As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
APU WILL NOT START. GROUNDED YES. DURING T/S FOUND APU LUBE MODULE DIFF PRESS PIN EXTENDED & END OF INDICATOR DAMAGED T/S TO INOP FUEL CONTROL WILL REQUIRE REPLACEMENT. INSTALLED FUEL CONTROL REMOVED. MIG 51 TAGS S/N 24974 27702 24146 AND 13623 INSTALLED ON ALL FUEL BOOST PUMP SWITCHES. R&R APU LUBE MODULE DIFF. PRESSURE INDICATOR PER AMM 49 91 13. INSTALLED FUEL CONTROL PER AMM 49 31 11.