N13113
Service difficulty reports · 126
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 = 'N13113' 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 = 'N13113' 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 CALA2025032403150Coffeemaker · failedFORWARD GALLEY LEFT COFFEE MAKER DOES NOT WORK AND ELECTRICAL BURN SMELL WHEN TURNED ON FOUND COFFEMAKER HOTPLATES ON WITH POTS ON AND NO LIQUID. TURNED OFF HOTPLATES, RAN A COUPLE OF BREW CYCLES. OPS CHKS NORMAL, NO ELECTRICAL SMELL.SDR CALA2025031402824Lanyard · out of positionDOOR 1L WONT ARM FOUND LANYARD STUCK IN DOOR GIRT BAR MECHANISM. REPOSITIONED LANYARD BACK IN PLACE, ARMED AND DISARMED DOOR SEVERAL TIMES AND NO DEFECTS NOTED. USED RENDER SAFE CHECKLIST AS REQUIRED. ADD EMP:U246571SDR CALA2025030702613Engine · vibrationR ENG N1 VIBRATION REACHED 5.0 FOR 20 MINS PER CREW, AT FL340 IN WEATHER AND RIGHT BEFORE THEY GOT A VIBRATION INDICATION, THEY SMELT OZONE, WHICH THEY SAID WAS THE FIRST INDICTION OF CRYSTAL ICING. VIB LEVEL AT THIS POINT WAS 2.5. FIRST STEP IN QRH WAS ENG HESDR CALA2025021702353Girt Bar · fodDOOR 1R WILL NOT ARM CLEARED DEBRI UNDER GERT BAR, ARMED AND DISARMED DOOR , OP'S CK NORMAL,SDR CALA2025020702246Contact · dirtyDOOR 1L SLIDE LIGHT NOT ILLUMNATING VERIFIED GIRT BAR MECHANISM FOR FREEDOM OF MOVEMENT AND SECURITY. REF TASK 25-66-10-202-039. CLEANED CONTACTS. SLIDE ARMED. OK TO CONTINUE.SDR CALA2024123001690Cone · missingGAP FAIRING AFT SIDE OF #1 PYLON IB SIDE JUST ABOVE ENGINE EXAUST CONE MISSING/ DAMAGED REPLACED MISSING GAP FAIRING WITH NEW AT AFT SIDE OF #1 PYLON IB PER IPC 71-00-02-04.SDR CALA2024110801083Lamp · inoperativeEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK {MULT-33-3-0001} - R/H EMERGENCY OVERWING LIGHT INOP REMOVED AND REPLACED OVERWING EMERGENCY LIGHT IN REFERENCE WITH AMM 33-51-06. OPS CHECK GOODSDR CALA2024110801082Lamp · inoperativeEMERGENCY LIGHTS (USING CONTROL SWITCHES) OPERATIONAL CHECK {MULT-33-3-0001} - #2 L/H DOOR EMERGENCY SLIDE LIGHT INOP REMOVED AND REPLACED LIGHT IN REFERENCE WITH AMM 33-51-06. NO HELP. ALSO CHECKED BATTERY PACK FUSES FOR CONTINUITY, ALL 4 FUSES ARE GOOD. REMOSDR CALA2024110601053Elec Connector · unsecureREPEAT WRITE UP RTO 80 KTS ENGINE 2 WILL NOT GO ABOVE 1.5 EPR REFERENCE FIM 71-06 TASK 807 FOR TROUBLESHOOTING. TOMC-MEREDITH CARRIED OUT TROUBLE SHOOTING AS PER FIM 73-21-00-301. EEC BITE CARRIED OUT PER FIM 73-21-00-902-001-R01, BITE SHOWS FAULT CODE 35 (LVSDR CALA2024080702174Actuator · failedLEADING EDGE SLAT DISAGREE AFTER TAKEOFF, FLAPS STUCK BETWEEN UP & 1 UNTIL ALT SYS USE. PERFORMED T/S WITH TECH SUPPORT AND FIM 27-51 FAULT TREE 805 SLAT DISAGREE, FOUND MESSAGE #310, DURING INSPECTION FOUND L/E PDU OVERLOAD INDICATOR ON LT & RT PDU TORQUE LISDR CALA2024022000484Lavatory · handler errorALL LAVS OVER SERVICED. SERVICED LAVS AS REQUIRED. OPS CHECK GOOD REF AMM TASK 12-17-01-613-001 ADD EMP:U348948SDR CALA2024020100274Transmitter · faultyLE SLAT DISAGREE. INSPECTED INSTALLATION, AND CORRECT RIG OF LH LEADING EDGE SLAT TRANSMITTER, REF AMM 27-58-01-501, NO DEFECTS NOTED. LOCKING UNLOCK REPLACED LEFT HAND LEADING EDGE SLAT POSITION TRANSMITTER. OPS CHECK GOOD. REF. AMM 27-88-01-024-001. TRANSMITSDR CALA2023090802741Accumulator · unknownHYDRAULIC MOTOR GENERATOR ACCUMULATOR GAUGE IS AT "0" PSI IN THE HYDRAULICS BAY ACCESS. PLEASE SEE ATTACHED PICTURES. HYDRAULIC MOTOR GENERATOR INOP, COMPLIED WITH MEL. COMPLIED WITH MEL. ADD EMP: U162957, U116736 DISPATCH DESK: 3392 NAME: KB DATE: 05-SEP-23-SDR CALA2023071202229Skin · damagedDAMAGE OCCURRED TO AIRCRAFT FROM BOARDING STAND LEFT SIDE OF FUSELAGE 10 INCHES AFT OF STA 580 AT STRINGER 20L. .057" WIDTH 1.10" A/Y=19.2 ALLOWABLE A/Y=30. REPAIRED AREA IAW 0100-0191. B757-200 SRM 53-00-01-2R-28 REPAIR 28. ACCOMPLISHED ON AMES NR EVALUATED DSDR CALA2023063002079Flange · corrodedFLANGE CORRODED ON THE APU RAM AIR INLET DOOR BOX REMOVED AND REPLACED FWD STRAP AT THE APU RAM AIR INLET DOOR BOX AT STA 1785. THE SSFR WAS COMPLETED AND UP DATED.SDR CALA2023061601889Frame · crackedFRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). FRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). ADD EMP:V921218SDR CALA2023061401857Unknown · corrodedCORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. CORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. ADD EMP:V921493SDR CALA2023061401856Unknown · crackedFRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). FRAME ATTACH BRACKET FOR OVERHEAD BIN IS CRACKED @ STA. 1120 L/H STRINGER 8. D. OSBORNE V921218 (M). ADD EMP:V921218SDR CALA2023061401855Frame · crackedCRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). CRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). ADD EMP:V931845SDR CALA2023061401850Frame · crackedFRAME CRACKED AT STA 760 BELOW STR 8-R UPPER CABIN AT ATTACH BRACKET RIVET HOLE FOR OVER HEAD STOWAGE BINS. V931857SDR CALA2023061601888Frame · crackedCRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). CRACK ON FRAME WEB ATTACH BRACKET FOR OVERHEAD BIN @ STA 760 L/H @ STRNGR 8. D. OSBORNE V921218 (M). ADD EMP:V931845SDR CALA2023061601887Floorbeam · corrodedCORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. CORROSION FOUND ON TOP OF FLOOR BEAM AT STA 720 BL 20R. DOCUMENTED ON AMES NR 159536-0200-0147. ADD EMP:V921493SDR CALA2022100702738Warning Light · illuminatedLEFT HYD QTY EICAS MSG WHEN ACFT WAS ON THE RUNWAY AND THROTTLES MOVED UP. SHOWED .27 THEN RECOVERED. PER CREW THE ACFT WAS 3 KNOTS OR LESS WHEN EVENT OCCURRED.NO LOW PRESSURE OR OVERHEAT INDICATIONS. PERFORMED LEFT HYDRAULIC SYSTEM QUANTITY CHECK. REF AMM 29-SDR CALA2022060201426Shutoff Valve · looseR BLEED EICAS ON TAKEOFF WHEN THRUST SET. REJECTED T/O AT 50KTS FOUND LOOSE MUSCLE LINE ON HIGH PRESSURE SHUTOFF VALVE. SECURED LINE RAN ENGINE AT MULTIPLE POWER SETTING NO FAULTS FOUND. OPS NORMAL ADD EMP:012816SDR CALA2022011800168Seat Track · crackedSEAT TRACK AT STA 1540 LBL 44 FOUND CRACKED REPORTED BY V921297 REMOVED AND REPLACED SEAT TRACK @ STA 1540 LBL 44 IAW UAL EC/RA 5300-02793, B757 SRM 51-40-02 PARA 7, AND BOEING B757 DWG 146N51 20 & REA 47485FAB01 REF NR 142974-0200-0060 FOR DETAILSSDR CALA2018062101487Life Raft · unlacedFOUND THE LEFT OVERWING EMERGENCY EXIT RAFT, ROW 21 ABC, LACING UNDONE. REPLACED THE RAFT.SDR CALA2018012600312Thrust Reverser · failedRIGHT REVERSER FAILED TO DEPLOY ON LANDING, SEVERAL ATTEMPTS MADE. DEPLOYED ON TAXIWAY. BLED HYDRAULIC SYSTEM FOR THE NR 2 ENGINE THRUST REVERSER IAW AMM 78-31-20-085-R04. THRUST REVERSER IS OPERATING NORMAL.SDR CALA2017121904523Smoke Detector · false activationDURING CLIMB EICAS DISPLAYED LAVATORY SMOKE. AFT RIGHT LAVATORY SMOKE ALARM SOUNDED. NO SMOKE OR ODOR PRESENT. EMERGENCY DECLARED. REMOVED AND REPLACED SMOKE AFT RIGHT REF TASK 26-14-00-735-001 OPS CK OK.SDR CALA2017050501243Intercostal · corrodedCORROSION ON THE FWD CARGO COMPARTMENT FLOOR STRUCTURE INTERCOSTAL LOWER ATTACH ANGLE BETWEEN BS 740 AND BS 760 RBL 10.75. REMOVED UNSERVICEABLE INTERCOSTAL FWD CARGO BS 740-760 RBL 10.75 IAW SRM 51-40-02 PAR 4, FABRICATED NEW INTERCOSTAL AND INSTALLED IAW SRMSDR CALA2017042801156Floor Support · corrodedFLOOR WEB AT BS 1400 RT BL 70 HAS SURFACE CORROSION. EVALUATED CORROSION ON FLOOR WEB AT BS 1400 RBL 70 AND FOUND SMALL AREA OF 100% MAX LOSS. REMOVED, FABRICATED, LOCATED , DRILLED AND INSTALLED NEW -46 WAS IAW SRM 51-40-02 PAR 7 FIG 1 2 AND DRAWING 146N5590.SDR CALA2017042101072Skin · gougedLEFT FUSELAGE SKIN BS 1580 ABOVE STRINGER 15L HAS TWO GOUGES AND ALSO DENTED. CUT AND REMOVED DAMAGED AREA, AND REPAIRED IAW SRM 53-00-01, REPAIR 3, FIG 201.SDR CALA2017042101060Doubler · damagedEXTERNAL SKIN DOUBLER DAMAGED BS 608 ABOVE 17L. THE DOUBLER WAS REMOVED AND REPLACED IAW SRM 53-00-01, REPAIR 3, FIG 201, REPAIR STEPS 1-5, REPAIR 3.SDR CALA2017041400966Intercostal · corrodedCORROSION FOUND IN AFT CARGO COMPT BILGE INTERCOSTAL BETWEEN BS1320 AND 1340 LBL11 VALUATED CORROSION ON AFT CARGO INTERCOSTAL BTWN BS1320 & 1340 LBL 11. FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00 -04 FIG 101 DETAIL 2. REMOVED AND REPLACED INTERCOSTAL ISDR CALA2017040800927Strap · corrodedCORROSION ON THE MAIN CABIN FLOOR STRUCTURE REPAIR DOUBLER BS 720 BETWEEN RBL 15.5 AND RBL 45.5 UPPER SURFACE EVALUATED CORROSION ON MAIN CABIN FLOOR STRUCTURE REPAIR DOUBLER BS 720 AT RBL 15.5 TO RBL 45.5. ORIGINAL MAT THICKNESS IS .071 MATERIAL REMOVED .059 SDR CALA2017032400693Floor Support · brokenMAIN CABIN FLOOR SUPPORT UPPER ATTACH ANGLE IS BROKEN BETWEEN BS 480 AND 500 RBL. 10.5. REPAIRED IAW SRM 51-40-02 PARA 7 FIG 12, AND SRM 51-40-05, PARA 4 FIG 1.SDR CALA2016091900657Unknown · odorAFT OVEN 412 GETTING AN ELECTRICAL ODOR WITH OVEN POWERED OFF. PULLED THE CIRCUIT BREAKER NO CHANGE. OVEN REMOVED AND AREA INSPECTED WITH NO FINDINGS OR ODOR. ALL OVEN CONTROLLER BOX UNPLUGGED AND CIRCUIT BREAKER PULLED AND COLLERED. OTHER GALLEY EQUIPMENT SDR CALA2016081500545Indicator · failedAT 100 FEET AGL DURING DEPARTURE, THE LEFT ALTIMETER FAILED. OFF FLAG IN VIEW UNTIL APPROX 100 FEET. REMOVED AND REPLACED THE LT ADC IAW AMM 34-12-01. REMOVED AND REPLACED CAPTAIN`S ALTIMETER IAW AMM 34-13-01. NO OFF FLAG PRESENT.SDR CALA2016071100419Line · leakingLEFT HYD QTY INDICATES ZERO. EICAS MESSAGES LT HYD QTY AND POWER TRANSFER UNIT ILLUMINATED. LEFT HYD SYSTEM WAS SELECTED OFF WHEN LEFT HYD QTY READ 30%. REMAIN OFF FOR THE REMIANING OF THE FLIGHT. BOTH DOWNLOCK LINES REPLACED, SERVICED HYDRAULICS, CHECKED LINESDR CALA2016032800190Warning System · false activationRIGHT ENG REVERSER LIGHT ILLUMINATED ON THE TAKEOFF R LL. INITIATED & COMPLETED A LOW SPEED REJECTED TAKEOFF AT 70 KNTS, OFF TIME WAS 1122 Z. COOLED BRAKES FOR 10 MINS BEFORE TAXIING. PLACARDED NR 2 ENG THRUST REVERSER INOPERATIVE. MX PLACED REVERSER ON MESDR CALA2014102401394Warning Light · intermittentINTERMITTENT APU DOOR LIGHT, APU STOPPED. EMER DECLARED. RAN APU SEVERAL TIMES NO FAULTS NOTED. R & R ECU PRECAUTION. ACFT PLACED ON ETOPS VERIFICATION LP 7928692.SDR CALA2014040100414Bulb · inoperativeEMERGENCY ESCAPE PATH LIGHTS HAVE BURNED OUT BULBS AT L2 DOOR LOWER PROXIMITY FWD, ROW 20 LT OVERWING LOWER PROXIMITY EXIT SIGN OVER THE OVERWING LT HAS 14 BURNED OUT BULBS. REPLACED BULBS IAW AMM 33-51-10, TESTED OK.SDR CALA2014040100413Skin · dentedDENT IN LOWER LT FUSELAGE BETWEEN STRINGERS 26 - 27L BS 510. FOUND TO BE WITHIN SRM 53-00-01 LIMITS. ACCOMPLISHED DOUBLER REPAIR BETWEEN BS 503 - 513 & STRINGERS 26 - 28L IAW ECRA 5331-01843.SDR CALA2014040100412Connector · inoperativeFIRST CLASS SEAT SHROUD EMERGENCY LIGHT INOPERATIVE. R & R CONNECTOR. PERFORMED OPS TEST OF EMERGENCY LIGHTS, CHECKED NORMAL IAW SWPM 20-61-28 & AMM 33-51-00.SDR CALA2014032600391Frame · dentedAFT CARGO PIT BS 1460 FRAME HAS MULTIPLE DENTS BETWEEN STRINGER 25L - 26L. FABRICATED DOUBLER FRAME REPAIR AT BS 1460 BETWEEN STRINGER 25L - 26L. TREATED & PRIMED TOP COATED REPAIR CYCLES AFTER THAT IAW SRM 53-00-07 FIG 201TABLE II IR DOUBLER AS PER SRM 51-2SDR CALA2014032600390Frame · dentedAFT CARGO PIT BS 1540 DENTED BETWEEN STRINGER 26L - 27L. FABRICATED DOUBLER FRAME REPAIR AT BS 1540 BETWEEN STRINGER 26L - 27L. TREATED & PRIMED TOP COATED CYCLES IAW SRM 53-00-07 FIG 201 TABLE II. REPAIR DOUBLER IAW SRM 51-20-01, INSTALLED NEW FRAME REPAIRSDR CALA2014032400385Skin · dentedSTR15L TO STR16L AREA, FUSELAGE SKIN DENT MARK FOUND. FOUND TO BE WITH IN LIMITS IAW SRM 53-00-01. ACCOMPLISHED REPAIR DOUBLER AS USING LFEC AS PER B757-2 SRM 53-00-01, REPAIR, TABLE V, PER B757-2 SRM 53-00-01 FIG 201, REPAIR 3, DETAIL I.SDR CALA2012120300829Power Supply · inoperativeEMERGENCY LIGHTS BY DOOR 1R INOPERATIVE. FOUND ALL LIGHTS POWERED BY CHARGER M730 INOPERATIVE. REPLACED M730 CHARGER IAW AMM 33-51-07-862-054.SDR CALA2012110200738Skin · dentedDENT IN SKIN AT BS 1486 BETWEEN S23- 24R. DENT IS APROX .025" DEEP APROX 1" IN DIA. REMOVED DAMAGED SECTION OF SKIN. FABRICATED DOUBLER. TREATED AND PRIMED AND INSTALLED IN REF TO SRM 53-00-01, FIG 201.SDR CALA2012110700760Skin · puncturedL4 ENTRY DOOR UPPER HINGE CUTOUT INNER SKIN HAS PUNCTURE. TRIMMED OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW EC/RA 520-02239,STEPS 1 THRU 12.SDR CALA2011120900802Battery · faultySTATUS MESSAGE "MAIN BAT CHGR". REPEAT WRITE-UP. AIR RETURN TO EWR. PERFORMED T/S PER FIM 24-31-00-815-802 PG 2; BLOCK 19. HARD FAULT REMOVED. REPLACED MAIN & APU BAT. AS PRECAUTIONARY ACMX MEASURE PER TOMC MAA #7993 IAW 777-200 AMM TASK 24-31-01 & 03.
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