Beechcraft T-34 Mentor — Flight Manual

This document provides detailed installation instructions for the T-34 Mentor series aircraft, specifically the T-34, T-34A, and T-34B models. It serves as an Alternate Means of Compliance (AMOC) to Airworthiness Directive 2004-25-51, outlining necessary inspections, replacements, and modifications to ensure continued airworthiness. The instructions include procedures for eddy current inspections, cold working of fastener holes, and the installation of the ALEC tension cable. Compliance with these instructions is mandatory for affected aircraft to remove flight restrictions imposed by the AD. The document is intended for maintenance personnel and aircraft owners who need to perform these modifications and inspections.

• The document is for Beechcraft T-34 Mentor series aircraft: T-34, T-34A, and T-34B.
• Compliance with the installation instructions is mandatory to remove flight restrictions from AD 2004-25-51.
• Estimated man-hours for the complete procedure are approximately 15 hours.
• The torque value for wing attach bolts is 2880 to 3000 in-lbs (240 to 250 ft-lbs).
• The installation of the ALEC tension cable requires careful balancing of thread engagement.