As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.
What was found
NR 2 ENGINE SQUIB TEST INOP FOR SYSTEM NR 1 AND NR 2. FOUND BOTH NR 1 AND NR 2 SQUIB CANNON PLUG DISCONNECTED FOR NR 2 ENG FIRE BOTTLE. CONNECTED NR 1 AND NR 2 SQUIB CANNON PLUG PER AMM 26-21-03-404-111 STEPS F(8) TO (12) OP CHECK NORMAL PER AMM 26-21-03-404-111 STEP G.