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 USAASB01224Outflow Valve · failedPIT - FLT 1146 - EN ROUTE FROM PHL TO CMH, AT FL350, THE CABIN ALTITUDE WARNING HORN SOUNDED. CREW NOTICED CABIN ALTITUDE AT 11,000 FEET. CREW WAS UNABLE TO CONTROL CABIN ALTITUDE, DESCENDED TO 10,000 FEET PER QUICK REF HANDBOOK PROCEDURES. FLIGHT DIVERTED SDR USAA011066Skin · crackedTPA - FOUND 1 INCH CRACK IN SKIN AFT OF EQUIPMENT COOLING EXH, LOWER LOBE SKIN BETWEEN S28L AND 28R STATION 380. INSTALLED DOUBLER PER TYPICAL REPAIR 53-30-07, SB 737-53-1117 REV 1. (M)SDR USAASB01222Transmitter · faultyORD - FLT 537 - A TRAILING EDGE FLAP ASYMMETRY OCCURRED ON APPROACH TO ORD FROM CLT. LEFT FLAP INDICATED 1 UNIT WHILE RIGHT FLAP INDICATED 1.5 UNITS. CREW DECLARED AN EMERGENCY, ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND COMPLETED A FLAPS 1 LANDING WITHOSDR USAA010963Skin · crackedCLT - FOUND STAB LOWER SKIN CRACKED 1.5 INCH, RIGHT STAB, STAB STATION 66.5 TO 110. DAMAGE REMOVED, FILLER AND DOUBLER INSTALLED PER TYPICAL REPAIR 55-10-07 REV A. (M)SDR USAASB01218Power Unit · failedCLT - DURING ANNUAL OPERATIONAL CHECK OF THE FORWARD RIGHT SERVICE DOOR ESCAPE SLIDE, THE SLIDE DEPLOYED NORMALLY BUT THE SLIDE MOUNTED EMERGENCY LIGHTS FAILED TO ILLUMINATE. SLIDE OPERATIONAL CHECK FAILED. MAINTENANCE FOUND THE POWER UNIT ASSEMBLY FOR THE ESDR SWAA012145Housing · brokenDURING SCHEDULED A1 CHECK, FOUND EMERGENCY EXIT LIGHT BATTERY HOUSING FUSE BROKEN. REMOVED AND REPLACED BATTERY HOUSING PER MM.SDR SWAA012130Fitting · crackedDURING SCHEDULED C3 CHECK, FOUND LH MLG BEAM HANGER FITTING CRACKED AT FWD END. R&R FITTING PER ALM INV. # SWA 10410.SDR USAASB01202Bungee Cord · damagedIND - FLT 461 - EN ROUTE FROM CLT-ORD, AT FL240, THE CABIN ALTITUDE WARNING HORN ACTIVATED AS CABIN ALTITUDE WAS AT 10,000 FT AND CLIMBING. STANDBY PRESSURIZATION WOULD NOT CONTROL CABIN AND SELECTING MANUAL SHOWED OUTFLOW VALVE FULL CLOSED. CREW SELECTED BOSDR USAASB01204Engine · malfunctionedMSY - FLT 239 - EN ROUTE FROM CLT-IAH - AT FL350, THE CREW FELT A JOLT AND THEN A NR 2 ENGINE VIBRATION ALONG WITH A RISE IN EGT. FLIGHT ATTENDANT REPORTED SEEING A FLASH FROM THE NR 2 ENGINE. CREW SHUT DOWN THE NR 2 ENGINE, DECLARED AN EMERGENCY AND DIVERTESDR USAA010867Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 1.25 INCH, BS 887, STRINGER 23R. INSTALLED REPAIR DOUBLER PER SRM 51-00-01. (M)SDR USAASB01197Battery · dischargedDCA - FOUND MID-CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY. (M)SDR USAASB01200Proximity Switch · dirtyDCA - FLT 556 - ON DEPARTURE FROM TPA, EN ROUTE TO DCA, THE RIGHT MLG RED AND GREEN LIGHTS REMAINED ILLUMINATED AFTER GEAR RETRACTION AND GEAR LEVER IN OFF POSITION. CREW ACCOMPLISHED QUICK REF HANDBOOK PROCEDURES AND RECYCLED LANDING GEAR. CREW RECEIVED NORSDR USAA010760Skin · crackedCLT - FOUND SKIN CRACKED 2 INCHES, BS 727E, STRINGER 22R AND 23R. DAMAGE REMOVED, REPAIR DOUBLER AND TRIPLER INSTALLED PER EA 71604. (M)SDR USAA010849Angle · crackedPIT - FOUND ANGLE CRACKED 3 INCHES, STATION 294.5 RIGHT WL 208.1 CREASE BEAM TO FLOOR STRUCTURE. REPLACED ANGLE PER T/R. (M)SDR USAA010854Angle · corrodedPIT - FOUND ANGLE CORRODED 1 INCH BY 18 INCH AREA, FORWARD SIDE FLOORBEAM STATION 270, WL 207.5 COCKPIT ENTRANCE. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED CORRODED HORIZONTAL FLANGE FROM Z-CHORD, REPLACED WITH REPAIR ANGLE PER EA 71097. (M)SDR USAA010852Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 3 INCH BY 6 INCH, NR 2 GALLEY MIDDLE SEAT TRACK STATION 328 GOING AFT. (M)SDR USAA010851Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 3 INCHES BY 6 INCHES, NR 2 GALLEY SEAT TRACK STATION 328 AFT. (M)SDR USAA010850Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 3 INCHES BY 30 INCHES, STATION 328 NR 3 GALLEY 10 INCHES RIGHT OF C/L TO FORWARD SERVICE DOOR. CUT OUT CORROSION OF FLOORBEAM T-CAP, SPLICED IN NEW SECTION PER PER RM 51-40-02. (M)SDR USAA010848Beam · corrodedPIT - FOUND BEAM CORRODED IN THREE AREAS 1 INCH BY 1 INCH, STATION 208.1 RIGHT UNDER GALLEY NR 1. CORROSION LEVEL 1, TASK NR C53-107-01. CLEANED AND TREATED PER C/N 53-46-53500-C-005. (M)SDR USAA010759Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCH, BS 727D, STRINGER 23R. DAMAGE REMOVED,INSTALLED REPAIR DOUBLER PER SRM 53-00-01, FIG 202. (M)SDR USAASB01182Battery Pack · inoperativePIT - MAINTENANCE FOUND THE AFT GALLEY OVERHEAD EMERGENCY EXIT LIGHT, RIGHT SIDE, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)SDR DL733011038Skin · puncturedFUSELAGE / SKIN / FS 277-295 / STRG. 19R-20R : GROUND DAMAGE CUTOUT REPAIR THE FUSELAGE SKIN BETWEEN FS 277 & 295 AT STRINGERS 19R & 20R WAS STRUCK BY GROUND EQUIPMENT RESULTING IN A PUNCTURE AND SEVERAL DENTS ANSDR USAA010810Skin · crackedPIT - FOUND SKIN CRACKED 2.75 INCH, STRINGER 23 BS 727D-E. DOUBLER REPAIR PER SRM 53-30-00 PAGE 201, FIG 201. (M)SDR USAA010747Skin · crackedPIT - FOUND SKIN CRACKED 2.75 INCH, STRINGER 23 BS 727DE. REPAIRED PER SRM 53-30-00 WITH DOUBLER MEASURING 16 BY 10.5 PER WRM 53-30-00 PAGE 201, FIG 201. (M)SDR USAA010680Bulkhead · dentedCLT - FOUND BULKHEAD WEB DENTED 3 INCHES BY .5 INCH, BS 1016 WL 156, RBL 51. DAMAGED REMOVED, INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-80-08, FIG 201. (M)SDR USAA010862Support · corrodedPIT - FOUND CARGO PANEL SUPPORT ANGLE CORRODED 1 INCH BY 3 INCH, STATION 787 FROM S19L TO S24L. BLENDED PER 53-00-07. (M)SDR USAA010861Support · corrodedPIT - FOUND SUPPORT CORRODED 1 INCH BY 1 INCH, STATION 967-986 AND 18.25 RBL. CORROSION LEVEL 1. REPLACED WITH PART NR 65-46812-169. (M)SDR USAA010860Floorbeam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 4 INCHES, BS 967 UPPER T-CAP. CORROSION LEVEL 1. REPLACED PER 53-00-51. (M)SDR USAA010859Beam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 36 INCH AREA, BS 986.6. CORROSION LEVEL 1. REPAIRED PER TR 53-10-05, BAC 1505-100880. (M)SDR USAA010806Skin Panel · crackedPIT - FOUND BULKHEAD SKIN PANEL CRACKED 1.5 INCH, STATION 178 BULKHEAD WL 201 AND 204 LBL 5.7. CUT OUT, INSTALLED DOUBLER PER SRM 53-10-08 FIG 211. (M)SDR USAA010674Attach Angle · crackedCLT - FOUND WEB ATTACH ANGLE CRACKED 1 INCH, BS 291, BETWEEN S10R AND S11R. REMOVED AND REPLACED WEB ATTACH ANGLE. (M)SDR USAA010675Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 278, S14R. STOP DRILLED CRACK, INSTALLED DOUBELR PER SRM 51-70-11. (M)SDR USAA010676Skin · crackedCLT - FOUND PYLON/STRUT SKIN CRACKED .75 INCH, NR 1 ENGINE STRUT, PANEL NR 5727 OPENING, OUTBOARD AFT RADIUS. STOP DRILLED CRACK, INSTALLED DOUBLER PER TR 54-30-07. (M)SDR USAA010677Attach Angle · crackedCLT - FOUND ATTACH ANGLE/FITTING CRACKED APPROXIMATELY 6 INCHES, BS 1120, H STAB CENTER SECTION, PRIME AND AUX THRUST BEAM. REMOVED AND REPLACED ATTACH FITTING ANGLE AT INTERSECTION OF PRIMARY, AUX AND THRUST BEAM PER SRM 51-10-02. (M)SDR USAA010672Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S12R AND S13R. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE PER SRM 51-10-02. (M)SDR USAA010673Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, BS 290, INTERCOSTAL BETWEEN S11R AND S12R. REMOVED AND REPLACED INTERCOSTAL ATTACH ANGLE PER SRM 51-10-02. (M)SDR USAA010670Stringer · crackedCLT - FOUND 18A SHELF CRACKED .5 INCH, LEFT WHEEL WELL, BS 725, LBL 62. REMOVED AND REPLACED 18A SHELF PER EA69680 AND SB 737-53-1170. (M)SDR USAA010671Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, BS 330, 4 INCHES ABOVE STRINGER 17R. DAMAGED REMOVED, INSTALLED DOUBLER AND TRIPLER. (M)SDR USAA010663Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 380, STRINGER 8R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA010664Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 867, BETWEEN STRINGERS 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA010665Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, BS 727D. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)SDR USAA010666Door Frame · crackedCLT - FOUND FRAME CRACKED INTERNAL .5 INCH, BS 295, FORWARD SERVICE DOOR CUTOUT, LOWER FORWARD CORNER. INSTALLED REPAIR ANGLES PER SRM 51-70-11. (M)SDR USAA010667Door Frame · crackedCLT - FOUND FRAME REVEAL CRACKED 1 INCH, FORWARD SERVICE DOOR, TOP SURROUND FRAME. REMOVED AND REPLACED FRAME REVEAL. (M)SDR USAA010668Stringer · corrodedCLT - FOUND STRINGER CORRODED APPROXIMATELY .5 INCH, BS 1100, STRINGER 5R. REMOVED DAMAGE, SPLICED IN NEW STRINGER SECTION PER SRM 53-00-03, 51-30-01, 51-40-02. (M)SDR USAA010669Stringer · crackedCLT - FOUND 18A SHELF CRACKED .5 INCH, RIGHT WHEEL WELL, BS 725, RBL 62. REMOVED AND REPLACED 18A SHELF PER EA 69680, AND BOEING DRAWING NR 65-46877. (M)SDR USAASB01172Battery Pack · dischargedPHL - MAINTENANCE FOUND VARIOUS EMERGENCY LIGHTS IN THE FORWARD, MIDDLE AND AFT CABIN INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AT THE FORWARD LEFT, MIDDLE LEFT, AND AFT LEFT SIDE OF CABIN. OPS CHECK GOOD. (M)SDR AWXA0001855Switch · out of adjDEN - ABORTED TAKEOFF - 6/9/01 - FLT 334 - ABORTED TAKEOFF AT APPROX 80 KTS DUE TO AFT ENTRY DOOR WARNING LIGHT CAME ON AND EXTINGUISHED TWICE; BRAKE COOLING COMPLIED. IN DEN MX INSPECTED THE DOOR AND FOUND IT CLOSED AND LOCKED NORMALLY; DETERMINED TO BE AN ISDR USAA010648SkinCLT - FOUND SKIN WITH PREVIOUSLY INSTALLED DOUBLER, 11 INCH BY 12.25 INCH, BS 895-907, STRINGER 16 AND 17L. DOUBLER HAS BEEN INSTALLED PER SRM 53-00-01. (M)SDR USAA010798Trunnion · corrodedPIT - FOUND FITTING HAS CORROSION PITTING, DEEPEST .021 INCH, NOSE GEAR SHOCK STRUT LEFT TRUNNION FITTING. REAMED BORE, INSTALLED SLEEVE PER EA 71444. (M)SDR USAA010805Skin Panel · crackedPIT - FOUND BULKHEAD SKIN PANEL CRACKED 2 INCHES STOP DRILLED, STATION 178 RBL 5.7 WL 201. CUT OUT, INSTALLED DOUBLER PER SRM 53-10-08 FIG 211. (M)
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