Boeing 737-3B7
Service difficulty reports · 4,722
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 = '7373B7' 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 = '7373B7' 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 USAA001320Clip · crackedCLT - FOUND CLIP CRACKED 1 INCH, STRINGER 5R AND FS 1104. REPAIRED PER SRM 51-40-00 AND 51-10-2. (M)SDR USAA001319Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178 RBL .5, WL 188. INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-10-08. (M)SDR USAA001304Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH IN 4 PLACES, FLOORBEAM WEB AT RBL 24.75 FROM FS 706 TO FS 711. CUTOUT DAMAGED AND INSTALLED DOUBLER PER EA 67780. (M)SDR USAA001303Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, INBOARD CHORD OF FRAME 616 AT WL 200 LT SIDE. INSTALLED FILLER AND STIFFENING ANGLE PER TR 53-62-01. (M)SDR USAA001302Skin · crackedCLT - FOUND SKIN AND DOUBLER CRACKED .5 INCH, RIGHT PYLON PANEL CUTOUT 5824R. FABRICATED AND INSTALLED DOUBLER PER EA 67781 AND TR 54-50-07. (M)SDR USAA001305Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 1 INCH IN FOUR PLACES, FLOORBEAM WEB AT LBL 24.75 FROM FS 706 TO FS 711. REMOVED AND REPLACED SECTION OF WEB AND INSTALLED DOUBLER PER EA 67780. (M)SDR USAA001301Stringer · corrodedCLT - FOUND STRINGER CORRODED .5 INCH BY 8 INCHES, STRINGER 25L BETWEEN FS 967 AND FS 986.5. REPAIRED STRINGER SPLICE PER SRM 53-00-03. (M)SDR USAA001300Frame · corrodedCLT - FOUND FRAME CORRODED 1 INCH BY 6 INCHES, FRAME 967 BETWEEN S24L AND S25L. INSTALLED DOUBLER AND NEW SHEAR PER SRM 53-00-07 FIG 205. (M)SDR USAASB00226Controller · malfunctionedPBI - FLT 855 - FLIGHT CREW ADVISED OVER ACARS OF AN ABNORMAL FLAP LANDING. CREW COULD NOT EXTEND FLAPS PAST 8 DEGREES. LEADING EDGE DEVICES EXTENDED, HOWEVER, TRAILING EDGE DID NOT. ALTERNATE FLAP SYSTEM FAILED ALSO. CREW DECLARED AN EMERGENCY INTO PBI ANSDR AWXA0000621Downlock Sensor · failed21AUG ON SHORT FINAL, RIGHT MAIN GEAR GREEN LIGHT FLICKERED RED/GREEN AND THE WARNING HORN SOUNDED INTERMITTENTLY. GEAR RECHECKED, DID GO-AROUND, TOWER OBSERVATION ACCOMPLISHED. UNEVENTFUL LANDING. 22 AUG, ON APPROACH, RIGHT MAIN GEAR LIGHT FLICKERED RED/GRSDR USAASB00228Light · inoperativeALB - DURING OVERNIGHT MAINTENANCE CHECK, MAINTENANCE FOUND THE FORWARD CABIN EMERGENCY LIGHTS DIM DURING OPERATIONAL CHECK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AND CHARGER ASSEMBLY WITH NO HELP. FOUND MAIN ENTRY DOOR EMERGENCY EXIT IDENTIFIER SDR USAASB00222Probe · faultyJFK - FLT 1849 - AFTER TAKEOFF FROM LGA, AT 6,000 FEET, THE NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED WITH THE EGT GAUGE FLUCTUATING. THE NEEDLE ON THE GAUGE WOULD SPIKE UP AND DOWN BETWEEN 1150-1295 DEGREES. THE NEEDLE THEN BECAME STUCK AT 1295 DEGREES. DUE TSDR USAASB00220Control Cable · out of adjMCO - FLT 808 - AFTER TAKEOFF FROM MCO, CREW WAS UNABLE TO RAISE LANDING GEAR. THE GEAR SELECTOR LOCKED AT MID-POINT. UPON FLAP TO ZERO, THE WARNING HORN BEGAN SOUNDING. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARESDR USAA001285Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 24 INCHES, LBL 56, S 294.5 TO S 360. REPLACED Z-ANGLE PER SRM 51-40-02/05/08. (M)SDR USAA001288Mount · corrodedCLT - FOUND ANTENNA MOUNT CORRODED 1 INCH BY 5 INCHES, BETWEEN STATION 727D AND 727E, BL 0. CORROSION LEVEL 1. INSTALLED DOUBLER AND ANGLE PER SRM 53-00-01. (M)SDR USAA001287Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 31 INCHES, STATION 328. INSTALLED DOUBLER T-CAP PER SRM 51-10-02 AND 53-10-51. (M)SDR USAA001286Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 20 INCHES, STATION 328. INSTALLED NEW T-CAP AND REPAIR ANGLE PER SRM 51-10-02 AND 53-10-51. CORROSION LEVEL 1. (M)SDR USAA001283Mount · crackedCLT - FOUND FRAME MOUNT CRACKED, 1 INCH BY 1 INCH, STATION 787, RBL 46 FRAME MOUNT HOLES. INSTALLED DOUBLER PER EA 67782. (M)SDR USAA001282Skin · crackedCLT - FOUND FUSELAGE SKIN CRACKED 2 INCHES, STATION 311, WL 210 SERVICE DOOR CUTOUT. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-10-01 FIG 202. (M)SDR USAA001284Pan · corrodedCLT - FOUND PAN CORRODED 3 INCHES BY 5 INCHES, AFT LAV SERVICE PAN INNER SURFACE. FABRICATED NEW PAN AND INSTALLED PER SRM 51-10-02. (M)SDR USAASB00219Solenoid · faultyMCO - FLT 676 - AFTER TAKEOFF FROM MCO, CREW RAISED GEAR HANDLE TO STOW THE GEAR BUT THE HANDLE STOPPED BEFORE REACHING THE GEAR UP POSITION. DURING TROUBLESHOOTING, CREW RECEIVED A WARNING HORN. FLIGHT RETURNED TO FIELD AND LANDED WITHOUT FURTHER INCIDENT. SDR USAASB00218Module · failedBWI - FLT 1924 - APPROX 20 MINS OUT OF ROC, EN ROUTE TO DCA, CREW RECEIVED AN APU DETECTION LIGHT AND A FAULT LIGHT FOR THE ENG FIRE LOOP. CREW ACCOMP FIRE LOOP. CREW ACCOMPLISHED FIRE LOOP TEST PER QUICK REFERENCE HANDBOOK PROCEDURES AND NONE OF THE FIRE LOSDR USAA001250Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH BY 1.5 INCH IN 14 PLACES, STATION 1016 END TO END TOP OF T-CAP. CUT REMOVED AND REPLACED T-CAP PER TR 53-10-05A. (M)SDR USAA001249Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH BY 1 INCH IN TWELVES PLACES, STATION 1006 END TO END TOP. CUT AND REMOVED AND REPLACED T-CAP PER TR 53-10-05A. (M)SDR USAA001251Stringer Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, STRINGER TIE CLIP AT FS 685 AND STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-02. (M)SDR USAA001252Tie Clip · crackedCLT - FOUND TIE CLIP .125 INCH, BS 663, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)SDR USAA001253Stringer · crackedCLT - FOUND SHELF CRACK .5 INCH, LEFT MLG, STRINGER 18A SHELF BS 727 BULKHEAD. INSTALLED NEWS 18A SHELF PER SRM 51-10-02. (M)SDR USAA001257Bulkhead · crackedCLT - FOUND BULKHEAD CRACKED 1 INCH, LOWER LEFT WEATHER RADAR ANTENNA MOUNT SKIN BS 178. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001258Bulkhead · crackedCLT - FOUND BULKHEAD 1 INCH CRACK, LOWER RIGHT WEATHER RADAR ANTENNA MOUNT SKIN BS 178. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001260Web · crackedCLT - FOUND WEB CRACKED .5 INCH, WL 207, RBL 28. REPAIRED PER EA 67735. (M)SDR USAA001261Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL .75, WL 188. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001262Stiffener · crackedCLT - FOUND STIFFENER CRACKED .75 INCH, VERT STIFFENER LBL 5.7 BELOW WL 195. INSTALLED NEW FABRICATED ANGLES PER SRM 51-10-02. (M)SDR USAA001263Bulkhead · crackedCLT - FOUND CRACK IN WEB .5 INCH, BS 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001264Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001265Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER AND FILLER PER SRM 53-10-08. (M)SDR USAA001266Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001267Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 6.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)SDR USAA001248Floorbeam · corrodedCLT - FOUND BEAM CORRODED 1 INCH BY 1 INCH IN 10 PLACES, BS 344, LBL 56 TO RBL 31. INSTALLED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1/ C53-107-02. (M)SDR USAA001246Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 8 INCHES, BS 967, LBL 49 TOP OF FLOORBEAM. INSTALLED UPPER T-CAP PER TR 53-10-05A. (M)SDR USAA001247Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 1 INCH BY 2 INCH IN 12 AREAS, STATION 294, LBL 1. INSTALLED DOUBLER PER SRM 51-40-00 AND 51-10-51. (M)SDR USAA001242Web · crackedCLT - FOUND WEB CRACKED .75 INCH, LEFT MLG W/W PRESS DECK STATION 663, LBL 30. INSTALLED DOUBLER PER TR 53-60-04 FIG 1. (M)SDR USAA001239Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 887, STRINGER 9L INBOARD FASTENER. INSTALLED FRAME REPAIR PER TR 53-10-14A. (M)SDR USAA001240Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, SHEAR TIE AT FS 1040, BETWEEN S10L, S11L. FABRICATED NEW SHEAR TIE PER SRM 51-10-2. (M)SDR USAA001241Frame · crackedCLT - FOUND FRAME FLANGE CRACKED .25 INCH, STATION 616, FLANGE BELOW STRINGER 7 LT. REMOVED AND REPLACED WITH FABRICATED PART PER DWG 66-24124 AND SRM 51-10-02. (M)SDR USAA001243Skin · crackedCLT - FOUND EXTERIOR SKIN CRACKED TWO PLACES .5 INCH, UPPER HINGE CUTOUT EXTERIOR SKIN. INSTALLED DOUBLER PER EA 67783. (M)SDR USAA001245Stringer · corrodedCLT - FOUND STRINGER CORRODED 3 INCHES BY 1 INCH, STATION 500D STRINGER 28L. INSTALLED DOUBLER PER SRM 53-30-12. (M)SDR USAA001244Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .250 INCH, UPPER T-CAP STATION 467 FROM RBL 55 TO LBL 55. REPLACED TOP T-CAP PER TR 53-10-05A. (M)SDR USAA001231Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, INBOARD CHORD OF FRAME 616 AT WL 206 RT SIDE. INSTALLED CHORD REPAIR PER TR 53-62-01. (M)SDR USAA001222Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 4L, BS 908. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-2. (M)SDR USAA001221Clip · crackedCLT - FOUND CLIP CRACKED .5 INCH, STRINGER TIE CLIP AT FS 663 AND STRINGER 10L. INSTALLED NEW CLIP PER SRM 51-10-2. (M)
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