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20070109003269I

Incident · Minor damage
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FAA incident report · Doug MD11F · New York, NY · January 9, 2007

FAA Aviation Safety Information Portal

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Date
January 9, 2007 · 06:45 local
Place
New York, NY
Airport
John F Kennedy International
Phase of flight
Roll-Out (Fixed Wing)
Operating rules
Foreign air carrier (Part 129)
Operator
AAPF
Damage
Minor damage
Aircraft
EIUPU
Reported as
Doug MD11F
Reported engine
GE CF6*
People aboard
2
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) Crew reported that during landing roll runway 31R jfk flight AZ9170, 01/09/07 at 0645 hrs with thrust reverser open, a right yaw movement was manually corrected. After thrust reverser closure the "reverser #1 fault alert on." Rohr thrust reverser system. After walkaround inspection the following damages were found: #1 eng. RH. T/r transcowl missing. #1 and #5 tires damaged, #1 eng. Pylon RH side, fair p/n AUB7763-502 having a dent of 3" dia. With cut. On skin several dents and scratches. LH inboard flap substantial damage.

As the FAA filed it

(-23) CREW REPORTED THAT DURING LANDING ROLL RUNWAY 31R JFK FLIGHT AZ9170, 01/09/07 AT 0645 HRS WITH THRUST REVERSER OPEN, A RIGHT YAW MOVEMENT WAS MANUALLY CORRECTED. AFTER THRUST REVERSER CLOSURE THE "REVERSER #1 FAULT ALERT ON." ROHR THRUST REVERSER SYSTEM. AFTER WALKAROUND INSPECTION THE FOLLOWING DAMAGES WERE FOUND: #1 ENG. RH. T/R TRANSCOWL MISSING. #1 AND #5 TIRES DAMAGED, #1 ENG. PYLON RH SIDE, FAIR P/N AUB7763-502 HAVING A DENT OF 3" DIA. WITH CUT. ON SKIN SEVERAL DENTS AND SCRATCHES. LH INBOARD FLAP SUBSTANTIAL DAMAGE.