N14214
Service difficulty reports · 85
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 = 'N14214' 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 = 'N14214' 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 CALA2026092919975Lens · brokenRED EMERGENCY PATH LIGHT BROKEN, SEAT 15C. REPLACED THE RED EMERGENCY LIGHT LENS AT SEAT 15C. LIGHT OPS CHECKED GOOD IAW AMM 33-51-11.SDR CALA2026092219656Light · no testOPS CHKD THE EMERGENCY LIGHTS, THE RIGHT AFT OVERWING, OVER THE DOOR EMERGENCY LIGHT WAS INOPERATIVE. WINDOW LIGHT FUNCTIONS NORMAL. OVERWING EXIT HATCH HANDLE LIGHT IS INOP. IAW MM 33-51-00-710-801, FIG 504. REMOVED AND REPLACED THE OVERWING EXIT LIGHT IAW SDR CALA2026082518906Light · inoperativeAILSE EMERGENCY LIGHT AT 29ABC OUT. R & R EMERGANCY FLOOR POROXIMITY LIGHT AT ROW 29ABC IAW AMM TASK 33-51-11-960-802.SDR CALA2026081718673Skin · crackedLEFT WING LOWER SKIN AT STR 9, DURING HFEC INSPECTION, A CRACK WAS FOUND AT OTBD MOST FASTENER. REF EA5725-01143 REVISION B OP. 003, SEQ 4. REFERENCE LP9951108 DIP GENERATED. PERFORMED REPAIR ON LT WING LOWER SKIN AT STR 9 AREA, ALL WORKS WERE ACCOMPLISHED ISDR CALA2026063017495Actuator · leakingFUEL LEAK IN NU 1 ENGINE NU ENGINE SHUT DOWN PER FM. OBSERVED 80 0LB IMBAL IN 30 MIN.30MIN DNCREW DE-BRIEF. ENG 1 SHUT DOWN WAS COMMANDED PER QRH FOR 800LBS LF TANK IN 30 MIN OR LESS. ENG SHUTDOWN TIME 0300Z . NO UPLIFT IN FF WHILE LEFT TANK WAS INDICIATION FUSDR CALA2026020513601Sensor · faultedDUCT PX SPLIT ON DPT LEFT 10PSI RIGHT 40PSI REMOVED AND REPLACED PRECOOLER CONTROL VALVE REF AMM 36-12-03, AND 450 SENSOR REF AMM 36-11-05. RAN ENGINES OPS CHECKS NORMAL, REF FIM 35-10-00-3 FIG 305.SDR CALA2026020313533Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN. HSS 138.70, TWO CRACK SIGNALS NOTED, CRACK NR 1 L= 1.075" TO 9.500 INCH FWD FROM AFT SPAR, CRACK NR 2 L=1.122" TO 17.300 INCH FWD FROM AFT SPAR. (REF. NR 3502714-2000-0060) PERFORMED PERMANENT REPAIR AT RT HORIZONTAL STAB LSDR CALA2025041403762Skin · damagedESR #004 DEFECT NR, REQUESTING ENGINEERING SUPPORT CLARIFICATION FOR EA 5310-08195 REV B OP 004 STEP (38) (R/H WINDOW). ED REQUIR EMENTS ARE NOT MET (LOOKING FWD, UPPER OUTBD ED .340", UPPER INB D ED .318 INCH, LOWER OUTBD ED .322", LOWER INBD ED .327". MINIM SDR CALA2024013000260Warning Light · false activationSTAB OUT OF TRIM LIGHT CAME ON DURING TAKEOFF ROLL. REPLACED STAB OUT OF TRIM LIGHT LENS, CKS OK. OPERATED STAB TRIM IN BOTH DIRECTIONS MANUALLY AND ELECTRICALLY, NO DEFECTS. ALL INDICATIONS NORMAL. ACFT IS OK TO CONTINUE.SDR CALA2024012200179Relay · not seatedBOTH CENTER FUEL PUMP LOW PRESSURE LIGHTS CAME ON WITH 13.7 STIL L IN CT R TANK VERIFIED CENTER FUEL PUMP C/BS CLOSED. DURING REMOVAL OF UFI ACCESS PANEL ELECTRICAL ARCING NOTED BETWEEN FASTNERS AND AIRFRAME ACCOMPLISHED INSPECTION OF AREA SURROUNDING UFI REF SDR CALA2024011700130Connector · dirtyANTISKID INOP LIGHT, LIGHT ON. CREW DEBRIEF - LIGHT CAME ON IN CRUISE BUT CLEARED ON APPROACH. DISCONNECTED CONNECTOR D928 TO PARKING BRAKE VALVE AND FOUND NO DEFECTS. ALL PINS AND SOCKETS GOOD. CLEANED AND SECURED CONNECTOR. OPS CK GOOD PER REF. AMM 32-42-21-SDR CALA2023122903750Actuator · faultedSTAB OUT OF TRIM LIGHT DURING TAKEOFF ROLL DFCS CURRENT STATUS AND FAULT HISTORY ONLY SHOWED FAULT FOR MCP DISPLAY. PHOTO ATTACHED. NEEDS FURTHER TROUBLE SHOOTING. REF FIM 22-11 TASK 851. PERFORMED STAB TRIM BITE TEST. SEE PICTURES FOR FAULTS. PERFORMED FIM 22SDR CALA2023031500743Beam · corroded(B737-53-3-0711) CORROSION AROUND FASTENER HOLES ALONG BS 328 RB L 14, 30, 39 ON MAIN DECK FLOOR STRUCTURE. STA 328 RBL30 CORROSION OUT LIMITS REPAIRED IAW B737-800 SRM 53- 10-51-2R07 REPAIR 7. SEE PARTIAL WORK FOR ACCOMPLISHED ON FORM 4 4-0008. DATA WAS TRANSSDR CALA2023031500742Floor Support · corroded(B737-53-3-0711) RBL +10 FLOORBEAM SUPPORT HAS SURFACE CORROSION STA 328-294 FLOORBEAM SUPPORTS CORROSION OUT OF LIMITS REF SRM 53-10-51-A PA RA 4B. REPLACED WITH NEW SUPPORTS REF SRM 51-40-02. DATA WAS TRA NSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24738 WORKSDR CALA2023031500736Unknown · corroded(B737-53-3-0711) L1 DOOR THRESHOLD STA 344 TO 320 HAS SURFACE CORROSION L1 DOOR THRESHOLD STA 344 TO 320 REMOVED AND REPLACED FOR NEW ON E IAW B737-800 SRM 51-40-02-0G-0 PAR 4.B. AND 7.A. DATA WAS TRAN SCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24706 WORK ACP BSDR CALA2023031000706Floor Support · corrodedB737-53-3-0740 AFT CABIN SUPPORT FWD OF L/H WEB HAS CORROSION STA 1006SDR CALA2023031000705Panel · corroded(B737-53-3-0740) AFT CABIN STA 1016 L/H WEB HAS CORROSIONSDR CALA2023031000704None · corrodedB737-53-3-0740 AFT CABIN STA 1016 LBL 18" HAS CORROSIONSDR CALA2023031000703Beam · corrodedB737-53-3-0711 FLOOR BEAM AT STA 340 INBD OF L1 HAS SURFACE CORROSION.SDR CALA2023031000702Beam · corrodedPASSENGER CABIN FLOOR BEAM 947-RH END UPPER CAP CORRODED AT FAST ENER. EVALUATED DAMAGE ON FLOOR BEAM UPPER FLANGE AT STA 947.5. ORIGIN 4/27/23. PERFORMED REPAIR AT MAIN CABIN STA 947.5 BETWEEN LBL 58 AL THICKNESS IS .185". LOW MAT .046", R.M. .141" FOUND TO BSDR CALA2023031000701Seat Track · corrodedB737-53-3-0740 L/H O/B SEAT TRACK AT STA 907 HAS CORROSION REMOVED AND INSTALLED SEAT TRACK L/H OB STA 887 AT STA 927 IAW B 737-800 SRM 51-40-02 PAR 7, 9. SFR #1031562. DATA WAS TRANSCRIBE D FROM PAPER DOC AERSALE WO 3826 NR 24799 WORK ACP BY MECH V9428 59 INSSDR CALA2023031000700Intercostal · corroded(B737-53-3-0711) BARE METAL ON AFT EDGE OF FLIGHT DECK AFT FLOOR ACCESS PANEL CUTOUT REMOVED CORROSION DAMAGE ON AFAT EDGE OF FLIGHT DECK AFT FLOOR A CCESS PANEL IAW B737-800 EC/RA #5321-01566. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24702 WORK SDR CALA2023031000699None · corrodedB737-53-3-0740 AFT CABIN SUPPORT BEAM STA 1016 RBL 18" HAS CORROSION PERFORMED WORK AT AFT CABIN STA 1016, RBL 18" IAW B737-800 SRM 5 1-40-02 PAR 407. FABRICATED AND REPLACED STRAP. DATA WAS TRANSCR IBED FROM PAPER DOC AERSALE WO 3826 NR 24790 WORK ACP BY MECHSDR CALA2023031000698Beam · corrodedB737-53-3-0740 FLOOR BEAM 986.5 RBL 23" AREA OF CORROSION FLOOR BEAM 986.5 RBL 23" WAS REPAIRED IAW SRM 53-00-51-2R-1 (REP AIR 1) PAR 4. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 382 6 NR 24792 WORK ACP BY MECH V940458 INSP BY AQC008SDR CALA2023031000697Beam · corrodedB737-53-3-0740 FLOOR SUPPORT AT 927 RBL 9" HAS CORROSION THE FLANGE OF A TRANSVERSES FLOOR BEAM CHORD WAS REPAIR IAW SRM 53-00-51-2R-1 PAR 4, A THROUGH L. DATA WAS TRANSCRIBED FROM PAPE R DOC AERSALE WO 3826 NR 24768 WORK ACP BY MECH V940903 INSP BY AQC028SDR CALA2023031000696None · corrodedB737-53-3-0740 L2 DOOR SILL PLATE HAS CORROSION IN SEVERAL AREAS NEW SILL PLATE WAS INSTALLED IAW SRM 51-40-02-0G-0 PARA 4 AND 9. SFR 1031557. DATA WAS TRANSCRIBED FROM PAPER DOC AERSALE WO 382 6 NR 24764 WORK ACP BY MECH V937322 INSP BY AQC009SDR CALA2023031000695Intercostal · corroded(SUPPORT TASK) AFT PASSENGER CABIN ENTRY DOOR AREA, OUTBOARD FLO OR SUPPORT INTERCOSTAL STA 927-947 IS CORRODED AT FASTENER POSIT ION REPLACED FLOOR SUPPORT INTERCOSTAL ON STA 927 TO 947 IAW SRM 51- 40-02-0G-0 PARA 7. SFR 1031556. DATA WAS TRANSCRIBED FROM PAPSDR CALA2023031000694Intercostal · corroded(B737-53-3-0711) INBD SEAT TRACK AT STA 340 LBL & 24 END OF SEAT TRACK HAS CORROSION REMOVED CORROSION AND INSTALL NEW STIFFENER AT STA 325 TO 340 LB L 44 IAW B737-800 SRM 51-40-02-0G-0 PAR 7. SFR #1031555. DATA WA S TRANSCRIBED FROM PAPER DOC AERSALE WO 3826 SDR CALA2023031000693Floor Support · corroded(SUPPORT TASK) MAIN CABIN L/H STA 947.5 LBL 50 FLOOR SUPPORT HAS CORROSION REPLACED FLOOR SUPPORT ON STA 947.5 LBL 50 LH IAW SRM 51-40-02-0 G-0 PARA 7. SFR #1031554. DATA WAS TRANSCRIBED FROM PAPER DOC AE RSALE WO 3826 NR 24989 WORK ACP BY MECH V937322 INSP BYSDR CALA2023031000692Intercostal · corroded(B737-53-3-0711) CORROSION BY 2 EA GALLEY FITTINGS AT BS 303 ON MAIN CABIN FLOOR STRUCTURE FOR GALLEY 1 REPLACED FITTINGS AT BS 303 ON MAIN CABIN FLOOR STRUCTURE GALLEY 1 IAW SRM 51-40-02-0G-0 PARA 7. SFR #1031553. DATA WAS TRANSCRI BED FROM PAPER DOC AERSALE SDR CALA2023031000691Intercostal · corrodedB737-53-3-0740 RH AFT LAV O/B MOUNT CORROSION ON FLOOR BEAM REMOVED AND REPLACED INTERCOSTAL AT RH AFT LAV OB MOUNT ON FLOOR BEAM IAW SRM 51-40-02-0G-0 PARA 7. D. SFR #1031552. DATA WAS TR ANSCRIBED FROM PAPER DOC AERSALE WO 3826 NR 24795 WORK ACP BY ME CH V93SDR CALA2023031000690Floor Support · corrodedB737-53-3-0740 FLOOR SUPPORT BETWEEN 927-947 RBL 10 HAS CORROSION. EVALUATED DAMAGE ON FLOOR STRUCTURE BTW STA 927 TO 947.5 RBL 10 REPLACED NEW ANGLE SUPPORT P/N: 147A5768-20 IAW B737-800 SRM 51- WITH DIMENSIONS L=2",W=2", D=.050". FOUND TO BE OUT OF LIMITS IASDR CALA2023030100574Window · crackedTHIS NR GENERATED FOR ESFR REPORTING ONLY L/H NO 1 WINDOW FRAME HAS CRACK EA 5310-04554 REV B.SDR CALA2022123003519Container · odorVERY STRONG ODOR COMING FROM TRASH BIN AT LOCATION 410. SMELLED LIKE BURNT RUBBER. PERFORMED ODOR / SMOKE AMM 05-51-26-800-801-C1 SENT QUESTIONNAIRE TO TOMC NO ODOR OR SMOKE AT THIS TIMESDR CALA2022112103189Trim Motor · failedSTABILIZER FAILS TO TRIM NOSE UP AND NOSE DOWN AFTER DEPARTURE SPEED TRIM DO NOT ARM LIGHT CAME ON.STAB TRIM F AILUR E.SMOOTH 153.5 OVRWT LDG PERFORMED FIM TASK PER FIM 27-32 TASK 801 NO HELP STILL NO STAB TRIM MANUAL OR ELECTRIC. ALSO PERFORMED FIM TASK 27-4SDR CALA2022090902322None · noneLOW SPEED REJECT UNDER 45KTS . AFT CARGO LT ON VERIFIED DOOR CLOSED AND LOCKED COMPLIED WITH MEL. ADD EMP:374265 ADD EMP:374265 APPROVED ACCOMPLISHED AMM 05-51-07 NO DAMAGE. ACCOMPLISHED PSEU BITE TEST, WITH NO EXISTING FAULTS, FAULT HISTORY SHOWS 32-64001 INSDR CALA2022071501769None · noneTHIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/15/22. RAMP REPORTED SMOKE FROM RIGHT LANDING GEAR APON FURTHER INSPECTION FOUND FIRE IN RIGHT HAND WHEEL WELL. REPLACED S73 SWITCH AND WIRE ASSEMBLY TO D46012P. TRING TIED WIRE BUNDLE ANSDR CALA2022020700333Light · damagedSEAT MOUNTED EMERGENCY LIGHT AT ROW 37ABC DAMAGED. REMOVED AND REPLACED WHITE LIGHT ASSY REF MM 33-51-11. OPS CK OK. VERIFIED IDT REQUIREMENTS FOR SEAT MOUNTED EMERGENCY LIGHT REPLACEMENT.SDR CALA2021091301567Proximity Sensor · intermittentFSEU FAULT HISTORY REPORTS LEADING EDGE FLAP RETRACT PROX SENSOR 2 INTERMITTENT DURING T/S, FOUND NO CURRENT FAULTS BUT FAULT HISTORY REPORTS FLAP RETRACT PROX SENSOR 2 INTERMITTENT. FOUND GROUNDING WIRE BROKEN. RETERMINATED GROUND WIRE, NO HELP. TRANSIT LIGHTSDR CALA2020030600564Fitting · crackedSHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. -SPT-6212455 REMOVED & REPLACED CRACKED SHEAR FITTING IAW B737-800 SRM 51-40- 02 & EC/RA NO.5714-01092. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 2/29/20 INSPECTION ACCEPTEDSDR CALA2020030600563Fitting · crackedSHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. -SPT-6212454 REMOVED & REPLACED CRACKED SHEAR FITTING IAW B737-800.SRM 51-40- 02 & EC/RA NO.5714-01090. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION 2/29/20 INSPECTION ACCEPTEDSDR CALA2020030600562Fitting · crackedSHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. -SPT-6212458 REMOVED AND REPLACED CRACKED SHEAR FITTING IAW B737-800 SRM 51-4 0-02 & EC/RA NO.5714-01093. SSFR REPORT, FORM 46-0024, ENTERED B Y UAL 2/29/20 INSPECTION ACCEPTEDSDR CALA2020030600561Fitting · crackedSHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED -SPT-6212453 REMOVED & REPLACED CRACKED SHEAR FITTING IAW B737-800. SRM 51-40 -02 & EC/RA NO.5714-01089, SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 2/29/20 INSPECTION ACCEPTEDSDR CALA2020030600560Fitting · crackedSHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. -SPT-6212456 REMOVED & REPLACED CRACKED SHEAR FITTING IAW B737-800. SRM 51-40 -02 & EC/RA NO.5714-01091. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 2/29/20 INSPECTION ACCEPTEDSDR CALA2020030600559Fitting · crackedSHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. -SPT-6212457 REMOVED & REPLACED CRACKED SHEAR FITTING IAW B737-800. SRM 51-40 -02 & EC/RA NO.5714-01094. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 2/29/20 INSPECTION ACCEPTEDSDR CALA2020020200291Skin · dentedFWD CARGO DOOR EXTERNAL SKIN LOWER SURFACE HAS DENT APPROXIMATELY 22" INCHES FROM AFT EDGE. (18-036) AS PER T/C 29-5230-1-2500 ACCOMPLISHED REPAIR AT FWD CARGO COMPARTMENT DOOR EXTERNAL SKIN LOWER SURFACE IAW EC/RA # 5231-01129 AND PER RES # 2015495-13SDR CALA2020020210273Cargo Track · brokenB737-25-3-0962 FWD CARGO NET HOLD DOWN FITTING IS BROKEN AT STATION 495 13" LEFT OF CENTER LINE. REF AAR NR 998688 72 REMOVED AND REPLACED FWD CARGO TIE DOWN TRACK LBL 18" FROM STA 396 TO STA 500 E+10" IAW B737-800 SRM 51-40-02 AND 57-00-53 .SDR CALA2020011900187Skin Panel · crackedCRACK FOUND AT LT HORIZ. STAB LWR INSPAR SKIN PANEL AT STA 101.90 11" FWD OF THE T/E, I/B OF FASTENER ROW. (REF NR 99868901) REPAIRED DAMAGE AT LT HORIZONTAL STAB, LOWER INSPAR, SKIN PANEL STA 101.90 11" FWD OF T/E, I/B OF FASTENER, ROW AS PER REF SRM 55-10-01SDR CALA2019091701546Skin · dentedDENT REPORTED APPROX STA 400, 4 FEET FWD OF FWD CARGO DOOR. LOCATION UPDATE ABOVE NEAR STRINGER 22R STA 400 ACCOMPLISHED STEPS A 1-A 8 PER ESC190905-0214-1. REQUEST HFEC HOLE PROBE, COUNTERSINK AND EDGE OF CUT OUT PER STEPS A.9-11. C/W HFEC EDGE OF CUT OUT REFSDR CALA2019071501206Fastener · shearedDOOR 1L DIFFICULT TO OPEN FOUND UPPER GUIDE ARM ATTACH PIN SECURE FASTENER SHEARED, CAPTURE WASHER MISSING, AND ATTACH PIN MIGRATED, RPL ITEMS 82, 85, 70 SCREW, WASHER, PIN REF IPC 52-11-21-01, ENSURED PROPER ENGAGEMENT OF LOWER LINK ARM, LUBED UPPER GUIDE AR
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