Boeing 737-317
Service difficulty reports · 1,542
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 = '737317' 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 = '737317' 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 SWAA050750Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND R1 DOOR SKIN CRACKED AT UPPER DOOR HINGE CUTOUT. REPAIRED SKIN PER SRM & SWA ACO.SDR SWAA050749Skin · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 760, BELOW STR 18R. REPAIRED SKIN PER SWA EA & SRM.SDR SWAA050731Web · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE BEADED WEB CRACKED AT BS 664.5, BETWEEN LBL 30.5 TO LBL 32.0. REPAIRED WEB PER SRM.SDR SWAA050670Bulkhead · crackedDURING SCHEDULED SPECIAL VISIT, FOUND 2 EA FUSELAGE WEB CRACKS AT BS 178 BULKHEAD, BETWEEN LBL 13.5 TO RBL 9 & BETWEEN WL 218 TO WL 234. REPAIRED FUSELAGE WEB PER SRM.SDR SWAA050657Frame · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STUB FRAME AT BS 360, BETWEEN STR 14L & STR 15L. REMOVED AND REPLACED STUB FRAME PER SRM.SDR SWAA050656Keelbeam · corrodedDURING SCHEDULED SPECIAL VISIT, FOUND CORROSION ON LT FUSELAGE KEELBEAM AT BS 540. REPAIRED KEEL BEAM PER SRM & ER.SDR SWAA050648Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 787, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.SDR SWAA050647Frame · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE BELT FRAME CRACKED AT BS 360, STR 14R. REPAIRED BELT FRAME PER SRM.SDR SWAA050624Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND STRINGER CLIP CRACKED AT STR 9L, BS 500A. REMOVED AND REPLACED STRINGER CLIP PER SRM.SDR SWAA050623Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT STR 9L, BS 400. REMOVED AND REPLACED STRINGER CLIP PER SRM.SDR SWAA050622Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.SDR SWAA050621Attach Angle · crackedDURING SCHEDULED SPECIAL VISIT, FOUND FUSELAGE FRAME TO SKIN ATTACH ANGLE CRACKED AT BS 400, STR 14L. REPAIRED FUSELAGE ATTACH ANGLE PER SRM.SDR SWAA050605Stringer Clip · crackedDURING SCHEDULED SPECIAL VISIT, FOUND CRACKED STRINGER CLIP AT BS 807, STR 9R. REMOVED AND REPLACED STRINGER CLIP PER SRM.SDR SWAA050563Fitting · crackedDURING SCHEDULED SPECIAL VISIT, FOUND R1 DOOR ESCAPE SLIDE GIRT BAR, AFT FLOOR FITTING CRACKED. REMOVED AND REPLACED R1 DOOR ESCAPE SLIDE FLOOR FITTING PER MM.SDR SWAA050559Skin · crackedDURING SCHEDULED C3 CHECK, FOUND SKIN CRACK AT BS 737, BELOW STR 19R. REPAIRED SKIN PER SRM.SDR 375PA0035Valve · crackedRIGHT ENGINE PRE-COOLER VALVE CRACKED. REPLACED PER-COOLER VALVE PER MM 36-12-35.SDR 375PA0042Floor Support · crackedAFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D + 7 AT RBL 3. REPAIRED PER SRM 53-00-53.SDR 375PA0041Floor Support · corrodedAFT CARGO FLOOR PANEL SUPPORT ANGLE HAS CORROSION AT BS 727D +7 AT RBL 7. REPAIRED PER SRM 53-00-53.SDR 375PA0039Floor Support · crackedAFT CARGO FLOOR PANEL SUPPORT ANGLE CRACKED AT NUT PLATE AT BS 727D +7 AT LBL 3. REPAIRED PER SRM 53-00-53.SDR 375PA00355Valve · failedRIGHT ENGINE PRECOOLER VALVE CRACKED. REPLACED PRECOOLER VALVE PER MM 63-12-35.SDR 375PA0032Keelbeam · corrodedCORROSION ON THE I/B SIDE OF THE RIGHT KEEL BEAM FORWARD OF BS 540. REPAIRED PER EA 53-028.SDR 375PA0031Keelbeam · corrodedCORROSION ON HORIZONTAL FLANGE OF THE RIGHT KEEL BEAM AT BS 520 AT RBL 6.5. REPAIRED PER EA 53-030.SDR 375PA0030Splice · corrodedSTRINGER 28 LT SPLICE IS CORRODED AT BS 907. REPLACED STRINGER SPLICE PER SRM 51-10-02 AND 51-40-02.SDR 375PA0026APrecooler · crackedRIGHT ENGINE PRECOOLER CRACKED IN O/B UPPER FORWARD CORNER. WELDED PER BAC SPEC 5975.SDR SWAA050486Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 737, STRINGER 19R, CRACKED. REPAIRED SKIN PER SRM.SDR SWAA050453Lens · brokenDURING SCHEDULED C3 CHECK, FOUND R2 DOOR OVERHEAD EMERGENCY EXIT LIGHT LENS, BROKEN. REMOVED AND REPLACED LIGHT LENS PER MM.SDR SWAA050452Skin · crackedDURING SCHEDULED C3 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS FROM BS 500D, BS 520, STRINGER 12R. REPAIRED SKIN PER EA.SDR SWAA050433Glowstrip · delaminatedDURING SCHEDULED A1 CHECK, FOUND 2 EACH SECTIONS OF EMERGENCY EXIT PHOTOLUMINESCENT STRIPS IN FWD CABIN, DELAMINATED. REMOVED AND REPLACED PHOTOLUMINESCENT STRIPS PER MM.SDR SWAA050326Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 747, STRINGER 21R, CRACKED. REPAIRED SKIN PER SRM.SDR SWAA050287Battery · inoperativeDURING SCHEDULED SERVICE CHECK, FOUND FWD CABIN EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PER MM.SDR SWAA050189Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 482, STRINGER 10R, CRACKED. REPAIRED SKIN PER SRM.SDR SWAA050061Skin · crackedDURING SCHEDULED C3 CHECK, FOUND FUSELAGE SKIN AT BS 752, STRINGER 24L, CRACKED. REPAIRED SKIN PER EA.SDR SWAA043686Skin · crackedDURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 294.5 + 16, STRINGER 18R, CRACKED. REPAIRED SKIN PER EA.SDR SWAA043685Skin · crackedDURING SCHEDULED A2 CHECK, FOUND FUSELAGE SKIN AT BS 518, STRINGER 12R, CRACKED. REPAIRED SKIN PER EA.SDR SWAA043629Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 885, ABOVE STRINGER 24R, CRACKED. REPAIRED SKIN PER EA.SDR F3LA200400113Pitot Head · obstructedREJECTED TAKEOFF, FLIGHT CREW REPORTED NR 2 AIRSPEED INDICATOR WOULD NOT INDICATE AIRSPEED. FLUSHED FIRST OFFICER'S UPPER RIGHT PITOT PROBE FROM DISCONNECT AT NR 2 AIR DATA COMPUTER. NR 2 AIRSPEED INDICATOR, OPS CHECKED NORMAL PER MM 34-11-00.SDR SWAA042842Skin · crackedDURING SCHEDULED C2 CHECK, FOUND 2 EACH FUSELAGE SKIN CRACKS AT BS 500A + 2, STRINGER 10R, BS 500A + 10, STRINGER 10R. REPAIRED SKIN PER SRM.SDR SWAA042841Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN AT BS 777, STRINGER 24L, CRACKED. REPAIRED SKIN PER SRM.SDR SWAA042768Battery · inoperativeDURING SCHEDULED A1 CHECK, FOUND RT FWD SIDEWALL EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PER MM.SDR SWAA042633Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.SDR SWAA042614Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN AT BS 767, STRINGER 20L, CRACKED. REPAIRED SKIN PER EA.SDR F3LA200400088Skin · damagedDURING C-2 CHECK, INSPECTION REPORTED SKIN REPAIR AT BS 917, STR. 20L, REPAIR DOCUMENTATION NOT SATISFACTORY TO LEASOR. REMOVED EXISTING FUSELAGE REPAIRS AT BS 927 AND BS 896 COMMON TO STR. 20L. ENLARGED CUTOUTS TO INCLUDE FASTENER HOLE FROM PREVIOUS REPAIRSSDR F3LA200400087Keelbeam · corrodedDURING C-2 CHECK, INSPECTION REPORTED KEELBEAM CORRODED AT STA 520 WHERE IT ATTACHES TO STRINGER 28-R. INSTALLED REPAIR TO RT. KEELBEAM AT CORRODED AREA BETWEEN BS 500D AND 520 IAW EA B3-53R-10478.SDR F3LA200400086Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON OTBD SIDE OF LBL 5.7 BELOW WL 207 ON 178 BULKHEAD. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 PER EA B3-53R-10470 AND SRM 53-10-08 FIG 210.SDR F3LA200400085Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACKS ON 178 BULKHEAD AT IB SIDE OF LBL 5.7 VERTICAL CORD AND BELOW WL 207. REPAIRED CRACKS ON 178 BULKHEAD BELOW WL 207 IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210.SDR F3LA200400084Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED TWO CRACKS AT BL 0, ABOVE WL 184.5 AT 188.0, 178 BULKHEAD. REPAIRED CRACKS AT BL 0 ABOVE WL 184.5 IAW SRM 53-10-08, FIG. 211, DETAIL VIII AND EA B3-53R-10470.SDR F3LA200400083Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7 VERTICAL CORD AND ABOVE WL 207. REMOVED DAMAGE FROM BULKHEAD AT BS 178 AT IB SIDE OF LBL 5.7. FABRICATED REPAIR DOUBLER AND INSTALLED IAW SRM 53-10-08.SDR F3LA200400082Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD, RBL 5.7, BELOW WL 207 IB OF RBL 5.7 AT LOWER RADAR ANTENNA MOUNT. PERFORMED REPAIR IAW EA B3-53R-10470 AND SRM 53-10-08, FIG. 210, DETAIL VII.SDR F3LA200400081Bulkhead · crackedDURING C-2 CHECK, INSPECTION REPORTED CRACK ON 178 BULKHEAD ON O/B SIDE OF RBL 5.7 ABOVE WL 207. REMOVED DAMAGE, FABRICATED REPAIR PARTS, TREATED, PRIMED AND INSTALLED PER EA B3-53R-10470 AND SRM 53-10-08, FIG 210, DETAIL 3.SDR F3LA200400080Bulkhead · scratchedDURING C-2 CHECK, INSPECTION REPORTED CRACK AT 178 BULKHEAD O/B OF RBL 5.7 AT WL 218. DETERMINED TO BE A SCRATCH, NOT A CRACK. FOUND TO BE OUT OF LIMITS. REMOVED DAMAGE, FABRICATED DOUBLER, TREATED, PRIMED AND INSTALLED REPAIR PER EA B3-53R-10470 AND SRM 53
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