JASC 5411
Service difficulty reports · 1,454
Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411' 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 = '5411' 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 DL76L100672Spar · misrepairedNR 1 PYLON MID SPAR WEB EXISTING REPAIR FASTENER PATTERN AND TRIM DEPTH FOUND DEVIATED WITH SB 767-54-0080. REPAIRED IAW ERA 479964-14AD, REV-0.SDR DL76L100671Spar · crackedNR 1 PYLON MID SPAR WEB CRACKED AT INBD MIDSPAR FITTING OTBD ROW MOST AFT FASTENER HOLE RUNNING FWD APPROX .1875" IN LENGTH REPAIRED IAW ERA 479969-14AD REV. 0.SDR DL76L100629Spar · damagedO/B MID SPAR CHORD NR 2 FASTENER HOLE (COUNT FROM AFT TO FWD) PREVIOUSLY OVERSIZED DIA 0.529 INCH HOLE. REPAIRED PER ERA479968-14AD REV 0.SDR DL76L100677Spar · crackedNR 1 PYLON UPPER SPAR WEB CRACKED AT FUEL SHROUD CUTOUT AREA AT NAC STA 174 APPROX. REPAIRED IAW ERA 479025-14, REV 0.SDR 2010FA0000361Frame · cracked(KADY) CRACK AT AFT FLANGE OF UPPER FRAME OF NR 1 ENGINE. MAJOR REPAIR ACCOMPLISHED BY TRIM OUT OF DAMAGED FRAME AND INSTALL REPAIR PARTS.SDR DL76L100288Spar · crackedNR 2 PYLON FWD UPPER SPAR WEB FUEL TUBE CUTOUT FOUND CRACKED. REPAIRED IAW ERA 473380-14.SDR SWIA201023875Spar Cap · crackedRIGHT NACELLE FORWARD SPAR CAP UPPER CORNER CRACKED. (C CHECK) INSTALLED DOUBLER REPAIR PER ETD.SDR SWIA201023874Frame · crackedLEFT NACELLE FRAME NR 1 CRACKED. (C CHECK) REPLACED FRAME PER EMB SB 120-54-0036.SDR Q2S2010F00018Frame · crackedNR 4 PYLON UPPER TORQUE BOX NAC STA 270 BLKHD INBD FRAME UPPER SECTION FOUND CRACKED.SDR Q2S2010F00016Frame · crackedNR 1 PYLON FRONT SPAR OTBD FRAME UPPER END FOUND CRCKED.SDR SWIA201023565Frame · crackedLEFT ENGINE FRAME 1 CRACKED AT INBOARD CORNER. (C CHECK) REPLACED FRAME PER SB120-54-0036.SDR SWIA201023556Frame · crackedRIGHT ENGINE FRAME 1 CRACKED. (C CHECK) REPLACED FRAME PER SRM.SDR HNAA2010012200014Longeron · crackedINBD UPPER LONGERON IS CRACKED AT THE FWD END. CRACK IS 1.3 INCH LONG AND IS IN THE INBD RADIUS. IT TRAVELS FROM THE FWD END, BELOW THE FIRST RIVET AND TO THE SECOND RIVET. INSTALLED RIVETS THRU VERTICAL LEG OF REPAIR ANGLE. REPAIRED IAW EO8-54 10-0007.SDR IXXA10WSAP021SFrame · crackedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD EDGE INBD ATTACH SUPPORT FRAME CRACKED. REMOVED FASTENER’S AS NEEDED TO PERFORM REPAIR. REMOVED CRACKED FRAME. INSTALLED EXISTING FASTENER’S AND NEW FRAME IAW AMM 20-11-00 REV97, SRM 51-40-02 SDR USAA2009122493418Rib · crackedSAL - BC7 - MAJOR REPAIR - CRACK ON RIB 12 OF AFT FIXED FAIRING OF RIGHT PYLON ENGINE NR 2. REPLACED RIB 12 OF AFT FIXED FAIRING OF RIGHT PYLON ENGINE NR 2 IAW A320 SRM 51-72-11 & AIRBUS DRAWING D54510054.SDR SWIA200923205Frame · crackedRIGHT NACELLE INBOARD FRAME 10 CRACKED. (C CHECK)REPAIRED PER SRM.SDR QXEA2009112300989Rib · chafedC CHECK - NACELLE PANEL 414AL HAS A CHAFED INTERNAL RIB UPPER AFT END OF PANEL. REMOVED DAMAGED RIB FROM PANEL, MATCH DRILLED NEW RIB TO PANEL AND INSTALLED NEW RIB IAW SRM 51-42-05.SDR QXEA2009112300987Rib · chafedC-CHECK - NACELLE PANEL 414AR HAS A CHAFED INTERNAL RIB UPPER AFT END OF PANEL. REMOVED DAMAGED RIB FROM PANEL, MATCH DRILLED AND INSTALLED NEW RIB IAW SRM 51-42-05.SDR QXEA2009112300988Rib · crackedC-CHECK - NACELLE PANEL 414AR HAS A CRACKED INTERNAL RIB, LOWER AFT END OF PANEL. REMOVED DAMAGED RIB FROM PANEL, AND INSTALLED NEW RIB FROM STOCK IAW SRM 51-42-05.SDR DL757100341Frame · damagedNR 2 ENG PYLON LT SKIN LWR FRAME FOUND TO EA OVERSIZED HOLES AT APPOX STA 125 AND STA 143. ACCOMPLISHED ERA 478203-14 AT SAA SAT REF NON ROUTINE CARD 139798.SDR DL757100188Rib · damagedNR2 PYLON RT SKIN OTBD SUBSTRUCTURE RIB FOUND 3EA INCOMING HOLES O/S AT STA 116.05/ ACCOMPLISHED ERA478028-14 REV ORG AT SAA SAT ON NON ROUTINE CARD 136559.SDR SWIA200923166Rib · crackedRIB CRACKED AT RIGHT INBOARD AND OUTBOARD UPPER NACELLE. (C-CHECK) REPLACED RIBS PER SRM.SDR SWIA200923161Fitting · crackedRIGHT NACELLE WHEEL WELL INBOARD AREA VERTICAL FRAME FITTING CRACKED. (C-CHECK) REPLACED FITTING PER SRM.SDR IPXA09657866Frame · crackedINSPECTION TYPE:C NR 1 PYLON INTERNAL FRAME CRACKED AT NAC STA 285.45 RT SIDE, (CRACK LENGTH 2 INCHES) NR 1 PYLON INTERNAL FRAME REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45 JUST AT NAC STA 285.45 RT SIDE.SDR SWIA200923162Frame · crackedLEFT NACELLE FRAME 1 INBOARD SIDE CRACKED. (C-CHECK) REPLACED LEFT NACELLE FRAME PER SRM.SDR KCSA091120Stiffener · crackedNR 2 PYLON STIFFENER CRACKED .5 INCH AT STA 221 LOWER WEB.SDR KCSA091119Stiffener · damagedPYLON NR 1 STIFFENER DAMAGED AT LOWER SPAR WEB STA 221.SDR SWIA200922729Frame · crackedRIGHT NACELLE FRAMES CRACKED. (C CHECK) REPLACED FRAMES PER SRM.SDR IPXA09B57453Frame · crackedINSPECTION TYPE:C NR 3 PYLON INTERIOR AREA STA 346.4 O/B SIDE VERTICAL CHORD FOUND CRACK. NR 3 PYLON INT AREA AT STA 346.4 O/B SIDE VERT FRAME CHORD REPAIRED AS PER HX RS R54-00-36429 REV A. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR WITH MAT'L 2024T62 0.090"SDR KCSA091100Frame · crackedNR 3 PYLON AFT OUTBOARD FRAME IS CRACKED (1.5 INCHES) AT NAC STA 221.9.SDR CA090904007Structure · crackedTHE 27-35008-010 KEELSON CAP WAS DISCOVERED CRACKED ON LR RADIUS. THIS IS A FAIRLY COMMON DEFECT AND WHEN NACELE SKIN WAS REMOVED TO REPLACE IT, 27-35004-002 CAP WAS FOUND CRACKED AS WELL. THIS PART CAN BE INSPECTED IN SERVICE BUT WOULD BE DIFFICULT TO SEE,SDR IPXA09657334Attach Fitting · crackedINSPECTION TYPE:C NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 FOUND CRACK. CRACK LENGTH 0.5 INCH. NR 1 PYLON MID SPAR ATTACH CLIP AT RT NAC STA 285.45 REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 REV 45.SDR KCSA091097Frame · crackedNR 4 PYLON FRAME CRACKED 5 INCHES AT NAC STA-236.5 NAC WL - 154.SDR Q2S2010F00002Frame · crackedPYLON NR 4 INTERIOR AT NAC STA 270 BULKHEAD FWD SIDE , FOUND OTBD FRAME CRACKED. REPAIR CARRIED OUT IAW EN NR 1363-09.SDR Q2S2010F00001Frame · crackedPYLON NR 4 INTERIOR AT NAC STATION 270 BULKHEAD FWD SIDE FOUND INBD FRAME CRACKED. REPAIR CARRIED OUT IAW EN NR:1363-09.SDR TAMF20090030SFrame · crackedDURING (SC3) CHECKS, INSP WAS FOUND A CRACK ON ENGINE NR 1 CORE COWL SKIN AFT FRAME STA 293.709 NR/00051. REPAIRED ACCOMPLISHED IAW EWO 767-54-059.SDR KCSA091081Frame · crackedNR 2 PYLON AFT ENGINE MOUNT FRAMES CRACKED APPROX 19 INCHES BELOW MID SPAR AT NAC STA 221.9.SDR KCSA091078Frame · crackedNR 1 PYLON I/B FRAME CRACKED AT NAC STA 210, 6 INCHES BELOW MID SPAR.SDR UALA2009080602376Spar · crackedNR 1 ENGINE PYLON, FWD UPPER SPAR CRACKED AT WIRE BUNDLE PASS THROUGH HOLE, NAC STA 181. MAJOR REPAIR ACCOMPLISHED. STOPPED DRILLED CRACK AND INSTALLED DOUBLER REPAIR. CAP SEALED TOP SIDE OF PYLON.SDR IPXA09557038Angle · crackedINSPECTION TYPE:C1 NR 1 ENG AFT STRUT I/B STA 240 FRAME LOWER ANGLE IS CRACKED. REMOVED AND REPLACED ANGLE PER SRM 51-40-02.SDR QXEA2009071000517Frame · chafedPDX - C5 - LT NACELLE FRAME AT APPROX STA XN 183.974 AND ZN 55.000 IS CHAFED BEHIND NR 1 HYD SUCTION LINE. REMOVED 1 SOLID RIVET IAW Q400 SRM 51-42-05 TO ALLOW FOR BLENDING. BLENDED LT NACELLE FRAME TO REMOVE CHAFE DAMAGE AS REQUIRED. HFEC INSPECTED BLENDEDSDR FDEA200907082527Spar · wornFOUND ELONGATED HOLE IN SPAR FOR DRAIN PIPE ON PYLON NR 1. REPAIR PERFORMED BY REAM UP THE HOLE AND REPAIR IAW DWG R546-10359, APPROVED BY RAS 70520790/004/2009 ISS A AND EA 6-5410-131237.SDR NWAA092416310Spar · damagedDURING IDG REPAIR FOUND THE MIDSPAR WEB DAMAGED AT NAC STA 174 AND NAC BL 7. REPAIRED PER EA 63-215321.SDR SWIA200922680Frame · crackedLEFT NACELLE O/B FWD COWL DOOR, FWD LWR NACELLE FRAME CRACKED. (C-CHECK) DRILLED OUT CRACKED FRAME ON LT NACELLE FWD LWR CORNER WHERE FWD COWL O/B DOOR LATCHES, INSTALLED SERVICEABLE FRAME PIECE.SDR SWIA200922184Frame · crackedLEFT NACELLE FRAME 8 CRACKED. (C CHECK) REPLACED PER SRM.SDR A6WA200940379Rib · crackedON LT PYLON, FIRE SHIELD RIB FOUND CRACKED ON FS 654.00 ON LT PYLON, NEW FIRE SHIELD RIB INSTALLED IAW SRM 51-42-06. (K)SDR USAA2009070891760Rib · crackedSAL - C7 - MAJOR REPAIR - CRACK ON RIGHT PYLON AFT FIXED FAIRING ON RIB 14 AT INTERNAL AREA LOWER SIDE. REPLACED RIGHT PYLON AFT FIXED FAIRING RIB 14 IAW A320 SRM 51-72-11.SDR FDEA200906152102Spar · corrodedFOUND CORROSION ON UPPER SPAR UNDER PYLON SPIGOT FITTING, RIB 12 REPAIR PERFORMED BY BLEND OUT THE CORROSION , NDT FOR CRACK FREE CONDITION IAW RAS 70519120/011/2009 ISS. A, APPROVED BY EA 6-5440-120195.SDR FDEA200905281834Spar · corrodedFOUND CORROSION IN NR 1 PYLON UPPER SPAR WEB UNDER FITTING A546-11024-204. REPAIR PERFORMED BY SMOOTH BLEND OUT AND NDT FOR CORROSION REMOVAL AND CRACK FREE CONDITION IAW RAS 70519602/018/2009 ISS. C, APPROVED BY EA 6-5410-129195.SDR KCSA091045Frame · crackedNR 3 PYLON INTERIOR HAS A 2 INCH CRACK ON 252 BULKHEAD FRAME LOWER O/B SECTION 2 INCHES ABOVE LOWER HORIZONTAL WEB.
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