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 USAA001223Stringer · crackedCLT - FOUND STRINGER CRACKED .25 INCH, STRINGER 4R AT BS 908. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-2. (M)Aug 8, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA001209Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 104 INCHES BY 2.1875, STATION 986, FLOORBEAM TOP SURFACE. CORROSION LEVEL 1, C53-107-02. INSTALLED T-CAP PER TR 53-10-05A. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001217Clip · crackedCLT - FOUND CLIP CRACKED .375 INCH, STRINGER TIE CLIP AT FS 727D AND STRINGER 6L. REMOVED AND REPLACED PER SRM 51-10-02 AND 51-40-03. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001216Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STRINGER TIE CLIP AT FS 706 AND 4L. REMOVED AND REPLACED PER SRM 51-10-2. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001215Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, BS 867 AT STRINGER 9L. INSTALLED REPAIR DAMAGE PER TR 53-10-14A. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001214Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STRINGER 4R AT BS 867. REMOVED AND REPLACED PER SRM 51-10-02 AND 51-40-03. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001213Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, STRINGER 4L AT BS 867. REMOVED AND REPLACED PER SRM 51-10-02 AND 51-40-03. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001212Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, STRINGER 10R AT BS 847. REMOVED AND REPLACED PER SRM 51-10-02 AND 51-40-03. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001211Frame · crackedCLT - FOUND FRAMED CRACKED .5 INCH, BS 807, STRINGER 9L. INSTALLED REPAIR DOUBLER PER TR 53-10-14A. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001210Floorbeam · crackedCLT - FOUND FLOORBEAM CRACKED 12 INCHES, STATION 312, BL 0 TO RBL 12. REPLACED BEAM PER SRM 53-10-51. (M)Aug 7, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001168Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 420, STRINGER 4L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001173Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, AT FS 907 BETWEEN STRINGER 8L AND 9L. INSTALLED DOUBLER PER TR 53-10-14A. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001172Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 807, STRINGER 10R. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001167Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 639, STRINGER 5R. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001166Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 639, STRINGER 4R. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001165Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 639, STRINGER 3R. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001164Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 639, STRINGER 2R. INSTALLED TIE CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001163Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616 STRINGER 5R. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001162Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 4R. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001161Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 4L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001160Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 3L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001159Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .125 INCH, BS 616, STRINGER 2L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00207Controller · failedCLT - FLT 1750 - EN ROUTE FROM PVD TO CLT, AIRCRAFT EXPERIENCED AN UNCOMMANDED ROLL IN CRUISE AT FL350, MACH .75. WITH B AUTOPILOT AND AUTOTHROTTLE ON AND UNAV AND LNAV ENGATED, THE YAW DAMPER DISENGAGED AND THE AIRCRAFT ROLLED 15-20 DEGREES LEFT. THE AUTOPIAug 4, 2000 · N516AU · Boeing 7373B7 · Rudder Control SystemSDR USAA001171Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 787, STRINGER 10R. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001170Clip · crackedCLT - FOUND CLIP CRACKED .25 INCH, STATION 480 STRINGER 2L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001169Clip · crackedCLT - FOUND CLIP CRACKED .250 INCH, STATION 440, STRINGER 16L. REPLACED CLIP PER SRM 51-10-2. (M)Aug 4, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001061Skin · crackedTPA - FOUND FUSELAGE SKIN CRACKED .700 INCH, RIGHT AFT SERVICE DOOR UPPER HINGE CUTOUT. INSTALLED DOUBLER PER SRM 53-60-01 FIG 205. (M)Jul 31, 2000 · N521AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB00202Indicator · failedPHL - FLT 409 - EN ROUTE FROM GSO TO PHL, AT 24,000 FT, CAPTIAN NOTICED THE NR 1 ENGINE OIL TEMPERATURE WAS REDLINED THEN BEGAN BOUNCING AROUND. POWER WAS PULLED BACK AND TEMPERATURE REMAINED IN YELLOW BAN BUT WENT BACK UP TO REDLINE. CREW ACCOMPLISHED PROCEJul 30, 2000 · N395US · Boeing 7373B7 · Engine Oil TemperatureSDR USAA001175Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED 60 INCHES, LEFT INBOARD SEAT TRACK FROM STATION 887-947. CORROSION LEVEL 1. NEW SECTION OF SEAT TRACK AND SPLICES PER EA 55955 AND SRM 53-00-52. (M)Jul 26, 2000 · N517AU · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001191Skin · gougedPIT - FOUND SKIN GOUGED .040 INCH BY 5 INCH, AFT CARGO DOOR CUTOUT FORWARD SIDE BS 794 INNER SKIN. DOUBLER INSTALLED AT FORWARD SIDE AND BOTTOM CORNER OF AFT CARGO DOOR CUTOUT PER EA 55941. (M)Jul 26, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB00199Outflow Valve · defectiveCLE - FLT 9550 - ON CLIMB-OUT FROM CLE, EN ROUTE TO PHL AT FL110, PILOT REPORTED THAT FLIGHT LOST CABIN PRESSURIZATION. AUTO, STANDBY AND MANUAL MODES WOULD NOT CONTROL OUTFLOW VALVE. CIRCUIT BREAKERS WERE RESET WITH NO CHANGE. LANDING GEAR WAS CYCLED DOWN,Jul 26, 2000 · N525AU · Boeing 7373B7 · Pressure Regulator/Outflow ValveSDR USAASB00205Battery Pack · dischargedPHL - MAINTENANCE FOUND THE FORWARD THIRD OF CABIN FLOOR PROXIMITY EVACUATION LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK AT SEAT ROW 1. OPS CHECK GOOD. (M)Jul 24, 2000 · N516AU · Boeing 7373B7 · Emergency LightingSDR USAA001190Structure · corrodedPIT - FOUND CORROSION ON T-CAP EXTRUSION, 1 INCH BY 4 INCH AREA, STATION 986.5 AFT GALLEY RIGHT SIDE. REMOVED AND REPLACED T-CAP PER SRM 53-10-05. CORROSION LEVEL 1. (M)Jul 23, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001060Skin · crackedPIT - FOUND SLAT OUTER SKIN CRACKED 1.9 INCH, NR 6 SLAT LOWER T/E SKIN, .0008 INCH FORWARD OF T/E. HFEC, REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER PER TR 57-50-01 AND BOEING DRAWING 65C30133. (M)Jul 21, 2000 · N517AU · Boeing 7373B7 · Leading Edge DevicesSDR USAASB00194Downlock Sensor · faultyCLT - FLT 250 - ON PREPARATION FOR LANDING AT CLT FROM PNS, THE RIGHT MLG GREEN LIGHT FLICKERED. WHEN GEAR WAS EXTENDED, THE RED UNSAFE LIGHT ILLUMINATED AND NO GREEN LIGHT. CREW ACCOMPLISHED A GO-AROUND AND MADE A VISUAL CHECK TO CONFIRM THAT THE GEAR WAS DJul 21, 2000 · N385US · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA001174Keelbeam · gougedPIT - FOUND KEEL BEAM LOWER FLANGE WITH THREE GOUGES, .375 INCH DIAMETER BY .007 INCH, .043 INCH, .036 INCH DEEP, LEFT KEEL BEAM LOWER FLANGE TOP SURFACE STATION 663-727. SPOT FACED AND INSTALLED STRAPS PER EA 55931. (M)Jul 18, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA001176Keelbeam · gougedPIT - FOUND RIGHT LOWER KEEL BEAM GOUGED 4 PLACES, .375 INCH DIAMETER BY .004 INCH, .007 INCH, .035 INCH, .015 INCH, RIGHT KEEL BEAM LOWER FLANGE UPPER SURFACE STATION 727-706. SPOT FACED AND INSTALLED STRAPS PER EA 55931. (M)Jul 18, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA001059Skin · crackedPIT - FOUND SLAT OUTER SKIN CRACKED .6 INCH, NR 6 SLAT LOWER T/E SKIN 1.125 INCH FORWARD OF TRAILING EDGE. REMOVED CRACKED AREA, HFEC, INSTALLED DOUBLER AND FILLER PER TYP 57-50-01. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA001058Attach Fitting · gougedPIT - FOUND FORWARD ATTACH LUG GOUGED, 1 INCH SEMI CIRCLE .025 INCH DEEP, FS 81.10 STANDBY ACT FORWARD ATTACH BOLT FITTING. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Vertical StabilizerSDR USAA001049Floorbeam · damagedPIT - FOUND FLOORBEAM HAS MECHANICAL DAMAGE IN 3 SPOTS, .250, .200, .500, BS 827, 9 INCHES RIGHT OF BL0, BOTTOM T. REMOVED AND REPLACED T-ANGLE PER SRM 53-00-51 AND EA 55434. (M)Jul 17, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001189Stringer · corrodedPIT - FOUND STRINGER CORRODED 1 INCH BY 3 INCHES, STATION 316-324 STRINGER 28R. REPLACED SECTION OF STRINGER PER EA 55710 AND SRM 53-00-03. CORROSION LEVEL 1, TASK NR C53-202-01. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA001188Stringer · corrodedPIT - FOUND STRINGER CORRODED 2 INCHES BY 6 INCHES, STRINGER 28R BETWEEN BS 312 AND BS 323.7. SPLICED IN NEW STRINGER PER SRM 53-00-03 AND EA 55710. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA001187Beam · corrodedPIT - FOUND BEAM CORRODED 1 INCH BY 4 INCH AREA, 328 LBL 10 UPPER CHORD LOWER SURFACE. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA001186Bushing · corrodedPIT - FOUND CORROSION IN BOTH BUSHINGS .25 INCH BY .25 INCH AREA, FOR NR 2 KRUEGER FLAP ACTUATOR. CORROSION LEVEL 1, TASK NR C57-302-01. POLISHED AND BLENDED PER SRM 20-50-03. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Leading Edge Slat ActuatorSDR USAA001057Fitting · corrodedPIT - FOUND FITTING CORRODED 2 INCHES BY 2 INCHES, NR 7 RUDDER HINGE SEGMENT MOUNT FITTING AT STATION 299.25. FRETTING CORROSION, LEVEL 1. REMOVED CORROSION, ROTO PEENED, TREATED AND PRIMED PER SRM 55-30-90, 51-20-01 AND SPM 20-14-20. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Rudder StructureSDR USAA001056Bushing · corrodedPIT - FOUND BUSHING CORRODED .25 INCH DIAMETER, IN OUTBOARD BUSHING FOR NR 1 KRUEGER FLAP ACTUATOR. BLENDED PER SRM 20-50-03. CORROSION LEVEL 1, TASK NR C57-302-01. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Aileron TabsSDR USAA001055Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 29.4 INCH AREA, TOP OF T-CAP UNDER FLOOR MOUNT. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED AND REPLACED WITH NEW INTERCOSTAL PER SRM 51-40-02, 51-40-05 AND MM 51-21-99. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001054Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 3 SQUARE INCHES, BS 1016 TOP OF T-CAP AND AT NUTPLATE HOLES. CORROSION LEVEL 1. REPAIRED PER EA 55695 AND TR 53-20-10, REF A. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001051Floorbeam · corrodedPIT - FOUND WEB CORRODED 110 INCHES IN 10 PLACES, STATION 1016 TO 986 SUPPORT WEBS, LEFT SIDE WET AREA. CORROSION TASK NR C53-107-02, LEVEL 1. REMOVED AND REPLACED FLOORBEAM 986.5 AND SUPPORT WEBS PER SRM 51-20-01, 51-40-03. (M)Jul 17, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001148Spar · gougedPIT - FOUND REAR SPAR TO RIB ANGLE GOUGED SEVERAL TIMES AT .125 INCH LONG, LEFT HORIZ REAR SPAR TO RIB ATTACH ANGLE STATION 138.70. TREATED AND PRIMED PER SRM 55-10-09 FIG 101. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Horizontal Stabilizer, Spar/Rib
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