EASA Regulations for Piper PA-44-180

2 airworthiness directives and regulatory documents affecting Piper PA-44-180.

EASA AD US-2024-10-04

Wings - Rear Wing Spar Attachment Fitting - Inspection

The Federal Aviation Administration's Airworthiness Directive 2024-10-04 addresses certain Piper Aircraft, Inc. models PA-28-181, PA-28R-201, PA-34-220T, and PA-44-180 airplanes. This directive mandates inspection of the rear wing spar attachment fitting due to a manufacturing defect involving a double-drilled bolt hole, which compromises structural integrity. The AD aims to prevent potential wing separation and loss of control by requiring inspections and corrective actions as necessary.

May 23, 2024

Airworthiness DirectiveMaintenanceSafety MgmtPiper Aircraft PA-28 (Archer)Piper Aircraft PA-28R (Arrow)Piper Aircraft PA-34 (Seneca)Piper Aircraft PA-44 (Seminole)Piper PA-28-181Piper PA-28R-201Piper PA-34-220TPiper PA-44-180

EASA SIB CE-11-37

Piper PA-44-180 & Cessna 172R and S Aeroplanes - Engine Oil Filter Interference

The Special Airworthiness Information Bulletin SAIB: CE-11-37 is an FAA informational bulletin addressing engine oil filter interference issues in Piper PA-44-180 aircraft with Lycoming O-360-A1H6 and LO-360-A1H6 engines, and Cessna 172R and S aircraft with Lycoming IO-360-L2A engines. The bulletin highlights potential interference between oil cooler hose fittings and the oil filter that could lead to improper installation and oil system problems. Other engines and aircraft models may also be affected.

Jun 6, 2011

Safety Information BulletinMaintenanceSafety MgmtPiper PA-44-180Cessna 172RCessna 172S