No fatalities

Engine Surge Leads to Aborted Take-off of Boeing 747-400 at Cape Town (G-BNLB)

On Runway 01 at Cape Town International Airport, ZA

On July 24, 2006, a BOEING B747-400 (registration G-BNLB) was involved in an aviation accident near On Runway 01 at Cape Town International Airport, ZA. No fatalities were reported. Investigators recorded the probable cause as: The cause of the engine surge was found attributable to the increased compressor blade tip clearances throughout the HP (High Pressure) Compressor module which had increased by 0.02 to 0.04 inches, which during engine operation could manifest itself in an… This summary draws on records from the South African Civil Aviation Authority (SACAA) Accident and Incident Investigations Division.

Sourcesthe South African Civil Aviation Authority (SACAA) Accident and Incident Investigations DivisionPrimary reportUpdated 2026-10-18Data APIEditorial standards
Aircraft registered G-BNLB
Aircraft registered G-BNLB. Photo: lkarasawa / CC BY 2.0, via Wikimedia Commons

During take-off at Cape Town International Airport, a Boeing 747-400 experienced an engine surge, prompting an aborted departure. No injuries occurred, and the aircraft returned to the parking bay.

Synopsis

On 24 July 2006, a Boeing 747-400 registered as G-BNLB, operating as flight BAW58L from Cape Town International Airport (FACT) to London Heathrow International Airport (EGLL), initiated its take-off roll on Runway 01. During the roll, the cockpit crew heard a loud bang from the left side of the aircraft. Air Traffic Control immediately informed the crew that flames were observed emanating from engine number one. The crew aborted the take-off at an indicated airspeed of 100 knots, approximately 1000 meters from the runway threshold where the take-off began, and brought the aircraft to a stop on the runway.

Event Details

After the abort, fire services inspected the engine, main landing gear, and all brake assemblies. The aircraft then taxied back to the parking bay, where the crew and passengers disembarked normally. There were no injuries during the incident.

Investigation Findings

The incident aircraft had previously experienced a compressor stall on its initial flight from London Heathrow to Cape Town. All four engine parameters were normal, and the crew continued the flight without further issues. Upon arrival at Cape Town, South African Airways technicians conducted a boroscope inspection of engine number one. They noted slight damage to a stator blade in the compressor module, which was deemed within acceptable limits. The engine underwent a ground test that performed satisfactorily, and the aircraft was released for service.

The investigation determined that the engine surge during the take-off was attributable to increased compressor blade tip clearances throughout the High Pressure (HP) Compressor module. These clearances had increased by 0.02 to 0.04 inches, which could manifest as an engine surge or stall during take-off.

Probable cause

The cause of the engine surge was found attributable to the increased compressor blade tip clearances throughout the HP (High Pressure) Compressor module which had increased by 0.02 to 0.04 inches, which during engine operation could manifest itself in an engine surge/stall during take off

Frequently asked questions

What happened in the 24 Jul 2006 BOEING B747-400 accident near On Runway 01 at Cape Town International Airport, ZA?

During take-off at Cape Town International Airport, a Boeing 747-400 experienced an engine surge, prompting an aborted departure. No injuries occurred, and the aircraft returned to the parking bay.

Were there any fatalities in the 24 Jul 2006 BOEING B747-400 accident?

No fatalities were recorded in this accident.

What aircraft was involved and where did it happen?

The accident on 24 Jul 2006 involved a BOEING B747-400, registration G-BNLB, at On Runway 01 at Cape Town International Airport, ZA.

What was the probable cause of the accident?

The cause of the engine surge was found attributable to the increased compressor blade tip clearances throughout the HP (High Pressure) Compressor module which had increased by 0.02 to 0.04 inches, which during engine operation could manifest itself in an engine surge/stall during take off