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 AWXA200500572Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION ON THE BOTTOM SURFACE OF THE BS 312 T-CAP LWR AFT REPAIR SPLICE ANGLE AT RBL 21 WL 208. MAINTENANCE REMOVED, FABRICATED, INSTALLED, REPLACEMENT SPLICE ANGLE ON BOTTOM SURFACE OF BS312 TEE CAP AT RBL21 WL208 IAWApr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200500571Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON THE TOP OF THE BS 986.5 T-CAP AT LBL 18, WL 208 ON PREVIOUS REPAIR CAP. MAINTENANCE REMOVED AND REPLACED TEE CAP REPAIR ON TOP OF BS 986.5 BEAM AT WL208 FROM LBL50 TO RBL50 IAW AWA ER 03-5310-0512Apr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200500563Intercostal · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .625 INCH CRACK WAS FOUND IN INTERCOSTAL AT BS 329, LBL 46, WL 208. MAINTENANCE REMOVED CRACKED INTERCOSTAL AT BS 329, LBL 46; FABRICATED A NEW REPLACEMENT INTERCOSTAL PER DWG 65-45834; INSTALLED REPAIR PART IAW B737-3Apr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA200500557Reveal · crackedDURING C-18 CHECK A .25 INCH CRACK WAS FOUND IN REVEAL AT UPPER AFT CORNER OF R-1 DOOR CUTOUT BS 323, STR 16 RT. MAINTENANCE REMOVED CRACKED REVEAL AT UPPER AFT CORNER OF R-1 DOOR CUTOUT BS 323, STR 16 RT; FABRICATED A NEW REPLACEMENT REVEAL PER DWG 65-53594;Apr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA200500553Channel · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .5 INCH CRACK WAS FOUND IN LOWER SURFACE OF STRINGER SPLICE CHANNEL AT BS 360, STR 15 LT. MAINTENANCE REMOVED CRACKED STRINGER SPLICE CHANNEL AT BS 360, STR 15 LT; FABRICATED A NEW REPLACEMENT SPLICE CHANNEL PER DWG 65Apr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA200500544Floorbeam · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON UPPER AND LOWER SURFACE OF TRANSVERSE BEAM AT BS 967, LBL 43, WL 208. MAINTENANCE CUT OUT CORRODED SECTION OF TRANSVERSE BEAM AT BS 967, LBL 43; FABRICATED A NEW REPLACEMENT SECTION OF BEAM AND 2 EApr 29, 2005 · N332AW · Boeing 7373B7 · Fuselage Main, Floor BeamSDR AWXA200500582Wedge · delaminatedMCN- FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 5 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 5 SLAT AApr 28, 2005 · N332AW · Boeing 7373B7 · Leading Edge DevicesSDR AWXA200500581Wedge · delaminatedMCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 4 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 4 SLAT Apr 28, 2005 · N332AW · Boeing 7373B7 · Leading Edge DevicesSDR AWXA200500579Wedge · delaminatedMCN - FLIGHT CONTROL - DURING C-18 CHECK, DELAMINATION WAS FOUND AT THE NR 6 SLAT WEDGE. DELAMINATION WAS FOUND ON TOP AND BOTTOM SURFACES. MAINTENANCE FOUND THAT THE DELAMINATION WAS BEYOND REPAIRABLE LIMITS. MAINTENANCE REMOVED AND REPLACED THE NR 6 SLAT Apr 28, 2005 · N332AW · Boeing 7373B7 · Leading Edge DevicesSDR USAA050553Support Beam · crackedBFM - FOUND AFT SUPPORT BEAM CRACKED, LT MLG BEAM AFT SUPPORT FITTING ON AFT SPAR, APPROX WBL 157.0 S1 WING. REMOVED FASTENERS, PERFORMED NDT INSPECTION, REINSTALLED FASTENERS PER TYPICAL REPAIR 57-40-13 REV A. (M)Apr 28, 2005 · N374US · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR AWXA200500545Skin · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK 2 EACH .75 INCH CRACKS WERE FOUND IN EXTERNAL FUSELAGE SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT BS 329, STR 17 RT. MAINTENANCE CUT OUT CRACKED SKIN AT LOWER AFT CORNER OF R-1 DOOR CUTOUT BS 329, STR 17 RT; FABRICATED Apr 28, 2005 · N332AW · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR AWXA200500543Structure · corrodedMCN - MAJOR REPAIR - DURING C-18 CHECK CORROSION WAS FOUND ON L-2 UPPER INNER CHORD BETWEEN BS 962 AND BS 983 AT LBL 51, WL 209. MAINTENANCE REMOVED CORRODED L-2 UPPER INNER CHORD FROM BS 962 TO BS 983 AT LBL 51; FABRICATED A NEW REPLACEMENT INNER CHORD PER DApr 28, 2005 · N332AW · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA200500590Bulkhead · scratchedMCN - MAJOR REPAIR - DURING C-18 CHECK NUMEROUS SCRATCHES WERE FOUND AROUND FASTENERS ON BS 178 BULKHEAD COMMON TO FASTENER AND DOME NUT LOCATIONS AT LT BL 6 BETWEEN WL 150 AND WL 182. THE DEEPEST SCRATCH WAS MEASURED 0.004 INCH DEEP AND FOUND BEYOND LIMITS PEApr 27, 2005 · N332AW · Boeing 7373B7 · Fuselage Main, BulkheadSDR AWXA200500564Door Frame · crackedMCN - MAJOR REPAIR - DURING C-18 CHECK A .375 INCH CRACK WAS FOUND IN R-1 DOOR FRAME AT 3RD DOOR STOP CUTOUT FROM BOTTOM ON AFT SIDE BS 328, STR 14 RT. MAINTENANCE TRIMMED OUT CRACK AT R-1 DOOR STOP CUTOUT BS 328, STR 14 RT; FABRICATED A REPAIR DOUBLER; INSTAApr 27, 2005 · N332AW · Boeing 7373B7 · Passenger/Crew DoorsSDR SB05050Battery Pack · dischargedPIT - MAINTENANCE REPORTED THE EMERGENCY EXIT LIGHTS AT THE LEFT OVERWING EXIT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.Apr 24, 2005 · N516AU · Boeing 7373B7 · Emergency LightingSDR USAA050540Seat Track · gougedBFM - FOUND SEAT TRACK WITH NICKS AND GOUGES, .90 INCH BY .2 INCH BY .022 INCH AND .40 INCH BY .10 INCH BY .025 INCH, MCD FROM STATION 480-520. FABRICATED NEW SEAT TRACK, REMOVED AND REPLACED PER SRM 53-00-52, SRM 51-40-02. (M)Apr 20, 2005 · N374US · Boeing 7373B7 · Fuselage, Seat/Cargo Attach FittingsSDR USAA050554Stringer Splice · crackedBFM - FOUND STRINGER SPLICE CRACKED .750 INCH, FASTENERS MOUNTING HOLE, AFT CABIN LEFT CEILING, STRINGER 4L AT BS 908. FABRICATED PARTS, INSTALLED FABRICATED CHANNEL ON STRINGER SPLICE PER SRM 51-40-02. (M)Apr 19, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050506Skin · crackedCLT - FOUND SKIN CRACKED 2.25 INCH, 727E STRINGER 24L. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)Apr 17, 2005 · N390US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR SB05048Wire · brokenCLT - PILOT REPORTED THE EMERGENCY EXIT LIGHT AT THE R1 DOOR WAS ILLUMINATED. MAINTENANCE FOUND A BROKEN WIRE BETWEEN BATTERY PACKS. RESPLICED WIRE. OPERATIONAL CHECK GOOD.Apr 16, 2005 · N390US · Boeing 7373B7 · Light System WiringSDR USAA050539Sleeve · chafedBFM - FOUND SUPPORT SLEEVE CHAFED MARK .086 WEAR, RT MLG FORWARD TRUNNION BEARING SUPPORT FITTING. REMOVED AND REPLACED FORWARD TRUNNION SUPPORT SLEEVE PER TYPICAL REPAIR 57-20-04. (M)Apr 15, 2005 · N374US · Boeing 7373B7 · Fuselage, Landing Gear Attach FittingsSDR AWXA200500455Battery · dischargedLAS - EMERGENCY EQUIPMENT - FLIGHT CREW REPORTED THE FORWARD EMERGENCY FLASHLIGHT WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERY IN THE FORWARD EMERGENCY FLASHLIGHT, OPERATIONAL CHECK WAS GOOD.Apr 15, 2005 · N332AW · Boeing 7373B7 · Emergency EquipmentSDR USAA050542Floorbeam · corrodedBFM - FOUND FLOORBEAM CORRODED 3 INCHES LONG BY 1 INCH WIDE BY .055 INCH DEEP AND 3 INCHES LONG BY 1 INCH WIDE BY .043 INCH DEEP, AFT CARGO FLOOR LBL 12.5 AND RBL 3. FABRICATED REPAIR ANGLES AND INSTALLED PER TYP REPAIR 53-10-06B. CORROSION LEVEL 1, TASK C53Apr 12, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050541Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT/ANGLE CORRODED 1 INCH LONG BY 1 INCH WIDE BY .028 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 867 LBL 8.10 INCH. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B AND SRM 53-60-53. (M)Apr 12, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050536Stiffener · corrodedBFM - FOUND STIFFENER EXFOLIATED AND CORRODED CHORD, BS 290-303, LBL 11.10 FLOOR SUPPORTS WL 208. INSTALLED FABRICATED PARTS PER SRM 53-10-51, 51-40-02. (M)Apr 8, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050538Support Angle · crackedBFM - FOUND SUPPORT ANGLE CRACKED 4 INCHES, LT WING TE NR 3 (INBOARD TO OUTBOARD) HINGE WS 573.872 WBL, 415.93. REMOVED, FABRICATED NEW, INSTALLED NEW SUPPORT ANGLE PER SRM 57-51-02, 51-40-05, 51-40-02. (M)Apr 7, 2005 · N374US · Boeing 7373B7 · Wing, Control Surface Attach FittingsSDR USAA050537Floorbeam · corrodedBFM - FOUND SUPPORT, T-ANGLE, WEB CORRODED AND CRACKED 4 INCHES LONG, 1 INCH WIDE AND 1 INCH, BS 994 WL 208 AFT CABIN FLOOR. BLENDED SUPPORT, REMOVED AND REPLACED T-ANGLE AND WEB WITH NEW FABRICATED PARTS PER SRM 51-40-02, 53-60-51. (M)Apr 7, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050524Channel · corrodedBFM - FOUND FLOOR SUPPORT CHANNEL CORRODED 2 INCHES LONG BY .90 INCHES WIDE BY .030 INCHES DEEP, AFT CARGO BS 704 RBL 8.10. INSTALLED REPAIR ANGLE PER TYPICAL REPAIR 53-10-06B. (M)Apr 7, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050526Shear Web · corrodedFOUND SHEAR WEB CORRODED 10 INCHES BY 27 INCHES, BS 1016 FLOOR BL 0 - LBL 27. CORROSION LEVEL 1, TASK C53-202-01. FABRICATED NEW SHEAR WEB AND INSTALLED NEW PARTS PER SRM 53-60-51, 51-30-01, 51-24-00, 51-40-02. (M)Apr 5, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050525Shear Tie · corrodedFOUND FRAME BOTTOM SHEAR TIE CORRODED, 2 INCHES LONG BY .80 INCH WIDE BY .032 INCH DEEP, BS 360 WL 148.5 RBL 4. REPLACED SHEAR TIE PER SRM 51-40-02. (M)Apr 5, 2005 · N374US · Boeing 7373B7 · Fuselage Internal Mounting StructureSDR SB05045Light · inoperativePIT LEFT AFT GALLEY EMERGENCY LIGHT FOUND INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY.Apr 5, 2005 · N353US · Boeing 7373B7 · Emergency LightingSDR SB05044Wire · brokenBOS COCKPIT EMERGENCY LIGHT SWITCH NOT WORKING PROPERLY. MAINTENANCE REPAIRED A BROKEN WIRE ABOVE ROW 20ABC.Apr 5, 2005 · N393US · Boeing 7373B7 · Light System WiringSDR USAA050452Frame · brokenCLT - FOUND FORMER BROKEN, STATION 535 WL 165, LBL 60. REPLACED FORMER. (M)Apr 2, 2005 · N394US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA050464Skin · crackedPIT - FOUND SKIN CRACKED 1.5 INCH LONG, BS 747 BETWEEN 19L AND 20L. INSTALLED DOUBLER SKIN REPAIR PER EA 83173, SRM 53-00-01. (M)Apr 2, 2005 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050534Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 2.5 INCHES LONG BY 1 INCH WIDE BY .045 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 773 LBL 12.5 - RBL 8.10. FABRICATED DOUBLERS AND INSTALLED PER TYPICAL REPAIR 53-10-06B. (M)Apr 1, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050528Channel · corrodedBFM - FOUND CHANNEL CORRODED 2 INCHES WIDE BY .056 INCHES DEEP BY 4.0 INCHES LONG, BETWEEN BS 986-1006, S-24L AND S-25L. INSTALLED REPAIR SUPPORT PLATE, CHANNEL, PER BOEING DWG 65-55843 AND SRM 51-40-02. (M)Apr 1, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050527Access Panel · corrodedBFM - FOUND ACCESS PANEL CRACKED AND CORRODED 1.5 INCH CRACK, 3 INCH CORROSION .050 DEEP, RIGHT W/W LOWER PANEL. FABRICATED NEW PART PER 51-40-02. (M)Mar 31, 2005 · N374US · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA050532Stringer · corrodedBFM - FOUND STRINGER CORRODED 8 INCHES LONG BY 1 INCH WIDE BY .035 INCH DEEP AREA, BS 967, STRINGER 25L. INSTALLED NEW STRINGER SECTION AND REPAIR SPLICE PER SRM 53-00-03. (M)Mar 30, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA050530Plate · corrodedBFM - FOUND PANEL FLANGE PLATE CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCH DEEP, NR 1 PYLON MID FAIRING PANEL FLANGE PLATE. INSTALLED REPAIR SPLICE PLATE PER SRM 54-50-70 AND BOEING DWG 313A1380. (M)Mar 30, 2005 · N374US · Boeing 7373B7 · Nacelle/Pylon Miscellaneous StructureSDR USAA050529Floorbeam · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 4 INCHES LONG BY 2.5 INCHES WIDE BY .05 INCHES DEEP, AFT CARGO COMPARTMENT FLOOR SUPPORT BS 727D PLUS LBL 12.5- RBL 8.10 INCH. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR ANGLE IAW TYPICAL REPAIR 53-10-06B AND 53-6Mar 30, 2005 · N374US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA050533Floor Support · corrodedBFM - FOUND FLOOR SUPPORT CORRODED 1 INCH WIDE BY 2 INCHES LONG BY .053 INCH DEEP, AFT CARGO FLOOR SUPPORT BS 825 LBL 8.10 INCH AND RBL 3. INSTALLED REPAIR ANGLE PER TYP REPAIR 53-10-06B, 53-60-53, 51-10-02. (M)Mar 30, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05042Battery Pack · faultyMAINTENANCE REPORTED THE EMERGENCY LIGHTS IN THE AFT CABIN WOULD NOT TURN OFF. MAINTENANCE REMOVED AND REPLACED THE AFT CABIN EMERGENCY LIGHT BATTERY PACKS. OPERATIONAL CHECK GOOD.Mar 30, 2005 · N393US · Boeing 7373B7 · Emergency LightingSDR USAA050535Floor Support · corrodedBFM - FOUND FLOOR SUPPORT ANGLE CORRODED 1.6 INCH BY .90 INCH BY .043 INCH, AFT CARGO COMPARTMENT 3 INCHES AFT OF BS 727B. CORROSION LEVEL 1, TASK C53-202-01. INSTALLED REPAIR IAW TR 53-10-06B, SRM 53-60-53. (M)Mar 28, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR SB05040Light · failedMAINTENANCE REPORTED THE LOW LEVEL SEAT MOUNTED EMERGENCY LIGHT AT ROW 10 ABC INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE LIGHT ASSEMBLY AT SEAT 10 ABC. OPERATIONAL CHECK GOOD.Mar 27, 2005 · N389US · Boeing 7373B7 · Emergency LightingSDR USAA050398Skin · crackedPIT - RON - SKIN, (2 INCH CRACK), 6.5 INCHES AFT OF BS 727D JUST ABOVE S24L. CUTOUT DAMAGE INSTALLED DOUBLER IAW SRM. (K)Mar 24, 2005 · N384US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050531Web · corrodedBFM - FOUND DOOR SILL WEB CORRODED 1 INCH BY 1 INCH BY .063 INCH AREA, FORWARD CARGO DOOR SILL BS 440-485. CORROSION LEVEL 1, TASK C53-208-01. FABRICATED SILL WEB TR 501886, SRM 53-30-15, 51-40-02. (M)Mar 23, 2005 · N374US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA050392Skin · crackedPIT - RON - SKIN, (2 INCH CRACK), 6.5 INCHES AFT OF BS 727D, JUST ABOVE S-24L. CUT OUT DAMAGE, INSTALLED DOUBLER IAW SRM. (K)Mar 23, 2005 · N384US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050364Skin · crackedPIT - RON - SKIN, 4.500 INCH CRACK, STA 727A, 727B, STR 22R. INSTALLED DOUBLER IAW SRM. (K)Mar 15, 2005 · N517AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA050363Forging · crackedCLT - C5 - FORGING, .3 INCH, CRACKED, FWD SERVICE DOOR CUTOUT UPPER FWD UPPER CORNER. REMOVED CRACKED REVEL AND REPLACED IAW DWG NR 65-55878. (K)Mar 10, 2005 · N527AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050354Support Fitting · crackedCLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK. LT WING MLG SUPPORT FITTING. ACCOMPLISHED REPAIR IAW TR 57-40-13. (K)Mar 10, 2005 · N519AU · Boeing 7373B7 · Wing, Landing Gear Attach FittingsSDR USAA050351Support Fitting · crackedCLT - Q2 - SUPPORT FITTING, .1250 INCH CRACK, MLG AFT SUPPORT FITTING. REPAIRED IAW TR57-40-13. (K)Mar 10, 2005 · N519AU · Boeing 7373B7 · Fuselage, Landing Gear Attach Fittings
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