JASC 5414
Service difficulty reports · 4,361
Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 jasc_code = '5414' 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 jasc_code = '5414' 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 04FDEA01919Skin · crackedNR 3 ENG PYLON CRACK RIGHT SIDE STA YN 320 ABOVE CORE COWL. TRIMMED OUT CRACK IAW DC10 SRM 54-00-01VOL 2, FABBED DOUBLER & FILLER IAW DC10 SRM 54-00-01 VOL 1, INSTALLED REPAIR IAW DC10 SRM 54-00-01 VOL 1.SDR 151AW0021Skin · crackedRIGHT PYLON UPPER SKIN AT NAC STA 213 LBL 10 CRACKED AT PANEL CUTOUT. REPAIRED PER SB 737-54-1035.SDR 04FDEA01880Doubler · gougedNR 3 ENG PYLON AFT UPPER FAIRING ANGLES LT AND RT GOUGED AND CHAFED AT AFT FASTENER HOLES. REMOVED AND REPLACED WORN ANGLES LT AND RT IAW SRM 51-35-01 AT MAE.SDR IXXA060148SAccess Panel · wornDURING ROUTINE C CHECK, FOUND NUMBER 3 PYLON FOOTSTOOL ACCESS PANEL HAS SEVERAL AREAS WITH DEEP FRETTING WEAR. FABRICATED NEW FOOTSTOOL ACCESS PANEL, LOCATED, DRILLED, TRIMMED, DEBURRED, TREATED, AND PRIMED NEW FOOTSTOOL ACCESS PANEL IAW DC8 SRM 53-2-0, 51-1-SDR IXXA060152SPanel · crackedDURING ROUTINE C-CHECK, FOUND NUMBER 1 ENGINE PYLON AFT OUTBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILLED, TRIMMED, DEBURRSDR 04FDEA01695Panel · damagedCOMPLY WITH EA 8-5410-78219, PYLON HORIZONTAL ENGINE PYLON LT ACCESS PANEL REPAIR. COMPLIED WITH EA 8-5410-78219.SDR IXXA060151SSkin · crackedDURING ROUTINE C CHECK, FOUND NUMBER 1 ENGINE PYLON AFT INBOARD SIDE ADAPTER PANEL CRACKED AT FORWARD UPPER PYLON SPAR ATTACH POINT APPROXIMATELY 1/2 INCH. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. FABRICATED DOUBLERS, LOCATED, DRILLED, TRIMMED, DEBURRESDR UIEA200400105Skin · crackedD-CHECK, DAMAGE WAS FOUND ON RT SIDE OF NR 1 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TRIMMED EDGE, SDR UIEA200400107Skin · cracked(D) CHECK, DURING MAINT INSP DAMAGE WAS FOUND ON RT SIDE OF NR 2 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER SKIN DOUBLER WAS TRIMMED, AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOSDR UIEA200400109Skin · crackedD-CHECK, DURING MAINT INSP, DAMAGE WAS FOUND ON RT SIDE OF NR 4 PYLON STRUCTURE ASSY. CRACK DAMAGE WAS AT PRECOOLER EXHAUST CUTOUT LOWER AFT CORNER AT NAC STA 248. INNER DOUBLER WAS TRIMMED AT GRILL ATTACHED HOLE TO REMOVE CRACK DAMAGE. INNER SKIN DOUBLER TSDR 04FDEA01470Panel · wornPNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01.SDR 04FDEA01469Panel · wornPNL 437LL SEAL IS WORN AND SEAL RETAINER IS CRACKED. FABBED NEW PANEL 437LL IAW DRAWING AUB7108, FABBED NEW SEAL RETAINER ON MAE TRAVLER T4/432661. INSTALLED SEAL AND SEAL RETAINER IAW SRM 57-31-01.SDR UIEA200400097Skin · wrinkledD CHECK AT SIN. DURING MAINTENANCE INSPECTION, FOUND NR 2 PYLON RT SIDE SKIN WRINKLED. DAMAGE WAS FOUND IN FOUR BAYS OF THE RT SUBJECT SKIN ASSEMBLY AFT OF NAC STA 286. THE DAMAGES ARE JUS AFT OF THE STRUT LARGE TITANIUM DOUBLER. SUBJECT SKIN ASSEMBLY WASSDR F3LA200400064Panel · damagedDURING C-6 CHECK, INSPECTION REPORTED SCREW BROKEN ON NR 1 PYLON TOP AFT FAIRING PANEL ATTACHED TO THE WING AND A CRACK FROM THE HOLE. REPLACED PANEL PER SRM 51-40-02, SRM 51-40-08 AND MM 28-11-00. PERFORMED LEAK CHECK. NO LEAKS NOTED.SDR USA2004F00049Panel · loose(2) SECONDS PRIOR TO TOUCHDOWN, A PASSENGER REPORTED THAT TWO PANELS DEPARTED THE NR 1 ENGINE PYLON. ONE PANEL WAS REPORTED THO HAVE STRUCK THE LT HORIZONTAL STABILIZER LEADING EDGE. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED NR 1 ENGINE PSDR UPS04442386Doubler · crackedINSPECTION TYPE: C, NR 3 PYLON LOWER WEB EXTERNAL O/B FWD OF REAR ENG BHD FITTING SKIN CRACKED AS RED MARKED (NAC 212-214 WBL R470). THE CRACK STOP DRILLED PER SRM 54-14-03 FIG 2 & REPAIR DOUBLER INSTALLED PER SRM 54-14-03 FIG 2, NDT CONFIRMED NO CRACK.SDR UIA9314Skin · crackedDURING TX CHECK FOUND LT NACELLE IB SKIN WAS CRACKED. REPAIR IAW RD-8-54-1900 RD-8-57-2830 RD-8-57-2832 TO BE DONE BY THE MFG OEM REPAIR TEAM.SDR SIMA200412101Skin · chafedABI - DURING AN MBV INSPECTION, THE LEFT NACELLES INBOARD SKIN AT THE WING TO NACELLE FAIRING WAS FOUND TO BE CHAFED. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION, NO DEFECTS NOTED FABRICATED A DOUBLER AND TRIPLER. ALSO FABRICATED SHIMS. REPAIR DOSDR UIEA200400050Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 4 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSEMBLY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITIOSDR UIEA200400049Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 3 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. SDR UIEA200400048Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 2 PYLON PRECOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. SDR UIEA200400047Skin · crackedD CHECK, DURING SCHEDULE MAINTENANCE. CRACKS WERE FOUND ON NR 1 PYLON PERCOOLER EXHAUST CUTOUT AFT LOWER CORNER. ON THE RT SIDE OF STRUT STRUCTURE ASSY, THE OUTER SKIN WAS TRIMMED. NDT INSPECTION WAS ACCOMPLISHED TO ENSURE CRACK AND DEFECT FREE CONDITION. SDR 2004F00272Panel · missingDURING POST FLIGHT WALKAROUND AT PIT FORND PRESSURE RELIEF VENT PANEL MISSING FROM NR 3 ENGINE. INSPECTED NR 3 ENGINE IAW 71-10-11. PERFORMED HIGH POEWR ENGINE RUN UP. BLEED PRESSURE EQUAL ON BOTH SIDES PER MM 75-31-0. RETURNED TO AIRCRAFT TO SERVICE. (M)SDR UIEA200400042Skin · dentedD CHECK, DURING A MAINTENANCE INSP, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 3 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSP, INCSDR UIEA200400041Skin · dentedDURING A MAINTENANCE INSPECTION, WRINKLED SKIN/ DENTS WERE FOUND ON THE EXTERIOR SKIN ASSEMBLY OF NR 2 PYLON JUST AFT OF THE TITANIUM DOUBLER, BETWEEN THE MID SPAR CHORD AND NR 5 STIFFENER. AFFECTED SKIN ASSEMBLY WAS TRIMMED TO REMOVE DAMAGE. NDT INSPECTION,SDR ASAA0410177Skin · chafedOKC - DURING MAINTENANCE, FOUND NR 1 ENGINE PYLON INBOARD SKIN CHAFED FORWARD OF PANEL 5143. REPAIR IAW EA. (M)SDR QXEA200400251Skin · damagedPDX - NACELLE SKIN DAMAGE AT LOWER COWL HINGE POINTS. REPAIRED IAW HORIZON AIR EA 6-54-288A.SDR QXEA200400250Panel · dentedPDX - DENT ON RIGHT HAND NACELLE PANEL 422CT, LEFT HAND SIDE 14.5 INCHES AFT OF PANEL 422AL AND 11.5 INCHES ABOVE PANEL 422BL. REPAIRED IAW HORIZON AIR EA 6-54-293.SDR CALA0400286Skin · gougedINSPECTION FOUND RIGHT ENGINE PLYON SKIN GOUGED UNDER PANEL 5829R, NAC STA 234.25 AND 246.63. REPAIRED IAW ECRA 5431-01022.SDR HNAA0400027Panel · corrodedNR 1 NACELLE REAR DECK UNDER FINGERNAIL HAS SURFACE CORROSION, R & R REAR DECKSDR 2004UALA00228Skin · crackedNR 2 PYLON ACCESS 446BR, UPPER FWD CORNER OF ACCESS CUTOUT IS CRACKED. MAJOR REPAIR ACCOMPLISHED. INSTALLED DOUBLER REPAIR.SDR SIMA200407905Skin · chafedABI - DURING AN MBV INSPECTION, THE RIGHT NACELLE INBOARD WALL INNER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION NO DEFECTS NOTED. FABRICATED FILLR AND DOUBLER. REPAIR DONE IAW SAAB 340 REPAIR STATEMENTSDR SIMA200407907Skin · chafedABI - DURING A MBV INSPECTION THE RIGHT INBOARD NACELLE OUTER SKIN PANEL WAS FOUND CHAFED BELOW SRM LIMITS AT THE FILLET FAIRING SEAL CONTRACT POINT. BLENDED THE CHAFED AREA AND PERFORMED NDT INSPECTION WITH NO DEFECTS NOTED. FABRICATED A REPAIR DOUBLER. RESDR AWXA200400281Panel · crackedMCN - MAJOR REPAIR - DURING C-20 CHECK A .75 INCH CRACK WAS FOUND ON LT PYLON PANEL 5727L ACCESS OPENING LANDING NAC STA 211. MAINTENANCE STOP DRILLED CRACK ON LT PYLON PANEL 5727L ACCESS OPENING LANDING AT NAC STA 21; PERFORMED A HFEC INSPECTION TO VERIFY CRSDR 0380Skin · crackedVISUALLY DETECTED CRACK IN PREVIOUS DOUBLER LEFT WING LEADING EDGE AT NR 2 ENGINE PYLON CUTOUT.SDR UIEA200400015Skin · wrinkledDURING D-CHECK AT SIN, FOUND NR 3 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSEMBLY WAS TRIMMED TO REMOVE THE WRINKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECITON OF SKIN TRIMMED EDGES AND REPAIR FASTENER HOLES WAS PERFORMED TSDR SWIA200413026Skin · crackedRIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP CRACKED AT RIVET. DISCOVERED DURING C-CHECK INSPECTION. REMOVED AND REPLACED RIGHT NACELLE FLAP UPPER SKIN TO RIB CLIP WITH A SERVICEABLE UNIT IAW SRM 51-10-02, 51-40-00.SDR UIEA200400014Skin · wrinkledDURING D-CHECK AT SIN, FOUND NR 2 PYLON HAS A WRINKLE CONDITION ON RIGHT SIDE. SKIN ASSY WAS TRIMMED TO REMOVED THE WRINKLED AREA. NDT INSPECTION OF THE REPAIR AREA, INCLUDING HFEC INSPECTION OF SKIN TRIMMED EDGES AND REPAIR FASTENERS HOLES WAS PERFORMED TO SDR CALA0400105Skin · crackedINSPECTION FOUND A 0.75 INCH CRACK IN NR 2 PYLON STRUT SKIN AT ACCESS DOOR 5824R CUTOUT, TOP FORWARD CORNER. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER AND FILLERS WERE INSTALLED IAW ECRA 5430-01204.SDR ASAA0480071Skin · debondedOKC - HV1 CHECK, FOUND LEFT ENGINE LOWER AFT COWL COMPOSITE MATERIAL IS SEPARATING AT FORWARD ATTACH HOOK. REBONDED COMPOSITE PER EA 7110-01220. (M)SDR ASAA0410046Panel · puncturedOKC - DURING SCHEDULED C-CHECK, FOUND THE NR 1 ENGINE PYLON PANEL NR 5140 PUNCTURED. REPAIRED PER EA. (M)SDR ASAA0440035Skin · wornGYR - NR 2 PYLON SKIN WORN OUTBOARD SIDE 22-30 INCH FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON SKIN OUTBOARD IAW ASA EA 5430-01128. (M)SDR ASAA0440026Skin · chafedGYR - NR 1 PYLON SKIN CHAFED OUTBOARD SIDE AT WING INTERFACE. REPAIRED NR 1 PYLON OUTBOARD SKIN IAW ASA EA 5430-01128. (M)SDR ASAA0440025Skin · wornGYR - NR 2 PYLON SKIN WORN INBOARD SIDE 22-30 INCHES FORWARD OF MIDSPAR FITTING. REPAIRED NR 2 PYLON INBOARD SKIN IAW ASA EA 5430-01128. (M)SDR ASAA0440034Skin · chafedGYR - FOUND LEFT ENGINE PYLON OUTBOARD SKIN CHAFFED AT WING INTERFACE. REPAIRED IAW EA 5430-01128. (M)SDR ASAA0440005Skin · wornGYR - DURING MAINTENANCE CHECK, NR 2 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257 RIGHT. REPAIR IAW EA. (M)SDR ASAA0440004Skin · chafedGYR - DURING MAINTENANCE CHECK, NR 1 ENGINE PYLON INBOARD AND OUTBOARD SIDE SKIN IS WORN FROM CONTACT WITH FIXED LEADING EDGE AT NACELLE STATION 257. REPAIR IAW EA. (M)SDR CALA0400034Skin · crackedINSPECTION FOUND A 1.25 INCH CRACK NR 2 PYLON PANEL NR 5842R. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.SDR COOSDR030052Skin · corrodedNR 2 ENGINE OB COWLING EXTERNAL SKIN CORRODED.SDR AWXA200400007Skin · erodedMCN - MINOR REPAIR - DURING C-02 CHECK THE NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN WAS FOUND ERODED. MAINTENANCE REMOVED ERODED NR 2 PYLON AFT FIXED FAIRING INBOARD SKIN; FABRICATED A NEW REPLACEMENT SKIN; INSTALLED REPAIR PART IAW A320 SRM 51-42-11, PG 8-1
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