Casualties unknown

2021-03-26: (CC-AZE) — PE

PE

On March 26, 2021, an aircraft (registration CC-AZE) was involved in an aviation accident near PE. Investigators recorded the probable cause as: Total loss of Yellow hydraulic fluid due to a crack in its return line located in the left main landing gear well, produced by the impact of rubber debris detached from the tread of tire #2 of the left main landing gear during takeoff from Arequipa. This summary draws on records from the Aircraft Accident Investigation Commission of Peru (CIAA), Ministry of Transport and Communications.

Sourcesthe Aircraft Accident Investigation Commission of Peru (CIAA), Ministry of Transport and CommunicationsPrimary reportUpdated 1782716661Data APIEditorial standards
Aircraft registered CC-AZE
Aircraft registered CC-AZE. Photo: Sky KoreSCL / CC BY-SA 4.0, via Wikimedia Commons

On March 26, 2021, an Airbus A320-251N (CC-AZE) operated by Sky Airline Peru experienced progressive yellow hydraulic fluid loss after takeoff from Arequipa. The crew declared an emergency and landed safely at Lima. Investigation attributed the cause to a cracked return pipe due to tire debris impact.

Flight Details

On March 26, 2021, at 19:55 local time, an Airbus A320-251N, registration CC-AZE, operated by Sky Airline Peru S.A.C., departed from Alfredo Rodríguez Ballón International Airport (SPQU) in Arequipa on scheduled flight SKX5142 to Jorge Chávez International Airport (SPJC) in Lima. The captain served as pilot monitoring (PM) and the first officer as pilot flying (PF).

Hydraulic Failure and Crew Actions

During the initial climb, at 19:56, the crew observed a gradual decrease in the hydraulic fluid level of the Yellow system reservoir. The Yellow system independently powers the nose wheel steering, parking and alternate brakes, engine #2 reverse thrust, yaw damper #2, and cargo doors. During cruise, approximately 40 nautical miles from Pisco Airport, a master warning activated with ECAM messages indicating low reservoir level (HYD Y RSVR LO LVL) and low pressure (HYD Y SYS LO PR). The crew followed the abnormal procedures from the FCOM for hydraulic system failures.

Emergency Declaration and Landing

The crew informed Lima Control of the failure, requested priority for approach, and indicated the need for towing due to the nature of the malfunction. At 21:09 local time, the aircraft landed safely on runway 15 at Lima, came to a stop on taxiway C, and the crew activated the brake fan and shut down the engines. The aircraft was then towed to parking position 7. All passengers and crew disembarked without incident.

Post-Flight Inspection and Damage

During a post-flight inspection, maintenance personnel discovered that tire #2 of the left main landing gear had lost tread material (stripped rib). Hydraulic fluid was found leaking from a rigid return line in the left main landing gear well. Additionally, damage consistent with foreign object impact was observed on the inner flap and lower left wing panel.

Probable Cause

The investigation determined the probable cause was a total loss of Yellow hydraulic fluid due to a crack in the return line located in the left main landing gear well. The crack was caused by impact from rubber debris that detached from the tread of tire #2 on the left main landing gear during takeoff from Arequipa.