QY5960
2024-NOV-25 · Zirniu Street, Liepkalnis, Vilnius, Lithuania

Swiftair — Flight QY5960

A Boeing 737-400SF cargo aircraft crashed into a residential area approximately 1.5 kilometers short of the runway during a night approach to Vilnius. The accident sequence began when the captain accidentally deactivated both hydraulic system B pumps while attempting to engage engine anti-ice, leading to an autopilot disconnect. Despite Hydraulic System A remaining functional and capable of operating the flaps, the crew failed to extend them. Suffering from a breakdown in resource management and situational awareness, the crew failed to complete landing checklists and misdialed air traffic control frequencies. The aircraft attempted a high-speed, flaps-up landing and impacted terrain during a late go-around attempt. Although the aircraft struck a residential building and caused significant destruction, all 13 occupants of the house were safely evacuated and there were no fatalities on the ground.

Aircraft
Boeing 737-400SF
Registration
EC-MFE
Phase
Approach
Cause
Human Factors (Operational)
Souls on Board
4
Fatalities
1
Origin → Dest
Leipzig/Halle Airport, Germany → Vilnius International Airport, Lithuania
Report
Interim

Investigation Summary

The investigation revealed a critical ergonomic and procedural failure. On the Boeing 737 overhead panel, the engine anti-ice switches are located in close proximity to the hydraulic system B pump switches. Approximately 13 minutes before impact, the captain mistakenly flipped the hydraulic switches. While Hydraulic System B was deactivated, Hydraulic System A remained functional, meaning the trailing edge flaps were still available for use. However, the crew failed to recognize that the flaps had not extended despite moving the flap lever. This resulted in an unstabilized approach at speeds significantly higher than normal for the configuration. Compounding the technical error, the crew lost communication with the tower after mistuning the radio frequency and failed to perform the landing checklist, which would have alerted them to the incorrect flap setting. The co-pilot only realized the flaps were at zero degrees 12 seconds before impact, triggered by the stick shaker and EGPWS warnings.

Final Conclusions

The interim report indicates the crash was caused by a chain of human errors including accidental system deactivation, failure to follow standard operating procedures (SOPs), and poor crew resource management. The aircraft was in a non-standard, high-speed configuration for landing, and the crew's late recognition of the state prevented a successful recovery during the go-around.

Photographic Evidence (1)

© Wikimedia Commons

Video Analysis

No video analysis linked for this case file yet.

Airframe & Maintenance

Airframe Hours
63,573
Cycles
43,745
Engines
CFM International CFM56-3C1

Crew Experience

Captain

Total hours
5,432
On type
1,298

48-year-old male; also had ATR-72 experience.

First Officer

Total hours
520
On type
190

34-year-old male; pilot flying at the time of the accident.

Systems & Failure Modes

i

Hydraulic System B

Provides pressure for trailing edge flaps and other flight controls; its accidental deactivation led to the flaps-up configuration.

i

Engine Anti-Ice

System intended to prevent ice buildup; the proximity of its switches to hydraulic controls led to the initial error.

i

EGPWS

Enhanced Ground Proximity Warning System provided 'Sink Rate' and 'Pull Up' alerts seconds before impact.

Interesting Facts

  • 01The aircraft was a 31-year-old Boeing 737-400SF converted freighter.
  • 02The captain was killed, while the co-pilot and two supernumerary crew members (cargo attendants) survived with injuries.
  • 03Hydraulic System B deactivation occurred, but trailing edge flaps remained available via System A; however, the crew never extended them.
  • 04The crew failed to complete the landing checklist during the approach.
  • 05According to news reports, all 13 occupants of the house struck by the aircraft were safely evacuated.
  • 06Preliminary investigation found no evidence of sabotage or foul play.

Safety Actions & Advisories

Interim Investigation Findings

The Lithuanian National Safety Investigation Authority released an interim report within 30 days to highlight the human factors and procedural omissions identified in the early stages of the probe.

Location

Zirniu Street, Liepkalnis, Vilnius, Lithuania · 54.6581, 25.3024

Case File History

  1. New evidenceUpdated findings.
  2. Status changeUpdated report status.

Related Cases

Case ID · swiftair-5960-2024Last updated · Filed

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