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20101220053999I

Incident · No damage
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FAA incident report · Boeing B-757 · Morristown, NJ · December 20, 2010

FAA Aviation Safety Information Portal

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Date
December 20, 2010 · 23:31 local
Place
Morristown, NJ
Airport
Morristown Municipal
Phase of flight
Landing: Approach
Operating rules
Foreign air carrier (Part 129)
Operator
E4YF
Damage
No damage
Aircraft
NONE
Reported as
Boeing B-757
People aboard
0
Fatal injuries
0
Other injuries
0
Pilot’s flight hours
0 total0 in this make and model0 in the last 90 days

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.

After departure from the gate at ory on 12/20/10, openskies flight 003, a B757-200, fh-avn, had an anti skid fault light illuminate and returned to the gate. Maintenance at ory followed the fim fault tree 32-42-806, due to history replaced auto brake / anti skid module iaw amm 32-42-09/401, tested iaw amm 32-42-802, cleared as all satisfactory. During take off roll subsequent to the anti skid module replacement at 120KT the anti skid warning illuminated and stayed on during the entire flight. Due to the speed and contaminated runway at ory the crew elected to continue the take off and continue to ewr. The crew requested runway 4R at ewr and performed a precautionary landing using maximum reverse. ARFF was alerted and the landing at ewr was uneventful. The aircraft taxied to the gate without incident. British air worked the aircraft actioning fim 32-42 fault tree 802. Antiskid/auto brake control unite bite check, transducer 2 message was displayed. Inspected transducer 2 and performed resistance check, checked normal. Anti skid system operational check did not function. Placed anti skid system on MEL 32-42-1.

As the FAA filed it

AFTER DEPARTURE FROM THE GATE AT ORY ON 12/20/10, OPENSKIES FLIGHT 003, A B757-200, FH-AVN, HAD AN ANTI SKID FAULT LIGHT ILLUMINATE AND RETURNED TO THE GATE. MAINTENANCE AT ORY FOLLOWED THE FIM FAULT TREE 32-42-806, DUE TO HISTORY REPLACED AUTO BRAKE / ANTI SKID MODULE IAW AMM 32-42-09/401, TESTED IAW AMM 32-42-802, CLEARED AS ALL SATISFACTORY. DURING TAKE OFF ROLL SUBSEQUENT TO THE ANTI SKID MODULE REPLACEMENT AT 120KT THE ANTI SKID WARNING ILLUMINATED AND STAYED ON DURING THE ENTIRE FLIGHT. DUE TO THE SPEED AND CONTAMINATED RUNWAY AT ORY THE CREW ELECTED TO CONTINUE THE TAKE OFF AND CONTINUE TO EWR. THE CREW REQUESTED RUNWAY 4R AT EWR AND PERFORMED A PRECAUTIONARY LANDING USING MAXIMUM REVERSE. ARFF WAS ALERTED AND THE LANDING AT EWR WAS UNEVENTFUL. THE AIRCRAFT TAXIED TO THE GATE WITHOUT INCIDENT. BRITISH AIR WORKED THE AIRCRAFT ACTIONING FIM 32-42 FAULT TREE 802. ANTISKID/AUTO BRAKE CONTROL UNITE BITE CHECK, TRANSDUCER 2 MESSAGE WAS DISPLAYED. INSPECTED TRANSDUCER 2 AND PERFORMED RESISTANCE CHECK, CHECKED NORMAL. ANTI SKID SYSTEM OPERATIONAL CHECK DID NOT FUNCTION. PLACED ANTI SKID SYSTEM ON MEL 32-42-1.