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.

SDR USAA002102Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, BS 827, STRINGER 9R. INSTALLED FRAME REPAIR PER TR 53-10-14A. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002103Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 847, STRINGER 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002104Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 887 STRINGER 9R. REPLACED CLIP PER SRM 51-10-2. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002105Floorbeam · corrodedCLT - FOUND TOP FLANGE CORRODED 46 INCHES, STATION 986, RBL 2 TO RBL 48. REPLACED UPPER FLANGE OF FLOORBEAM PER TR 53-15-01B AND SRM 53-60-51. (M)Dec 11, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002067Frame · crackedCLT - FOUND FRAME CRACKED .5 INCH, STATION 500A STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)Dec 6, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002068Frame · crackedCLT - FOUND FRAME CRACKED .250 INCH, BS 887, STRINGER 9R. INSTALLED FRAME REPAIR PER TR 53-10-14A. (M)Dec 6, 2000 · N523AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002069Skin · crackedCLT - FOUND SKIN CRACKED 1.25 INCH, RIGHT FUSELAGE EXT AT STATION 747 STRINGER 24R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)Dec 6, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA002070Skin · crackedCLT - FOUND SKIN CRACKED 1.125 INCH, RIGHT FUSELAGE EXT STATION 867 STRINGER 23R. INSTALLED DOUBLER PER SRM 53-00-01 FIG 201. (M)Dec 6, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA002072Stringer · crackedCLT - FOUND STRINGER CRACKED 2 INCHES, BS 1141, STRINGER 5AL. INSTALLED REPAIR DOUBLER PER SRM 53-00-01. (M)Dec 6, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA002073Skin · corrodedCLT - FOUND EXTERIOR SKIN CORRODED 10 INCHES BY 20 INCHES, NR 3 VHF ANTENNA MOUNT STATION 727C AND 727E, LBL 5 TO RBL 5. CORROSION LEVEL 2 C53-107-02. INSTALLED DOUBLER PER SRM 53-00-01 FIG 202. (M)Dec 6, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA002066Flange · crackedCLT - FOUND FLANGE CRACKED IN 4 PLACES, ONE AT 1 INCH AND 3 AT 4 INCHES, UPPER FLANGE INTERCOSTAL STATION 380 TO 400 BL 0. FABRICATED NEW UPPER FLANGE AND INSTALLED PER SRM 51-10-2, 51-20-01 AND 53-30-51. (M)Dec 6, 2000 · N523AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002071Beam · crackedCLT - FOUND SUPPORT BEAM CRACKED .250 INCH, LEFT MAIN LANDING GEAR SUPPORT BEAM. REPLACED MLG SUPPORT BEAM PER EA 68529. (M)Dec 6, 2000 · N521AU · Boeing 7373B7 · Main Landing Gear Attach SectionSDR USAA002074Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 46 INCHES, SERVICE DOOR ENTRY STATION 294-340. CORROSION LEVEL 2 C53-107-02. INSTALLED SPLICE ANGLE AND SUPPORT ANGLE PER 51-10-02 AND 51-40-02. (M)Dec 6, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002075Floorbeam · corrodedCLT - FOUND T-CAP CORRODED, BS 344, LBL 10. CORROSION LEVEL 2 C53-107-02. INSTALLED NEW T-CAP PER SRM 53-10-51. (M)Dec 6, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002058Floorbeam · corrodedCLT - FLOORBEAM T-CAP CORRODED 1 INCH, BS 947.5, LBL 50 TO RBL 50. CORROSION LEVEL 2. REMOVED AND REPLACED FLOORBEAM T-CAP TR 53-10-05A. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002059Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCHES, BS 967, LBL 41 AND 47.5. INSTALLED UPPER FLANGE/CHORD REPAIR PER TR 53-10-05A AND SRM 53-00-51. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002060Angle · corrodedCLT - FOUND Z-ANGLE SUPPORT CORRODED 6 INCHES, BS 971 AT LBL 50. REPAIRED PER SRM 51-70-11 AND 51-10-2. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAAA002061Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED, STATION 986.5, RBL 50 TO LBL 50. CORROSION LEVEL 2. REMOVED AND REPLACED UPPER T-CAP PER TR 53-10-05A. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002062Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 43 INCHES, BS 993-950 LEFT Z-ANGLE LBL 50. INSTALLED NEW Z-ANGLE PER SRM 51-70-11 AND 51-10-2. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002063Angle · corrodedCLT - FOUND Z-ANGLE 37 INCHES, BS 955 TO 992, LBL 50. INSTALLED Z-ANGLE PER SRM 51-70-11 AND 51-10-2. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002057Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 578, STRINGER 10L. REPLACED TIE CLIP PER SRM 51-10-02. (M)Dec 4, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00339Control Handle · defectivePIT - FLT 214 - AFTER TAKEOFF FROM MCI, EN ROUTE TO PIT, THE LANDING GEAR LEVER WOULD NOT GO INTO THE LOCKED POSITION. LEVER WAS APPROX ONE INCH BELOW THE FULL UP POSITION AND COULD NOT BE RAISED UP ANY FURTHER. GEAR SEEMED TO OPERATE NORMALLY EXCEPT FOR NOSDec 2, 2000 · N526AU · Boeing 7373B7 · Landing Gear SelectorSDR USAA002050Stringer · crackedCLT - FOUND STRINGER CRACKED .75 INCH, STRINGER 18A SHEAR BEAM WEB STATION 726, LBL 65, WL 188. REMOVED AND REPLACED PER SRM 51-40-02. (M)Dec 1, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA002046Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORODED .5 INCHES, BS 986, RBL 29.5, 31.5, 36, 40 AND 43. REMOVED AND REPLACED T-CAP PER TR 53-10-05A. (M)Nov 30, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA002047Stringer · crackedCLT - FOUND STRINGER CRACKED 2 INCHES, STRINGER 5A, STATION 1141 LEFT SIDE. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 221. (M)Nov 30, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA002041Angle · corrodedCLT - FOUND ANGLE CORRODED 20 INCHES, STATION 270, LBL 10 TO RBL 10. CORROSION LEVEL 1. REMOVED DAMAGED Z-ANGLE PER TR 53-20-08. (M)Nov 29, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA002040Web · crackedCLT - FOUND WEB CRACKED .5 INCH, BS 708, RBL 25. INSTALLED BEAM WEB, DOUBLER AND SHIM PER EA 68484A. (M)Nov 29, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00337Valve · faultyPIT - FLT 307 - AIRCRAFT DEPARTED PIT WITH THE RIGHT PACK INOPERATIVE DUE TO MEL 21-19C (RIGHT PACK AIR MIX VALVE INOPERTIVE). AFTER TAKEOFF, THE AIRCRAFT WOULD NOT PRESSURIZE. FLIGHT RETURNED TO FIELD AT PIT AND LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCNov 29, 2000 · N391US · Boeing 7373B7 · Cabin Pressure Control SystemSDR USAA002039Stiffener · corrodedCLT - FOUND RADIAL STIFFENER CORRODED 1 INCH, BS 1016 PLUS 1 INCH AT BL 0. INSTALLED NEW STIFFENER AND DOUBLER PER EA 68560 AND EA 68441. (M)Nov 28, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR DL733002318Skin · crackedFUSELAGE / SKIN / AFT GALLEY DOOR CUTOUT / LWR HINGE CUTOUT:CRACK REPAIR. THE LOWER HINGE CUTOUT OF THE AFT GALLEY DOOR OPENING SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. THE CRACK WAS IN THE SKIN AND BONDED DOUBLER ONLY WITH NO CRACKING IN THE BEARNov 28, 2000 · N951WP · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA002012Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 827 ABOVE STRINGER 9L. INSTALLED DOUBLER PER EA 68493. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002013Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 847 ABOVE STRINGER 9R. INSTALLED DOUBLER PER EA 68493. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002014Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 887 ABOVE STRINGER 9L. INSTALLED DOUBLER PER EA 68493. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001987Frame · crackedCLT - FOUND CHORD CRACKED, WL 207, FS 178 LEFT SIDE. SPLICED IN NEW CHORD PER EA 68455. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001988Angle · crackedCLT - FOUND SUPPORT ANGLE CRACKED .500 INCH, BS 312-10 JUST BELOW STRINGER 13L. INSTALLED NEW PART PER SRM 51-10-01. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001989Skin · crackedCLT - FOUND SKIN CRACKED 1.5 INCH, FORWARD SERVICE DOOR AFT LOWER CORNER BS 328, WL 210. REPAIRED DOUBLER PER SRM 53-10-01. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001990Frame · crackedCLT - FOUND FRAME CRACKED 1 INCH, BS 616, LBL 63, WL 201. INSTALLED REPAIR ANGLE PER TR 53-62-01. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001991Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, ABOVE STRINGER 9L, STATION 787. INSTALLED DOUBLER PER TR 53-10-14A. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001992Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 887, ABOVE STRINGER 9R. INSTALLED DOUBLER TR 53-10-14. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001993Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 907, ABOVE STRINGER 9R. INSTALLED DOUBLER PER TR 53-10-14A. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001994Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED .25 INCH, BS 908 STRINGER 4L STRINGER SPLICE. INSTALLED NEW SPLICE PER SRM 51-40-00. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001995Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .75 INCH, STATION 178 BULKHEAD WEB, RBL 1, WL 206.5. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001996Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH, BS 178, RBL 7, WL 198. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001997Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .5 INCH, BS 178, LBL 7, WL 198. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001998Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1 INCH, BS 178, LBL 5, WL 198. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001999Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .625 INCH, BS 178, RBL 5, WL 198. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002000Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED 1.25 INCH, BS 178, RBL 5, WL 201. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002001Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH, BS 178, LBL 5, WL 201. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002002Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .5 INCH, BS 178, LBL 7, WL 201. INSTALLED DOUBLER PER EA 68459. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA002003Bulkhead · crackedCLT - FOUND BULKHEAD WEB CRACKED .25 INCH, BS 178, RBL 7, WL 201. INSTALLED DOUBLER PER EA 68549. (M)Nov 27, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Bulkhead
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