N312AA
Service difficulty reports · 139
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N312AA' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N312AA' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR IXXA120314IAI006SPressure Blkhd · dentedDURING C18 CHECK INSPECTION, DAMAGE WAS OBSERVED AT THE AFT PRESSURE BULKHEAD, BS 1582 ON THE DOME WEB BETWEEN RS 19 AND RS 20. CREASE SIGNS ARE SEEN AT THE CENTER OF THE AFFECTED AREA. CUT OUT THE DAMAGED WEB PORTION AT BS 1582 BETWEEN RS 19 AND RS 20. PERFOSDR IXXA120314IAI001SStringer · crackedDURING C18 CHECK INSPECTION, A CRACK WAS OBSERVED AT STRINGER S8L END, BS 676 POINTING AFT. THE DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING FOR ABOUT 2 INCHES. THE AFFECTED STRINGER SPLICES TO THE MAIN DECK CARGO DOOR SURROUND STRUCTURE. TRIMMED OUT DAMSDR IXXA120326IAI007SStringer · crackedDURING C18 CHECK INSPECTION, FOUND A CRACK AT STRINGER S25L END, BS 676, POINTING AFT. DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING FOR ABOUT 5 INCHES. TRIMMED OUT DAMAGED. PERFORMED HFEC INSPECTION OF TRIM OUT AND 3 INCHES AROUND INSURE CRACK FREE ISDR IXXA120314IAI005SStringer · crackedDURING C18 CHECK INSPECTION, A CRACK WAS OBSERVED AT STRINGER S24L END, BS 676 POINTING AFT. THE DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING ABOUT 2 INCHES. THE AFFECTED STRINGER SPLICES TO THE MAIN DECK CARGO DOOR SURROUND STRUCTURE. TRIMMED OUT THE DAMSDR IXXA120314IAI004SStringer · crackedDURING C18 CHECK INSPECTION, A CRACK WAS OBSERVED AT STRINGER S19L END, BS 676 POINTING AFT. THE DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING ABOUT 1.5 IN. THE AFFECTED STRINGER SPLICES TO THE MAIN DECK CARGO DOOR SURROUND STRUCTURE. TRIMMED OUT THE DAMAGSDR IXXA120314IAI003SStringer · crackedDURING C18 CHECK INSPECTION, A CRACK WAS OBSERVED AT STRINGER S18L END, BS 676 POINTING AFT. THE DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING ABOUT 1 INCH. THE AFFECTED STRINGER SPLICES TO THE MAIN DECK CARGO DOOR SURROUND STRUCTURE. TRIMMED OUT THE DAMAGSDR IXXA120314IAI002SStringer · crackedDURING C18 CHECK INSPECTION, A CRACK WAS OBSERVED AT STRINGER S-17L END, BSTA 676 POINTING AFT. THE DAMAGE IS LOCATED AT THE STRINGER WEB EXTENDING ABOUT 3 IN. THE AFFECTED STRINGER SPLICES TO THE MAIN DECK CARGO DOOR SURROUND STRUCTURE. TRIMMED OUT THE DAMAGSDR IXXA110068OFuel Tank · leakingDURING TAKEOFF, THE CREW SMELLED A STRONG FUEL ODOR IN COKPIT WITH PACKS OFF. THEY CONTINUED ON WITH THE FLIGHT AND LANDED WITHOUT FURTHER INCIDENT. MX TROUBLESHOT SYS AND FOUND FUEL LEAK AT INBD LT WING OVER WING ROOT. THEY CLEANED, RESEALED, LEAK CHECKED GSDR ABXA201011190156Skin · damagedLIGHTNING STRIKE DAMAGE AT BS 148 - BS 157. DAMAGE ENCOMPASSES UNDERLYING CHORD AT S27L. REPAIRED IAW B767 SRM 53-00-01 FIG 201 REPAIR 1. SKIN REPAIR DIMENSION ARE 18" X 9.5" EXTENDING FROM BS 143 TO BS 161.5 USING .090 2024 T3 DOUBLER. CUT OUT DAMAGE AT SSDR AALA20031007Wire · damagedLAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTING WAS OBSERVED TO BE INOPERATIVE IN THE AFT CABIN. REPAIRED ELECTRICAL WIRE CONNECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20021898Light · disconnectedJFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHTS AT SEAT 29H INOPERATIVE. RECONNECT EMERGENCY EXIT LIGHT ASSEMBLY TO HARNESS AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20021615Wire · damagedLAX - DURING OVERNIGHT MAINTENANCE, RIGHT EMERGENCY LIGHT BY FORWARD GALLEY INOPERATIVE. REPAIRED WIRE AT EMERGENCY EXIT LIGHT AT FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20021021Light · damagedLAX - DURING OVERNIGHT MAINTENANCE, LEFT AFT GALLEY UNDER FLIGHT ATTENDANT SET B1 DIRECTIONAL EMERGENCY EXIT LIGHT DAMAGED. REPLACED LEFT AFT GALLEY B1 DIRECTIONAL EMERGENCY EXIT LIGHT ASSEMBLY. (M)SDR AALA20020725Wire · damagedLAX - DURING OVERNIGHT MAINTENANCE, TWO FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS INOPERATIVE. REPAIRED FIRST CLASS FLOOR LEVEL EMERGENCY EXIT LIGHTS WIRE UNDER GALLEY FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20020212Connector · brokenSFO - DURING OVERNIGHT MAINTENANCE, FOUND EMERGENCY PATH LIGHTING AT SEAT 28H INOPERATIVE. REMOVED AND REPLACED BROKEN CONNECTOR AT LOWER SIDEWALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20011321Socket · defectiveLAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 32HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET AT SEAT 32HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA20011037Light · inoperativeSFO - DURING OVERNIGHT MAINTENANCE, R1 DOOR EMERGENCY EXIT EXTERIOR LIGHT ASSEMBLY INOPERATIVE. UNABLE TO ACCESS LIGHT ASSEMBLY WITHOUT REMOVING GALLEY. AWAITING MAINTENANCE SCHEDULING. (M)SDR AALA20001319Wire · brokenBOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 33A INOPERATIVE. REPAIRED WIRE AT SEAT 33A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)SDR AALA20004003Skin · corrodedAFW - WING BOX UPPER SKIN HAS CORROSION ON UPPER SURFACE. REMOVED FASTENERS, HFEC THE BLENDED AREA, SHOT/FLAP PEEN THE AFFECTED AREA PER SRM. APPLY ALODINE AND 2 COATS OF PRIMER TO AREA. REWORK EXISTING COUNTERSINK PER 767SRM 51-40-08 PER REF /C/. INSTALL SDR AALA991058Wire · brokenLHR - DURING ROUTINE MAINTENANCE, EMERGENCY EXIT SEAT LIGHTS AT SEATS 8HJ AND 34H INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRING AT SEATS 8HJ AND 34H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)SDR AALA981931Wire · brokenSFO - DURING OVERNIGHT MAINTENANCE, FORWARD GALLEY BIDIRECTIONAL EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPAIRED BROKEN WIRE AT FORWARD GALLEY BIDIRECTIONAL EMERGENCY FLOOR PATH LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA981526Light · inoperativeSFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY CEILING LIGHT AT SEAT ROW 7 RIGHT SIDE WOULD NOT ILLUMINATE. REPLACED EMERGENCY CEILING LIGHT ASSEMBLY AT SEAT ROW 7 RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA984172Beam · corrodedAFW - FOUND CORROSION IN THE BORE FOR THE AFT MLG TRUNNION BUSHING. THE BORE WAS HONED OUT TO A DIA OF 8.272 INCH, AFTER HONING SOME LOCAL PITTING REMAINED WHICH WAS BLENDED AND THE PITTING WAS IN THE 1R O'CLOCK AREA. (M)SDR AALA980317Connector · defectiveSFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT ROW 30HJ WOULD NOT ILLUMINATE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT ROW 30 HJ. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA971418Wire · brokenSFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT MID-GALLEY INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT WIRE BY MID-GALLEY LIGHT L9027. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA971261Idg · failedBOS - LEFT ONE LIGHT ILLUMINATED AND GEN DISCONNECTED. CONFIRMED DELTA P FILTER BUTTON POPPED. REPLACED LEFT IDG. NEW IDG DEFECTIVE FROM STOCK AS UNABLE TO RESET FIELD, S/N CO105 DFW. NEEDS ANOTHER IDG. NIS BOS. PLACARDED LEFT IDG INOP PER MEL REF 2401 ASDR AALA961891Idg · failedLGW - FLT 0174 - RIGHT GENERATOR DRIVE LIGHT AND GENERATOR OFF LIGHT ILLUMINATED AT FL 100 ABOVE GRD DURING APPROACH. REPEAT ITEM ACCOMPLISHED OM PROCEDURE. DISCONNECTED IDG. CHECKED RT IDG SCAVENGE FILTER. NO DEBRIS FOUND. SERVICED LT IDG TO FULL. CHECKSDR AALA961889Idg · failedBRU - FLT 0088 - RIGHT GENERATOR DRIVE EICAS MESSAGE WITH ASSOCIATED RT GEN OFF LIGHT. REPLACED SCAVENGE FILTER (SMALL CHIPS FROM NORMAL WEAR). LOW OIL PRESSURE+UNDERFREQ TRIP+IDG/PMG WIRING ON BPCU BIT. IDG REMAINS DISCONNECTED. IDG SERVICED. APU SERVICESDR AALA961217Housing · defectiveSFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 3H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING AT PAX SEAT 3H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)SDR AALA950054HFitting · damagedAFW - EDGE DAMAGE BEYOND SRM 57-20-90-1 FIG 101 DETAIL V LIMITS. BLENDED DAMAGED AREA, NDT INSPECT, FLAP PEEN AND RESTORE FINISH PER ENGINEERING MRB 767-1034. (M)SDR AALA950053HFloor Beam · corrodedAFW - FOUND CORRODED BEYOND LIMITS. CUT OUT DAMAGED FLOOR BEAM AND INSTALLED REPAIR SPLICE PER ENGINEERING MRB 767-1031. (M)SDR AALA950052HFail/Safe Strap · corrodedAFW - FORWARD CARGO DOOR FAIL/SAFE STRAP HAD CORROSION BEYOND SRM LIMITS. REMOVED CORROSION AND REPLACED FASTENERS PER ENGINEERING MRB 767-1023. (M)SDR AALA950051HStringer · corrodedAFW - REMOVED STRINGER SECTION, CORRODED BEYOND SRM LIMITS. FABRICATE LONGER SPLICE FROM SAME MATERIAL TYPE AND SHAPE PER ENGINEERING MRB 767-1032. (M)SDR AALA950050HFloor Beam · corrodedAFW - FLOOR BEAM HAS CORROSION BEYOND LIMITS. FABRICATED REPAIR DOUBLER FROM 0.050 CRES STEEL AND INSTALL WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1030. (M)SDR AALA950049HSkin · corrodedAFW - WING BOX SKIN HAS CORROSION BEYOND SRM LIMITS. BLENDED AND APPROVED FOR CONTINUED SERVICE PER ENGINEERING MRB 767-1029. (M)SDR AALA950048HFloor Beam · corrodedAFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS. FABRICATE REPAIR DOUBLER FROM 0.050 CRES AND INSTALLED WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1028. (M)SDR AALA950047HFloor Beam · corrodedAFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMTS. FABRICATE REPAIR STRAP FROM 0.050 THK CRES AND INSTALL WET PER ENGINEERING MRB 767-1027. (M)SDR AALA950046HFloor Beam · corrodedAFW - FLOOR BEAM HAS CORROSION BEYOND SRM LIMITS. FABRICATED REPAIR DOUBLER FROM .050 STAINLESS STEEL INSTALLED WET WITH BMS 5-95 SEALANT PER ENGINEERING MRB 767-1026. (M)SDR AALA950045HFloor Beam · corrodedAFW - FOUND FLOOR BEAM HAS CORROSION BEYOND LIMITS. ALODINED, FILLED WITH BMS 5-92 SEALANT. INSTALLED REPAIR STRAP WET WITH BMS 5095 SEALANT, PRIMED AND PAINTED PER ENGINEERING MRB 767-1025. (M)
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