N37293
Service difficulty reports · 47
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 = 'N37293' 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 = 'N37293' 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 CALA2026101220303Door · crackedLEFT MLG STRUT DOOR CRACKED ABOVE ATTACHEMENT RIVET AT STRUT BRACKET. ACCOMPLISHED INSTALLATION OF REPAIR PARTS AT LT MLG CENTER DOOR IAW SRM 52-80-02-2R-2.SDR CALA2026100520073Floorbeam · corrodedCORROSION ON FLOORBEAM UPPER SURFACE FROM LBL 50 TO LBL 59, BS 344. ACCOMPLISHED A FLOORBEAM REPAIR AT BS 344 BETWEEN LBL 35 TO LBL 60 IAW SRM 53-10-51-2R-10.SDR CALA2026100520067Floor Support · corrodedCORROSION ON FLOOR SUPPORT BTWN BS 294.5 - 312, LBL 10. R & R THE FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 141A5600.SDR CALA2026100520061Floor Support · corrodedCORROSION ON FLOOR SUPPORT, L1 DOOR LOWER SILL INNER CHORD LBL 60 FROM BS 312 - 360. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 142A0050.SDR CALA2026100520059Stringer · crackedCRACK FOUND AT RIGHT WING FUEL TANK AT U-9 REIFORCEMENT AT WSTA 617. ACCOMPLISHED REPAIR OF U-9 STRINGER AT RT WING WS 617 IAW ECRA 5720-03687.SDR CALA2026100520053Strap · corrodedSPOT OF CORROSION ON AFT WET AREA FLOOR SUPPORT WEB STRAP, RBL 3, BS 1016. REMOVED AND REPLACED THE FLOOR SUPPORT WEB STRAP IAW SRM 51-40-02-0G-0, AND DWG 147A570.SDR CALA2026100520051Structure · corrodedSPOTS OF SURFACE CORROSION AT AFT L2 DOOR LOWER SILL INNER CHORD LBL 60 FROM BS 947.75 - 992.8, REMOVED AND REPLACED L2 DOOR INNER CHORD IAW SRM 51-40-02-0G-0 AND DWG 147A5700.SDR CALA2025102110342Light · inoperativeROW 8 ABC ECONOMY PASSENGER SEAT EMERGENCY PATH LIGHTING (EPL) INOP. REPLACED ROW 8ABC EMERGENCY PATH LIGHTING (EPL) ASSY REF AMM 33-51-11 OPS CHECK GOOD OKAY FOR SERVICESDR CALA2025102110341Light · inoperativeROW 11ABC ECONOMY PASSENGER SEAT EMERGENCY PATH LIGHTING (EPL) INOP REPLACED ROW 8/11 ABC EMERGENCY PATH LIGHTING (EPL) ASSY REF AMM 33-51-11 OPS CHECK GOOD OKAY FOR SERVICE INFO ONLYSDR CALA2025101309971Cvr · inoperativeCOCKPIT VOICE RECORDER DOES NOT TEST. R & R CVR IAW AMM REF TASK 23-71-11-000-801, OPS CHECK GOOD.SDR CALA2025101309966Panel · inflt separationRIGHT WING AERODYNAMIC PANEL BELOW ELEPHANT EAR CAME OFF AROUND 14K FEET CAUSING DAMAGE. FOUND PANEL HAD COME OFF IN FLIGHT AND DAMAGED THE TAIL END OF THE RIGHT WING INBD CANOE. NR 6 CANOE TAILCONE ON RT WING TRAILING EDGE FLAP DAMAGED. CREW GAVE VERBAL TURNOSDR CALA2025012301979Idg · faultyAC GENERATOR DRIVE SYSTEM DRIVE LIGHT IS ILLUMINATED GEN-2 REPLACED IDG #2 REF AMM 24-11-11. OPS CHECK GOOD. C/W PER AMM 24-11-11 AND GMM 09-10-05 ADD EMP:U192746SDR CALA2024080500359Baffle · crackedINSPECT (GENERAL VISUAL) FORWARD CARGO UNDERFLOOR AREA FOR: BAY 12 R/H WEB HAS CRACK ON FWD CORNER. REMOVED BAFFLE ASSEMBLY. REF SRM 51-40-02 REPLACED WITH NEW BAFFLE ASSEMBLY AND PERFORM REPAIR TO MAKE IT EASIER TO INSTALL REPLACEMENT BAFFLE AS PER SRM 53-30SDR CALA2023120403540Battery Pack · dischargedSEAT 22 TO 31 EMERGENCY PATHWAY LIGHTING INOP (REF. AAR NR 99990 114).SDR CALA2023111703416Rib · crackedREPAIRED RH HORIZONTAL STABILIZER RIB STABILIZER LOWER RH FLANGE, WORK PERFORMED IAW B737-800 SRM 55-10-09-2R-5, 51-40-05-0G-0,51-20-10-0G-0,SOPM 20-41-02,NDTM PT6(57-00-00 PROC 23, 51-00-00 PROC 16.(REF AAR NR 99990443) REPAIRED RH HORIZONTAL STABILIZER RIB SSDR CALA2023112003439Skin · dentedRE-SKIN FWD CARGO DOOR (REF: AAR NR 99990119)SDR CALA2023112003437Skin · dentedRE-SKIN AFT CARGO DOOR (REF: AAR NR 99990120)SDR CALA2023111703419Skin · crackedNDT CRACKS FOUND CRACK 1 FOUND AT L/H HORIZONTAL STAB STA 101.90 MARKED ON LOWER SKIN. (REF: AAR NR 99990386) REMOVED DAMAGE CRACKS AND REPAIRED AREA AT L/H HORIZONTAL STAB 101.90 LOWER SKIN IAW B737-800;SRM 55-10-01-2R-11. THIS REPAIR IS A CATEGORY B REPAIR ASDR CALA2023111703418Rib · crackedNDT CRACK FOUND CRACK FOUND R/H STAB STA 101.90 MARKED ON LOWER SKIN. (REF: AAR NR 99990387) REPAIRED RH HORIZONTAL STABILIZER LOWER SKIN STA 101.9, WORK PER FORMED IAW B737-800 SRM 55-10-01-2R-11,55-10-2R-11,55-10-09-2R-5 ,51-20-01-0G-0,NDT PT6 51-00-00 PROC SDR CALA2023111703417Skin · crackedNDT CRACKS FOUND CRACK LH HORIZONTAL STAB FOUND STA 184.70 MARKED ON LOWER SKIN (REF: AAR NR 99990388) REMOVED DAMAGE CRACKS AND REPAIRED AREA AT L/H HORIZONTAL STAB. AT STA 184.70 IAW B737-800;SRM 55-10-01-2R-11. THIS REPAIR IS A CATEGORY B REPAIR AND REQUIRESDR CALA2023072602336Fseu · unknownSPLIT FLAPS WHEN 5 SELECTED. LOG PAGE LOCKED FOR POSITIVE FIX FSEU BITE SHOWS NOTHING FOR CURRENT FAULTS, BUT SHOWS ''TE FLAPS SNSR DIS'' MAINT MSG 27-52261 ON LAST FLT. REF FIM 27-51 TASK 832. UNLOCKING FOR MX ACCOMPLISHED FIM TASK 27-51 TASK 832 FOUND ALL MSDR CALA2022091902411None · tornFLIGHT ATTENDANT SEAT BOTTOM COVER TORN AT DR-2R LT JUMPSEAT SEAT USEABLE.PLACED SEAT COVER ON INT. R&R FA SEAT COVER JUMPSEAT DR-2R LTSDR CALA2021121002332None · crackedRT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638163 REPAIRED RT MLG W/W VERTICAL PRESSURE WEB AS PER B737 SRM 57-10-10-2R-3 WORK ACCOMLPISHED BY V937767SDR CALA2021121002313Pressure Blkhd · crackedLT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638162 REPAIRED LT MLG W/W VERTICAL PRESSURE WEB AS PER B737 SRM 57-10-10-2R-2 ALTERNITIVE 2 PREFORMED HFEC AND LFEC RE-INSPECT AT EVARY 36,000 FC WITH A THRESHOLD OF 56,000 FC I.A.W B737 SRM 57-10-10-SDR CALA2021121002312Pressure Blkhd · crackedRT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638163 REPAIRED RT MLG W/W VERTICAL PRESSURE DECK WEB AS PER B737 SRM 57-10-10-2R-3 ALTERNATIVE 2 PERFORM HFEC AND LFEC RE-INSP AT EVERY 36,000 FC WITH A THRESHOLD OF 56,000 FC AFTER REPAIR COMPLETION SDR CALA2021120802304Pressure Deck · crackedLT MLG W/W VERTICAL PRESSURE DECK WEB CRACKED REF AAR N/R 9638162 REPAIRED LT MLG W/W VERTICAL PRESSURE DECK WEB AS PER B737 SRM 57-10-10-2R-3 WORK ACCOMPLISHED BY V894495SDR CALA2021111802131Floor Support · corrodedFOUND CORROSION AT FLOOR STRUCTURE STA 328 RBL 55 REF AAR N/R 9637647 REMOVED CORROSION FOUND OUT OF LIMITS PER ECRA 5321-01330 REV B REMOVED DAMAGE AREA FROM FR328 RLB 55 AND INSTALLED REPAIR AS PER B737 SRM 53-10-51-2R-7 REPAIR 7 FIG 206 WORK ACCOMPLISHED BYSDR CALA2020010600104Pressure Deck · crackedON WALK AROUND FOUND POSSIBLE CRACK IN RIGHT WHEEL WELL VERTICAL PRESSURE DECK WEB. PERFORMED HFEC INSPECTION ON RT W/W VERTICAL PRESSURE DECK WEB AND FOUND 1EA CRACK, CRACK IS APPROX. 2IN 3/16" LONG. REF 737 NDT MANUAL PART 6 51-00-00 PROC 23. REMOVED SEAT 22SDR CALA2020010600103Pressure Deck · crackedREF L/P 4226246. I/B CRACK MEASURING 11/16" LOCATED @ LWW PRESURE DECK WEB BETWEEN LBL 31.83 & LBL 40.00 WILL BE REPAIRED ON THIS L/P. STOP DRILLED END OF THE CRACK. REQUEST Q/C. HFEC OF STOP DRILL HOLES. CRACK BEEN STOP. OK TO CONTINUE WITH SLOT REPAIR. PERFSDR CALA2020010600102Pressure Deck · crackedREF L/P 4226246. O/B CRACK MEASURING 2 AND 1/16" LOCATED LWW PRESURE DECK WEB BETWEEN LBL 40.00 AND LBL 45.64 WILL BE REPAIRED ON THIS L/P. STOP DRILLED END OF THE CRACK. REQUESTN Q/C PERFORM STEP 4.C. HFEC OF STOP DRILL HOLE. CRACK BEEN STOP. OK TO CONTINUE SDR CALA2017110603946Actuator · faultyREVERSE THRUST LEVER HAS LOST MOTION, NO THRUST REVERSER OPERATION ENGINE 1 FOUND NR 1 ENG OTBD THRUST REVERSER LOWER ACTUATOR AND SYNC LOCK INOP. R&R NR 1 ENG OTBD LOWER THRUST REVERSER ACTUATOR AND LOWER SYNC LOCK REF AMM 78-31-03, ALSO R&R UPPER AND LOWER SSDR CALA2017071402189Control Unit · failedAT FL 390 2.5 HRS INTO FLT MASTER CAUTION IRS DC FAIL LIGHTS CAME ON SW/HOT BAT BUS CB TRIPPED. EMERGENCY DECLARED. REPLACED STANDBY POWER CONTROL UNIT PER AMM 24-34-11, INSTALLATI ON TEST GOOD, NO FAULTS NOTED, CLEARED FAULTS ON ELECTRICAL PANELSDR CALA2017032600730Control Lever · intermittentWHILE RAISING GEAR THE 3 RED DISAGREE LIGHTS REMAINED ILLUMINATED RAN QRH. EMERGENCY DECLARED. BITE TEST ON PSEU FOUND FAULT 32-62008 AND FIM TASK FOUND CONTROL LEVER INTERMITTENT. R/R SAME PER AMM 32-31-11.SDR CALA2015050400362Seat Track · crackedAFT INBD HOLE HAS CRACK INDICATION ON SEAT TRACK FLANGE & SPLICE PLATE. THE MINIMUM EDGE DISTANCE CANNOT BE MAINTAINED ON INSTALLATION OF NEW SPLICE STRAP AT SEAT TRACK FLANGES IAW EA 5320-02076 REV F OP 4 FIGURE 11 NOTE D. VERIFY INSTALLATION OF FLOORBEAM USDR CALA2015042800333Rib · crackedLEFT HORIZONTAL STAB IN SPAR RIB AT STATION 92.70 STIFFENER NR 2 IS CRACKED AT LOWER TRANSITION RADIUS. REF LOG PAGE 9737466 WRITTEN IN ERROR. REPAIRED STAB IN SPAR RIB IAW ECRA 5510-02523.SDR CALA2015042800327Rib · crackedLEFT HORIZONTAL STABILIZER IN SPAR RIB AT STATION 129''50 STIFFENER NR 3 CRACKED AT LOWER TRANSITION RADIUS. REPAIRED STABILIZER IN SPAR RIB IAW ECRA 5510-02523.SDR CALA2015042800326Rib · crackedLEFT HORIZONTAL STABILIZER IN SPAR RIB AT STATION 92.70 STIFFENER NR 3 CRACKED AT LOWER TRANSITION RADIUS. REPAIRED IN SPAR RIB IAW ECRA 55 10-02523.SDR CALA2015042000316Stiffener · crackedLEFT HORIZONTAL STAB NEEDS ACCESS CUT OUT FOR IN SPAR RIB STATION 129.50, STIFFENER 3 CRACK REPAIR. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. INITIATED DIP TO INSPECT AT 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & EVERY 9000 FLIGHT CYCLES THERSDR CALA2015042000314Rib · damagedLEFT HORIZONTAL STAB NEEDS CUT OUT LOWER SKIN FOR ACCESS TO REPAIR IN SPAR RIB STATION 92.70. INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. INITIATED DIP TO INSPECT AT 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & EVERY 9000 FLIGHT CYCLES THEREAFTERSDR CALA2015042000307Skin · puncturedRIGHT ELEVATOR UPPER SKIN HAS A HOLE PUNCHED IN IT 8.5" FROM FWD EDGE & 5.5" FROM INBD EDGE. REPAIRED PUNCTURE DAMAGE ON UPPER SKIN OF ELEVATOR IAW SRM 51-70-04.SDR CALA2015042000291Skin · dentedFORWARD CARGO DOOR EXTERIOR SURFACE HAS DENT LOCATED 20.5" FROM FWD EDGE & 16" FROM TOP EDGE, L=8", W=4", Y=.150", W/Y=26. DENT IS OUT OF LIMITS IAW SRM 52-30-01. ALLOWABLE DAMAGE 1, FIGURE 103 DETAIL F. CUT OUT DAMAGE ON FWD CARGO DOOR. FABRICATED, LOCATESDR CALA2015041300276Skin · crackedRIGHT HORIZONTAL STAB LOWER SKIN HAS A CRACK INDICATION AT RIB STATION 129.50 AFT OF DRAIN HOLE. INSTALLED HORIZONTAL STAB LOWER IN SPAR SKIN EXTERNAL DOUBLER IAW SRM 55-10-01 REPAIR 11. INSPECTION THRESHOLD OF 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION &SDR CALA2014100601307Battery Pack · dischargedSUPPORT L1 DOOR EXTERIOR EMER LIGHT INOPERATIVE ON INBOUND. TROUBLESHOOTING REVEALED FAULTY BATTERY PACK. R & R BATTERY PACK IAW AMM 33-51-06. OPERATIONS CHECKED GOOD IAW AMM 33-51 -06.SDR CALA2013091800686Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE AT AFT GALLEY. BATTERY LOCATED AT M1673 NEEDS REPLACED. R & R EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06-960-805. OPERATIONS CHECKED GOOD.SDR CALA2009121400707Extinguisher · leakingSEAL ON HALON COCKPIT FIRE EXTINGUISHER BAD. COULD HEAR HALON BEING DISCHARGED. MOVED EXTINGUISHER TO FWD CABIN. REPLACED HALON BOTTLE WITH SERVICEABLE UNIT.SDR CALA0600505Battery Pack · dischargedTHE AISLE EMERGENCY LIGHTS WERE FOUND INOPERATIVE BETWEEN SEAT ROWS 14 AND 25. THE BATTERY PACK WAS REPLACED IAW MM 33-51-06, 960-805.SDR CALA0600207Engine · failedTHE NR 1 ENGINE FLAMED OUT DURING CLIMBOUT OF DTW AT ABOUT 13K. ALL PARAMETERS SPOOLED DOWN, THE ENGINE FAIL LIGHT ILLUMINATED, AND THE OIL PRESSURE WENT TO ZERO. THE AIRCRAFT WAS DIVERTED TO CLE WHERE IT LANDED WITHOUT INCIDENT. THE NR 1 ENGINE WAS REMOVED
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