EASA SIB CE-14-22
Piper PA-28 Aeroplanes — Fuel Selector/Shut-Off Valve
Summary
Special Airworthiness Information Bulletin SAIB: CE-14-22 is an FAA informational bulletin addressing a fuel selector valve issue in Piper Aircraft Models PA-28-140, PA-28-150, PA-28-160, PA-28-180, PA-28R-180, and PA-28R-200 airplanes. It highlights the risk of inadvertent fuel selector valve shutoff or binding during fuel tank switching, which can cause engine power loss in flight. The bulletin provides recommendations to prevent such occurrences but does not mandate regulatory action.
What Changed
This bulletin introduces awareness of a potential airworthiness concern involving the fuel selector valve on specified Piper PA-28 models. It recommends installing a fuel selector valve cover with a lockout device to prevent accidental shutoff and maintaining the fuel selector valve to avoid binding. No new regulatory requirements or airworthiness directives are issued at this time.
Why It Matters
This information is critical for operators and maintenance personnel to prevent inadvertent fuel shutoff that could lead to engine power loss and possible accidents. Proper understanding, inspection, and maintenance of the fuel selector valve improve flight safety and reduce the risk of incidents related to fuel management. Compliance with the recommendations can enhance operational reliability and safety margins.
What To Do
Owners and operators of affected Piper PA-28 models should familiarize themselves with the fuel selector valve operation, including the positions and tactile feedback. They should replace existing fuel selector valve covers with lockout designs as per Piper Service Bulletin 840A and perform inspections and maintenance according to Piper Service Bulletin 355. Additionally, pilots should ensure fuel tank selection is correct before landing and switch tanks only over flat terrain. No specific compliance deadlines are provided.