Boeing 737-2X6C

Service difficulty reports · 1,351

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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 = '7372X6C'
  ORDER BY difficulty_date DESC"

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SDR TSAA20130423005Frame · crackedCARGO DOOR HAS 1.2500" CRACK ON Z-FRAME. REPAIR IS A TYPICAL FORMED SECTION REPAIR FROM SRM.Apr 23, 2013 · N840AL · Boeing 7372X6C · Cargo/Baggage DoorsSDR TSAA20130421004Intercostal · crackedCRACK FOUND ON INTERCOSTAL INSIDE OF FWD SERVICE DOOR FRAME BS 332.Apr 21, 2013 · N840AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA20130421003Door Frame · crackedCRACK FOUND ON FWD SERVICE DOOR DOOR FRAME B.S. 332.Apr 21, 2013 · N840AL · Boeing 7372X6C · Fuselage Main, StructureSDR TSAA20130421002Structure · cracked1.7500" CRACK FOUND ON FWD SERVICE DOOR, BS 328.Apr 21, 2013 · N840AL · Boeing 7372X6C · Service DoorsSDR TSAA20130110001Skin · crackedDURING SERVICE CHECK FOUND AN APPROX 2" CRACK ON THE LT SIDE FUSELAGE AT BS 802, ABOVE STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIG. 48.Jan 10, 2013 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA20121211008Skin · crackedDURING SERVICE CHECK, FOUND A 3 INCH SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS 827, STRINGER 19L. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XI, PROCEDURE IV & VII.Dec 11, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA20121211009Skin · crackedDURING SERVICE CHECK, FOUND A 2 INCH SKIN CRACK ON THE LT SIDE AFT OF THE T/E WING TO BODY FAIRING BS 787, STRINGER 18L. REPAIRED IAW SRM 53-30-3, FIG 48, DETAIL XI, PROCEDURE IV & VII.Dec 11, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR TSAA20121002007Plug · failedAFTER TAKEOFF, BOTH HYDRAULIC A LOW PRESSURE LIGHTS ILLUMINATED THEN EXTINGUISHED. HYDRAULIC PRESSURE NORMAL BUT HYDRAULIC QUANTITY AT ZERO. DECLARED EMERGENCY AND RETURNED DEPARTURE. INSPECTED ACFT AND FOUND PLUG FROM LT MLG ACTUATOR DAMAGED. R & R PLUG.Oct 2, 2012 · N840AL · Boeing 7372X6C · Landing Gear ActuatorSDR TSAA20121001005Skin · crackedDURING SERVICE CHECK, FOUND AN APPROXIMATELY 2 INCH CRACK ON THE LT SIDE FUSELAGE AT BS 887, ABOVE STRINGER 17L. REPAIRED CRACK IAW SRM 53-30-3, FIG 48, DETAIL XI.Oct 1, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR 7AHR201205252279Stringer Clip · crackedSTRINGER CLIP CRACKED AT FUSELAGE BS 277 AT STRINGER 15R. REMOVED DAMAGED STRINGER CLIP IAW SRM 51-30-02. FABRICATED NEW STRINGER CLIP IAW SRM 51-30-06. INSTALLED NEW STRINGER CLIP IAW SRM 51-30-2.May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Attach FittingsSDR 7AHR201205252294Skin · corrodedLT HORIZONTAL STABILIZER UPPER SURFACE REAR SPAR HAS A BROKEN RIVET HEAD AND A BULGE IN SKIN AROUND BROKEN RIVET AT STABILIZER STATION 66.5. REMOVED T/E SKIN FASTENERS. DISCOVERED CORROSION AROUND AFT SPAR OF HORIZONTAL STABILIZER. REMOVED CORROSION ON AFT SMay 25, 2012 · N841AL · Boeing 7372X6C · Horizontal Stabilizer, Plate/SkinSDR 7AHR201205252210Stringer Splice · corrodedCORROSION ON STRINGER SPLICE AT STA 907 AT STRINGER 26L. FOUND STRINGER SPLICE TO BE EXFOLIATED OUT OF LIMITS. REMOVED STRINGER SPLICE IAW SRM 51-30-2. FABRICATED STRINGER SPLICE FILLER MATERIAL IAW SRM 53-10-3 AND INSTALLED REPAIR PARTS IAW SRM 51-30-2.May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201205252424Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 787 AND RBL 40 THROUGH 55. REMOVED CORROSION IAW SRM 51-30-2. FABRICATED FLOORBEAM REPAIR IAW ECO 53-04407-1. INSTALLED FABRICATED FLOORBEAM IAW DWG 53-04407-1.May 25, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR201205242306Plate · gougedNR 2 ENGINE CROSSBEAM LOWER INBD ENGINE TO WING FAIRING HAS GOUGES ON CROSSBEAM FACE. REMOVED DAMAGED PLATE FROM CROSSBEAM IAW 51-30-2. FABRICATED NEW PLATE IAW SRM 51-20-1. INSTALLED NEW PLATE ON CROSSBEAM FACE SRM 51-30-2.May 24, 2012 · N841AL · Boeing 7372X6C · Nacelle/Pylon, Main FrameSDR 7AHR201205242207Stringer · corrodedCORROSION AT BS 1016 AT AFT PRESSURE BULKHEAD AT STRINGER 24L. REMOVED STRINGER END FITTING AND ALSO FOUND END OF STRINGER WAS ALSO CORRODED. FABRICATED NEW STINGER END FITTING AND STRINGER SPLICE, ALL REPAIR PARTS INSTALLED IAW SRM 53-10-3.May 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201205242213Support · crushedBS 727 AT STRINGER 19R HORIZONTAL BULKHEAD PANEL SUPPORT FRAME IS CRUSHED IN AFT PIT. REMOVED HORIZONTAL BULKHEAD PANEL SUPPORT FRAME AT FUSELAGE STATION 727 IAW SRM 51-30-2. FABRICATED NEW SUPPORT FERAME IAW SRM 51-20-01. INSTALLED NEW SUPPORT FRAME IAW SRMMay 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR 7AHR201205292272Shear Tie · corrodedCORROSION AT FUSELAGE STA 400 AND STRINGER 26R, FUSELAGE FRAME. REMOVED CORRORED SHEAR TIE IAW SRM 51-30-02, FABRICATED AND ISTALLED A NEW SHEAR TIE IAW SRM 51-10-02 AND 51-30-02.May 24, 2012 · N841AL · Boeing 7372X6C · Fuselage Internal Mounting StructureSDR 7AHR201205222468Fairing · damagedNR 3 FLAP FAIRING FORWARD LOWER L/E IS DAMAGED. REPAIRED IAW SRM`S 51-30-2, & 51-40-3.May 22, 2012 · N841AL · Boeing 7372X6C · Trailing Edge FlapsSDR 7AHR201205222209Stringer Splice · corrodedCORROSION AT FUSELAGE STA 907 AT STR 27L AT STRINGER SPLICE. REMOVED STRINGER SPLICE AND STRINGER CLIP DUE TO CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. FABRICATED REPAIR COMPONENTS IAW SRM 53-10-03. INSTALLED REPAIR COMPONENTS IAW SRM 51-30-02.May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201205222466Frame · corrodedAFT TAIL CONE ACCESS DOOR PANEL NR 3802 FRAME HAS CORRODED RIVET HEADS AND RUB PADS. REMOVED RIVETS AND RUB PADS FROM TAIL CONE ACCESS DOOR IAW SRM 51-30-2. FABRICATED NEW RUB PADS AND INSTALLED RUB PADS AND NEW FASTENERS AS IAW SRM 51-30-2.May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, StructureSDR 7AHR201205222074Skin · misrepairedLOWER FUSELAGE PRESSURIZATION LEAK AT EXTERNAL REPAIR FWD EDGE AT STA 907 AT STRINGER 20L AT LAP SEAM AND BUTT SPLICE DOWN TO STR 25L LAP SEAM. REMOVED FASTENERS IN EXISTING REPAIR AT STR 20L STA 907 - 917. REAMED HOLES TO PROPER SIZE IAW SRM 51-30-05, FIG 3May 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR 7AHR38412A2073Skin · misrepairedLOWER FUSELAGE, PRESSURIZATION LEAK AT EXTERNAL REPAIR (APPROX 30 RIVETS) BELOW R-1 DOOR. STA 312 AT STRINGER 19R LAP SEAM. REMOVED FASTENERS AT LOWER FUSELAGE AT STA 312 STR 19R AT LAP SEAM. PERFORMED NDT INSP OF FASTENER HOLES, NO DEFECT NOTED. FOUND WHENMay 22, 2012 · N841AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR 7AHR201204132167Skin · corrodedEXFOLIATION CORROSION AT STA 1016 AT STRINGER 26R TO 27R IN AREA OF OUTER WASTE DRAIN PAN. REMOVED CORROSION, AFTER REMOVAL OF CORROSION IT WAS DETERMIND THAT THERE WAS EXCESSIVE MATERIAL LOSS, WHICH DETERMIND THE AREA TO BE OUT OF LIMITS. AFTER EVALUATION IApr 13, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Plate/SkinSDR 7AHR35012D2219Stringer Splice · corrodedCORROSION AT FUSELAGE BULKHEAD BS 1016 AT STRINGER 25R. REMOVED CORROSION, AFTER CORROSION REMOVAL, AREA FOUND TO BE OUT OF LIMITS AT STRINGER 25R FROM STA 1016 TO 1026. FABRICATED REPAIR SPLICE AND INSTALLED REPAIR COMPOENENTS IAW SRM.Apr 13, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201204132155Skin · corrodedCORROSION RT WING UPPER SURFACE UNDER WING WALKWAY PAINT AT WING STA 765.9 AT WBL 92.5. BLENDED CORROSION, AFTER CORROSION REMOVAL IT WAS DETERMIND THE MATERIAL LOSS WAS OUT OF LIMITS. AFTER REVIEWING THE CURRENT SRM IT WAS DETERMIND THERE WAS NOT REPAIR IN Apr 13, 2012 · N840AL · Boeing 7372X6C · Wing, Plate/SkinSDR 7AHR201204132381Floor Support · corrodedCORROSION ON FLOOR SUPPORT AT STA 663 NEAR RBL 45. REMOVED CORROSION FROM FOUND SUPPORT, CORROSION FOUND TO BE OUT OF LIMITS. R & R FLOOR SUPPORT IAW CURRENT SRM.Apr 13, 2012 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR 7AHR201204112458Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 767 AT RBL 45. REMOVED CORROSION, AFTER CORROSION REMOVAL, DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED CORRODED FLOORBEAM, AND FABRICATED REPAIR STRAPS AND INSTALLED STRAPS IAW CURRENT SRM.Apr 11, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR201204112459Floorbeam · corrodedCORROSION ON FLOORBEAMS AT BS 706 AT RBL 45. REMOVED CORROSION FROM FLOORBEAM BS 706. CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS FOR FLOORBEAM AND INSTALLED ALL REPAIR PARTS IAW CURRENT SRM.Apr 11, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR201204112597Rib · crackedNR 2 ENGINE FIXED FAN COWL HAS CRACKED RIB. REMOVED CRACKED RIB AND FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW CURRENT SRM.Apr 11, 2012 · N840AL · Boeing 7372X6C · Nacelle/Pylon, Frame/Spar/RibSDR 7AHR201204112562Frame · crackedCRACK AT INTERNAL FRAME, STRINGER 5R BODY STATION 380. REMOVED 2 EA STRINGER CLIPS 5R AT BODY STATION 380, REMOVED DAMAGED INTERIOR FRAME, FABRICATED REPAIR PARTS AND INSTALLED ALL REPAIR PARTS IAW SRM.Apr 11, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, FrameSDR 7AHR201204092598Rib · crackedLEFT FORE FLAP WBL 355 INBD SIDE OF RIB HAS A CRACK IN FITTING. R & R IAW SRM.Apr 9, 2012 · N840AL · Boeing 7372X6C · Leading Edge DevicesSDR 7AHR201204092588Rib · corrodedCORROSION ON AFT RIB OF LT MLG INNER DOOR. FOUND RIB ON INNER DOOR FOR LT MLG CORROSION BEYOND LIMITS. R & R RIB IAW SRM.Apr 9, 2012 · N840AL · Boeing 7372X6C · Landing Gear DoorsSDR 7AHR201204092258Access Panel · corrodedCORROSION AT LT WING FWD LOWER SPAR AT ACCESS PANEL MATING SURFACE FROM WBL 227.0 TO WBL 522.0. REMOVE ALL CORROSION FROM PANEL MATING SURFACE. MATERIAL LOSS FOUND TO OUT OF LIMITS AT WBL 291.82 AND WBL 314.76. DAMAGE FOUND TO BE OUTSIDE OF THE PARAMETER OUTApr 9, 2012 · N840AL · Boeing 7372X6C · Wing, Plate/SkinSDR 7AHR201204092154Skin · corrodedCORROSION ON TOP OF LT WING UNDER WALKWAY PAINT. BLENDED CORROSION, AFTER CORROSION REMOVAL FROM WING SKIN, MATERIAL LOSS FOUND TO BE OUT OF LIMITS. REPAIR REQUIREMENTS FOUND TO BE OUTSIDE OF STANDARD SRM REPAIR. FABRICATED REPAIR PARTS AND INSTALLED ALL RApr 9, 2012 · N840AL · Boeing 7372X6C · Wing, Plate/SkinSDR 7AHR201204072657Stringer · corrodedCORROSION AT BS 1004, AT STRINGER 27L. CUT OUT CORRODED SECTION OF STRINGER. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.Apr 7, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201204072391Stringer Splice · crackedSTRINGER SPLICE CRACKED AT S4L AT BS 908. REMOVED CRACKED STRINGER SPLICE, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.Apr 7, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Longeron/StringerSDR 7AHR201204072456Seat Track · corrodedCORROSION ON SEAT TRACK AT STA 540 TO 578 AT LBL 24.75. REMOVED CORROSION, SEAT TRACK FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM.Apr 7, 2012 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR201204072138Retainer Seal · corrodedCORROSION ON RT NR 5 L/E SLAT LOWER SEAL RETAINER. REMOVED CORROSION, SEAL RETAINER FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAL REATINER AND INSTALLED IAW WITH CURRENT SRM.Apr 7, 2012 · N840AL · Boeing 7372X6C · Leading Edge DevicesSDR 7AHR201204072417Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 312 AT RBL 12. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS. CUT OUT TEE CAP EXTRUSION, FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW SRM.Apr 7, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR201204062296Angle · crackedAFT CARGO BAY LEFT TRANSITION PANEL ANGLE CRACKED BETWEEN STATION 907 AND 927. REMOVED CRACKED ANGLE AND FABRICATED REPLACE PARTS IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Miscellaneous StructureSDR 7AHR201204062249Retainer Seal · corrodedCORROSION ON NR 2 L/E SLAT LOWER RUB SEAL RETAINER OTBD OF SLAT ACTUATOR ATTACH POINT. REMOVED CORRODED SEAL RETAINER, FABRICATED REPAIR PARTS AND INSTALLED SEAL RETAINER IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Wing Miscellaneous StructureSDR 7AHR201204062571Bracket · crackedLEFT INBD MID FLAP - OTBD CARRIAGE ASSY PULLEY SUPPORT BRACKET CRACKED. R & R PULLEY SUPPORT BRACKET IAW WITH MM 27-51-21.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Attach FittingsSDR 7AHR201204062581Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 540 AND LBL 24. REMOVED CORROSION, FLOOR SUPPORT FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR STRAP AND INSTALLED REPAIR PARTS IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Cabin Equipment/FurnishingsSDR 7AHR201204062580Seat Track · corrodedCORROSION ON SEAT TRACK AT STATION 540 AND RBL 64. AFTER CORROSION REMOVAL, SEAT TRACK FOUND TO BE OUT OF LIMITS. REPLACED SEAT TRACK IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR2012040600003Rub Strip · gougedLT INBD ENGINE TO WING FLAP SUPPORT FITTING RUB STRIP IS GOUGED. REMOVED RUB STRIP, FABRICATED REPAIR STRIP AND INSTALLED STRIP IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Wing Miscellaneous StructureSDR 7AHR201204062365Floorbeam · corrodedCORROSION ON FLOORBEAM CAP AT STA 727B AND APPROX LBL 40. AFTER CORROSION REMOVAL FLOORBEAM FOUND TO BE OUT OF LIMITS. FABRICATED A REPAIR STRAP AND INSTALLED IAW CURRENT SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR201204062357Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 727B AND RBL 24. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED ALL REPAIR PARTS IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR2012040600002Floorbeam · corrodedCORROSION ON FLOORBEAM AT STA 727 AND RBL 24 TO 36. REMOVED CORROSION, FLOORBEAM FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR STRAP AND INSTALLED IAW CURRENT SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Floor BeamSDR 7AHR2012040600001Seat Track · corrodedCORROSION ON SEAT TRACK AT STA 663 TO 727 AND LBL 62. REMOVED CORROSION, SEAT TRACK BECAME OUT OF LIMITS. R & R SEAT TRACK IAW SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage, Seat/Cargo Attach FittingsSDR 7AHR201204062366Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 967 AND RBL 12. CORROSION FOUND TO BE OUT OF LIMITS. PERFORMED A SPLICE REPAIR TO THE FLOORBEAM IAW CURRENT SRM.Apr 6, 2012 · N840AL · Boeing 7372X6C · Fuselage Main, Bulkhead
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