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 USAA200701001Skin · damagedA 3.625 INCH CRACK FOUND AT RIGHT SECTION 46 SKIN BETWEEN STA 867 & 887 AT LAP JOINT S25R. REMOVED DAMAGE & INSTALLED DOUBLER & TRIPLER REPAIR PER BOEING SRM 53-00-01 FIG 201.Dec 31, 2006 · N503UW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB06126Circuit Breaker · failedPBI FLT1286 ON CLIMBOUT FROM PBI, AT 1,300 FEET AGL, THE CAPTAIN REPORTED LOST ALL OF HIS PRIMARY FLIGHT INSTRUMENTS. CONTROL OF AIRCRAFT WAS GIVEN TO THE FIRST OFFICER, WHEREAS, HIS INSTRUMENTS FUNCTIONED PROPERLY. FLIGHT RETURNED TO FIELD AT PBI AND LANDEDDec 27, 2006 · N588US · Boeing 737301 · AC Power Distribution SystemSDR USAASB06125Charger · inoperativeBOS - MAINTENANCE REPORTED THE EMERGENCY LIGHTS AT THE AFT LEFT ENTRY AND AFT RIGHT SERVICE DOORS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACKS AND CHARGER ASSEMBLIES PER MM 33-51-00. OPERATIONAL CHECK GOOD.Dec 26, 2006 · N502UW · Boeing 737301 · Emergency LightingSDR SWAA065075Light · inoperativeDURING SCHEDULED MV1 CHECK, FOUND RIGHT OVERWING EMERGENCY EXIT SIDEWALL LIGHT INOP. REMOVED AND REPLACED LIGHT BULB PER MM.Dec 23, 2006 · N660SW · Boeing 737301 · Emergency LightingSDR USAA200612003Skin · crackedA 3.250 INCH CRACK FOUND AT BS 767 + 17" S-24L. INSTALLED EXTERNAL DOUBLER REPAIR PER SRM 53-00-01, REPAIR 31.Dec 20, 2006 · N502UW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA200612002Skin · crackedSKIN HAS A 1.5 INCH CRACK FOUND AT BS 747 + 13 INCHES, S-12L. INSTALLED EXTERNAL DOUBLER/TRIPLER IAW SR 53-00-01 REP. 31 AND EA 98355, TYP REP. 53-60-03A.Dec 20, 2006 · N502UW · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA061450Floorbeam · corrodedFLOORBEAM AT BS 986.5 AND RBL 44, REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW TR 53-60-01 LEVEL 2 C53-107-02. DEFECT SIZE: 6 INCHES.Dec 19, 2006 · N501UW · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA061451Angle · corrodedANGLE AT STA 727-727A, DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02 LEVEL 2 C53-202-01, DEFECT SIZE: 20 INCHES X 1INCH.Dec 19, 2006 · N501UW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA061452Floorbeam · corrodedLOCATION: STA 294.5, REMOVED DAMAGED SECTION, AND INSTALLED REPAIR PARTS IAW SRM 53-10-51 2R6 LEVEL 2 C53-202-01, DEFECT SIZE: .25 INCH.Dec 19, 2006 · N501UW · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA061453Shear Tie · corrodedSTA 984-986 BL0 STRG 26L AND 26R, REMOVED AND REPLACED STRAP AND SHEAR TIE IAW SRM 51-10-02 LEVEL 2 C53-208-01. DEFECT SIZE: 2 INCHES X 5 INCHES.Dec 19, 2006 · N501UW · Boeing 737301 · Fuselage Internal Mounting StructureSDR USAA061441Attach Angle · crackedSTA 639 LEFT SIDE JUST BELOW AND AFT OF THE OVERWING EXIT CRACKED. REMOVED DAMAGED ATTACH ANGLE AND REPLACED ANGLE IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.Dec 18, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061442Frame · crackedBS 480 FRAME CRACKED AT PSU RAIL ATTACH BRACKET BETWEEN S 8R-9R CRACKED. INSTALLED DOUBLER IAW TR 53-10-20D, DEFECT SIZE: .25 INCH.Dec 18, 2006 · N501UW · Boeing 737301 · Fuselage Main, FrameSDR USAA061422Support · corrodedFWD SERVICE DOOR SILL SUPPORTS CORRODED. BLENDED AND TREATED THREE OF FOUR ANGLES IAW SRM 51-10-02, LEVEL 2 C53-107-02, DEFECT SIZE: 2 INCHES.Dec 13, 2006 · N501UW · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA061419Skin · crackedOUTBOARD END OF NR 1 SLAT CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 57-43-01, DEFECT SIZE: .50 INCH.Dec 12, 2006 · N501UW · Boeing 737301 · Leading Edge DevicesSDR USAA061418Stringer Clip · crackedSTA 807 STR 7L HAS CORROSION. REMOVED OLD PART, REAMED HOLES IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.Dec 12, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061417Attach Angle · corrodedSTA 1011 RBL 6 HAS CORROSION. REMOVED DAMAGED BRACKET, FABRICATED AND INSTALLED REPLACEMENT IAW 65C19715 LEVEL 1 C53-107-02, DEFECT SIZE: 2 INCHES.Dec 12, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061416Attach Angle · corrodedSTA 1011 LBL 6 CORROSION. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED ANGLE IAW DWG 65C19715 LEVEL 1 C53-107-02, DEFECT SIZE: 3 INCHES.Dec 12, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061415Bracket · crackedBRACKET STA 663 BETWEEN STR 5R AND STR 6R DAMAGED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-40-00, DEFECT SIZE: 3 INCHES.Dec 12, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061420Stringer Clip · crackedBS 663 S4L CRACKED. DEFECTIVE PART REPLACED WITH IDENTICAL PART IAW SRM 51-10-02, DEFECT SIZE: .50 INCH.Dec 12, 2006 · N501UW · Boeing 737301 · Fuselage Main, Attach FittingsSDR USAA061404Skin · crackedA 49 INCHES FROM I/B END OF RIGHT O/B AFT FLAP. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: .25 INCH.Dec 11, 2006 · N591US · Boeing 737301 · Trailing Edge FlapsSDR SWAA064697Skin · crackedDURING SCHEDULED SERVICE CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 540, STR 17L. REPAIRED SKIN PER SWA EA.Dec 4, 2006 · N659SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA064632Skin · crackedDURING SCHEDULED C2 CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 730E, STR 18R. REPAIRED SKIN PER SWA EA.Nov 30, 2006 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA064631Skin · delaminatedDURING SCHEDULED C2 CHECK, FOUND LEFT WING INBOARD FOREFLAP DELAMINATED AT UPPER SURFACE. REMOVED AND REPLACED FOREFLAP PER MM.Nov 30, 2006 · N660SW · Boeing 737301 · Trailing Edge FlapsSDR USAASB06117Windshield · leakingCLT FLT 1902 - ON CLIMBOUT FROM CLT, AT 15,000 FEET, CREW REPORTED AN EXTREMELY LOUD SQUEAL FROM THE CAPTAIN'S L1 WINDSHIELD. PRESSING ON THE LEFT MIDDLE SIDE OF WINDSHIELD WOULD CHANGE THE PITCH OF THE SQUEAL. NOISE WAS BAD ENOUGH TO IMPAIR COMMUNICATION. Nov 26, 2006 · N503UW · Boeing 737301 · Flight Compartment WindowsSDR SWAA064491Skin · crackedDURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT GARGO DOOR AFT LOWER CUTOUT. REPAIRED SKIN PER ER.Nov 19, 2006 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA064490Skin · crackedDURING SCHEDULED SPV CHECK, FOUND FUSELAGE SKIN CRACKED AT AFT GARGO DOOR FWD LOWER CUTOUT. REPAIRED SKIN PER ER.Nov 19, 2006 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA064489Skin · crackedDURING SCHEDULED SPV CHECK, FOUND FUSELAGE BELLY SKIN CRACKED AT RADIO ALT ANTENNA CUTOUT, BS 450. REPAIRED SKIN PER ER & BOEING SERVICE BULLETIN.Nov 19, 2006 · N660SW · Boeing 737301 · Fuselage Main, Plate/SkinSDR SWAA064465Failsafe · crackedDURING SCHEDULED SPV CHECK, FOUND FUSELAGE FRAME FAIL-SAFE CHORD CRACKED AT BS 440, STR 27R. REPAIRED CHORD PER SRM.Nov 16, 2006 · N660SW · Boeing 737301 · Fuselage Main, FrameSDR USAASB06113Hose · leakingCLT - FLT 1627 - ON APPROACH TO CLT, FROM CHS, THE NR 2 ENGINE HYDRAULIC-B PUMP LOW PRESSURE LIGHT ILLUMINATED. CREW WENT THROUGH QUICK REFERENCE HANDBOOK PROCEDURES AND CONTINUED TO LAND. AFTER EXTENSION OF LANDING GEAR AND FLAPS, THE HYDRAULIC-B ELECTRIC PNov 15, 2006 · N501UW · Boeing 737301 · Hydraulic System, MainSDR SWAA064326Slide · out of adjustDURING SCHEDULED SPV CHECK, FOUND R2 DOOR EMERGENCY EVAC SLIDE OUT OF ADJUST. ADJUSTED EVAC SLIDE PER MM.Nov 9, 2006 · N660SW · Boeing 737301 · Escape SlideSDR PIDR2006041Frame · crackedFORWARD FRAME OF THE FORWARD CARGO DOOR CUTOUT (BS 440 FRAME) CRACKED AT LOWER FORWARD STOP FITTING. REPAIRED CRACK PER INSTRUCTIONS FROM MFG WITH FAA APPROVED 8100-9 DATED NOV.6, 2006.Nov 7, 2006 · N573US · Boeing 737301 · Fuselage Main, FrameSDR PIDR2006039Skin · delaminatedDELAMINATION AT THE IB END OF THE LT OB FORE FLAP. REPAIRED DAMAGED AREA IAW SRM 51-70-10.Nov 1, 2006 · N573US · Boeing 737301 · Trailing Edge FlapsSDR PIDR2006042Bear Strap · crackedCRACK INDICATION IN FASTENER HOLE JUST FORWARD AND BELOW THE L1 DOOR UPPER HINGE CUTOUT IN THE BEAR STRAP (SECOND LAYER) CONFIRMED BY HFEC. REPAIRED IAW MFG INSTRUCTIONS WITH FAA APPROVED 8100-9 DATED NOV 3, 2006.Oct 31, 2006 · N573US · Boeing 737301 · Fuselage Main, Plate/SkinSDR PIDR2006038Fitting · crackedLT MLG FITTINGS CRACKED AT THE NR 2 HOLE. REPLACED FITTING IAW SB 737-57-1216.Oct 27, 2006 · N573US · Boeing 737301 · Wing, Landing Gear Attach FittingsSDR USAASB06106Transmission · failedPVD - FLT 1110 ON APPROACH TO PVD FROM DCA, CREW REPORTED THE TRAILING EDGE FLAPS WOULD NOT EXTEND FOR LANDING NORMALLY OR ALTERNATE. LEADING EDGE FLAPS DID EXTEND FULLY WITH ALTERNATE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REMOVED AND REPLACOct 24, 2006 · N588US · Boeing 737301 · Trailing Edge Flap Control SystemSDR USAASB06105Transmitter · failedPIT - FLT1906 ON APPROACH TO PIT FROM ORD, CREW ADVISED DISPATCH, UNABLE TO EXTEND THE FLAPS. WHEN SELECTING INITIAL FLAPS, CREW RECEIVED A SPLIT FLAP INDICATION PRIOR TO FLAPS 1, ALONG WITH A LEADING EDGE FLAP LIGHT. CREW DECLARED AN EMERGENCY AND PERFORMEOct 24, 2006 · N502UW · Boeing 737301 · Trailing Flap Position Indicating SystemSDR PIDR2006035Beam · crackedLOWER LT AND RT INTERNAL BEAMS CRACKED. REPAIRED BEAMS SB 737-52A1079.Oct 19, 2006 · N573US · Boeing 737301 · Cargo/Baggage DoorsSDR USAASB06101Socket · corrodedBOS - MAINTENANCE REPORTED THE R2 DOOR EXTERIOR EMERGENCY ESCAPE SLIDE LIGHT, IN THE FUSELAGE, WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT SOCKET DUE TO CORROSION. OPERATIONAL CHECK GOOD.Oct 19, 2006 · N591US · Boeing 737301 · Light System WiringSDR PIDR2006033Frame · crackedCRACK IN BS 616 FRAME RT SIDE BELOW FLOOR. REPAIRED DAMAGED AREA IAW SB 737-53-1182.Oct 16, 2006 · N573US · Boeing 737301 · Fuselage Main, FrameSDR PIDR2006034Stringer · corrodedSTRINGER 28RT CORRODED BETWEEN BS 312 AND BS 328. REPLACED STRINGER SECTION IAW SRM 51-40-02.Oct 13, 2006 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA061204Frame · crackedFOUND CRACK FRAME STATION 727L ABOVE STRINGER 14L. INSTALLED DOUBLER REPAIR IAW EA 97996, DEFECT SIZE: 1".Oct 5, 2006 · N502UW · Boeing 737301 · Fuselage Main, FrameSDR USAA061205Skin · crackedFOUND CRACK BS 727D STRINGER 23L, DEFECT SIZE: 2".Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA061206Skin · crackedFOUND FUSELAGE SKIN CRACKED, BS 727D STINGER 23R. REMOVED DAMAGE AND INSTALLED REPAIR DOUBLER IAW EA 98130, DEFECT SIZE: 2".Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA061207Skin · crackedFOUND SKIN CRACKED RADIO RACK EXHAUST CUTOUT. INSTALLED DOUBLER IAW EA 98129, DEFECT SIZE: 1".Oct 5, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA061201Frame · corrodedFOUND FRAME STA 380 BETWEEN STR 28R AND 28L. REMOVED DAMAGE, INSTALLED REPAIR PARTS IAW SRM 53-00-07 REPAIR 3, DEFECT SIZE: 2" BY 4".Oct 4, 2006 · N592US · Boeing 737301 · Fuselage Main, FrameSDR USAA061202Skin · crackedFOUND CRACK BS 727D STRINGER 23R. REMOVED DAMAGE, AND INSTALLED REPAIR DOUBLER PER EA 98130, DEFECT SIZE: 2".Oct 4, 2006 · N592US · Boeing 737301 · Fuselage Main, Plate/SkinSDR SB06095Switch · dirtyON APPROACH, CREW REPORTED AN ASYMMETRICAL FLAP INDICATION AS THE TRAILING EDGE FLAPS LOCKED OUT. LT FLAP WAS INDICATING 15 UNITS AND THE RT FLAP 10 UNITS. PILOT REPORTED THERE WAS NO CONTROL ISSUE WITH THE FLAPS LOCKED OUT. FLIGHT LANDED WITHOUT FURTHER INCIDOct 4, 2006 · N592US · Boeing 737301 · Trailing Edge Flap Control SystemSDR 2007FA0000135Frame · crackedFRAME IS CRACKED AT BODY STATION 727, STRINGER 14L. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, FrameSDR 2007FA0000128Skin · dentedBODY STATION 915 ABOVE STRINGER 25L LAP JOINT FUSELAGE SKIN HAS DENT. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Plate/SkinSDR 2007FA0000126Frame · crackedFRAME IS CRACKED AT BODY STAION 727, STRINGER 14L. (K)Sep 27, 2006 · N586US · Boeing 737301 · Fuselage Main, Frame
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