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 USAA061326Frame · crackedBS 380 FRAME BETWEEN S-19L S-23L CRACKED. FABRICATED AND INSTALLED REPAIR ANGLE IAW SRM 51-70-11, DEFECT SIZE: .50 X 1 INCH.Nov 6, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061314Skin · gougedLEFT STAB L/E STA 133.15 GOUGED. REMOVED DAMAGE, INSTALLED FILLER, SHIMS AND DOUBLER IAW SRM 55-10-01 FIG 201, DEFECT SIZE: .22 X .05 X .022 INCH.Nov 6, 2006 · N406US · Boeing 737401 · Horizontal Stabilizer, Plate/SkinSDR USAASB06109Ignition Unit · faultyCHS FLT1758 DURING CRUISE, ENROUTE FROM PBI TO PHL, CREW RECEIVED AN OVERHEAT WARNING ON THE NR 1 ENGINE CSD. CREW ACCOMPLISHED QRH PROCEDURES AND DISCONNECTED THE NR 1 ENGINE CSD. WHEN ATTEMPTING TO START THE APU AT VARIOUS ALTITUDES, THE APU WOULD NOT STNov 1, 2006 · N423US · Boeing 737401 · APU Start/Ignition SystemSDR USAA061306Slat Track · delaminatedNR 1 SLAT T/E 15 INCHES I/B OF I/B AUX TRACK DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 3 INCHES.Nov 1, 2006 · N406US · Boeing 737401 · Leading Edge DevicesSDR USAA061307Skin · delaminatedHORIZONTAL STAB STA 83.00 UPPER T/E DELAMINATED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 98185, DEFECT SIZE: 2 INCHES.Nov 1, 2006 · N406US · Boeing 737401 · Horizontal Stabilizer, Plate/SkinSDR USAA061308Floor Support · corrodedCARGO BAY STA 500G RIGHT SIDE CORROSION. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR PARTS IAW SRM 51-70-12 LEVEL 2 C53-208-01, DEFECT SIZE: 4 X 1 INCHES.Nov 1, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061309Angle · gougedSUPPORT UPPER ANGLE AT STA 383 LBL 10 GOUGED. REMOVED DAMAGED PART AND INSTALLED FABRICATED REPAIR PART IAW SRM 51-30-01, DEFECT SIZE: 2 INCHES.Nov 1, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061285Floorbeam · corrodedFOUND CORROSION STA 967 LBL 30. FABRICATED UPPER CHORD REPLACEMENT CAP AND REPAIR SPLICE ANGLES IAW TR 53-10-05B LEVEL 1, DEFECT SIZE: 1".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA061294Skin · crackedFOUND SKIN CRACKED NR 1 ENG PYLON AT PANEL 5727 O/B SIDE. INSTALLED DOUBLER IAW TY 54-30-07, DEFECT SIZE: 3".Oct 30, 2006 · N406US · Boeing 737401 · Nacelle/Pylon, Attach FittingsSDR USAA061290Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STA 986. INSTALLED NEW T CAP IAW TY 53-10-05B, LEVEL 1 C53-107-02, DEFECT SIZE: 2" BY 60".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA061288Skin · corrodedFOUND SKIN CORRODED, STA 795 BL0. INSTALLED DOUBLER IAW SRM 53-00-01, DEFECT SIZE: 6" BY 8".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA061286Channel · corrodedFOUND CORROSION STA 500-500A 0BL S2R-2L. REMOVED OLD ANTENNA BASE. INSTALLED NEW IAW 65-45783 LEVEL 2, DEFECT SIZE: 6.0".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061277Frame · crackedFOUND FRAME CRACKED BS 727 STR 15L. INSTALLED DOUBLERS IAW EA 98146, DEFECT SIZE: 1.05".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061280Stop Fitting · crackedFOUND CRACK STA 294.5 UPPER FWD STOP FITTING. REMOVED DAMAGED PART AND REPLACED WITH NEW IAW SRM 51-10-02, DEFECT SIZE: .25".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, StructureSDR USAA061279Stringer Clip · crackedFOUND CLIP CRACKED, STA 277, S10R. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, DEFECT SIZE: .25".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA061278Floorbeam · corrodedFOUND FLOORBEAM CORRODED, STA 967 LBL30. FABRICATED UPPER CHORD REPLACEMENT CAP AND REPAIR SPLICE ANGLES IAW TR 53-10-05B LEVEL1, DEFECT SIZE: 1" BY .5".Oct 30, 2006 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAASB06108Fan · failedCLT - FLT945 - EN ROUTE FROM ROC TO CLT, CREW REPORTED EXHAUST FUMES IN CABIN AND FLIGHT DECK. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE LEFT RECIRCULATION FAN INOPERATIVE DURING OPERATIONAL CHECK. REPLACED THE LEFT RECIRCULATION FAN ANDOct 27, 2006 · N425US · Boeing 737401 · Air Distribution FanSDR USAA061275Skin · corrodedTRAILING EDGE LIP OF OUTER SKIN CORROSION. BLENDED MINOR SURFACE CORROSION, IAW SRM 52-40-01, DEFECT SIZE: 3 X .50 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Electrical/Electronic Compartment DoorsSDR USAA061274Intercostal · crackedSTA 294.5, S12L CRACKED. REMOVED DAMAGED PART, INSTALLED NEWLY FABRICATED PART IAW SRM 51-40-02, DEFECT SIZE: .5 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061273Floor Support · corrodedSTA 500 PLUS 6 CORROSION. REPLACED WITH IDENTICAL PART, FABRICATED NEW PART IAW BOEING DWG 69-41210 LEVEL 1, DEFECT SIZE: 1 X 1 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061272Hinge · corrodedFWD E AND E DOOR O/B SIDE OF HINGE ARM CORROSION. BLENDED OUT MINOR SURFACE CORROSION, WITHIN LIMITS PER SRM 52-40-02, DEFECT SIZE: 1 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Service DoorsSDR USAA061271Bracket · crackedSTA 500-500A CRACKED. REMOVED DAMAGED PART, INSTALLED NEW FABRICATED PART IAW SRM 51-10-02, DEFECT SIZE: .500 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061270Angle · corrodedSTA 990 LBL 40 CORROSION. REMOVED AND REPLACED WITH PART WITH IDENTICAL PART IAW SRM 53-60-51 LEVEL 1 C53-107-02, DEFECT SIZE: 1 X 2 INCHES.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Main, Attach FittingsSDR USAA061269Angle · corrodedSTA 947-990 AT AFT EMERGENCY DOOR UNDER THRESH HOLD. INSTALLED NEW Z-ANGLE IAW SRM 51-10-02, DEFECT SIZE: 6 INCHES.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061268Frame · dentedFRAME DENT IN UPPER FLANGE AT STA 747 S25R. INSTALLED DOUBLER IAW SRM 51-40-02, DEFECT SIZE: .5 INCH.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061267Floorbeam · corrodedSTA 986 FLOORBEAM HAS CORROSION. INSTALLED NEW T-CAP IAW 53-10-05B, DEFECT SIZE: 2 X 60 INCHES.Oct 27, 2006 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA061262Skate Angle · wornVERTICAL STAB FWD END OF SKATE ANGLE HAS WEAR. FABRICATED AND INSTALLED REPAIR PART IAW SRM 51-10-02, DEFECT SIZE: 1 X 2 INCHES.Oct 25, 2006 · N406US · Boeing 737401 · Vertical StabilizerSDR USAA061263Angle · wornFWD END OF LEFT SKATE ANGLE AT VERTICAL STAB HAS WEAR. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-10-02, DEFECT SIZE: 1 X 2 INCHES.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061261Intercostal · crackedBS 328 LBL 45 CRACKED. REMOVED AND REPLACED WITH NEW INTERCOSTAL, DEFECT SIZE: 1 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061260Skin · crackedINTERIOR SKIN 5TH STOP FITTING FROM BOTTOM CRACKED. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 52-10-16, DEFECT SIZE: .25 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Passenger/Crew DoorsSDR USAA061259Flap Track · wornNR 5 FLAP TRACK HAS WEAR. FABRICATED AND INSTALLED NEW PART IAW DWRG 69-50719, DEFECT SIZE: .25 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Trailing Edge FlapsSDR USAA061258Stiffener · crackedREAR SPAR BULKHEAD STA 663 LBL 6.15 LBL 24 CRACK. FABRICATED AND INSTALLED REPAIR PART IAW DWG 654502, DEFECT SIZE: .25 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Wing Miscellaneous StructureSDR USAA061257Frame · crackedBS 616 RIGHT FRAME CRACK. FABRICATED 5' REPAIR ANGLE IAW T/R 53-62-01, DEFECT SIZE: .50 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061256Support · corrodedAT 727G BETWEEN STR 24L-25L CORROSION. REPLACED PART IAW SRM 51-40-02 LEVEL 1 C53-202-01, DEFECT SIZE: 2 INCHES.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061253Frame · crackedSTA 907R S8R AND S9R CRACKED. FABRICATED TWO FRAME DOUBLERS IAW SRM 53-10-20, DEFECT SIZE: .25 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061252Frame · crackedSTA 380 S9R CRACKED. REMOVED DAMAGE, INSTALLED 11 INCH DOUBLER REPAIR PARTS IAW TR 53-10-20D, DEFECT SIZE: .180 INCH.Oct 25, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061264Skin · debondedNR 4 SLAT UPPER INBOARD SURFACE DISBOND. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRM 51-70-10, DEFECT SIZE: 3 X 5 INCHES.Oct 25, 2006 · N406US · Boeing 737401 · Leading Edge DevicesSDR USAA061246Strap · crackedFOUND STRAP CRACKED, BS 328 BL 0. REMOVED CRACKED STRAP AND INSTALLED NEW ONE, IAW SRM 51-10-02, DEFECT SIZE: 1.50".Oct 23, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061247Skin · delaminatedFOUND NR 5 SLAT UPPER TE WEDGE. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 3.0" BY 6.50".Oct 23, 2006 · N406US · Boeing 737401 · Leading Edge DevicesSDR USAA061248Intercostal · crackedFOUND INTERCOSTAL WEB CRACKED, BS 294 S16L. FABRICATED AND INSTALLED NEW INTERCOSTAL IAW SRM 53-10-15, DEFECT SIZE: 4".Oct 23, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061249Stiffener · crackedFOUND CRACK, BS 328 LBL 45 TOP RADIUS OF VERTICAL STIFFENERS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-01, DEFECT SIZE: 1.5" AND 1.25".Oct 23, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061243Web · crackedAFT SERVICE ENTRY CUTOUT, CRACK IN LOWER END OF CUTOUT STA 947 S11R. REMOVED DAMAGED, INSTALLED REPAIR PARTS IAW SRM 51-70-11, DEFECT SIZE: .175 INCH.Oct 19, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061244Floorbeam · corrodedSTA 344 LBL 34 TO RBL 60 CORROSION. PART REPLACED WITH IDENTICAL T-CAP IAW SRM 53-10-51 FIG 101 LEVEL 1, DEFECT SIZE: 2 X 40 INCHES.Oct 19, 2006 · N406US · Boeing 737401 · Fuselage Main, Floor BeamSDR USAA061245Skin · crackedUPPER LT CORNER OF CAPTAINS WINDOW CRACKED. REMOVED DAMAGED, INSTALLED FILLER IAW SRM 53-10-01, DEFECT SIZE: .500 INCH.Oct 19, 2006 · N406US · Boeing 737401 · Fuselage Main, Plate/SkinSDR USAA061242Frame · crackedSTA 303 STR 8L CRACKED. REMOVED DAMAGE AND INSTALLED FABRICATED REPAIR IAW SRM 51-40-02, DEFECT SIZE: 1 INCH.Oct 18, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061221Attach Bracket · crackedBS 360 S11L CRACK. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 51-10-02, DEFECT SIZE: 1 INCH.Oct 16, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061222Channel · corrodedS947.5 RBL 13.8 CORROSION. REPLACED WITH IDENTICAL PART IAW SRM 51-40-02, DEFECT SIZE: .25 INCH.Oct 16, 2006 · N406US · Boeing 737401 · Fuselage Miscellaneous StructureSDR USAA061220Stringer Splice · crackedSTA 360 S15L CRACK. INSTALLED NEW SPLICE IAW DWG 65-61777-7, DEFECT SIZE: 1 INCH.Oct 16, 2006 · N406US · Boeing 737401 · Fuselage Main, Longeron/StringerSDR USAA061219Frame · crackedBS 492.4 S24R CRACK. REMOVED CRACKED FRAME. DRILLED UP AND INSTALLED NEW FRAME IAW SRM 51-10-02, DEFECT SIZE: .75 INCH.Oct 16, 2006 · N406US · Boeing 737401 · Fuselage Main, FrameSDR USAA061217Stringer Splice · corrodedSTA 907 S22R CORROSION. PART REPLACED WITH IDENTICAL PART IAW SRM 51-40-02 LEVEL 1 C53-202-01, DEFECT SIZE: 6 X 2 INCHES.Oct 13, 2006 · N406US · Boeing 737401 · Fuselage Main, Longeron/Stringer
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