Boeing 737-752
Service difficulty reports · 2,590
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 = '737752' 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 = '737752' 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 SWAA2023112414485Floor Panel · pulledFLOOR PANEL 232RF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232RF WITH UPPER SKIN HAS AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL USING BMS 4-23 TY 2 LOT#1541638-1; RESIN FOR INSERTS BMS 5-107 LOT#1538621-1; THERMOMESDR SWAA2023112414486Floor Panel · pulledFLOOR PANEL 232SF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232SF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023112414478Floor Panel · pulledFLOOR PANEL 231AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 231AF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] PANEL REPLACED. JOB COMPSDR SWAA2023112414479Floor Panel · pulledFLOOR PANEL 231BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1 AND MEASUREMENT TABLE.SDR SWAA2023112414480Floor Panel · pulledFLOOR PANEL 231CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.;[02] VERIFIED CORRECTIVE ACTION ISDR SWAA2023112414482Floor Panel · pulledFLOOR PANEL 241UF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF ALL OF THE DAMAGE; DECIDED TO FABRICATE A NEW FLOOR PANEL USING BMS4-23 TYPE II LOT 1541638-1 AND BMS5-107 LOT 1540837-1 RESIN; CURED THE RESIN UNDER A HEAT LAMP USING THERMOMESDR SWAA2023112414483Floor Panel · pulledFLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 231XF IAW SRM 53-00-50-2R-0 AND BOEING DWG 144A5810 ID:0126.;[02] VERIFIED FABRICATION OF FLOOR PANEL 231XF PER SRM 53-00-50-2R-0 AND BOEING SDR SWAA2023112414484Floor Panel · pulledFLOOR PANEL 241YF UPPER SKIN HAS AREAS OF PULLED STRANDS. PANEL IS ACTUALLY 231YF.<[01] FLOOR PANEL 231YF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] INSPECTED AND VERIFIED. JOB COMPLETE.SDR SWAA2023112414487Floor Panel · pulledFLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FABRICATED FLOOR PANEL 241AF IAW SRM 53-00-50-2R-0;[02] VERIFIED FABRICATION OF FLOOR PANEL 241AF PER SRM 53-00-50-2R-0 AND DWG 144A5810-127.SDR SWAA2023112414488Floor Panel · pulledFLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241DF UPPER SKIN WITH PULLED STRANDS WAS REPLACED WITH A NEW FABRICATED PANEL IAW SRM 53-00-50-2R-0 AND BAC DWG 144A5810 ID:0128.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023112414491Floor Panel · pulledFLOOR PANEL 242PF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 242PF FLOOR PANEL FROM BMS4-23TY2 LOT#1541638-1; INSERTS INSTALLED USING BMS5-107 LOT#1538621-1 THEN CURED USING HEAT LAMP AND THERMOMETER ATS2192 CAL DUE DATSDR SWAA2023112414492Floor Panel · pulledFLOOR PANEL 231ZF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 231ZF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPLACED WITH A NEWLY FABRICATE FLOOR PANEL PER SRM 53-00-50-2R-0.;[02] INSPECTED AND VERIFIED. JOB COMPLETE.SDR SWAA2023112414493Floor Panel · pulledFLOOR PANEL 241BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 241BF WAS REPLACED BY FABRICATION IAW SRM 53-00-50-2R-0 AND DRAWING 144A5810 SHEET 190.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023112414481Floor Panel · pulledFLOOR PANEL 232BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FLOOR PANEL 232BF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023112714016Bulkhead · crackedR/H STA 663 VAPOR BARRIER COMPOSITE BULKHEAD IS CRACKED FROM WL 165 TO 149; RBL 46 TO 52.<[01] RIGHT HAND STATION 663 VAPOR BARRIER COMPOSITE BULKHEAD CRACK; FROM WATERLINE 165 TO 149; RBL 46 TO 52 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] FINAL INSPECTION. JOSDR SWAA2023112714017Bulkhead · crackedL/H STA 663 VAPOR BARRIER COMPOSITE BULKHEAD IS CRACKED FROM WL 160 TO 150; LBL 46 TO 52.<[01] LEFT HAND STATION 663 VAPOR BARRIER COMPOSITE BULKHEAD CRACK; FROM WATERLINE 160 TO 150; LBL 46 TO 52; WAS REPAIRED IAW SRM 51-70-04-2R-10.;[02] FINAL INSPECTION. JOSDR SWAA2023112714470Elbow · crackedELBOW FITTING CRACKED COMMON TO THE 'B' SYSTEM RETURN LINE P/N 272A4451-116<[01] INSTALLED NEW ELBOW FITTING COMMON TO THE 'B' SYSTEM RETURN LINE P/N: 272A4451-116PER AMM 20-10-51-400-804. TORQUE WRENCH USED ID: ATS2321 DUE: 06/2024.;[02] LEAK CHECK REQUIRED.;SDR SWAA2023112714474Strap · corrodedCORROSION ON STRAP AT MID PASSENGER CABIN BS703 RBL63 WL202. MARKED<[01] 'REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASK.';[02] VERIFIED CORRECTIVE ACTION #1;[03] REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASSDR SWAA2023112714475Strap · corrodedCORROSION ON STRAP AT MID PASSENGER CABIN BS713 RBL67 WL202. MARKED<[01] 'REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASK.';[02] VERIFIED CORRECTIVE ACTION #1;[03] REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASSDR SWAA2023112714476Strap · corrodedCORROSION ON STRAP AT MID PASSENGER CABIN BS719 RBL67 WL202. MARKED<[01] 'REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASK.';[02] VERIFIED CORRECTIVE ACTION #1;[03] REFER TO FAULT TTG8Q00P7PBV WHERE EA 23-153-03217 WAS ADDED AS A SUBTASSDR SWAA2023112714471Panel · crackedCRACKED PANEL BREAK AT MID CABIN BS540 RBL1 WL208.<[01] REMOVED; LOCATED; DRILLED AND INSTALLED NEW PANEL BREAK AT MID CABIN BS 540 BL 0 TO RBL 24 PER SRM 51-40-02; SRM 51-40-05 AND DWG143A0060;[02] CORRECTED MEASUREMENT TABLE;[03] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023112716589Fitting · looseRT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACH FITTING HAS LOOSE ATTACH BOLTS.<[01] REPAIRED RT WING DEFLECTION CONTROL RIB UPPER PANEL ATTACH FITTING IAW SRM 57-51-02-2R-4 REPAIR 4 AND CHECKED GOOD FLAP TO PANEL GAP IAW MM 57-50-01-820-801.SDR SWAA2023112414003Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL47 WL159.<[01] LH VAPOR BARRIER REPAIRED IN CUSTOMER FAULT TTG8Q00P70A5;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH MEASUREMENTS VERIFIED.SDR SWAA2023112414004Bulkhead · crackedCRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL50 WL152.<[01] RH VAPOR BARRIER REPAIRED IN CUSTOMER FAULT TTG8Q00P707H;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH MEASUREMENTS VERIFIED.SDR SWAA2023112414007Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] REPAIRED B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5;[02] CUSTOMER CARD COMPLETESDR SWAA2023112214006Light · inoperativeEMERGENCY EGRESS LIGHTING FROM SEAT 11DEF AFT IS NOT ILLUMINATED.<[01] PERFORMED OPS CHECK ON EMERGENCY EXIT LIGHT AT SEAT 11DEF AFT IAW AMM 33-51-01-960-801 STEP 2.C.(2) TEST WAS GOOD; EMERGENCY EXIT LIGHT WAS ILLUMINATED.;[02] VERIFIED CORRECTIVE ACTION STEPSDR SWAA2023102312441Seal · crackedR/H HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL IS CRACKED. OLD SEAL IN DAL H-RON OFFICE HGR REQ #2710. REMOVED SEAL REF MM 53-31-31 AND CDL 55=10-01. REPLACED RT HAND HORIZ. STAB. UPPER FWD. SLIDING SEAL. VERIFIED NORMAL OPERATION. REF AMM 53-31-31<BRSDR SWAA2023102012660Fastener · missingSWA - REPAIR - NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP MISSING FASTENERS - PERMANENT<[01] REPLACED MISSING FASTENER ON NG DOOR SLIDE COVER GIRT BAR RETAINER CLIP PER SRM 51-40-02SDR SWAA2023101610663Bracket · looseFWD GIRT BAR ASSEMBLY BRACKET LOOSE.<[01] INSTALLED TEMPORARY REPAIR FASTENER IAW EA M-23-125-01839.SDR SWAA2023101209911Girt Bar · looseFOWARD PROVISIONING DOOR GIRT BAR BRACKET LOOSE.<[01] SECURED GIRT BAR BRACKET PER S.I.P.SDR SWAA2023092604051Battery Pack · inoperativeR1; ROW 6DEF AND L1 EXIT SIGN E LIGHTS OUT.<[01] R/R BATTERY PACK (M1674) IAW AMM 33-51-06.SDR SWAA2023091400014Battery Pack · inoperativeOVERHEAD BIN EMERGENCY LIGHTS AT 14 AND 17 ABC ARE INOP.<[01] REMOVED AND REPLACED BATTERY PACK M1670 FOR EMERGENCY LIGHTS. IAW AMM 33-51-06. OPS CHECK GOOD.SDR SWAA2023090898247Transmitter · faultyNO LE OR TE FLAPS ON APPROACH TO BUR. ALT EXTEND FLAPS IN ONT. ALL HYDRAULIC PRESSURE NORMAL. EXTENDED FLAPS TO 15. NO HARD LANDING OR HIGH SIDE LOAD. NO HIGH ENERGY STOP. T/O WARNING OCCURRED AT TOUCHDOWN (MOMENTARILY).<[01] PERF FSCU BITE PER FIM 27-51 TASK SDR SWAA2023091395307Nut Plate · corrodedWHILE WORKING CUSTOMER CARD TTG8Q00MWAWZ FOUND CORROSION ON NUTPLATE STRAP P/N 146A8128-18 BS 794-801 RBL 19 W/L 155<[01] UPDATED STEPS 1 AND 2;[02] UPDATED STEPS 1 AND 2;[03] UPDATED STEP 2.;[04] REMOVED DAMAGE NUT PLATE STRIP AND INSTALLED NEW NUT PLATE STRISDR SWAA2023083094822Lens · missingFO SIDE EMERGENCY EXIT ROW FWD LIGHT LENS COVER MISSING<[01] INSTALLED MISSING LENS ON F/O'S OVERWING EMERGENCY PER 33-51-03SDR SWAA2023082893718Handle · looseFWD ENTRY DOOR HANDLE LOOSE<[01] FOUND FWD ENTRY HANDLE BOLTS LOOSE; SECURED IN REF TO AMM 52-11-31SDR SWAA2023090693205Panel · crackedPANEL 195CL HAS A CRACK IN THE AFT EDGE LOWER RADIUS<[01] REPAIRED CRACK DAMAGE IN THE AFT EDGE LOWER RADIUS OF PANEL 195CL IAW SRM 51-70-05-2R-6.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023090692967Sidewall Support · corrodedCORROSION ON 727D SIDEWALL SUPPORT ON FWD SIDE OF FRAME BETWEEN STR 24L AND 25L<[01] UPDATE STEP 1;[02] STEPS 2 & 3 COMPLETE.;[03] STEP 4 COMPLETE.;[04] REMOVED AND REPLACED NEW CHANNEL SIDEWALL SUPPORT AT BS 727D BETWEEN STR 19 TO STR 25 LH IAW SRM 51-40-02-0SDR SWAA2023090690303Intercostal · crackedCRACKED INTERCOSTAL AT FWD CABIN BS344+6 BL0 WL208.<[01] REMOVED CRACKED INTERCOSTAL AT FWD CABIN BS344+6 BL0 WL208 <BR>PER <BR>SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT);[02] VERIFIED ACTION 1.;[03] UPDATE STSDR SWAA2023090690302Support Angle · corrodedCORROSION ON FWD SERVICE DOOR THRESHOLD SUPPORT ANGLE BS311 RBL57 WL208.<[01] UPDATED STEP 1;[02] UPDATED STEP 2;[03] UPDATED STEP 2;[04] UPDATED MEASUREMENT TABLE;[05] CERTIFY EDIT;[06] CORRECTED ENTRY 17 ON MEASUREMENT TABLE;[07] CERTIFIED EDIT TO MEASUREMENSDR SWAA2023090690301Attach Angle · crackedCRACKED ATTACH ANGLE AT FWD PASSENGER CABIN BS294 RBL54 WL208.<[01] INSTALLED NEW ATTACH ANGLE AT FWD PASSENGER CABIN BS294 RBL54 WL208 PER SRM 51-40-05-0G-0 AND DWG 141A8310.;[02] VERIFIED CORRECTIVE ACTION #1SDR SWAA2023090690300Stub Frame · crackedFWD CABIN SERVICE DOOR SURROUND LOWER STUB FRAME CRACKED BS294 RBL55 WL209.<[01] INSTALLED NEW FSD LOWER SURROUND LOWER FRAME AT BS294 RBL55 WL209 PER SRM 51-40-05-0G-0 AND DWG 141A8370.;[02] UPDATED PART;[03] VERIFIED CORRECTIVE ACTION STEP 1. VERIFIED MEASURSDR SWAA2023091390294Web · corrodedCORROSION ON WEB AT ACB BS767+15 RBL20 WL157.<[01] UPDATED MEASUREMENTS.;[02] PARTIAL UPDATE TO STEP 1 AND 2;[03] CORRECTED STEP 3 TO INCLUDE EQUIPMENT USED.;[04] THIS WORK TO BE COMPLETED BY CUST SYSTEM ID : TTG8Q00MWC6J;[05] THIS FAULT BEING REFERENCED TO TTSDR SWAA2023091290289Strap · corrodedCORROSION ON STRAP AT ACB BS787+5; BS787+13; BS787+17. BS827+15; RBL19 WL156.<[01] ENTERED MEASUREMENTS;[02] PARTIAL ON STEPS 1-5;[03] STEP 5 PARTIAL;[04] UPDATED STEP 2.;[05] REMOVED DAMAGE; EVALUATED; FOUND PART (IN-LIMTS) THEN TREATED AND PRIMED IAW SRM 53-SDR SWAA2023090690286Attach Angle · crackedCRACKED ATTACH ANGLE AT ACB BEHIND WATER SERVICE PANEL BS918 RBL12 WL171.<[01] UPDATED STEP 1.;[02] UPDATED STEPS 1-3.;[03] UPDATED STEP 2.;[04] CORRECTION ON STEP 2 RBL TO RBL POSITION.;[05] DWG 147A7221;[06] REMOVED AND REPLACED NEW STIFFENER(ATTACH ANGLE) PSDR SWAA2023090690299Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727A - BS727D; BS747 - BS807 LBL21 WL157.<[01] VERIFIED STEPS 4;5 IN PARTIAL.;[02] VERIFIED STEPS 4;5 IN PARTIAL.;[03] VERIFIED STEP 6 IN PARTIAL.;[04] OK TO INSTALL<BR>STEP 3;[05] UPDATED STEP 3;[06] COMPLETED SSDR SWAA2023090690295Attach Angle · corrodedCORROSION ON FWD SHIELD ATTACH ANGLE BS767+1 RBL21 WL157.<[01] UPDATED STEPS 1-4; 6.;[02] UPDATED STEP 5;[03] UPDATED STEP 7;[04] UPDATED STEP 3 AND 7;[05] UPDATED STEP 3 AND 7;[06] ALL STEPS COMPLETE. REMOVED AND INSTALLED NEW REPLACEMENT ANGLE. IAW SRM 51-40SDR SWAA2023090690298Strap · corrodedCORROSION ON STRAP AROUND NUT PLATES AT ACB BS787+3 RBL20 WL151.<[01] UPDATED MEASUREMENTS;[02] PARTIAL UPDATE TO STEPS 1; 2.;[03] UPDATED STEP 2;[04] CORRECTION TO LINE 1: FIXED MEASUREMENT #19 TO MINOR;[05] STEP 1 REQ. OK TO INSTALL NEW STRAP.;[06] STEP 1; OSDR SWAA2023090690297Web · corrodedCORROSION ON WEB AT ACB BS786 RBL20 WL157.<[01] UPDATED STEP 1;[02] UPDATED MEASUREMENTS.;[03] UODATED STEP 2;[04] FIXED PART# IN MEASUREMENTS.;[05] PARTIAL UPDATE TO STEP 3;[06] PARTIAL UPDATE STEP 5;[07] UPDATED STEP 7;[08] FIXED PART NUMBER ON MEASUREMENT TSDR SWAA2023090690296Sidewall Support · corrodedCORROSION ON SIDEWALL SUPPORT AT ACB BS727D S-25L LBL25. MARKED.<[01] EVALUATED DAMAGE ON SIDEWALL SUPPORT AT ACB BS727D S-25L LBL25 FOUND TO BE OUT OF LIMITS FOR NO ALLOWABLE DAMAGE PER SRM. PART IS TO BE REPLACED ON CUSTOMER CARD NUMBER TTG8Q00N0UTL.;[02] VE
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