Boeing 737-3B7

Service difficulty reports · 4,722

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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 = '7373B7'
  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 USAA050074Crease Beam · crackedPIT - FOUND CREASE BEAM CRACKED 2.5 INCHES, AFT OF FRAME 616 RT SIDE CREASE BEAM. MODIFIED PART INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050176Skin · chafedPIT - FOUND LOWER SKIN SURFACE WITH CHAFE DAMAGE, 1.5 INCH BY 2.5 INCH, NR 2 SLAT INBOARD CORNER AND OUTBOARD CORNER LOWER SURFACE. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050175Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED .5 INCH BY .5 INCH AREAS AROUND 6 NUTPLATES, FLOORBEAM STATION 967 17L-17R. TOP CP REPAIR, FLOOR EXTRUSION AND SPLICES PER TYPICAL REPAIR 53-10-05B. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050174Support Bracket · corrodedFOUND WALL SUPPORT BRACKET CORRODED 1 INCH BY .5 INCH AREA AROUND 6 SCREW HOLES, STATION 500D 26R-26L. REMOVED AND REPLACED WALL SUPPORT BRACKET. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050172Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 1 INCH BY .5 INCH IN THREE AREAS, FLOORBEAM FROM STATION 967-986 LBL 18. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-10-02. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050171Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 18 INCHES LONG, LBBL 8 STATION 344. CORROSION LEVEL 1. WEB MFG PER 53-00-51 FIG 202. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050170Skin · bentPIT - FOUND SLAT EXT SKIN BENT AREA 3.5 INCH BY 1.5 INCH AREA, NR 1 SLAT UPPER T/E SURFACE INBOARD END. REMOVED DAMAGED AREA, INSTALLED FILLER AND INTERNAL DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050169Skin · delaminatedPIT - FOUND COMPOSITE SKIN DELAMINATED 1 INCH AREA, RT AILERON TAB OUTBOARD T/E. INSTALLED REPAIR PLYS PER SRM 51-60-01 AND 51-70-16. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · AileronsSDR USAA050168Skin · delaminatedPIT - FOUND TOP SKIN/CORE BOND DELAMINATED 3 INCHES BY 2 INCHES AREA, NR 3 SLAT INBOARD T/E. REMOVED DELAMINATED TOP SKIN AND CORE MATERIAL, BONDED IN NEW CORE, INSTALLED TOP DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050173Floorbeam · corrodedPIT - FOUND FLOORBEAM CORRODED 1 INCH BY .75 INCH AREA, FLOORBEAM STATION 328 RBBL 24.50 LBBL 24.50. CORROSION LEVEL 1. REMOVED CORROSION, FABRICATED STRAP REPAIR PER SRM 53-00-51 PAGE 212-215 AND 53-10-51 PAGE 114. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050082Web · crackedPIT - FOUND WEB CRACKED 1.25 INCH, STATION 927-947.5 INTERCOSTAL CRACKED 1.25 INCH FROM FORWARD CORNER. INSTALLED SAME PART PER DWG 69-36656. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050166Stringer · crackedPIT - FOUND STRINGER CRACKED 1.5 INCHES LONG, FS 380 STRINGER 15R. SPLICED IN NEW SECTION OF STRINGER PER SRM 53-00-03, FIG 201, DWG 65-45768. (M)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA040081AFlange · crackedFOUND FLANGE CRACKED .5 INCH,PANEL 582-8R OPENING IN RT PYLON. STOP DRILLED THE CRACK, INSTALLED DOUBLER PER TYPICAL REPAIR 54-30-07. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Structure (General)SDR USAA050060Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 6 INCH AREA, BOTTOM SIDE 14 INCHES FROM INBOARD END. REMOVED DAMAGE, INSTALLED INTERNAL DOUBLERS AND FILLRS PER SRM 51-70-10. (M)Jan 1, 2005 · N518AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA050053Skin · crackedPIT - FOUND NR 1 SLAT WITH .125 INCH CRACKS ON 6 RIVET HOLES, CENTER OF SLAT BY ACTUATOR MOUNT LOWER SKIN. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050050Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .25 INCH, INTERCOSTAL AT BL0 BETWEEN STATION 344 AND 360. INSTALLED DOUBLER, STOP DRILLED PER SRM 51-70-11. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050073Beam · crackedPIT - FOUND BEAM CRACKED .75 INCH, STATION 616 BELOW RT SIDE CREASE BEAM. ROUTED OUT CRACK, INSTALLED FILLER AND REPAIR ANGLE PER TYPICAL REP 53-62-01. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050072Intercostal · crackedPIT - FOUND INTERCOSTAL CRACKED .125 INCH, FORWARD END INTERCOSTAL FASTENER BS 328 LBBL 44. REPLACED INTERCOSTAL PER SRM 53-10-51. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050068Panel · delaminatedPIT - FOUND PANEL DELAMINATED, INBOARD AND OUTBOARD ENDS OF NR 5 SLAT PANEL. INSTALLED DOUBLER PER SRM 51-70-10. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050066Angle · brokenPIT - FOUND ANGLES BROKEN, RAM AIR INLET DUCT UPPER SUPPORT LEFT SIDE. DEFECTIVE PART REPLACED WITH IDNT PART PER TYPICAL REPAIR 21-50-07C. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050056Attach Fitting · crackedPIT - FOUND ATTACH CLIP CRACKED .125 INCH, STRINGER TO FRAME ATTACH CLIP AT BS 706, S-11L. DEFECTIVE PART REPLACED WITH IDENT PART PER BOEING DWG 66-23574. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050055Door Frame · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED .125 INCH, DOOR FRAME NR 6 DOOR STOP AFT SIDE. CUT OUT DAMAGE, INSTALLED DOUBLER PER TYPICAL REP 52-10-16. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA050052Skin · chafedPIT - FOUND FLAP SKIN LEADING EDGE WITH CHAFE MARK .020 BY 4.25 INCH LONG BY .5 INCH WIDE, RT OUTBOARD MID FLAP ADJACENT TO OUTBOARD FLAP TRACK. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Trailing Edge FlapsSDR USAA050051Skin · crackedPIT - FOUND NR 3 SLAT CRACKED .125 INCH, LOWER SURFACE AT MID SPAN RIVET HOLE. INSTALLED DOUBLER PER SRM 57-43-01 FIG 206. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050048Stringer · crackedPIT - FOUND STRINGER CRACKED .125 INCH, FRAME 380 AT S16R. REPAIR FILLER AND FABRICATED SHEAR TIE PR SRM 53-00-07. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050067Frame · brokenPIT - FOUND FRAME BROKEN OUT EDGES, DOOR FRAME STATION 492 AT STATION 27R, LOWER AFT CORNER OF CARGO DOOR FRAME. FABRICATED DOUBLER PER SRM 51-70-13. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050057Beam · crackedPIT - FOUND BEAM CRACKED 1 INCH, FORWARD OF FRAME 639 RIGHT SIDE CREASE BEAM. MODIFIED PART C/C 1109171 AND INSTALLED PER TYPICAL REPAIR 53-10-02 REV A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050054Angle · crackedPIT - FOUND ANGLE CRACKED .25 INCH LONG, EDGE OF SUPPORT ANGLE AT FS 294.5, FORWARD LOWER CORNER AT FLOOR LINE. DEFECTIVE PART REPLACED WITH IDENT PART PER SRM 51-40-02. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050024Floorbeam · corrodedPIT - FOUND CHORD AND ANGLE CORRODED AT SCREW HOLES, STATION 344 RBBL -13 TO LBBL -24. CORROSION LEVEL 1, TASK NR C53-107-02. REMOVED T-CAP, FABRICATED NEW CHORD AND ANGLE SPLICES, INSTALLED PER SRM 53-10-51. (M)Jan 1, 2005 · N518AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050070Skin · chafedPIT - FOUND SKIN CHAFED, .023 INCH DEEP, SKIN STATION 860-880 AT DORSAL FIN. INSTALLED DOUBLER, TRIPLER AND BONDED STAINLESS RUB STRIP PER SRM 53-60-01 FIG 209. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050065Clip · brokenPIT - FOUND BROKEN FRAME CLIP, STATION 597 STRINGER 8R. REMOVED AND REPLACED FRAME CLIP PER SRM 51-40-00. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050061Skin · delaminatedPIT - FOUND LOWER SKIN CORE BOND DELAMINATED 6 INCH BY 4.5 INCH AREA, 34 INCHES FROM F/B EDGE. REMOVED DAMAGE, INSTALLED FILLERS, DOUBLERS PER SRM 51-70-10. (M)Jan 1, 2005 · N518AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA050047Web · crackedPIT - FOUND WEB CRACKED 1 INCH, STATION 664 8 INCHES OUTBOARD OF LT INVD SEAT TRACK. PRESSURE DECK WEB REPAIR PER SRM 53-60-51. (M)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050049Frame · crackedPIT - FOUND RIVET CRACKED .125 INCH, FRAME 360, RIVET AT S9L. INSTALLATION OF TWO, REPAIR ANGLES PER TYP REP 53-10-20A. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050069Skin · delaminatedPIT - FOUND SLAT DELAMINATED 4 INCHES BY 6 INCHES, NR 3 SLAT. REMOVED TOP SKIN CORE AND DAMAGE, INSTALLED FILLER, DOUBLER PER SRM 51-70-09. (M)Jan 1, 2005 · N522AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050165Channel · crackedPIT - Q6 - CHANNEL, .7500 INCH CRACK; ST277, BL0, FWD CABIN FLOOR; DEFECTIVE PART REPLACED WITH IDENT PART IAW MFG DWG. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050160Skin · crackedPIT - Q6 - NR 6 SLAT, .5 INCH CRACK; LOWER SKIN AFT ROW RIVET 4 INCHES FROM OB END; INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050159Intercostal · crackedPIT - Q6 - INTERCOSTAL, NUMEROUS CRACKS, .5 INCH. .7500 INCH, 1.5 INCH; SCREW HOLES UPPER FLANGE OF INTERCOSTAL, BS 380-400. REPAIR ANGLE INSTALLED IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050158Door Frame · crackedPIT- Q6 - DOOR EDGE FRAME, .2500 INCH CRACK; FWD SERVICE DOOR, LOWER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Service DoorsSDR USAA050157Door Frame · crackedPIT - Q6 - DOOR EDGE FRAME, .1250 INCH CRACK; FWD SERVICE DOOR, UPPER MIDDLE DOOR STOP CUTOUT, AFT EDGE FRAME; INSTALLED DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Service DoorsSDR USAA050156Skin · crackedPIT - Q6 - NR 1 SLAT, 1 INCH CRACK; LOWER SKIN AFT ROW RIVETS AT NR 2 AUX TRACK. INSTALLED DOUBLER IAW SRM. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Leading Edge DevicesSDR USAA050155Skin · crackedPIT - Q6 - SKIN, APPROX 1 INCH CRACK; NR 2 ENG OB WING/LEADING EDGE AT SLAT STA3.25, LWR SKIN PANEL. FABRICATED SKIN FILLER/ DOUBLER IAW TYP REP. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA050154Floor Support · crackedPIT - Q6 - FLOOR SUPPORT, 1 INCH CRACK; STA 540, BL0.0; REPLACED SUPPORT BRACKET IAW SRM 53-00-51. (K)Jan 1, 2005 · N521AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050119Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 16 INCH WIDE SPREAD CORROSION; CORROSION; LEVEL 1; TASK C53-107-01, 02; BS 312 AND 328 BL0 RT 10 INCHES; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050118Sill · corrodedPIT - Q6 - DOOR SILL, 1 INCH X 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-01, FWD SVC DOOR SILL (AFT) AT NUT PLATE. REPAIRED IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050117Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 1 INCH DIA AREAS ( 8 EA ); CORROSION; LEVEL 1; TASK NR C53-107-02; FLOOR SUPPORT BS 967-986.5, RBL 17 INCHES. DEFECTIVE PART, REPLACED WITH IDENT PART IAW SRM AND MFG DWG. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050116Web · corrodedPIT - Q6 - SHEAR WEB, 2 INCH X 2 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-202-01, BS 1016, LBL 16 SHEAR WEB; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02 AND MFG DWG. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050115Gate · corrodedPIT - Q6 - AFT ENTRY LWR EXHAUST, 1 INCH X 1 INCH AREA (4 PLACES) CORROSION; LEVEL 1; TASK NR C53-107-01; LOWER EXHAUST GATE LOWER IB SURFACE. DEFECTIVE PART REPLACED WITH IDENT PART NR. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA050114Floorbeam · corrodedPIT - Q6 - FLOORBEAM, .5 INCH X .5 INCH, CORROSION; LEVEL 1; TASK NR C53-107-01; TOP SURFACE OF FLOORBEAM 20 INCH RT OF BL0, BS312; INSTALLED BEAM DOUBLER IAW SRM. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050113Floor Support · corrodedPIT - Q6 - FLOOR SUPPORT, 20 INCH X 1.5 INCH AREA, CORROSION; TOP OF FLOOR SUPPORT BETWEEN STA 947-967, RBL 46; DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-40-02-1 AND 51-40-03. (K)Jan 1, 2005 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
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