N14107
Service difficulty reports · 121
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 = 'N14107' 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 = 'N14107' 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 CALA2026080518317Skin · crackedLEFT WING LOWER O/B INTERSPAR SKIN AT PANEL 543BB IS CRACKED AT HOLE 27 AT THE 12-O'CLOCK LOCATION (ABOUT 0.74" LENGTH) AND AT THE 6-O'CLOCK LOCATION. SEE BAM N/R 3543867 AND EC/RA 5720-03647SDR CALA2026080518315Splice Plate · crackedTHIS ELB IS FOR ESFR/SDR REPORTING ONLY. LT WING INTER SPAR LOWER SKIN SPLICE AT WSTA 711.50 IS CRACKED AT HOLES 193, 194, 243, 244, & 245. SEE BAM N/R'S 3543867, 3563704 AND EC/RA 5720-03667 FOR WORK PERFORMED.SDR CALA2026080718357Skin Panel · crackedLEFT WING, LWR OTBD SKIN PANEL OTBD OF SPLICE AT WS 711.50, REPLACED BY INTERIM REPAIR PER PART 1 OF EC/RA 5720-03667 DUE TO FINDINGS. ACCOMPLISHED A PERMANENT REPAIR IAW PART 3 OF THE LATEST REVISION OF EC/RA 5720-03667SDR CALA2026080718355Skin · crackedLEFT WING LOWER OTBD WING SKIN.SDR CALA2026083119108Door Frame · crackedR2 DOOR FRAME CRACKED AT UPPER HINGE FRAME CUT OUT. REF ST SAA N/R 0038736.FOUND CRACK OUT OF LIMITS IAW SRM 52-10-02A1 L=.302. REPAIRED R2 DOOR FWD FRAME AT UPPER HINGE CUT OUT IAW SRM 52-10-02-R1, FIG 201. THIS IS CATAGORY B REPAIR WITH INSPECTION REQU IREMESDR CALA2026083119106Door Frame · crackedL2 DOOR FRAME CRACKED AT UPPER HINGE FRAME CUT OUT, 16-64. REPAIRED DAMAGE AT L2 DOOR FRAME UPPER HINGE CUT OUT IAW SRM 52-10-02, REPAIR 1 FIG. 201. THIS IS CATEGORY B REPAIR WITH INSPECTION REQUIREMENTS PER TABLE 203. 50,000 TOTAL DOOR F/C OR 1,900 F/C AFTERSDR CALA2026060916942Oven · odorOVEN 413 EMITTING STRANGE SOUND AND SMELL. FLIGHT ATTENDANT ELECTED NOT TO USE IT. OVEN 413 OLD LINER REMOVED AND DISCOVERED DEFORMED AND MAKING CONTACT WITH REAR OF OVEN. WHEN REMOVED AND REPLACED WITH NEW LINER, OPS CHECKED ALL NORMAL. NO NOISE OR BURNING SMSDR CALA2026060316785Light · inoperativeRIGHT OVERWING SLIDE FWD EMERGENCY LIGHT NOT ILLUMINATING, REMOVED AND REPLACED OVERWING FOWARD SLIDE LIGHT OPS CHECKED GOOD AT THIS TIME IAW AMM 33-51-06.SDR CALA2026042115571Oven · fireOVEN NR 1, SMOKING DURING FLIGHT. FAS INFORMED CREW, SMELLED LIKE FIRE BURNED FOOD CONTAINED WITHIN OVEN RACK . REMOVED AND REPLACED NR 1 OVEN IAW AMM 25-34-00-000-801-C3. PERFORMED AREA CLEANING IAW 25-31-05-167-002.SDR CALA2026042015486Oven · dirtySMOKE COMING OUT OF OVEN INTO CABIN, CREW DECLARING EMG AND AIR RETURNING TO EWR. RAN OVEN FOR 15 MINS NOT NOTICIABLE BURNING ODOR DETECTED, NOTE BURNING ODOR WAS COMMING FROM OVERSPILLED CARAMEL BEEN BURN INSIDE OVEN, FOUND NO EVIDENCE OF ELECTRICAL BURNINGSDR CALA2025092509278Pressure Switch · faultedRIGHT HYDRAULIC SYS EICAS & BRAKE SOURCE EICAS ON, WITH NORMAL SYS QTY & PRESSURE. CREW REPORTS BRAKE SOURCE LIGHT INFLIGHT WITH CORRESPONDING RT HYDRAULIC PRESSURE LIGHT. CREW NEVER NOTICED A RT HYD QTY DROP. TURNING OFF RT SIDE ENGINE PUMPS & RE-ENGAGING SDR CALA2025081507834Rope · unsecureL1 DOOR ROPE HANGING FROM BOTTOM OF DOOR REINSTALLED SLIDE COVER LOWER STRAP, REF AMM 25-26-01.SDR CALA2025081407717Switch · malfunctionedEMERGENCY LIGHTS UNARMED LIGHT ILLUMINATED WITH SWITCH IN ARMED OR ON POSITION WIGGLED ON LIGHT SWITCH, UNARMED LIGHT EXTINGUISHED, TOGGLE SWITCH OP CHECKED NORMAL AS WELL, OK TO CONTINUE.SDR CALA2025070306188Panel · missingUPON ETOPS WALK AROUND FOUND PANEL ON LEFT SIDE OF LEFT PYLON MISSING REF IPC 54-53-01-05 DETAIL A ITEM 180. CORRECTION IPC 54-53-01-05 ITEM NUMBER 175 DOOR ASSY. LEFT ENGINE PYLON DOOR ASSY INSTALLED AND SECURE.SDR CALA2025060405268Module · faultedLDG GEAR MONITOR STATUS MESSAGE PERFORMED BITE CHECK , T/S AS PER FIM 32-09 FAULT TREE 804 AND DUE TO LANDING GEAR HANDLE FEELS LIKE ITS STICKING R & R LANDING GEAR CONTROL HANDLE MODULE IAW AMM 32-31-01-404-011 UP TO AND INCLUDING STEP 10(B). CONTINUED MX ACSDR CALA2025051304645Door · missingPDA 2 #1 ENGINE IDG SERVICE DOOR MISSING UPON LANDING AT SFO. A SDR REPORT MUST BE ACCOMPLISHED PDA CAT 2 # 1 ENGINE IDG DOOR WAS FOUND MISSING UPON LANDING AT SFO. OUR BELIEVE IS WHEN AIRCRAFT DEPARTING FROM EWR (FLT 1475) THE IDG DOOR WAS NOT FULLY LATCHED SDR CALA2025050104373Unknown · odorCREW REPORTS SMOKE IN THE CABIN WHILE PACKS RUNNING WITH APU BLEED. APU OIL SERVICED 7QTS IN 10 DAYS. RAN APU AND CYCLED BLEED VALVE SEVERAL TIMES. UNABLE TO DUPLICATE SMOKE IN CABIN. APU WAS REPLACED ON APRIL 27, SO OIL CONSUMPTION DOES NOT APPLY TO THIS APUSDR CALA2025022402432Switch · damaged. EMERGENCY LIGHT TEST WITH AT DOOR L2 HAS ONE PIN DAMAGED. SEE ST NON ROUTINE 121489. REMOVED ABD REPLACED EMERGENCY LIGHT TEST SWITCH AT DOOR L2 IAW SWPM 20-84-14. OPS CHECKS GOOD.SDR CALA2025022400409Pin · brokenLOG ENTRY FOR SDR REPORTING. EMERGENCY LIGHT TEST SWITH AT DOOR L2 HAS ONE PIN DAMAGED. SEE ST NON ROUTINE 121489. REMOVED ABD REPLACED EMERGENCY LIGHT TEST SWITCH AT DOOR L2 IAW SWPM 20-84-14. OPS CHECKS GOOD.SDR CALA2024112001204Housing · damagedREF. L/ P #9898533 FOUND DURING T/S OF 2L DOOR ARM LIGHT; ANNUN. LT. SW. BASE TERM. STUD BROKEN FROM HOUSING. (EQUIP# L405) REF. WDM 25-66-11-901. REQ P/N: 19-3350-2-0069. IN STOCK, ORDERED EWR. AT DOOR 2L, REMOVED AND REPLACED DOOR ARM ANNUNCIATOR LIGHT SWITSDR CALA2024093000723Liner · missingPDA 2 ON ENG 2 DISCOVERED MISSING ACOUSTIC ATTENUATOR LOCATED AT 9 OCLOCK POSITION. SEE PHOTO REMOVED AND REPLACED ENG NO.2 9 OCLOCK ACOUSTIC ATTENUATOR IAW MM 75-32-10 OK TO CONTINUESDR CALA2024081600442Pressure Switch · faultyCHECK LIGHTBULB IN OVHD BY ENTRY OF FLIGHT DECK LIGHT INOP AT THRESHOLD LIGHT OUTSIDE FLIGHT DECK. PHOTOS ADDED FOR LOC REF. REQUEST MEL 3321B FOR THRESHOLD LT OUTSIDE FWD LAV APPROVED MEL 3321B COMPLIED WITH RELAMPED (FWD LAV OUTSIDE CEILING BULB), OPS CHECSDR CALA2024081902234O-Ring · leakingRIGHT HYD SYS PRESSURE LIGHT AND EICAS ELECTRIC HYDRAULIC PUMPS. ALL HYDRAULIC QUANTITIES NORMAL. AUTO EVENT ATTACHED, SHOWS RSVR PRESS HIGH ON ALL 3 SYSTEMS. DURING CLIMB OUT AT FL180, RIGHT HYDRAULIC PRESSURE LIGHT INDICATOR ILLUMINATED AND EICAS MESSAGE. NOSDR CALA2024073100336Flex Line · faultyFLIGHT CREW STATES ON T/O WHILE BRINGING UP FLAP HANDLE NOTICED LT HYD QTY DECREASING, SELECTED BOTH LT EDP & LT ACMP OFF. LT HYD FLUID QTY NOW AT .15 PERCENT ON EICAS. AMM 29-11-00/201 CONDITION 1 TABLE 1. FOUND LEAK COMING FROM LT MLG DOOR ACTUATOR. FLEX LINSDR CALA2024072902131Hydraulic Line · rupturedFLIGHT CREW STATES ON T.O. WHILE BRINGING UP FLAP HANDLE NOTICED LEFT HYD QTY DECREASING : SELECTED BOTH LEFT EDP AND LEFT ACMP OFF. LEFT HYD FLUID QTY NOW AT .15 PERCENT ON EICAS. SEE AMM 29-11-00/201 CONDITION 1 TABLE 1. FOUND LEAK COMING FROM LEFT MLG DOOR SDR CALA2024071800249Tire · unknownPDA 1 REF LP 8545126: LAX REPORTED A MLG GEAR TIRE MAY HAVE DEPARTED THE AIRCRAFT. CREW OBSERVED AN ANTISKID EICAS ON TAKEOFF THEN WENT AWAY. CABIN CREW FELT A SHUDDER ON TAKEOFF PICS ONLY FLAGGED AS SDR SDR HAS BEEN CREATED REF SDR# 1036734 OIL SERVICE ACCOMPSDR CALA2024071102005Wheel · detachedPDA 1 REF LP 8545126: LAX REPORTED A MLG GEAR TIRE MAY HAVE DEPARTED THE AIRCRAFT. CREW OBSERVED AN ANTISKID EICAS ON TAKEOFF THEN WENT AWAY. CABIN CREW FELT A SHUDDER ON TAKEOFF.SDR CALA2024062400064Skin · canningDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR, PERFORMED INTERIM REPAIR PER ECRA 5330-07276 PART 1 STEPS 1-4. REF EC/RA 5330-07276 PERFORMED HFEC SURFACE INSPECTION IAW NDT PART 6 51-00-19, NO CRACKS DETECTED. PERMANENT REPAIR COMPLETED SDR CALA2024062601905Skin · dentedDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR. ACCOMPLISH PART 3 PERMANENT REPLAIR WITHIN 2 FLIGHT CYCLES PER ECRA 5330-07276. PER ECRA 5330-07276 "ACCOMPLISH PART 3 PERMANENT REPAIR WITHIN 2 TOMC-APPROVAL FROM SC1ELBYC COMMENT FLIGHT CYCLSDR CALA2023100602971Clutch · malfunctionedR ENG WOULDNT GET ABOVE 1.51EPR DURING T/O. L ENG SHOWED T/O POW ER OF 1.60EPR. DEBRIEFED CREW AND CONFIRMED THIS WAS AN A-T ENGAGED T-O ATTEMPT . INITIAL MANUAL CYC OF THRUST LEVERS SHOW DIFF IN STIFFNESS AND IT LOOKS TO NEED THROTTLE RIG CHK (BOTH ENGINES) TSDR CALA2023081802571Transmitter · faultyDURING T/O ROLL RT ENG EPR SETTING FLUCTUATED WITH A/T ON. NOTAB LE THROTTLE SPLIT. MCDP AUTOTHROTTLE NO FAULTS TRST OK. RIGHT EEC BITE READS FOLLOWED FIM 76-11 FAULT TREE 804--UP TO STEP 13 - POWERPLANT REMOVED #2 ENG EPR TRANSMITTER IN REF WITH AMM 77-11-01.SDR CALA2023050101310Engine · unknownRT ENG OIL PRESS EICAS RED PRESS IND. 0 FOLLOWED BY ENGINE FAIL WINDMIL APPX 30 MINS. REMOVED CHIP DETECTORS AND FOUND LARGE AMOUNTS OF METAL PARTICLES IN BOTH MASTER ANDEXTERNAL GEAR BOX . NONE IN INTERNAL GEARBOX. REMOVED SCAVENGE FILTER AND FOUND METAL PARTSDR CALA2022051601269Bleed Air Sys · false indicationREJECTED TAKEOFF LOW SPEED DUE TO ENGINE BLEED OFF INDICATION FOUND TO BE OPERATING NORMAL FOR MEL PROCEDURES UNDER FLIGHT CREW NOTES.SDR CALA2022042901100Idg · failedALL ELEC FAIL ON TAKEOFF RGEN RECOVERED 15 SECS LATER STARTED AP U AND RAN QRH FOR LGEN OFF CHECKED AT GENERATOR AND FOUND T2 TERMINAL OF GENERATOR DISPLAYING SAME READINGS. NEEDS GENERATOR REPLACED. AT THE GATE, PERFORMED BITE CHKOF THE BPCU, ALL THE FAULTS WSDR CALA2022021600392Fitting · corrodedSHEAR TIE CORRODED AT STA 28L FWD OF STA 1560. REMOVED AND REPLACED SHEAR TIE AT STA 1560 S-28L IAW B757 SRM 51 -40-02 PARA 4. WORK PERFORMED BY V936267, V933877 SEE REF AMES NR142726-0100-0082 FOR INSPECTION RII SIGN OFF BY INSPECTOR V933877SDR CALA2022020200294Skin · damagedALC DOOR AFT LOWER SKIN HAS A LARGE BLENDED AREA. REPAIRED ALC DOOR AFT LWR SKIN IAW 47493REA05 AND EC/RA 5320-021 79SDR CALA2022020200293Skin · damagedNO 2 CARGO DOOR HAS A REINFORCING REPAIR ON THE OUTER SKIN AT LO WER FWD CORNER. DOCUMENT REPAIR LOCATION, SIZE AND BASIC DESCRIP TION/CONDITION IAW EA 5100-02345 REV E STEP 11.2. REPAIRED ALC FWD LWR CORNER SKIN IAW 47493REA06 AND EC/RA 5320-0 2178 ADD EMP:V9SDR CALA2022011400127Plate · corrodedUPPER FLOOR BEAM WEB STA 1680-1686 LBL19-LBL29 HAS CORROSION. REMOVED AND REPLACED REPAIR DOUBLER AT STA 1680-1686 LBL19-LBL29 PER B757 SRM 53-60-51 REPAIR 2. WORK PERFORMED BY V921314,V9212 24. RII ACCOMPLISHED ON AIMS NR 0144 IS ACCEPTED.SDR CALA2021062800981Plug · bent#1 ENGINE - IP BORESCOPE PLUG, APPROX 5 O''CLOCK POSITION TURBINE CASE, INNER PLUG STEM BENT. REQUIRES REPLACEMENT PLUG. M/E 19-7250-3-0001 INSTALLED IP BORESCOPE PLUG, REF TASK CARD 19-7200-1-2400 IDT INSP C/W OF IP BORESCOPE PLUG INSTALLATION PER ABOVE REF QSDR CALA2021012000058Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1620 ABOVE S-20R. DAMAGE BETWEEN STRINGERS S-19R AND S-20R. REMOVED 25 EXISTING FASTENERS AROUND THE PERIMETER OF DAMAGE FOR REPAIR. COMPLIED WITH STEPS 1 THRU 5 OF AVO 8768 PERFORMED HFEC ON TRIM OUT, PER PT 6 51-00-01,SDR CALA2021012000059Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1701 BETWEEN STRINGERS S-20R AND S-21R. FOUND A PREVIOUS REPAIR OVER STRINGER 19R AFT OF STA 1701 APPROXIMATELY AND ABOVE TO DMG AREA. REMOVED REPAIR FOR ACCESS. COMPLIED WITH AVO 8767 STEPS 1 THRU 5 TO CONTINUE. HFEC CSDR CALA2021011500046Stringer · deformedSTRINGER S-21R IS DEFORMED AND DENTED BETWEEN STA 1701 AND 1720. CUT AND REMOVED STRINGER S-21R FROM STA 1681.8 +17 TO STA 1720, REFERENCE NEEDS TO BE UPDATED. AVO 8767 REV A STEP 17. REMOVED STRINGER CLIP AND SHEAR TIE FOR ACCESS. CUT AND REMOVED STRINGERSDR CALA2021011500045Stringer · damagedSTRINGER S-20R IS COMPLETELY SEVERED BETWEEN STA 1701 AND 1720 CUT AND REMOVED STRINGER S-20R FROM STA 1682.8 +17 TO STA 1720. REFERENCE NEEDS TO BE UPDATED AVO 8767 REV A STEP 16. REMOVED STRINGER CLIP AND SHEAR TIE FOR ACCESS. CUT AND REMOVED STRINGER S-2SDR CALA2021011100036Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1620 ABOVE S-20R. DAMAGE BETWEEN STRINGERS S-19R AND S-20R. REMOVED 25 EXISTING FASTENERS AROUND THE PERIMETER OF DAMAGE FOR REPAIR. COMPLIED WITH STEPS 1 THRU 5 OF AVO 8768. PERFORMED HFEC ON TRIM OUT, PER PT 6 51-00-SDR CALA2021011100035Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1701 BETWEEN STRINGERS S-20R AND S-21R. FOUND A PREVIOUS REPAIR OVER STRINGER 19R AFT OF STA 1701 APPROXIMATELY AND ABOVE TO DAMAGE AREA. REMOVED REPAIR FOR ACCESS. COMPLIED WITH AVO 8767 STEPS 1 THRU 5 TO CONTINUE. HFESDR CALA2019091701553Pin · unsecureFOUND SEAT MOUNTED EEL LIGHTING INOP ROWS 32-40ABC. FOUND FUSE FOR PIN 13 ON POWER SUPPLY M736 OPEN. TROUBLESHOT SHORT TO SEAT CONNECTOR AT ROW 36ABC SHORTED TO GROUND (PIN NOT FULLY HOME) RESECURED PIN AND RECONNCTED CONNECTOR. FUSE REPLACED IN POWER SUPPLY MSDR CALA2019010700049Not Reported · leakingB757-53-3-5301 BLUE WATER IN AREA AFT OF AFT CARGO ABOVE AFT LAV SERVICE PAN AND SURROUNDING STRUCTURE FROM STA 1640-1700. REF N/R 0038799. CLEANED BLUE WATER, NEUTRALIZED AND RE-APPLIED CIC ON AFT CARGO ABOVE AFT LAV SERVICE PAN AND SURROUNDING STRUCTURE FROMSDR CALA2019010600033Not Reported · leakingBLUE WATER IN AREA AFT OF AFT CARGO ABOVE AFT LAV SERVICE PAN AND SURROUNDING STRUCTURE FROM STA 1640-1700. CLEANED BLUE WATER, NEUTRALIZED AND RE-APPLIED CIC ON AFT CARGO ABOVE AFT LAV SERVICE PAN AND SURROUNDING STRUCTURE FROM STA 1640 TO STA 1700 IAW EC/RA SDR CALA2019010600023Not Reported · leakingBLUE WATER ON FWD CARGO STRUCTURE AND FEW SECTIONS OF INSULATION FROM STA 560 TO STA 900 LT SIDE FROM STR 22L TO 28R. CLEANED BLUE WATER ON FWD CARGO STRUCTURE FROM STA 560 TO STA 900 LT SIDE FROM STR 22L TO 28R IAW EC/RA 2011-01000. INSULATION BLANKET HAS BEESDR CALA2018123102685Pan · chafed(SUPPORT TASK EA 5210-01364 REV G) L4 DOOR PASSENGER DOOR, EXTERIOR HANDLE PAN HAS SEVERAL CHAFFING MARKS. 3EA. CHECKED LIMITS ON L-4 DOOR EXTERIOR HANDLE PAN FOUND TO BE OUT O F LIMITS PER B757-200 SRM 52-10-01 AD 1. FIG 101 DETAIL XIII ORG L MATL .063 MATL L
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