What was found
YYC - C4 RIGHT HAND NACELLE, MAIN LANDING GEAR AREA, SHOCK STRUT HAS CHAFING DAMAGE AT LOWER/FORWARD END OF CYLINDER. CHAFING IS CAUSED BY WEIGHT ON WHEEL WIRING CONDUIT CONTACT. REPAIRED IAW RD8-32-1575 AND EA 2-32-108.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
YYC - C4 RIGHT HAND NACELLE, MAIN LANDING GEAR AREA, SHOCK STRUT HAS CHAFING DAMAGE AT LOWER/FORWARD END OF CYLINDER. CHAFING IS CAUSED BY WEIGHT ON WHEEL WIRING CONDUIT CONTACT. REPAIRED IAW RD8-32-1575 AND EA 2-32-108.