EASA SIB CE-13-16: Cessna 172RG, R182, 210 and T303 Aeroplanes — Hydraulic Power Pack / Landing Gear System

What to do

Owners and operators of the affected Cessna models should follow the inspection and corrective procedures outlined in Cessna Service Letters MEL-29-01 and SEL-29-01. These procedures include checking wire routing, ensuring protective covers are installed, and repairing any hydraulic leaks. Although the bulletin does not specify a compliance deadline, timely action is recommended to mitigate the identified risks.

Summary

The Special Airworthiness Information Bulletin SAIB: CE-13-16 is an FAA advisory concerning the hydraulic power pack and landing gear system on Cessna Aircraft Company Models 172RG, R182, TR182, FR182, 210N, T210N, 210R, T210R, P210N, P210R, and T303 airplanes. It addresses an airworthiness concern related to potential fire hazards originating from the landing gear hydraulic power pack system due to improper installation and wiring issues. This bulletin provides safety information but does not mandate regulatory action.

What changed

SAIB CE-13-16 introduces awareness of a fire risk linked to the hydraulic power pack system in certain Cessna models following an accident investigation. It highlights improper installation of terminal lugs, missing terminal covers, and unsecured wiring as potential ignition sources. The bulletin references Cessna Service Letters MEL-29-01 and SEL-29-01, which provide inspection and corrective procedures for affected aircraft.

Why it matters

This bulletin is important for aviation professionals because it identifies a safety risk that could lead to in-flight fires and hull loss if not addressed. Operators and maintenance organizations must be vigilant in inspecting and maintaining the hydraulic power pack wiring and protective covers to prevent similar incidents. Compliance with the recommended service letters enhances aircraft safety and reduces the risk of costly accidents and injuries.