Boeing 737-301
Service difficulty reports · 4,797
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 = '737301' 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 = '737301' 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 USAA990757Bulkhead Web · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5 WL 200 WEB. INSTALLED DOUBLER PER TR 53-10-07 REV A. (X)SDR USAA990756Bkhd Intercostal · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 25, WL 195 INTERCOSTAL. REPAIRED PER TR 53-10-18. (X)SDR USAA990755Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 787 BETWEEN STR 8 AND STR 9R. INSTALLED DOUBLER PER EA 65040. (X)SDR USAA990754Bulkhead · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5, WL 204 WEB. FABRICATED DOUBLER AND FILLERS PER SRM 53-10-07 AND 08. (M)SDR USAA990753Bulkhead Angle · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5.5, WL 188 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-1-08 FIG 205, SHEET 12. (X)SDR USAA990752Bulkhead Angle · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A 1 INCH CRACK AFT SIDE PRESSURE BULKHEAD BS 178, LBL 5.7, WL 181 T-ANGLE. FABRICATED 2 ANGLES AND 1 STRAP PER SRM 53-10-08 FIG 205 SHEET 12. (X)SDR USAA990751Skin · crackedCLT - DURING Q-1 CHECK VISUAL AND EDDY CURRENT INSPECTION, FOUND A .75 INCH CRACK AND 5 INCH CRACK IN SKIN AROUND PANEL 5724L. INSTALLED DOUBLER PER TR 54-40-040. (X)SDR USAA990711Clip · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK AT STRINGER TIE CLIP STA 616 STR 2R. INSTALLED DOUBLER PER SRM 53-00-03. (X)SDR USAA990709Angle · corrodedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND CORRODED AREA VARIOUS SIZES AND PLACES ON Z-ANGLE/GIRT BAR MOUNTS FORWARD ENTRY DOOR AT BS 312 TO BS 344. INSTALLED NEW Z-ANGLE AND GIRT BAR MOUNTS PER SRM 51-40-02 AND SRM 53-10-15. (X)SDR USAA990708Tie Clip · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 616 STR 1 TIE CLIP. INSTALLED NEW CLIP PER SRM 51-10-02. (X)SDR USAA990707Skin · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK FORWARD SERVICE DOOR AFT LOWER CUT-OUT BS 324, WL 211 SKIN. INSTALLED DOUBLER AND FILLERS PER SRM 53-10-01. (X)SDR USAA990706Floorbeam · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK 1.5 INCHES AFT OF STA 663.75 AT BL ZERO BEAM (FRAME). INSTALLED FLOORBEAM REPAIR PER EA 64999 AND BOEING SB 737-57-1210 FIG 4 AND 8. (X)SDR USAA990679Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 400 BETWEEN STR 8R AND STR 9R. INSTALLED DOUBLER PER SRM 53-00-07. (X)SDR USAA990678Web · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT LBL 25 WEB AT HOLES 707, 708, 709, 710, AND 713, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (X)SDR USAA990677Skin · crackedDLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK UPPER AFT CORNER OF CUT-OUT FOR ACCESS TO EXTERNAL DOOR HANDLE AFT CARGO DOOR EXTERIOR SKIN. REMOVED DAMAGED AREA AND INSTALLED DOUBLER PER SRM 52-00-3. (X)SDR USAA990676Frame · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK IN FUSELAGE FRAME AT FASTENER HOLE BS 480 BETWEEN STR 8 AND STR 9L. CUT-OUT DAMAGED AREA AND INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X)SDR USAA990675Beam · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK LOWER WEB OF RBL 25 AT STA 712 WL 203 BEAM. INSTALLED DOUBLER PER SRM 51-70-13. (X)SDR USAA990674Web · crackedCLT - DURING A Q-1 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK SHEAR WEB LOWER CHORD STA 305.5 STR 4L. INSTALLED DOUBLER PER SRM 51-70-11.SDR USAA990661Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9L IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER. (X)SDR USAA990660Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 480 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. FABRICATED REPAIR ANGLE AND FILLER INSTALLED DOUBLER PER SRM 53-00-07 FIG 202. (X)SDR USAA990659Frame · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 807 BETWEEN STR 8 AND STR 9R IN FUSELAGE FRAME AT FASTENER HOLE. INSTALLED DOUBLER PER SRM 53-00-07. (X)SDR USAA990658Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK AT STA 616 STR 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (X)SDR USAA990657Tie Clip · crackedCLT - DURING Q-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT BS 1006 AT FIRST STRINGER ABOVE FLOOR LEVEL ON RT SIDE TIE CLIP. REPLACED WITH IDENTICAL PART. (X)SDR SWAA991266Light · burnedAIR TURNBACK, 10 MINS AFTER TAKEOFF F/A REPORTED AN ELECTRICAL ODOR AT MID CABIN. FOUND SIDEWALL LIGHT AT ROW 7 ABC AND 8 ABC BURNED INTERNALLY. REMOVED AND REPLACED LIGHT ASSY PER MM.SDR F3LA99107Support · corrodedDEN - DURING C-CHECK, INSPECTION REPORTED LEFT MAIN LANDING GEAR FORWARD UPLOCK SUPPORT SHAFT LUG CORRODED, STA 685. MAINTENANCE REPLACED NR 1 MAIN LANDING GEAR PER MM 32-11-00. TC: 15,691. (X)SDR USAA990791Stringer · crackedCLT - DURING Q3 CHECK, FOUND .75 INCH CRACK AT BS 727 STRINGER 18A WEB S18AL. REPAIRED WITH REPLACEMENT REF SB 737-53-1170. (M)SDR USAA990790Frame · crackedCLT - DURING Q3 CHECK, FOUND VARIOUS 1 INCH AREAS OF CORROSION AT NUTPLATE HOLES IN FRAME/WEB AT BS 605 TO 845 STRINGER 25R TOP FLANGE. REPLACED WITH IDENTICAL PART NUMBER. (M)SDR USAA990789Intercostal · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT STATION 178, 195 INTERCOSTAL RT SIDE. REPLACED WITH IDENTICAL PART NUMBER. (M)SDR USAA990788Post · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CAPTAINS UPPER O/B CORNER OF EXTERIOR WINDSHIELD (POST). INSTALLED EXTERNAL DOUBLER PER EA 64979. (M)SDR USAA990787Skin · crackedCLT - DURING Q3 CHECK, FOUND 3 CRACKS ONE 1.375 INCH, TWO .5 INCH ON SKIN AT NR 1 L/E SLAT. INSTALLED REPAIR DOUBLER PER TYPICAL REPAIR 57-50-01 REV 'H'. (M)SDR USAA990786Clip · crackedCLT - DURING Q3 CHECK, FOUND .25 INCH CRACK AT TIE CLIP AT STATION 663 S10L. REPLACED WITH IDENTICAL PART PER SRM 51-10-2. (M)SDR USAA990785Skin · crackedCLT - DURING Q-3 CHECK, FOUND .5 INCH CRACK E/E COOLING DUCT OUTLET INNER FUSELAGE FUSELAGE SKIN AT BS 380 BL 0. INSTALLED EXTERNAL FUSELAGE SKIN DOUBLER 23 INCH BY 40 INCH PER TR 53-30-07 AND BOEING DWG NR 65C33930. (M)SDR USAA990784Angle · crackedCLT - DURING Q3 CHECK, FOUND 1 INCH CRACK AT CREASE BEAM INNER CHORD ANGLE BS 294.5 RBL 45 WL 208. INSTALLED CHORD ANGLE PER SRM 51-10-02. (M)SDR USAA990783Splice · crackedCLT - DURING Q3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4LT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)SDR USAA990782Splice · crackedCLT - DURING Q-3 CHECK, FOUND .250 INCH CRACK AT BS 908 STRINGER SPLICE STRINGER 4RT. REPLACED STRINGER SPLICE WITH IDENTICAL PART. (M)SDR USAA990781Frame · crackedCLT - DURING Q3 CHECK, FOUND .125 INCH CRACK IN FRAME AT STATION 616 RBL 64 WL 201 INBOARD CHORD ANGLE. INSTALLED REPAIR FILLER AND STIFFENING ANGLE PER EA 65007 TR 53-10-23 (737-200). (M)SDR USAA990780Frame · crackedCLT - DUIRNG Q-3 CHECK, FOUND .25 INCH CRACK IN FRAME AT BS 480 S9R. INSTALLED DOUBLER PER EA 65009. (M)SDR USAA990779Tie Clip · crackedCLT - DURING Q3 CHECK, FOUND TIE CLIP CRACKED IN HALF. ALSO, FOUND STRINGER CRACKED BELOW CLIP LOCATION, STATION 616, S-4L. INSTALLED STRINGER DOUBLER PER SRM 53-00-03 FIG 204 AND FABRICATED TIE CLIP AND INSTALLED PER SRM 51-10-1. (M)SDR USAA990772Stringer · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 4 INCH AREA OF CORROSION AT STATION 727A PLUS 14 INCHES, STRINGER 26L. CORROSION TASK NR C53-202-01, CORROSION LEVEL 2. INSTALLED FABRICATED STRINGER REPAIR CHANNEL ANDRADIUS FILLERS PER SRM 53-00-03 FIG 201. (SDR USAA990771Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 6 SQUARE INCH OF CORROSION MED Z-ANGLE UPPER SURFACE. CORROSION LEVEL 2. REPLACED Z-ANGLE PER SRM 51-10-02. (M)SDR USAA990770Stabilizer Link · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION RIGHT GEAR STABILIZER LINK ATTACH POINTS. CORROSION LEVEL 2. REMOVED AND REPLACED STABILIZER LINK PER MM 32-32-93 AND 32-13-21. (M)SDR USAA990769Angle · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND CORROSION AT BS 957 AND 987, LBL 45, WL 208 CREASEBEAM INNER CHORD ANGLE. CORROSION LEVEL 2, CORROSION TASK NR C53-107-02. INSTALLED NEW CHORD ANGLE PER SRM 51-40-02. (M)SDR USAA990768Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 6L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)SDR USAA990729Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .50 INCH CRACK FRAME 312 AT STR 5L. CRACK TRIMMED OUT AND DOUBLER INSTALLED PER SRM 53-00-07 FIG 202 AND EA 65075. (X)SDR USAA990728Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .500 INCH CRACK MAIN ENTRY DOORWAY UPPER HINGE H-STRAP DOORWAY FRAME. FABRICATED AND INSTALLED NEW H-STRAP PER SRM 51-10-02 AND BOEING DWG 90-7822. (X)SDR USAA990727Angle · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AT AFT END STA 360 STR 14L SHEARBEAM OUTBOARD CHORD ANGLE. REPAIRED PER BOEING DWG NR 69-48985/51-10-02. (X)SDR USAA990726Frame · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK AFT ENTRY DOOR CUT-OUT FRAME UPPER FORWARD SECTION AT BOTTOM HOLE FORWARD EDGE FRAME. INSTALLED DOUBLER PER SRM 51-70-11. (X)SDR USAA990725Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STA 639 STR 4L TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (X)SDR USAA990724Tie Clip · crackedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 639 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)SDR USAA990723Tie Clip · crackedCLT - DURIGN Q-3 CHECK VISUAL INSPECTION, FOUND A CRACK AT STATION 616 STRINGER 4R TIE CLIP. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)
Back to Boeing 737-301