Boeing 737-4B7

Service difficulty reports · 5,757

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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 = '7374B7'
  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 USAA060062Support Angle · crackedFOUND SUPPORT ANGLE CRACKED STA 616, RBL 64.5. REMOVED DAMAGE, FAB AND INSTALLED DOUBLER PER TYPICAL REPAIR 53-62-01 FIG 2. DEFECT SIZE: CABIN AT EMERGENCY EXIT STA 616, RBL 64.5 SUPPORT ANGLE CRACKED, CRACK IS 0.25Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060063Stringer Clip · crackedFOUND STRINGER CLIP CRACKED 11R AT BS 500. REMOVED AND INSTALLED NEW FABRICATED TIE CLIP IAW BOEING DWG 69-45156 AND SRM 51-10-02, DEFECT SIZE: STRINGER 11R TIE CLIP CRACKED IN RADIUS, APPROX 0.250".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060054Frame · tornFWD CARGO DOOR CUT-OUT FWD FRAME, FABRICATED WEB REPAIR PER SRM 51-70-13 FIG 1, DEFECT SIZE: .125.Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060065Frame · crackedFOUND FRAME CRACKED STA 440 AT RT PSU SUPPORT RAIL. INSTALLED FILLER AND DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: .250" CRACK.Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060053Attach Angle · crackedFOUND ATTACH ANGLE CRACKED, STA 727B 0BL. FABRICATED NEW ANGLE AND INSTALLED SRM 51-10-02 DWG 65-45410, DEFECT SIZE: 1.00".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060067Repair · unknownFOUND PREVIOUS REPAIR L/E 81" O/B OF I/B END. UPDATED SDA AS REQUIRED IAW SRM 55-10-01, DEFECT SIZE: PREVIOUS REPAIR FOR RT HORZIONTAL REMOVABLE L/E 81" O/B OF I/B END, FLUSH PATCH.Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060068Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, L/E 38" O/B OF I/B END. MAJOR REPAIR, UPDATED SDA AS REQUIRED SRM 55-10-01. DEFECT SIZE: PREVIOUS REPAIR ON SDA FOR LEFT HORIZONTAL REMOVE L/E 38" O/B OF I/B END FLUSH PATCH.Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060069Skin · damagedABOVE RSS 140, 6" OUTBD OF FUSELAGE, UPPER WING SKIN, BLENDED DAMAGE OUT SHOT PEENED AND TREATED SKIN PER SRM 51-20-06 FIG 1, DEFECT SIZE: 7.0" BY 2.25" AREA, CHAFFED SKIN.Jan 17, 2006 · N784AU · Boeing 7374B7 · Wing, Plate/SkinSDR USAA060070Skin · gougedFOUND DEEP GOUGE AFT CARGO DOOR SKIN ABOVE HANDLE CUTOUT. REMOVED DAMAGED, INSTALLED FILLER AND DOUBLER IAW SRM 52-30-01, 52-00-01, DEFECT SIZE: 2.00" BY .016" DEEP GOUGE.Jan 17, 2006 · N784AU · Boeing 7374B7 · Cargo/Baggage DoorsSDR USAA060071Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, OUTER DOOR SKIN. UPDATED SDA AS REQUIRED IAW SRM 52-30-01, DEFECT SIZE: 34" BY 43".Jan 17, 2006 · N775AU · Boeing 7374B7 · Standard Practices/StructuresSDR USAA060072Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, 178 BULKHEAD. UPDATED SDA IAW EO 5300V153 DEFECT SIZE: UNKNOWN.Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060073Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR, I/B END LWR SURFACE. SDA UPDATED AS REQUIRED IAW TR 57-50-26A, DEFECT SIZE: UNKNOWN.Jan 17, 2006 · N775AU · Boeing 7374B7 · Wing StructureSDR USAA060074Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR I/B END UPPER SURFACE. UPDATED SDA AS REQUIRED IAW TR 57050-26A, DEFECT SIZE: 10 BY 4.Jan 17, 2006 · N775AU · Boeing 7374B7 · Wing StructureSDR USAA060075Repair · unknownFOUND SLAT SKIN WITH PREVIOUS REPAIR LWR SURFACE AT I/B AUX TRACK. SDA UPDATED AS REQUIRED IAW TR 54-43-01, DEFECT SIZE: 12" BY 4".Jan 17, 2006 · N775AU · Boeing 7374B7 · Wing StructureSDR USAA060064Structure · crackedFOUND SLAT CRACKED OTBD END, LOWER SURFACE AT AFT FASTENER ROW, 3.5" BY 8" DOUBLER ON OUTBD END INSTALLED IAW SRM 57-43-01 AND 57-56-22, DEFECT SIZE: APPROX TOT ACCUMULATIVE LENGTH 0.375".Jan 17, 2006 · N775AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060044Attach Angle · crackedFOUND ATTACH ANGLE CRACKED STA 737B 0BL. FABRICATED NEW ANGLE AND INSTALLED IAW SRM 51-10-02 DWG 65-45410, DEFECT SIZE: 1.00".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060033Frame · crackedFOUND FRAME CRACKED STA 787 FRAME BETWEEN S8L AND S9L. REPAIRED AND INSTALLED DOUBLER IAW TR 53-10-20C, DEFECT SIZE: .125".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060034Frame · crackedFOUND FRAME CRACKED 827 S9R AT I/B PSU SUPPORT BRACKET RIVET. INSTALLED DOUBLER IAW 53-10-20-C, DEFECT SIZE: .500".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060035Frame · crackedFOUND FRAME 787 CRACKED AT I/B PSU SUPPORT RIVET S9R. INSTALLED REPAIR ANGLES PER TR 52-10-20C, DEFECT SIZE: .500".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060036Floorbeam · corrodedFOUND FLOORBEAM CORRODED AT BS 986.5 AND LBL 8 TO RBL 43. REMOVED DAMAGE AND INSTALLED FABRICATED T CAP FROM LBL 6 THRU RBL 30 IAW SRM 53-60-01A, DEFECT SIZE: 6".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060037Wedge · unknownFABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-02, NR 2 SLAT UPPER O/B T/E WEDGE SURFACE, DEFECT SIZE: 3" BY 5".Jan 17, 2006 · N775AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060038Skin · crackedFOUND SKIN CRACKED STA 179 BETWEEN S-16 AND S-15L. FABRICATED DOUBLER 3" BY 5" IAW EO 5300V157, DEFECT SIZE: 3" BY 5".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Plate/SkinSDR USAA060039Wedge · unknownUPPER I/B T/E WEDGE SURFACE, FABRICATED DOUBLER THAT MEASURES 3" BY 5" IAW 57-42-01, DEFECT SIZE: 3" BY 5".Jan 17, 2006 · N775AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060040Repair · unknownFOUND SKIN WITH PREVIOUS REPAIR STA 179 BETWEEN S16R AND S15R. SDA UPDATED AS REQUIRED IAW EO 5300V157, DEFECT SIZE: 3" BY 5".Jan 17, 2006 · N775AU · Boeing 7374B7 · Aircraft StructuresSDR USAA060041Repair · unknownFOUND NR 1 ENGINE NOSE COWL AT 4 O'CLOCK POSITION. UPDATED SDA AS REQUIRED IAW SRM 54-10-01, DEFECT SIZE: 5" BY 8".Jan 17, 2006 · N775AU · Boeing 7374B7 · Nacelle/Pylon, Main FrameSDR USAA060055Skin · delaminatedFOUND DELAMINATION UPPER OTBD END OF T/E WEDGE. REMOVED DAMAGE INSTALLED CORE AND DOUBLER IAW SRM 51-70-10, DEFECT SIZE: 4.750" BY 5.250.Jan 17, 2006 · N784AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060043Skin · crackedFOUND NR 1 SLAT CRACKED, FASTENER HOLES LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW BOEING SRM 57-43-01, DEFECT SIZE: .050".Jan 17, 2006 · N775AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060032Stringer Clip · crackedFOUND TIE CLIP CRACKED AT BS 400 AND STRINGER 16R . REMOVED AND REPLACED WITH A FABRICATED TIE CLIP IAW SRM 51-10-02, DEFECT SIZE: 1".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060045Support · corrodedFOUND SUPPORT CORRODED, STA 313-328 RBL 12. REMOVED AND REPLACE WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: 1.000".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060046Floorbeam · corrodedFOUND FLOORBEAM CORRODED STA 312 FROM BLO 0 TO RBL 10.10" BY 2". INSTALLED T CAP IAW SRM 53-10-51 FIG 201, DEFECT SIZE: 10.10" BY 2".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060047Floorbeam · corrodedFOUND FLOORBEAM CORRODED, BS 927 AND RBL 10. CUT OUT TO REMOVE DAMAGE AND INSTALLED REPAIR ANGLE PER SRM 53-60-51, DEFECT SIZE: UNKNOWN.Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060048Skin · crackedFOUND NR 1 SLAT CRACKED, FASTNER HOLE LOWER SURFACE T/E. INSTALLED EXTERNAL DOUBLER IAW SRM 57-43-01, DEFECT SIZE: .050".Jan 17, 2006 · N775AU · Boeing 7374B7 · Leading Edge DevicesSDR USAA060049Shear Tie · crackedSHEAR TIE CRACKED BS 967 BETWEEN S-6L AND S7-L. REMOVED DAMAGED SECTION OF FRAME. FABRICATED AND INSTALLED REPAIR SHEAR TIE IAW SRM 53-00-07-2R-07, DEFECT SIZE: 1.5".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Internal Mounting StructureSDR USAA060050Stringer Clip · crackedFOUND TIE CLIP CRACKED, BS 312 S-27L. FABRICATED AND INSTALLED NEW TIE CLIP IAW SRM 51-40-03 AND 02 AND BOEING DRW 69-37411, DEFECT SIZE: .25".Jan 17, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060051Splice · crackedFOUND CRACK STA 908 STR 4 R. REPLACED SPLICE IAW SRM 51-10-02, DEFECT SIZE: .125".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060052Splice · crackedFOUND CRACK BS 908 AND S41L. FABRICATED SPLICE AND INSTALLED STRINGER SPLICE AND NEW TIE CLIP PER SRM 51-10-02, DEFECT SIZE: .250".Jan 17, 2006 · N775AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060042Repair · unknownPREVIOUS REPAIR UPPER IB T/E. UPDATED SDA AS REQUIRED IAW TR 57-42-02 DEFECT SIZE: 5" BY 5".Jan 17, 2006 · N775AU · Boeing 7374B7 · Wing StructureSDR USAA060013Frame · crackedFOUND CRACK STA 440, S-8L. FABRICATED ANGLES FROM NR 1133534 AND 1133533, INST DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060007Frame · defectiveBS 639 FRAME AT OVERWING DOOR STOP LT SIDE, DEFECTIVE PART REPLACED WITH IDENTICAL PART:ORDERED "T" ANGLE 1717710 STOCK, FAB`D REPLACED IAW DWG65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060006Frame · crackedFOUND CRACK BS 727F BETWEEN S-8R AND S-9R AT AIRCONDITIONAL ATTACH BRACKET. CUTOUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR ANLGE IAW TR 53-10-20C, DEFECT SIZE: APPROX 1/2" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060005Attach Angle · crackedFOUND ANGLE CRACKED BS 877; S-11L. REMOVED CRACKED ANGLE. FABRICATED AND INSTALLED NEW ANGLE IAW BOEING DRW 69-45156; SRM 51-10-02, DEFECT SIZE: APPROX 1/4" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060012Angle · crackedFOUND ANGLE CRACKED BETWEEN STA 927 AND 947.5 AT BL 0. INSTALLED NEW ANGLE IAW SRM 51-40-02, DEFECT SIZE: 1" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060014Frame · crackedFOUND FRAME CRACKED STA 907, BELOW S-8L. FAB`D FROM ANGLES NR 1133534 AND 1133533. INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: FRAME CRACKED 0.25".Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA060015Stringer Clip · crackedFOUND TIE CLIP CRACKED S-4R, BS 727E. INSTALLED NEW CLIP CC NR 1133482. INSTALLED IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL NR 5958 S-4R TIE CLIP CRACKED BS 727E.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Attach FittingsSDR USAA060009Splice · crackedFOUND STRINGER SPLICE CRACKED STA 907, S-4L. REMOVED AND REPLACED WITH NEW PART IAW SRM 51-10-02, DEFECT SIZE: .500" CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Miscellaneous StructureSDR USAA060016Floorbeam · corrodedFOUND SHEET METAL CORRODED ON FLOORBEAM STA 328 RBL 21. INSTALLED DOUBLER IAW SRM 53-00-51 FIG 201, DEFECT SIZE: SHEETMETAL ITEM 1030M EVIDENCE OF CORROSION ON FLOORBEAM 1" BY 2", STA 328 RBL 21.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA060010Floor Panel · unknownLOCATION, COCKPIT ENTRY FLOOR, REMOVED AND REPLACED W/NEW PART KIT IAW SRM 51-10-02, DEFECT SIZE: SHEETMETAL ITEM 1036, NOSE GEAR DOWN LOCK VIEW SUP STRUCTURE CRACKED ON FWD END.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Floor PanelSDR USAA060011Floorbeam · corrodedFOUND FLOORBEAM CORRODED BS 986.5 CABIN FLOORBEAM LBL 18, 21,24,30. REPLACED "T" CAP IAW TR 53-60-01A, DEFECT SIZE: SEVERAL 1" BY 1" CORRODED AREAS.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Floor BeamSDR USAA0613Frame · crackedSTA 440, S-8L CRACKED. FABRICATED ANGLES FROM 1133534 & 1133533, INSTALLED DOUBLERS IAW TR 53-10-20C, DEFECT SIZE: 0.25 INCH CRACK.Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, FrameSDR USAA068Frame · defectiveBS 639 FRAME & OVERWING DOOR STOP RIGHT SIDE DEFECTIVE. PART REPLACED WITH IDENT PART: ORDERED T-ANGLE 1717710 STOCK FAB & INSTALLED PER DWG 65-46450, DEFECT SIZE: 1.5 INCH BY 1.5 INCH MISSING T-ANGLE (MISSING SINCE MANUFACTURE).Jan 10, 2006 · N784AU · Boeing 7374B7 · Fuselage Main, Frame
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