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20160206001239I

Incident · Minor damage
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FAA incident report · Rockwell International NA-265-65 · West Memphis, AR · February 6, 2016

FAA Aviation Safety Information Portal

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Date
February 6, 2016 · 16:00 local
Place
West Memphis, AR
Phase of flight
Landing: Rollout
Operating rules
General operating rules (Part 91)
Damage
Minor damage
Aircraft
N779CS
Reported as
Rockwell International NA-265-65
Reported engine
AiResearch TFE731 series
People aboard
2
Fatal injuries
0
Other injuries
0
N779CSRegistration cancelled Jan 4, 2024 · Rockwell International NA-265-65S/N 465-29 · Built 1980Airframe modelRockwell International NA-265-65Engine modelAiResearch TFE731 seriesTurbo-jet

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.

On February 6, 2016 at approximately 16:00 CST, N779CS a Rockwell international, model NA-265-65 (sabre liner) aircraft, operated by a ATP rated pilot experienced a failure of the number one hydraulic pump during landing rollout. The subsequent application of emergency braking resulted in a partial collapse of the left main landing gear due to a failure of the main landing gear side brace clevis assembly after brake application. The aircraft sustained minor damage; the pilot and copilot were not injured.

As the FAA filed it

ON FEBRUARY 6, 2016 AT APPROXIMATELY 16:00 CST, N779CS A ROCKWELL INTERNATIONAL, MODEL NA-265-65 (SABRE LINER) AIRCRAFT, OPERATED BY A ATP RATED PILOT EXPERIENCED A FAILURE OF THE NUMBER ONE HYDRAULIC PUMP DURING LANDING ROLLOUT. THE SUBSEQUENT APPLICATION OF EMERGENCY BRAKING RESULTED IN A PARTIAL COLLAPSE OF THE LEFT MAIN LANDING GEAR DUE TO A FAILURE OF THE MAIN LANDING GEAR SIDE BRACE CLEVIS ASSEMBLY AFTER BRAKE APPLICATION. THE AIRCRAFT SUSTAINED MINOR DAMAGE; THE PILOT AND COPILOT WERE NOT INJURED.