As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
THE VALVE DESCRIBED AT LEFT, WAS INSTALLED DUE TO THE UNIT INSTALLED PRIOR HAVING AN EXTERNAL LEAK. DURING INSTALLATION THE VALVE WAS ADJUSTED TO THE SPECIFICATION DESCRIBED IN THE CMP CODE (ATA CODE) ABOVE. THE AIRCRAFT WAS THEN PUT THROUGH A GEAR SWING (10) TEN TIMES WITH THE UNIT OPERATING NORMALLY. THE AIRCRAFT AND PART DESCRIBED WERE INSPECTED AND THE AIRCRAFT DISPATCHED.