Boeing 737-3B7

Service difficulty reports · 4,722

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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 USAA001146Frame · crackedPIT - FOUND CHORD ANGLE CRACKED 5 INCHES, HORIZ CENTER BOX, LEFT THRUST BEAM UPPER CHORD ANGLE. REMOVED AND REPLACED BRACKET PER SRM 51-40-05 AND BOEING DRAWING 71046. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001145Skin · crackedPIT - FOUND SKIN CRACKS RANGING FROM .0625 TO 1 INCH, OUTBOARD END OF NR 5 SLAT LOWER L/E SKIN. CUTOUT CRACK AREA MFG DOUBLER HFEC PER TYP REPAIR 57-50-01. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Wing, Plate/SkinSDR USAA001185Frame · crackedPIT - FOUND FRAMED CRACKED .125 INCH, FRAME 500A BETWEEN 58L AND 59L. FRAME REPAIR PER T/R 53-10-14 AND SRM 51-40-02. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001184Frame · crackedPIT - FOUND FRAME CRACKED .25 INCH, FS 480 BETWEEN 58L AND 59L. FRAME REPAIR PER T/R 53-10-14 AND SRM 51-40-02. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001183Structure · gougedPIT - FOUND ZEE FRAMED GOUGED .625 INCH LONG, .050 INCH WIDE, .024 INCH DEEP, DOOR 3701 AFT OUTBOARD SIDE OF ZEE FRAME. REPAIRED GOUGE PER SRM 51-70-11, 52-40-02, AAM 5-2-1 AND BWG MM 52-49-11. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001182Frame · crackedPIT - FOUND FRAMED CRACKED .25 INCH, FRAME 480 BETWEEN 58R AND 59R. FRAME REPAIR PER T/R 53-10-14 AND SRM 51-40-02. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001181Channel · crackedPIT - FOUND CHANNEL SPIDER WEB CRACKING 4 INCHES, CHANNEL BS 540 BOTH ENDS LBBL 24 AND BBL0. NEW PART INSTALLED PER SRM 51-20-01 AND 51-40-02. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001180Angle · crackedPIT - FOUND FRAME TIE ANGLE CRACKED .25 INCH, STATION 727B, BETWEEN 520L-519L. MANUFACTURED AND REPLACED FRAME TIE ANGLE PER SRM 51-40-00, 51-40-02 AND BOEING DRAWING 65-46596. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001179Spar · gougedPIT - FOUND REAR SPAR TO RIB ANGLE WITH SEVERAL GOUGES .125 INCH LONG, LEFT HORIZ REAR SPAR TO RIB ATTACH ANGLE STATION 125 INBOARD. TREATED AND PRIMED PER SRM 55-10-09. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Horizontal Stabilizer, Spar/RibSDR USAA001178Spar · gougedPIT - FOUND REAR SPAR TO RIB ANGLE WITH SEVERAL GOUGES .125 INCH LONG, LEFT HORIZ REAR SPAR RIB ATTACH ANGLE STATION 200 AND 210. TREATED AND PRIMED PER SRM 55-10-09 FIG 101. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Horizontal Stabilizer, Spar/RibSDR USAA001177Spar · gougedPIT - FOUND SEVERAL GOUGES IN REAR SPAR RIB ANGLE .125 INCH LONG, LEFT HORIZ REAR SPAR TO RIB ATTACH ANGLE STATION 170 INBOARD. TREATED AND PRIMED PER SRM 55-10-09 FIG 101. (M)Jul 17, 2000 · N517AU · Boeing 7373B7 · Horizontal Stabilizer, Spar/RibSDR USAA001147Skin · crackedPIT - FOUND LEFT TAB SKIN CRACKED IN 3 PLACES .25 INCH, .5 INCH AND .25 INCHES LONG, LEFT ELEV TAB 3 MOST OUTBOARD HINGE CUTOUTS. RADIUS OUT CRACKS PER SRM 55-20-01. (M)Jul 12, 2000 · N517AU · Boeing 7373B7 · Elevator, Tab StructureSDR USAA001052Stringer · corrodedPIT - FOUND BEAM STRINGER CORRODED 1 INCH BY 6 INCHES, STRINGER 27L KEEL BEAM AT STRINGER STATION 813. CORROSION LEVEL 2, TASK NR C53-208-01. CUT OUT DAMAGED PORTION OF KEEL BEAM AND SPLICED NEW PART PER EA 55680. (M)Jul 12, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR AWXA0000444Floorbeam · corrodedUPPER SURFACE OF FLOORBEAM CORRODED AT STA 312 RBL 12. REMOVED AND REPLACED FLOORBEAM IAW B737 SRM 53-10-51 FIG 205.Jul 7, 2000 · N332AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA0000443Floorbeam · corrodedFLOORBEAM CORRODED AT STA 328 RBL 10 TO RBL 43. REMOVED AND REPLACED UPPER CHORD IAW B737 SRM 53-10-50 FIG 205.Jul 7, 2000 · N332AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA000973Web · tornPIT - FOUND WEB TORN AND MINOR CORROSION LEVEL 1, AFT CARGO STRINGER 25 STATION 794.3 AT WEB. INSTALLED DOUBLER PER SRM 51-70-11. (M)Jul 5, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00184Circuit Board · faultyPVD - FLT 2004 - ON APPROACH TO PVD, THE LEFT MAIN LANDING GEAR INDICATED UNSAFE AT 100 FEET ABOVE GROUND AFTER INDICATING SAFE FOR ABOUT TWO MINUTES. CREW ACCOMPLISHED GO-AROUND AND SAFE INDICATION RETURNED. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENAJul 3, 2000 · N504AU · Boeing 7373B7 · Landing Gear Position and WarningSDR DL733001255Slide · dislodged1R DOOR ESCAPE SLIDE ON FLOOR. SLIDE PARTILLY DEPLOYED UPON REMOVAL. RPLD DOOR SLIDE.Jul 3, 2000 · N951WP · Boeing 7373B7 · Escape SlideSDR USAA000959Frame · corrodedPIT - FOUND FRAME CORRODED 4 INCHES BY 3 INCHES, STATION 1006 AT STRINGER 18 AND 19 RIGHT SIDE. CORROSION LEVEL 2, TASK NR C53-206-01. CUT FRAME AND REPLACED PER SRM 51-20-05, SRM 51-40, SRM 53-00-07 FIG 201. (M)Jun 26, 2000 · N373US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA000960Channel · crackedPIT - FOUND U-CHANNEL CRACKED 1 INCH, U-CHANNEL SUPPORT PYLON MID SECTION RIGHT WING NAC 145.63. LOCALLY MFG U-CHANNEL PER EA 55424 AND SRM 51-40-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Nacelle/Pylon StructureSDR USAA000963Support Bracket · crackedPIT - FOUND SUPPORT ANGLE CRACKED 1 INCH AND CHAFED 6 INCHES BY 2 INCHES, RIGHT ENG PYLON SUPPORT STRUCTURE FOR PANEL 5842. INSTALLED SPLICE PLATE PER SRM 54-50-71 AND SRM 51-40-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Nacelle/Pylon StructureSDR USAA000964Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED .25 INCH REMOVED ORIGINALLY THICKNESS .070 INCH, AFT CARGO STATION 947.5, LT FLOOR SUPPORT RAIL STRINGER 21L. INSTALLED LEFT AFT FLOOR SUPPORT PER SRM 51-10-02. CORROSION LEVEL 2, TASK NR C53-208-01. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000965Support Bracket · corrodedPIT - FOUND SUPPORT ASSEMBLY CORRODED 10 INCHES, ATTACH FLANGE ANGLE FOR PYLON PANEL 57422. REMOVED AND REPLACED CHAFE STRIP PER SRM 51-40-00. CORROSION LEVEL 2. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Nacelle/Pylon StructureSDR USAA000966Floor Support · corrodedPIT - FOUND CORROSION ON SUPPORT ANGLE, BETWEEN 312 AND 328, 11 INCHES LEFT OF BL 0. CORROSION LEVEL 2, TASK NR C53-107-02. INSTALLED FLOOR SUPPORT SECTION PER SRM 53-10-51. CORROSION LEVEL 2, TASK NR C53-107-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000967Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORRODED 17 INCHES, BETWEEN STATION 277 AND 294.5, 11 INCHES TO LEFT BL 0. REPLACED FLOOR SUPPORT AND T-CAP PER SRM 53-10-51. CORROSION LEVEL 2, TASK NR C53-107-02. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000968Angle · corrodedPIT - FOUND SUPPORT ANGLE CORRODED 10 INCHES, OBLIQUE 1006-1016 LT SUPPORT. REPLACED OBLIQUE SUPPORT PER SRM 51-40. CORROSION LEVEL 2. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000969Web · corrodedPIT - FOUND CORROSION ON STRAP AND SHEAR WEB 10 INCHES BY 10 INCHES, CENTER LINE BEAM 1016. REPLACED SHEAR WEB AND STRAPS PER SRM 51-40. CORROSION LEVEL 2. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000970Skin · chafedPIT - FOUND LEADING EDGE MID FLAP CHAFED 1 INCH BY 2 INCH AREA, LT OUTBOARD. INSTALLED DOUBLER PER TYPICAL REPAIR NR 57-50-25 FIG 2. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA000971Frame · corrodedPIT - FOUND FRAME CORRODED 3 INCHES BY 4 INCHES, STATION 1006L STRINGER 18 AND 19 BELTFRAME. REPLACED FRAME CUTOUT AND INSTALLED DOUBLER PER EA 55673, SRM 53-00-07. CORROSION LEVEL 2, TASK NR C53-202-01. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA000972Access Panel · crackedPIT - FOUND CRACKED ACCESS PLATE CRACKED 1 INCH, 5727L NR 1 ENGINE PYLON. DOUBLER INSTALLED PER TYP REPAIR 54-30-07. (M)Jun 26, 2000 · N375US · Boeing 7373B7 · Nacelle/Pylon, Plate/SkinSDR USAA001053Seat Track · corrodedPIT - FOUND SEAT TRACK CORRODED .050 INCH BY .5 INCH BY 1 INCH, STATION 328R TO 344R RIGHT OUTBOARD SEAT TRACK. INSTALLED SEAT TRACK SECTION PER SRM 53-00-52. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Jun 25, 2000 · N375US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA001048Floor Support · corrodedPIT - FOUND FLOOR SUPPORT CORROSION 2 INCHES BY .25 INCH, RIGHT OF BL0 328-344.11 FLOOR SUPPORT. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. (M)Jun 25, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000961Flap Track · crackedPIT - FOUND OUTBOARD TRACK CRACKED .5 INCH, NR 2 OUTBOARD TRACK CUTOUT LE AT STA 750. TYPICAL REPAIR PER 57-20-08 REV A. (M)Jun 22, 2000 · N375US · Boeing 7373B7 · Leading Edge DevicesSDR USAASB00170Proximity Switch · dirtyLGA - FLT 758 - AFTER TAKEOFF AND GEAR RETRACTION FROM LGA, THE RIGHT MAIN LANDING GEAR INDICATED DOWN (GREEN LIGHT). LIGHT REMAINED ON WITH HANDLE IN OFF POSITION. CREW RECYCLED GEAR AND LIGHT STILL REMAINED ON. FLIGHT CONTINUED ONTO BUF AND LANDED WITHOUTJun 17, 2000 · N504AU · Boeing 7373B7 · Landing Gear Position and WarningSDR USAA000850Skin · crackedCLT - FOUND SKIN FUSELAGE CRACKED 1.5 INCH, BS 727D PLUS 17.5 INCH JUST ABOVE STRINGER 23R. FABRICATED AND INSTALLED REPAIR DOUBLER PER SRM 53-00-01 FIG 202 AND TR 53-60-03. (M)Jun 14, 2000 · N394US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA000962Stringer · corrodedPIT - FOUND PIECES OF STRINGER MISSING, STRINGER 25L AT STATION 967. CORROSION LEVEL 1. DEFECTIVE PART REPLACED WITH IDENTICAL PART PER SRM 53-00-03. (M)Jun 12, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA0000385Panel · leakingDIVERTED TO ELP DUE TO POSSIBLE FUEL LEAK ON TOP OF NR 1 ENGINE. ISOLATED LEAK TO UPPER PYLON FAIRING PANEL (5 FASTENERS AND DOME SEALED), LEAK CHECK GOOD.Jun 12, 2000 · N328AW · Boeing 7373B7 · Wing, Plate/SkinSDR USAA000831Angle · crackedPIT - FOUND L-ANGLE CRACKED 1 INCH, GLIDE SLOPE ANTENNA MOUNT BRACKET LOWER CENTER L-ANGLE. INSTALLED REPAIR ANGLE PER SRM 51-70-11 FIG 1. (M)Jun 11, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000825Panel · corrodedPIT - FOUND PANEL .375 INCH DIAMETER BY .035 INCH DEEP CORRODED, STATION 720-727 LWR RT MLG WW AFT BELLY ATTACH POINTS. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA000824Flange · corrodedPIT - FOUND FLANGE CORRODED 1 INCH WIDE BY 77 INCHES LONG LOWER SURFACE, STATION 640-727 ATTACH FLANGE LBL 6:30. CORROSION LEVEL 2. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA000822Skin · crackedPIT - FOUND SKIN CRACKED 4.5 INCH, FORWARD SERVICE DOOR APERATURE AFT LOWER CORNER. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA000821Fitting · gougedPIT - FOUND ACT SPAR INBOARD FITTING GOUGED BY NR 4 SLAT, .5 INCH SEMI CIRCLE BY .002 INCH DEEP, FRONT SPAR ATTACH FITTING, INBOARD LUG FITTING. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Leading Edge DevicesSDR USAA000820Keelbeam · corrodedPIT - FOUND KEEL WEB CORRODED 1 INCH BY 4 INCHES, LT A/C BAY KEEL WEB STATION 540. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA000826Keelbeam · corrodedPIT - FOUND KEEL WEB LOWER CHORD CORRODED 1 INCH BY 82 INCHES, BS 645-BS 727 LT A/C BAY KEEL WEB LOWER CHORD. (M)Jun 7, 2000 · N375US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA000780Strap · crackedTPA - FOUND STRIP CRACKED .25 INCH, MAIN ENTRY DOOR, INNER STRUCTURE UPPER HINGE WEB. REPLACED STRAP PER SRM 51-10-2. (M)Jun 2, 2000 · N385US · Boeing 7373B7 · Passenger/Crew DoorsSDR USAASB00152Seal · leakingCLT - FLT 2339 - ON CLIMB-OUT FROM CLT, THE FORWARD ENTRY DOOR BEGAN MAKING A VERY LOUD AIR NOISE. PRESSURIZATION WAS NORMAL. FLIGHT RETURNED TO FIELD AT CLT AND LANED WITHOUT FURTHER INCIDENT. NO EMERGENCY WAS DECLARED. MAINTENANCE REMOVED AND REPLACED THMay 31, 2000 · N533AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA000739Skin · crackedCLT - FOUND SKIN PANEL CRACKED, BS 716, LBL 5 KEEL BEAM LOWER SKIN PANEL. REPLACED PANEL PER EO 67341. (M)May 31, 2000 · N528AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAASB00146Relief Valve · misinstalledCLT - WHILE ON THE GATE AT CLT, THE A SYSTEM HYDRAULIC RESERVOIR EXPLODED. MAINTENANCE FOUND THE PRESSURE RELIEF VALVE INSTALLED IMPROPERLY. THE VALVE AND RESERVOIR WERE REPLACED. (M)May 21, 2000 · N392US · Boeing 7373B7 · Hydraulic Pressure Relief Valve, MainSDR USAA000719Skin · crackedCLT - FOUND SKIN CRACKED TWO PLACES 1.5 INCH, BS 665, RBL 42, WL 203. INSTALLED FILLERS, DOUBLER AND ANGLE PER TR 53-60-04. (M)May 16, 2000 · N389US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA000718Skin · crackedCLT - FOUND SKIN CRACKED, BS 665, LBL 30 WL 203. INSTALLED FILLER AND DOUBLER PER TR 53-60-04. (M)May 16, 2000 · N389US · Boeing 7373B7 · Fuselage Main, Plate/Skin
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