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 SWAA2023082482671Floorbeam · crackedCRACK FLOOR BEAM LOCATED STA294.5 AND RBL53; WL208.1 AT FWD GALLEY AREA 2023-461421<[01] TOOL USED EDDY CURRENT EQUIPMENT PN. NORTEC 600D; SN 220272712; DUE DATE 17-DEC-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 142811020; DUE DATE: SDR SWAA2023082382523Angle · crackedCRACK ANGLE LOCATED AT LEVEL BS1016 AT VERTICAL STABILIZER 2023-461410<[01] REPLACED ANGLE AND FASTENERS LOC BS 1016 AT VERTICAL STABILIZER IAW B737-700 SRM 51-40-02;SRM 51-10-02 AND DWG 176A3100 SHEET 4 REV.-. SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STESDR SWAA2023082482253Tie Clip · crackedCRACK TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN 2023-461351<[01] REPLACED TIE CLIP LOCATED BS277 AND STR10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110 SHEET 18 REV -. <BR>SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] TASK CARD COMPLETED <BSDR SWAA2023082482248Support · corrodedCORROSION SUPPORT ZEE LOCATED BTW BS 727E PLUS 7 INCHES TO BS 807 LBL 21 WL 156 AFT CARGO COMPARTMENT 2023-461338<[01] REPLACED SUPPORT ZEE LOCATED BTW BS727E +7' TO BS847 LBL 21 WL 156 AFT CARGO COMPARTMENT IAW SRM B737-700 SRM 53-00-53-2R-6 REPAIR 6 FIG. 203SDR SWAA2023082482250Support · corrodedCORROSION SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT 2023-461341<[01] REPLACED SUPPORT ZEE LOCATED BETWEEN BS727D TO BS767 RBL21 AND WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 146A7500 SHEET 85 REVSDR SWAA2023082482073Support Bracket · crackedCRACK TRAILING EDGE ON SUPPORT BRACKET LOCATED ORSS 261 AT RT WING 2023-461336<[01] REPLACED SUPPORT BRACKET LOCATED ORSS 261 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9;[02] COMPLETEDSDR SWAA2023082482072Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2023-461334<[01] REPLACED SUPPORT ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B373-700 SRM SRM 51-10-02. PARAGRAPH 9;[02] CORRECTIVE ACTION CERTIFIED;[03] STEP 1 CSDR SWAA2023082482068Support Angle · crackedCRACK ON SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING 2023-461335<[01] REPLACED SUPPORT ANGLE LOCATED INBOARD AUXILIARY TRACK OF SLAT 1 AT LT WING IAW B373-700 SRM SRM 51-10-02. PARAGRAPH 9;[02] STEP 1 CORRECTED <BR>REPLACED SUPPORT ANGLESDR SWAA2023082482249Frame · crackedCRACK ON FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA 2023-461340<[01] TRIMMING OUT FRAME LOCATED BS 312 AT LEVEL STR 5L AT FWD GALLEY AREA IAW EA M-22-153-01244;[02] CERTIFIED WORK PERFORMEDSDR SWAA2023081782231Panel · crackedRT WING L/E PANEL 621PB IS CRACKED AT CORNER (MARKED) PANEL IS ACTUALLY 621HB.<[01] PANEL 621HB WAS REPAIRED IAW SRM 51-70-05-2R-10 AND SRM 51-70-14-2R-3.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023081782232Panel · crackedRT WING L/E PANEL 621PB HAS CRACK AT CORNER (MARKED)<[01] PANEL 621PB WAS REPAIRED IAW SRM 51-70-05-2R-6 AND SRM 51-70-14-2R-3.;[02] VERIFIED CORRECTIVE ACTION 1SDR SWAA2023082481750Support Angle · crackedCRACK SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN 2023-461289<[01] REPLACED SUPPORT ANGLE LOCATED BS867 AND BETWEEN STR2R TO STR3R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 146A7901 SHEET 66 REV.A;[02] TASK CARD COMPLETSDR SWAA2023082481747Intercostal · corrodedCORROSION WEB - INTERCOSTAL LOCATED BETWEEN BS492 TO BS500A AND STR26R FWD CARGO COMPARTMENT 2023-461235<[01] REPLACED WEB - INTERCOSTAL LOCATED BETWEEN BS492 TO BS500A AND STR26R FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 143A0080; SHEET 33; REV SDR SWAA2023082481406Access Panel · delaminatedDELAMINATED ACCESS PANEL 194BR 2023-461071<[01] TOOL USED CALIPER P/N: 500-197-30; S/N: A21303945; DUE DATE: 25-SEP-23.;[02] TOOL USED CALIPER P/N: 500-197-30; S/N: A21303945; DUE DATE: 07-NOV-23.;[03] TOOL USED SCALE P/N: CR5200; S/N: 8343110772; DUE DATE: 20SDR SWAA2023082481596Vapor Barrier · crackedCUSTOMER REQUEST - CRACK ON VAPOR BARRIER LOCATED BS 663 LH SIDE AT MAIN WHEEL WELL COMPARTMENT 2023-461131<[01] TOOL USED CALIPER P/N: 500-464; S/N B17030933; DUE DATE: 17-OCT-23.;[02] TOOL USED HOT BONDER P/N HCS9200B-AV; S/N 18196127; DUE DATE: 22-JAN-24.;[SDR SWAA2023082481403Skin · crackedCRACK INDICATION ON EXTERNAL SKIN LOWER PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.900 INCH. APPROX. AT RT HORIZONTAL STABILIZER 2023-461062<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500XSDR SWAA2023082481599Access Panel · crackedCRACK ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2023-461152<[01] TOOL USED: HOT BONDER P/N: HCS9200B-AV; S/N: 18196127; DUE DATE: 22-JAN-24.;[02] TOOL USED: SCALE P/N CR5200 S/N 8343110809 DUE DATE 21/FEB/24.;[03] TOOL USED: HOT BONDER HCS9200B-AV S/N: 18175SDR SWAA2023082480945Skin · crackedCRACK ON FLEXI SKIN LOCATED LEADING EDGE ON SLAT 6 AT RT WING 2023-460947<[01] TOOL USED; CALIPER PN: 500-464; SN: B17030933; DUE DATE: 17/OCT/23.;[02] REPAIRED FLEX SKIN ON SLAT 6 AT RT WING IAW EA 23-157-02428. SEE INDIVIDUAL SIGNOFFS BELOW.;[03] TASK COMPLESDR SWAA2023082480950Angle · crackedCRACK ON ANGLE LOCATED AUXILIARY TRACK SLAT 7 AT RT WING 2023-460942<[01] REPLACED ANGLE AND FASTENERS LOCATED AUXILIARY TRACK SLAT 7 AT RT WING IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9.SEE INDIVIDUAL SIGN OFF BELOW;[02] REPLACED ANGLE AND FASTENERS LSDR SWAA2023082481205Door · crackedCUSTOMER REQUEST CRACK ON INTERNAL AREA OF CENTER MLG DOOR LT SIDE 2023-460976<[01] TOOL USED: ET EQUIPMENT P/N: NORTEC 500D; S/N: N500X12101V022233; DUE DATE: 30-AUG-23;[02] PERFORMED PERMANENT REPAIR ON INTERNAL SURFACE OF CENTER MLG DOOR LT SIDE IAW B737-70SDR SWAA2023082380947Support Bracket · crackedCRACK TRAILING EDGE ON SUPPORT BRACKET LOCATED ORSS261 AT LT WING 2023-460937<[01] REPLACED SUPPORT BRACKET (FITTING) LOCATED TRAILING EDGE ORSS261 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG 115A2930; SHEET 7; REV -. SEE INDIVIDUAL SIGNS-OFF BELOW.;[02] CERTSDR SWAA2023081781201Intercostal · crackedCRACKED INTERCOSTAL AT AFT CABIN BS927+14 BL0 WL208. MARKED.<[01] CLEANED 'MARKED' AREA IAW AMM 20-10-34-110-802; REQUESTING NDI TO VERIFY ENDS ON CRACK;[02] HFEC INSPECTED SUSPECTED CRACK AREA IAW 737 NDTM PART 6; 51-00-00 PROCEDURE 23.<BR>.3' CRACK NOTED WITSDR SWAA2023081780893Scuff Plate · crackedAFT CARGO BAY FWD CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY FWD CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUISDR SWAA2023081780892Scuff Plate · crackedAFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED<[01] WELDED CRACK ON AFT CARGO BAY AFT CORNER SCUFF PLATE USING ER4043 FILLER ROD LOT NUMBER 1131216 PER SRM 53-60-15-2R-1 PARAGRAPH 4.B.(2) AND (4). REPAIR AREA STILL REQUIRES A DYE PENETRANT INSPECTION.<BR>EQUISDR SWAA2023081780909Web · corrodedCORROSION ON SUBTHRESHOLD WEB AT ACB BS807 - BS827 RBL26 WL159.<[01] VERIFIED SRM 53-60-15-0I-1 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE.;[02] STEPS 1 AND 2 FOUND TO BE OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 1 COMPLETE AND UPDATED SDR SWAA2023081780910Shield · corrodedCORROSION ON FWD SHIELD AT ACB BS767 - BS787 RBL21 WL157.<[01] VERIFIED APPLICABILITY FOR ALLOWABLE DAMAGE LIMITS ON FWD SHIELD AT ACB BS 767 TO BS 787 RBL21 WL 157 IAW SRM 51-10-02;[02] NO ALLOWABLE DAMAGE LIMITS IN SRM REPAIR BY REPACEMENT IAW SRM 51-10-02-0SDR SWAA2023081780901Support · corrodedCORROSION ON FLOOR TO SIDEWALL SUPPORT AT ACB BS727E - BS767 RBL21 WL157.<[01] VERIFIED SRM 53-60-53-0I-2 FOR IDENTIFICATION AND SRM 53-00-53-1A-2 FOR ALLOWABLE DAMAGE.;[02] STEPS 1 AND 2 FOUND TO BE OUT OF LIMITS.;[03] VERIFIED CORRECTIVE ACTION 1 AND UPDATEDSDR SWAA2023081780510Floor Panel · pulledAFT FLOOR PANEL 242RF UPPER SKIN HAS PULLED STRANDS.<[01] FABRICATED NEW FLOOR PANEL 242RF; INSTALLED INSERTS WITH BMS 5-107 LOT#AK2KP8383K-1; CURED WITH THERMOMETER ID:ATS2208 CAL DUE 10/2023 PER SRM 51-40-02-0G-0 AS SHOWN IN SWA ACO 8722-25 STEP 42 AND AIPC SDR SWAA2023081780517Floor Panel · pulledFWD FLOOR PANEL 221BF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] FWD FLOOR PANEL 221BF WITH UPPER SKIN THAT HAS 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] JOB COMPLETSDR SWAA2023081780522Floor Panel · pulledFWD FLOOR PANEL 221DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] COMPLETED STEPS 1; 2; 3 AND 5.;[02] FWD FLOOR PANEL 221DF UPPER SKIN WITH AREAS OF PULLED STRANDS WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[03] INSPECTED ASDR SWAA2023081780888Gusset · crackedFWD CARGO BAY - CRACK ON GOOSED BS 500D S-19L (MARKED)<[01] REMOVED AND REPLACED AT FORWARD CARGO BAY LOCATED BS.500D STR19L IAW SRM 51-40-02 DWG#143A7902 REV: E.;[02] VERIFIED TASK CARD COMPLETE.SDR SWAA2023081780889Stringer · corrodedAFT OF FORWARD CARGO COMPARTMENT - CORROSION ON STRINGER 23R BS 540 (MARKED)<[01] EVALUATED CORROSION DAMAGE ON STRINGER 23R BS 540; L= 2' W= 1' ORIGINAL THICKNESS 0.036' MAT LOSS MORE THAN 80%; FOUND TO BE OUT OF LIMIT IAW SRM 53-00-03-1A-1;;[02] PERFORMED CUSDR SWAA2023081780724Panel · crackedCRACK ON BREAK PANEL AT FASTENER BS 540; LBL 1; WL 207<[01] REMOVED BREAK PANEL ON BS 540; LBL 1; WL 207 FOUND PART HAS NOT SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACENENT IAW SRM 51-10-02 STEP 9;[02] LOCATED AND DRILLED NEW BREAK PANEL ON BS 540; LBL 1; WSDR SWAA2023081780322Attach Angle · crackedB.S. 663 VAPOR BARRIER UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 8 W.L. 160.<[01] UPDATE STEP 2.;[02] INSTALLED NEW UPPER ATTACH ANGLE BS 663 VAPOR BARRIER PER SRM 51-40-02 AND DWG 111A1322;[03] UPDATE STEP 3;[04] UPDATED STEP 4;[05] COMPLETED STEP 4.;[06] ALL WSDR SWAA2023081780323Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 165.<[01] REMOVED AND REPLACED UPPER ATTACH ANGLE BS 663 RBL 6 TO RBL 65 ON N/R # TTG8Q00MAZFH JOB COMPLETED;[02] UPDATE ITEM 1;[03] VERIFIED CORRECTIVE ACTION STEPS 1 AND 2. VESDR SWAA2023081780320Attach Angle · crackedB.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT L.B.L. 45; W.L. 165.<[01] VERIFIED COMPLETION STEP 6 ITEM 1;[02] REMOVED AND REPLACED B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE AT L.B.L. 45; W.L. 165 IAW SRM 51-40-02-0G-0; SRM 51-4SDR SWAA2023081780500Floor Panel · pulledAFT CABIN FLOOR PANEL 241AEF HAS A PULLED THROUGH INSERT<[01] AFT CABIN FLOOR PANEL 241AEF WITH A PULLED THROUGH INSERT WAS REPAIRED PER SRM 53-00-50-2R-1. ATTACHED CURE SHEETS TO THIS FAULT RECORD.;[02] FINAL INSPECTION. JOB COMPLETE.SDR SWAA2023081780052Doubler · crackedLH HORIZONTAL STABILIZER LOWER SKIN - .8' CRACK 18' FROM FWD EDGE ON RIB 193.90<[01] VERIFIED APPLICABILITY OF SRM 55-10-01-2R-11 REPAIR 11.;[02] REMOVED THE DAMAGE AREA OF THE SKIN IAW SRM 55-10-01-2R-11 4. (2) FIG 204/REPAIR 11 DETAIL B AND SRM 51-10-02.<BR>SDR SWAA2023081779431Battery Pack · inoperativeREMOVE AND REPLACE EMERGENCY EXIT LIGHT BATTERIES PRIOR TO DELIVERY<[01] PARTIAL WORK FOR STEPS 1 THRU 8.;[02] CERTIFIED ACTION 1.;[03] REMOVED AND REPLACED ALL EMERGENCY EXIT LIGHT BATTERY PACKS AND PERFORMED GOOD INSTALLATION TEST IAW AMM 33-51-06-960-805.;[SDR SWAA2023081779639Panel · pulledR/W L/E PANEL 621SB HAS PULLED FASTENER HOLES (MARKED)<[01] EDITED STEP 9.;[02] RIGHT-WING LEADING-EDGE PANEL 621SB WITH PULLED FASTENER HOLES WAS REPAIRED IAW SRM 51-70-04-2R-9.;[03] VERIFIED CORRECTIVE ACTION #2SDR SWAA2023070675470Flashlight · inoperativeAFT GALLEY FLASHLIGHT INOP. R&R FLASHLIGHT ASSEMBLY IN AFT GALLEY. REF AMM 25-64-00.SDR SWAA2023062772040Slide · low pressureFWD ENTRY ESCAPE SLIDE PRESSURE OUT OF GREEN BAND<[01] R&RD L1 DOOR ESCAPE SLIDE IAW MT 725-61-06SDR SWAA2023070360681Angle · crackedCRACK ANGLE WING TO BODY FAIRING AT LEVEL BS 500D AND STR 19L AT LOWER FUSELAGE 2023-360395<[01] REPLACED ANGLE WING TO BODY FAIRING AT LEVEL BS 500D AND STR 19L AT LOWER FUSELAGE IAW B737-700 SRM-51-40-02 AND DWG-116A3110 REV: B SEE INDIVIDUAL SIGN-OFF BELOW;SDR SWAA2023062060905Panel · crackedRT WING UPPER SURFACE PANEL #651ET HAS APPROX 14 INCH CRACK<[01] REMOVED AND REPLACED PANEL PER AMM 57-50-01;[02] C/W INSPECTIONSDR SWAA2023062958772Angle · crackedCRACK ANGLE LOC BS 727B UPPER AREA LBL 51 AT AFT CARGO COMPARTMENT 2023-360385<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE LOCATED ON BS 727A MORE 13.5? TO BS 727B MORE 5? LBL 51 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-70-11-2R-0; REPAIR GENERAL. SSDR SWAA2023062958773Angle · crackedCRACK ANGLE LOC BS 727E UPPER AREA LBL 51 AT AFT CARGO COMPARTMENT 2023-360386<[01] PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE LOCATED ON BS 727A MORE 13.5? TO BS 727B MORE 5? LBL 51 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-70-11-2R-0; REPAIR GENERAL. ASDR SWAA2023061558553Girt Bar · looseGIRT BAR ON AFT GALLEY(CAPT SIDE ) KEEP FALLING OUT OF ITS HOLDER<[01] PROPERLY INSTALLED GIRT BAR ON AFT GALLEY CAPT-SIDE DOOR IAW AMM 25-66-01SDR SWAA2023070357844Fitting · wornWEAR ON FLOOR PANEL HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA 2023-360162<[01] REPLACED FLOOR PANEL HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801;[02] REPLACED FLOOR PANEL HARDWARE GIRT BAR FITTING AT FWD GALLEY AREA I.A.WSDR SWAA2023070357845Fitting · wornWEAR ON FLOOR PANEL HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA 2023-360163<[01] REPLACED ON FLOOR PANEL HARDWARE GIRT BAR FITTING AT AFT GALLEY AREA I.A.W B737-700 AMM 25-66-02-400-801;[02] CORRECTED STEP 1 REPLACED ON FLOOR PANEL HARDWARE GIRT BAR FITTING ASDR SWAA2023070355652Panel · crackedCRACK ACCESS PANEL 661CB HOLES AT RT WING 2023-360324<[01] TOOL USED: CALIPER: P/N:500-464 S/N:B17030933 DUE DATE:17-OCT-23;[02] TOOL USED: HOT BONDER PN: HCS9200B-AV; SN: 18185733; DUE DATE: 23-JAN-24.;[03] TOOL USED SCALE P/N: SPX621 S/N: 8340225484 DUE DATE
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