N354US, cancelled Aug 29, 2007
Service difficulty reports · 62
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N354US' AND deregistration_id = 'N354US-2007-08-29' 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.
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 n_number = 'N354US' AND deregistration_id = 'N354US-2007-08-29' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR USAA050768Skin · crackedCLT - FOUND SKIN CRACKED 4 INCHES, STATION 727D, S23R. INSTALLED DOUBLER IAW SRM 53-00-01, FIG 229 DETAIL XI. (M)SDR USAA050767Skin · puncturedCLT - FOUND SKIN PUNCTURED 1 INCH BY 2.5 INCH, BS 312-322 AT S23R. INSTALLED DOUBLER IAW SRM 53-00-01 FIG 229. (M)SDR USAA050221Plate · crackedPIT - FOUND HINGE DOUBLER PLATE CRACKED .3750, MED TOP FORWARD HINGE CUTOUT INSIDE BOTTOM FORWARD CORNER. INSTALLED WEB PER SRM 51-40-02 AND DWG 65-17684. (M)SDR USAA040065Floor Support · crackedFOUND FLANGE CRACKED 1.5 INCH FLOOR SUPPORT STATION 937 BL 0. REMOVED TOP FLANGE OF FLOOR SUPPORT, REPLACED WITH NEW PART EPN 1138864 PER SRM 51-40-00. (M)SDR USAA040064Shear Web · corrodedFOUND SHEAR WEB CORRODED 3 INCHES BY 10 INCHES, TOP AND LOWER SURFACE OF FLOOR PAN AT AFT PRESS BULKHEAD, RBL 0-15. DEFECTIVE PART REPLACED WITH IDENTICAL PART NR PER SRM 51-40-2. CORROSION LEVEL 1, TASK NR C53-107-02. (M)SDR USAA040063Floor Panel · gougedFOUND FLOOR PANEL GOUGED 4 INCHES, STATION 992 RBL 39. MANUFACTURED OUT OF 2024 T3 020 PER SRM 51-40-02. (M)SDR USAA040120Keelbeam · corrodedFOUND KEELBEAM CORRODED AND PITTING 1 INCH BY 4 INCH AREA, RT KEELBEAM LOWER SURFACE STATION 663.75 TO 727. INSTALLED REPAIR STRAP PER EA 78097. LEVEL 1 TASK NR C53-212-01. (M)SDR USAA040095Skin · crackedFOUND SKIN WITH 3 INCH STRESS CRACK, FORWARD OF AFT BAGGAGE PIT DOOR BS 727E S18R. STRESS CRACK REPAIR PER SRM 53-00-01 FIG 201, AND OM-7 NR 27801. (M)SDR USAA030169Support · corrodedFOUND UPPER SUPPORT CORRODED .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH, NLG UPPER SUPPORT. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAA030152Support · corrodedPHL - FOUND UPPER SUPPORT CORRODED TOP AND BOTTOM, .004 INCH TOP AND BOTTOM TOTAL OF .008 INCH. DEFECTIVE PART REPLACED WITH IDENT PART NR. (M)SDR USAASB01288Indicator · faultyBUF - FLT 1157 - AFTER TAKEOFF FROM BUF, EN ROUTE TO CLT, CREW EXPERIENCED A FLAP ASYMMETRY PROBLEM DURING FLAP RETRACTION. ONE FLAP WAS IN THE 5 DEGREE POSITION AND THE OTHER WAS IN THE 2 DEGREE POSITION. CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD AT SDR USAASB00231Wire · brokenPIT - MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT BEHIND THE LEFT WING INOPERATIVE. MAINTENANCE FOUND A BROKEN WIRE AT SPLICE JUST ABOVE EMERGENCY LIGHT IN AFT CARGO BAY. INSTALLED NEW SPLICE. OPS CHECK GOOD. (M)SDR USAA001122Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZONTAL STAB LOWER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1 C-53-701-02. REMOVED CORROSION PER SRM 55-10-10. (M)SDR USAA001121Bushing · corrodedCLT - FOUND LUG AND BUSHING CORRODED .25 INCH, LEFT HORIZ STAB UPPER ATTACH BOLT FRONT SPAR. CORROSION LEVEL 1. REMOVED CORROSION PER SRM 55-10-10. (M)SDR USAA001125Pressure Panel · crackedCLT - FOUND PRESSURE DECK WITH TWO CRACKS .5 INCH AND 1 INCH, PRESS DECK MLG WHEEL WELL STRINGER 663, LBL 30. REMOVED DAMAGE INSTALLED REPAIR DOUBLER AND FILLER PER TR 53-60-04. (M)SDR USAA001124Floorbeam · corrodedCLT - FOUND FLOORBEAM T-CAP CORRODED 2 INCHES, STATION 328, LBL 49. CORROSION LEVEL 1, C53-107-01. REMOVED CORROSION AND INSTALLED NEW T-CAP PER SRM 51-70-12 FIG 1. (M)SDR USAA001123Beam · crackedCLT - FOUND SUPPORT BEAM CRACKED .375 INCH, LEFT MLG SUPPORT BEAM. ACCOMPLISHED INTERMIN REPAIR PER EA 67644 AND TR 57-40-13. (M)SDR USAA001085Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH BY 2 INCH AREA, STATION 294.5, RBL 45. REMOVED AND INSTALLED FABRICATED ANGLE PER SRM 53-10-08 AND 51-40-02. (M)SDR USAA001090Splice · crackedCLT - FOUND STRINGER SPLICE CRACKED .25 INCH, STRINGER 4R SPLICE STATION 907. REMOVED DAMAGE AND INSTALLED PER SRM 51-10-02. (M)SDR USAA001089Frame · crackedCLT - FOUND FRAME CRACKED .025 INCH, AFT SIDE FRAME 847 AT TWO RIVETS JUST ABOVE STRINGER 9L. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-00-07 FIG 201 AND TR 53-10-14A. (M)SDR USAA001088Skin · crackedCLT - FOUND SKIN CRACKED .375 INCH, FUSE SKIN AT LOWER AFT CORNER OF DOOR CUTOUT. REMOVED DAMAGE AND INSTALLED REPAIR PER SRM 53-10-01 FIG 202. (M)SDR USAA001087Door Frame · crackedCLT - FOUND FRAME CRACKED .125 INCH, FORWARD SERVICE DOOR JAMB FORWARD FRAME AT LOWER OUTBOARD CORNER. REMOVED AND REPLACED PER SRM 51-40-02 AND BOEING DWG 65 45807. (M)SDR USAA001086Attach Angle · crackedCLT - FOUND ATTACH ANGLE CRACKED 1 INCH, HORIZ STAB CENTER BOX LOWER CHORD TO WEB. INSTALLED NEW ANGE PER TR 51-10-02. (M)SDR USAA001010Support Bracket · crackedCLT - FOUND DOOR SUPPORT CRACKED .25 INCH, STATION 294.5, FRAME AT STRINGER 14L. FABRICATED NEW WEB AND INSTALLED PER SRM 51-70-11. (M)SDR USAA001009Door Frame · crackedCLT - FOUND FRAME CRACKED .25 INCH, STATION 294.5, STRINGER 7L. REPAIRED PER SRM 53-10-15. (M)SDR USAA001008Door Frame · crackedCLT - FOUND FRAME CRACKED 2.5 INCHES, STATION 294.5, FORWARD SERVICE DOOR FRAME WL 208. REMOVED DAMAGED AREA INSTALLED REPAIR DOUBLER PER SRM 50-70-11. (M)SDR USAA001007Web · crackedCLT - FOUND WEB CRACKED .500 INCH, STRINGER 14R, WEB INNER CHORD ANGLE STATION 278. FABRICATED NEW WEB AND INSTALLED PER SRM 51-40-00 AND DWG 6 45807. (M)SDR USAA001006Bulkhead · crackedCLT - FOUND WEB CRACKED TWO PLACES .25 INCH AND 1.5 INCH, STATION 178 BULKHEAD, WEB RBL 6.75, WL 201. FABRICATE REPAIR DOUBLER PER SRM 53-10-08 DETAIL 111. (M)SDR USAA001005Angle · crackedCLT - FOUND CHORD ANGLE CRACKED .5 INCH, LBL 5.7 VERT CHORD L/B FLANGE STATION 178, WL 184. INSTALLED REPAIR ANGLE AND STRAPS PER SRM 53-10-08. (M)SDR USAA001004Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 36. FABRICATED T-CAP PER REPAIR DOCUMENT 53-10-51. (M)SDR USAA001003Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 28. REMOVED AND REPLACED T-CAP PER SRM 53-10-51. CORROSION LEVEL 1. (M)SDR USAA001002Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 344, LBL 14. CORROSION LEVEL 1. FABRICATED T-CAP PER SRM 53-10-51. (M)SDR USAA001001Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, LBL 12. REMOVED DAMAGED T-CAP PER SRM 53-10-51 FIG 205. (M)SDR USAA001022Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 328, LBL 28. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND INSTALLED PER REPAIR 51-70-12. (M)SDR USAA001021Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 2 INCHES, STATION 312, BL 0. CORROSION LEVEL 1. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. (M)SDR USAA001020Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED 1 INCH, STATION 312, RBL 36. FABRICATED NEW T-CAP AND SPLICE ANGLE PER SRM 53-10-51. CORROSION LEVEL 1. (M)SDR USAA000891Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .5 INCH, BS 344 STRINGER 11R. FABRICATED CLIP PER BOEING DWG 6938939. (M)SDR USAA000892Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STRINGER 1 BS 380. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)SDR USAA000893Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, STATION 380, STRINGER 2L. INSTALLED NEW TIE CLIP PER SRM 51-40-02. (M)SDR USAA000894Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .0625 INCH, BS 616, STRINGER 4L. INSTALLED NEW TIE CLIP PER SRM 51-10-2. (M)SDR USAA000895Tie Clip · crackedCLT - FOUND TIE CILP CRACKED .0625 INCH, BS 639, STRINGER 4L. INSTALLED CLIP PER SRM 51-10-2. (M)SDR USAA000896Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, FORWARD SIDE FRAME 907, BELOW STRINGER 1. REPLACED TIE CLIP PER BOEING DWG 69-47869. (M)SDR USAA000897Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED TWO PLACES .5 INCH, FS 663, STRINGER 10L. INSTALLED CLIP PER SRM 51-10-2. (M)SDR USAASB00142Light · failedPHL - MAINTENANCE FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT ROW 12ABC INOPERABLE. MAINTENANCE REMOVED AND REPLACED THE SEAT MOUNTED EMERGENCY LIGHT ASSEMBLY AT SEAT ROW 12ABC. OPERATIONAL CHECK GOOD. (X)SDR USAASB99305Fire Loop · failedMCI - FLT 328 - AFTER TAKEOFF FROM MCI, THE RIGHT WING TO BODY OVERHEAT LIGHT ILLUMINATED. THREE MINUTES LATER, THE LEFT WING TO BODY OVERHEAT LIGHT ILLUMINATED AND A STRONG BURNING SMELL WAS PRESENT IN THE COCKPIT. FLIGHT RETURNED TO FIELD AT MCI AND LANDEDSDR USAASB99085Splice · defectiveROC - WHOLE ACCOMPLISHING OVERNIGHT CHECK, MAINTENANCE FOUND THE LOW LEVEL EMERGENCY LIGHT ON SEAT ROW 16 END BAY INOPERATIVE. MAINTENANCE REPLACED DEFECTIVE WIRE SPLICES AND SECURED WIRING BENEATH SEAT ADJACENT TO END BAY. OPERATIONAL CHECK GOOD. (M)SDR USAA980600Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC FOUND A .125 INCH CRACK UPPER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 6 AND EA 63034. (M)SDR USAA980599Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD SERVICE DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M)SDR USAA980598Skin · crackedTPA - DURING CX-1 CHECK VISUAL INSPECTION VERIFIED WITH HFEC, FOUND A .375 INCH CRACK LOWER HINGE CUTOUT ON FORWARD ENTRY DOOR SKIN. FABRICATED DOUBLER AND INSTALLED PER SB 737-52-1096 FIG 3 AND EA 63034. (M)SDR USAASB98233Transmitter · inoperativeCLT - FLT 1080 - AT FL370, THE 'B' SYSTEM HYDRAULIC PRESSURE GAUGE WENT OT 750 PSI. SHORTLY THEREAFTER, THE 'B' SYSTEM HYDRAULIC QUANTITY RESERVOIR STARTED TO DECREASE. CREW DECIDED TO DIVERT TO CLT DUE TO POSSIBLE HYDRAULIC FLUID LOSS. FLIGHT LANDED WITHOUT
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