Boeing 737-7BD
Service difficulty reports · 7,528
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 = '7377BD' 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 = '7377BD' 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 SWAA2022072525476Web · corrodedAFT CARGO DOOR-WEB SUPPORT THRESHOLD HAS SPOTS OF CORROSION. / [01] REMOVED CORROSION FROM AFT CARGO COMPARTMENT THRESHOLD WEB AS PER REFERENCE B737-700 SRM 51-10-02-0G-0.;[02] VERIFIED STEP 1.;[03] PERFORMED UT THICKNESS INSP ON REWORKED AREA IAW B737 NDT P4 SDR SWAA2022070725522Lens · out of positionMISSING EXIT SIGN BY AFT SERVICE DOOR / [01] TAPED AFT SERVICE DOOR EMERGENCY EXIT LIGHT LENS IN PLACE WITH MYLAR TAPE PER EA 33-51-00-710-801SDR SWAA2022070525303Clamp · looseGIRT BAR CLIP IS LOOSE - FORWARD ENTRANCE PASSENGER DOOR / [01] TIGHTEN CLIP FOR GIRT BAR AT FWD ENTRY DOOR IAW MM SIPSDR SWAA2022072524745Doubler · crackedCRACK FOUND AT LT HORIZONTAL STAB. LWR SKIN STAB STA 184.70 ; 10.5' FROM REAR SPAR I/B ROW. CRACK LENGTH : 0.343' CRACK FOUND AT LT HORIONTAL STAB. LWR SKIN STAB STA 184.70 10.5" FROM REAR SPAR I/B ROW. CRACK LENGTH : 0.343" / [01] REMOVED EXISTING REPSDR SWAA2022072524746Skin · crackedCRACK FOUND AT LT HORIZONTAL STAB. LWR SKIN STAB STA 193.90 ; 16.5' FROM FRONT SPAR I/B ROW. CRACK LENGTH : 1.0' CRACK FOUND AT LT HORIONTAL STAB. LWR SKIN STAB STA 193.90 16.5" FROM FRONT SPAR I/B ROW. CRACK LENGTH : 1.0" / [01] REMOVED EXISTING FASTESDR SWAA2022072724552Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BSDR SWAA2022072734896Baffle · crackedFWD CARGO COMP. LEFT SIDE BAFFLE IS CRACK AT FWD END BETWEEN STA 500A AND 500B LBL-24. / [01] REMOVED FWD CARGO LT.SIDE BAFFLE AT STA 500A AND 500B LBL 24 IN REF SRM 51-40-02-0G-0;[02] VERIFIED STEP 1;[03] PEROFRMED HFEC ROTO INSP ON FASTENER OPEN HOLES; IAW BSDR SWAA2022072724554Channel · crackedFWD CARGO COMP. RIGHT/Z-CHANNEL HAS A CRACK BETWEEN STA 500C-STA 500D RBL-24. / [01] LOCATED AND DRILLED NEW FWD CARGO RT. SIDE 'Z' CHANNEL IN REF SRM 51-40-05-0G-0;[02] VERIFIED STEP # 1;[03] TREATED AND PRIMED FWD CARGO RT. Z CHANNEL AS PER SRM 51-20-01-0G-0SDR SWAA2022072724547Angle · crackedAFT CARGO COMP. FWD BULKHEAD CENTER LOWER SUPPORT ANGLE IS CRACK AT STA 727+4 RBL-5. / [01] REMOVED DAMAGED SUPPORT ANGLE FROM AFT CARGO FWD BULKHED AT STA 727+4 RBL-5;[02] CORRECTION. REMOVED DAMAGED SUPPORT ANGLE FROM AFT CARGO FWD BULKHED AT STA 727+4 RBL-5SDR SWAA2022072724543Channel · corrodedAFT CARGO COMP. RIGHT/Z-CHANNEL HAS CORROSION AROUND FASTENERS HOLE FROM STA 727B TO STA 767 RBL-22. / [01] FOUND EXFOLIATED CORROSION TO BE OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2;[02] RECIEVED NEW PART 146A7502-51; NEW PART WILL BE INSTALLED UNDER TASK CSDR SWAA2022072724546Channel · corrodedAFT CARGO COMP. LEFT/Z-CHANNEL HAS CORROSION AROUND FASTENERS HOLE FROM STA 727C TO STA 787 LBL-22. / [01] FOUND EXFOLIATED CORROSION TO BE OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2;[02] RECIEVED NEW PART 146A7502-27; PART WILL BE INSTALLED UNDER TASK CARD: SDR SWAA2022070124217Ballast · inoperativeCA SIDE EMERGENCY EXIT DOOR LIGHT INOP / [01] REMOVED AND REPLACED BALLAST PER AMM 33-51-01SDR SWAA2022072723940Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #2 STIFFENER #2 LOWER FLANGE HAS A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] PERFORMED HFEC INSP ON RSDR SWAA2022072723941Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #2 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[06] CUT OSDR SWAA2022072723942Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #3 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR SWAA2022072723943Stiffener · crackedL/H HORIZONTAL STABILIZER RIB #5 STIFFENER #4 LOWER FLANGE; WITH A CRACK. STAB. STA-129.50 / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUT OSDR SWAA2022070124065Cover · looseEMERG EXIT LIGHT COVER FELL OFF / [01] RE-INSTALLED LIGHT COVER IAW AMM 33-23-00SDR SWAA2022072723921Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #3 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] RT STABILAIZER RIB 4 STSDR SWAA2022072723923Stiffener · crackedR/H HORIZONTAL STABILIZER RIB #4 STIFFENER #4 LOWER FLANGE WITH A CRACK. / [01] PERFORMED HFEC INSP ON RIB STIFFENER LOWER FLANGE IAW B737 NDT P6 51-00-00 PROC.23; CRACK CONFIRMED.<BR>TOOL USED : NORTEC 600 B/C 172389 CALDUE: 03/23;[02] CUTOUT THE DAMAGE AREA SDR SWAA2022072722896Shield · corroded**CORROSION**AFT CARGO DOOR CUTOUT SHIELD JUST AFT OF CARGO DOOR CUTOUT; CORRODED. STA 847-867; WL-156; BL-33 / [01] RECIEVED NEW PART P/N: 146A8127Y10ATSMRO. NEW PART WILL BE INSTALLED UNDER TASK CARD: TTG8Q0048PN3;[02] CORRECTION FOR STEP #1 SHOULD READ: RECSDR SWAA2022072722895Shield · crackedAFT CARGO DOOR CUTOUT SHIELD JUST FWD OF CARGO DOOR CUTOUT; CRACKED. / [01] RECIVED NEW SHIELD P/N 453A2611-1; NEW HIELD WILL BE INSTALL <BR>ON EA MOC CARD TTG8Q0043PN3;[02] VERIFIED STEP 1.SDR SWAA2022072722893Web · crackedL/H MAIN W/W FWD WALL; VERTICAL PRESSURE WEB HAS A CRACK. STA-663 LBL-40 / [01] MEASUREMENTS;[02] REMOVED PREVIOUS REPAIR AND PERFORMED VISUAL INSPECTION FOUND CRACK SIZE 16' AND FOUND UNWANTED MATERIAL ON VAPOR BARRIER PER B737NTM51-05-01 PART 1;[03] PREPAREDSDR SWAA2022072722748Slat · crackedRIGHT WING L/E SLAT #5 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 85.19. (51-002) / [01] PERFORMED HFEC INSP. ON A POSSIBLE CRACK IAW B737 NDT PART 6; 51-00-00; PROCEDURE 23. CRACK NOTED AND MARK (CRACK LENGTH .156') <BR>TOSDR SWAA2022072722752Slat · crackedRIGHT WING L/E SLAT #7 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 322.71. (51-004) / CRACK NOTED AND MARK (CRACK LENGTH .156') <BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/20/22;[02] REMOVED COVE PANELS 624CB; 624DB; 624EB AND SDR SWAA2022072722751Slat · crackedRIGHT WING L/E SLAT #6 LOWER SURFACE SKIN HAS VISUAL CRACK INDICATION AT ACTUATOR FITTING SLAT STATION 202.45. (51-003) / CRACK NOTED AND MARK (CRACK LENGTH .125') <BR>TOOL: NORTEC 600 B/C: 166317 DUE: 10/20/22;[02] REMOVED EXISTING FAST. LOCATED AND DRILLED NSDR SWAA2022062721893Fitting · looseCUSTOMER WALK: L-2 DOOR GIRT BAR FITTING IS LOOSE. / [01] RE-SECURED L2 DOOR GIRT BAR FITTING. REF B737 SOPM 20-50-01.;[02] VERIFIED STEP 1.SDR SWAA2022062721347Light · contaminatedL & R ROW 1 PHOTO ILLUMINESENT STRIPS HAVE CONDENSATION / [01] R&R PHOTO ILLUMINESENT STRIPS PER AMM 33-51-15SDR SWAA2022062721088Battery Pack · inoperativeEMERGENCY LIGHTS AROUND R/H OVER WING EMERGENCY EXIT ARE INOP. / [01] R&R RH EMERGENCY EXIT BATTERY PACK PER AMM 33-51-06SDR SWAA2022062721089Indicator · brokenRH EMERGENCY EXIT ROW LOWER EMERGENCY EXIT INDICATOR BROKEN / [01] R&R RH EMERGENCY EXIT INDICATOR PER AMM 33-51-01.SDR SWAA2022062720659Battery · inoperativeEMERGENCY LIGHTS INOP AT 7ABC; 8DEF; 9ABC; 12ABC. / [01] PERFORMED T/S FOUND BATTERY PACK POSITION M2335 INOP; AS PER WDM 33-51-12 AND AMM 33-51-06-960-805.;[02] VERIFIED STEP 1;[03] REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACK M2335 AS PER REF AMM 33-51SDR SWAA2022070120398Floor Panel · crackedCRACK FLOOR PANEL 140BF AT AFT CARGO COMPARTMENT 2022-266168 / [01] FABRICATED FLOOR ACCESS PANEL 140BF AT AFT CARGO COMPARTMENT IAW B737-700 AMM 25-52-01-201-801.DWG 453A2610; SHEET 20; REV: E. USED MATERIAL: ALUMINUM SHEET 2024T3-071; PO: 2021 210316.;[02] CSDR SWAA2022062220375Megaphone · inoperativeFWD MEGAPHONE INOP / [01] REMOVED AND REPLACED FWD MEGAPHONE BATTERIES; OPS CHECK GOOD. REFERENCE AMM 25-64-00.SDR SWAA2022062220069Sign · inoperativeLH OVERWING EMERGENCY EXIT SIGN FWD BULB INOP. / [01] RELAMPED LH OVERWING EXIT EXIT SIGN LIGHT IAW AMM 33-51-01.SDR SWAA2022062719301Scuff Plate · crackedAFT CARGO COMPARTMENT FWD SCUFF PLATE CORNER CRACKED ON TOP MARKED / [01] REPAIRED SCUFF PLATE BY OUT SIDE VENDOR J.L WELDING FAA REPAIR STATION NUMBER: JLWR146K AS PER SRM 53-60-15-2R-1;[02] SERVICEABLE ECUFF PLATE PANEL WILL BE INSTALL ON WORK CARD TTG8Q003GSDR SWAA2022061618820Battery Pack · inoperativeALL EMERGENCY LIGHTS ON BATTERY PACK M2335 ARE INOP. REMOVED BATTERY AT 500C L/H ; M2335 IAW AMM 33-51-06-960-805. INSTALLED NEW BATTERY PACK POSITION 500C L/H M2335. PERFORMED OPS CHECK STATUS GOOD/PASSED.SDR SWAA2022062717470Scuff Plate · crackedAFT CARGO DOOR FWD SCUFF PLATE CORNER CRACKED UPON INSTALLATION. / [01] SCUFF PLATE FDW CORNNER REPARED BY OUTSIDE VENDOR J.LWELDING;INC FAA REPAIR STATION NUMBER JLWR146K AS PER B737-700 SRM 53-60-15-2R-1;[02] VERIFIED STEP # 1SDR SWAA2022062717574Vapor Barrier · crackedC/R RT STA 663 VAPOR BARRIER CRACKED IN MULTIPLE AREAS MARKED WITH RED DOTS / [01] REMOVED THE DAMAGED PLIES AND PREPARED DAMAGED AREA TO APPLY DRY OUT. DRILLED STOP HOLES AT THE CRACKS END. REF B737-700 SRM 57-10-10-2R-2 PARAGRAPH 6 AND SRM 51-70-04-2R-10 REPSDR SWAA2022061516617Battery Pack · inoperativeMISC AFT LEFT EMERGENCY EXIT LIGHTS ARE INOP<[01] REMOVED OLD BATTERY OK TO INSTALL NEW BATTERY FOR EMERGENCY LIGHT AT STATION 727C IAW AMM 33-51-06-960-805;[02] REMOVED BATTERY PACK AT STATION L/H 727C;[03] OK TO INSTALL;[04] REPLACED WITH NEW BATTERY AT STATSDR SWAA2022061516619Battery Pack · inoperativeMISC L/H OVERWING EXIT EMERGENCY LIGHTS ARE INOP<[01] REMOVED OLD BATTERY OK TO INSTALL NEW BATTERY FOR EMERGENCY LIGHTS IAW AMM 33-51-06-960-805;[02] OK TO INSTALL;[03] REPLACED WITH NEW BATTERY AT STATION 603 IAW AMM 33-51-06-960-805 PERFORMED OPS CHECK ON LSDR SWAA2022060915971Radome · delaminatedRADOME HAS DELAMINATION / [01] ACCOMPLISHED EA 22-153-01684; PER TSR #2022004444. APPLY SCOTCHBRAND 853 OR PERMACEL P280 TAPE TO DAMAGED AREA WITHIN 5 FLIGHT CYCLES. ACCOMPLISH INSPECTION EVERY 480 FLIGHT HOURS AND PERMANENT REPAIR DUE WITHIN 85 DAYS.;[02] ACCSDR SWAA2022060815786Light · inoperativeEMERGENCY LIGHT EXTINGUISHED AFT OF LEFT WING FAIRING. / [01] RELAMPED LH OVER WING EMERGENCY LIGHT PER AMM 33-51-04. OPS CHECK GOOD.SDR SWAA2022060815288Megaphone · inoperativeFORWARD FA MEGAPHONE WILL NOT TEST. / [01] R?D AND R?D FORWARD FA MEGAPHONE PER AMM 25-64-00SDR SWAA2022062714837Angle · corrodedAFT CARGO R/H ZEE ANGLE WITH CORROSION SPOTS FROM STA 727D+10' TO 767 AND RBL-22 AND ABOUT WL-160 / [01] FOUND AFT CARGO R/H ZEE ANGLE EXFOLIATED CORROSION OUT OF LIMITS AS PER B737 SRM 53-00-53-1A-2;[02] NEW ZEE ANGLE WILL BE INSTALLED UNDER AFT CARGO COMPARTSDR SWAA2022062714833Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION BETWEEN STA 727D-277E AND ABOUT WL 160 / [01] FOUND AFT CARGO L/H ZEE ANGLE EXFOLIATED CORROSION OUT OF LIMITS AS PER 53-00-53-1A-2;[02] RECEIVED NEW PART P/N 146A7502-51; P.O.#1728471 . THIS PART WILL BE INSTALLED ON FAUSDR SWAA2022062714830Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION AT STA 727+14' AND LBL-22 AND ABOUT WL 158 / [01] WORK WILL BE ACCOMPLISHED UNDER (TTG8Q00CU24B);[02] CORRECTION FOR STEP #1 TT NUMBER SHOULD READ: WORK WILL BE ACCOMPLISHED UNDER (TTG8Q0047ZRC);[03] L/H ZEE CHANNEL REPLASDR SWAA2022062714831Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION BETWEEN STA 727B+6' TO 727C AND LBL-22 AND ABOUT WTL 160 / [01] WORK WILL BE ACCOMPLISHED UNDER (TTG8Q00CU24B);[02] CORRECTION FOR STEP #1 TT NUMBER SHOULD READ: WORK WILL BE ACCOMPLISHED UNDER (TTG8Q0047ZRC);[03] L/H ZEESDR SWAA2022062714832Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION FROM STA 727C-727D AT LBL-22 AND ABOUT WL-160 / [01] WORK WILL BE ACCOMPLISHED UNDER (TTG8Q00CU24B);[02] CORRECTION FOR STEP #1 TT NUMBER SHOULD READ: WORK WILL BE ACCOMPLISHED UNDER (TTG8Q0047ZRC);[03] L/H ZEE CHANNEL RESDR SWAA2022062714840Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION SPOTS FROM STA 767-787 AND LBL-22 AND ABOUT WL-160 / [01] WORK WILL BE ACCOMPLISHED UNDER (TTG8Q00CU24B);[02] CORRECTION FOR STEP #1 TT NUMBER SHOULD READ: WORK WILL BE ACCOMPLISHED UNDER (TTG8Q0047ZRC);[03] L/H ZEE CHANNSDR SWAA2022062714836Angle · corrodedAFT CARGO L/H ZEE ANGLE WITH CORROSION SPOTS FROM STA 787 TO 787+15' AND LBL-22 AND WL-160 / [01] WORK WILL BE ACCOMPLISHED UNDER (TTG8Q00CU24B);[02] CORRECTION FOR STEP #1 TT NUMBER SHOULD READ: WORK WILL BE ACCOMPLISHED UNDER (TTG8Q0047ZRC);[03] L/H ZEE CHANSDR SWAA2022060714764Panel · elongated193B PANEL HAS ELONGATED HOLE AT THE #17 POSTION / [01] REMOVED AND REPLACED 193B PANEL <BR>REF AMM 53-51-21;[02] CW
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