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 USAA001442Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED .09375 INCH AROUND SCREW HOLES, OUTBOARD SEAT TRACK RIGHT SIDE BETWEEN STATION 663 AND 685. CORROSION LEVEL 1, TASK NR C53-107-01. BLENDED PER SRM 53-00-52 PER SRM SRM 53-00-52. (M)Aug 28, 2000 · N577US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAASB00231Wire · brokenPIT - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BEHIND THE LEFT WING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SPLICE JUST ABOVE EMERGENCY LIGHT IN AFT CARGO BAY. INSTALLED NEW SPLICE. OPS CHECK GOOD. (M)Aug 26, 2000 · N354US · Boeing 737301 · Light System WiringSDR USAASB00232Light · failedCLT - PILOT REPORTED THAT THE RIGHT AFT GALLEY DOOR EMERGENCY EXIT LIGHT IS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Aug 26, 2000 · N588US · Boeing 737301 · Emergency LightingSDR USAA001356Clevis · corrodedCLT - FOUND CLEVIS LUG CORRODED .5 INCH BY .5 INCH, RIGHT HORIZ STAB FORWARD UPPER CLEVIS ON BOX BEAM. CORROSION LEVEL 1. MACHINED SPOT FACES BOTH FORWARD AND AFT CLEVIS LUGS PER SRM 55-10-10. (M)Aug 25, 2000 · N573US · Boeing 737301 · Empennage Flight Control Surfaces, Attach FittingsSDR USAA001355Clevis · corrodedCLT - FOUND CLEVIS LUG CORRODED .5 INCH BY .5 INCH, FORWARD AND AFT CLEVIS LUGS LEFT HORIZ STAB. MACHINE SPOT FACES BOTH FORWARD AND AFT CLEVIS LUGS PER SRM 55-10-10. CORROSION LEVEL 1. (M)Aug 25, 2000 · N573US · Boeing 737301 · Empennage Flight Control Surfaces, Attach FittingsSDR USAA001358Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FRAME 867 BETWEEN STRINGER 8R AND 9R. FABRICATED DOUBLER AND FILLER PER TR 53-10-14. (M)Aug 25, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001357Frame · crackedCLT - FRAME CRACKED .25 INCH, STATION 787 STRINGER 9LT. FABRICATED REPAIR DOUBLER AND INSTALLED PER TR 53-10-14. (M)Aug 25, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR SWAA001609Light · inoperativeDURING SCHEDULED C4 CHECK, FOUND FWD SERVICE DOOR EMERGENCY LIGHT INOP. RELAMPED PER MM.Aug 25, 2000 · N660SW · Boeing 737301 · Emergency LightingSDR USAA001525Stringer · corrodedPIT - FOUND STRINGER CORRODED, INBOARD OF OUTBOARD SEAT TRACK RIGHT SIDE STATION 615-639. CORROSION LEVEL 1, TASK NR C53-107-01. TREATED AND PRIMED NUTPLATE AREA PER SRM 51-10-02 AND 53-00-52. (M)Aug 24, 2000 · N577US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001436Floorbeam · corrodedPIT - FOUND FLOORBEAM AND SUPPORTS CORRODED .5 INCH BY 4 INCHES, STATION 947-967, LEFT TO RIGHT CUSP. CORROSION LEVEL 1, TASK NR C53-107-02. REPLACED FLOORBEAMS PER SRM 51-40-02. (M)Aug 24, 2000 · N577US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001328Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FS 847 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Aug 24, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001327Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FS 827 BETWEEN STRINGER 8R AND 9R. INSTALLED DOUBLER PER TR 53-10-14. (M)Aug 24, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001326Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, FS 787 BETWEEN STRINGER 8R AND 9R. INSTALLED REPAIR DOUBLER PER TR 53-10-14. (M)Aug 24, 2000 · N573US · Boeing 737301 · Fuselage Main, FrameSDR USAA001325Web · corrodedCLT - FOUND WEB CORRODED 1 INCH BY 1 INCH, CREASE BEAM SHEAR WEB BETWEEN 616/639, STRINGER 17R. INSTALLED NEW WEB SRM 51-10-02 AND TR 53-10-02. (M)Aug 24, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001343Beam · corrodedPIT - FOUND BEAM CORRODED .5 INCH BY .75 INCH, RBL 18 AND 368. CORROSION LEVEL 1, TASK NR C53-107-02. CLEANED CORROSION, TREATED AND PRIMED PER SRM 51-10-02. (M)Aug 24, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001520Stringer · gougedPIT - FOUND STRINGER HAS GOUGED METAL, LOWER RIGHT SIDE BS 492.4 AND ABOVE SIDE PLATE RBL 21.8. REMOVED AND REPLACED AFFECTED AREA. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001518Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED .25 INCH, AFT LEFT LAV, FORWARD MOUNT HOLES. CORROSION LEVEL 1, TASK NR C53-107-02. DEFECTIVE PART REPLACED WITH IDENTICAL PAR NR PER SRM 51-40-00. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001533Plate · corrodedPIT - FOUND SIDE PLATE CORRODED 1 INCH BY 15 INCHES, ALL NUTPLATES ON SIDE PLATE AT RBL 21.8 BS 500D-500. CORROSION LEVEL 1. REMOVED CORROSION, TREATED, PRIMED AND INSTALLED SILL PLATE PER MM 51-20-01. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001532Frame · corrodedPIT - FOUND STRINGER CORRODED 1 INCH BY 10 INCHES, UNDER NUTPLATES ON FRAME 500D STRINGER 18R-26R. CORROSION LEVEL 1. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-20-04. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, FrameSDR USAA001531Floor Support · corrodedPIT - FOUND CORRSION 1 INCH BY 6 INCHES, FLOOR SUPPORT AFT OF BS 500, MINOR AT BBL 0.0 RIVET. CORROSION LEVEL 1. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-40-02. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001530Stringer · corrodedPIT - FOUND STRINGER CORRODED .5 INCH BY .5 INCH, UNDER NUTPLATE STRINGER 246 BS 500. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-40-02, AND 51-10-02, AND 51-20-01. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001529Skin · corrodedPIT - FOUND SKIN CORRODED 2 INCHES BY 1 INCH, BS 500D LBL 21.8 ON SIDE PLATE. CORROSION LEVEL 1. REMOVED CORROSION, TREATED AND PRIMED PER SRM. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Plate/SkinSDR USAA001528Stringer · corrodedPIT - FOUND STRINGER CORRODED 10 INCHES BY 3 INCHES, STATION 540-520 AND STRINGER 276 KEEL BEAM. CORROSION LEVEL 1. TREATED AND PRIMED PER SRM. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001527Stringer · corrodedPIT - FOUND STRINGER CORRODED 6 INCHES BY 3 INCHES, STATION 540-520 AND STRINGER 276 KEEL BEAM. TREATED AND PRIMED PER SRM. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001519Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED .25 INCH, CENTER LAV MOUNTS AFT OF STATION 1016. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-00. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, Floor BeamSDR USAA001461Frame · crackedPIT - FOUND CIRCUM FRAME CRACKED .5 INCH, FS 787L AT PSU SUPPORT BRACKET. FABRICATED SUPPORT BRACKET PER 53-10-14. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, FrameSDR USAA001460Frame · crackedPIT - FOUND FRAME CRACKED 1 INCH, CIRCUM FRAME 827L AND PSU SUPPORT BRACKET. FABRICATED SUPPORT BRACKET PER SRM 53-10-14. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, FrameSDR USAA001459Frame · crackedPIT - FOUND CIRCUM FRAME CRACKED 1.5 INCHES, FS 867 RT PSU SUPPORT BRACKET RIVET HOLE. FABRICATES SUPPORT BRACKET PER 53-10-14. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Main, FrameSDR USAA001458Seat Track · corrodedPIT - FOUND 3 INCHES OF CORROSION ON SEAT TRACK BETWEEN STATION 663.75-685, LT OUTBOARD. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-00-52, MM 51-20-01. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001457Angle · corrodedPIT - FOUND .500 INCH CORROSION, LT SIDE CREASE BEAM ATTACH ANGLE STATION 696. CORROSION LEVEL 1, TASK NR C53-107-01. REMOVED CORROSION, TREATED AND PRIMED PER CPM 20-40-00. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001456Crease Beam · corrodedPIT - FOUND BEAM CORRODED .250 INCHES IN DIAMETER, TOP OF CREASE BEAM LT SIDE BETWEEN STATION 706-727. REMOVED CORROSION, TREATED AND PRIMED PER SRM 51-10-02. (M)Aug 23, 2000 · N577US · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA0000599Frame · crackedC-CHECK, CO-PILOTS WINDOW FRAME CRACKED EXTERIOR UPPER LT CORNER. REMOVED DAMAGE FROM FRAME AND GUSSET, INSTALLED REPAIR PARTS IAW 737 SRM 53-10-01 FIG 210.Aug 23, 2000 · N325AW · Boeing 737301 · Flight Compartment WindowsSDR AWXA0000598Frame · crackedC-CHECK, CAPTIANS WINDOW FRAME CRACKED EXTERIOR UPPER RT CORNER. REMOVED DAMAGE FROM FRAME AND GUSSET, INSTALLED REPAIR PARTS IAW 737 SRM 53-10-01 FIG 210.Aug 23, 2000 · N325AW · Boeing 737301 · Flight Compartment WindowsSDR AWXA0000597Channel · corrodedC-CHECK, HAT CHANNEL AT FS 986.5 RBL 16 IS CORRODED AROUND FASTENER HOLE AT I/B END. REMOVED PART, FABED, AND INSTALLED HAT CHANNEL IAW 737 SRM 51-40-02 AND DWG 66C19883.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Miscellaneous StructureSDR AWXA0000596Angle · crackedC-CHECK, AFT CARGO DOOR, TOP AFT INTERNAL WEB CRACKED ON O/B SIDE. REMOVED, FABED, AND INSTALLED ANGLE IAW 737 SRM 51-70-11 AND 51-40-02.Aug 23, 2000 · N325AW · Boeing 737301 · Cargo/Baggage DoorsSDR AWXA0000595Frame · damagedC-CHECK, FRAME SPLICE DAMAGED FS 1006 STR 23R OVERSIZED HOLES AND COUNTERSINKS. REMOVED, FABED, AND INSTALLED REPAIR SPLICE IAW 737 SRM 53-00-07 FIGS 101 AND 201, SRM 51-40-02, AND 51-20-01.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000594Frame · corrodedC-CHECK CORROSION, FRAME AT FS 1006 STR 19R - 20R CORRODED. REMOVED, FAB''D, AND INSTALLED REPAIR SEGMENT IAW 737 SRM 51-90-05, 53-00-07, AND 51-40-05.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000593Frame · crackedC-CHECK, SIDE CHORD CRACKED FS 178 WL 207 RBL 26. OPENED WEB, VERIFIED NO CRACK (HFEC) CUT ACCESS HOLES, FAB''''D AND INSTALLED DOUBLERS AND COVER PLATES IAW 737 SRM 53-10-08 FIG 204, 53-10-08 FIG 206, AND 51-40-02.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000592Frame · crackedC-CHECK, SIDE CHORD CRACKED FS 178 WL 207 LBL 26. OPENED WEB, VERIFIED NO CRACK (HFEC), CUT ACCESS HOLES, FABED AND INSTALLED DOUBLERS AND COVER PLATES IAW 737 SRM 53-10-08 FIG 204, 53-10-08 FIG 206, AND 51-40-02.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000591Skin · damagedC-CHECK, AFT FUSLAGE BELLY SKIN CREASED AT STA 827 STR 27L AND 27R. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER, AND INSTALLED REPAIR PARTS IAW 737 SRM 53-00-01.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, Plate/SkinSDR AWXA0000590Frame · corrodedC-CHECK CORROSION LEVEL 1, AFT CARGO BIN FRAME AT 727B LT SIDE CORRODED STR 25-26R. REMOVED DAMAGED AREA, FAB''D, AND INSTALLED REPAIR PARTS IAW 737 SRM 53-00-07.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000589Frame · corrodedC-CHECK CORROSION LEVEL 1, FS 807 AND 827 STR 27L AND 27R GUSSETS ARE CORRODED. REMOVED DAMAGED SECTION, FABED, AND INSTALLED REPAIR PARTS IAW 737 SRM 53-00-07 FIG 203.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000588Frame · corrodedC-CHECK CORROSION LEVEL 1, FRAME AT STA 827 STR 27L AND 27R IS CORRODED AT GUSSET WHERE FRAME ATTACHES TO FUSLAGE SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, TREATED AND INSTALLED PARTS IAW 737 SRM 53-00-07 FIG 203.Aug 23, 2000 · N325AW · Boeing 737301 · Fuselage Main, FrameSDR AWXA0000587Skin · damagedC-CHECK, AFT CARGO DOOR OUTER SKIN HAS NUMEROUS DENTS AND MIS-DRILLED LOWER CHORD. FABED AND INSTALLED REPAIR SKIN AND ANGLE IAW 737 SRM 51-20-01, 51-40-02, AND DWG 65-47952.Aug 23, 2000 · N325AW · Boeing 737301 · Cargo/Baggage DoorsSDR USAA001314Stringer · crackedCLT - FOUND STRINGER CRACKED .125 INCH, STRINGER SPLICE AFT OF FS 907 AT STRINGER 4R. INSTALLED STRINGER SPLICE AND TIE CLIP PER 51-10-02. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Main, Longeron/StringerSDR USAA001313Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 685, STRINGER 10L. REPLACED TIE CLIP PER SRM 51-10-01. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001312Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED IN TWO PLACES .5 INCH, BS 663 STRINGER 10L. REPAIRED PER SRM 51-10-02. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001311Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663, STRINGER 10R. REPLACED TIE CLIP PER SRM 51-10-1. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001310Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 663, STRINGER 5R. REPLACED TIE CLIP PER SRM 51-10-01. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous StructureSDR USAA001309Intercostal · crackedCLT - FOUND INTERCOSTAL ANGLE CRACKED .5, BS 288 JUST ABOVE RS 11. REPLACED WITH IDENTICAL PART PER SRM 51-10-02, 51-20-01 AND 51-40-00. (M)Aug 22, 2000 · N573US · Boeing 737301 · Fuselage Miscellaneous Structure
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