Boeing 737-2Y5

Service difficulty reports · 334

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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 = '7372Y5'
  ORDER BY difficulty_date DESC"

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SDR F3LA200300080Seat Track · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION IN AND AROUND SCREW HOLES AT SEAT TRACK BETWEEN STA. 328 AND STA. 344, RBL 54. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-3.Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA200300078Intercostal · corrodedDURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON AFT GALLEY FLOOR INTERCOSTAL AT STA. 957, LBL 18.75 THRU LBL 40.5. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 51-30-02. FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL PER EA 53-737-198 AND SRM 51-Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300077Seat Track · corrodedDURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT NUTCLIP HOLES, RT. SIDE BETWEEN FLOORBEAM AT STA. 986.5 TO STA. 1016. REPLACED SEAT TRACK PER SRM 53-10-01, FIG. 3, SRM 51-30-02, MM 51-21-41 AND SOPM 20-41-02.Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage, Seat/Cargo Attach FittingsSDR F3LA200300075Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA. 312, LBL 13 TO RBL 10. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED NEW CAP PER SRM 53-10-1.Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300076Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM AT SCREW HOLE, STA. 328, LBL 29. REMOVED TOP CAP REPAIR ANGLE, FABRICATED AND INSTALLED REPAIR ANGLE TO TOP CAP PER SRM 51-40-02.Feb 19, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300074Stringer · corrodedDURING C-4 CHECK, INSPECTION REPORTED SURFACE CORROSION ON STRINGER 18-R AT STA. 727B + 16. REPAIRED DAMAGED SECTION OF STRINGER PER SRM 53-10-1, PAGE 6, DETAIL VI, SRM 53-10-3, PAGE 10, DETAIL VII AND SOPM 20-41-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/StringerSDR F3LA200300073Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON BULKHEAD ANGLE AT STA. 947.5 LOWER ANGLE. FABRICATED AND INSTALLED REPLACEMENT ANGLE PER SRM 51-30-1, 53-20-01, FIG. 5, DETAIL II, 51-30-02 AND SOPM 20-41-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300072Panel · puncturedDURING C-4 CHECK, INSPECTION REPORTED SMALL PUNCTURE IN TRANSITION PANEL BETWEEN STA. 767 AND 794. REPAIRED PANEL PER SRM 53-10-13 AND SOPM 20-4-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300071Seat Track · corrodedDURING C-4 CHECK, INSPECTION REPORTED SEAT TRACK CORRODED AT STA 290, RBL 16. FABRICATED AND INSTALLED REPLACEMENT SEAT TRACK PER SRM 51-30-2 AND 53-10-2.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300070Clip · corrodedDURING C-4 CHECK, INSPECTION REPORTED TIE CLIP AND ATTACHING HARDWARE CORRODED AT AFT END OF RT MOP SILL BEHIND R-2 DOOR. REPLACED CLIP HARDWARE PER SRM 51-30-2. NO CORROSION WAS FOUND ON CLIP. CLEANED AREA PER SOPM 20-41-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300069Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, LBL 3, AT NUT PLATE ON UNDERSIDE OF FLANGE. FABRICATED AND INSTALLED FLOOR SUPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300068Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM BETWEEN STA 727 AND 727A, RBL 3, AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE. FABRICATED AND INSTALLED FLOOR SUPPPORT AND SPLICE PER SRM 53-10-3, FIG 11, AND SOPM 20-41-02.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300067Support Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOOR/LAVATORY SUPPORT BEAM BETWEEN STA 986.5 AND STA 1006 CORRODED. REMOVED SUPPORT ANGLE AND HAT CHANNEL PER SRM 51-30-02. FOUND CORROSION ON BOTH HAT CHANNEL AND SUPPORT ANGLE OUT OF LIMITS PER SRM 51-30-02. FABRICATFeb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300066Stringer · corrodedDURING C-4 CHECK, INSPECTION REPORTED HEAVY CORROSION AT STR 27-L BETWEEN STA 945 AND STA 953.5. REPLACED STRINGER FROM STA 945 TO STA 967.5, LBL 3, STR 27-L, PER SRM 53-10-3, 51-20-2 AND 51-30-5.Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Longeron/StringerSDR F3LA200300065Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON FLOORBEAM CAP AT STA 344, LBL 60 - RBL 14. REMOVED DAMAGE ON WEB BETWEEN STA 332 AND STA 344 AFT OF R-1 DOOR PER SRM 51-40-2, PAGES 1-3. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-02, PAGES 1-3, AND SOPM Feb 18, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300064Attach Angle · corrodedDURING C-4 CHECK, INSPECTION REPORTED RT RAM AIR DUCT ANGLE ATTACH POINT FOR CROSS BRACE UNDER WING BLEED AIR DUCT CORRODED AT STA 540, STR 22R. REMOVED DAMAGED ANGLE, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3, FIG 1, SHEET 2, 51-40-3.Feb 17, 2003 · N921WA · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200300063Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP CORRODED AT STA 290, RBL 15. FABRICATED AND INSTALLED REPLACEMENT CAP STRIP PER SRM 53-10-2 AND 53-10-9.Feb 17, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300062Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED FLOORBEAM CAP AT STA 1006 CORRODED IN VARIOUS AREAS FROM CENTERLINE EXTENDING TO LEFT SIDE. REPAIRED PER SRM 53-10-9, FIG 7.Feb 14, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR F3LA200300061Floorbeam · corrodedDURING C-4 CHECK, INSPECTION REPORTED CORROSION ON CARGO FLOORBEAM AT NUT PLATE ON UNDERSIDE OF UPPER FLANGE, STA 794, LBL 8. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-01. FABRICATED AND INSTALLED REPAIR PER SRM 53-10-05, SRM 53-10-05, FIG 11, SHEET Feb 13, 2003 · N921WA · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR TSAA0353037Skin · crackedNINE RIVETS ON STRINGER 16R SHOW SIGNS OF STRESS CRACKS EMANATING FROM THE FASTENER HOLES. REMOVED RIVETS, OVERSIZED HOLES BY 1/16, HFEC VERIFIED FASTENER HOLES CRACK FREE. FABRICATED FILLER AND DOUBLER. ALODINED AND PRIMED ALL BARE SURFACES. INSTALLED REPAFeb 9, 2003 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR F3LA200200397Trunnion · corrodedDURING NOSE GEAR CHANGE, INSPECTED REPORTED LT NOSE GEAR TRUNNION BOSS CORRODED. REPLACED NOSE GEAR TRUNNION BOSS.Dec 23, 2002 · N921WA · Boeing 7372Y5 · Nose/Tail Landing Gear Attach SectionSDR FL3A200200389Check Valve · inoperativeDURING CLIMB OUT, THE FLIGHT CREW NOTED AN ILLUMINATED WING/BODY OVERHEAT LIGHT WHICH WOULD NOT EXTINGUISH WHEN QUICK REFERENCE HANDBOOK ITEMS WERE ACCOMPLISHED. THE AIRCRAFT RETURNED TO THE DEPARTURE AIRPORT.MAINTENANCE REMOVED AND REPLACED THE START MANIFOLNov 16, 2002 · N118RW · Boeing 7372Y5 · Pneumatic SystemSDR TSAA0233228Battery Pack · dischargedREPLACED NR 4 POSITION FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency LightingSDR TSAA0233229Light · inoperativeREPLACED LT OVERWING IDENT LIGHT DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Nov 8, 2002 · N810AL · Boeing 7372Y5 · Emergency LightingSDR F3LA200200385Hydraulic Line · damagedDURING FLIGHT, A SYSTEM HYDRAULIC QUANTITY DROPPED TO ZERO FOLLOWED BY THE FAILURE OF THE NUMBER 2 ENGINE, ENGINE DRIVEN HYDRAULIC PUMP. A SYSTEM PRESSURE REMIAINED NORMAL. ON FINAL APPROACH TO DIVERSION SITY AIRPORT, A SYSTEM PRESSURE DROPPED TO ZERO. STANNov 6, 2002 · N118RW · Boeing 7372Y5 · Hydraulic Power SystemSDR TSAA0253201Structure · gougedCUTOUT DAMAGE, PERFORMED A DETAILED VISUAL AND HFEC INSPECTION OF THE CUTOUT AND ALL LAP SPLICE FASTENERS HOLES IN THE REPAIR AREA, NO DEFECTS NOTED. FABRICATED A DOUBLER, TRIPLER STRUCTURAL FILLER. AIRCRAFT RETURNED TO SERVICE.Oct 2, 2002 · N810AL · Boeing 7372Y5 · Cargo/Baggage DoorsSDR F3LA200200265A/C Pack · malfunctionedAIR TURN BACK. FLIGHT CREW REPORTED SMOKE IN CABIN, LT WING/BODY OVERHEAT ILLUMINATED AND RT PACK TRIPPED OFF. DECLARED AN EMERGENCY AND RETURNED TO DEN. AIRCRAFT LANDED WITHOUT INCIDENT. ON APPROACH, AILERONS WERE DIFFICULT TO MOVE AND HAD A SHUDDER BELOWSep 25, 2002 · N118RW · Boeing 7372Y5 · Cabin Cooling SystemSDR F3LA200200258Odor · detectedAIR TURNBACK. FLIGHT CREW REPORTED FWD LAVATORY SMOKE ALARM ACTIVATED WHILE CLIMBING THROUGH 8000 FT. PASSENGERS IN ROW 2 NOTED DISTINCT SMELL/ODOR OR SMOKE (OVEN/ELECTRICAL) DURING FLIGHT. NR 2 PACK TRIP OFF LIGHT ILLUMINATED IMMEDIATELY BEFORE SMOKE ALARMSep 10, 2002 · N118RW · Boeing 7372Y5 · Air Distribution SystemSDR F3LA200200201Overheat Loop · out of positionDURING CLIMBOUT, THE FLIGHT CREW DISCOVERED A WIND/BODY OVERHEAT LIGHT ON. QRH ITEMS ACCOMPLISHED AND LIGHT EXTINGUISHED. AIR TURNBACK ACCOMPLISHED. UPON INSPECTION BY MAINTENANCE, AFT CARGO PIT HAD TWO AREAS WHERE THE OVERHEAT DETECTOR WAS TOUCHING THE BLEJul 26, 2002 · N118RW · Boeing 7372Y5 · Overheat DetectionSDR TSAA0253183Frame · corrodedAUXILIARY POWER UNIT COMPARTMENT CORRODED AT BS 1156 REMOVED DAMAGED SECTION OF FRAME FABRICATED AND INSTALLED REPAIR FILLER AND DOUBLER FROM SRM, AIRCRAFT RETURNED TO SERVICE.Jun 29, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, FrameSDR TSAA0253152Skin · crackedFOUND CRACK ON FUSELAGE SKIN, STRINGER 21L AT BS 985.5. TRIMMED OUT DAMAGED AREA AND VERIFIED USING HFEC METHOD NO DEFECTS NOTED. FABRICATED AND INSTALLED FILLER AND REPAIR DOUBLER PER SRM. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.Jun 17, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR F3LA200200152Fire Detector · false activationUPON ARRIVAL AT GATE, FLIGHT CREW REPORTED THE FIRE BELL SOUNDED AND THE NR 1 ENGINE FIRE HANDLE WAS ILLUMINATED. PULLED NR 1 FIRE HANDLE AND DISCHARGED THE LEFT BOTTLE INTO THE NR 1 ENGINE. INSPECTED NR 1 ENGINE FOR EVIDENCE OF FIRE, NONE FOUND. INSPECTED May 21, 2002 · N118RW · Boeing 7372Y5 · Fire DetectionSDR TSAA0253142Skin · corrodedFOUND CORROSION ON THE LEFT HAND OUTBOARD WING MAIN BOX UPPER SKIN AT WBL 71.24, STR 5, 7 AND WBL92.5 STR 1, 5. BLENDED OUT CORROSION AT A 10:1 RATIO MINIMUM PER SRM. ULTRASOUND INSPECTED TO ENSURE NO REMAINING CORROSION. HFEC AFFECTED FASTENER HOLE BORE FOMay 15, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253141Skin · wornFOUND SKIN WORN THROUGH ON THE RIGHT LEADIN EDGE LOWER WING SKIN SURFACE AT FS 413. CUT OUT DAMAGED LEADING EDGE FILLER AND SKIN. FABRICATED REPAIR PARTS, ALODINED, PRIMED AND INSTALLED THE REPAIR PARTS WITH FASTENERS. APPLIED BMS 5-95 SEALANT TO THE MATINGMay 13, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253134Pressure Panel · corrodedFOUND CORROSION ON NOSE LANDING GEAR BULKHEAD AT BS 227.8. CUT OUT CORROSION AND VERIFIED REMOVED BY VISUAL INSPECTION. FABRICATED CHORD AND REPAIR ANGLES. INSTALLED CHORD AND REPAIR ANGLES. COMPLETED REPAIR.May 13, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0251133Skin · gougedFOUND GOUGE IN SKIN AT STRINGER 16L AT BS 843. BLENDED OUT DAMAGED AREA TO A SMOOTH SURFACE. VERIFIED NO CRACKS USING HFEC. REPAIR COMPLETED IAW SRM. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Plate/SkinSDR TSAA0251132Bracket · chafedFOUND NR 8 FLAP JACKSCREW TRAILING EDGE MOUNT BRACKET CHAFFING AT FLAP TRACK FAIRING. BLENDED OUT DAMAGED AREA. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Trailing Edge FlapsSDR TSAA0251130Slat · corrodedFOUND CORROSION ON THE RIGHT WING AFT OF THE NR 5 SLAT FITTING. BLENDED OUT CORROSION. FABRICATED AND INSTALLED PARTS. REWORK COMPLETED. AIRCRAFT RETURNED TO SERVICE.May 10, 2002 · N810AL · Boeing 7372Y5 · Leading Edge DevicesSDR TSAA0253146Skin · wornRIGHT WING LEADING EDGE LOWER SKIN AT FSS 413 WORN BEYOND LIMITS. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED FILLER, SPLICE PLATE AND DOUBLER. AIRCRAFT RETURNED TO SERVICE.Apr 25, 2002 · N810AL · Boeing 7372Y5 · Wing, Plate/SkinSDR TSAA0253125Spar · corrodedFOUND CORROSION ON RIGHT WING FRONT SPAR, LOWER CHORD FORWARD HORIZONTAL FLANGE FORWARD LIP AT FSS 413. REMOVED CORROSION BY BLEND OUT. HFEC AREA TO ENSURE FREE OF CRACKS AND CORROSION. FABRICATED A REPAIR FILLER. INSTALLED REPAIR FILLER. REPAIR COMPLETEDApr 25, 2002 · N810AL · Boeing 7372Y5 · Wing SparSDR TSAA0253127Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, RBL 5.7 DURING INSPECTION. CUTOUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PART.Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0253126Bulkhead · crackedFOUND CRACK ON THE BLK 178 AT WL 212, LBL 5.7 DURING INSPECTION PER ECO 3137. CUT OUT CRACK AND REMOVED DAMAGED SECTION OF WEB. VERIFIED CRACK REMOVAL USING HFEC. FABRICATED DOUBLER AND FILLERS. INSTALLED REPAIR PARTS. AIRCRAFT RETURNED TO SERVICE.Apr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, BulkheadSDR TSAA0253128Stringer · dentedFOUND DENT ACROSS STRINGER 15L AT BS 900. CUTOUT STRINGER SEGMENT AT BS 900. REMOVED THE SEGMENT OF THE STRINGER AFT TO THE PRODUCTION SPLICE. FABRICATED NEW STRINGER SEGMENT. INSTALLED STRINGER PER SRM 53-10-3. COMPLETED REPAIR. AIRCRAFT RETURNED TO SERApr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Longeron/StringerSDR TSAA0253131Floorbeam · crackedFOUND CRACKS AT BL 0 FLOOR BEAM AT BS 663 AND BETWEEN BS 700-717 WEB. REMOVED AND DISCARDED A SECTION OF THE WEB AND DOUBLER CONTAINING THE CRACKS. FABRICATED ALL REPAIR PARTS. INSTALLED SPLICE ANGLES AND STRAPS WITH NUT PLATES. COMPLETED INSTALLATION OF RApr 23, 2002 · N810AL · Boeing 7372Y5 · Fuselage Main, Floor BeamSDR SPAA0200053Power Supply · power lossAIRCRAFT BATTERY LOW VOLTS, POSSIBLE BATTERY AMP/VOLTS DRAW FROM OTHER SOURCE.Apr 22, 2002 · N712S · Boeing 7372Y5 · Emergency LightingSDR SPAA0200051Panel · delaminated#5 SPOILER PANEL HAS AREAS OF DELAMINATION NOTED ON PREFLIGHT MAINTENANCE CHECK.Mar 15, 2002 · N712S · Boeing 7372Y5 · Flight Control SystemSDR SPAA0200052Panel · delaminatedFOUND RT INBOARD TRAILING EDGE MIDFLAP WEDGE PANEL DELAMINATED.Mar 14, 2002 · N712S · Boeing 7372Y5 · Trailing Edge FlapsSDR F3LA200200103Cowling · crackedDURING C-3 CHECK, INSPECTION REPORTED CRACK ON AFT LOWER CORNER OF NR 2 ENGINE OUTBOARD FIXED COWL NEXT TO FIRE SEAL. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3 AND 51-30-2.Feb 28, 2002 · N118RW · Boeing 7372Y5 · Engine Cowling SystemSDR F3LA200200102Web · corrodedDURING C-3 CHECK, INSPECTION REPORTED AFT LAVATORY FLOOR WEB CORRODED, STA 1016, AT DRAIN TO LBL 30.Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous StructureSDR F3LA200200101Attach Angle · corrodedDURING C-3 CHECK, INSPECTION REPORTED CORROSION ON SIDEWALL PANEL ATTACH ANGLE AT STA 727, LBL 21 TO LBL 25.Feb 28, 2002 · N118RW · Boeing 7372Y5 · Fuselage Miscellaneous Structure
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