20160217001169I

Incident · Minor damage

FAA incident report · Boeing 747-87UF · Miami, FL · February 17, 2016

Date
February 17, 2016 · 08:49 local
Place
Miami, FL
Airport
Miami International Airport
Phase of flight
Takeoff: Rotation
Operating rules
Air carrier (Part 121)
Operator
UIEA
Damage
Minor damage
Aircraft
N859GT
Reported as
Boeing 747-87UF
People aboard
0
Fatal injuries
0
Other 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.

Atlas air inc. N859GT bound for buenos aires (eze) encountered just prior rotation brake limiter, anti -skid and tire pressure eicas messages. Emergency checklist was completed, fuel was jettisoned and aircraft returned back to mia. Landing was not overweight and uneventful. Upon landing #6 main wheel/tire assembly showed signs of FOD. #8 main wheel/tire assembly was deflated and severely damaged with thread separation. Initial damage assessment revealed sustained damage behind left hand (LH) body gear from tire debris at lower center section fuselage fairing panels, fairing frame, LH body gear electrical wire harness, junction box and associated brackets.

As the FAA filed it

ATLAS AIR INC. N859GT BOUND FOR BUENOS AIRES (EZE) ENCOUNTERED JUST PRIOR ROTATION BRAKE LIMITER, ANTI -SKID AND TIRE PRESSURE EICAS MESSAGES. EMERGENCY CHECKLIST WAS COMPLETED, FUEL WAS JETTISONED AND AIRCRAFT RETURNED BACK TO MIA. LANDING WAS NOT OVERWEIGHT AND UNEVENTFUL. UPON LANDING #6 MAIN WHEEL/TIRE ASSEMBLY SHOWED SIGNS OF FOD. #8 MAIN WHEEL/TIRE ASSEMBLY WAS DEFLATED AND SEVERELY DAMAGED WITH THREAD SEPARATION. INITIAL DAMAGE ASSESSMENT REVEALED SUSTAINED DAMAGE BEHIND LEFT HAND (LH) BODY GEAR FROM TIRE DEBRIS AT LOWER CENTER SECTION FUSELAGE FAIRING PANELS, FAIRING FRAME, LH BODY GEAR ELECTRICAL WIRE HARNESS, JUNCTION BOX AND ASSOCIATED BRACKETS.

Other reports on N859GT · 1

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