Boeing 737-301

Service difficulty reports · 4,797

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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.

SDR USAA000569Floorbeam · corrodedCLT - FOUND FLOOR FRAME CORRODED 1 INCH, STATION 312, BL 0, RBL 8, RBL 36. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Apr 17, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000577Skin · corrodedCLT - FOUND FUSELAGE SKIN CORRODED, .75 INCH BY .75 INCH, BS 500C PLUS 10, LBL 18. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Apr 17, 2000 · N562AU · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA0000250Wire · brokenNON ROUTINE, 7C EMERGENCY LIGHT INOP. SPLICED BROKEN WIRE AT SEAT 7C.Apr 17, 2000 · N325AW · Boeing 737301 · Light System WiringSDR USAA000557Skin · crackedCLT - FOUND SKIN CRACKED .500 INCH, AFT ENTRY DOOR UPPER HINGE FITTING. INSTALLED DOUBLER PER TR 53-10-11. (M)Apr 14, 2000 · N351US · Boeing 737301 · Passenger/Crew DoorsSDR USAA000561Floorbeam · corrodedFOUND FLOORBEAM CORRODED .500 INCH, STATION 360 RBL 52 - RBL 72. INSTALLED T-CAP PER SRM 53-00-51 AND 51-70-11. CORROSION LEVEL 2 NR C53-107-01. (M)Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000562Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 3 INCHES BY 1 INCH, STATION 328, RBL 51 TOP SURFACE. INSTALLED T-CAP PER SRM 53-10-51. CORROSION LEVEL 2 NR C53-107-01. (M)Apr 14, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000554Frame · crackedCLT - FRAME CRACKED .75 INCH CRACK, FS 907 JUST LEFT OF STRINGER 1 FRAME. INSTALLED FILLER AND DOUBLER PER EA 66974. (M)Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000555Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH, STATION 1016, LBL 6 AND LBL 10 SCREW HOLES. REPAIRED PER TR 53-20-10 AND EA 66954. (M)Apr 13, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00113Line · chafedCLT - FLT 825 - ON DESCENT INTO CLT, CAPTAIN REPOTED THE NR 1 ENGINE HYDRAULIC LOW PRESSURE LIGHT ILLUMINATED. CAPTAIN POSITIONED THE NR 1 ENGINE HYDRAULIC SWITCH TO OFF AND DECLARED AN EMEGENCY. FLIGHT LANDED WITHOUT FURTEHR INCIDENT. AIRCRAFT WAS TOWED TOApr 11, 2000 · N585US · Boeing 737301 · Hydraulic System, MainSDR USAA000538Floorbeam · crackedCLT - FOUND FLOORBEAM WEB CRACKED 4 PLACES .25 INCH, BS 328, RBL 44, WL 202.5 RIVET HOLES. REMOVED DAMAGED PER EA 66993. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000539Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 4L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000540Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 5L. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000541Frame · crackedCLT - FOUND FRAME CRACKED .500 INCH, BS 887, STRINGER 9L. REMOVED CRACK, INSTALLED DOUBLER PER TR 53-10-14. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000542Angle · crackedCLT - FOUND ANGLE CRACKED .5 INCH, BS 639, LBL 45, WL 203 VERT ATTACH ANGLE. REMOVED AND REPLACED ANGLE PER SRM 51-30-02 AND DWG 65-46540. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000543Angle · corrodedCLT - FOUND ANGLE CORRODED 1 INCH BY 15 INCHES, AFT ENT Z-CHANNEL ANGLE. REMOVED AND REPLACED Z-ANGLE PER SRM 51-40-02. (M)Apr 10, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000548Skin · crackedPIT - FOUND SKIN CRACKED .25 INCH, STATION 380 AT A/C BELLY CENTER LINE. INSTALLED EXTERIOR DOUBLER PER SRM 53-30-04. (M)Apr 8, 2000 · N587US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA000530Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH, STATION 1016, LBL 15 FLOORBEAM. INSTALLED REPAIR PER SRM 53-00-51 FIG 203. (M)Apr 7, 2000 · N351US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000537Frame · corrodedCLT - FOUND FRAME CORRODED 2 INCHES, STATION 500D, LBL 18 SKIN. INSTALLED DOUBLER, T-ANGLE AND SHIM PER SRM 53-00-07. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000531Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178, BULKHEAD WEB RBL 4.75, WL 201. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000532Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 201. INSTALLED DOUBLER. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000533Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB LBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000534Bulkhead · crackedCLT - FOUND WEB CRACKED .5 INCH, STATION 178 BULKHEAD WEB RBL 4.75, WL 198. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000535Stiffener · crackedCLT - FOUND VERTICAL STIFFENER CRACKED 1 INCH, STATION 178 BULKHEAD VERTICAL STIFFENER LBL 6, WL 184. INSTALLED DOUBLER AND ANGLES PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000536Bulkhead · crackedCLT - FOUND WEB CRACKED .25 INCH LONG, STATION 178 BULKHEAD WEB RBL 1, WL 206. INSTALLED DOUBLER PER SRM 53-10-08. (M)Apr 7, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000528Web · crackedCLT - FOUND WEB CRACKED .25 INCH, BS 710-717, BBL 0, WL 203. INSTALLED DOUBLER PER SRM 51-70-13. (M)Apr 5, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00104Panel · malfunctionedIPT - FLT 296 - EN ROUTE FROM LGA-CMH, AT APPROXIMATELY FL270, THE ALTITUDE WARNING HORN SOUNDED. CABIN ALTITUDE WAS APPROXIMATELY 13-14K. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND DESCENDED TO FL100. FLIGHT DIVERTED TO PIT AND LANDED WITHOUApr 5, 2000 · N577US · Boeing 737301 · Cabin Pressure Control SystemSDR AWXA0000229Warning Light · illuminatedAIR TURNBACK, WHEN L/G WAS SELECTED TO UP ON TAKEOFF, RED NOSE GEAR INTRANSIT LIGHT REMAINED ON. RED LIGHT REMAINED ON IN BOTH POSITIONS, GEAR VISUALLY CHECKED DOWN AND LOCKED. REMOVED AND REPLACED DOWNLOCK PROX SENSOR S846 AND CARD M1215, OPS CHECKED GOOD. Apr 5, 2000 · N325AW · Boeing 737301 · Landing Gear Position and WarningSDR USAA000520Skin · crackedCLT - FOUND DOOR SKIN CRACKED 5 INCHES BY 5 INCHES, FORWARD SERVICE DOOR LOWER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 52-00-01 FIG 203. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Service DoorsSDR USAA000523Channel · corrodedCLT - FOUND Z-CHANNEL CORRODED, AFT SERVICE DOOR. REPLACED WITH NEW Z-CHANNEL PER SRM 51-4-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Service DoorsSDR USAA000524Angle · corrodedCLT - FOUND DOOR Z-ANGLE CORRODED 6 FT BY 3 INCHES, STATION 947-1006, LBL 60, AFT ENTRY DOOR Z-ANGLE. INSTALLED NEW Z-ANGLE PER SRM 51-40-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Passenger/Crew DoorsSDR USAA000522Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 18 SHELF AT AFT END INBOARD RIVET IN WEB. REPLACED PER SRM 51-10-02. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA000521Frame · crackedCLT - FOUND FRAME CRACKED .75 INCHES LONG, BOTTOM END OF STATION 616 INBOARD CHORD ANGLE RIGHT SIDE. FABRICATED ANGLE AND FILLER PER TR 53-62-01. (M)Apr 4, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAASB00096Seal · fodPIT - FLT 1626 - ON CLIMB-OUT FROM PIT, AT APPROXIMATELY 5,000 FEET, ALL ATTEMPTS TO PRESSURIZE AIRCRAFT FAILED. NO ABNORMAL INDICATIONS WERE NOTED. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCEApr 2, 2000 · N584US · Boeing 737301 · Passenger/Crew DoorsSDR F3LA00031Light · inoperativeDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EMERGENCY PATH LIGHTING BETWEEN ROWS 6 AND 11 INOPERATIVE. MAINTENANCE REPLACED FUSE ON BATTERY PACK CHARGER UNIT. (M)Apr 2, 2000 · N578US · Boeing 737301 · Emergency LightingSDR USAA000513Frame · crackedCLT - FOUND FRAME WEB WITH 2 CRACKS 1.5 INCHES LONG, BS 727D BETWEEN STRINGER 27L AND 27R. REPAIRED DOUBLER PER EA 66864. (M)Mar 31, 2000 · N350US · Boeing 737301 · Fuselage Main, FrameSDR USAA000526Support Bracket · crackedPIT- FOUND SUPPORT BRACKET CRACKED 2 INCHES, STATION 727D-727E STRINGER NR 1 A/C CENTER LINE NR 3 VHF. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER. (M)Mar 30, 2000 · N563AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000508Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727A, STRINGER 2R TIE CLIP AFT SIDE. REPLACED TIE CLIP PER SRM 51-10-02. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000509Stringer Clip · crackedCLT - FOUND STRINGER TIE CLIP WITH TWO CRACKS .5 INCH LONG, STATION 639, STRINGER 4R FUSELAGE FRAME. REPLACED TIE CLIP PER SRM 51-10-02 AND 51-40-02. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000510Door Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FORWARD SERVICE DOOR FRAME LOWER FORWARD CORNER. INSTALLED DOUBLER AND FILLER PER SRM 51-10-11. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, StructureSDR USAA000512Bulkhead · crackedCLT - FOUND .5 INCH CRACK IN BULKHEAD, STATION 178, WEB LBL .75, WL 188. INSTALLED DOUBLER REPAIR PER SRM 53-10-08. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, BulkheadSDR USAA000507Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, STATION 827, STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, FrameSDR USAA000506Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 986, RBL 14 UPPER CHORD FLOORBEAM. REPLACED NEW T-CAP PER TR 53-10-05A. (M)Mar 30, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000490Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344 AT BL 0, LBL 22. CORROSION LEVEL 1. INSTALLED FLOORBEAM TOP CAP PER SRM 51-70-12. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA000491Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH BY .5 INCH, BS 1006, LBL 10 BEAM SCREW HOLES. REPAIRED DOUBLER PER SRM 53-00-51. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000492Seat Track · corrodedCLT - FOUND SEAT TRACK CORRODED 2 INCHES BY 2 INCHES, STATION 344, LBL 25. INSTALLED NEW SEAT TRACK PER SRM 53-00-52. (M)Mar 29, 2000 · N562AU · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB00089Power Supply · failedTPA - DURING ANNUAL OPERATIONAL CHECK OF THE AFT LEFT 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 ASSY FOR THE ESCAPE SLIMar 28, 2000 · N300AU · Boeing 737301 · Emergency LightingSDR USAA000464Stringer Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 727B, STRINGER 16. REMOVED AND REPLACED WITH NEW TIE CLIP PER SRM 51-10-02. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000465Beam · corrodedCLT - FOUND BEAM CORRODED .5 INCH, STATION 967, LBL 5 UPPER CHORD SCREW HOLE BEAM. INSTALLED T-CAP PER SRM 53-00-51. CORROSION LEVEL 1. (M)Mar 27, 2000 · N562AU · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000466Floor Support · crackedCLT - FOUND FLOOR SUPPORT ANGLE CRACKED .250 INCH, BETWEEN STATION 500D AND 520, BL 0. INSTALLED NEW ANGLE PER SRM 51-10-02. (M)Mar 27, 2000 · N350US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA000467Frame · crackedCLT - FOUND FRAME CRACKED .20 INCH, BS 500A, STRINGER 9L. INSTALLED REPAIR DOUBLER PER EA 66834. (M)Mar 27, 2000 · N350US · Boeing 737301 · Fuselage Main, Frame
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