Boeing 737-824
Service difficulty reports · 9,839
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 = '737824' 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 = '737824' 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 CALA2025070106108Skin · crackedEXT PWR RECEPTACLE CUT OUT INNER DOUBLER CRACKED AT LWR END. ACCOMPLISHED REPAIR AT EXT PWR RECEPTACLE CUT OUT INNER DOUBLER REF SRM 53-10-15-2R-4.SDR CALA2025070206150Rub Strip · wornR1 DOOR LUBRICATION - R1 DOOR SLIDE RUB STRIP WORN. REMOVED AND REPLACED R1 DOOR SLIDE IAW MM 25-66-01. CORRECT INSTALLATION, SAFYETY PIN REMOVAL AND OPERATIONAL CHECK REF AMM 25-66-01SDR CALA2025063006074Skin · crackedCRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. CRACK LENGTH : 0.468". REPAIRED CRACK FOUND AT LOWER SKIN OF RIGHT HORIZONTAL STABILIZER AT STAB STA 92.70, 12" FROM REAR SPAR, I/B ROW. IN REF SRM 55-10-SDR CALA2025070106107Floorbeam · damagedSTA 947/LBL 4'-11' STA 947/RBL 5' ELONGATED HOLES AND CORROSION. ACCOMPLISHED REPAIR AT STA 947.50 FROM LBL 4 - LBL 11 IAW EC/RA 5370-01181, B737/800 SRM 53-00-51-2R-1.SDR CALA2025063006079Toilet · leakingLAV D FLUSHES CONTINUE OUSLY REF FIM 38-30 TASK 816 VERIFIED NO CLOG VERIFIED RINSE VALVE OPENS AND CLOSES SUSPECT FLUSH CONTROL ASSEMBLY NEEDS TO BE CHANGED REQUEST MEL 3802D REQUESTING MEL TOILET VALVE MANUALLY CLOSED IN ACCORDANCE WITH MEL. SLAVE IN LAV FLSDR CALA2025063006054Girt Bar · no discrepancyDOOR SLIDE AT 1R. IS STARTING TO SAG AND INTERFERING WITH ARMIN G/DISARMING INSPECTED R1 DOOR SLIDE ASSY REF AMM 25-66-01. GIRT MATERIAL SHOWING WITHIN SERVICEABLE LIMITS. GIRT BAR STOWS/ENGAGES LOCKS NORMALLY. OPERATED DOOR OPEN/CLOSE, GIRT MATERIAL NOT TOUCHSDR CALA2025063006050Skirt · out of positionSLIDE MATERIAL DOOR 1R PROTRUDING OUT BOTTOM OF SLIDE HOUSING REPOSITIONED SKIRT. REF AMM 25-66-01-401. OK FOR SERVICE. ABOVE ITEM IS RII ITEM. VERIFIED R1 DOOR SLIDE INSTALLATION PER REF AMM 25-66-01-401. L/P CLEAREDSDR CALA2025071706649Stop Fitting · worn(SUPPORT TASK) L-2 DOOR, UPPER FWD DOOR STOP FITTING IS GOUGED. EVALUATED DAMAGE AND FOUND OUT OF LIMITS IAW SRM 52-10- 90-1A-1. REMOVED AND REPLACED UPPER FWD STOP FITTING PN#147A6128 U53 IAW SRM 51-40-02 AND DWG 147A6125 REVB. RESTORED SURFACE PROTECTION ISDR CALA2025070806329Web · corrodedAFTER FURTHER EVALUATION AT THE FWD CARGO DOOR SURROUND STRUCTURE MAIN SILL WEB FOUND TO BE OUT OF LIMIT REQURIE REPLACEMENT (RE F. AAR NR 1000042333) ESFR TRANSACTION COMPLETE REMOVED AND REPLACED THE FWD CARGO DOOR LOWER MAIN SILL BTW STA. 440 TO 500 R/H IAWSDR CALA2025070106106Crease Beam · corrodedAFT WET AREA RH DOOR CREASE BEAM HAS MULTIOPLE SPOTS OF CORROSION. REMOVED CORROSION ORG THICKNESS .180 REMOVED .105 REMAINING .075 AND FOUND TO BE OUT OF LIMITS PER EC/RA 5321-01330 REV A AND SRM 53-70-15-1A-1. REMOVED CREASE BEAM PER B737-800 SRM 51-40-02. SDR CALA2025070106105Floor Support · corrodedMAIN CABIN STA 946 RBL 50 SUPPORT HAS CORROSION, WITH 100% MATERIAL LOSS ON UPPER SURFACE. REMOVED AND REPLACED INTERCOSTAL AT ST STA.949 - STA 967 RBL50 PER B737-800 SRM 51-40-02 AND BAC DWG 147A5762SDR CALA2025062705983Cover · unsecureROW 20F EMER EXIT HANDLE COVER WILL NOT REMAIN ATTACHED NOTICED HOLD IN CLIPS SPREADING OPEN SLIGHTLY ALLOWING IT TO FALL OUT. SQUEEZED CLIPS TOGETHER NOW HOLDS COVER FIRMLY.OK FOR CONTINUED USE AT THIS TIME.SDR CALA2025062705982Slide · exposedFA REPORTS DOOR 1R SLIDE MATERIAL HANGING ON FLOOR INSPECTED R1 DOOR ESCAPE SLIDE SYS, RESECURED GIRT MATERIAL INTO SLIDE COVER. GIRT MATERIAL SHOWING WITHIN SERVICEABLE LIMITS REF AMM 25-66-01-400-803. OK TO CONTINUE SERVICE.SDR CALA2025071506571Service Panel · corroded(SUPPORT TASK) AFT CARGO COMPARTMENT,WASTE SERVICE PAN HAS CORROSION.SDR CALA2025071506570Floor Support · crackedFOUND FLOOR SUPPORT INTERCOSTAL T CHORD CRACKED AT LBL 14 BETWEEN STA 380 AND 400 REF AAR N/R 9983624 ESFR INFORMATION ENTERED.SDR CALA2025063006031Insulation · contaminatedSMOKE AGAIN IN MAIN WHEEL WELL. OPERATED FLIGHT CONTROLS, FLAPS, BOTH ENGINE THRUST REVERSERS, AND PARKING BRAKE WHILE BOTH HYDRAULIC EMDPS WERE RUNNING MULTIPLE TIMES, FOUND NO ACTIVE HYDRAULIC LEAK IN THE WHEEL WELLS AT THIS TIME. CORRECTED HYDRAULIC LSDR CALA2025062706010Fire Loop · damaged1 ENG OVERHEAT ILLUM AND EXTINGUISHED FOR APPROX 5-10 SECONDS ON INITIAL CLIMB TOMC LOCKS LOG PAGE AFTER DUAL AIR RETURN WHILE PERFORMING INSPECTION WHEN REMOVING LEFT CORE HARNESS DETECTOR CERAMIC SHIELDING CRACKED AND BROKE APART ALSO FOUND RIGHT SIDE GROUNDSDR CALA2025062706002Web · corrodedAFT CARGO COMPARTMENT, SILL PLATE INNER WEB HAS EXFOLIATED CORROSION. REMOVED AND REPLACED AFT CARGO COMP SILL PLATE, LOCATED AND DRILLED, IAW B737-800 SRM 51-40-02, 51-40-05.SDR CALA2025062705986Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK AT M1694 FAILS 15 MIN CAPACITY. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1694 IAW AMM 33-52-06-960-805.PARTS USED: 99-3351-3-0015, QTY :1SDR CALA2025062605887Girt Bar · out of adjustDOOR 1R GIRT BAR NOT STOWING IN DISARM POSITION. READJUSTED DOOR 1R GIRT BAR CLIP IAW AMM 25-66-01, OPS CKS NORMAL.SDR CALA2025062605913Floor Support · corrodedAFT WET AREA R/H SIDE INNER CHORD BETWEEN STA 947 TO STA 987 HAS SEVERAL SPOTS CORRORED. REMOVED AND REPLACED R2 DOOR INNER CHORD IN REF B 737-800 SRM 51-40-02-0G-0 AND DWG# 147A8501.SDR CALA2025062605912Floor Support · corrodedFWD WET AREA R/H SIDE INNER CHORD HAS CORROSION FROM STA 312 TO STA 344. REMOVED AND REPLACED INNER CHORD AT FWD WET AREA R/H SIDE REF. SRM 51-40-02-0G-0 & DWG # 141A8310.SDR CALA2025062605909Floor Support · crackedFOUND FLOOR SUPPORT INTERCOSTSL T CHORD CRACKED AT RBL 9 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTAL CHORD AT RBL 9 BETWEEN STA 380 AND STA 400.IN REF TO SRM 51-40-02.SDR CALA2025062605908Floor Support · crackedFOUND FLOOR SUPPORT INTERCOSTAL T CHORD CRACKED AT BL 0 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FLOOR SUPPORT INTERCOASTAL T CHORD AT BL 0 BETWEEN STA 380 AND STA 400. IN REF TO SRM 51-40-02.SDR CALA2025062605884Slide · unsecureSLIDE PACK 2L LOOSE PERFORMED DOOR MOUNTED SLIDE PACK CHECK AND ADJUSTED Z FOLD ON ESCAPE SLIDE PACK IAW AMM TASK 25-66-01-400-801 STEP D).(2)E. DOOR OPEN AND CLOSES WITHOUT HURT BAR INTERFERENCESDR CALA2025062605898Floorbeam · corrodedAFT WET AREA FLOOR BEAM STA 987 RBL 43 UPPER FLANGE HAS CORROCION. ACCOMPLISHED FLOOR BEAM REPAIR AT AFT WET AREA STA 986.5 RBL 43 IN REF SRM 53-70-51-2R-6 REPAIR 6.SDR CALA2025062605878Bracket · looseDOOR 1L RIGHT SIDE GIRT BAR IS LOOSE. ADJUSTED GIRT BAR STOWAGE CLIP OK FOR SERVICE. ADJUSTED GIRT BAR STOWAGE CLIP OK FOR SERVICE.SDR CALA2025072206838Pressure Web · crackedCENTER WING BOX REAR SPAR VERTICAL PRESSURE WEB HAS CRCK INDICATION BETWEEN RBL 31.83 AND RBL 40 (LENGTH 2") RBL 40- RBL 45. 64 (LENGTH 2" ) (REF AAR NR 1000038 596)REPAIRED DAMAGE CRACK AT THE CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 31.83 ANSDR CALA2025070806328Angle · corrodedFWD WET AREA R-1 CENTER THRESHOLD SUPPORT HAS CORROSION AROUND FASTENER HOLE STA 312+ 11" RBL58 .DOT251-007 REF AAR N/R 9987991 REMOVED AND REPLACED THRESHOLD SUPPORT AT FWD WET AREA FLOOR STRUCTURE R1 DOOR RBL 58 IAW SRM 51-40-021-0G-0 ,DWG # 141A8310 , NSDR CALA2025062605921None · noneREF. LP 5268054. PER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL HFEC INSPECTIONS AT 15,0 00 FLIGHT CYCLE INTERVALS AROUND RIVET HEADS OF THE TWO OUTER RI VET ROWS OF THE INNER SKIN AND THE OUTER ROW OF THE OUTER SKIN. RESDR CALA2025062605920None · nonePER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM INTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 15,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FO R SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO THE REPAIR DOUBLER SDR CALA2025062605919Skin · damagedPER SRM 53-00-01-2R-12 SEC. 5(B), AFTER 50,000 TOTAL AIRPLANE CYCLES, PERFORM EXTERNAL DETAILED VISUAL (DET) IN SPECTIONS AT 4,000 FLIGHT CYCLE INTERVALS OF THE REPAIR AREA FOR SKIN CRACKS AT THE OUTER PERIMETER ROW OF FASTENERS COMMON TO T HE REPAIR DOUBLER ASDR CALA2025062605918Window Frame · not reportedACCOMPLISH INSPECTION REQUIREMENTS OF THE LH #3 FLIGHTDECK WINDOW FRAME E-F POST, PER PART 2 OF EC/RA 5311-03372 ON OR BEFORE THEAIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES.SDR CALA2025062605888Lamp · inoperative21F SIDEWALL LIGHT ON EMERG EXIT INOPERATIVE SIDE WALL LIGHT BY SEAT 21F INOP. EMERGENCY LIGHT OPS CHECKS GOOD. LAMP REPLACED AT SEAT ROW 21F AND CABIN SIDEWALL (WINDOW) LIGHT TEST OK. AMM 33-20-00-710-001-001.SDR CALA2025062505860Cover · dislodgedON ARMING DOOR 02L COVER FOR SLIDE POPPED OPEN. BUSTLE INTACT AND SECURE CHECKED SLIDE PACK FOR SECURITY REFE AMM 25-66-01-200-802.SDR CALA2025062505859Slide · no discrepancyDOOR 2L SLIDE PRESSURE ISSUE. PRESSURE IN RED ZONE. DOOR 2L SLIDE PRESSURE WITHIN LIMITS REF AMM 25-66-01-200-801SDR CALA2025062505858Cover · no discrepancyREMOVED R1 SLIDE PACK AND COVER REF AMM 25-66-01 RE-INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01. INCOMPLETE AMM REFERENCE RE-INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01-400-803. VERRIFIED TECH INSTALLED R1 SLIDE PACK AND COVER REF. AMM 25-66-01SDR CALA2025062305821Floor Support · corrodedAFT WET AREA INTERCOASTAL BETWEEN BS 947 - 967, RBL 50 UPPER FLANGE HAS CORROCION AROUND FASTENER HOLE. REMOVED AND REPLACED INTERCOSTAL AT AFT WET AREA BETWEEN BS 947 - 967, RBL 50 IAW SRM 51-40-02-0G-0 AND DWG 147A5760.SDR CALA2025071506572Floor Support · corrodedAFT WET AREA FLOOR PANEL SUPPORT STA 987+6 LBL 36 HAS CORROCION . REMOVED AND INSTALLED PANEL SUPPORT AT AFT WET AREA STA 987+6 LBL 36 IN REFERENCE TO B737 SRM 51-40-02-0G-0. STEP 4.B.SDR CALA2025070806330Floor Support · corrodedAFT WET AREA FLOOR PANEL SUPPPORT STA 987 +6 RBL 36 HAS CORROCION .DOT251-017 REF AAR N/R 9988006 REMOVED AND REPLACED PANEL SUPPORT AT AFT WET AREA BS 987+6 RBL 36 IN REFERENCE TO B737 SRM 51-40-02-0G-0. STEP 4.B. REMOVED AND REPLACED PANEL SUPPORT AT AFTSDR CALA2025062605917Skin · dentedDENT IN FUSELAGE SKIN FS500B PLUS 12" STRINGER 27RC/W REPAIR PER SRM 53-00-01-2R-3. REF NR 2723023 FOR WORK ACCOMPLISHED. ESFR INFORMATION ENTERED. REFERENCE NON-ROUTINE 002723023 FOR WORK DETAILS ACCOMPLISHED. DIP INITIATED TO ACCOMPLISH INSPECTIONS PER SRM 5SDR CALA2025062505851Girt Bar · no discrepancyFRONT SERVICE DOOR SLIDE MATERIAL DRAGGING VERIFIED GIRT BAR MATERIAL IS NOT MORE THAN 11 INCHES PER AMM 25-66-01-400-803 FIGURE 401, NO MAINTENANCE ACTION REQUIREDSDR CALA2025062505850Life Raft · no discrepancyINSPECT INFLATABLE LIFE RAFT INSIDE FWD CENTER OVERHEAD STOWAGE. THERE ARE REPORTS INFLATABLE LIFE RAFT MAY NOT BE INSTALLED CORRECTLY IN FWD CTR OVERHEAD COMPARTMENT. TASK 03-25-66-200-805. REPOSITIONED LIFE RAFT IN OVERHEAD BIN 7DEF REF AMM 03-25-66.SDR CALA2025062305804Battery Pack · dischargedEMERGENCY EXIT SIGNS AT BOTH AFT EMERGENCY EXIT HATCHES INOP. REPLACED BATTERY PACK ON POWER SUPPLY M1695 IAW AMM 33-51-06. OPS CHECK GOOD.SDR CALA2025062305813Floor Support · cracked(B737-53-3-0737) MAIN CABIN FWD WET AREA, MACHINED INTERCOSTAL FROM STA 344-360 BL 0 HAS 2EA POSSIBLE CRACKS IN UPPER FLANGE AT FLOOR PANEL ATTACH HOLES. REMOVED AND REPLACED MACHINED INTERCOSTAL IAW DWG NO. 141A540010 REV B AND SRM 51-40-02.SDR CALA2025062005737Battery Pack · malfunctioned3 EMERGENCY LIGHT CIRCUIT SECTIONS FAILED TO STAY ON PAST 15 MIN FOR EMERGENCY LIGHTING FUNCTIONAL CHECK AFFIILATED WITH EMER BATTERY PACKS M1694, M1670, M1673. BATTERY PACKS M1694, M1670, M1673 FAILED DURING EMERGENCY LIGHT SYSTEM OPERATIONAL CHECK 29-3350-1-SDR CALA2025062005748Battery Pack · no testEMERGENCY LIGHT BATTERY PACK AT M1673 FAILS 15 MIN. CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT M1673 IAW 737NG AMM 33-51-06-960-805. OPS CHECK GOOD. PARTS USED: 99-3351-3-0015,QTY :1SDR CALA2025062005745Elec Connector · unsecureROW 7 AISLE SEAT EMERGENCY EXIT LIGHT INOP. FOUND POOR CONNECTION UNDER MIDDLE SEAT. CLEANED AND RESEATED CONNECTION, OPS CHECK GOOD.SDR CALA2025062005744Battery Pack · no testEMERGENCY LIGHT BATTERY PACK AT M1675 FAILS 15 MIN. CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY AT M1675 IAW 737NG AMM 33-51-06-960-805. OPS CHECKS GOOD. PARTS USED: 99-3351-3-0015,QTY :1SDR CALA2025062005740Unknown · odorFA REPORTS BRAKE FLUID LIKE ODOR IN AFT LAV D ACP ENGINE RUN AND RAN PACKS , COULD NOT DUPLICATE SMELL IN CABIN. FLIGHT ATTENDANT REPORTED SMELL WENT AWAY IN FLIGHT.
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