Looks Like Wiring

Preliminary Report


 

Sure looks like a wiring-related mishap. Not all that odd. Full pressurization differential causes the fuselage to expand by up to an inch in all directions (and it would be more if the extreme -30 deg Celsius temperatures at height wasn't causing a contraction). That's all you need to stretch a wire across a piece of structure
Occurrence Number: 200105338
Release Date: 01-Dec-01
Occurrence Type: Serious-Incident
Location: 19 km SE Nyngan, Aero.
State: New South Wales (NSW)
Occurrence Date: 06-Nov-01
Time/Zone: 1746 hours EST
Highest Injury Level: Minor
Investigation Category: 3
Injuries: Fatal Serious Minor None Total
Crew 0 0 0 0 0
Passenger 0 0 0 0 0
Ground 0 0 0 0 0
Total 0 0 0 0 0
Aircraft Details
Aircraft Manufacturer: Boeing Co
Aircraft Model: 747-400
Aircraft Registration: 9V-SPP of Singapore Airlines
Serial Number:  
Type of Operation: Air Transport, Scheduled
Damage to Aircraft: Nil
Departure Time: 1718 hours EST
Departure Point: Sydney, NSW
Destination: Changi, SINGAPORE
Crew Details: Role Class of Licence Hours on Type Hours Total
  Pilot-In-Command Senior Commercial 8609 19094
Crew Details: Role Class of Licence Hours on Type Hours Total
  Co-Pilot/1st Officer Commercial 1007 2992
FACTUAL INFORMATION

As the Boeing 747-400 was approaching flight level 360, the flight crew observed a cabin altitude warning message and an increase in cabin altitude. As the crew carried out the non-normal checklist, the cabin altitude continued to rise and could not be controlled. The pilot in command decided to carry out an emergency descent and deploy the passenger oxygen masks. As the aircraft descended, all the electronic flight data display screens went blank. The crew continued the descent to an altitude of 10,000 ft using standby instruments. One passenger reported ill effects as a result of the descent. The aircraft was then turned back to Sydney where an uneventful, but overweight, landing was conducted.

An inspection by ground engineers revealed that the upper cabin pressure relief valve had operated, indicating that at some time during the flight the aircraft's internal pressure had exceeded its maximum differential with the ambient pressure. After a number of system

 circuit breakers were cycled the aircraft's display screens returned to normal operation. An engine ground run was carried out, but the inflight faults could not be reproduced. The primary components of the aircraft's pressurization and flight deck display systems were removed for further analysis.

The investigation is continuing.

from this link


to Wiring Menu