What was found
DURING CLIMB, HYDRAULIC QUANTITY IN THE NR 3 SYSTEM WENT TO ZERO. FOUND UPPER PRIMARY STABILIZER TRIM CONTROL VALVE CRACKED. REMOVED AND REPLACED VALVE IAW 27-40-2. OPERATIONAL AND LEAK CHECKS GOOD.
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
DURING CLIMB, HYDRAULIC QUANTITY IN THE NR 3 SYSTEM WENT TO ZERO. FOUND UPPER PRIMARY STABILIZER TRIM CONTROL VALVE CRACKED. REMOVED AND REPLACED VALVE IAW 27-40-2. OPERATIONAL AND LEAK CHECKS GOOD.