Boeing 737-401

Service difficulty reports · 2,961

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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 = '737401'
  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 USAA070494Stringer Clip · crackedFOUND STA 344 STRINGER 11R. REMOVED AND REPLACED TIE CLIP PER SRM 51-10-02, DEFECT SIZE: 1/2".Jun 28, 2007 · N418US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA070493Angle · crackedFOUND CRACK BS 294.5, S-11L. FABRICATED AND INSTALLED NEW ANGLE PER SRM 51-40-03, BOEING DWG 65-17684, DEFECT SIZE: 1".Jun 28, 2007 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070492Intercostal · crackedFOUND CRACK STA 294.5 STRINGER 11L. REMOVED, FABRICATED AND INSTALLED NEW INTERCOSTAL PER BOEING DWG 66-14208 AND JOB CARD, DEFECT SIZE: 3".Jun 28, 2007 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070491Attach Angle · crackedFOUND CRACK STA 294.5 AT STRINGER 12L. REMOVED, FABRICATED AND INSTALLED NEW ATTACH ANGLE PR BOEING DWG 65-17684, DEFECT SIZE: .250.Jun 28, 2007 · N418US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA070490Stringer Splice · crackedFOUND CRACK BS 360 S-15L. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 51-10-02, DEFECT SIZE: .250".Jun 28, 2007 · N418US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA070482Frame · crackedINBD FASTENER HOLE FOR A/C RAIL ATTACH BRACKET, BS 400 STR 8R AND 9R. CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLERS PER 53-10-20E, DEFECT SIZE: 1/8".Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070487Stiffener · crackedFOUND BS 328 FLOORBEAM AT LBL 27, VERTICAL STIFFENER. REPLACED STIFFENER PER SRM 52-10-01, DEFECT SIZE: 1".Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070486Frame · crackedFOUND CRACKED STA 747 BETWEEN STRINGERS 8R AND 9R. INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 2".Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070485Stringer Splice · crackedFOUND CRACK BS 360 S-14L. REMOVED AND REPLACED STRINGER SPLICE PER SRM 51-20-01, DEFECT SIZE: .500.Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA070484Attach Angle · crackedVERT STIFFENER/ATTACH ANGLE FWD SIDE BS 328 FLOORBEAM LBL 45. REMOVED AND REPLACED ATTACH ANGLE PER SRM 51-10-02, DEFECT SIZE: .050.Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA070483Attach Angle · crackedVERT STIFFENER ATTACH ANGLE, AFT SIDE OF BS 328 FLOORBEAM AT LBL 45. REMOVED CRACKED ANGLE AND REPLACED WITH NEW PART PER SRM 51-10-02 DEFECT SIZE: 1/8".Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA070488Frame · crackedFOUND STA 500C ACTION: INSTALLED DOUBLER PER INSTALLED DOUBLER PER T/R 53-10-20E, DEFECT SIZE: 1".Jun 27, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR SB07049Circuit Breaker · faultyCLT FLT1053 JUST AFTER TAKEOFF FROM CLT, EN ROUTE TO NAS, CREW COULD NOT RAISE THE LANDING GEAR HANDLE. CREW FOLLOWED QUICK REFERENCE HANDBOOK PROCEDURES AND THEN RAISED THE GEAR. FOUND THE -LANDING GEAR LATCH & PRESSURE WARNING- CIRCUIT BREAKER POPPED. CONJun 23, 2007 · N425US · Boeing 737401 · Landing Gear Retraction/Extension SystemSDR USAA070473Intercostal · crackedBL 0 FASTENER HOLE AT ATTACH POINT TO BS 312 FLOORBEAM UPPER CHORD HAS CRACK. FAB'D & INSTALLED NEW REPAIR ANGLE PER SRM 51-70-13, DEFECT SIZE: .500 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070474Stiffener · crackedSTA 328, RBL 31.5 HAS CRACK. REMOVED, FAB'D & INSTALLED NEW VERTICAL STIFFENER PER SRM 51-10-02, DEFECT SIZE: .500 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070475Frame · crackedAROUND INBOARD LOCK FASTENER HEAD AT STA 867 BETWEEN S81 & S91 HAS CRACK. CUT OUT DAMAGE & INSTALLED DOUBLER PER TR 53-10-20E, DEFECT SIZE: .0625 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070476Stringer · crackedBS 295 S-10L HAS CRACK. FABRICATED STRINGER REPAIR PER SRM 51-70-11, DEFECT SIZE: .250 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA070477Rib · crackedLEFT WING RIB STA 135.5 AFT END JUST BEFORE REAR SPAR HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PER EA 98713, DEFECT SIZE: .625 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Wing, Rib/BulkheadSDR USAA070478Frame · crackedFUSELAGE FRAME STA 787 BETWEEN STR 8L & 9L AT A/C PSU RAIL ATTACH BRACKET HAS CRACK. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLERS PER TR 53-10-20E, DEFECT SIZE: .0625 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070479Frame · crackedBS 440 FWD CARGO DOOR FWD FRAME WL 180 HAS CRACK. REMOVED DAMAGE & INSTALLED REPAIR PARTS PER SRM 51-10-02 & DWG 65-20722, DEFECT SIZE: .125 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070480Frame · crackedBS 492 FWD CARGO DOOR AFT FRAME S-24R WL 163 HAS CRACK. REMOVED & REPLACED FWD CARGO AFT FRAME PER SRM 51-10-02, DWG 65-20723, DEFECT SIZE: .500 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Main, FrameSDR USAA070481Shear Tie · crackedSTA 1040 BETWEEN S2L AND S3L HAS CRACK. FABRICATED SHEAR TIE, HEAT TREATED & INSTALLED PER SRM 51-40-02, 51-20-01, DEFECT SIZE: .5 INCH.Jun 22, 2007 · N418US · Boeing 737401 · Fuselage Internal Mounting StructureSDR USAA070467Floorbeam · corrodedBS 328, LBL 28 - RBL 53, T-CAP CORRODED AT FASTENER HOLES. T-CAP OF FLOORBEAM REPAIR INSTALLED PER SRM 53-10-51; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: .25 X .25 INCH.Jun 18, 2007 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA070468Skin · damagedBS 796 S-25R, SKIN CREASE. INSTALLED DOUBLER PER EA 98668, DEFECT SIZE: 3 INCHES.Jun 18, 2007 · N420US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA070453Support Angle · corrodedBS 318-340, S17L; DOORWAY SILL SUPPORT ANGLE HAS CORROSION. INSTALLED NEW ANGLE PER SRM 51-10-02, 51-30-00; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: .5 X 1 INCH.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070459Door Frame · crackedCRACK IN FRAME WEB, FWD CARGO DOOR FWD FRAME AT LOWER DOOR STOP FITTING. INSTALLED REPAIR DOUBLER PER EA 98691, DEFECT SIZE: 1.5 INCH.Jun 7, 2007 · N424US · Boeing 737401 · Fuselage Main, StructureSDR USAA070457Floorbeam · corrodedBS 328 + 8, RBL 44 - 59 FLOORBOARD SUPPORT HAS CORROSION. NEW SUPPORT INSTALLED PER SRM 51-10-02; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 3 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA070456Attach Angle · corrodedZ-SHAPED DOOR SILL ATTACH ANGLE BS 322 - 334, LBL 60 HAS CORROSION. REMOVED & REPLACED ANGLE PER SRM 51-10-02; CORR TASK C53-107-01; LEVEL 2, DEFECT SIZE: 12 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA070454Floorbeam · corrodedBS 344, LBL 35 - RBL 8, TEE CAP OF FLOORBEAM HAS CORROSION. FABRICATED REPAIR PARTS & INSTALLED PER TR 53-10-01B, SRM 53-10-51 REP 6; CORR TASK C53-107-02, DEFECT SIZE: 3 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA070446Frame · crackedTHREE EACH RADIATING CRACKS AT STA 480L, BETWEEN S8L & S9L. CUT OUT CRACKED AREA, INSTALLED REPAIR ANGLES PER TR 53-10-20E, DEFECT SIZE: .080 INCH.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, FrameSDR USAA070452Sill · corrodedSEVERAL; AREAS, BS 312 - 354, S-17: Z-CHORD ANGLE AT FWD, ENTRY DOOR SILL HAS CORROSION. INSTALLED NEW ANGLE PER SRM 51-10-02, 51-20-00; CORR TASK C53-107-01, CORR LEVEL 2, DEFECT SIZE: 1 X 1 INCH.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070451Skin · corrodedSTA 753 BL 0 HAS CORROSION. CUT OUT DAMAGE, INSTALLED DOUBLER PER SRM 53-00-01 FIG 201, REP 31; CORR LEVEL 1, DEFECT SIZE: 2 X 2 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA070450Floorbeam · corrodedBS 312, LBL 11 - RBL 49; CABIN FLOORBEAM, UPPER CHORD HAS CORROSION. FAB'D & INSTALLED NEW FLOORBEAM UPPER CHORD SECTION & SPLICE ANGLES PER SRM 53-10-51, REP 5, DEFECT SIZE: 1 X 2 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA070449Skin · delaminatedOUTBOARD END UPPER & LOWER T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED INTERNAL & EXTERNAL DOUBLERS & INSTALLED. DEFECT SIZE: 9 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Leading Edge DevicesSDR USAA070448Skin · delaminatedINBOARD END OF NR 1 SLAT T/E DELAMINATED. REMOVED DAMAGED AREA, FABRICATED DOUBLER & INSTALLED PER SRM 51-70-10, DEFECT SIZE: 1 X 3 INCHES.Jun 7, 2007 · N420US · Boeing 737401 · Leading Edge DevicesSDR USAA070447Floor Support · crackedCRACKS, 3 EA, BS 500G - BS 520, BL-0. NEW SUPPORT INSTALLED PER SRM 51-10-02, DEFECT SIZE: 1 INCH.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070455Angle · corrodedZEE ANGLE, RBL 59 FS 947 - 990 AFT UPPER FLANGE. L ANGLE REPAIR INSTALLED PER SRM 51-70-11; CORR TASK C53-107-02; LEVEL 2, DEFECT SIZE: 1 INCH.Jun 7, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070432Intercostal · crackedRADIUS OF INTERCOSTAL TO SKIN ATTACH ANGLE JUST ABOVE S10L BS 301 HAS CRACK. FABRICATED NEW WEB & INSTALLED PER DWG 65-17684, SRM 51-10-02, DEFECT SIZE: 2 INCHES.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070433Intercostal · crackedAFT END OF SKIN TO INTERCOSTAL ATTACH ANGLE AT S13, BS 301 HAS CRACK. FABRICATED NEW PART & INSTALLED PER DWG 65-17684, SRM 51-10-02, DEFECT SIZE: 1 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070434Door Frame · crackedFWD SERVICE DOOR CUTOUT FWD FRAME LOWER STRINGER 17 HAS CRACK. INSTALLED FILLER AND REPAIR ANGLE PER SRM 51-70-11, DEFECT SIZE: 3 INCHES.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, StructureSDR USAA070435Angle · crackedINNER CHORD ANGLE, RT SIDE BETWEEN STA 291.5 & 294, STR 17 HAS CRACK. REMOVED & REPLACED ANGLE PER SRM 51-10-02, DEFECT SIZE: 2.5 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070436Stringer · crackedSTA 907, S4L, STRINGER SPLICE HAS CRACK. REMOVED DAMAGED PART, INSTALLED NEW SPLICE PART PER SRM 53-40-02, DEFECT SIZE: .250 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA070437Skin · crackedCHAFE AREA FWD & AFT OF CRACK, BS 880.60, S1L, LEFT DOSAL FIN SEAT AREA. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TRIPLER, DEFECT SIZE: 2 INCH CRACK AND 12 X 1 INCH CHAFE.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA070438Rib · crackedNR 7 RIB OF LEADING EDGE ON LEFT HORIZONTAL STAB, CRACK & FASTENER PULLED. REMOVED AND REPLACED RIB PER SRM 51-40-00, DEFECT SIZE: .5 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Horizontal Stabilizer, Spar/RibSDR USAA070439Gusset · crackedUPPER RADIUS, STA 259.5, BL 0 HAS CRACK. REMOVED DAMAGED GUSSET & REPLACED WITH NEW PER SRM 53-1-14, FIG 101, DEFECT SIZE: 2 INCHES.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070440Angle · crackedMED STUB BEAM TURN DOWN ANGLE, STA 294, ADJACENT TO S12L HAS CRACK. REMOVED DAMAGED PART & INSTALLED NEW PER SRM 51-10-02, BOEING DWG 65-17684, DEFECT SIZE: 0.5 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA070441Frame · crackedBS 867, BETWEEN S-8R AND S-9R HAS CRACKS. CUT OUT CRACKS, INSTALLED REPAIR ANGLES PER TR 53-10-20E, DEFECT SIZE: .5 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, FrameSDR USAA070442Skin · crackedCRACK & DEEP CHAFED AREA FOUND AFT OF CRACK AT BS 880.60, S1L, LT DORSAL. REMOVED DAMAGED AREA & INSTALLED DOUBLER & TRIPLER PER SRM 53-60-01, DEFECT SIZE: 2 INCH CRACK, 12 X 1 INCH CHAFED.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA070443Floorbeam · crackedSTA 578, RBL 64 JUST BELOW CABIN FLOOR LEVEL NEAR S-18R HAS CRACK. REMOVED & REPLACED FLOOR SUPPORT PER SRM 51-10-02, BOEING DWG 6AA5C32755, DEFECT SIZE: 0.5 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA070444Frame · crackedSTA 440R BETWEEN S8R & S9R AC SUPPORT BRACKET ATTACH POINT HAS CRACK. REPAIRED PER T/R 53-10-20E, DEFECT SIZE: .125 INCH.Jun 6, 2007 · N420US · Boeing 737401 · Fuselage Main, Frame
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