20020214004369I

Incident · Minor damage

FAA incident report · Doug DC-8-71F · Orlando, FL · February 14, 2002

Date
February 14, 2002 · 22:00 local
Place
Orlando, FL
Airport
Orlando International
Phase of flight
Takeoff Ground Roll
Operating rules
Air carrier (Part 121)
Operator
IXXA
Damage
Minor damage
Aircraft
N830BX
Reported as
Doug DC871F
People aboard
3
Fatal injuries
0

From the FAA’s Accident/Incident Data System (AIDS), through its Aviation Safety Information Portal, as reported. The NTSB investigates accidents separately, and its record of an accident is the fuller one. The aircraft is matched to the registry by N-number and event date, checked against the reported make and model; the registry’s history has gaps, so older matches can be wrong. Compare the reported make and model.

What happened

The FAA’s narrative, in sentence case. The FAA writes it in capitals and removes private details.

(-23) On 02/14/2002, ixxa mechanics removed and replaced the #2 engine bleed air regulator valve in order to correct a deferral on that system. The new valve did not correct the problem, so the deferral was continued. At the end of the day shift, after the item was approved for return to service, it was determined that the mechanics had failed to re-deactivate the system in accordance with ixxa MEL requirements. One ixxa mechanic returned to the aircraft, opened the #2 engine cowls, deactivated the high stage bleed valve, and started to close the engine. Another mechanic assisted closing the core cowls (reverser cowls) and one fan cowl, but left to finish a walk-around. The mechanic working the #2 engine assumed that the mechanic who assisted him with the cowls also latched the fan cowls. The assumption was not correct. Both mechanics returned to the ixxa office, unaware of their error. During preparation for launch, the f/e accomplished his originating preflight, but did not notice that the #2 engine fan cowls were unlatched. On takeoff, the fan cowls opened and were torn off by the slipstream, coming to rest on the runway. The aircraft returned to mco, executing an uneventful landing.

As the FAA filed it

(-23) ON 02/14/2002, IXXA MECHANICS REMOVED AND REPLACED THE #2 ENGINE BLEED AIR REGULATOR VALVE IN ORDER TO CORRECT A DEFERRAL ON THAT SYSTEM. THE NEW VALVE DID NOT CORRECT THE PROBLEM, SO THE DEFERRAL WAS CONTINUED. AT THE END OF THE DAY SHIFT, AFTER THE ITEM WAS APPROVED FOR RETURN TO SERVICE, IT WAS DETERMINED THAT THE MECHANICS HAD FAILED TO RE-DEACTIVATE THE SYSTEM IN ACCORDANCE WITH IXXA MEL REQUIREMENTS. ONE IXXA MECHANIC RETURNED TO THE AIRCRAFT, OPENED THE #2 ENGINE COWLS, DEACTIVATED THE HIGH STAGE BLEED VALVE, AND STARTED TO CLOSE THE ENGINE. ANOTHER MECHANIC ASSISTED CLOSING THE CORE COWLS (REVERSER COWLS) AND ONE FAN COWL, BUT LEFT TO FINISH A WALK-AROUND. THE MECHANIC WORKING THE #2 ENGINE ASSUMED THAT THE MECHANIC WHO ASSISTED HIM WITH THE COWLS ALSO LATCHED THE FAN COWLS. THE ASSUMPTION WAS NOT CORRECT. BOTH MECHANICS RETURNED TO THE IXXA OFFICE, UNAWARE OF THEIR ERROR. DURING PREPARATION FOR LAUNCH, THE F/E ACCOMPLISHED HIS ORIGINATING PREFLIGHT, BUT DID NOT NOTICE THAT THE #2 ENGINE FAN COWLS WERE UNLATCHED. ON TAKEOFF, THE FAN COWLS OPENED AND WERE TORN OFF BY THE SLIPSTREAM, COMING TO REST ON THE RUNWAY. THE AIRCRAFT RETURNED TO MCO, EXECUTING AN UNEVENTFUL LANDING.

Other reports on N830BX · 1

Matched to the same aircraft by N-number and date.