N1013A
Service difficulty reports · 298
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 = 'N1013A' 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 = 'N1013A' 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 ABXA20261019472Generator · faultedL GEN DRIVE DISC LIGHT FLICKERING ON PUSHBACK AFTER ENGINE STARTA/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C. MTX DEFERRED LH GEN FOR DEPARTURE IAW MEL ABX MEL 24-00-1-1 MEL PROCEDURES C/W A/C DOWNGRADED TO ETOPS 120 PLACARD ROTATED MEL PLACARD INSTALLESDR ABXA20260923433Motor · defectiveDURING TAXI, LE SLAT DISAGREE. CREW RETURNED TO THE GATE (BTB). CHECKED WIRING OF ALTERNATE INBORAD SLAT DRIVE MOTOR M494 AND FOUND CB C324 POPPING DURNING ACT SYSTEM OPERATION PER WDM 2781-11. CONFIRMED M494 DRIVE MOTOR IN SHORT. REMOVED AND REPLACED RT (I/B)SDR ABXA20260801344Controller · malfunctionedL ENG BLEED OFF AND L PACK OFF EICAS LIGHT AND L ENG OFF (PNEUMATIC) VALVE LIGHT AND PACK OFF OVERHEAD LIGHT. C/X MC 227 AND CYCLED L ENG BLEED VALVE. AT 85% N2 AND VALVE NEVER OPENED, TOLD BY MAINTENANCE CONTROL TO RETURN TO THE GATE T/S AS PER FIM. 36-20 FTSDR ABXA20260731342Anti-Ice Valve · malfunctionedLEFT ENG ANTI-ICE VALVE ON TAXI. C/W NNC 3.3 CANNOT TAKEOFF REQUIRES HIGH THRUST CYCLED ENG ANTI ICE AND EICAS/ VALVE LIGHT DISAPPEARED CALLED DISPATCH & MAINTENANCE THEY SAID RTB A/C RETURNED TO GATE AND MTX GROUNDED A/C. MTX REMOVED AND REPLACED LEFT ENGINE SDR ABXA20260711313Audio Panel · malfunctionedDURING SERVICE CHECK FOUND CAPTAINS OXYGEN MASK MICROPHONE INOP. SWAPPED CAPTANS AUDIO PANEL WITH FIRST OBSERVERS, IAW AMM 23-12-02 OPS CHECK GOOD. AND DEFERRED . FIRST OBSERVER SEAT POS. IAW MEL 25-11-2-1A. RETURNED AC TO SERVICE.SDR ABXA20260625286Proximity Switch · malfunctionedENTRY DOOR LIGHT WON'T EXSTINGUISH WHEN ENTRY DOOR IS CLOSED. MTX DEFERRED L1 DOOR INDICATION FOR DEPARTURE IAW MEL ABX-52-71-1-1 .RETURNED AC TO SERVICE ,THEN LATER REPLACED PSEU IAW AMM 32-09-04.SDR ABXA20260625284Proximity Switch · defectiveDURING TAXI, STS MSG "LDG GEAR MONITOR" "MN CARGO DOOR IND". CREW RETURNED TO THE GATE (BTB). AFTER INTERROGATE PSEU MSG CODE 006 SHOWS R/R PSEU IAW AMM 32-09-04 OPS CHECK OK MESSAGES CLEARED. A/C RETURNED TO SERVICE.SDR ABXA20260624278Hmu · defectiveDURING CRUISE LEFT ENG LOST PARTIAL PWR, WOULD NOT ADVANCE BEYOND 67.5 N1 AND 22 FF ON FINAL PWR APPEARED TO RESTORE. ACFT DIVERTED TO ORD AND AN EMERGENCY WAS DECLARED. REMOVED AND REPLACED NR 1 ENG HMU IAW B767 AMM 73-21-14 OPS AND LEAK CHECK GOOD. NO FURTHESDR ABXA20260511194Pitot Head · malfunctionedDURING TAXI OUT,LE SLAT ASYM CAUTION MSG AND LIGHT ON AFTER START CHECKLIST. SEEMS TO HAPPEN WHEN SELECTING APU OFF WHILE FLAPS ARE IN TRANSIT.A/C RETURNED TO THE GATE AND MTX GROUNDED A/C MTX T/S LE SLAT ASYM MSG PER B767 FIM 27-81 FT 809 FOUND MAIN BATTERY ISDR ABXA20260320122Cowl Door · missingDURING MAINTENANCE INSPECTION, FOUND PANEL 446AL ON #2 ENG I/B PYLON MISSING. REPLACED PANEL 446AL IAW AMM 54-53-01. THIS CLOSES DI# 71620. PLACARD REMOVED. NO MX ACTIONS TO C/W REF LP 39398-16/2. AIRCRAFT RETURNED TO SERIVCE.SDR ABXA20260314108Stiffener · crackedDURING C6 CHECK, FOUND CRACKED STIFFENER ON FLOOR SUPPORT BEAM AT STA 246 AND RBL40. (BETWEEN NLG CENTER BOX AND FLIGHT DECK FLOOR STRUCTURE) (NR 0078). MAINTENANCE REMOVED DAMAGE ANGLE STIFFENER. INSTALLED 1 EA NEW ANGLE STIFFENER AT FLOOR SUPPORT BEAMEAT STSDR ABXA20260206055Fire Loop · faultedDURING MAINTENANCE INSPECTION, MAIN CARGO LOOP 1 & 2 INTERMITTENT. RESTORE AIRCRAFT POWER ON IAW AMM 26-22-00. PERFORM T/S IAW FIM 26-14 FT 809. SYSTEM TEST OK. NO FAULTS FOUND AT THIS TIME. AIRCRAFT RETURNED TO SERVICE.SDR ABXA2026020231043Start Valve · failedON TAXI OUT WHILE STARTING LEFT HAND ENGINE START VALVE DID NOT OPEN ,LEFT STARTER EICAS MESSAGE APEARED. AC RETURNED TO THE GATE AND MTX GROUNDED AC AND DEFERRED LH START VALVE FOR DEPATURE IAW MEL ABX-80-00-2-1.AND RETURNED AC TO SERVICE.SDR ABXA20260129035Start Valve · faultedON TAXI OUT, LEFT ENGINE EICAS LEFT ENGINE START AND OVERHEAD VALVE LIGHT ILLUMINATED DURING START. ACFT RETURNED TO BLOCKS (BTB). CYCLED START VALVE AND ACCOMPLISHED NR 1 ENGINE START IAW AMM 71-00-00, NO FAULTS NOTED DURING ENGINE START A/C REMAINS NO ETOSDR ABXA20260127030Warning Message · illuminatedDURING TAXI OUT, LEFT ENGINE EICAS, LEFT ENGINE START AND OVERHEAD VALVE LIGHT ILLUMINATED DURING START. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED IAW B767 MEL 80-00-2-1. MBCB 02-06-2026. PLACARD INSTALLED, MAINTENANCE PROCEDURE C/W. A/C REMSDR ABXA20251231365Fire Loop · false indicationAFTER LANDING STATUS MSG "MN CARGO LOOP 2" ILLUMINATED. ACCOMPLISHED FIM 26-14 FT 809 BLOCKS 1-2-3-4-5-6 AND 7 AFTER AFOLTS TEST, NO MN CARGO LOOP 2 PRESENT. CARGO SMOKE DETECTION SYSTEM OK. AIRCRAFT RETURNED TO SERVICE.SDR ABXA20251212331Pcb · defectiveRED MAIN DECK CARGO FIRE WARNING WITH ASSOCIATED LIGHTS AND MASTER CAUTION INTERMITTENTLY EVERY 5 MINS.MTX GROUNDED A/C .MTX REMOVED AND REPLACED PRINTED CIRCUIT CARD IN P54 M2026 IAW B767 AMM 26-10-01 & OPS CHECKS GOOD & NO FAULTS NOTED AT THIS TIME. AND RETUSDR ABXA20251212330Overheat Loop · false indicationINTERMITENT MN CARGO LP 1 AND 2 STATUS MESSAGE W/FIRE WARNING.MTX GROUNDED A/C AND PERFORM MAIN CARGO/ENG/APU/FIRE/OVHT TEST. IAW AMM 26-14-00. OPS CHECKED NORMAL. NO MSG. RETURNED ACFT TO SERVICE.SDR ABXA20251019274Battery · faultedDURING TAXI ,APU BATTERY, NO STBY STATUS MESSAGE DISPLAYED. ADVISED BY MTC TO RETURN TO PARKING (BTB). MTX GROUNDED ACFT AND REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04 AND REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-04. OPS CHECK GOOD. ACFSDR ABXA20250708143Warning Message · illuminatedPER MXC REQUEST VERIFY LOCK POSITION IN MCD , A/C RETURNED TO THE GATE AND GROUNDED BY MTX, MTX THEN VERIFIED LOCK RBL:33, LBL:33 +LBL:11 PREVIOUSLY INSTALLED IN STA.756.45, RELOCATED TO STA.755.45 IAW BCF CMM 25-51-70. ALL LOCKS SECURED. AND RETURNED A/C TO SSDR ABXA20250527106Director · malfunctionedAFTER TAKE-OFF, RT FLIGHT DIRECTOR DISAPPEARED TROUBLE SHOT IT AFTER 18K AND COULDN'T GET RESOLUTION SWITCHED RIGHT SIDE TO CENTER AND SGL SOURCE FD TCAS MSG APPEARED. MX MADE CALL TO RETURN TO AFW, (ATB) DEFERRED RT FLIGHT DIRECTOR SYSTEM IAW MEL C ABX-34-SDR ABXA20250305053Pump · warning messageDURING TAXI, L FWD FUEL PUMP EICAS MSG DISPLAYED AFTER ENGINE START. A/C RECTURNED TO GATE. (BTB) DEFERRED L FWD FUEL PUMP FOR DEPARTURE IAW MEL ABX-28-22-1. MTX RETURNED A/C TO SERVICE.SDR ABXA20241111222Pump · inoperativeDURING TAXI OUT THE RIGHT HAND AFT FUEL PIMP INOP MSG APPEARED AFTER ENGINE START A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C . MTX FOUND INCORRECT BREAKER WAS LOCKED OUT FOR LH PUMP DEFERRAL . RESET RH BREAKER AND COLLARED CORRECT BREAKER.OPS CHECK GOOD RSDR ABXA20241111221Pump · warning messageDURING TAXIOUT THE L FWD FUEL PUMP EICAS MSG APPEARED AND AC RETURNED TO BLOCK (BTB) AND MAINTENANCE GROUNDED AC .MTX DEFERRED LH FWD FUEL PUMP IAW MEL ABX-28-22-1 . AND RETURNED AC TO SERVICE .SDR ABXA20241103213Fire Warning · false activationDURING LOADING OF AIRCRAFT MAIN DECK CARO FIRE WARNING ACTIVATED MULTIPLE TIMES.FIRE DEPARTMENT CAME AND DECLARED NO SIGNS OF FIRE OR SMOKE IN MCD, OR LOWER CARGOS. MX PERFORMED TEST OF TAIM TEST BOXES PER B767 AMM 26-14-00, NO FAULTS NOTED. PERFORMED AFOLTS SSDR ABXA20241002183Warning Message · illuminatedAFTER ENGINE START L FWD FUEL PUMP EICAS ILLUMINATED DURING TAXI.AC RETURNED TO BLOCK AND MTX GROUNDED AC , DEFERRED FOR DEPARTURE .IAW MEL ABX-28-22-1 AC WAS RETURNED TO SERVICE AND AC DEPARTED .SDR UIEA2024052300416Shoe · wornNOSE LANDING GEAR BOTH BRAKE SHOES OF WHEELS UPPER GEAR WITH WEAR(<P>NOSE LANDING GEAR BRAKE SHOES OF WHEELS WERE REPLACED I.A.W. AMM 32-45-05-022-001 REV. 142 DATE 22 APR 24 AND AMM 32-45-05-422-007.REV. 142 DATE 22 APR 24. TORQUE APPLIED 35 IN LB , S/N 12229SDR UIEA2024052300417Metering Valve · leakingNOSE LANDING GEAR STEERING VALVE WITH HYDRAULIC LEAK IN THE BODY(<P>NOSE LANDING GEAR STEERING METERING VALVE WAS REPLACED IAW AMM 32-51-04-404-013 REV. 142 22-APR-24. OPS CHK GOOD.</P>)SDR UIEA2024052300418Bushing · excess playNOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS(<P>NOSE LANDING GEAR AFT DOORS BOTH WITH EXCESSIVE PLAY IN THE PIVOT POINTS, BUSHINGS WERE REPLACED AIW AMM 32-21-01-404-036 REV 142 22-APR-24 STEP H (29) TORQUE APPLIED 60 FT LB / SERIALSDR UIEA2024052300420Bonding Jumper · brokenMAIN LANDING GEAR WELL LH PART AFT LOWER (STA 1065 ) WITH BROKEN BONDING BUMPER ON APU FUEL DRAIN LINE(<P>MAIN LANDING GEAR WELL, LEFT REAR LOWER STA 1065 BONDING BUMPER REPLACED ON APU FUEL DRAIN LINE I.A.W SWPM 20-20-10 REV. 85 DATE 15 FEB 24 BONDING APPLIEDSDR UIEA2024052300421Vent · misinstalledRIGHT WING MAIN, TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE MISSING ON BOTH NUT RETAINER(<P>RIGHT WING MAIN TANK, BETWEEN RIB 19 AND RIB 18, FUEL DUCT VENT, LOCKWIRE WAS INSTALLED CORRECTLY IAW AMM 20-10-23-420-801 REV 142, APR 22,2023; TORQUE ASDR UIEA2024052300422Skin · dentedLH WING, INBOARD FLAP SURFACE LEADING EDGE AREA UPPER OUTSIDE CORNER WITH TWO DENTS.(<P>LH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 FIG 201 SHEET 5 PAG 2-6 AND SRM 51-70-17-0G-0 PAR 4.A FIG 10 PAG 13,14,34 REV 49 APR 15/-2024. NO FURTHESDR UIEA2024052300423None · noneFAA AGING INSPECTION RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WITH WIRES BROKEN.(<P>RH A/A PACK EXHAUST RAM AIR ACTUATOR BONDING LEAD WAS REPLACED IAW AMM TASK 21-53-03-404-012 REV. 142, APR 22, 2024. BONDING TEST WAS PERFORMED 0.003 MILLIOHMS. BONDINSDR UIEA2024052300424Control Cable · abnormalSECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STA 1605.5 LH SIDE.(<P>SECTION 48 INTERNAL AREA, LH ELEVATOR CONTROL CABLE RUBBING WITH PULLEY BRACKET (DUE BAD INSTALLATION) LOCATED AT B. STASDR UIEA2024052400437Skin · delaminatedRH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024.SDR UIEA2024052800463Skin · delaminatedRH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WITH DELAMINATION(<P>RH WING, INBOARD AILERON, TRAILING EDGE, RH SIDE WAS REPAIRED IAW SRM 57-60-01-2R-1 REPAIR 1 TABLE II FIG 201 PAG 1-6 AND SRM 51-70-03-0G-0 PAR 5A(2) FIG 12 PAG 10,11, 36 REV 49 APR 15/2024.SDR UIEA2024052400438Skin · corrodedPYLON #1 UPPER SURFACE, CORROSION DAMAGE ON THE BUSHING OF THE INBD LUG OF FWD UPPER SPAR FITTING.(<P>REPAIR FOR CORROSION DAMAGE ON THE BUSHING OF THE INB LUG OF FWD UPPER SPAR FITTING WAS ACCOMPLISHED IAW TRE 6754190 ISSUED DATE MAY 16,2024. FAA FORM 8100-9 SDR UIEA2024052400439Skin · dentedRH WING, INBOARD FLAP, MAIN FLAP, AT 2" FROM TRAILING EDGE AND 6" FROM INBOARD EDGE, DENT ON UPPER SKIN(<P>RH WING, INBOARD FLAP, MAIN FLAP WAS REPAIRED IAW SRM 57-53-01-2R-1 TABLE I FIG 201 SHEET 5 PAG.2,3,6 AND SRM 51-70-03-0G-0 PAR 5.A FIG.5 PAG 10,11,25 RESDR UIEA2024052400440Skin · puncturedLH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 SDR UIEA2024052400442Skin · puncturedLH INB ELEVATOR UPPER PANEL, PUNCTURE AT ELEV STA 104.2 APPROX. AND 28" FROM T.EDGE.(<P>LH INBOARD ELEVATOR, UPPER PANEL WAS REPAIRED IAW SRM 55-20-01-2R-1 REPAIR 1 FIG 201 TABLE I PAG 1-3, SRM 51-70-04-0G-0 PAR.5.B PAG.16 AND SRM 51-70-17-0G-0 PAR 4.B FIG.24 SDR UIEA2024052400441Fitting · corrodedLH WING FWD LOAD PITCH FITTING, CORROSION DAMAGE ON INB FITTING.(<P>CORROSION ON INBD FITTING WAS REWORKED IAW TRE6757246, REV 1, MAY 20, 2024. LEVEL CORROSION 2. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2023053000529Evas Unit · unknownCAPTAINS EVAS IS INOP(<P><SPAN>REMOVED AND REPLACED CAPTAINS EVAS AS PER 25-60-00 (AMM) OPS CHECKED NORMAL.</SPAN></P>)SDR UIEA2023050800425Smoke Goggles · unknownFIRST OBSERVERS SMOKE GOGGLES INOP(<P>TRANSFERRED TO MDDR 185104 PER MEL 25-11-02-01A CAT A DUE 17MAT23. PLACARDS INSTALLED. LOGPAGE 1773702 M3: REMOVED AND REPLACED FIRST OBSERVERS SMOKE GOGGLES IAW AMM 25-64-00. THIS ACTION CLEARS DMI 185109. MCC NOTIFIED. PSDR UIEA2022102601174First Aid Kit · noneFIRST AID KIT NEXT TO OVHEAD BIN COMPROMISED MISSING RED SEAL.(<P>REMOVED AND REPLACED FIRST AID KIT IW B767 AMM 25-64-03.</P>)SDR UIEA2022102201170None · noneCORROSION DAMAGE ON RIGHT INBOARD TE FLAP TORQUE TUBE(<P>RIGHT INBOARD TE FLAP TORQUE TUBE WAS REPLACED IAW SB 767-57A0066</P>)SDR UIEA2022102201169None · noneTHREE DENTS ON ENGINE #2 PRIMARY EXHAUST OUTER SKIN BETWEEN 6/8 O´CLOCK AND BETWEEN NAC STA 323.42/344.67(<P>WELD FILL REPAIR IAW BOEING MSG: CMA-TLS-22-0022-02B</P>)SDR UIEA2022102101168None · noneCORROSION ON ACCESS PANEL SUPPORT FOR KEEL BEAM BETWEEN STA 889 TO STA 915.5(<P>ACCESS PANEL SUPPORT P/N 145T8629-2 WAS REPLACED PER PRODUCTION DRAWING AND SRM 51-10-02</P>)SDR UIEA2022102101167None · nonePUNCTURE ON LH ELEVATOR LOWER SKIN AT 44 INCH OF THE INBOARD CLOUSURE RIB AND 26 INCH OF THE TRAILING EDGE.(<P>AFFECTED AREA WAS REPAIRED ON LH ELEVATOR LOWER SKIN IAW SRM 55-20-01-2R-1 & 51-70-17-0G-0</P>)SDR UIEA2022102101166None · noneRH WING OUTBOARD FLAP ACCESS PANEL "666KT" WITH DENT AT 33 INCH FROM EXTERNAL PANEL EDGE & 25 INCH FROM FLAP TRAILING EDGE AND SECOND ONE AT 68 INCH FROM EXTERNAL PANEL EDGE & 25 INCH FROM FLAP TRAILING EDGE.(<P>DENTS WERE REPAIRED PER SRM 57-53-01-2R-1 AND 51SDR UIEA2022102101165None · noneRH WING OUTBOARD FLAP ACCESS PANEL "666MT" WITH DENT AT 5 INCH FROM INTERNAL PANEL EDGE AND 25 INCH FROM FLAP TRAILING EDGE(<P>DENT WAS REPAIRED PER SRM 57-53-01-2R-1 AND 51-70-10-2R-0.</P>)
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