N313AA

Service difficulty reports not matched to an aircraft · 34

They name N313AA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N313AA' AND registry_match IS NULL
  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.

SDR ABXR201072000023ACheck Valve · cracked(ABXR) DURING A MX INSP EVENT, WHILE DOING AN INSP OF THE NR 1 ENG 8TH STAGE CHECK VALVE IAW AD 90-12-02 IAW SB 36-2078, REV 2, FOUND APPROX A 1 INCH CRACK IN THE CONE SEAT AREA. R & R THE VALVE IAW MM.Sep 16, 2008 · N313AA · Boeing 767223 · Pneumatic Distribution SystemSDR AALA20020795Idg · failedJFK - FLT 679 - DURING TAKEOFF RECEIVED EICAS MESSAGES, RIGHT GEN OFF, RIGHT GEN DRIVE LT, AND RIGHT UTIL BUS RESET GEN DRIVE LIGHT ON STEADY. COMPLETED CHECKLISTS, RETURNED AND LANDED. REMOVED RIGHT IDG. INSTALLED NEW IDG OPS AND LEAK CHECK OK. (M)May 29, 2002 · N313AA · Boeing 767223 · AC Generation SystemSDR AALA20020834Idg · failedJFK - FLT 679 - EN ROUTE JFK-AUA - RIGHT ENGINE IDG FAILED. RETURNED JFK LANDING WITHOUT INCIDENT. REPLACED RIGHT ID GENERATOR. PERFORMED OPERATIONS CHECKED PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 29, 2002 · N313AA · Boeing 767223 · AC Generator-AlternatorSDR AALA20010909Battery Pack · dischargedJFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS FLICKER AT ROWS 30 THROUGH 37 LEFT. REPLACED BATTERY PACK FOR ROWS 30 THROUGH 37. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)May 3, 2001 · N313AA · Boeing 767223 · Emergency LightingSDR AALA20010166Light · damagedBOS - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT MID GALLEY DAMAGED. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jan 30, 2001 · N313AA · Boeing 767223 · Emergency LightingSDR AALA20000408Wire · damagedJFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHT AT ROW 35 INOPERATIVE. REPAIRED WIRE AT SEAT 35A. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Mar 8, 2000 · N313AA · Boeing 767223 · Light System WiringSDR AALA991696Girt Bar · brokenSFO - DURING OVERNIGHT MAINTENANCE, RIGHT SLIDE PACK RELEASE BAR BRACKETS BROKEN. REPLACED RIGHT SLIDE PACK. SYSTEM GROUND CHECK NORMAL OPERATION. (M)Nov 8, 1999 · N313AA · Boeing 767223 · Escape SlideSDR AALA991175Connector · looseMIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B INOPERATIVE. RESECURED CONNECTOR TO EMERGENCY EXIT FLOOR PATH LIGHTS AT SEATS 28B AND 32B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Aug 14, 1999 · N313AA · Boeing 767223 · Emergency LightingSDR AALA984259Floorbeam · corrodedAFW - FLOORBEAM AT STATION 1480 HAS CORROSION REMOVAL ON UPPER SURFACE. BLENDED OUT CORROSION, ALODINE AND PRIMED ALL BLENDS AND REPAIR PARTS WITH 2 COATS BMS 10-11 PRIMED. FILLED BLENDS WITH BMS 5-95 SEALANT. INSTALLED 301 1/2H STAINLESS STEEL STRAP WET WIDec 14, 1998 · N313AA · Boeing 767223 · Fuselage Main, Floor BeamSDR AALA981416Connector · failedSFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 37B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT SEAT 37B. SYSTEM GROUND CHECKED NORMAL OPERATION. (X)Jul 21, 1998 · N313AA · Boeing 767223 · Emergency LightingSDR AALA981283Coffee Maker · failedLHR - FLT 0046 - EN ROUTE ORD/LHR - BUSINESS CLASS NR 3 COFFEE MAKER EMITTED SMOKE. TURNED OFF COFFEE MAKER. LANDED LHR WITHOUT INCIDENT. REPLACED NR 3 COFFEE MAKER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)Jun 29, 1998 · N313AA · Boeing 767223 · Buffet/GalleysSDR AALA980094Fmc · failedLHR - FLT 0095 - IN-FLIGHT, RIGHT FMC FAILED. REPLACED RT FMC AND RT CDU. PERFORMED CROSS-LOAD PER SIC 2900. ALL OPS AND INDICATIONS NOW NORMAL. 31334F8FF/1520.09JAN.LHR. (X)Jan 9, 1998 · N313AA · Boeing 767223 · Flight Management Computing Hardware SystemSDR AALA971671Pin · needed reseatedSFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 31H INOPERATIVE. RESEATED PIN AT CONNECTOR FOR EMERGENCY EXIT LIGHT AT PAX SEAT 31H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 1, 1997 · N313AA · Boeing 767223 · Emergency LightingSDR AALA971670Light · defectiveSFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT HOUSING ASSEMBLY AT PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Sep 1, 1997 · N313AA · Boeing 767223 · Emergency LightingSDR AALA970721Idg · failedRIGHT GEN DRIVE LIGHT ILLUMINATED. RIGHT GEN DRIVE DISCONNECTED IN FLIGHT. PLACARDED RIGHT ENG IDG INOP PER MEL. ACCOMPLISHED MPM 24-01 ENTERED IN MIC. REMOVED AND REPLACED RIGHT IDG LEAK AND OPS CHECK NORMAL. REMOVED PLACARD NR 04-164DC-B. CLEARED MIC. Apr 10, 1997 · N313AA · Boeing 767223 · AC Generator-AlternatorSDR AALA970172Apu · low oilJFK - FLT 0105 - TAKEOFF + 1 HR RIGHT GEN CONT OFF LIGHT ILLUMINATED. TROUBLESHOT SYSTEM. REPLACED RIGHT IDG. ALL SYS CKS NORMAL. TAKEOFF + 4 HRS APU SHUT DOWN WITH FAULT LT OAT -53C FUEL -19C. SERVICED APU OIL TO FULL RAN APU FOR 5 HOURS. NO LEAKS FOUNDJan 16, 1997 · N313AA · Boeing 767223 · APU Oil SystemSDR AALA960874Connector · looseSFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29AB INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR ON BACK OF LIGHT ASSEMBLY AT PAX SEAT 29AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Jun 7, 1996 · N313AA · Boeing 767223 · Emergency LightingSDR AALA960243Wire · brokenSFO - DURING OVERNIGHT CHECK, MID-GALLEY EMERGENCY EXIT EGRESS LIGHTS INOPERATIVE. REPAIRED BROKEN WIRES AT MID-GALLEY FOR EMERGENCY EXIT EGRESS LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)Feb 7, 1996 · N313AA · Boeing 767223 · Light System WiringSDR AALA960194Skin · gougedAFW - FUSELAGE SKIN GOUGED FORWARD OF LOWER FORWARD CORNER OF FORWARD CARGO DOOR CUT-OUT. BLENDED GOUGE, PARENT MATERIAL .202 INCH THICK. LOW POINT OF BLEND .143 INCH THICK. APPROVED FOR CONTINUED SERVICE IN NOTED CONDITION BY ENGINEERING PER MRB 767-1110. Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Plate/SkinSDR AALA960193Stringer · corrodedAFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .70 INCH OF STRINGER FORWARD OF SPLICE. REMOVED ALL CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE. REPAIR APPROVED BY ENGINEERING PER MRB 767-1109. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Longeron/StringerSDR AALA960192Chord · corrodedAFW - FOUND AND BLENDED CORROSION IN TWO LOCATIONS ON INNER SURFACE OF FAIL-SAFE CHORD. REMOVED CORROSION. ROTO-PEENED TREATED AND PAINTED. APPROVED BY ENGINEERING PER MRB 767-1111. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR AALA960191Splice · corrodedAFW - STRINGER CORRODED. DAMAGE REQUIRED REMOVAL OF .90 INCH OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENINEERING PER MRB 767-1113. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR AALA960190Rear Spar · corrodedAFW - FOUND AND REMOVED CORROSION ON WING BOX REAR SPAR ASSY UPPER CHORD. CORROSION ALSO REMOVED FROM UPPER SKIN AT SAME LOCATION AND LOWER CHORD TO FLOOR BEAM (T-EXTRUSION) WAS CUT TO REMOVE CORROSION. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1116.Jan 24, 1996 · N313AA · Boeing 767223 · Wing SparSDR AALA960189Stringer · corrodedAFW - STRINGER CORRODED. DAMAGE REQUIRED THE REMOVAL OF 2.5 INCHES OF STRINGER AT AFT END OF SPLICE. REMOVED CORROSION. FABRICATED AND INSTALLED NEW REPAIR SPLICE. APPROVED BY ENGINEERING PER MRB 767-1112. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Longeron/StringerSDR AALA960188Skin · corrodedAFW - CORROSION REMOVED FROM CENTER WING UPPER SKIN AT AFT DRAINS LOCATIONS. APPROVED AND REPAIRED PER INSTRUCTIONS OF MRB 767-1117. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Wing, Plate/SkinSDR AALA960187Floor Beam · corrodedAFW - FOUND AND REMOVED CORROSION ON FLOOR BEAM. AFTER BLENDING, FOUND BEYOND SRM LIMITS. EDDY CHECKED BLEND-OUTS. ROTO-PEENED AND REFINISHED BLENDED AREAS. APPROVED BY ENGINEERING PER MRB 767-1118. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Floor BeamSDR AALA960186Floor Beam · corrodedAFW - FLOOR BEAM CORRODED AND BLENDED ON THE UPPER OUTER SURFACE. FOUND THE BLEND-OUT EXCEEDED SRM LIMITS. REMOVED FLOOR BEAM SECTION FROM STA 849 TO STA 878. SPLICED IN NEW SECTION. APPROVED BY ENGINEERING PER MRB 767-1119. TST: 42,562.49 HRS. CYCLES, 1Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Floor BeamSDR AALA960185Floor Beam · corrodedAFW - FLOOR BEAM CORRODED. AFTER BLENDING, FOUND DAMAGE BEYOND SRM LIMITS. ALODINED BLENDED AREA. FABRICATED AND INSTALLED REPAIR STOP USING .050 INCH 301 1/2 HARD STAINLESS STEEL. APPLIED TWO COATS OF PRIMER. APPROVED BY ENGINEERING PER MRB 767-1124. TSJan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Floor BeamSDR AALA960184Chord · corrodedAFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE 146T1213-11 INNER CHORD. THE BLEND-OUT EXCEEDS SRM MAXIMUM LIMITS. REFINISHED BLENDED AREA PER SRM. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1123. TST: Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR AALA960183Floor Beam · gougedAFW - FLOOR BEAM WEB GOUGED. DAMAGE BLENDED AND FOUND BEYOND SRM LIMITS. FABRICATED AND INSTALLED .071 INCH THICK 7075-T6 DOUBLER. APPROVED BY ENGINEERING PER MRB 767-1126. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, Floor BeamSDR AALA960182Chord · corrodedAFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD IN AFT CARGO. PRIMED AND FILLED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1131. TST: 42,562.49 HRS. CYCLES, 10,821. (X)Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR AALA960181Chord · corrodedAFW - OVERSIZED EXISITNG HOLE ON CHORD TO ELIMINATE INNER GRANULAR CORROSION. INSTALLED FREEZE PLUG IN HOLE AFTER DRILLING. DRILLED NEW HOLE THROUGH FREEZE PLUG. CHORD TO BE REPLACED AT NEXT MBV. APPROVED BY ENGINEERING PER MRB 767-1132. TST: 42,562.49 HJan 24, 1996 · N313AA · Boeing 767223 · Fuselage Miscellaneous StructureSDR AALA960180Bulkhead · corrodedAFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE MAIN CABIN PRESSURE DECK. BLEND-OUTS EXCEEDED SRM MAXIMUM LIMITS. REMOVED CORROSION, ROTO-PEENED. ALODINED, PRIMED, AND PAINTED. APPROVED BY ENGINEERING WITH NOTED CONDITION PER MRB 767-1115Jan 24, 1996 · N313AA · Boeing 767223 · Fuselage Main, BulkheadSDR AALA950514Eel Wire · brokenMIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT FIRST CLASS GALLEY INOPERATIVE. REPLACED BROKEN/SHORTED EMERGENCY FLOOR LIGHT WIRES AT FWD FLIGHT ATTENDANT SEAT. SYSTEM GROUND CHECKED NORMAL OPERATION.Mar 23, 1995 · N313AA · Boeing 767223 · Emergency Lighting
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