N14102
Service difficulty reports · 93
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 = 'N14102' 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 = 'N14102' 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 CALA2017052801628Latch · dirtyR3 DOOR WILL NOT DISARM. THE R3 DOOR SLIDE DISARM OPS NORMAL. INSPECTED THE GIRT BAR, NO DISCREPANCIES NOTED. PERFORMED RENDER SAFE CHECKLIST. REMOVED DEBRIS AND LUBED GIRT BAR. ACFT RETURNED BACK TO NORMAL IAW AMM 52-11-25SDR CALA2017041701039Battery · dischargedEMERGENCY FLASHLIGHT DOOR 1L INOP. R&R FLASHLIGHT BATTERY IN 1L DOOR. OPS GOOD.SDR CALA2017041401001Light · unsecureSEAT 28D EMERGENCY EXIT ROW LIGHT HAS SEPARATED FROM SEAT AND IS HANGING. RESECURED 28D EMERGENCY EXIT ROW LIGHT, OPS CHK GOOD.SDR CALA2017040400816Ballast · faultyA/C LEFT EMER EXIT ROW WALL LIGHTS OUT. REMOVE AND REPLACED LIGHT AND BALLAST ASSY ON SIDEWALL BY ROW 20 A IAW AMM 33-21-30. OPS CHECK GOOD.SDR CALA2016122301163Anti-Ice System · malfunctionedR FWD WINDOW HEAT FAILED ON TAKEOFF. ELEC SMELL NOTED. SWITCH OFF SMELL WENT AWAY. PERFORMED WINDOW INSPECTION R-1 WINDOW FOUND NORMAL. PERFORMED BITE ON WINDOW HEAT CONTROLLER PER FIM TASK 30-41-00 TEST PASSED. PERFORMED WINDOW HEAT TEST PER MM 30-41-00. WINDSDR CALA2016042900263Light · inoperativeEMERGENCY LIGHTS INOPERATIVE AT 29C & CLOSET AFT OF 4B INOPERATIVE ON 2 SERVICE CHECKS. 29C RELAMPED & CLOSET ON MEL.SDR CALA2015072400604Skin · crackedR1 DOOR INTERIOR SIDE, HAS CRACK AT LIGHTNING HOLE, TOP END, UNDER DOOR SLIDE FWD ATTACH BRACKET. COMPLIED WITH ECRA 5210-02655. SEE WIPS FOR ALL WORK ACCOMPLISHED.SDR CALA2015071700580Skin · dentedREINSPECTED DENT AFT CARGO DOOR SKIN 7.5" ABOVE LOWER EDGE & 8.5" FROM AFT EDGE. FOUND DIMENSIONS AS FOLLOWS A=1.7"Y=.059" A/Y=28.81 OUT OF LIMITS. REPAIRED DENT IAW SRM 52-30-01 REPAIR 4.SDR CALA2015071700577Floorbeam · corrodedCABIN FLOORBEAM STATION 365 BETWEEN RBL 6 TO RBL 19, CORROSION. REMOVED CORROSION AT CABIN FLOORBEAM STATION 365, BL0 TO RBL 24.75 .027. REMOVED RBL 10.25 & .014, REMOVED AT RBL 14.25 FROM .125 THICKNESS FOR CLEANUP & IS OUT OF LIMITS. ALL OTHER BLEND AREASSDR CALA2015033000215Sense Line · crackedRIGHT ENG NORMAL INDICATIONS ON TAKEOFF AS ACFT CLIMBED OUT, INDICATIONS WERE DECREASING POWER ON LT ENG. AT 32,000 FEET N1, N2, N3 ALL LOWER, FUEL FLOW 1/2 OF LT ENG. AT LOW ALTITUDE FUEL FLOWS, N1, N2 CLOSER TO NORMAL PRESSURIZED P1 SYS ON RT ENG & FOUND PSDR CALA2012062500414Torque Box · debondedON NDT INSPECTION, FOUND LT HORIZONTAL STAB LOWER TORQUE BOX TO BE DISBONDED REPAIRED IAW ECRA 5510-01920.SDR CALA2012042300291Pca · malfunctionedCENTER HYD SYS LOST QTY BELOW .38 - AS PRECAUTION, SUGGEST CHANGING CENTER HYD RUDDER PCA (LOWER) . R & R CENTER RUDDER PCA IAW AMM 27-21-20. SEE N/R 4539233 FOR OPS CHECK AND /OR ADJUSTMENT IAW AMM 27-21-20-42 2-025 STEP J TO END. (INSTALLATION ONLY). ROTABLSDR CALA2012012600048Skin · dentedREF TO LOG PAGE 8696793, REINSPECT FUSELAGE DENT BODY STATION 760 BETWEEN STR 16 AND 17L, PER SRM. INSTALLED REPAIR AS PER ECRA 5331-01580, PLACED ON A DIP 53-DIP CONTROL NUMBER 14371 PERMANENT REPAIR AS PER PART 3 BEFORE 23 MONTH.SDR CALA2012012600047Skin · dentedREF TO LOG PAGE 8696793, REINSPECT FUSELAGE DENT BODY STATION 760 BETWEEN STR 16 AND 17L, PER SRM. INSTALLED REPAIR AS PER ECRA 5331-01580, PLACED ON A DIP 53-DIP CONTROL NUMBER 14371 PERMANENT REPAIR AS PER PART 3 BEFORE 23 MONTH.SDR CALA2011033100243Reflector · wornL1 DOOR EXTERNAL EMERGENCY LIGHT INOP. RELAMPED, NO HELP. FUSE CHECKS GOOD. REPLACED REFLECTOR ASSY. OPS CHECK GOOD.SDR CALA2009122800770Bottle · defectiveFOUND EMERGENCY SLIDE RT BOTTLE PRESSURE TEST INOPERATIVE. REMOVED AND REPLACED RT EMERGENCY SLIDE PRESSURE BOTTLE AS PER M/M CHAP 25-65-02, OPS CHECKS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT 1265237 S/N OFF 05379 BOTTLE, ESCAPE OFF 19-2565-9-9007 537SDR CALA2009121600716Battery Pack · dischargedLAST FOUR EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BOTH AFT BATTERY PACK AND AFT GALLEY EMERGENCY LIGHTS SWITCH. PER W/D 33-51-15, TESTED LIGHTS, OPS CHECKS GOOD.SDR CALA2009102200638Light · inoperativeL1 EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. RELAMPED L1 EMERGENCY EXIT LIGHT PER AMM 33-51-06. SYSTEM OP CHECKS NORMAL.SDR CALA2009070200356Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1040 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200355Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1026 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE SDR CALA2009070200354Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1020 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200353Skin · corrodedCORROSION NOTICED ON RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1015 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200352Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1010 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200351Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 1004 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200350Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGE STATION 999 WITH SOME METAL FLAKING. REPAIRED UPPER SURFACE OF RT WING APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0, FUSELAGESDR CALA2009070200349Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 994 WITH SOME METAL FLAKING REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 994 PESDR CALA2009070200348Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STA 983 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 983 PER ESDR CALA2009070200347Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 977 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 977 SDR CALA2009070200346Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STA 968 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 968 PER SDR CALA2009070200345Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 965 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 965 SDR CALA2009070200344Skin · corrodedCORROSION NOTICED AT RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SKIN SPLICE, AT WING STA 0 FUSELAGE STATION 960 WITH SOME METAL FLAKING. REPAIRED RT WING UPPER SURFACE APPROX 4 INCHES O/B OF WING TO BODY SPLICE, AT WING STA 0, FUSELAGE STA 960 SDR CALA2009043000229Frame · corrodedFRAME AT STATION 1460 WL 144 TO WL 138.50, LBL 9 TO RBL 9 HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED FRAME AT STATION 1460 WL 144 TO WL 138.50 PER SRM 51-40-02 AND BOEING PRINTS 146N1014.SDR CALA0500415Socket · shortedSMOKE BEGAN COMING FROM A CABIN CEILING FLUORESCENT FIXTURE LIGHT AT SEAT 24A (MID LEFT CABIN) WHILE ON CLIMBOUT OF TPA. A TECHNICIAN ON THE FLIGHT REMOVED THE CEILING PANEL, REMOVED THE LIGHT BULB, AND THE SMOKE CEASED. FOUND THE SOCKET WHERE THE BULB PLUGSSDR CALA0500121Controller · failedFIRST CLASS VIDEO SYSTEM HAD BURNING ODOR. REPLACED VIDEO SYSTEM CONTROLLER AND TAPES AND CASES.SDR CALA0400497Structure · gougedINSPECTION FOUND THE NR 2 ENGINE PYLON STRUCTURE LOWER CHORD GOUGED IN TWO PLACES AT STA 260. THE AREA WAS REPAIRED IAW ECRA 5450-01565.SDR CALA0400489Skin · gougedINSPECTION FOUND R-1 DOOR INTERIOR SKIN GOUGED AT BS 354, WL 245. THE SKIN WAS REPAIRED IAW ECRA 5210-01769 AND A DIP WAS ISSUED TO REINSPECT THE AREA ON OR BEFORE 37,500 CYCLES AND TO PERFORM A REPEAT INSPECTION EVERY 12,000 CYCLES THEREAFTER.SDR CALA0400485Floorbeam · corrodedINSPECTION FOUND FLOORBEAM UPPER CHORD CORRODED AT BS 720 FROM RBL 58.2 TO LBL 58.2. REPAIRED IAW ECRA 5320-01753, SRM 51-10-02, FIGURE 12, PARAGRAPH 6 AND 51-40-02, FIGURE 3 AND 12.SDR CALA0400484Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT BS 740 FROM RBL 9 TO LBL 4. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA0400483Skin · corrodedINSPECTION FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 778 BETWEEN LBL 6 AND RBL 6. THE CORRODED AREA OF SKIN WAS REMOVED AND A REPAIR WAS INSTALLED IAW SRM 53-00-01 FIGURE 204.SDR CALA0400459Floorbeam · corrodedINSPECTION FOUND FLOORBEAM CORRODED AT STA 1640 BETWEEN LBL 9 AND RBL 14, WL 208. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 203.SDR CALA9802050Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 625 BETWEEN STRINGERS 16L AND 17L. REPAIRED IAW SRM 53-00-01, FIGURE 101.SDR CALA9800824Slide · jammedR2 DOOR JAMMED IN DOORWAY DURING SAMPLE SLIDE DEPLOYMENT, SLIDE COVER HIT DOOR JAMB. REPLACED SLIDE AND ASSIST BOTTLE PER CAL WORKCARDS.SDR CALA9600963Circuit Module · inoperativeTHE RT MAIN LANDING GEAR DOWN LIGHT DID NOT ILLUMINATE WHEN GEAR WAS EXTENDED ON APPROACH TO EWR. THERE WAS NO ASSOCIATED EICAS MESSAGE. THE APPROACH WAS ABORTED AND THE GEAR WAS CONFIRMED DOWN DURING A TOWER FLY-BY. THE AIRCRAFT LANDED WITHOUT INCIDENT. M
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