| Date: | Saturday 15 June 1996 |
| Time: | 17:44 |
| Type: | Boeing 747-121 |
| Owner/operator: | Corsair |
| Registration: | F-GKLJ |
| MSN: | 19660/50 |
| Year of manufacture: | 1970 |
| Fatalities: | Fatalities: 0 / Occupants: 3 |
| Other fatalities: | 0 |
| Aircraft damage: | Substantial |
| Location: | Cardiff-Wales Airport (CWL/EGFF) -
United Kingdom
|
| Phase: | Standing |
| Nature: | - |
| Departure airport: | |
| Destination airport: | |
| Investigating agency: | AAIB |
| Confidence Rating: | Accident investigation report completed and information captured |
Narrative:The accident occurred as the aircraft was being prepared for handover to the operator following major maintenance. The Flight Data Recorder (FDR) was not running at the time of the incident, but the Cockpit Voice Recorder (CVR) contained a complete record of the event. Security cameras outside the hangar had also recorded the pushback and the incident. Statements were taken from thestaff involved. These were in generally good agreement and togetherwith the recorded information described the following sequence of events leading up to the incident. The aircraft had been on a 'C' check and the Estimated Time to service (ETS) had been delayed from the previous day, due to the workload on the aircraft. It was rescheduled for 1800 hrs local time (L) on the 15th. The task continued to run late, however the dayshift fully expected to deliver the aircraft for service as scheduled, just before the end of their shift at 1800 hrs L, and so no 'handover' had been prepared. During this period the aircraft was under the control of the day shift aircraft controller. At about 1730 hrs L the nightshift began to arrive and having arrived early, began to assist the dayshift.
Prior to the arrival of the night shift, there had been some discussion concerning the landing gear pins. The pins, which had been removed prior to the pushback from the hangar, were re-fitted as required for some work card items which were still outstanding. The workcard items outstanding were, in particular, a function check ofthe landing gear module and nose gear alternate extension checks. In addition, the tug driver was unwilling to push back unless the nose gear pins were in place. At about 1810 hrs L the aircraft was pushed back from the hangar to the apron outside. As the aircraft was being pushed back, an engineer on the night shift team saw the pins in place and queried with two of the day shift controllers whether the pins were the property of the operator or the maintenance organisation. He was advised that they did not belong to the operator, and understood the reply to mean that they could be removed after the aircraft was parked. It is not clear how this understanding arose, however the night shift were generally unaware of the outstanding work card items.
To expedite matters, the loading of freight began and the three members of the operator's flight crew boarded the aircraft in readiness for it to be handed over to them. Although the flightcrew were on board, the Certificate of Release to Service (CRS) had not been signed and the flight crew were not in command of the aircraft. They were, however, on board with the intention of flight as it was understood that, once the CRS was signed the engineers would leave the aircraft and the flight crew would take command. The day shift team leader was seated in the left handseat and was in contact with an engineer on the ground by headset. A number of other engineering personnel were around the aircraft, including several night shift personnel Prior to carrying out the landing gear functions, the team leader asked the engineer on the headset to confirm that all the landing gear pins were in place. The engineer on the headset visually checked that allthe landing gear pins were in place and advised the team leader on the flight deck accordingly.
During this time two engineers on the night shift were proceeding with the removal of the pins from the main and body landing gears. They then attempted to remove the nose gear pins, but could not reach them unaided. The removed main gear pins were deposited on the ground by the nose gear while an engineer went to obtain a tool to reach the nose gear pins. Even though some discussion with the engineer on the headset occurred concerning the landing gear doors, there was no effective communication between the two groups concerning the landing gear pins. The team leader, on the flight deck, then selected the landing gear to UP. At this point a 'shudder' was felt and some discussion ensued as to the cause, which was initially attributed to the freight being loaded. However the team leader was not satisfied with this explanation and he then selected the landing gear lever to DOWN. Further inspection showed that both body gears were out of downlock and that there were no pins in the wing or body gears. The pins were then seen lying by the nose-wheel. From the associated statements it was clear that the engineer on the headset was surprised (and "horrified") to see that the pins had been removed, and the engineers who had removed the pins were equally surprised that landing gear functions were being performed. The aircraft was shut down and the situation assessed ; several attempts were made to put the body gears into down-lock. The wing gear pins were re-fitted, however the body gear pins could not be fitted with the gears out of lock.
At about 1840 hrs L it was decided to tow the aircraft back into the hangar where the body gears could be more easily moved. A Tow bar and tow vehicle were connected, the other engineer onboard took the flight engineer's position, and the brakes were released. Upon brake release the aircraft slowly tipped up onto its tail causing the tow bar attachments to break and the body-gears to partly collapse, this in turn causing considerable damage to the body gear hydraulic actuators. Some damage to the lowerskins and frames of the rear fuselage occurred. The personnel on the flight deck and in the cabin, who were uninjured, vacated the aircraft from the rear.
Accident investigation:
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| Investigating agency: | AAIB |
| Report number: | |
| Status: | Investigation completed |
| Duration: | |
| Download report: | Final report
|
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Sources:
https://assets.publishing.service.gov.uk/media/5422ff15e5274a1317000a15/dft_avsafety_pdf_500540.pdf https://www.jetphotos.com/photo/6221044 (Photo)
Revision history:
| Date/time | Contributor | Updates |
| 23-Mar-2025 06:51 |
Justanormalperson |
Added |
| 23-Mar-2025 06:52 |
ASN |
Updated [Narrative, Accident report, ] |
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