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 SWAA2023051930224Mount · brokenR-1 DOOR AFT DOOR SLIDE MOUNT BRACKET SHOCK MOUNT BROKEN<[01] REMOVED AND REPLACED R-1 DOOR AFT DOOR SLIDE MOUNT BRACKET SHOCKMOUNT PER B737-700 SRM 51-40-02-0G-0;[02] VERIFIED SHOCKMOUNT REPLACEMENT.<BR>OK TO INSTALL PLATE.;[03] INSTALLED R-1 DOOR AFT DOOR SLSDR SWAA2023052229760Channel · corrodedFWD CARGO RIGHT 'Z' CHANNEL AT 500B-500D HAS LIGHT CORROSION AROUND NUT PLATES<[01] OK TO APPLY ALODINE AND PRIMER AND TOP COAT.;[02] TREATED; PRIMED AND TOP COAT APPLIED AT FWD CARGO COMP. FIGHT 'Z' CHANNEL FR0M STA 500B THRU STA 500D PER B737-700 SRM 51-20-0SDR SWAA2023052229353Channel · corrodedCORROSION FOUND AFT CARGO RH 'Z' CHANNEL FROM STA 727 TO STA 767 RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO RH 'Z' CHANNEL FROM STA 727 TO STA 767 RBL 21 WL 155.5 AS PER SRM 51-10-02-0G-0. ORIGINAL TICKNESS 0.040'; MATSDR SWAA2023052229354Shield · corrodedCORROSION FOUND AFT CARGO DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION AT AFT CARGO DOOR CUTOUT FWD SHIELD FROM STA 767 TO STA 787 RBL 21 WL 155.5 AS PER SRM 51-10-2-0G-0.<BR>PERFORMED BSDR SWAA2023052229358Strap · corrodedCORROSION FOUND AFT CARGO FLOOR STRAP AT STA 767 + 5 FROM LBL 6 TO RBL 21 WL 155.5 HAS MULTIPLE SPOTS OF CORROSION.<[01] REMOVED CORROSION FROM AFT CARGO FLOOR STRAP AND FOUND TO BE OUT OF LIMITS PER B737 SRM 53-00-53-1A-2 TOOL B/C: 172991 DUE DATE: 25-JUL-23;SDR SWAA2023052228869Angle · crackedPASSENGER CABIN FLOOR STRUCTURE AT STA 695 BL 0 WL 204 ANGLE SUPPORT CRACK.<[01] ACCOMPLISHED HEAT TREAT ON ANGLE BY AAR FORM OP 84 AND SERVICEABLE TAG #407960;[02] OK TO APPLY ALODINE AND PRIMER.;[03] REPLACED FABRICATED BRACKET AT CABIN FLOOR STRUCTURE STA 6SDR SWAA2023052228868Attach Angle · crackedAFT CABIN INERCOSTAL BETWEEN STA 927 AND STA 947.5 AT RBL 0 WL 208.1 UPPER ATTACHED ANGLE IS CRACKED AS MARKED. 124-056<[01] REMOVED AND REPLACED AFT CABIN INTERCOASTAL BETWEEN STA 927 AND STA 947.5 AT RBL 0 WL 208.1 AS PER B 737-700 SRM 51-40-02-0G-0.;[02] VESDR SWAA2023052228884Floor Support · crackedPASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 277 AND STA 294.5 BL 0 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN FWD WET AREA BETW. STA 277 THRU STA 294.5 BL 0 PER B737-700 SRM 51-40-02-0G-0 AND DRAWING #141A5SDR SWAA2023052228885Intercostal · crackedPASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] OK TO INSTALL NEW INTERCOSTAL.;[02] REMOVED AND REPLACED CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 LBL 46 WL 208.1 AS PER B737-700 SRSDR SWAA2023052228886Floorbeam · crackedSUSPECT CRACK AT PASSENGER CABIN FWD SIDE OF FLOOR BEAM STA 294.5 RBL 51 WL 208.1 HAS A CRACK.<[01] ACCOMPLISHED DVI ON ADJACENT STRUCTURE AREAS; NO CRACKS; NO CORROSIONS OR OTHER DAMAGES NOTED. REF B737-7 SRM 53-10-51-2R-16 STEP 4.C.(4);[02] OK TO APPLY ALODISDR SWAA2023052228875Intercostal · crackedPASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30 WL 208.1 HAS A CRACK AROUND FASTENER HOLE.<[01] OK TO INSTALL NEW INTERCOSTAL.;[02] REMOVED AND REPLACE PASSENGER CABIN FLOOR INTERCOSTAL BETWEEN STA 312 AND STA 328 RBL 30 WL 208.1 PER B737-SDR SWAA2023052229341Support Angle · crackedMAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 LBL 13; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER SUPPORT ANGLE AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 LBL13 PER B737-700 SRSDR SWAA2023052229342Support Angle · crackedMAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 BL 0; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] REMOVED AND REPLACED INTERCOSTAL UPPER SUPPORT ANGLE AT MAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 BL0 PER B737-700 SRM 51SDR SWAA2023052229343Support Angle · crackedMAIN CABIN FLOOR STRUCTURE BETWEEN STA 380 AND STA 400 RBL 9; INTERCOSTAL UPPER SUPPORT ANGLE CRACKED AT FASTENERS HOLES.<[01] RII; VERIFIED INSTALLATION STEPS.SDR SWAA2023052228878Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN LBL 35 AND LBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-047<[01] CORRECTION ON TABLE STEP 17 REMAINING THICKNESS IS 0.121;[02] VERIFIED CORRECTION;[03] REPAIR AFT CABIN FLOOR BEAM STA 986SDR SWAA2023052228865Floorbeam · corroded*CORROSION* AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 HAS CORROSION AROUND FASTENER HOLES AS MARKED. 124-051<[01] REPAIR AFT CABIN FLOOR BEAM STA 986.5 BETWEEN RBL 39 AND RBL 44 WL 208.1 ACCOMPLISHED ON THE ITEM TTG8Q00KJ1J7;[02] CORRECSDR SWAA2023052228844Floor Panel · damagedMAIN CABIN AFT WET AREA FLOOR PANEL # 241ADF HAS A PREVIOUS REPAIR AT TOP SKIN<[01] FABRICATED MAIN CABIN AFT WET AREA FLOOR PANEL #241ADF BY OUTSIDE VENDOR (AERO MARINE) WITH P.O. #2017549.THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00J71MC;[02] VERIFIED FABRICSDR SWAA2023052228847Floor Panel · peelingMAIN CABIN FWD WET AREA FLOOR PANEL #221A TOP SKIN PEELING OFF SEVERAL AREAS<[01] REPLACED MAIN CABIN FWD WET AREA LEFT SIDE FLOOR PANEL #221A REF. B737-700 AMM 53-21-00-400-801. THIS PANEL WILL BE INSTALL ON FAULT #TTG8Q00KH44V;[02] VERIFIED REPLACEMENT OF PASDR SWAA2023052228845Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #242AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] APPLIED GLASS FABRIC REPAIR PLIES AT DAMAGED AREA ON MAIN CABIN CENTER FLOOR PANEL #242AF. REF B737 SRM 53-00-50-2R-1 REPAIR 1 PARAGRAPH 3. MATERIAL USED GLASS FABRIC PLIES PO#: 17385SDR SWAA2023052228846Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #241AF TOP SKIN PEELING OFF SEVERAL AREAS<[01] APPLIED REPAIR IN DAMAGED AREA AT FLOOR PANEL 241AF AS PER B737 SRM 53-00-50-2R-1; MATERIAL USED RESIN PO#1799598 AND CLOTH PO#1738579;[02] VERIFIED STEP 1.SDR SWAA2023052228848Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #231ZF TOP SKIN PEELING OFF SEVERA AREAS<[01] REPAIRED DAMAGE AREAS AS MARKED WITH A PERMANENT REPAIR ON TOP SURFACE OF MAIN CABIN FLOOR PANEL #231ZF AS PER B737 SRM 53-00-50-2R-1. MATERIALS USED PO#1738579 AND PO#1799598 AND PERFSDR SWAA2023052228849Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #231UF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.SDR SWAA2023052228850Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #231DF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.SDR SWAA2023052228854Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #231GF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.SDR SWAA2023052228855Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #231KF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.SDR SWAA2023052228856Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #241KF TOP SKIN PEELING OFF SEVERAL AREAS<[01] VERIFIED STEPS.SDR SWAA2023052228857Floor Panel · peelingMAIN CABIN CENTER FLOOR PANEL #242CF TOP SKIN PEELING OFF SEVERAL AREAS<[01] 'LATE ENTRY' REMOVED MAIN CABIN CENTER AREA FLOOR PANEL #242CF FOR COMPOSITE REPAIR PER B737-700 AMM 53-00-50-2R-0 (PERFORMED BY RHR 19811);[02] MAIN CABIN FLOOR PANEL #242CF WILL BE SDR SWAA2023052228863Strap · corroded*CORROSION* AFT CABIN FLOOR WEB STRAP AT STA 1016+12 RBL 17 WL 208;1 AS MARKED. 124-042<[01] REMOVED CORROSION AT AFT CABIN FLOOR WEB STRAP AT STA 1016+12 RBL 17 WL 208.1. ORIGINAL THICKNESS 0.071'. MATERIAL LOSS 0.021'. REMAINING MATERIAL 0.050'; FOUND OUT OFSDR SWAA2023052228391Stiffener · crackedLEFT HORIZONTAL STABILIZER RIB #4 CRACKED AT STIFFENER #4 LOWER SECTION<[01] MIXED SEALANT PS870B2 ON REPAIR PARTS AT 9:30PM 04/22/2023 .SQUEEZE OUT TIME 11:30PM 04/22/2023 AND INSTALLED FASTENERS ON REPAIR PARTS AT L/H HORIZONTAL STAB RIB #4 AS PER REF B/737-SDR SWAA2023052328186Bracket · elongatedFWD CARGO COMP. LOWER BRACKET TO ATTACH SIDEWALL STRUCTURE WITH ELONGATED HOLE<[1] REPLACED FWD CARGO COMP. FWD LOWER BRACKET TO ATTACH SIDEWALL ACCESS PANEL 122BW REF. B737-700 AMM 25-52-06-400-801. THIS BRACKET WILL BE INSTALL ON FAULT #TTG8Q00J7277;[2] VERISDR SWAA2023052228246Panel · corrodedRT WING L/E FUELING STATION AT 621GB DOOR - P-15 PANEL HAS SURFACE CORROSION AROUND I/B AND O/B GAUGES. 124-011<[01] FAULT WAS RESOLVED ON ANOTHER FAULT. FAULT NUMBER TTG8Q00KFP2Q;;[02] VERIFIED TTG8Q00KFP2QSDR SWAA2023051929581Angle · crackedLEFT VAPOR BARRIER UPPER ANGLE CRACKED AT FASTENER HOLE LBL 2' CORRECTION ON ORIGINAL WRITE UP LEFT VAPOR BARRIER UPPER ANGLE CRACKED AT FASTENER HOLE LBL 6'<[01] OK TO APPLY ALODINE AND PRIMER COAT TO REPAIR PARTS.;[02] TREATED WITH ALODINE AND PRIMER REPAIR SDR SWAA2023052228062Bracket · elongatedLEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET HAS ELONGATED HOLES JUST UNDER ACCESS PANEL 511AT. (DOT #28-1)<[01] REMOVED AND REPLACED LEFT WING L/E ANTI-ICE DUCT SUPPORT BRACKET JUST UNDER ACCESS PANEL 511AT. IN REF SOPM 20-50-01;[02] VERIFIED STEP 1.SDR SWAA2023052228064Handle · out of adjustFWD ENTRY DOOR LINER LOWER ASSIST HANDLE NUT IS CRACKED<[01] REMOVED AND REPLACED FWD ENTRY DOOR LINER LOWER ASSIST HANDLE NUT REF BOEING 737 AMM 52-11-31-400-802;[02] VERIFIED STEP 1.SDR SWAA2023052327569Slat · crackedL/W NO-1 SLAT NOSE L/E SKIN CRACKED @ ACTUATOR RIB ATTACHED POINT OUB MKD DOT<[01] ACCOMPLISHED PART TRANSACTION.;[02] REMOVED AND REPLACED L/W #1 SLAT ASSY IN REFERENCE AMM 27-81-000-801 AND AMM 27-81-21-400-801.;[03] RII -- VERIFIED L/W #1 SLAT ASSY REPLACEMSDR SWAA2023052227584Fitting · damagedL/W REAR SPAR FIXED T/E PANEL 551GB INB AFT SUPPORT STRUT LOWER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED FITTING AT 551-GB. PANEL. USED REF. SRM-51-40-02-0G-0.;[02] VERIFIED FITTING REPLACEMENT.SDR SWAA2023052227583Fitting · elongatedL/W REAR SPAR FIXED T/E PANEL 551GB INB FWD SUPPORT STRUT UPPER ATTACHED FITTING HAS ELONGATED HOLE MKD DOT<[01] REMOVED AND REPLACED SUPPORT STRUT AT PANEL # 551-GB. REF. SRM- 51-40-02-0G-0.;[02] INSPECTED REPLACEMENT OF BEAM FITTING.SDR SWAA2023052227576Fairing · peelingR/H WING TOBODY FAIRING 192BR FWD END EXTERIOR SKIN PEELING MKD DOT<[01] DUPLICATE ITEM - THIS FAULT WILL BE ACCOMPLISHED ON FAULT #TTG8Q00KFNWQ;[02] VERIFIED DUPLICATED.SDR SWAA2023051943850Panel · delaminatedLOWER RT WING TO BODY FAIRING PANEL 192BR DELAMINATED<[01] REMOVED AND REAPPLIED GLASS FABRIC PLIES; PRIMED AND TOPCOATED PANEL 192BR. REF B737 SRM 53-40-70-2R-1 AND SRM 51-70-04-2R-1 REPAIR 1 PARAGRAPH 4; AMM 51-21-72-370-804; AMM 51-21-73-370-803<BR>MATERIALSDR SWAA2023051927574Door · crackedR/H MAIN LANDING GEAR CENTER DOOR CRACKED.<[01] PARTS TRANSACTION FOR ROUTING OUT FOR REPAIR;[02] REMOVED AND REPLACED R/H MAIN LANDING GEAR DOOR ASSEMBLY. REF:B-737 AMM 32-13-11-000-803 AND AMM 32-13-11-420-803.;[03] VERIFIED REMOVED AND REPLACED R/H MAIN LANSDR SWAA2023040422846Seat Back · out of adjustSEAT 11E RECLINES IN FRONT OF EXIT ROW<[01] ADJUSTED SEAT LOCK ASSEMBLY ON SEAT 11E PER CMM 25-21-42.SDR SWAA2023033021806Lens · brokenFWD LOWER EMERGENCY EXIT INDICATOR LENS AT ROW 12DEF IS BROKEN<[01] REMOVED AND REPLACED FWD LOWER EMERGENCY EXIT LIGHT LENS IAW AMM 33-51-01.SDR SWAA2023032118276Window · failedAIRCRAFT FAILED TO PRESSURIZE; FO SLIDING WINDOW LOCKED BUT DID NOT FULLY SEAL.<[01] FOUND FO?S SLIDING WINDOW NOT PROPERLY CLOSED; R & R?D FO?S SLIDING WINDOW PER MT 756-12-03. PERFORMED SATISFACTORY CABIN PRESSURE LEAK TEST PER AMM 05-51-91.SDR SWAA2023031516327Flap Track · looseLEFT WING OUTBOARD AFT FLAP #3 TRACK LOOSE AT AFT ATTACH POINT<[01] REMOVED AND REPLACED LH WING OUTBD AFT FLAP TRACK #3 PER AMM 27-51-26SDR SWAA2023031516328Flap Track · looseLEFT WING OUTBOARD AFT FLAP #4 TRACK LOOSE AT AFT ATTACH POINT<[01] REMOVED AND REPLACED LH WING OUTBD AFT FLAP TRACK #4 PER AMM 27-51-26SDR SWAA2023031414547Slide · draggingL2 DOOR SLIDE GRIT DRAGGING DOOR WAY<[01] REPACKED L2 DOOR ESCAPE SLIDE PER AMM 25-66-01;[02] REPACKED SLIDE PER MT 725-61-06 . ORIGINALLY USED WRONG REFERENCE .SDR SWAA2023031414550Battery Pack · failed4 EMERGENCY LIGHT BATTERY PACKS FAILED CAPACITY CHECK.<[01] R&R 4 EMERGENCY LIGHT BATTERY PACKS AT LOCATIONS M1670; M1669; M1675 AND M1668 PER AMM 33-51-06.SDR SWAA2023031414561Handle · looseFWD GALLEY SERVICE DOOR HANDLE CAM HAS EXCESSIVE PLAY.<[01] FOUND LOOSE NUT ON FWD GALLEY SERVICE DOOR HANDLE CAM. FASTENED LOOSE NUT IAW AMM 52-41-11.SDR SWAA2023030812849Girt Bar · looseGIRT BAR SCREWS LOOSE ON FORWARD SERVICE DOOR.<[01] SECURED FASTENERS ON FWD SVC DOOR GIRT BAR PER SIP.SDR SWAA2023022104240Battery Pack · inoperativeEMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 INOP<[01] REPLACED; AND PERFORMED GOOD INSTALLATION TEST OF EMERGENCY LIGHT BATTERY PACK M1673.;[02] ADDITION FOR CORRECTIVE ACTION 1: WORK PERFORMED PER AMM 33-51-06-960-805.;[03] VERIFIED CORRECTIVE AC
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