Boeing 737-924
Service difficulty reports · 828
Newest first. General aviation reporting is voluntary.
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 aircraft_model_key = '737924' 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 aircraft_model_key = '737924' 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 CALA2024031200694Window Frame · crackedAFTER NDT ON L/H WINDOW FRAME MOD INSPECTION FOUND ONE CRACK , REPAIR TO BE PERFORMED WILL BE CONFIGURATION C OPTION 2.(REF AAR NR 100001689)SDR CALA2024031400729Regulator · failedPASSING 14500 FEET ON DEPT FELT COMPRESSOR STALL ON LEFT ENG PARAM NORMAL CREW REPORT ENGINE REMAINED AT IDLE PARA. NORMAL WITH OIL TEMP. @ 107 UNTIL RETURN TO FIELD. PERFROMED VISUAL INSP. INLET/EXHAUST NO DISCREPANCIES NOTED. PERFORMED EEC BIT #1 ENG. NO EXCSDR CALA2024031200704Warning Message · false activationREJECTED TAKEOFF AT 95 KTS DUE TO FWD ENTRY OPEN INDICATION REF LOG PAGE #7290074 FOR DOOR INDICATION SIGN OFF PERFORMED HIGH ENERGY STOP CONDITIONAL ; .INSPECTION PER AMM 05-51-07-210-801 STEP D ; NO FAULTS NOTED ; NO LEAKED NOTED.SDR CALA2024030800660Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK (M1675) INOP (REF. AAR NR 1000 01577). REMOVED AND INSTALLED NEW BATTERY PACK AT M1675 IAW B737 AMM 33- 51-06-960-805 TEST GOOD.SDR CALA2024030800659Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK (M1674) INOP (REF. AAR NR 1000 01576). REMOVED AND INSTALLED NEW POWER SUPPLY BATTERY PACK M1674 IAW B7 37 AMM 33-51-06-960-805 OP TEST GOOD.SDR CALA2024030800658Battery Pack · inoperativeEMERGENCY EXIT LIGHT BATTERY PACK (M1673) INOP (REF. AAR NR 100 001575). REMOVED AND INSTALLED NEW POWER SUPPLY BATTERY PACK IAW B737 AMM 33-51-06-960-805 P TEST GOOD.SDR CALA2024030800663Sensor · faultyCLIMBING THROUGH 13000 FELT SHARP BUMP THEN VIBE IN AIRFRAME..EGT SPIKED AND N1 ROLLBACK INCREASED NORMALLY, HOWEVER, NOTICEABLE VIBRATIONS RETURNED AND FELT THROUGH CABIN. DURING FA DEBRIEF, PAX NOTICED SPARKS/SMALL FLAMES FROM E1 EXHAUST. DEBRIEF CREW: NORMASDR CALA2024013100271Sensor · out of adjustFWD ENTRY LIGHT ON T/O. RTO SPEED WAS 125 KNOTS, WEIGHT 154,200 LBS PER CREW. REQUESTING MEL FOR FWD ENTRY DOOR INDICATION LIGHT INOP. DOOR VERIFIED TO CLOSE AND LATCH PROPERLY MEL APPLIED. VERIFIED DOOR CLOSED AND LATCHED PROPERLY PRIOR TO PUSHBACK FOR FLT. SDR CALA2023120403535Lamp · inoperativeEMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - DOOR 1L EMERGENCY ESCAPE SLIDE LIGHT INOP REPLACED DOOR 1L EMERGENCY ESCAPE SLIDE LIGHT WITH NEW IAW AMM TASK 33-51-04-960-801, OPS CHECKED OKAY IDT C/W FOR 1L ESCAPE SLIDE LIGHT REF GMM 09-10-05SDR CALA2023111703408Drain · out of positionWINDOW MADE LOUD NOISE WIND DURING TAKEOFF PER CREW IT WAS R2 WINDOW, CHECKED WINDOW AREA FOUND FWD DRAIN HOSE WAS OUT OF POSITION AND WAS PINCH BY R2 WINDOW, NO OTHER FAULTS NOTICED, OPS CHECKED WINDOW, REF AMM 56-12-11-710-803, OPEN AND CLOSED WITH NO DIFFICSDR CALA2023080402426Tire · blownPOSSIBLE TIRE BLOW OUT ON TAXI IN TO GATE # 1 AND # 2 TIRE BLOW OUT ON TAXI IN TO GATE. REMOVED AND REPLACED # 1 MAIN TIRE FOR TOWING AIRCRAFT FROM TAXI WAY,REF AMM 32-45-11 WITH WHEEL ASSY S/N OFF 4340 AND WHEEL ASSY S/ N ON 2601. PARTS USED: 60-3249-9-000SDR CALA2023010400020Light · inoperative36C EXIT PATH LIGHT NEEDS REATTACHED. SEAT36C EMERGENCY PATH LIGHT WAS REPLACED. OPS CHECK OF LIGHT IS REQUIRED. LIGHT OPS CHECKED GOOD. REF AMM 33-51-11SDR CALA2022121903421Stop Fitting · damagedPDA 3 LEFT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED & MISSING A SECTION ENTIRE LENGTH -- SEE PHOTO PHOTO ADDED PARTS ADDED REF IPC 21-51-03-06A AND IPC 21-51-03-05ASDR CALA2022120703326Disk · no testREMOVAL AND REPLACEMENT OF OPTICAL DISK IN DFDAU - WOULD NOT TEST PER OP 7. R & R DFDAU OPTICAL DISK .SDR CALA2022110903094Warning Light · false activationT/O CONFIG LIGHT AT 6K W/ GEAR AND FLAPS UP EXTINGUISHED ON APPR W/ FLAPS 1 PSEU FAULT MSG 31-51001 FOUND GROUND SPOILER INTERLOCK VALVE CABLE DISCONNECTED. INSTALLED MISSING LOCK WASHER AND REINSTALLED LOWER SLIDER PER AMM TASK 27-62-51-400-802 . ALL OPERATIOSDR CALA2022100602727Egt Indication · reads highLEFT ENGINE EGT EXCEEDED LIMITS UP TO 976 FOR ABOUT 1 MINUTE. TEMP OK AFTER LEVER REDUCE. #1 ENG SER# 875892 REMOVED AND SER# 854722 INSTALLED ROTABLE PARTS CHANGE WAS INDICATED - 1803196 ACP RII INSP REF GMM 09-25-05. PARTS UPDATE #1 ENGINE REPLACED TT 18031SDR CALA2022082402151Skin · damagedR/H HORIZONTAL STAB LOWER SKIN AT STA. 101.90 REQUIRES ACCESS HOLES TO BE CUT IN SKIN FOR #3 RIB REPAIR REF. BAM N/R 000804044 AND N/R 000844208. REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LSDR CALA2022082402150Stabilizer · crackedRIGHT HORIZONTAL STABILIZER-CRACK FOUND AT APPROXIMATE STAB STA 147.90 AND 23.5 INCHESS AFT OF THE FRONT SPAR. REF.BAM N/R 000803532 REQUIREMENTS PER SRM 55-10-01-2R REPAIR 11 TABLE 204. INSPECTION PERFORM DETAILED VISUAL INSPECTION AND EXTERNAL LFEC EVERY 9,0SDR CALA2022082202140Circuit Breaker · not seatedABORTED T/O AT 60 KNOTS DUE TO ENG 1 WOULDNT GO ABOVE 70 PERCENT. DETERMINED HPSOV CNTL C/B INCORRECTLY COLLARD . RESET C/B AND AND COMPLIED WITH CORRECT C/B FOR HPSOV IND. OK TO CONTINUE.SDR CALA2022081602094Skin · interferenceLH HORZ STAB LOWER SKIN REQUIRES CUTOUT FOR STA 92.70 VERTICAL RIB STIFFENER #3 CRACK REPAIR( N/R 000841433)AND N/R 000841447. REPAIR DOUBLER INSTALLED ISSUED DIP TO READ " INSPECTION THRESS EXTERNAL (LFEC) INSPECTION OF REPAIR DOUBLER. REPEAT INSPECTIONS REPASDR CALA2022060801466Pseu · failedLEFT FWD OVERWING AND LEFT AFT OVERWING DOOR LIGHTS IN FLIGHT PERFORMED FIM TASK 52-20 TASK 801 FROM STEP A UP TO AND INCLUDING STEP E.(2) A. FAULTS ARE CLEARED, DOOR LIGHTS ARE OUT, WAS INTERMITTANT FAULT PER FIM. A/C RESTORED TO NORMAL (ALL CIRCUIT BREASDR CALA2022060601431Skin · crackedR HORIZ. STAB LOWER SKIN HAS A CRACK INDICATED BY THE ''C'' SCAN. CRACK LOCATED AT RHORIZ. STAB STATION 147.90 AND 19 IN. FWD OF THE STAB REAR SPAR (APPROX. 1 INCH LONG)(MARKED)SDR CALA2022042101029Skin · crackedCRACK FOUND AT RIGHT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 170.34, I/B ROW, 8" FROM FRONT SPAR , CRACK LENGHT : 0.947" REF. AAR NR:9649201 REQUIREMENTS INSPECTION THRESHOLD 56,000 TOTAL FLIGHT FLIGHT CYCLES EXTERNAL LOW FREQUENCY EDDY CURRENT (LFECSDR CALA2022042101028Skin · crackedCRACK FOUND AT LEFT HORIZONTAL STABILIZER LOWER SKIN AT STAB STA 142.45 I/B ROW, 15" FROM REAR SPAR , CRACK LENGHT : 0.551". REF. AAR NR:9649199 REQUIREMENTS INSPECTION THRESHOLD 56,000 TOTAL FLIGHT FLIGHT CYCLES EXTERNAL LOW FREQUENCY EDDY CURRENT (LFEC) CYCSDR CALA2022040600890Skin · dentedUPPER FUSELAGE SKIN FROM STA 807-827 STR 5L-6L DENT #17 REQUIRES PERMANENT REPAIR (REF. AAR NR 99927801).SDR CALA2022040600884Skin · dentedDENTS #1,2, AND 3 AT STA 360-380 STR 7L TO 9L REQ ALT REPAIR (RE F. AAR NR 99927731). SKIN INSTALLED BETWEEN STA 360 AND STA 380 FROM STR6L TO STR10L ON AC N38403 IAW THE LATEST REV OF ECRA 5331-02871. UPON THE ACCUMULATION OF 50,000 TOTAL FLIGHT CYCLES PERFORSDR CALA2022021400378Skin · crackedONE CRACK FOUND AT THE LEFT-HAND HORIZONTAL STABILIZER LOWER INSPAR SKIN AT STA 166.30, 17" FROM REAR SPAR I/B OF DRAIN HOLES, CRACK LENGTH IS 0.984" . REF. AAR N/R:9649646 , CRACK LENGTH IS 0.984" . REF. AAR N/R:9649646.REQUIRES REPEAT INTERVALS (EXTERNAL):EXSDR CALA2022021400369Frame · gougedUPON REMOVAL OF EXTERNAL POWER RECEPTACLE FOUND GOUGES ON FRAME AT STA 235.8 WL181.1 BL55.5. (DOT AP56-065).(REF AAR RFD NR 99927570).SDR CALA2022010500020Skin · crackedREF FOR FLEET CYCLE...L/H HORIZONTAL STAB. LWR SKIN STA. 101.90 HAS CRACK INDICATION 14" AFT OF FRONT SPAR.(MARKED) ACCOMPLISHED SFR 1027346 -01-2R-11. 5A TABLE 204, "REPEAT INSPECTIONS 56,000 TOTAL FLIGHT FREQUENCY EDDY CURRENT INSP. PER 737 NDT PART6. 51-00-SDR CALA2022010500019Pressure Web · crackedFOUND 2EA CRACKS IN VERTICAL PRESSURE WEB AT STA 663.75 AND APPROX LBL 33. REF FLEET CYCLE N/R 9793198.CARD COMPLETE SEE WIPS AND TASKS FOR WORK PERFORMED.PER AMM 57-10-10-2R-3 REPAIR 3 ALTERNATIVE DIP 57-DIP NO TASK AND LIMITATIONS ENTERED INTO CORRECTIVE ACTSDR CALA2021111002063None · noneCRACK FOUND AT L/H VERTICAL PRESSURE WEB BETWEEN LBL 45.64 AND LBL 40.00 CRACK LENGTH 0.787IN REF AAR N/R 9635562 ACCOMPLISHED REPAIR AT VERTICAL PRESSURE WEB BETWEEN LBL 45.64 ANDLBL 40.00 AS PERR EF B737 SRM 57-10-10-2F-3 ALTERNTITVE 2 INSP REQUIRED 56,00 FLSDR CALA2021102501963Skin · noneCATERING TRUCK HIT AIRCRAFT REAR LEFT DOOR FOUND DENT ON L2 DOOR 6 IN VELOW HANDLE, 8 IN FWD AFT EDGE OF DO OR. DENT DIMS L: 2.00 IN ; W: 1.500 IN; Y: 0.150 IN. INSPECTED P ER SRM 52-10-01. OK TO DIP FOR REINSPECTION EVERY 1500 F/HRS. FOUND DENT ON L2 DOOR 6 SDR CALA2021102501960Bulkhead · crackedRIGHT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPAR VERTICAL WEB AT STA 663, RBL 42 , APROX 5" FROM CEILING, HAVE A CRACK INDICATION REF FLEETCYCLE LOG PAGE 9786602 INITIATED DIP TO PERFORM INSPECTIONS AS GIVEN IN TABLE FLIGHT CYCLE INTERVALS. INSPECTION METSDR CALA2021102501961Spar · crackedLEFT MAIN GEAR WHEEL WELL, CENTER WING BOX REAR SPA VERTICAL WEB, STA 663 LBL 34.83, AND APPROX. 4" FROM CEILING, HAVE A CRACK INDICATION REF FLEET CYCLE LP# 9786603. THIS LP IS FOR DIP AND ESFR ONLY. REPAIR DISCREPANCY REF SRM 57-10-10 2R-3 ALT 2. SEE LP# 978SDR CALA2021101801923None · warning messageALL 3 NO. 2 UPPER DU WARNING MSGS FLASHED SIMULTANEOUSLY BTWEEN 60-80KTS.NO M/C LIGHT. PER CREW, LIGHTS WERE ON AFTER ENGINE SHUT DOWN THEY STAYED ON FOR 2-4 MINUTES THEN WENT OUT. THE LIGHTS CAME BACK ON INTERMITTENTLY AND WERE FLICKERING. FURTHER DETAILS ASDR CALA2021100601790Skin · crackedLH HORIZONTAL STAB LOWER SKIN HAS CRACK AT STAB STA 138.70, 18.50" FROM T/E AND 2.00" INBOARD OF DRAIN HOLE. CRACK LENGTH 0.187". REF. EA 5510-01843 REV H. REF. AAR N/R: 9635461 CAT B REPAIR REQUIRES INSPECTIONS AT 9000 FLIGHT CYCLES PER TABLE 204.DETAILED VISSDR CALA2021090101480Battery Pack · inoperativeEMERGENCY BATTERY PACK INOP MOUNTED ON THE CEILING PANEL JUST TO THE LEFT OF THE FDR ACCESS PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED ON THE CEILING PANEL JUST TO THE LEFT OF THE FDR ACCESS PANEL REF. 737-900 AMM 33-51-06 REV 75SDR CALA2021090101479Battery Pack · inoperativeEMERGENCY BATTERY PACK INOP MOUNTED ON THE CEILING PANEL JUST TO THE RIGHT OF THE FDR ACESS PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED ON THE CEILING PANEL JUST TO THE RIGHT OF THE FDR ACCESS PANEL REF. 737-900 AMM 33-51-06 REV 75SDR CALA2021090101478Battery Pack · inoperativeEMERGENCY BATTERY PACK INOP MOUNTED JUST TO THE RIGHT OF THE FWD ENTRY LIGHT PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK MOUNTED JUST TO THE RIGHT OF THE FORWARD ENTRY LIGHT PANEL REF. 737-900 AMM 33-51-06 REV 75SDR CALA2021090101476Battery Pack · inoperativeEMERGENCY BATTERY PACK INOP LOCATED ON ROW 27CBA BEHIND DADO PANEL REMOVE AND REPLACE EMERGENCY BATTERY PACK LOCATED ON ROW 27CBA BEHIND DADO PANEL REF. 737-900 AMM 33-51-06 REV 75SDR CALA2020030700579Skin · damagedAIRCRAFT FUSELAGE SKIN DAMAGE AT STA 500G-500H BETWEEN S18L A S19L. REF EC/RA 5330-06738. SEE L/P 4633454 FOR WORK ACCOMPLI ED.DIP REQUIREMENTS, ACCOMPLISH A INSPECTION PER PART 2 ON OR BEFORE 50,000. TOTAL AIRFRAME CYCLES.PLANNNING TO CONTACT ENGI ERING AFTESDR CALA2020020300315Support Bracket · damagedON WALK AROUND FOUND RIGHT PACK EXHAUST PLENUM DEFUSER DAMAGED. MOUNT BRACKETS APPEAR TO BE BROKEN. REMOVED R/H PRIMARY AND SECONDARY HEAT EXCHANGERS PER MM 21-51-03 REPLACED RT PACK EXHAUST PLNUM DIFFUSER, REF L/ P 4286420. REINSTALLED PRIMARY AND SECONDARY HSDR CALA2020010600085Seal · damagedENGINE SHUTDOWN AT 1640Z 0 OIL QUANTITY OIL PRESSURE IN RED RANG E DEBRIEF WITH CREW CONFIRMED ENGINE SHUTDOWN WAS 1640Z AND LANDED AT 1710Z FOR A TOTAL WINDMILL TIME OF 30 MINUTES. LEAKING FROM IDG AND HYDRAULIC PUMP DRAIN TUBES ALSO FOUND OIL LEAKING FROM MOSDR CALA2019121602218Unknown · abnormalFWD CARGO PIT MAGIC CARPET DISCHARGING STATIC DURING OPERATION ACROSS FWD L/H EXTENSION ARM AND ROLLER GUIDE PANEL. INVESTIGATING AND CLEANED MOUNTING HARDWARE. UNKNOWN REASON FOR STATIC DISCHARGE. CONTACTED TECH SUPPORT. NEED MORE GROUND TIME TO TROUBLESHOOSDR CALA2019121302200Lamp · inoperativeLH ROW 21, EMERGENCY EXIT DOOR, FWD EMERGENCY THRESHOLD LIGHT, IS INOP RELAMPED, OP CHECKS GOOD REF AMM TASK 33-51-00-710-801SDR CALA2019121302198Lamp · inoperativeRH ROW 21 EMERGENCY EXIT DOOR, AFT EMERGENCY THRESHOLD LIGHT, IS INOP RELAMPED, OP CHECKS GOOD REF AMM TASK 33-51-00-710-801SDR CALA2019120902173Lamp · inoperativeLH ROW 20, EMERGENCY EXIT DOOR, FWD EMERGENCY THRESHOLD LIGHT, IS INOP RELAMPED, OP CHECKS GOOD REF AMM TASK 33-51-00-710-801SDR CALA2019111101966Unknown · odorRIGHT MAIN WHEEL WELL HAD HEAVY FUEL SMELL DURING WALKAROUND THEN NOTICED RIGHT SIDE OF VAPOR BARRIER HAS 3 CRACKS ANDONE LOOKS LIKE IT IS MORE THAN 17 INCHES. CHECKED BOTH LEFT AND RIGHT MAIN W/W AREAS FOR FUEL LEAK OR FUEL SMELL, NONE FOUND. 30-10 REQUIRES OSDR CALA2019101801776Window · crackedCOCKPIT WINDOW R 1 HAS A CRACK ON THE UPPER RT CORNER. INSPECTED IAW 737 NDT PART 6 51-00-00 PROC. 23. 56-11-41-000-801C2. REMOVED RH 4 & 5 WINDOW BLANKS FOR EASE OF MAINTENANCE. REF AMM REPEAT LOG. REF LOG PAGE 3553793 FOR REMOVAL OF WINDOW BLANKS COMPLIED WISDR CALA2019101101734Unknown · odorSMOKE IN MAIN CABIN INFLIGHT. ACP ALL TESTS AND CHECKS PER 05-51-26-800-801C, NO ODORS OR SMOKE DURING ANY OF THE ENGINE RUNS.
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