226A
1999-SEP-14 · Girona–Costa Brava Airport, Spain

Britannia Airways — Flight 226A

Britannia Airways Flight 226A crashed during a second landing attempt at Girona Airport during a severe thunderstorm. After a destabilized approach in torrential rain, the airport's runway lighting failed for 11 seconds just as the aircraft reached 250 feet. The captain, losing visual reference, pushed the nose down, leading to a high-G impact that bounced the aircraft and damaged its electrical systems. The second impact caused the nose gear to collapse and triggered an uncommanded increase in engine thrust. The aircraft veered off the runway, broke into three sections, and came to rest in a field. While all occupants initially survived the impact, one passenger died five days later from internal injuries.

Aircraft
Boeing 757-204
Registration
G-BYAG
Phase
Cause
Souls on Board
245
Fatalities
1
Origin → Dest
Cardiff Airport, Wales → Girona–Costa Brava Airport, Spain
Report

Investigation Summary

The accident sequence began with a series of operational challenges during a night approach in convective weather. During the first approach to Runway 02, the aircraft was struck by lightning on the left wing, and the captain inadvertently left the speed brakes extended for 14 minutes, which increased fuel consumption and workload. After a missed approach due to a sudden tailwind shift, the crew faced a tightening fuel margin and elected to attempt an ILS approach to Runway 20. During this second attempt, a lightning strike on the airport's power infrastructure caused a total failure of the runway lighting at a critical height of 250 feet. The captain, experiencing a loss of visual cues and potentially affected by the 'black hole' effect or mental shock, applied significant nose-down elevator. The aircraft struck the runway at 3.11g in a nose-down attitude. This impact caused the nose landing gear to collapse upward, severing wiring looms in the electronics bay. The resulting short circuits caused the autothrottle to command an increase in thrust to 1.18 EPR on both engines, despite the crew's attempts to decelerate. The aircraft traveled through a perimeter fence and over an earth mound before breaking apart in a field.

Final Conclusions

The CIAIAC concluded the probable cause was the destabilization of the approach below decision height following the loss of external visual references and automatic height callouts. The failure of the runway lights at the most critical moment of the landing was a primary contributing factor. The investigation also highlighted the uncommanded forward thrust increase caused by system damage during the first impact, which prevented the aircraft from stopping on the runway. Other factors included the crew's insufficient evaluation of the storm's severity and the lack of specific simulator training for initiating a go-around below decision height.

Video Analysis

Britannia Airways 226A Accident: A Boeing 757, a Storm, and 11 Critical Seconds — A detailed breakdown of the 1999 crash at Girona, examining how a thunderstorm, a sudden power failure, and mechanical malfunctions led to the destruction of a Boeing 757.

If playback is blocked, the owner has disabled embedding — use the link above.

Airframe & Maintenance

Airframe Hours
26,429
Cycles
9,816
Engines
Rolls-Royce RB211-535E4

Crew Experience

Captain

Total hours
16,700
On type
3,562

Brendan Nolan, 57 years old

First Officer

Total hours
1,494
On type
1,214

33 years old

Systems & Failure Modes

i

Runway Lighting

The airport lighting system failed due to a storm-related power surge, depriving the pilots of visual orientation at the moment of flare.

i

Autothrottle / EEC

Damage to the electronics bay during the first impact caused the engines to increase thrust to 1.18 EPR, fighting the crew's braking efforts.

i

GPWS

Automatic height callouts were suppressed by a 'SINK RATE' audio caution, leaving the crew without altitude awareness in the darkness.

Interesting Facts

  • 01The runway lights were dark for exactly 11 seconds due to a lightning strike on the power grid.
  • 02The initial impact recorded a peak vertical acceleration of 3.11g.
  • 03The aircraft was structurally severed at two points but no fire broke out.
  • 04The sole fatality was a passenger who died five days later from unsuspected internal injuries.
  • 05The captain had over 16,000 flight hours, while the first officer had approximately 1,500 hours.

Safety Actions & Advisories

Simulator Training

Recommendations were made to include simulator training for go-arounds initiated below decision height, even after touchdown.

Airport Infrastructure

Improvements to the reliability and backup speed of airport emergency lighting systems were recommended.

Location

Girona–Costa Brava Airport, Spain · 41.8991, 2.7557

Case File History

  1. CorrectionUpdated investigation summary.

Related Cases

Case ID · britannia-226a-1999Last updated · Filed

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