As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
1) "A" SYSTEM HYDRAULIC FAILURE AFTER TAKE-OFF, "0" QUANTITY FOLLOWED ABNORMAL PROCEDURE.2) INSPECTED & FOUND ELEVATOR FEEL COMPUTER "A" SYSTEM FILTER CAP CRACKED. R & R "A" SYSTEM CAP & SEAL PER M/M 27-30-101. INSPECTED #1 & #2 ENGINE HYDRAULIC PUMP CASE DRAIN FILTERS IAW M/M 29-41-11. NO PARTICLES FOUND OK FOR SERVICE.