Casualties unknown

2001-11-23: PIPER PA-38-112 (G-BYMC) — Near Alsater, Staffordshire, GB

Near Alsater, Staffordshire, GB

On November 23, 2001, a PIPER PA-38-112 (registration G-BYMC) was involved in an aviation accident near Near Alsater, Staffordshire, GB. Investigators recorded the probable cause as: The No 1 cylinder lower spark plug had not been installed correctly and tightened during the last 50-hour maintenance check, resulting in only the last two threads engaging, which led to the plug loosening and causing engine power loss. This summary draws on records from the UK Air Accidents Investigation Branch (AAIB).

Sourcesthe UK Air Accidents Investigation Branch (AAIB)Primary reportUpdated 1785053200Data APIEditorial standards

During a training flight near Alsager, Staffordshire, a Piper PA-38 lost power after a loud pop. The instructor executed a forced landing; no injuries occurred. Investigation revealed the No 1 cylinder lower spark plug was incorrectly installed during a previous maintenance check.

Aircraft and Flight Details

The aircraft involved was a Piper PA-38-112, registration G-BYMC, manufactured in 1982 and powered by a single Lycoming O-235-L2C piston engine. It was being used for an instructional flight on 23 November 2001, departing for an area suitable for practice forced landings (PFLs) after a normal takeoff and climb out of Manchester Airport controlled airspace.

Incident Sequence

The crew, consisting of an instructor and a student pilot, successfully completed two PFLs into a field near Alsager, Staffordshire. While climbing away to move to a new area for further PFLs, they heard a loud 'pop' followed by a reduction in engine power. The engine was observed running very roughly and vibrating badly.

After performing all relevant checks without success, the instructor decided to carry out a full forced landing. The landing was executed without injury to either occupant. However, during the landing roll, the left wing tip struck a hedge at the end of the field, causing superficial damage to the left wing tip and leading edge.

Investigation Findings

Inspection by the aircraft's maintenance organisation revealed that the lower spark plug of the front right (No 1) cylinder had come out of its threaded hole and was retained only by its lead. Examination of the threads on both the plug and the cylinder head showed that only the last two threads on each exhibited any evidence of engagement and wear, indicating that the plug had not been installed correctly and tightened during the last 50-hour maintenance check, which had been performed 16 flying hours prior to the incident.

Maintenance Action

The maintenance organisation has taken action to prevent a recurrence of this problem, though the specific measures are not detailed in the report.

Probable cause

The No 1 cylinder lower spark plug had not been installed correctly and tightened during the last 50-hour maintenance check, resulting in only the last two threads engaging, which led to the plug loosening and causing engine power loss.