Boeing 737-228
Service difficulty reports · 371
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 = '737228' 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 = '737228' 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 F3LA200200006Torque Box · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON TORQUE BOX AT UPPER AND LOWER MOUNT PADS AFT END OF L-2 DOOR. REPLACED TORQUE BOX ASSY PER OHM 52-16-03.SDR F3LA200200005Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM AT STA 528, RBL 10, CORRODED. REMOVED DAMAGED PORTION OF FLOORBEAM UPPER CHORD PER SRM 51-30-2. FABRICATED AND INSTALLED REPLACEMENT UPPER CHORD PER SRM 53-10-9.SDR F3LA200200004Stringer · corrodedDURING C-7 CHECK, INSPECTION CORROSION AROUND RIVET HEAD AT STR 16-R, STA 797, ON ANGLE TO WEB ATTACHMENT. FABRICATED REPLACEMENT ANGLE AND INSTALLED REPAIR PER SRM 51-10-2, 51-30-2 AND SOPM 20-41-2.SDR F3LA200200003Frame · brokenDURING C-7 CHECK, INSPECTION REPORTED BROKEN FRAME AT NR 2 ENGINE INBOARD FIXED COWL AFT CROSSOVER RIB. REPLACED BROKEN INTERCOSTAL (FRAME) PER SRM 51-30-2, 51-30-5 AND 51-30-6.SDR F3LA200200001Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, LBL 2.5. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1 AND 53-10-5.SDR F3LA200100150Intercostal · crackedDURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL BENT AND CRACKED AT STA 500, STR 26-L. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 51-10-1.SDR F3LA200200002Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED CARGO BEAM CORRODED AT FLOOR PANEL SPLICE, STA 770, RBL 8. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-1, 53-10-3 AND 53-10-5.SDR F3LA200100148Floor Panel · crackedDURING C-7 CHECK, INSPECTION REPORTED FLOORBEAM PANEL CRACKED AND CORRODED ABOVE STRINGER 25-R AT STA 787. FABRICATED AND INSTALLED REPLACEMENT PANEL PER BOEING DRAWING 69-43477 AND SRM 51-10-2 AND 51-30-2.SDR F3LA200100147Stringer · crackedDURING C-7 CHECK, INSPECTION REPORTED STR 16-L CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER SERVICE BULLETIN B737-53-1145 AND EA 53-737-148.SDR F3LA200100146Stringer · crackedDURING C-7 CHECK, INSPECTION REPORTED STR 16-R CRACKED ON FWD AND AFT ENDS OF WING ICE LIGHT AT STA 510. REPAIRED PER SERVICE BULLETIN B737-53-1145 AND EA 53-737-148.SDR F3LA200100145Angle · crackedDURING C-7 CHECK, INSPECTION REPORTED ANGLE CRACKED AT 178 BULKHEAD, WL 200, LBL 17.1. REPAIRED CRACK IN ANGLE PER SRM 51-20-1 AND 51-30-2.SDR F3LA200100144Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 294 FROM LBL 17 TO LBL 25. FABRICATED REPAIR AND INSTALLED PER SRM 51-40-3, FIG 1 AND 53-10-9, FIG 5.SDR F3LA200100143Skin · crackedDURING C-7 CHECK, INSPECTION REPORTED CRACK IN RADIUS OF R-2 DOOR TOP HINGE CUTOUT. FABRICATED A FILLER AND INSTALLED REPAIR DOUBLER PER SRM 53-30-02.SDR F3LA200100142Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED INTERCOSTAL CRACKED AT STR 26-L, STA 460. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-10-2 AND 51-10-02.SDR F3LA200100141Angle · corrodedDURING C-7 CHECK, INSPECTION REPORTED ANGLE CORRODED AT AFT SIDE OF STA 787, STR 25-R. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 53-10-2 AND 51-10-02.SDR F3LA200100140Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED WEB INTERCOSTAL ON AFT SIDE OF STA 787, STR 25-R, CORRODED. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER SRM 53-10-2 AND 51-10-02.SDR F3LA200100139Web · corrodedDURING C-7 INSPECTION, INSPECTION REPORTED KEEL BEAM WEB CORRODED FROM B.S. 787 TO B.S. 807, RBL 10. FABRICATED AND INSTALLED REPLACEMENT WEB PER SRM 53-10-2, ITEM 33, PAGE 32, 41.SDR F3LA200100134Floorbeam · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT STA 312, FROM LBL 13 TO RBL 13. REMOVED DAMAGED SECTION OF FLOOR BEAM, FABRICATED REPLACEMENT FLOORBEAM AND ANGLE SPLICES AND INSTALLED PER SRM 53-10-4.SDR F3LA200100130Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 L/E SLAT HAD PULLED AND WORKING RIVETS ON INSIDE L/E OTBD OF ACTUATOR AND INBD OF OTBD MAIN TRACK. REPLACED FASTENERS PER SRM 51-30-02.SDR F3LA200100127Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON LOWER T/E SKIN AROUND ACTUATOR AND INBD OF TRACKS. REPLACED RIVETS PER SRM 51-30-02.SDR F3LA200100128Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 4 SLAT LOWER INNER SKIN RIVETS LOOSE FROM INSIDE STRUCTURE BETWEEN ACTUATOR AND OTBD OF TRACKS. REPLACED LOOSE FASTENERS PER SRM 51-30-2.SDR F3LA200100129Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 6 SLAT HAD PULLED AND WORKING RIVETS ON LOWER SKIN T/E AROUND ACTUATOR. REPLACED FASTENERS PER SRM 51-30-02.SDR F3LA200100131Rivet · looseDURING C-7 CHECK, INSPECTION REPORTED RT WING NR 5 SLAT HAD WORKING RIVETS ON INNER SKIN NEXT TO ACTUATOR CUTOUT. REPLACED FASTENERS PER SRM 51-30-2.SDR F3LA200100052Outflow Valve · obstructedAIR TURNBACK. FLT CREW REPORTED PRESSURIZATION NORMAL THROUGH 10,000 FT ACFT WENT TO STANDBY MODE AND CABIN PRESSURE CONTINUED TO CLIMB. SET STANDBY MODE AT 5.6 PSI AND CABIN STILL CONTINUED TO CLIMB. MANUALLY CLOSED OUTFLOW VALVE AND SUBSEQUENTLY OXYGEN SDR F3LA200100037Relief Valve · failedAIR TURNBACK. FLIGHT CREW REPORTED FUEL LEAK FROM LT WING ON TAKEOFF AND CLIMB. FOUND LT WING SURGE TANK RELIEF VALVE FAILED OPEN AND REPLACED SAME PER MM 28-13-41.SDR F3LA200100012Housing · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON RT WING INSPECTION LIGHT HOUSING MATING SURFACE BETWEEN HOUSING AND FUSELAGE SKIN. REPLACED RT WING INSPECTION LIGHT HOUSING PER SRM 51-30-02.SDR F3LA200100011Web · corrodedDURING C-7 CHECK, INSPECTION REPORTED AFT CARGO DOOR SCUFFPLATE WEB CORRODED. REPLACED STRAP PER SRM 51-30-2 AND DRAWING NR 65-47957.SDR F3LA200100016Strap · corrodedDURING C-7 CHECK, INSPECTION REPORTED AFT CARGO COMPARTMENT FLOOR NUT PLATE STRAP AT STA 770 CORRODED. REPLACED STRAP PER SRM 51-10-2.SDR F3LA200100015Shear Tie · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON SHEAR TIE AT STA 500A BETWEEN STR 27L AND 26L. FABRICATED AND INSTALLED REPLACEMENT SHEAR TIE PER SRM 53-10-2, SRM 53-10-4, SRM 51-30-2 AND SOPM 20-41-02.SDR F3LA200100007Shear Tie · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER TO FRAME TIE CLIP IN FORWARD CARGO COMPARTMENT STA 540, STR 25L. FABRICATED AND INSTALLED REPLACEMENT TIE CLIP PER SRM 53-10-2, 51-30-4 AND 51-30-2.SDR F3LA200100003Window · looseAIR TURN BACK. FLIGHT CREW REPORTED PRESSURIZATION LEAK AT R-1 WINDOW, WHICH HAD BEEN REPLACED THE PREVIOUS NIGHT. RETURNED TO ELP WITHOUT INCIDENT. MAINTENANCE RETORQUED AND RESEALED R-1 WINDOW.SDR F3LA200100149Fitting · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON R-2 DOOR AFT FITTING, BOTTOM SIDE OF WEB AT STA 986. FABRICATED AND REPLACED WEB AT THRESHOLD OF R-2 DOOR AT STA 947 TO 986 PER SRM 53-20-1 AND 53-30-2.SDR F3LA200100002Fairing · crackedDURING C-7 CHECK, INSPECTION REPORTED A 1/2 INCH CRACK ON INSIDE AFT CORNER OF NR 2 ENGINE INBOARD FIXED FAIRING. MAINTENANCE REMOVED DAMAGED GUSSET AND "L" ANGLE AND FABRICATED AND INSTALLED REPLACEMENT PARTS PER SRM 54-10-2, 51-10-2 AND 51-30-2.SDR F3LA200000276Light · corrodedDURING C-7 CHECK, INSPECTION REPORTED LT. WING INSPECTION LIGHT HOUSING CORRODED AROUND OUTER PERIMETER OF MATING SURFACE TO FUSELAGE SKIN AT STA. 500B INSIDE AIRCRAFT. MAINTENANCE REMOVED LIGHT HOUSING AND CLEANED, TREATED AND PRIMED AREA. INSTALLED NEW LIGSDR F3LA200000274Angle · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION UNDER AFT CARGO COMPARTMENT SUPPORT ANGLE THRESHOLD. MAINTENANCE REPLACED AFT CARGO COMPARTMENT SUPPORT ANGLE UNDER THRESHOLD PER SRM 51-30-2 AND DRAWING NO. 69-43233.SDR F3LA200000027Angle · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION UNDER AFT CARGO COMPARTMENT SUPPORT ANGLE THRESHOLD. MAINTENANCE REPLACED AFT CARGO COMPARTMENT SUPPORT ANGLE UNDER THRESHOLD PER SRM 51-30-2 AND DRAWING NO. 69-43233.SDR F3LA200000270Intercostal · corrodedDURING C-7 CHECK, INSPECTION REPORTED FLOOR INTERCOSTAL CORRODED FROM STA. 947.6 TO 967, RBL 8". REPLACED FLOOR INTERCOSTAL PER SRM 53-10-9 AND 51-10-2.SDR F3LA200000269Intercostal · crackedDURING C-7 CHECK, INSPECTION REPORTED CRACK IN WEB BETWEEN STA. 344 AND STA. 360, STR. 16L. MAINTENANCE REMOVED DAMAGED AREA AND FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 51-40-2.SDR F3LA200000268Angle · crackedDURING C-7 CHECK, INSPECTION REPORTED ANGLE CRACKED UNDER WING-TO-BODY FAIRING AT STA. 540, STR. 22-R. MAINTENANCE STOP DRILLED CRACKS, FABRICATED AND REPLACEMENT ANGLE PER SRM 51-30-02.SDR F3LA200000267Web · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION UNDER AFT CARGO COMPARTMENT THRESHOLD IN THE FRAME AREA (UNDER KICK PLATE). MAINTENANCE REMOVED CORROSION, TREATED AND PRIMED AREA PER SRM 53-10-1.SDR F3LA200000266Stringer Clip · crackedDURING C-7 CHECK, INSPECTION REPORTED STRINGER TIE CLIPS CRACKED AT STA. 1040, STRINGERS 13L, 14L, 15L AND 16L. REPLACED STRINGER CLIPS PER SRM 51-10-2 AND 51-30-2.SDR F3LA200000265Stringer · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION ON STRINGER 27L AT STA. 510A, FORWARD CARGO PIT. MAINTENANCE FABRICATED REPLACEMENT STRINGER AND INSTALLED IN ACCORDANCE WITH SRM 53-10-3 AND SRM 51-30-2.SDR F3LA200000264Shear Tie · corrodedDURING C-7 CHECK, INSPECTION REPORTED CORROSION AND CRACK ON SHEARTIE AT STA. 500, STRINGER 25R, AFT OF FORWARD CARGO DOOR, LOWER CORNER. MAINTENANCE REMOVED DAMAGED AREA AND REPAIRED IN ACCORDANCE WITH SRM 53-10-4.SDR F3LA200000262Indicator · out of positionUPON ARRIVAL, MAINTENANCE REPORTED R-2 DOOR SLIDE INDICATOR NOT IN VIEW. REPLACED R-2 DOOR SLIDE.SDR EF2R2000317Web · corrodedDURING ROUTINE INSPECTION, FLOOR WEB AT BS995, LBL 43 WAS FOUND CORRODED BEYOND ALLOWED LIMITS. REMOVED DAMAGED WEB, FABRICATED REPLACEMENT WEB, INSTALLED.SDR EF2R2000316Attach Fitting · crackedDURING ROUTINE INSPECTION, LEFT MAIN LANDING GEAR BEAM WING SPAR ATTACH FITTING WAS FOUND CRACKED AT THE SECOND FROM OUTBOARD HOLE. REMOVED AND REPLACED LEFT MAIN LANDING GEAR BEAM WING SPAR ATTACH FITTING.SDR EF2R2000315Rib · crackedDURING ROUTINE INSPECTION, THERT HORIZONTAL STABILIZER LEADING EDGE, 3RD RIB FROM OB END WAS FOUND CRACKED AT UPPER AFT END. REMOVED RIB, STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR. REINSTALLED RIB.SDR EF2R2000314Fairing · crackedDURING ROUTINE INSPECTION, THE NR2 ENGINE THRUST REVERSER OB ACTUATOR FAIRING WAS FOUND CRACKED. REMOVED FAIRING, STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR, REINSTALLED FARING.SDR EF2R2000313Bulkhead · crackedDURING ROUTINE INSPECTION, THE BS 178 BULKHEAD WEB WAS FOUND TO BE CRACKED AT LBL 8, WL 218. CUT OUT DAMAGED AREA. FABRICATED AND INSTALLED WEB.SDR EF2R2000312Frame · crackedDURING ROUTINE INSPECTION, THE BS 178 BULKHEAD VERTICAL CHORD AT LBL 5.7 WAS FOUND TO BE CRACKED AT WL 184 IB RADIUS. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR.
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