CESSNA 310Q — Maintenance Manual

3 maintenance manual references for the CESSNA 310Q.

Overview

2014

This document serves as an Instructions for Continued Airworthiness (ICA) supplement for the Cessna 310 series aircraft, specifically addressing the Tailcone Stinger Assembly installation. It provides maintenance technicians with essential information to ensure the airworthiness of the tailcone stinger assembly, which is modified under FAA STC SA00873WI. The document outlines inspection requirements, maintenance schedules, and troubleshooting procedures specific to the tailcone stinger assembly. It is crucial for operators to integrate this information into their aircraft maintenance manuals and scheduled maintenance programs to comply with FAA regulations. The document emphasizes the importance of regular inspections and provides guidelines for the installation and maintenance of the tailcone stinger assembly, ensuring the aircraft remains in a safe and airworthy condition.

Inspect the tailcone stinger assembly every 100 hours or annually.
Check for cracks around the assembly and attachment screws during inspections.
The tailcone stinger assembly weighs 5.5 lbs ± 0.5 lbs without paint.
No airworthiness limitations are added by the installation of the tailcone stinger assembly.
Troubleshooting should be performed by FAA-approved repair stations.

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Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

3 documents