N37462
Service difficulty reports · 34
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 = 'N37462' 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 = 'N37462' 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 CALA2026090119172Wire Harness · damagedEMERGENCY LIGHT AT SEAT 38C INOPERATIVE. REPLACED THE LAMPS, NO HELP. ALL OTHER EMERGENCY PATH LIGHTS WORKS, ONLY LIGHT 38C INOPERATIVE. MEL 3319E APPROVED, COMPLIED WITH MEL. VERIFIED SEAT TRACK HARNESS HAS DAMAGED WIRES NEAR FLOORBOARD CONNECTION. COULSDR CALA2026072417966Skin · missingLEFT WING OTBD TE AFT FLAP MISSING LARGE SECTION OF LOWER FLAP SURFACE, NO DAMAGE TO HONEYCOMB. LT WING OTBD AFT FLAP SKIN MISSING HONEYCOMB SHOWING OK TO INSTALL LTT OTBD AFT FLAP. REMOVED LT AFT FLAP IAW AMM 27-51-22. VERIFIED INSTALLATION OF LEFT OUTBD ASDR CALA2026021913915Light · damagedROW 3 ABC EXIT LIGHT DETACHED ITEM PLACED ON MEI. THIS IS THE FWD SEAT LIGHT AT 3B. THE AFT SEAT LIGHT FUNCTIONS NORMALLY. ALL OTHER EMERGENCY LIGHT FUNCTIONS ARE NORMAL. CAP IS MISSING TAPED OVER LIGHT ASSY. POSES NO DANGER TO PASSENGERS OR CREW. TOMC OK ITEMSDR CALA2025101410047Slide · no discrepancyDOOR SLIDE SAFETY PIN INSTALLED AT 2R REMOVED SAFETY PIN FROM SLIDE AT #2R. STOWED IN POUCH. VERIFIED SLID PIN REMOVED IAW GMM 09-10-05SDR CALA2025092409218Bolt · looseLEFT WHEEL WELL, AILERON CABLE PULLEY HARDWARE BACKING OFF. AMM-20-51-11-910-801. RETORQUED HARDWARE. NO DEFECTS NOTED.SDR CALA2025082007951Slide · no discrepancyMAIN DOOR SLIDE HAS EXCESS MATERIAL EXPOSED. INSPECT DOOR SLIDE FOUND MATERIAL FROM SLIDE WITHIN LIMITS AS PER AMM 25-66-01SDR CALA2025081807877Light · detachedMID LAV EMER LIGHT DETACHED. REINSTALLED MID LAV EMERGENCY LIGHT AND ALL OPS GOOD.SDR CALA2025061705586Outflow Valve · faultedRAPID RISE IN DIFF PRESS URE. CABIN PRESSURE DECREASED INTO NEGA TIVE. REF FIM 21-31 TASK 801 PERFORMED BITE CHECK OF DCPC 1 AND 2. FOUND ACTIVE FAULT ON DCPC 1, CAB PRESS SW ACTIVE MESSAGE. NO FAULTS FOUND ON DCPC 2. REF FIM TASK 21-31 TASK 820 FOR CAB PRESS SDR CALA2025041403832Light · unsecureDOOR LIGHT AT 20 KTS HATCH 1L HANDLE WASNT SEATED PERFORMED OPS CK OF FWD ENTRY DOOR SEVERAL TIMES FROM OUTSIDE AND INSIDE REF AMM 52-11-00. DOOR FULLY CLOSES AND LIGHTS OPS NORMAL.SDR CALA2024080502153Crease Beam · corrodedB737-53-3-0736: MAIN CABIN R/H SIDE CREASE BEAM INNER CHORD UPPER SURFACE IS CORRODED BETWEEN STA 787 AND 807. TRANSCRIBED FROM HAECO GSO NRC 9288511. REPAIRED CREASE BE33AM INNER CHORD FORM STA 787 TO STA 867 IAW UAL EC/RA 5360-01845 REV-. HAECO GSO MECH V8SDR CALA2024080602173Connector · disconnectedLAV T FWD CONNECTED LAV T CONNECTOR P21 IAW CMM 25-40-01. TEST GOOD IAW B737NG AMM 33-31-00.SDR CALA2024080602172Connector · damaged(SUPPORT TASK) BOTH LAV T EMER LIGHTS INOP. RESEATED PIN ON P16 OF LAV T AND CONNECTED CONNECTOR P21 IAW CMM 25-40-01. TEST GOOD IAW AMM 33-51-00.SDR CALA2024073102144Rib · crackedSUPPORT TASK: RH ELEVATOR END RIB FOUND CRACKED. TRANSCRIBED FROM HAECO GSO NRC 9288653.SDR CALA2024073102143Floorbeam · corrodedB737-53-3-0736: MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT STA 380 APPROX LBL54. TRANSCRIBED FROM HAECO GSO NRC 9288451.SDR CALA2024072602112Door Frame · gouged(B737-52-3-0727) L1 DOOR, FRAME, FORWARD EDGE, UPPER AND LOWER C ORNERS ARE GOUGED. TRANSCRIBED FROM HAECO NR 9288604.SDR CALA2024072202076Floorbeam · corroded(B737-53-3-0737) MAIN CABIN FLOOR BEAM UPPER SURFACE IS CORRODED AT STA 1016 APPROX RBL35. TRANSCRIBED FROM HAECO GSO NRC 9288545.SDR CALA2024072202074Crease Beam · corroded(B737-53-3-0737) MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE HAS CORROSION FROM STA 967-986 LBL 52. TRANSCRIBED FROM HAECO GSO NRC 9288529. PLEASE SEE LOG PAGES 8649819 & 8649695 MAIN CABIN CREASE BEAM INNER CHORD UPPER SURFACE AT L2 DOOR SURROUND REPAIRESDR CALA2024071102008Web · corrodedSUPPORT TASK: AFT CARGO ENTRANCE, WEB HAS SEVERAL AREAS OF CORROSION. REMOVED DAMAGE-CORROSION-FOUND OUT OF LIMITS. ORIGINAL THICKNESS .045, MAT LOSS .020, REMAINING .025 (<0.10+). RECEIVED AND INSTALLED NEW WEB P/N 146A8123U25. REMOVED DAMAGED WEB IAW B737SDR CALA2024070801973Stop Fitting · gougedB737-52-3-0690 MAIN CABIN L2 DOOR AFT UPPER DOOR STOP FITTING HAS GOUGE. TRANSCRIBED FROM HAECO GSO NRC 9288110. REMOVED AND REPLACED L-2 DOOR AFT UPPER STOP FITTING REF B737-900ER SRM 51-40-02, BAC DWG 147A6116 REV B AND BAC DWG 147A6125 REV-. HAECO GSO MESDR CALA2023052201590Lens · missingEMG EXIT LT COVER AT 1L MISSING REPLACED EMERGENCY EXIT LIGHT LENSE AT FWD CLOSET/ MONUMENT AFT CORNER REF IFM 25-20-23. OPS CHECK GOOD.SDR CALA2023042801280Probe · inoperativeEGT LIMIT EXCEEDED APPRX 50AGL ON TAKEOFF APPRX 950 DEGREES NOTE D AS PER PILOT REPORT, ENGINE TEMPERATURE EXCEEDED FOR CREW REPORTED ENG WAS NOT SHUT DOWN IN FLIGHT. NORMAL ENG SHUT APPROXIMATELY 10SECONDS, AT 102.3 POWER SETTING WITH NO OTHER DOWN AT GATE. ESDR CALA2023031700791Windshield · unknownBIRD STRIKE. MULTIPLE. HIT WINDSHIED AND OTHER AREAS. ACCOMPLISHED AFTER BIRD STRIKE IAW AMM TASK 05-51-18-210-801. NO DAMAGE, NO DENTS, NO DELAMINATION ON WINDSHIEL. OK TOCONTINUE.SDR CALA2022062001544Engine · overtempREJECTED TAKEOFF APROXIMATELY 110KTS DUE RED EGT ENGINE 2 INDICATION #2 ENG EXCEEDANCE WAS 950 DEGREES CELSIUS FOR 4 SECONDS, PEAKED OPENED ENGINE FOR BORESCOPE REF AMM 72-00-00-200-807-F00 AND ACP BOROSCOPES USING AMM72-00-00-200-807F00, AND AT 980 DEGREES CESDR CALA2019052000792Control Cable · brokenINSP A/C FOUND SPOILER BODY CABLE HANGING IN FWD E&E COMPARTMENT / INTERROGATED PSEU FOUND FAULT CODES 31-52108 GS PRESS A FAULT AND 31-52109 GS PRESS B FAULT. DO NOT DISPATCH. PERFORMED INSPECTION OF SPEED BRAKE CONTROL CABLES SBA-2 & SBB-2 FROM FWD. ACC. COMSDR CALA2018120702538Lamp · inoperativeDOOR 2L EXTERIOR EMERGENCY LIGHT INOP RELAMPED DOOR 2L EXTERIOR EMERGENCY LIGHT OPS CHECK OK ACCOMPLISHED THE INSPECTIN OF DOOR 2L EMERGENCY LIGHT INSTALLATI ON.SDR CALA2017062602000Light · looseSEAT 25C EEL LIGHT BROKEN OFF OF SEAT SHROUD. LIGHT IS STILL WORKING. RESECURED LIGHT.SDR CALA2017042801138Unknown · malfunctionedFUEL QUANTITY INDICATION, FLIGHT COMPARTMENT IMBAL MESSAGE SHOWS DURING CLIMB, FUEL IMBALANCE ILLUMINATE. FUEL FLOW SAME. EMERGENCY DECLARED. INSPECTED AC FOR FUEL LEAKS. NONE FOUND. PERFORMED FQIS BITE, NO FAULTS FOR INFLIGHT OR ON THE GROUND. VERIFIED FQIS SDR CALA2016121901120Fuse · faultyOVERHEAD EMERGENCY LIGHT INOP AT 29 DEF AND 34DEF. REPLACED FUSE IN BATTERY CHARGER M2627 MM 33-51-06. OP CKS GOOD.SDR CALA2016072800464Housing · looseEMERGENCY LIGHT AT SEAT 26C FOUND LOOSE. SECURED LIGHT IN PLACE. REPLACED LIGHT HOUSINGSDR CALA2015050600376Unknown · odorELECTRICAL FUME SMELL AFTER TAKEOFF, ENTIRE AIRPLANE. DIVERT, PLANE CHG FROM 426 TO 462 RAN APU & BOTH ENGS TRYING TO ISOLATE CAUSE OF ODOR. DETERMINED TO BE OIL WHILE APU BLEED IS ON. CREW CONCURRED WITH OIL SMELL TO BE WHAT THEY SMELLED. NO ACTIVE EXTERNSDR CALA2015021200099Light · inoperativeSUPPORT SEAT ROW 9 ABC EPL LIGHT INOPERATIVE. R & R INOPERATIVE LIGHT EPL AT SEAT ROW 9 ABC IAW IFM CMM 25-26-12. OPERATIONS CHECKED GOOD.SDR CALA2015020600082Battery Pack · dischargedSUPPORT TASK 8 ABC - 14 ABC EMER LIGHTS INOPERATIVE. TROUBLESHOOTING REVEALED AN INOPERATIVE BATTERY PACK M2503, AN INOPERATIVE FUSE. REPLACED BATTERY PACK IAW AMM 33-51-06. REPLACED FUSE IAW AMM 33-51-06. EMER LIGHTS TESTED OK IAW AMM 33-51-00.SDR CALA2013112600864Terminal · burnedRT CTR TANK RELAY R963 ON TERMINAL B2, WIRE TERMINAL SHOW S SIGNS OF BURNING. R & R TERMINAL LUG B2 AT R963 IAW SWPM 20-30-11 WDM 28-23-11, TESTED OK.SDR CALA2013112600863Wire · out of positionIAW WC 29-2820-1-7802 STEP 01C 19A & 19B AT RELAY R963 PINS X1 & X2 VOLTAGES ARE INCORRECT RT CTR TANK RELAY. IAW WDM 28-23-11 PROPERLY POSITIONED & SECURED R963 WIRE W6 210-0214-20 TO X1 & 0215-20 TO X2 IAW WDM & SWPM 20-11-30. ALL READINGS SATISFACTORY IAW
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