Casualties unknown

2015-12-22: Embraer E170 — CTR EPWA, PL

CTR EPWA, PL

On December 22, 2015, an Embraer E170 was involved in an aviation accident near CTR EPWA, PL. Investigators recorded the probable cause as: Leak in the Precooler (P/N 1002165-3). This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL).

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards

An Embraer E170 experienced a cabin pressurization technical problem after takeoff from Warsaw Chopin Airport, prompting a return to the airport. No emergency was declared. Investigation identified a leak in the Precooler as the cause.

Overview

On December 22, 2015, an Embraer E170 aircraft was involved in an incident during a flight departing from Warsaw Chopin Airport (EPWA). The flight crew reported a technical problem with cabin pressurization shortly after takeoff. The aircraft returned to EPWA, and the crew did not declare an emergency. After landing, the crew filed an Air Safety Report (ASR). The incident was linked to a separate occurrence under investigation (incident number 2631/15).

Sequence of Events

After takeoff, a cabin pressurization issue was identified. The decision was made to return to EPWA. The crew did not indicate any distress. The landing was uneventful, and the subsequent report led to a technical investigation by the aircraft operator.

Investigation and Cause

The investigation determined that the underlying cause of the pressurization problem was a leak in the Precooler (part number 1002165-3). The troubleshooting process revealed that earlier repair actions had been ineffective. During ground tests, the fault could not be reproduced. Subsequent data downloads on February 7, 2016, indicated a persistent error code for loop #5, suggesting a leak not only in the pipe from the precooler but also likely from the precooler seal or the unit itself. A replacement of the precooler was ordered.

Corrective Actions

Following the replacement of the precooler, no further bleed leak indications were recorded. Data from the Flight History Data Bank (FHDB) after two initial sectors showed no loop errors or overheat warnings. After ten additional sectors, no errors were present. The aircraft continued to be monitored under routine surveillance. The final corrective action—replacement of the precooler—proved successful, as the BLEED 2 LEAK fault did not recur. An Engineering Reliability Report was prepared by the operator's engineer, documenting the troubleshooting, tests, component replacements, and probable causes.

The investigation committee did not issue any safety recommendations regarding this incident.

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2015-2634/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.