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Accident description
Last updated: 29 May 2016
Date:Thursday 24 July 2014
Type:Silhouette image of generic MD83 model; specific model in this crash may look slightly different
McDonnell Douglas DC-9-83 (MD-83)
Operating for:Air Algérie
Leased from:Swiftair
Registration: EC-LTV
C/n / msn: 53190/2148
First flight: 1996
Total airframe hrs:38362
Engines: 2 Pratt & Whitney JT8D-219
Crew:Fatalities: 6 / Occupants: 6
Passengers:Fatalities: 110 / Occupants: 110
Total:Fatalities: 116 / Occupants: 116
Airplane damage: Destroyed
Airplane fate: Written off (damaged beyond repair)
Location:80 km (50 mls) NW of Gossi (   Mali)
Phase: En route (ENR)
Nature:International Scheduled Passenger
Departure airport:Ouagadougou Airport (OUA/DFFD), Burkina Faso
Destination airport:Algiers-Houari Boumediene Airport (ALG/DAAG), Algeria
A McDonnell Douglas MD-83 passenger plane, registration EC-LTV was destroyed when it crashed 80 km northwest of Gossi, Mali. All 116 occupants sustained fatal injuries.
The airplane was operated by Spanish airline Swiftair on behalf of Air Algérie as flight AH5017 from Ouagadougou, Burkina Faso to Algiers, Algeria.
Flight AH5017 took off from runway 22 at Ouagadougou Airport (OUA) at 01:15 UTC (and local time). Following a right turn after takeoff the aircraft headed to the EPOPO point and started climbing to the planned cruising altitude of FL310.
At an altitude of about 10,500 ft, autopilot 1 was engaged, the autothrottle having been active since takeoff. Nine minutes after takeoff, the crew said that they were passing through FL145 and that they estimated EPEPO point at 01:38.
At 01:28, the airplane was transferred to the Ouagadougou CCR and the crew said that they were turning to the left on heading 356° to avoid an bad weather in the area.
During the climb towards FL310, the crew made three heading alterations to the left (of 28°, of 4° then of 8°), then an alteration to the right of 36° to return to heading 019°, close to the initial heading.
At 01:37, the airplane levelled off at FL310 at Mach 0.740. The autopilot then maintained the altitude and heading, while the speed was controlled by the autothrottle. At the same time, the airplane was transferred to the Niamey CCR. In the two minutes following level-off, the airplane's speed increased.
From 1 h 38 min 34, and for about 30 seconds, the autothrottle was in MACH ATL mode. This mode automatically engaged because the thrust needed to reach the Mach speed selected by the pilots was greater than the EPR limit.
The engines' EPR stabilised around 1.92 and the Mach changed from 0.758 to 0.762. The autothrottle then returned to MACH mode and the airplane continued to accelerate up to Mach 0.775.
At 01:39:36, the airplane's speed started to decrease. About one minute later the autothrottle changed back to MACH ATL while the Mach was 0.752. Following that, the altitude remained stable, pitch and EPR increased progressively, while the engines' N1 remained stable and the speed continued to decrease.
Between 01:41:38 and 01:44:29, the Niamey CCR and flight AH5017 tried to get in contact, but did not manage to do so. Flight RAM543K offered to act as the intermediary. The crew of flight AH5017 said, at 01:44:29, that they were at FL310 on a weather avoidance manoeuvre. The Niamey CCR heard this radio exchange and asked them to call back passing GAO and to transmit estimates for MOKAT point. No answer, nor any other messages from flight AH5017, reached the Niamey CCR.
At 01:44, EPR and N1 fluctuations on both engines appeared for about 45 seconds. Then, for about 25 seconds, the EPR decreased then increased again on two occasions from 1.6 to about 2.5. The N1s varied between 70% and 91%. Some roll oscillations between 4° to the left and to the right appeared. The autothrottle disengaged between 01:45:02 and 01:45:06. This disengagement occurred between the first and second EPR variations.
At 01:45:06, the calibrated airspeed was 203 kt, the Mach 0.561 and the airplane started to descend. Pitch increased until it reached 10° at 01:45:17, then decreased slightly while the deflection of the elevators and the position of the trimmable horizontal stabiliser continued pitching up. The EPR and the engines' RPM started to decrease towards values corresponding to idle. The roll oscillations continued and the speed continued to decrease.
At 01:45:35, the autopilot disengaged. The altitude decreased by about 1,150 ft in relation to the flight level, the calibrated airspeed was 162 kt, the Mach 0.439 and both engines were almost at idle. The airplane's pitch began to decrease and the bank was increasing to the left.
The airplane's pitch and bank were then subject to significant changes. They reached, respectively, 80° nose-down and 140° bank to the left. The airplane was pitched nose-down and banked to the left until it struck the ground. The heading decreased continuously and the flight control surfaces remained mainly deflected pitch-up and in the direction of a bank to the right. Around twenty seconds before the impact, the engine speed and EPR increased again and reached values close to maximum thrust.

Analysis of the recorded parameters by the flight data recorder, indicates that about two minutes after the leveling off at FL310, the engine pressure ratio (EPR) value became become incoherent in relation to other engine parameters. This anomaly occurred on the right engine and about 55 seconds later on the left engine. These false readings were probably caused by an obstruction of the pressure sensors located on the nose cone of the engine, presumably by icing. This icing may have been caused by the presence of cold, moist air on the edge of the storm cell, considering the fact that none of the anti-icing systems were activated.
Due to the incorrect values, the auto-throttle tried to maintain a lower thrust than was necessary. The aircraft lost speed and developed a tendency to descend. The autopilot, engaged in altitude hold mode, then attempted to raise the nose in order to maintain altitude. The aircraft ultimately stalled.

Causes (translated from French):
The speed of the aircraft, controlled by the auto-throttle, decreased due to clogging of the pressure sensors located on the nose cone of the engines, presumably by ice crystals. The autopilot then gradually increased the attitude of the aircraft to maintain altitude until the aircraft stalled. The stall of the aircraft was not recovered. The plane descended in a nose down attitude and a left bank while the rudders remain largely steered in the direction of a bank to the right. The plane hit the ground at high speed.
The accident resulted from the combination of the following:
- Non-activation of engine anti-icing systems;
- Clogging of pressure sensors Pt2, presumably by ice crystals, resulting in erroneous EPR values which caused the auto-throttle to limit the thrust delivered by the engines to a level lower than the thrust needed to maintain FL310;
- Late reaction from the crew at the decrease in speed and erroneous EPR values, possibly related to the crew workload associated with the avoidance of convective zone and communication difficulties with air traffic control;
- The lack of reaction from the crew to the appearance of the buffet, the stick shaker and the stall warning;
- The absence of appropriate action on the flight controls to exit a stall situation.

These events can find their explanations in the combination of the following factors:
- FCOM procedure for activating anti-icing systems was not adapted to the situation of blockage of Pt2 sensors by ice crystals;
- Insufficient information for operators on the consequences of blocking of the Pt2 sensor by an icing phenomenon;
- The trigger logic of the stick shaker and stall alarm that led these devices to trip late to the stall of the aircraft in cruise;
- The logic of the autopilot allowing it to continue to give orders to pitch beyond the impact of stall aggravating the situation leaving and increasing the difficulty of recovery by the crew.

Lack of usable CVR recording limited the possibilities to analyse the crew behavior during the flight.
In particular it was not possible to study aspects CRM or to assess the potential contribution of the employment framework and experience of the crew.

Loss of control (presumed)

» Swiftair statement

METAR Weather report:
01:00 UTC / 01:00 local time:
DFFD 240100Z 23008KT 9999 FEW020 BKN100 26/23 Q1015 NOSIG

02:00 UTC / 02:00 local time:
DFFD 240200Z 22006KT 9999 TS FEW020 FEW033CB BKN100 25/23 Q1014 TEMPO 4000 TSRA
Wind 220 degrees at 6 knots; Visibility 10+ km; Thunderstorm; few clouds at 2000 feet AGL few CB clouds at 3300 feet AGL; broken clouds at 10000 feet AGL; Temperature 25°C; Dewpoint: 23°C; Pressure 1014 mb

Official accident investigation report
investigating agency: Commission d’Enquete sur les Accidents et Incidents d’Aviation Civile - Mali
report status: Final
report number: Final report
report released:22 April 2016
duration of investigation: 1 year and 9 months
download report: Accident on 24 July 2014 in the region of Gossi in Mali to the MD-83 registered EC-LTV operated by Swiftair S.A. (CEAIAC Final report)

Follow-up / safety actions

EASA issued 1

Show all AD's and Safety Recommendations


photo of McDonnell Douglas MD-83 EC-LTV
EC-LTV operating on Air Algérie flight 1021 to Algiers
photo of McDonnell Douglas MD-83 EC-LTV
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Aircraft history
date registration operator remarks
June 1996 SU-ZCA McDonnell Douglas first flight
23 August 1996 SU-ZCA Heliopolis Airlines delivered
9 December 1997 N190AN AWAS
13 February 1998 HK-4137X Avianca registered
17 August 2000 N190AN Avianca re-registered
30 June 2004 N190AN Avianca Main gear tire tread separated on takeoff; loss of power on left engine; returned to land
10 December 2004 N190AN Avianca Contained left engine failure during climb at 15.000 feet due to T3/T4 blade failure
22 December 2006 N190AN AWAS returned
19 January 2007 LV-BHN Austral Líneas Aéreas delivered
15 May 2008 LV-BHN Austral Líneas Aéreas stored
28 August 2008 LV-BHN Austral Líneas Aéreas returned to service
01 February 2012 LV-BHN Austral Líneas Aéreas stored
30 March 2012 N190AN AWAS returned
24 October 2012 EC-LTV Swiftair bought (remained stored)
04 December 2012 EC-LTV Swiftair ferry flight to new storage location
01 January 2013 EC-LTV Swiftair ferry flight to new storage location
27 February 2013 EC-LTV Swiftair Issue of registration certificate; operated flights for a.o. CCM, Vueling, Jetairfly, RAM and others
20 June 2014 EC-LTV Swiftair ACMI charter to Air Algérie

This map shows the airport of departure and the intended destination of the flight. The line between the airports does not display the exact flight path.
Distance from Ouagadougou Airport to Algiers-Houari Boumediene Airport as the crow flies is 2732 km (1708 miles).

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