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Printed page label not indexed. PDF page 24.
and pivoting it upwards on its aft hinge. Beneath it were drain holes and a missing screw on the © Crown copyright 2026 24 All times are UTCOpen official document at PDF page 24AAIB final report: G-ONEE
Printed page label not indexed. PDF page 25.
Subsequent tests showed that the drain hole was clear and did not leak. The missing screw created a hole that could have allowed water to pass down directly on top of the drip shield above the E1/E2 racks. Figure 15Open official document at PDF page 25AAIB final report: G-ONEE
Printed page label not indexed. PDF page 35.
condition and security. ● Checking the Power Drive Unit number 4 attachment bolts and screws for condition and security. Location of GCUs on Boeing 747-8 The upgraded Boeing 747-8 entered service in 2011. At the time this report was draftedOpen official document at PDF page 35AAIB final report: G-ONEE
Printed page label not indexed. PDF page 40.
dam was missing so water could flow beyond the mat to the floor area above the MEC. A screw was missing from PDU 4 which provided a hole for water to pass from the floor onto the top of theOpen official document at PDF page 40AAIB final report: G-ONEE
Printed page label not indexed. PDF page 41.
standing height which could miss sealant and tape issues and would not detect missing PDU screws as the PDU needs to be manually pivoted upwards to see the screws underneath. As © Crown copyright 2026 41 All times are UTCOpen official document at PDF page 41AAIB final report: G-ONEE
Printed page 8. PDF page 10.
surface 79 Figure 60: Front view of engine 80 Figure 61: Trimmable horizontal stabiliser screwjack after being raised on board 80 Figure 62: Evolutions of recorded angles of attack and of the stall warning trigger threshold 89 Figure 63: ComparisonOpen official document at PDF page 10Final Report: Accident on 1st June 2009 to the Airbus A330-203 registered F-GZCP operated by Air France flight AF 447