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 SWAA2023090690292Cargo Track · crackedCRACKED TRACK AT ACB BS767 LBL17 WL157.<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3;[03] PARTIAL ON STEP 3;[04] UPDATED STEP 3;[05] CHANGED STEP 4 TO PARTIAL;[06] SIGNED FOR PART;[07] CRACK ON AFT BAY CARGO TIEDOWN TRACK BS 767 LBL 17 WL 157; FOUND TO BE OUTSDR SWAA2023090690291Cargo Track · crackedCRACKED TRACK AT ACB BS767 RBL13 WL157.<[01] PARTIAL STEP 1-3;[02] COMPLETED STEP 2;[03] COMPLETED STEP 4-5-6 AND 8;[04] PARTIAL STEP 9-11;[05] UPDATE STEPS 9-11.;[06] REMOVED AND REPLACED CARGO TRACK FROM B/S 727 TO B/S 787 RBL 13 WL 157 IAW SRM 51-40-02; ANDSDR SWAA2023090690290Tie Down · corrodedCORROSION ON TRACK TIEDOWN AT ACB BS787+4 LBL17 WL158.<[01] UPON FURTHER INVESTIGATION THERE IS A CRACKED AT ACB TRACK AT LBL 17 WL 158 P/N: 146A7501-1. TRACK WILL BE REPAIRED BY REPLACEMENT ON CUST CARD # TTG8Q00MWAXE;[02] UPON FURTHER INVESTIGATION THERE IS SDR SWAA2023090690285Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS927+6 RBL21 WL177.<[01] UPDATED STEP 1 AND 2;[02] UPDATED STEP 3;[03] UPDATED STEP 4;[04] VERIFIED STEP 4 IN PARTIAL.;[05] UPDATED STEP 3;[06] VERIFIED STEP 3 IN PARTIAL.;[07] UPDATED STEP 5<BR><BR>THERE IS NO SRSDR SWAA2023091389744Housing · crackedAPU COMPESSOR SCROLL HOUSING HAS INTERSECTING CRACKS NEAR THE EXIT DUCT.<[01] FOUND TO BE OUT OF LIMITS PER AMM 49-11-00 PART REPLACEMENT REQUIRED PER AMM 49-11-00 STEP 2 E. (F) 1);[02] UPDATED MEASUREMENTS VERIFIED;[03] VERIFIED FOUND TO BE OUT OF LIMITS PER SDR SWAA2023090689874Web · corrodedCORROSION; AFT WET AREA; BS1016; WL208;LBL12; AROUND FASTENER HEAD<[01] VERIFIED APPLICABILITY FOR SRM 51-10-02. <BR>REMOVED CORROSION FROM WEB AT AFT WET AREA; BS1016; WL208;LBL12 IN AN AREA OF L: 3' X W: 1' PER SRM 51-10-02-0G-0. THE SRM DOESN'T HAVE ALLOWABSDR SWAA2023090689873Intercostal · crackedINTERCOSTAL CRACKED BS380-400; WL208; RBL10<[01] UPDATED STEP #1;[02] UPDATED STEP #2;[03] UPDATED STEP #3;[04] UPDATED STEP #3;[05] COMPLETED REMAINING AMT STEPS;[06] COMPLETED STEPS;[07] UPDATED PART REQUIREMENT;[08] OPENED STEP 5 FROM COMPLETE TO PARTIAL.;[SDR SWAA2023090689882Floor Panel · pulledFWD FLOOR PANEL 222DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] AREA OF PULLED STRANDS ON UPPER SKIN OF FWD FLOOR PANEL 222DF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLESDR SWAA2023090689880Floor Panel · pulledFWD FLOOR PANEL 221FF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] I UPDATED THE MEASUREMENTS TABLE.;[02] FWD FLOOR PANEL 221FF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIEDSDR SWAA2023090689879Floor Panel · pulledFWD FLOOR PANEL 221EF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221EF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETESDR SWAA2023090689883Floor Panel · pulledFWD FLOOR PANEL 221CF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] UPDATED THE MEASUREMENT TABLE.;[02] FWD FLOOR PANEL 221CF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] VERIFIED RISDR SWAA2023090689878Sidewall Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727 - BS767 RBL21 WL156.<[01] COMPLETED STEP 1.;[02] VERIFIED STEP 1 COMPLETE.;[03] PARTIAL STEP 2.;[04] COMPLETED STEP 2.;[05] COMPLETED STEP 3.;[06] UPDATED MEASUREMENT TABLE.;[07] COMPLETED STEP 4.;[08] PARTIASDR SWAA2023090689875Intercostal · crackedINTERCOSTAL CRACKED; BS380-400; WL208; LBL13<[01] UPDATED STEPS 1 & 2.;[02] UPDATED STEPS 3;4;[03] UPDATE STEP 5;[04] REMOVED AND REPLACED THE UPPER CHORD ANGLE ON THE INTERCOSTAL AT BS380-400 LBL13; WL 208 DUE TO NO REPAIR LIMITS IN THE SRM. INSTALLED IAW SRMSDR SWAA2023090689373Floor Panel · pulledAFT FLOOR PANEL 242VF UPPER SKIN HAS PULLED STRANDS<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 242VF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED JOB COMPLETE AND CURE SHEETS;[03] EDITED STEPS TO INCLUDE RII INSPECTION ITEMS.;[04] FINAL INSPESDR SWAA2023090689369Floor Panel · pulledAFT FLOOR PANEL 241ACF UPPER SKIN HAS PULLED STRANDS<[01] FLOOR PANEL 241ACF UPPER SKIN DAMAGE HAS BEEN REPAIRED IAW SRM 53-00-50-2R-1.<BR><BR>ATTACHED ALL CURE SHEETS TO THIS FAULT.;[02] FINAL INSPECTION. JOB COMPLETE.;[03] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023090689367Floor Panel · pulledAFT FLOOR PANEL 241AAF UPPER SKIN HAS PULLED STRANDS<[01] FABRICATED REPLACEMENT FLOOR PANEL 241AAF IAW SRM 53-00-50-2R-0 AND BOEING DWG: 147A5810 ID: 0008.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023090689366Floor Panel · pulledAFT FLOOR PANEL 241ZF UPPER SKIN HAS PULLED STRANDS.<[01] PULLED STRANDS ON UPPER SURFACE SKIN OF AFT PANEL 241ZF WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED RII STEPS COMPLETE;[03] VERIFIED JOB COMPLETE AND MEASUREMENT TABLESDR SWAA2023090689363Floor Panel · damagedFLOOR PANEL 232SF IS MISSING AN INSERT ALONG THE O/B EDGE. (MARKED)<[01] FOUND DAMAGE AT MISSING INSERT LOCATION ON O/B EDGE OF FLOOR PANEL 232SF; DUE TO THE EXTENT OF DAMAGE; FABRICATED NEW FLOOR PANEL 232SF FROM BMS 4-23TY2 LOT#1534174-1; INSTALLED INSERTS USDR SWAA2023090689359Sidewall Support · corrodedCORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT ANGLE AT STA: 500A+2; 500A+6; 500A+10; & 500B+18; WL 156; RBL 24.5< FOUND TO BE OUT OF LIMIT IAW SRM 53-00-53-1A-2<REMOVED AND REPLACED NEW FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0G AND DWG 143A7500 ISDR SWAA2023090689358Shield · corrodedCORROSION ON FWD CARGO BAY DOOR CUT-OUT AFT SHIELD AT STA: 500+6 & 500+10; WL 156; RBL 24.5.<[01] COMPLETED STEP 1.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] UPDATED MEASUREMENT TABLE.;[04] UPDATED STEPS 2 AND 3.;[05] EDIT TO STEP 3; NOW HAS CORRECT REFERENSDR SWAA2023090789352Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED BS 540; LBL 1; WL 207<[01] UPDATED STEPS;[02] EDIT UPDATE TO STEP #1;[03] CERTIFY STEP #1;[04] UPDATED MEASUREMENT TABLE;[05] STEPS 1;4 COMPLETE;[06] STEP 4 COMPLETE;[07] REMOVED AND REPLACED PANEL BREAK AT BS BL0 TO SDR SWAA2023090789351Panel · crackedWING CENTER SECTION BREAK PANEL IS CRACKED BS 540; RBL 1; WL 207<[01] UPDATED STEPS;[02] CERTIFIED STEPS;[03] UPDATED MEASUREMENT TABLE;[04] CERTIFIED CORRECTIVE ACTION; MEASUREMENT TABLE;[05] REMOVED AND REPLACED PANEL BREAK AT BS BL0 TO RBL25; WL 207 DUE TO SDR SWAA2023090689354Frame · cracked312 FRAME IS CRACKED IN RADIUS JUST ABOVE FWD ENTRY DOOR HEADER<[01] B.S. 312 FRAME JUST ABOVE FWD ENTRY DOOR HEADER WAS REPAIRED PER M-22-153-012 (TTG8Q00MV151) IN SUBTASK ATTACHED.;[02] VERIFIED CORRECTIVE ACTIONS 1.SDR SWAA2023090689355Threshold · corrodedFWD CARGO DOOR SUB THRESHOLD HAS CORROSION AT BS 440+11 - 480+3 RBL 28 WL 157<[01] UPDATED STEP 1 AND 2;[02] VERIFIED STEP 1 & 2 COMPLETE.;[03] UPDATED STEP 3;[04] MEASUREMENT TABLE INCORRECT. SEE STEP 6;[05] UPDATED MEASUREMENTS TABLE;[06] UPDATED STEP 5 AND SDR SWAA2023090688991Floorbeam · corrodedFLOOR BEAM AT BS 986 LBL 25-45 HAS MULTIPLE AREAS OF CORROSION< REMOVED CORROSION FROM FLOOR BEAM AT BS 986.5 WL 208 BLEND OUT AREAS MEASURE: LBL 44: L: 2.5' W: 1.2' REMAINING THICKNESS: .104' ORIGINAL THICKNESS .150'; FOUND FLOOR BEAM TO BE OUT LIMITS PER SRMSDR SWAA2023090688992Floorbeam · corrodedFLOOR BEAM AT BS 986 RBL 25-45 HAS MULTIPLE AREAS OF CORROSION<[01] VERIFIED APPLICABILITY FOR BOEING 737-700 SRM 53-70-51-1A-1.;[02] CERTIFIED STEP 2;[03] STEP 3 COMPLETE.;[04] VERIFIED STEP 3 COMPLETE.;[05] VERIFIED STEP 3 COMPLETE AND MEASUREMENT TABLESDR SWAA2023081688708Girt Bar · out of adjustFWD SERVICE DOOR GIRT BAR HANGER LOOSE<[01] RESECURED FWD SVC DOOR GIRT BAR HANGAR IAW SRM 51-40-02SDR SWAA2023090688541Scuff Plate · crackedFWD SERVICE DOOR SCUFF PLATE CRACKED (MARKED)<[01] WELDED CRACK ON RADIUS OF FWD SERVICE DOOR SCUFF PLATE USING AMS 4954 .045' FILLER ROD LOT NUMBER M798431 PER SRM 53-10-15-2R-2 PARAGRAPH 4.B. (3) AND (4). REPAIR WELD STILL REQUIRES A DYE PENETRANT INSPECTIONSDR SWAA2023090687586Bulkhead · crackedCRACKED LOWER R/H COMPOSITE BULKHEAD AT BS663 RBL32 WL151.<[01] EDITED STEPS 2 AND 4.;[02] CRACKED LOWER R/H VAPOR BARRIER BS633 RBL32 WL151 WAS REPAIRED IAW SRM 51-70-04-2R-10.;[03] UPDATED MEASUREMENTS;[04] VERIFIED CORRECTIVE ACTIONS 1-3<BR><BR>VERIFIED MEASDR SWAA2023090687585Bulkhead · crackedCRACKED LOWER L/H COMPOSITE BULKHEAD AT BS663 LBL40 WL160.<[01] PART/MATERIAL IDENTIFIED PER SRM 57-10-10-0I-2 FIGURE 2 TABLE 2 ITEM 4.<BR>CUMULATIVE CRACK LENGTHS 30' EXCEED THE ALLOWABLE LIMITS AS GIVEN IN SRM 57-10-10-1A-2 PARA 4. D. (1).<BR>REPAIR TO BE PESDR SWAA2023081487359Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS ARE INOP<[01] R&R EMERGENCY LIGHT BATTERY PACKS LOCATED ABOVE FWD ENTRY LIGHT PER AMM 33-51-06SDR SWAA2023082484391Support Bracket · crackedCRACK SUPPORT BRACKET AT FWD GALLEY AREA LOC BS 294.5 AND LBL 12 2023-461545<[01] REPLACED SUPPORT BRACKET LOCATED BS 294.5 AND LBL 12 AT FWD GALLEY AREA IAW SRM B737-700 51-40-02 ; SRM B737-700 51-10-02 PARAGRAPH 9 AND DRAWING # 251A2204 SHEET 1 REV. - SEE INSDR SWAA2023082484071Angle · crackedCRACK INNER CHORD BS 294.5 AND RBL56 WL208.1 AT FWD GALLEY AREA 2023-461541<[01] REPLACED INNER CHORD LOCATED BS 268.25 TO BS 360 AT LEVEL STR 17R AND RBL56 WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A8310; SHEET 25 SEE INDIVIDUAL SIGNS-OFSDR SWAA2023073183712Cover · missingAFT SERVICE DOOR EXIT COVER MISSING<[01] REPLACED MISSING EXIT COVER AFT SERVICE DOOR PER SIP; ALL CHECKS GOOD.SDR SWAA2023082483489Support Bracket · crackedCRACK TRAILING EDGE ON SUPPORT BRACKET IRSS 143 AT RT WING 2023-461515<[01] REPLACED SUPPORT BRACKET ON TRAILING EDGE IRSS 143 AT RT WING IAW B737-700 SRM 51-40-02.;[02] TASK CARD COMPLETE.SDR SWAA2023083094946Bracket · corrodedCORROSION TRAILING EDGE BRACKET ON BONDING JUMPER AT LT WING (2 EA) 2023-461484<[01] REPLACED TRAILING EDGE BRACKET ON BONDING JUMPER AT LT WING IAW B737-700 AMM 28-22-41-000-801 STEP 2.H(8) UP TO 2.H(12) AND B737-700 AMM 28-22-41-400-801 STEP 3.H(17) UP TO 3.SDR SWAA2023082983198Panel · corrodedCORROSION ON WEB FUEL INDICATORS LOCATED OFSS 275 AT RT WING 2023-461500<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE DATE: 31-JAN-24.;[02] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 60009161631; DUE SDR SWAA2023082483190Angle · crackedCRACK ANGLE TRAILING EDGE ON ACCESS PANEL 551FB AT LT WING 2023-461472<[01] MEASURE OF CRAK L: 0.168? TOOL USED DIGITAL CALIPER P/N: 500-196-30 S/N: A26231842 DUE DATE: 21/FEB/24; NOT FOUND ALLOWABLE DAMAGE IN B737-700 SRM 57-51-01-1A-1 AND MUST REPLACED; AND SDR SWAA2023082482970Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED STA294.5 AND RBL55; WL208.1 AT FWD GALLEY AREA 2023-461458<[01] REPLACED ANGLE AND FASTENERS FLOOR STRUCTURE LOCATED STA294.5 AND RBL55; WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G Ï¿½TEM 9 AND DSDR SWAA2023082482978Angle · crackedCRACK ANGLE FLOOR STRUCTURE LOCATED BETWEEN STA927 TO STA947.5 AND BL 0; WL208.1 AT AFT GALLEY AREA 2023-461467<[01] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 25-JAN-24; TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N:SDR SWAA2023082482963Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA 312 TO STA 328 AND RBL 31; WL208.1 FWD GALLEY AND LAV 2023-461451<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA 312 TO STA 328 AND RBL 31; WL208.1 FWD GALLEY AND LAV IAW B737-700SDR SWAA2023082482966Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA344 TO STA360 AND BL0; WL208.1 FWD GALLEY AND LAV 2023-461446<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA344 TO STA360 AND BL0; WL208.1 FWD GALLEY AREA IAW SRM B737-700 51-40-02SDR SWAA2023082482967Intercostal · corrodedCORROSION WEB INTERCOSTAL LOCATED BETWEEN STA 294.5 TO STA 312 AND LBL 11; WL208.1 AT FWD GALLEY AREA 2023-461453<[01] REPLACED NEW WEB INTERCOSTAL ; FASTENERS AND CHANNEL FLOOR ; ANGLES (2E/A) LOCATED BETWEEN STA 294.5 TO STA 312 AND LBL 11; WL208.1 AT FWD GASDR SWAA2023082483197Plate · crackedCRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS240 AT LT WING 2023-461487<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS240 AT LT WING IAW B737-700 51-40-02 AND 51-10-02 PARAGRAPH 9 SEE INDIVIDUAL SIGN OFF BELOW.;[02] TASK CARD COMPLETE. <BR><BR><SDR SWAA2023083094945Bracket · corrodedCORROSION TRAILING EDGE SUPPORT BRACKET BONDING JUMPER AT RT WING 2023-461428<[01] REPLACED SUPPORT BRACKET BONDING JUMPER AT RT WING IAW B737-700 AMM 28-22-41-000-801 STEP 2.H(8) UP TO 2.H(12) AND B737-700 AMM 28-22-41-400-801 STEP 3.H(17) UP TO 3.H(22)(A);(BSDR SWAA2023082982675Bracket · crackedCRACK BRACKET ON BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY 2023-461427 CORRECTED LOCATION: BS 540 AT LEVEL LBL 6<[01] REPLACED BRACKET ON BS 540 AT LEVEL RBL 6 AT AIR CONDITIONING BAY IAW B737-700 SRM 51-40-02 AND 51-10-02;[02] STEP CORRECTED <BR>REPLACED SDR SWAA2023082482676Intercostal · crackedCRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 WL208.1 FWD GALLEY AND LAV 2023-461426<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA 312 TO STA 328 AND RBL 31; WL208.1 FWD GALLEY AND LAV NEW IAW B737-700SDR SWAA2023082482673Bracket · brokenBROKEN BRACKET KEEL BEAM ON BS 580 AT LEVEL RBL 4 AT LOWER FUSELAGE 2023-461424<[01] REPLACED BRACKET KEEL BEAM ON BS 580 AT LEVEL RBL 4 AT LOWER FUSELAGE IAW. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02.;[02] REPLACED BRACKET KEEL BEAM ON BS 580 AT LEVEL RBSDR SWAA2023082482674Bracket · brokenBROKEN BRACKET KEEL BEAM ON BS 580 AT LEVEL LBL 4 AT LOWER FUSELAGE 2023-461425<[01] REPLACED BRACKET ON KEEL BEAM LOCATED BS 580 AT LEVEL LBL 4 AT LOWER FUSELAGE IAW. B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02;[02] REPLACED BRACKET ON KEEL BEAM LOCATED BS SDR SWAA2023082482672Angle · crackedCRACK INNER CHORD LOCATED STA303.9 AND LBL54; WL208.1 AT FWD GALLEY AREA 2023-461423<[01] REPLACED INNER CHORD LOCATED BETWEEN BSTA277 TO BSTA380 AND LBL54; WL208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 PARAGRAPH 9 AND DWG 141A8110; REV: A
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