NTSB investigations · 1
Matched to this aircraft by N838AT and the event date: up to this one’s cancellation.
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N838AT and the event date: up to this one’s cancellation.
Service difficulty reports · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR AT0000374Smoke · detectedFOUND SMOKE IN COCKPIT. AIRCRAFT OUT OF SERVICE, FURTHER EVALUATION AND TROUBLE SHOOTING REQUIRED.SDR AT0000219Acm · malfunctionedDURING CLIMBOUT, FUMES CAME INTO THE CABIN THROUGH THE AIR CONDITIONING VENTS AND SET AFT LAVATORY SMOKE DETECTORS. AIRCRAFT RETURNED TO STATION. FOUND RIGHT AIR CYCLE MACHINE SURGING. REMOVED AND REPLACED RIGHT ACM AND REPLACED COALESCER BAGS.SDR AT9900849Frame · crackedFOUND LEFT HAND MAIN FRAME NR 737 HAD 2 CRACKS. REMOVED AND REPLACED LEFT HAND MAIN FRAME NR 737 IAW DC9 SRM 51-30-2, 51-30-5 AND EO 1253-1129-B1044.SDR AT9900848Frame · crackedFOUND RIGHT HAND MAIN FRAME AT FRAME NR 718 HAD 2 CRACKS. REMOVED AND REPLACED RIGHT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-30-2, 51-30-5, EO 1253-11-29-B1044.SDR AT9900850Frame · crackedFOUND RIGHT HAND FRAME AT BS 699 HAD 4 CRACKS. REMOVED AND REPLACED RIGHT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-30-2, 51-30-5 AND EO 1253-1129-B1044.SDR AT9900843Floorbeam · chafedFOUND FLOORBEAM CHAFED 8 INCH AREA AT BS 870 BETWEEN LBL 5 - LBL 15, CHAFED AREA OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR ANGLE AND STAINLESS STEEL WRAP STRIP IAW DC9 SRM 53-05 FIGURE 20A.SDR AT9900842Support · crackedFOUND FORWARD PIT FLOOR SUPPORT AT BS 389 HAS TWO EACH CRACKS. REMOVED, WEILDED AND REINSTALLED FLOOR SUPPORT IAW EA 12-5321-29-C1362 AND DC9 SRM 51-10-03, 51-30-2.SDR AT9900847Web · corrodedFOUND RIGHT HAND AFT CABIN AT BS 908-965 RBL 50, FLOOR SUPPORT WEB WAS CRACKED AND CORRODED. REMOVED CORROSION, STOP DRILLED CRACK, FABRICATED, INSTALLED REPAIR IAW DC9 SRM 53-01, 51-10-3, 51-30-1.SDR AT9900854Floor Panel · corrodedFOUND FLOOR PANEL CRACKED (HAT SECTION) AND CORRODED AROUND SCREW HOLE. FABRICATED PANEL REPAIR, FABRICATED 5 REPAIR HAT SECTIONS, DRILLED, DEBURRED, TREATED, PRIMED, AND INSTALLED REPAIR AND HAT SECTIONS IAW DC9 SRM 51-10-4, 51-10-3, 51-30-2, AND DC9 MM 25-1SDR AT9900853Floor Panel · corrodedFOUND FLOOR PANEL NR 4692A WAS CORRODED. GAINED ACCESS, REMOVED HAT SECTIONS, FABRICATED NEW FLOOR PANEL, TREATED, PRIMED INSTALLED HAT SECTIONS AND PANEL IAW DC9 SRM 51-30-2, 57-10-2, 51-10-3, 51-70-2 AND DC9 MM 53-20-1.SDR AT9900852Floorbeam · chafedFOUND FLOORBEAM CHAFED AT BS 915. BLENDED AND FABRICATED REPAIR ANGLE AND FILLERS, TREATED, PRIMED, INSTALLED REPAIR IAW DC9 SRM 53-01 FIGURE 1, 51-30-1, 53-05 FIGURE 20A, 51-10-3, 51-30-5.SDR AT9900851Frame · crackedFOUND LEFT HAND MAIN FRAME AT BS 699 HAD 3 CRACKS. REMOVED AND REPLACED LEFT HAND MAIN FRAME AT BS 699 IAW DC9 SRM 51-30-2, 51-30-5 AND EO 1253-1129-B1044.SDR AT9900845Floor Panel · corrodedFOUND UPPER SKIN LOOSE AND CORROSION ALONG AFT EDGE OF FLOOR PANEL NR 4695. REMOVED, FABRICATED AND INSTALLED UPPER SKIN AND HAT SECTIONS IAW DC9 SRM 53-01, 51-10-31, 53-21-0, 51-30-3, DC9 MM 25-11-0.SDR AT9900841Strap · corrodedFOUND AFT PIT AFT BULKHEAD RIGHT HAND PANEL WAS CORRODED. REMOVED CORROSION FROM STRAP MATT LOSS OF 50 PERCENT OUT OF LIMITS. FABRICATED STRAP, TREATED, PRIMED IAW DC9 SRM 51-10-2, 51-10-3, 51-10-4, 53-01 FIGURE 1.SDR AT9900552Bus Control · failedAFTER TAKEOFF, ELECTRICAL POWER WAS LOST FOR A FEW SECONDS AND THEN CAME BACK ON. THIS HAPPEN TWO MORE TIMES. AIRCRAFT RETURN TO ATLANTA AND LANDED AT A WEIGHT OF 100,503 POUNDS. REMOVED AND REPLACED A/C BUS CONTROL PANEL, OPS CHECK WITH ENGINE RUNS AND NUM