N27246
Service difficulty reports · 149
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 = 'N27246' 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 = 'N27246' 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 CALA2020012600253Shear Angle · crackedLEFT OVERWING BOX BS 540 SHEAR ANGLE WAS CRACKED AT LBL 40.87. REMOVED AND REPLACED THE OVERWING BOX SHEAR ANGLE. IAW SRM 51-40-02 AND DWG 1112401.SDR CALA2020012600252Shear Angle · crackedRIGHT OVERWING BOX, BS 540 SHEAR ANGLE WAS CRACKED AT RBL 32.53. REMOVED AND REPLACED THE OVERWING BOX, BS 540 AT RBL 32.53 SHEAR ANGLE IAW SRM 51-40-02, AND DWG 1112401.SDR CALA2020012600251Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE WAS CRACKED AT LBL 54.6. REMOVED AND REPLACED THE OVERWING BOX BS 540, LBL 54.6 SHEAR ANGLE IAW SRM 51-40-02, AND DWG 111A2401.SDR CALA2020012600250Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE CRACKED AT LBL 15.04. REMOVED AND REPLACED THE OVERWING BOX BS 540 AT LBL 15.04 SHEAR ANGLE IAW SRM 51-40-02, AND DWG 111A2401.SDR CALA2020012600249Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE WAS CRACKED AT RBL 40.87. REMOVED AND REPLACED THE OVERWING BOX SHEAR ANGLE IAW SRM 51-40-02, AND DWG 111A2401.SDR CALA2020012600248Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE WAS CRACKED AT RBL 15.04. REMOVED AND REPLACED THE OVERWING BOX SHEAR ANGLE IAW SRM 51-40-02 DWG1112401.SDR CALA2020012600247Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE WAS CRACKED AT RBL 54.6. REMOVED AND REPLACED THE SHEAR FITTING IAW SRM 51-40-02 AND DWG 1112401.SDR CALA2020012600246Shear Angle · crackedOVERWING BOX BS 540 SHEAR ANGLE CRACKED AT LBL 32.53. REMOVED AND REPLACED THE SHEAR ANGLE IAW SRM 51-40-02, DWG 111A2401.SDR CALA2020012600245Fitting · crackedB737-06-3-0024 OVER WING BOX STA 540 ANGLE CRACKED AT LBL 6.01. REMOVED AND REPLACED OVER WING BOX STA 540 ANGLE (SHEAR FITTING) IAW B737-800 SRM 51-40-02, DWG: 1112401. AT LBL 6.01. . REMOVED AND REPLACED OVER WING BOX STA 540 ANGLE (SHEAR FITTING IAW B737-80SDR CALA2020011900185Structure · corrodedAFT WET AREA R-2 DOORWAY INBOARD CHORD CORRODED. REF TO NR 2675N389. REMOVED CORROSION AT R-2 DOOR WAY INBOARD L/10RD FOUND TO BE OUT OF LIMITS IAW SRM 53-70-15 RECEIVED NEW PART LOCATED AND DRILLED IAW SRM 51-40-05 INSTALLED NEW PART IAW SRM 51-40-02. WORK PESDR CALA2018020500490Fuse · faultyEMERGENCY SEAT MOUNTED FLOOR PROXIMITY LIGHTS INOP, ROWS 22-31. REMOVED AND REPLACED EMG BATT PK M1670 FUSES AS PER AMM 33-51-06 , SECURED CARPET RISER AND OPS CKS GOOD. ACFT OK TO CONTINUE.SDR CALA2018012600331Light · inoperativeLEFT SEAT EMERGENCY LIGHTS DO NOT ILLUMINATE BETWEEN ROWS 22 - 31. RESET BATTERY PACK AND CONNECTOR AT M1670. OPS CHECKED OKSDR CALA2017103003870Battery Pack · dischargedEMERGENCY LIGHTS OUT AT LEFT SEATS 7-14, OVERHEAD EMERGENCY LIGHTS OUT AT RIGHT OVERHEAD BINS 21-28, AND EXTERIOR OVERWING EMERGENCY LIGHTS OUT. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT SPOTS 1671 AND 1676 IAW AMM 33-51-06. OPS CHECK GOOD.SDR CALA2017082502891Battery Pack · faultyEMERGENCY LIGHTS AT THE L2 DOOR AND AFT ROWS OF SEATS NOT ILLUMINATING DURING TEST. REMOVED AND REPLACED THE M1673 BATTERY PACK. OPS CHECKED GOOD. ALL LIGHTS ILLUMINATED IAW AMM 33-51-06.SDR CALA2017061801875Lens · unsecureEMERGENCY EXIT LENS HAS FALLEN OFF. OVER WING EMERGENCY EXIT SECURED LENS.SDR CALA2017061601843Transmitter · shortedWHILE NR 2 ENGINE WAS RUNNING,,THERE WAS NO THROTTLE MOVEMENT RESPONCE, AFTER ENGINE SHUTDOWN AND RESTART, THE THROTTLE MOVEMENT AND RESPONCE STARTED ONCE AGAIN. FOUND CHANNEL B OF THE NR 2 ENGINE OIL PRESSURE LVDT T429 SHORTED CAUSING PEO LVDT & TRA SIGNAL SDR CALA2017041701044Cover · looseEMERGENCY EXIT SIGN BROKEN OFF, MISSING A LATCHING MECHANISM. RE-INSTALLED OVERHEAD EMERGENCY EXIT SIGN COVER. OK TO CONTINUE.SDR CALA2017010900045Altimeter · erraticSTANDBY ALTIMETER STICKS. INDICATES 340 WHEN ACFT IS 335. THEN JUMPS 500 FEET RESET OPEN C/B PER AMM TASK 20-60-01-860-801. OPS CHECKED NORMAL.SDR CALA2016102800825Skin · crackedLT HORIZ STAB LOWER SKIN HAS A CRACK .5" LONG AT STA 111.10 10" FWD OF AFT SPAR. LT HORIZ STAB LOWER INSPAR SKIN HAS BEEN REPAIRED IAW SRM 55-10-01 REP 11.SDR CALA2016083000610Windshield · failedWINDOW ARCING (SPARKS AND SMOKE) F/O FORWARD WINDSHIELD LOWER RIGHT. WINDOW REPLACED IAW MM 56-11-11. WINDOW HEAT AND LEAK CHECKED GOOD.SDR CALA2016031100160Skin · not reportedECRA 5331-02078 REPAIR TO FUSELAGE SKIN, BS 907 - 927, BETWEEN STRINGER -20L & -23L.SDR CALA2015011200035Sensor · failedFLAP POSITION INDICATOR NEEDLES ARE SPLIT IN UP POSITION. WHEN MOVING TO FLAPS 1 TE FLAPS DID NOT MOVE. COMPLETED FLAPS TE FLAPS ASYMMETRY CHECKLIST THEN TE FLAPS UP CHECKLIST. FSEU BITE SHOWS FLAP SKEW SENSOR 1 FAILED. REPLACED SAME IAW MM 27-59-01. OPERSDR CALA2014063000821Battery Pack · dischargedFORWARD CABIN L1 DOOR EMER FLOOD LIGHT INOPERATIVE. LAMP & R & R POWER SUPPLY BATTERY PACK IAW AMM 33-51-06-960- 805. OPERATION NORMAL.SDR CALA2014051900615Floor Support · corrodedCORROSION FOUND ON THE FLOOR SUPPORT BS 991 - 997 RBL 32. REMOVED & INSTALLED FLOOR SUPPORT IAW SRM51-40-02 GEN REV 50 & DWG 147A57 00.SDR CALA2014052900695Support · wornSEVERAL WEAR WERE FOUND ON SIDEWALL SUPPORT OF FWD CARGO STATION 494 STRINGER 25L ONE EACH STRINGER 22L, ONE EACH STRINGER 20L, ONE EACH STRINGER 23L, ONE EACH STRINGER 19L & ONE EACH S=0.3X0.2L. R & R DAMAGED SUPPORT WITH NEW SUPPORT IAW DWG 143A94505-7, 143SDR CALA2014052900694Floorbeam · corrodedSEVERAL AREAS OF CORROSION WERE FOUND ON THE FLOORBEAM UPPER SURFACE BS 967 RBL 11 - 16. REMOVED CORROSION, MEASURED DAMAGED AREA. FABRICATE REPAIR STRAP & INSTALLED REPAIR IAW ECRA 5320- 02230 & EN 737EN-53-0249.SDR CALA2014052800693Fitting · crackedEA 5320-02076 REV B & 2013-23-04 AMDT 39-17659 PERFORMED EA 5320-02076 REV B OP002 STEP 2 2 B. HFEC INSPECTED THE FASTENER HOLE FOUND CRACK INDICATION. L=0.005". DISASSEMBLED SEAT TRACK TO DETERMINE ACTUAL LOCATION OF CRACK IAW SRM 51-40-02 GEN REV 50. REPASDR CALA2014052800692Strap · crackedAD 2013-23-04 AMPT 39-17659, CRACK WAS FOUND ON RETAIN SPLICE STRAP OF CABIN SEAT TRACK STATION 727B LBL 45.50 L=1.5". PERFORMED ECRA 5320-02235.SDR CALA2014052800691Strap · crackedAD 2013-23-04 AMDT 39-17659 CRACK WAS FOUND ON RETAIN SPLICE STRAP OF CABIN SEAT TRACK STATION 727B, LBL 24.75 L=0.3". PERFORMED ECRA 5320-02235.SDR CALA2014052800690Seat Track · crackedEA 5320-02076 REV B & AD 2013-23-04 AMDT 39-17659, PERFORMED EA 5320-02076 REV B OP 01 STEP 4 1 C. HFEC INSPECTION THE FASTENER HOLE, FOUND CRACK INDICATION LBL45.50 1 EA. TRIMMED THE FLANGE, MADE INSURANCE CUT. MADE & INSTALLED REPAIR PARTS IAW ECRA 5330-0SDR CALA2014052800689Seat Track · crackedEA 5320-02076 REV B & AD 2013-23-04 AMDT 39-17659 PERFORMED EA 5320-02076 REV B OP 01 STEP 3 1 C. HFEC INSP FOUND FASTENER HOLE CRACK INDICATION LBL 24.75 2 EACH. TRIMMED THE FLANGE, HFEC FOR CRACKS, NONE FOUND. MADE & INSTALLED REPAIR PARTS IAW ECRA 5320-SDR CALA2014052700682Seat Track · crackedEA 5320-02076 REV B & AD 2013-23-04 AMDT 39-17659, PERFORMED HFEC INSP OF FOUR FASTENERS HOLES COMMON TO THE SPLICE STRAP & FWD SEAT TRACK OTBD FLANGES, FWD OF THE STATION 727B, RBL 24.75 FOUND CRACK IN THE INSIDE HOLE AFT. OVERSIZED THE CRACKED HOLE, HFEC TSDR CALA2014052700666Seat Track · crackedPERFORMED HFEC INSP OF FOUR FASTENERS HOLES COMMON TO THE SPLICE STRAP & FWD SEAT TRACK FLANGES, FWD OF THE STATION 727B, RBL45.5. FOUND CRACK IN THE OTBD FWD HOLE TRIMMED THE FLANGE, PERFORMED HFEC, NO CRACK, INSTALLED REPAIR PARTS IAW ECRA 5320-02235.SDR CALA2014052700681Web · corrodedSEVERAL AREAS OF CORROSION WERE FOUND ON THE FLOOR SUPPORT BS 986.5 -989 LBL 31 - 33. REMOVED AND REPLACED WEB IAW SRM 51-40-02.SDR CALA2014052300655Doubler · corrodedSEVERAL CORROSIONS WERE FOUND ON UPPER SURFACE OF FWD CARGO BOTTOM ANTENNA DOUBLER STATION 500 - STATION 500A STRINGER 28L - STRINGER 28R S=3"X2". REMOVED CORROSION, MEASURED AREA, TRIMED OUT DAMAGED AREA & INSTALLED NEW DOUBLER IAW ECRA 5331-01884 PART 1. ISDR CALA2014052300654Web · corrodedSEVERAL AREAS OF CORROSION WERE FOUND ON SUPPORT WEB UPPER SURFACE OF FWD CARGO DOOR CUT OUT BS 450 - 490 RBL 28. REMOVED AND REPLACED THE DAMAGED WEB IAW SRM 51-40-02 GEN REV 50.SDR CALA2014052300653Threshold · corrodedTHRESHOLD UPPER SURFACE CORRODED BS 806 - 815 RBL 26. REMOVED AND REPLACED THE DAMAGED THRESHOLD IAW SRM 51-40-02 GEN REV 50.SDR CALA2014052300652Stringer · corrodedCORROSION WAS FOUND ON FWD CARGO BOTTOM STRINGER 3" AFT STATION 500G, STRINGER 27 S=0.5"*0.5". CUT OUT DAMAGED SECTION IAW SRM53-00-03 REPAIR I REV 50. MADE & INSTALLED THE REPAIR PARTS IAW SRM53-00-03 REPAIR I REV 50. ACP RII INSPECTION IAW ALL CRITICAL STESDR CALA2014051600607Door Sill · corrodedMAIN DECK RT LOWER MAIN SILL INNER CHORD LOWER SURFACE HAS CORROSION. S=0.4"*0.4" STATION 350.5 RBL 62. REPLACED NEW INNER CHORE IAW SRM 51-40-00 GEN REV 50 & 737EN-53 -0254 & ECRA5310-06047.SDR CALA2014051600609Floorbeam · corrodedTWO CORROSIONS WERE FOUND ON THE FLOOR SUPPORT OF MAIN DECK. SMAX=0.2"*0.2" STATION 991.5 RBL 36 RBL43. REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02 GEN REV 50. OK TO INSTALL. INSTALLED THE NEW FLOOR SUPPORT IAW SRM 51-40-02 REV 58.SDR CALA2014051600608Floor Support · corrodedMAIN DECK FLOOR SUPPORT UPPER SURFACE IS CORROSION S=1"*0.8", STATION 950 RBL 29. REMOVED THE FLOOR SUPPORT IAW SRM 51-40-02 GEN REV 50. REPLACED THE NEW FLOOR SUPPORT IAW SRM 51-40-02 GEN REV 50.SDR CALA2014051600610Floorbeam · corrodedCORROSION WAS FOUND ON THE INTRINSIC REPAIR FILLER OF MAIN DECK FLOORBEAM. S=0.15"*0.15" STATION 986 RBL 29. REPAIRED THE STATION 986 FLOORBEAM UPPER FLANGE IAW LP 9141729.SDR CALA2014051500600Seat Track · corrodedMAIN DECK SEAT TRACK CROWN HAS CORROSION STATION 369 - STATION 379 LBL 22 - 09 L=10". R & R DAMAGED SEAT TRACK IAW SRM 53-00-52 REPAIR 4 REV 50 & ECRA 5320-0228.SDR CALA2014051500599Floorbeam · corrodedCORROSION WAS FOUND ON THE FLOOR SUPPORT WEB OF MAIN DECK. SMAX=2.5"*2" STATION 986 - STATION 991 RBL 32 - RBL 44. REMOVED THE FLOORBEAM WEB IAW SRM 51-40-02 GEN REV 50. REPLACED WEB LOWER SUPPORT PN 147A8530-14, 147A5709-2, 147A5709-4 IAW SRM 51-40-02 GEN SDR CALA2014051500598Floorbeam · corrodedSEVERAL AREAS OF CORROSION WERE FOUND ON THE FLOORBEAM UPPER SURFACE OF MAIN DECK SMAX=0.5"X0.2" STATION 986.5 LBL 30 - LB 45. CUT & REMOVED THE DAMAGED FLANGE BETWEEN LBL 40 & RBL 40, LBL 40 & LBL 60 & RBL 40 & RBL 60. LOCATED & DRILLED UP T CHORD, SHEAR TISDR CALA2014051500594Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER SURFACE IS CORROSION. S MAX=0.6"*0.5" STATION 986, LBL 4, RBL 4. REMOVED AFFECTED REPAIR FILLER IAW SRM51-40-0 2GEN REV 50, BLENDED OUT CORROSION IAW SRM 51-10-02 GEN REV 50. REPAIRED THE STATION 986 FLOORBEAM UPPER FLANGE IAW LP 91SDR CALA2014051500592Floor Support · corrodedCORROSION WAS FOUND ON THE FLOOR SUPPORT OF MAIN DECK. S=0.4"*0.3" STATION 991 - STATION 1016 LBL 32. REMOVED THE FLOOR SUPPORT IAW 51-40-02 GEN REV 50, OK TO INSTALL . INSTALLED THE SUPPORT IAW SRM 51-40-02 GEN REV 50 DWG 147A5700 & 015968.SDR CALA2014051500593Floorbeam · corrodedCORROSION WAS FOUND ON THE FLOOR SUPPORT OF MAIN DECK. SMAX = 0.5"*0.3" STATION 1020 LBL 32 - RBL 32. FABRICATED THE FLOOR SUPPORT IAW DWG 147A5710-5 & NR53-0 10 & CONTROL SHEET FOR SELF-FABRICATING PART UAL. OK TO INSTALL. INSTALLED THE NEW FLOOR SUPPORTSDR CALA2014050900573Frame · crackedAFTER REMOVING THE BRACKET PERFORMED HFEC INSPECTION OF FRAME & BRACKET AT STA 400 BTW STRINGER 8R & STRINGER 9R FOUND CRACK ON THE FRAME. REMOVED DICATION. APPLIED PRIMER 02 TASK 9.0 FIG 3 STEP 10 DRILLED HOLES IN ANGLE A FLANGE, THE SUPPORT BRACKET FASTENERSDR CALA2014050900572Frame · crackedAFTER REMOVING THE BRACKET PERFORMED HFEC INSPECTION OF FRAME & BRACKET AT STATION 500A BETWEEN STRINGER 8L & STRINGER 9L FOUND CRACK ON THE FRAME. IAW EA5310-04716 REV G OPERATION 02 TASK 9.0 FIG 3 STEP 1 REMOVED DICATION. DRILLED HOLES IN ANGLE A FLANGE IA
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