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 SWAA2018012219220Doubler · crackedEXTERNAL POWER DOOR CUT OUT INNER SKIN DOUBLER FORWARD LOWER EDGE CRACKED. REPAIRED SKIN IAW SRM.SDR SWAA2022020799377Panel · crackedL/H LEADING EDGE ACCESS PANEL 521QB IS CRACKED AT SCREW HOLE. (MARKED) / REMOVED AND REPLACED L/H WING LEADING EDGE ACCESS PANEL 521QB AS PER AMM 57-41-02.SDR SWAA2018010318831Sign · defectiveL2 EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROWS. R&R SIGN IAW AMM.SDR SWAA2018010318830Sign · defectiveRT OVERWING EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROWS. R&R SIGN IAW AMM.SDR SWAA2018010318757Sign · brokenRT OVER WING LOWER EXIT SIGN BROKEN. R&R SIGN PER AMM.SDR SWAA2018010318752Sign · defectiveR2 EMERGENCY EXIT SIGN MISSING DIRECTIONAL ARROWS. R&R SIGN IAW AMM.SDR SWAA2018010318748Cover · unsecureLT FORWARD EMERGENCY EXIT LIGHT COVER FELL OFF ON LANDING. SECURED COVER PER SIP.SDR SWAA2022020799994Angle · corrodedCORROSION IN AND AROUND NUTPLATE HOLES FOR RH TRANS ANGLE FRO STA 767 TO STA 792 / REMOVED AND REPLACED TRANSITION ANGLE PER SRM 51-40-02SDR SWAA2018010218706Crease Beam · corrodedRT INBOARD CREASE BEAM UPPER SURFACE CABIN FLOOR STRUCTURE CORRODED BETWEEN BS 685 TO BS 727. R&R CREASE BEAM IAW SRM.SDR SWAA2018010218705Crease Beam · corrodedLT INBOARD CREASE BEAM UPPER SURFACE CABIN FLOOR STRUCTURE CORRODED BETWEEN BS 685 TO BS 727. R&R CREASE BEAM IAW SRM.SDR SWAA2018010218704Support Channel · crackedCABIN FLOOR PANEL SUPPORT CHANNEL CRACKED AT FASTENER, BS 540, RBL 24. R&R CHANNEL PER SRM.SDR SWAA2018010218703Crease Beam · corrodedRT INBOARD CREASE BEAM LOWER SURFACE CORRODED AT BS 727 AROUND FASTENER HOLE. R&R CREASE BEAM IAW SRM.SDR SWAA2018010218702Floor Support · crackedCABIN FLOOR SUPPORT CHANNEL CRACKED AT FASTENER, BS 540, RBL 1. R & R THE FLOOR SUPPORT IAW SRM.SDR SWAA2017122818700Rib · crackedRIGHT HORIZONTAL STAB RIB CRACKED AT HSS 129.5. REPAIRED THE RIB IAW SRM.SDR SWAA2022020799367Angle · corrodedAFT CARGO R/H TRANSITION ANGLE HAS CORROSION AROUND NUT PLATE HOLES FROM STA 787 TO STA 801. / CORRECTED ATA CODE. REMOVED AND REPLACED TRANSITION ANGLE AT STA 787-801 AS PER SRM'S 51-10-02 AND 51-40-02.SDR SWAA2022020799920Skin · dentedDENT WITH CREASE IN FUSELAGE SKIN; BS506; BETWEEN STR 17-18R. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2022020799921Skin · dentedSKIN DENT WITH CREASE AT STA 498; BETWEEN STR 18-19L. / FACT AS A RESULT OF POST REPAIR INSPECTIONSDR SWAA2022020799360None · crackedUPPER(TITANIUM) CHORD COMMON TO THE STA.663 PRESSURE BULKHEAD HAS 1EA. HOLE WITH A CRACK INDICATION AT APPROX.RBL.40(MARKED) VERIFIED PER NDT MANUAL PART.6; 51-00-00 PROC.17. / OVER-SIZED FASTENER HOLE TO MAX NOMINAL DIMENSIONS OF .191'; DEBURRED HOLE AND CLEASDR SWAA2022020799359Plate · crackedLEFT WING LOWER REAR SPAR 4TH WIGGLE PLATE OUTBOARD OF #2 FLAP TRACK IS CRACKED / INSTALLED WIGGLE PLATE PER SRM 51-40-02SDR SWAA2022020799721Intercostal · crackedR/H WING UPPER FIXED T/E SHELF PANEL JUST I/B OF DEFLECTION RIB INTERCOSTAL IS CRACKED. / REMOVED INTERCOSTAL PER SRM 51-40-02; ACQUIRED NEW INTERCOSTAL FROM STORES SI# 7570737; LOCATED AND DRILLED NEW INTERCOSTAL PER SRM 51-40-06; INSTALLED NEW INTERCOSTAL (WSDR SWAA2022020499321Fairing · crackedPANEL 193B HAS DAMAGE TO THE LANDING; CRACKING AND WEAR. PANEL IS THE LWR BELLY PANEL FWD OF THE WHEEL WELL CUTOUT. / REPAIRED PER SRM 51-7O-05-2R-6. RESTORED FINISH PER MM 51-21-81.SDR SWAA2022020799295Plate · crackedLH LOWER REAR SPAR CHORD WIGGLE PLATE CRACKED IB OF #3 FLAP TRACK / REMOVED WIGGLE PLATE AND INSTALLED NEW WIGGLE PLATE PER SRM 51-10-02SDR SWAA2022020799269Rib · crackedTHIRD FROM FORWARD RIB INBOARD FLANGE CRACKED AT STAB STA 120.30 / REPAIRED THIRD FROM FORWARD RIB INBOARD FLANGE CRACKED AT STAB STA 120.30 PER SRM 55-10-09-2R AND EA #1-755-3960. SEE SUBTASK AND WIP SIGN-OFFS FOR WORK ACCOMPLISHEDSDR SWAA2022020799296Plate · crackedLH LOWER REAR SPAR CHORD WIGGLE PLATE CRACKED IB OF DEFLECTION ROLLER FITTING / REMOVED AND REPLACED INSTALLED NEW WIGGLE PLATE PER SRM 51-10-02. SEE WORK PERFORMED FOR INDIVIDUAL SIGN OFFS.SDR SWAA2022020799298Floor Panel · pulledCENTER CABIN FLOOR PANEL 241AF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799299Floor Panel · pulledCENTER CABIN FLOOR PANEL 231XF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799300Floor Panel · missingCENTER CABIN FLOOR PANEL 241DF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799301Floor Panel · missingCENTER CABIN FLOOR PANEL 232RF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799302Floor Panel · missingCENTER CABIN FLOOR PANEL 232SF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799303Floor Panel · missingCENTER CABIN FLOOR PANEL 242CF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799304Floor Panel · missingCENTER CABIN FLOOR PANEL 241CF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799305Floor Panel · missingCENTER CABIN FLOOR PANEL 231YF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799306Floor Panel · missingCENTER CABIN FLOOR PANEL 231ZF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799307Floor Panel · missingCENTER CABIN FLOOR PANEL 241FF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799308Floor Panel · missingCENTER CABIN FLOOR PANEL 241EF HAS MISSING FIBERS. / REMOVED AND REPLACED CABIN FLOOR PER AMM 53-21-00.REINSTALLED PANEL ON SWA ROUTINE CARD # JPANEL-231-CLOSE.SDR SWAA2022020799311Plate · crackedR/H WING REAR SPAR WIGGLE PLATE JUST INBD OF #6 FLAP TRANSMISSION IS CRACKED AT A FASTNER . / REMOVED AND REPLACED WIGGLE PLATE PER SRM 51-40-02.SDR SWAA2022020799268Rib · crackedSECOND FROM FORWARD RIB INBOARD FLANGE CRACKED AT STAB STA 120.30 / REPAIRED RIB PER SRM 55-10-09-2R-4.SDR SWAA2018010918899Scuff Plate · crackedAFT CARGO DOOR AFT CORNER SCUFF PLATE CRACKED AT FORWARD EDGE. REPAIRED THE SCUFF PLATE IAW SRM.SDR SWAA2018010918898Scuff Plate · crackedAFT CARGO DOOR FORWARD CORNER SCUFF PLATE CRACKED AT FORWARD EDGE. REPAIRED THE SCUFF PLATE IAW EA.SDR SWAA2017121918570Pressure Panel · crackedRT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 43. REPAIRED WEB PER SRM.SDR SWAA2017121918569Pressure Panel · crackedRT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 34. REPAIRED WEB PER SRM.SDR SWAA2017121918568Pressure Panel · crackedRT MAIN WHEEL WELL VERTICAL PRESSURE WEB CRACKED AT BS 663, RBL 36. REPAIRED WEB PER SRM.SDR SWAA2022020496177Support Angle · crackedAFT OF #1 PYLON UPPER T/E PANEL INBD OF DEFLECTION RIB; SUPPORT ANGLE CRACKED ON FWD SIDE. / REMOVED AND REPLACED SUPPORT ANGLE IAW SRM 51-40-02.SDR SWAA2022020499515Balance Weight · corrodedRUDDER BALANCE ARM WEIGHT HAS CORROSION ON UPPER SURFACE. / REMOVED AND REPLACED RUDDER BALANCE ARM WEIGHT PER SRM 51-60-07-0G-0 PARAGRAGH STEPS (6)(C) TO (6)(C) 2)D). SEE SUBTASKS AND WIPS FOR INDIVIDUAL SIGNOFFSSDR SWAA2022020499517Plate · crackedL WING TRAILING EDGE PANEL SUPPORT WIGGLE PLATE OTBD OF MAIN GEAR ACTUATOR CRACKED.(MARKED) / REMOVED & REPLACED WIGGLE PLATE IAW SRM 51-40-02; ALSO RESTORED FINISH IAWAMM 51-21-99.SDR SWAA2022020499518Plate · crackedR/H WING T/E LOWER SPAR WIGGLE PLATE IS CRACKED JUST I/B OF #6 FLAP TRACK / REMOVED; AND REPLACED WIGGLE PLATE. REF. SRM.51-40-02SDR SWAA2022020499562Seat Track · corroded#4 PASSENGER SEAT TRACK IS CORRODED ON UPPER SURFACE STA 850 / REMOVED AND REPLACED RBL 45.5 SEAT TRACK SECTION FROM STA. 727B TO STA.887 PER SRM 51-40-02.SDR SWAA2022020499561Seat Track · cracked#4 PASSENGER SEAT TRACK IS CORRODED ON UPPER SURFACE STA 820 / RBL 45.5 SEAT TRACK SECTION WILL BE REMOVED AND REPLACED FROM STA. 727B TO STA.887 ON N/R G513234.SDR SWAA2017121318434Seat Track · corrodedNR 4 PASSENGER SEAT TRACK CORRODED ON UPPER SURFACE AT BS 727C+15, RBL 45.5. REPAIRED SEAT TRACK PER SRM.SDR SWAA2017121118343Web · crackedRT WING UPPER TRAILING EDGE SHELF PANEL OUTBOARD NR 7 SPOILER VERTICAL WEB CRACKED AT OUTBOARD UPPER FASTENER. R&R WEB PER SRM.
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