HB-AAM
2000-JAN-13 · Off Marsa Brega, Libya

Sirte Oil Company — Flight HB-AAM

On January 13, 2000, a Shorts 360-300 operated by Sirte Oil Company ditched into the Mediterranean Sea approximately 5 kilometers (3.1 miles) off Marsa Brega after both engines flamed out during descent. The investigation determined that the flight crew failed to activate the engine anti-icing system while flying through icing conditions. As the aircraft descended into warmer air, ice that had accumulated in the engine intakes melted and was ingested, causing a double flameout. The crew was distracted by a non-pertinent conversation regarding the operating systems and flight techniques of a Fokker F28 aircraft—a type also operated by the company—leading to a fatal breakdown in situational awareness. Of the 41 people on board, 22 perished (21 confirmed dead and one missing, presumed dead), including the cabin crew member.

Aircraft
Shorts 360-300
Registration
HB-AAM
Phase
Cause
Souls on Board
41
Fatalities
22
Origin → Dest
Tripoli International Airport (TIP) → Marsa Brega Airport (LMQ)
Report

Investigation Summary

The flight was a routine employee transport service leased from the Swiss firm Avisto. During the cruise at FL070, the aircraft encountered meteorological conditions conducive to icing, with outside air temperatures around -6°C. Although the crew noticed ice forming on the windshield and activated the windshield and pitot anti-icing systems, they neglected to turn on the engine anti-icing. Cockpit Voice Recorder (CVR) data revealed the pilots were deeply engaged in a technical discussion about the Fokker F28, an aircraft also operated by the company, which distracted them from monitoring engine parameters. As the aircraft descended toward Marsa Brega, it passed through the freezing level (approximately 5,200 feet). The sudden melting of accumulated ice led to massive water ingestion in both Pratt & Whitney Canada PT6A-67R engines. The left engine flamed out first, followed shortly by the right. The crew failed to activate the engine ignition system, which could have provided continuous ignition to prevent the flameout or facilitate an immediate relight. The crew attempted to ditch the aircraft, but the impact destroyed the nose and caused the tail to detach, leading the wreckage to sink rapidly in 38 meters of water. Survival was further compromised by a lack of lifejackets and the fact that many passengers were unaware that their seat cushions were designed to be used as flotation devices.

Final Conclusions

The Libyan Civil Aviation Authority concluded the primary cause was the melting of ice formed at the engine intakes, resulting in water ingestion and subsequent double engine flameout. Contributing factors included the flight crew's failure to operate the engine anti-icing system and their engagement in a discussion not relevant to the flight, which detracted from their monitoring of the aircraft's condition.

Video Analysis

No video analysis linked for this case file yet.

Airframe & Maintenance

Airframe Hours
7,138
Engines
Pratt & Whitney Canada PT6A-67R

Crew Experience

Captain

Total hours
8,814
On type
3,840

Libyan national, aged 42.

First Officer

Total hours
10,422
On type
1,950

Libyan national, aged 49.

Systems & Failure Modes

i

Engine Anti-Icing

A system designed to prevent ice buildup in the engine intakes; its non-use led to ice accumulation and subsequent water ingestion.

i

Engine Ignition System

A system that, if activated, provides continuous ignition to prevent flameouts in heavy precipitation or icing; the crew failed to use this to attempt a relight.

i

GPWS

The Ground Proximity Warning System activated during the final descent after the total loss of engine power as the aircraft approached the water in an unsafe flight condition.

i

PT6A-67R Engines

The turboprop engines flamed out after ingesting water from melted ice accumulated during the flight.

Interesting Facts

  • 01The aircraft was leased from Swiss operator Avisto Air Service.
  • 02The freezing level at the time of the accident was approximately 5,200 feet.
  • 03There were no lifejackets on board the aircraft.
  • 04The wreckage sank to a depth of 38 meters about 5 kilometers (3.1 miles) from the coast.
  • 05Both the Captain and First Officer survived the ditching.
  • 06The 22 fatalities include 21 confirmed dead and one person missing, presumed dead.
  • 07Due to a company shortage of first officers, the flight was operated by two captains, though one served in the First Officer role.
  • 08The 41 souls on board included 16 Libyans (including 2 crew), 13 Britons, 3 Indians, 3 Filipinos, 2 Canadians, 2 Croatians, 1 Pakistani, and 1 Tunisian (crew).

Safety Actions & Advisories

Ditching Procedures Review

Investigators recommended the inclusion of correct ditching techniques in zero-flaps conditions following a total loss of power in training manuals.

Passenger Safety Briefings

Recommendations were made to ensure passengers are clearly informed of the flotation capabilities of seat cushions when lifejackets are not provided.

Known Controversies & Unanswered Questions

Absence of Lifejackets

Reference ↗

The investigation highlighted a significant safety oversight: the aircraft was not equipped with lifejackets despite operating over water. This led to several drownings as passengers were unaware that seat cushions were intended for flotation.

Crew Distraction and CRM

Reference ↗

The CVR revealed the crew spent a significant portion of the flight discussing the Fokker F28, a different aircraft type. This non-pertinent conversation was cited as a primary reason for their failure to notice icing conditions and engine parameter changes.

Location

Off Marsa Brega, Libya · 30.3960, 19.4693

Case File History

  1. New evidenceUpdated event timeline and findings.
  2. New evidenceUpdated event timeline and findings.
  3. New evidenceUpdated event timeline, investigation summary, systems analysis and open questions.

Related Cases

Case ID · marsa-brega-2000Last updated · Filed

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