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 USAA050991Stringer Splice · crackedCLT, Q6, SPLICE CRACKED AT STA 907, S4R. REMOVED AND REPLACED STRINGER SPLICE IAW SRM. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050992Frame · crackedCLT, Q6 FRAME, 1.4 INCH CRACK, BS 616 RT BOTTOM OF FRAME INNER CHORD BS 616 RT. REMOVED DAMAGE, INSTALLED FILLER AND DOUBLER IAW TR 53-62-01. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050993Frame · crackedCLT, Q6, FRAME .125 INCH CRACK, STRINGER 9 LT STA 500A. REPAIRED IAW TR 53-10-20B. (K)Aug 8, 2005 · N588US · Boeing 7373B7 · Fuselage Main, FrameSDR AWXA200500919Battery · lowPHX - EEL - DURING 4 DAY CHECK, THE EXTERIOR EMERGENCY ESCAPE LIGHT AT L2 DOOR WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED POWER SUPPLY AND BATTERY ABOVE AFT GALLEY IAW BOEING 737-300 AMM 33-51-51-201. POWER SUPPLY; RADIANT ILLUM; PN 100865, SN UNK; INAug 8, 2005 · N332AW · Boeing 7373B7 · Emergency LightingSDR SB05088Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE FORWARDED EMERGENCY LIGHTS NOT ILLUMINATING. MAINTENANCE REMOVED AND REPLACED THE FORWARD EMERGENCY LIGHT BATTERY PACK. OPERATIONAL CHECK GOOD.Aug 7, 2005 · N396US · Boeing 7373B7 · Emergency LightingSDR USAA050984Beam · crackedCLT - Q6 - BEAM, 3 INCH CRACK, STRINGER 8R, STA 500. ACCOMPLISHED SPLICE REPAIR. (K)Aug 5, 2005 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050973Stringer · crackedCLT - FOUND STRINGER CRACKED .5 INCH, STRINGER 8R AT STATION 500. REMOVED DAMAGED SECTION. FABRICATED AND INSTALLED REPAIR PIECES IAW SRM 53-00-03. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050972Crease Beam · crackedCLT - FOUND CREASE BEAM CRACKED .75 INCH, BS 576, S17R. REPLACED WITH FACTORY NEW PART IAW SRM 51-10-02. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050968Clevis · corrodedCLT - FOUND ATTACH CLEVIS CORRODED 2 INCHES DIAMETER BY .015 TYPICAL, RIGHT HORIZ STAB FORWARD SPAR ATTACH CLEVIS AFT FACE. REMOVED CORROSION AND BUSHED IAW 55-10-10. (M)Aug 4, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050969Attach Fitting · corrodedCLT - FOUND STAB LUG CORRODED, R1 LUG AFT FACE RIGHT HORIZONTAL STABILIZER. REMOVED CORROSION AND INSTALLED BUSHING IAW SRM 55-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050967Attach Angle · wornCLT - FOUND ATTACH ANGLE CRACKED 1 INCH DIAMETER, WORN AREAS, RT WHEEL WELL STATION 727 RBL 14 BOTTOM OF BULKHEAD. REMOVED DAMAGED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DWG 65-48689 AND SRM 51-10-02 AND 51-40-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050966Web · crackedCLT - FOUND WEB CRACKED 2 INCHES, AFT CARGO DOOR CUTOUT FRAME, LOWER WEB. REMOVED DAMAGED WEB, FABRICATED AND INSTALLED NEW WEB IAW BOEING DWG 65-20723 AND SRM 51-10-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050965Angle · corrodedCLT - FOUND C-ANGLE CORRODED 2 INCHES, UPPER SURFACE OF FORWARD ENTRY DOOR THRESHOLD C-ANGLE. REMOVED DAMAGED ANGLE AND REINSTALLED NEW ANGLE IAW SRM 53-10-15. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050964Floorbeam · corrodedCLT - FOUND BEAM CORRODED 28 INCHES, T-CAP OF FLOORBEAM STATION 312, LBL 2, RBL 26. REMOVED PREVIOUS T-CAP AND REPLACED WITH NEW CAP EXTENDING SPLICES PER SRM IAW SRM 53-10-51. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050963Stringer Clip · crackedCLT - FOUND STRINGER TIE CRACKED .25 INCH, BS 847, STRINGER 4R. REMOVED CRACKED TIE, BS 847, STRINGER 4R. REMOVED CRACKED TIE CLIP AND INSTALLED NEW CLIP IAW SRM 51-10-02 AND 51-40-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA050962Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 327, BL 0, CABIN FLOOR STRUCTURE. REMOVED CRACKED STRAP AND REPLACE WITH NEW FROM STOCK IAW SRM 51-10-02 AND 51-40-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050948Bushing · corrodedCLT - Q6 - LUG/BUSHING, CORROSION, L6 LUG, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050947Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L3, AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050941Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK. L5, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050961Strap · crackedCLT - FOUND STABILIZER STRAP CRACKED 1 INCH, BS 326, LBL 11. DEF PART REPLACED WITH IDENTICAL PART, IAW SRM 51-10-02 AND 51-40-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050960Floorbeam · corrodedCLT - FOUND BEAM T-CAP CORRODED 6 INCHES, STATION 360, RBL 55 - RBL 61. REMOVED DAMAGED METAL, INSTALLED NEW T-CAP FROM RBL 35 - RBL 72 IAW SRM 53-00-51. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050959Stiffener · corrodedCLT - FOUND STIFFENER CORRODED .5 INCHES BY 6 INCHES, STRINGER 26R BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION ATTACH FITTING AND STIFFENER IAW SRM 53-60-03 AND 51-10-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050958Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCH BY .015 INCH, FORWARD SPAR ATTACH LUG AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM 55-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050957Skin · crackedCLT - FOUND PYLON SKIN CRACKED 2 INCHES, RT ENGINE PYLON UNDER PANEL 5858. REMOVED DAMAGE FABRICATED AND INSTALLED DOUBLER IAW TR 57-41-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA050943Lug · corrodedCLT - Q6 - LUGS, CORROSION; NO LEVEL OR TASK, L2/L5 BORES, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHINGS IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050942Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L5, AFT FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050956Floorbeam · corrodedCLT - FOUND FLOORBEAM UPPER CHORD CORRODED 1 INCH BY 1 INCH, BS 344 BETWEEN LBL 55 - RBL 13. REMOVED UPPER CHORD OF FLOORBEAM. INSTALLED NEW CHORD AND ASSOCIATED REPAIR SPLICES IAW SRM 53-10-51. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA0540944Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L2, FWD FACE LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050955Intercostal · corrodedCLT - FOUND INTERCOSTAL CORRODED 2 INCHES BY 3 INCHES, STATION 312 AND 394.5 ATL LBL 12. REMOVED PART, FABRICATED NEW AND INSTALLED IAW SRM 51-10-02. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050954Beam · corrodedCLT - FOUND BEAM CORRODED 6 INCHES, STATION 986, EXTREME RT END. REPLACED T-CAP IAW TR 53-60-05B. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA050945Bushing · corrodedCLT - Q6 - LUG/BUSHING, 2 INCH X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, LT,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050946Bushing · corrodedCLT - Q6 -LUG/BUSHING, 2 INCH DIA X .015 TYPICAL, CORROSION; NO LEVEL OR TASK, L1,AFT FACE, LT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM. (K)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050953Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCHES BY .015 TYPICAL, LT STAB CENTER SECTION FORWARD LOWER LUG. REMOVED CORROSION, FABRICATED NEW BUSHING. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050952Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCH DIAMETER BY .015 TYPICAL, L3, FORWRD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050951Bushing · corrodedCLT - BUSHING CORRODED, L1, FORWARD FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050950Bushing · corrodedCLT - FOUND LUG/BUSHING CORRODED 2 INCHES IN DIAMETER BY .015 TYPICAL, L6, AFT FACE LEFT HORIZONTAL STABILIZER. REMOVED CORROSION, FABRICATED NEW BUSHING IAW SRM 53-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050949Bushing · corrodedCLT - FOUND CORROSION ON LUG/BUSHING 2 INCHES BY .015, LEFT STAB, FORWARD LOWER LUG LEFT HORIZ STABILIZER. OVERSIZED LUG, FABRICATED NEW BUSHING IAW SRM 55-10-10. (M)Aug 3, 2005 · N588US · Boeing 7373B7 · Horizontal Stabilizer, Attach FittingsSDR USAA050971Skin · crackedCLT- C4 - SKIN, OB LOWER LE SKIN OF NR 6 SLAT CRACKED MKD 1 INCH CRACK. INSTALLED DOUBLER IAW SRM. (K)Aug 3, 2005 · N511AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA200508001Skin · cracked1/2" CRACK AT AFT CARGO DOOR LOWER FWD CORNER OF OUTER SKIN, REPAIR: INSTALLED FILLER, DOUBLER, TRIPLER PER EA 96770.Jul 29, 2005 · N504AU · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA200507005Skin · delaminated3 INCH BY 4 INCH AREA OF DELAMINATION ON TRAILING EDGE OF TAB, 18 INCH FROM OUTBOARD END. WET COMPOSITE LAYUP PER SRM 51-70-16.Jul 29, 2005 · N531AU · Boeing 7373B7 · Aileron TabsSDR USAA050906Stiffener · corrodedCLT - Q6 - STIFFENER, .5 INCH X 6 INCH CORROSION; NO LEVEL OR TASK. STR 26R, BS 1006-1016. REMOVED DAMAGE INSTALLED NEW STRINGER SECTION, ATTACH FITTING AND STIFFENER IAW SRM. (K)Jul 28, 2005 · N588US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05083Battery Pack · dischargedPVD MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHT OVER THE AFT LEFT ENTRY DOOR INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Jul 21, 2005 · N520AU · Boeing 7373B7 · Emergency LightingSDR USAA050884Skin · crackedCLT - C - SKIN, .75 CRACKED, LT NACELLE STRUT AT NACELLE STATION 218.840. STOP DRILLED AND OVERSIZED HOLE IAW SRM. (K)Jul 18, 2005 · N393US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA050880Flange · wornCLT - Q2 - KEELBEAM FLANGE, 60 INCHES SURFACE WEAR. FUSELAGE KEELBEAM LT OB FLANGE STA 664-727. INSTALLED REPAIR STRAP IAW EA. (K)Jul 14, 2005 · N526AU · Boeing 7373B7 · Fuselage Main, KeelSDR USAA200507004Skin · cracked5 IN CRACK FOUND BETWEEN FRAME 727D AND 727E STR 24L. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229.Jul 12, 2005 · N392US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA200507003Frame · cracked1.5 IN CRACK FOUND AT FRAME 767, STR 24L. INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229.Jul 11, 2005 · N392US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA200507001Skin · crackedCRACK AT BS 767 BETWEEN STRINGERS 21 RT AND 22 RT ON FUSELAGE SKIN. REMOVED DAMAGED FUSELAGE SKIN AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 229, DETAIL X.Jul 9, 2005 · N385US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050852Skin · crackedCLT - FOUND SKIN CRACKED 1.75 INCH, FS 745 AT STRINGER 24L. INSTALLED REPAIRED DOUBLER IAW SRM 53-00-01 DETAIL XI. (M)Jul 8, 2005 · N505AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050848Skin · crackedCLT - FOUND SKIN CRACKED 1.3 INCH, MAIN ENTRY LOWER HINGE CUTOUT AT LOWER RADIUS. INSTALLED DOUBLER IAW TYPICAL REPAIR NR 52-10-12. (M)Jul 7, 2005 · N505AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050849Skin · crackedCLT - FOUND SKIN CRACKED .25 INCH, FORWARD SERVICE DOOR, LOWER HINGE CUTOUT ON THE SKIN. INSTALLED DOUBLER IAW EA 96719. (M)Jul 7, 2005 · N505AU · Boeing 7373B7 · Fuselage Main, Plate/Skin
Back to Boeing 737-3B7