjured, while the other pilot suffered minor injuries; and
o) The aircraft sustained substantial damage.
Contributing factors:
Concerning the operation of the aircraft
a) Attitude – a contributor
The captain failed to comply with norms and procedures by accepting to fly an aircraft on his day of rest, even knowing that he was to start his on-call duty hours as soon as he landed in SBBE.
He also showed to be overconfident when he decided to fly directly from SBSP to SBBE, trusting the 7-hour fuel endurance of his aircraft and the fuel consumption information displayed by the instruments, even after identifying their malfunction. The pilot under training, in turn, was complacent by accepting and agreeing with the pilot-in-command’s decision, without questioning his calculations or motivations for flying direct to the destination.
b) Motivation – a contributor
The captain was eager to return to SBBE on that same day, because he was supposed to start his on-call duty hours in the air taxi company for which he worked.
c) Decision-making process – a contributor
The captain failed to comply with important aspects concerning the route conditions and aircraft instruments by making a decision to fly directly from SBSP to SBBE.
Psychosocial information
a) Communication – a contributor
There was lack of assertiveness on the part of the copilot since he did not question the captain’s calculations and/or motivations to fly non-stop, when he (the copilot) considered that making a stop for refueling would be safer.
b) External influence – a contributor
The involvement of the captain with activities of another company on that same day, in addition to events belonging to his private life, had influence on his decisions in the initial planning of the flight and during the flight en route.
Organizational information
a) Work organization – a contributor
The company delegated responsibility for the entire planning of the flight to the pilots. Therefore, there was not any interference on the part of the company in the crew’s work day and in the legs defined for the flight.
b) Organizational culture – a contributor
The fact that the company performed an operation for which it was not certified reflected the fragility of an organizational culture which allowed it to perform activities unfavorable to operational safety.
Operational Factor
Concerning the operation of the aircraft
a) Flight indiscipline – a contributor
On several occasions during the flight, the pilots failed to comply with the norms and regulations in force, such as the sections 91.167 and 91.205 of the RBHA 91, the Pilot Operating Handbook and FAA Approved Airplane Flight Manual, and the Lei do Aeronauta (Law of the Aeronaut, Law nº 7.183 of 5 April 1984).
b) Training – undetermined
Before the ditching, the pilot unlocked the rear door of the aircraft and, then, failed to instruct the passengers as to the opening of the emergency exit. This fact shows a probable deviation in the process of training previously received by the captain, since the procedure prescribed for the situation was to abandon the aircraft through the emergency exit, which had to be unlocked after the ditching.
c) Piloting judgment – a contributor
At the moment of their decision to proceed non-stop to the destination, there was an inappropriate evaluation on the part of the crew, because they did not consider the hourly consumption until that point, and the malfunction of the fuel capacity indicator did not allow them to know the exact amount of fuel remaining in the tanks.
d) Flight planning – a contributor
There was a mistake on the part of the captain relative to the planning of the flight, since, in addition to a total flight time of 5 hours and 40 minutes, he did not consider the fuel necessary to fly to an alternate airport plus 45 minutes of flight. The captain and the pilot under training made an inappropriate evaluation of the effects brought by the operational conditions along the flight route.
Final Report: