Boeing 737-2B7

Service difficulty reports · 1,360

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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 = '7372B7'
  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 USAA991410Frame · crackedCLT - DURING Q-5 CHECK HFEC INSPECTION, FOUND A CRACK AT BS 727 STRINGER 18A LEFT CHORD. REPAIRED PER EA 66261 AND EO 5394G068. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, FrameSDR USAA991409Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CRACK LOWER AFT CORNER FORWARD SERVICE DOOR CUTOUT SKIN. INSTALLED TRIPLERS PER SRM 53-30-3 FIG 26. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991408Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 1 INCH AREA OF CORROSION STATION 294.5 LBL 13 TO RBL 1 FLOORBEAM. CORROSION LEVEL 2. REPLACED T-CAP PER TR 53-10-04 B. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991381Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 3 INCH AREA OF CORROSION STRINGER 28R, STATION 313 TO 324.. CORROSION LEVEL 2. INSTALLED STRINGER SPLICE REPAIR AND CLIP PER SRM 53-10-3. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA991380Door Frame · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH BY 2 INCH AREA OF CORROSION ON SURFACE STATION 847, RBL 24, AFT CARGO DOOR CUTOUT AFT FRAME. CORROSION LEVEL 1. REPAIRED PER EA 66271. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991378Stiffener · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .75 INCH CRACK AFT SIDE 663 BULKHEAD, LBL 7, 16 FT UP FROM KEEL BEAM STIFFENER. REMOVED AND REPLACED STIFFENER PER EA 66242. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991377Beam · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH CRACK IN RADIUS OF FLOOR SUPPORT ANGLE STA 294.5 RBL 54. REMOVED AND REPLACED ANGLE PER SRM 51-40-1. (X)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991376Floorbeam · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH CRACK AT BS 663, BL ZERO FLOORBEAM. INSTALLED REPAIR SECTION OF FLOORBEAM PER TR 57-10-04. (X)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991374Web · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 4 INCH BY 1 INCH DAMAGED FASTENER HOLE CUTOUT AT BS 294.5, WL 208, RBL 21-RBL 25 WEB. INSTALLED DOUBLER PER SRM 51-40-2. (X)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991372Angle · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATE HOLES IN Z-ANGLE, STA 300 TO STA 333, RBL 55 TO RBL 60, WL 208.1 CREASE BEAM INNER CHORD ANGLE. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. INSTALLED NEW Z-ANGLE PER SRM 51-10-1.Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991371Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION AROUND NUTPLATES HOLES IN FLOORBEAM 6 EACH 1 INCH BY 1 INCH STATION 328, BL 0 TO RBL 35. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. REPLACED T-CAP SECTION PER TR 53-10-13. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991370Floorbeam · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND CORROSION .5 INCH BY 5 INCH BY 15 INCHES AT BS 344, WL 208, BL 0 - LBL 15 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-01. INSTALLED REPAIR STRAPS PER TR 53-10-13. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991369Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK LEFT STRINGER 18A SHELF, STATION 725 TO 727, 4 INCHES OF SKIN. INSTALLED NEW AFT SHELF SECTION PER SRM 51-10-1 AND 51-30-3. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA991360Splice · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK IN STRINGER PRODUCTION SPLICE BS 908 STRINGER 4R. INSTALLED NEW STRINGER SPLICE PER SRM 51-10-01. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991359Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 4R STATION 767 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991358Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STRINGER 2L STATION 727A TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991338Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .1875 INCH CRACK AT STRINGER 4L STATION 907 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991337Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .3125 INCH CRACK AT STRINGER 2L STATION 867 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991336Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STRINGER 5L STATION 847 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991335Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 2L STATION 827 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991334Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 10L STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991333Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991332Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 807 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991331Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 9L STATION 787 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991330Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 6R STATION 767 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991329Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 767 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991328Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 747 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991327Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 7R STATION 727B TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01 AND SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991326Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 6L STATION 727B TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991325Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3L STATION 727B TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991324Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 7L STATION 727A TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991323Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 5R STATION 727A TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991322Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 8R STATION 706 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991321Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND TWO 1.125 INCH CRACKS AT STRINGER 4L STATION 685 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991320Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3R STATION 685 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-01. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991319Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK AT STRINGER 10R STATION 663 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991318Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 4R STATIN 639 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991317Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .125 INCH CRACK AT STRINGER 3R STATION 639 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-2. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991316Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .0625 INCH CRACK AT STRINGER 3L STATION 597 TIE CLIP. REPAIRED PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991315Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .375 INCH CRACK AT STRINGER 8L STATION 578 TIE CLIP. INSTALLED TIE CLIP PER SRM 51-30-02. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991314Tie Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND .125 INCH CRACK AT FASTENER BS 500B STRINGER 3R TIE CLIP. REPAIRED PER SRM 51-10-1. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991313Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A .25 INCH BY .25 INCH AREA OF CORROSION AROUND NUT PLATE HOLES STATION 312, LBL 7 FLOORBEAM. CORROSION LEVEL 2. CORROSION TASK NR C53-107-02. SPLICED IN NEW T-CAP SECTION PER TR 53-10-13. (M)Dec 25, 1999 · N273AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAASB99297Pressure Switch · failedBWI - FLT 2740 - ON DESCENT INTO BWI, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW SHUTDOWN THE NR 1 ENGINE AT 6,000 FT PER HANDBOOK PROCEDURES. FLIGHT LANDED AT BWI WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. TOTAL SINGLE ENGINE TIME Dec 18, 1999 · N286AU · Boeing 7372B7 · Engine Starting SystemSDR USAA991414Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK UPPER AFT CORNER OF HANDLE CUTOUT, FORWARD CARGO DOOR SKIN. INSTALLED REPAIR DOUBLER PER SRM 52-30-2 FIG 3. (M)Dec 16, 1999 · N281AU · Boeing 7372B7 · Cargo/Baggage DoorsSDR USAASB99291Pcu · failedMCO - FLT 2611 - CAPTAIN REPORTED THAT 40 MILES NORTH OF MCO, AT FL120, THEY EXPERIENCED A POSSIBLE LEFT UNCOMMANDED RUDDER MOVEMENT. ROLL DISCONTINUED WHEN AUTOPILOT WAS DISENGATED. THE FIRST OFFICER OBSERVED THE AIRCRAFT ROLLED 25 DEGREES. FLIGHT CONTINUEDDec 9, 1999 · N283AU · Boeing 7372B7 · Rudder Control SystemSDR USAA991344Floorbeam · corrodedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND CORROSION ON FLOORBEAM APPROX 6 FT FORWARD CABIN STATION 328 - RBL 51. CORROSION LEVEL. INSTALLED DOUBLER PER TR 53-10-13. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA991294Skin · crackedCLT - DURING Q-6 CHECK EDDY CURRENT INSPECTION, FOUND A 2.25 INCH CRACK AT BS 324 STRINGER 17R SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 26. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991293Skin · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A ..250 INCH CRACK AT BS 806 STRINGER 13L LOWER HINGE CUTOUT SKIN. INSTALLED FILLER AND DOUBLER PER SRM 53-30-03. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA991292Tie Clip · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND A ..25 INCH CRACK AT BS 727B STRINGER 2-23 TIE CLIP. REMOVED AND REPLACED PER SRM 51-10-1. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA991291Skin · crackedCLT - DURING Q-6 CHECK VISUAL INSPECTION, FOUND .25 INCH CRACK AT RIGHT AFT SERVICE DOOR UPPER HINGE CUTOUT SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M)Dec 8, 1999 · N276AU · Boeing 7372B7 · Fuselage Main, Plate/Skin
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