Casualties unknown

2018-06-05: Boeing 737-800 (SP-ENP) — Pilot samolotowy liniowy — TMA/CTR EPWA / Warszawa (EPWA), PL

TMA/CTR EPWA / Warszawa (EPWA), PL

On June 5, 2018, a Boeing 737-800 (registration SP-ENP) operated by Pilot samolotowy liniowy was involved in an aviation accident near TMA/CTR EPWA / Warszawa (EPWA), PL. Investigators recorded the probable cause as: Failure of the LEADING EDGE FLAPS block. This summary draws on records from the Polish State Commission on Aircraft Accidents Investigation (PKBWL); 8 related events involving the same aircraft type or operator are linked below.

Sourcesthe Polish State Commission on Aircraft Accidents Investigation (PKBWL)Primary reportUpdated 1785092869Data APIEditorial standards
Aircraft registered SP-ENP
Aircraft registered SP-ENP. Photo: Rob Hodgkins / CC BY-SA 2.0, via Wikimedia Commons

A Boeing 737-800 crew encountered 'Leading Edge flaps transit' warnings during two approaches. After go-arounds, they landed safely with flaps 15. The cause was a faulty Leading Edge Flaps block.

Occurrence

During pre-flight preparation on June 5, 2018, at EPWA, the flight crew of a Boeing 737-800 detected an abnormal position of slot No. 3 and a 'Leading Edge flaps transit' indication. Hydraulic pump activation did not clear the fault. Maintenance diagnosed a sensor issue on slot No. 3 and replaced it, causing a two-hour delay. The aircraft was then cleared for service.

On approach for landing, after the approach briefing, the crew decided to land with flaps 40. When selecting flaps 25, the 'Leading Edge flaps transit' warning reappeared, accompanied by unnatural speed indications and low-speed buffets. Due to the slot failure warning, the crew changed the flap selection to 30 degrees, but the problem persisted. There was also a flap overspeed of about two knots for six seconds with flaps at 30 degrees. The crew then moved the flap lever to 25 degrees and maintained current speed to avoid a stall warning (low buffet speed increased significantly). At 744 feet, they initiated a go-around. During holding, they performed the 'Non-normal checklist: Leading Edge flaps transit' and configured the aircraft for landing with flaps 15, per the checklist. The landing was uneventful. After landing, the fault was logged, and maintenance performed tests that passed, clearing the aircraft for further service.

On a subsequent flight sector, the crew prepared for an approach with flaps 30 and a contingency plan for flaps 15 if the problem recurred. During approach, after selecting flaps 10, the 'Leading Edge flaps transit' warning returned. Following their plan, the crew configured for flaps 15 landing per the non-normal checklist. The landing was conducted with flaps 15 in turbulent conditions. In the final approach phase, the aircraft deviated above the glide path (about 1.5 dots). After landing and taxiing to the stand, the captain logged the fault. Maintenance performed operational tests and identified a faulty 'Leading Edge Flaps' block, which was replaced. The aircraft was then returned to service.

Cause

The cause of the incident was a failure of the 'LEADING EDGE FLAPS' block.

Probable cause

Failure of the LEADING EDGE FLAPS block

Investigation report by the Polish State Commission on Aircraft Accidents Investigation (PKBWL). Original record: https://pkbwl.gov.pl/raporty/2018-1458/. This page is a structured re-presentation; facts and quotes are in the Panstwowa Komisja Badania Wypadkow Lotniczych (PKBWL), Poland.