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.

SDR USAASB00250Battery Pack · dischargedBOS - WHILE ACCOMPLISHING A-CHECK, MAINTENANCE FOUND THE FOLLOWING EMERGENCY LIGHTS INOPERATIVE, L1 DOOR EXTERIOR LIGHT, LEFT OVERWING EXTERIOR LIGHT, LEFT CABIN BULLNOSE LIGHTS AT SEAT ROWS 5 AND 9, LEFT CAIBN ESCAPE PATH LIGHTS AT SEAT ROWS 5 THROUGH 9 AND TSep 11, 2000 · N334US · Boeing 737301 · Emergency LightingSDR USAA001502Beam · crackedCLT - FOUND VERTICAL BEAM CRACKED .250 INCH, BL 178, LBL 5.7, WL 184. INSTALLED REPAIR ANGLES, STRAPS AND FILLERS PER SRM 53-10-08 FIG 205. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001501Angle · crackedCLT - FOUND ANGLE CRACKED 2 INCHES, BOTTOM FORWARD CORNER SERVICE DOOR CUTOUT FRAME. REPLACED ANGLE PER 51-10-02 AND 51-40-00. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001500Frame · crackedCLT - FOUND FRAME CRACKED .75 INCH, FRAME 907 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001499Intercostal · crackedCLT - FOUND INTERCOSTAL CRACKED .5 INCH, BS 179, WL 207, LBL 28. REPLACED FABRICATED INTERCOSTAL PER SRM 51-10-02. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001484Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED 1 INCH, STATION 178 PRESS BULKHEAD AFT SIDE WL 190, BL 0. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001483Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .5 INCH IN TWO PLACES, AFT SIDE 178 PRESSURE BULKHEAD RBL 5.5, WL 201 AND 198. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001482Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .5 INCH IN TWO PLACES, AFT SIDE STATION 178 BULKHEAD, RBL 1 AND LBL 1, WL 208. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001481Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .25 INCH, AFT SIDE STATION 178 PRESS BULKHEAD, WL 201, RBL 7.5. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001480Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .500 INCH, BULKHEAD 178, WL 213. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001479Bulkhead · crackedCLT - FOUND BULKHEAD SKIN CRACKED .500 INCH IN TWO PLACES, AFT SIDE STATION 178 PRESS BULKHEAD LBL 5.5 WL 201 AND 198. INSTALLED EXT DOUBLER PER SRM 53-10-08 AND EA 67899. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, BulkheadSDR USAA001478Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .5 INCH BY 1 INCH, STATION 312, LBL 12. INSTALLED REPAIR PE SRM 53-10-51. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001477Floorbeam · corrodedCLT - FOUND T-CAP CORRODED 15 INCHES, STATION 270 AT BL 0. CORROSION LEVEL 1. REMOVED DAMAGE AND SPLICED IN REPAIR PART PER TR 53-20-08. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001476Support Bracket · corrodedCLT - FOUND ANT SUPPORT BRACKET 1 INCH BY 5 INCHES, BL 0 BETWEEN BS 500 AND 500A. CORROSION LEVEL 1 C53-208-01. REPAIRED PER SRM 51-10-02. (M)Sep 11, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00251Acm · overservicedPIT - FLT 9228 - AFTER TAKEOFF, CLIMBING THROUGH 2,000 FEET, CREW NOTICED AN INCREASING OILY SMELL IN THE FLIGHT COMPARTMENT. ODOR SEEMED TO BE MORE OILY THAN ELECTRICAL RELATED. NORMAL ENGINE READINGS AND PACK INDICATIONS WERE NOTED. CREW DONNED THEIR OXYGSep 11, 2000 · N563AU · Boeing 737301 · Cabin Cooling SystemSDR DL733001751Oven · odorA/C DIVERTED TO CYS AFTER EXPERIENCING FUMES IN THE CABIN. REPLACED F/C OVEN.Sep 10, 2000 · N948WP · Boeing 737301 · Buffet/GalleysSDR USAASB00245Battery Pack · dischargedGSO - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHTS AT THE OVERHEAD BIN DOORS WEAK. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Sep 5, 2000 · N346US · Boeing 737301 · Emergency LightingSDR 20010112SG062Connector · faultyPIT - FLT 856 - AFTER TAKEOFF, THE NR 1 ENGINE GENERATOR DROPPED OFF LINE. CAPTAIN STARTED THE APU AND THE APU GENERATOR DROPPED OFF LINE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN REPORTED LOSISep 4, 2000 · N559AU · Boeing 737301 · DC Generating SystemSDR USAASB00244Harness · faultyPIT - FLT 856 - AFTER TAKEOFF, THE NR 1 ENGINE GENERATOR DROPPED OFF LINE. CAPTAIN STARTED THE APU AND THE APU GENERATOR DROPPED OFF LINE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. CAPTAIN REPORTED LOSISep 4, 2000 · N559AU · Boeing 737301 · AC Generation SystemSDR USAASB00240Battery Pack · dischargedPHL - MAINTENANCE FOUND THE MID CABIN EMERGENCY LIGHTS INOPERTIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Sep 3, 2000 · N334US · Boeing 737301 · Emergency LightingSDR USAASB00243Warning Light · illuminatedPIT - FLT 1624 - ON CLIMB-OUT FROM PIT, THE LEADING EDGE FLAP TRANSIT LIGHT ILLUMINATED AS LEADING EDGE SLATS AND FLAPS DID NOT FULLY RETRACT. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE PERFORSep 3, 2000 · N585US · Boeing 737301 · Trailing Flap Position Indicating SystemSDR USAASB00242Switch · faultyPHL - FLT 663 - AFTER TAKEOFF FROM PHL, AT 1,500 FEET, CREW TRIED TO RETRACT FLAPS AND SLAT DISAGREEMENT LIGHTS ON PEDESTAL AND OVERHEAD PANEL ILLUMINATED. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES BUT PROBLEM REOCCURRED. CAPTAIN ADVISED THAT VISSep 2, 2000 · N563AU · Boeing 737301 · Leading Edge Slat Control SystemSDR USAA001417Stringer · crackedCLT - FOUND STRINGER 18A SHEAR BEAM CRACKED .5 INCH, STRINGER 18A SHEARBEAM WEB 1 INCH FORWARD STATION 727 LT SIDE. INSTALLED NEW SHELF PER SRM 51-10-2. (M)Sep 1, 2000 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001416Stringer · crackedCLT - FOUND STRINGER CRACKED 1 INCH, BS 727 SHELF 18A RIGHT. REPAIRED PER SRM 51-10-02 AND 51-40-03. (M)Sep 1, 2000 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001415Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 616 BELOW STRINGER 17. INSTALLED DOUBLER PER TR 53-62-01. (M)Sep 1, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001414Angle · crackedCLT - FOUND ANGLE CRACKED 1 INCH, FRAME TO INTERCOSTAL ATTACH ANGLES STATION 360 STRINGER 4L. INSTALLED FABRICATED ANGLE PER BOEING 65 58280. (M)Sep 1, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00239Line · leakingCLT - FLT 2271 - DURING CLIMB-OUT FROM PHL, EN ROUTE TO BNA, CAPTAIN SENT ACARS MESSAGE THAT THE MAIN LANDING GEAR WOULD NOT LOCK IN THE UP POSITION. GEAR INDICATION SHOWED NORMAL AFTER RECYCLING GEAR. FLIGHT DIVERTED TO CLT FOR MAINTENANCE DUE TO LIKELIHOODSep 1, 2000 · N352US · Boeing 737301 · Landing Gear Retraction/Extension SystemSDR USAA001408Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .375 INCH, BS 328, RBL 24.50 TO SERVICE DOOR. INSTALLED ANGLES PER SRM 53-00-51. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001407Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 5 INCHES BY .25 INCH, BS 328M 11.5 INCHES IN FROM FORWARD SERVICE DOOR. INSTALLED REPAIR ANGLES, T-CAP PER SRM 53-00-51 FOG 201. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001411Stiffener · corrodedCLT - FOUND STIFFENER CORRODED 3 INCHES BY 1 INCH, AFT BULKHEAD STIFFENER STATION 1016 BETWEEN STRINGER 27L AND 27R. INSTALLED SECTION CHANNEL REPAIR PER RM 53-80-08 AND 51-70-11. CORROSION LEVEL 1. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001410Web · corrodedCLT - FOUND WEB CORRODED 1 INCH IN 18 AREAS, BS 440 TO BS 480 PLUS 12 BETWEEN STRINGER 25R AND 26R. REPLACED WEB PER SRM 51-10-02 FIG 201. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001409Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES BY 3 INCHES, STATION 344, 14 INCHES LBL. CORROSION LEVEL 1 C53-107-01. INSTALLED T-CAP FLOORBEAM REPAIR PER SRM 53-10-51. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001406Frame · crackedCLT - FOUND FRAME CRACKED, FS 887 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001405Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 887, STRINGER 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001404Frame · crackedCLT - FRAME CRACKED .25 INCH, FRAME 807 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001403Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED TWO PLACES .25 INCH, BS 663 AND STRINGER 10R. REPLACED TIE CLIP PER SRM 51-10-02. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001402Web · crackedCLT - FOUND WEB CRACKED 1.25 INCH, STATION 344, LBL 35 AT FLOORBEAM. INSTALLED DOUBLER AND FILLER PER EA 67905. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001401Stringer · crackedCLT - FOUND STRINGER CRACKED .25 INCH, STRINGER SPLICE AFT SIDE OF FS 907 AT STRINGER 4R. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-10-02. (M)Aug 31, 2000 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001435Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 1 INCH BY 1 INCH, STATION 950 AFT ENTRY DOOR TOP SURFACE. CORROSION LEVEL 1, TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 53-60-51 AND 51-40-02. (M)Aug 30, 2000 · N589US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAASB00236Sensor · failedSAV - FLT 2382 - EN ROUTE FROM CLT TO SAV, AT FL220, THE CABIN BEGAN TO LOSE PRESS AND THE A/C EXPERIENCED SEVERAL INFLIGHT PROBLEMS WHICH SEEMED TO INDICATE AN AIR/GROUND SENSE FAULT. ACARS, TCAS, FLIGHT DIRECTOR, TRANSPONDER AND LNAV WERE AFFECTED. CAPTAINAug 30, 2000 · N351US · Boeing 737301 · Ground Proximity SystemSDR USAASB00256Battery Pack · dischargedRDU - WHILE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LEFT OVERHEAD EXIT LIGHTS, THE OVERWING DOOR EXIT LIGHTS, THE SEAT MOUNTED EXIT LIGHT AT OVERWING DOOR ROW AND ONE BULLNOSE EMERGENCY LIGHT OVER SEAT ROW 14, RIGHT SIDE, WOULD NOT HOLD CHARGE AFTAug 29, 2000 · N585US · Boeing 737301 · Emergency LightingSDR USAA001378Crease Beam · corrodedCLT - FOUND WEB CORRODED 1 INCH BY 6 INCHES, CREASE BEAM SHEAR WEB BETWEEN STATION 616 AND 639 STRINGER 17. REPAIRED PER TR 53-10-02. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, StructureSDR USAA001392Skin · crackedTPA - FOUND SKIN CRACKED .800 INCH, AFT SERVICE LOWER HINGE CUTOUT STATION 947.5 STRINGER 10R. INSTALLED DOUBLER PER SRM 53-60-01 FIG 207. (M)Aug 29, 2000 · N339US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001379Shear Tie · crackedCLT - FOUND SHEAR TIE CRACKED .5 INCH, BS 597 BELOW STRINGER 13R. REMOVED DAMAGE AND INSTALLED PART PER SRM 53-00-07. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, StructureSDR USAA001377Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 400, STRINGER 9R. INSTALLED DOUBLER AND FILLER PER TR 53-10-14. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001376Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, FS 907 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001375Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 867, STRINGER 9L. REMOVED AND INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001374Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 847, STRINGER 9L. REMOVED DAMAGE AND INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 29, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001444Web · corrodedPIT - FOUND WEB CORRODED 6 SQUARE INCHES, AFT CARGO DOOR LOWER SILL WEB. CORROSION LEVEL 1, TASK NR C53-202-01. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)Aug 28, 2000 · N577US · Boeing 737301 · Cargo/Baggage DoorsSDR USAA001443Angle · corrodedPIT - FOUND Z-ANGLE CORRODED 4 INCH AREA CORROSION, AFT LT DOOR SILL STATION 967 TO 986.5. CORROSION LEVEL 1, TASK NR C53-107-02. BLENDED PER SRM 53-00-52. (M)Aug 28, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous Structure
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