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| Title: | Landing gear fire during touch-and-gos, Boeing 757-236, G-BMRE |
| Micro summary: | While this Boeing 757-236 was performing touch-and-gos, flames were seen emanating from the landing gear. |
| Event Time: | 2005-07-30 at 0819 UTC |
| File Name: | 2005-07-30-UK.pdf |
| Publishing Agency: | Aircraft Accident Investigation Board (AAIB) |
| Publishing Country: | United Kingdom |
| Report number: | EW/G2005/07/37 |
| Pages: | 6 |
| Diversion Airport: | Nottingham East Midlands Airport, Leicestershire, England |
| Site of event: | Nottingham East Midlands Airport |
| Departure: | Nottingham East Midlands Airport, Leicestershire, England |
| Destination: | Nottingham East Midlands Airport, Leicestershire, England |
| Airplane Type(s): | Boeing 757-236 |
| Flight Phase: | Landing |
| Registration(s): | G-BMRE |
| Operator(s): | British Airways |
| Type of flight: | Revenue |
| Occupants: | 4 |
| Fatalities: | 0 |
| Serious Injuries: | 0 |
| Minor/Non-Injured: | 4 |
| Other Injuries: | 0 |
| Diverted to: | Nottingham East Midlands Airport, Leicestershire, England |
| Executive Summary: | The aircraft had been positioned at Nottingham East Midlands Airport early in the morning of 30 July 2005, following which various maintenance activities took place, including changing the No 3 wheel brake unit. The aircraft subsequently took off to fly training circuits but, on the second touch-and-go, the Control Tower advised the crew that flames were seen to be coming from the right main landing gear. The commander elected to continue the touch-and-go and to fly a circuit with the landing gear down, as he was concerned about stopping the aircraft in the runway distance remaining. After a successful landing, the aircraft was brought to a stop on the runway and inspected by the fire service, prior to being towed to a stand. The fire was later attributed to a failure in the No 3 brake unit. This was caused by the end cap of the brake torque rod not being refitted during the maintenance activity, thus allowing one end of the brake torque rod to become detached and scrape along the ground during the landing. The brake unit rotated with the wheel during the rollout, causing damage to the wheel, severance of the brake hose and damage to the brake temperature monitoring components. |
| Learning Keywords: | Systems - Brake/Tire/Wheel Well Fire |
| Systems - Landing Gear |
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