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 QXEA0100413Rib · chafedPDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED AT XN137.35 AND ZN17.0. REPAIRED IAW HORIZON AIR EA 9-54-288 AND DHC-8 SRM 51-20-11.SDR QXEA0100412Rib · chafedPDX-RIGHT NACELLE OUTBOARD STIFFENER/RIB CHAFED IN TWO AREAS XN141.95 AND ZN18.0. REPAIRED IAW HORIZON AIR EA 9-54-287 AND DHC-8 SRM 53-00-16, PAGE 4.SDR C2XA01A015Frame · crackedSHV - DURING MAINTENANCE INSPECTIN, THE LEFT NACELLE HALF FRAME FOR THE LEFT MAIN LANDING GEAR AFT OUTBOARD DOOR FORWARD HINGE POINT WAS FOUND TO BE CRACKED. THE AIRCRAFT WAS FERRIED TO IAH WHERE IT LANDED WITHOUT INCIDENT, AND MAINTNANCE PERFORMED A DOUBLER SDR C2XA01IA029Frame · crackedIAH - DURING MAINTENANCE INSPECTION, THE LEFT NACELLE HALF FRAME FOR THE AFT OUTBOARD GEAR DOOR HINGE POINT WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR 20001026SH029Frame · crackedDURING C-CHECK INSPECTION, THE NR 2 ENGINE NR 1 FRAME WAS FOUND CRACKED IN THE UPPER INBOARD TORQUE TUBE MOUNT WEB. POSSIBLE CAUSE: FATIGUE FROM ENGINE TORQUE. (X)SDR ABXA000402Frame · crackedNR 1 PYLON LEADING EDGE INBOARD FORMER CRACKED AT LOWER AFT END. REPLACED FORMER IAW DC9 SRM 51-30-2.SDR 20000828SH028Frame · crackedDURING C-CHECK INSPECTION, THE NR 1 ENGINE FRAME WAS FOUND CRACKED IN THE UPPER INBOARD TORQUE TUBE MOUNT WEB. POSSIBLE CAUSE, FATIGUE FROM ENGINE TORQUE. (X)SDR 20000810SH017Frame · crackedDURING ROUTINE MAINTENANCE C-CHECK, A CRACK WAS FOUND ON BOTH ENGINE NACELLE FRAMES NR 1. THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING HOLE AND THE OUTBOARD EDGE OF THE FRAME. SUBMITTER RECOMMENDED REPLACINGSDR MALA000385Frame · corrodedFOUND DURING C-CHECK, FRAME AT 258.0 HAS CORROSION. MAINTENANCE REMOVED MATERIALS, FABRICATED FWD STIFFENER TP SAMLE FROM 2024T3.040, FABRICATED REPAIR DOUBLER PER REF 51-20-41, 42, AND 43. INSTALLED STIFFENER AND REPAIR ANGLE AS PER SRM 51-40-21.SDR ASOA00064Frame · crackedDURING INSPECTION, FOUND NR 1 NACELLE FRAME CRACKED. MAINTENANCE REPAIRED CRACK IAW EMB 120-54-0027B. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR 20000516SH028Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED A CRACK IN THE RIGHT NACELLE FORWARD FRAME NR 1. POSSIBLE CAUSE IS STILL UNDETERMINED. SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. SB 120-54-0036 IS BEING INCORPORATED. (X)SDR 20000516SH027Frame · crackedFLUORESCENT PENETRANT INSPECTION INDICATED A CRACK IN THE LEFT NACELLE FORWARD FRAME NR 1. POSSIBLE CAUSE IS STILL UNDETERMINED. SUSPECT ENGINE TORQUE AND VIBRATION TO BE POSSIBLE CONTRIBUTING FACTORS. SB 120-54-0036 IS BEING INCORPORATED. (X)SDR EIAA2000119Rib · crackedHAECO-HKG - C6/D-CHECK/PLY MOD - NR 4 PYLON LEFT SIDE FRAME AT NAC STA 235, APPROX 12.0 INCHES ABOVE LOWER FIREWALL, HAD 2 CRACKS APPROX 1.0 INCH IN LENGTH. NR 4 PYLON AT NAC STA 235 LT SIDE FRAME REPLACED PER SRM 51-10-01. (X)SDR AU000350Frame · cracked(AUS) LT ENGINE PYLON TOP WEB CRACKED AT THE FORWARD INBOARD CORNER OFTHE POWER FEEDER CABLE CUTOUT. CRACK LENGTH 9.525MM (0.375IN).SDR 2000UALA00122Spar · burnedAPPROX .375 INCH DIAM ARCING BURN-THROUGH DAMAGE TO NR 2 PYLON FWD MID SPAR WEB AT CORNER OF LIGHTENING HOLE. DAMAGE WAS DUE TO ARCING BURN-THROUGH OF WORN GENERATOR FEED CABLE TO NR 2 PYLON FWD MID SPAR WEB (P/N: 311U4156-1). A WEB DOUBLER REPAIR ADAPTED FRSDR C2XAOOIA045Frame · crackedDURING CONTINENTAL EXPRESS AIRLINES C-CHECK, FOUND LT NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW EC5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE (M)SDR 0000576740Frame · crackedDURING M-CHECK, FOUND CRACK ON WEBS OF BOTH FORWARD AND AFT FRAMES, LEFT HAND SIDE IN NR 2 PYLON ENGINE MOUNT LOWER BULKHEAD ASSY AT NACELLE STATION 221. REPAIRED PER EA67-173186.SDR EISA2000026Frame · crackedDURING ACCOMPLISHMENT OF A NON-ROUTINE WORK CARD, FOUND NR 3 ENGINE PYLON UPPER FORWARD MOUNT AFT T-CAP CRACKED FROM FASTENER HOLE. REMOVED AND REPLACED T-CAP ANGLE ON NR 3 PYLON PER SRM 51-10-1 AND 51-30-2. (M)SDR ASOA99171Frame · crackedDURING INSPECTION, FOUND BOTH LT AND RT NR 1 FRAMES CRACKED. MAINTENANCE C/W EO 120-54-0034, WHICH OUTLINED FRAME REPLACEMENT PROCEDURES. AIRCRAFT IS CURRENTLY IN C-CHECK. (X)SDR AT9900917Rib · crackedRIGHT ENGINE PYLON LEADING EDGE HAS CRACKED RIB ANGLE. STOP DRILLED CRACK IAW DC9 SRM 57-01.SDR ASOA99160Frame · crackedUPON INSPECTION, FOUND LT NACELLE UPPER FRAME NR 1 CRACKED. MAINTENANCE COMPLIED WITH EO 120-54-0034. OPERATIONAL CHECKS WERE GOOD. AIRCRAFT RETURNED TO SERVICE. (X)SDR AWXA9900421Fastener · shearedDURING ENGINE CHANGE SEVERAL FASTENERS ON THE PYLON ATTACH FITTING, WHERE THE DIAGONAL WING BRACE ATTACHES WERE LOOSE AND 2 WERE SHEARED. ACTION IS CURRENTLY BEING EVALUATED FOR DISPOSITION AND REPAIR.SDR C2XA99IA574Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT AND RIGHT NACELLE NR 1 FRAMES CRACKED. REMOVED AND REPLACED LEFT AND RIGHT ENGINE NACELLE NR 1 FRAMES IAW SRM 51-25-00 AND 54-10-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR 99ZZZM790Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT AND RIGHT NACELLE NR 1 FRAMES CRACKED. REMOVED AND REPLACED LEFT AND RIGHT ENGINE NACELLE NR 1 FRAMES IAW SRM 51-25-00 AND 54-10-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR 99UAL900556Rib · crackedDURING INSPECTION OF THE OUTBOARD STRUTS RIBS (OUTBOARD AND INBOARD) AT NAC STA 236.5, THE OUTBOARD RIB ON STRUT NR 4 WAS FOUND CRACKED UNDERNEATH THE 65B90150-3 BRACKET. THE APPROXIMATE LENGTH OF THE CRACK IS 6 INCHES. ALSO, THE BRACKET WAS FOUND CRACKED. SDR C2XA99IA554Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT ENGINE NACELLE NR 1 FRAME CRACKED. REMOVED AND REPLACED NR 1 FRAME IAW SB 120-54-0036 AND EC5410-01034. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR UF6A991012Former · damagedSBN - THE RIGHT MODULAR 7 HAS A CRACKED THIRD INBOARD FORMER. MAINTENANCE REPAIRED FORMER. ALL WORK WAS DONE IAW BAE ATP SRM 51-60-01 FIGURE 1. (M)SDR UF6A991011Frame · damagedSBN - THE NR 1 MODULAR 6 IS CRACKED AT THE AFT FRAME ASSEMBLY. MAINTENANCE STOP DRILLED AND INSTALLED REPAIR. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01 AND ENGINEERING REPORT NR 99-051. (M)SDR GAIA99149Frame · misdrilledMDT - DURING ROUTINE MAINTENANCE, IT WAS DISCOVERED THAT AT STATION 1342.4 RIGHT SIDE HAD LOOSE FASTENERS BETWEEN WL 260 ADN WL 195. REMOVED AND REPLACED SKIN PANEL IAW BOEING SRM ANS S/B 727-53-155. INSTALLED AN INTERNAL REPAIR STRAP IAW FVI DRAWING NUMBER SDR UF6A991006Frame · crackedSBN - THE NR 2 MODULAR 6 IS CRACKED AT THE 7 O'CLOCK POSITION. MAINTENANCE STOP DRILLED AND INSTALLED REPAIR. ALL WORK WAS DONE IAW BAE ATP SRM 51-10-01 AND ENGINEERING REPORT NR 99-051. (M)SDR C2XA99IA545Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND RIGHT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR UF6A990946Frame · crackedSBN - THE RIGHT MODULAR 6 EXHAUST SHROUD HAS 2 CRACKS. MAINTENANCE STOP DRILLED CRACKS AND INSTALLED PATCH. ALL WORK WAS DONE IAW UFS SRM SUPPLEMENT 99-03 AND ENGINEERING ORDER 99-051. (M)SDR UF6A990941Frame · crackedSBN - THE UPPER AFT FRAME ON THE MODULAR 5 IS CRACKED. MAINTENANCE REPAIRED UPPER AFT FRAME. ALL WORK WAS DONE IAW BAE ATP SRM 54-10-00. (M)SDR MALA976574Frame · crackedDURING HEAVY CHECK, SOME RIVETS ATTACHING TO LOWER FRAME THROUGH THE EXTERNAL SKIN, NEAR NAC WL 94, HAVE POOR PITCH & EDGE DISTANCE. THERE IS A CRACK IN THE LOWER FRAME IN THIS AREA STARTING FROM A FASTENER HOLE GOING TO THE EDGE OF THE FRAME. MAINTENANCE RESDR UIEA99064Frame · crackedNR 3 PYLON INTERIOR AFT MOUNT BULKHEAD WEB AFT SIDE AT NAC STATION 286 FOUND WITH CRACK. DAMAGED AREA WAS TRIMMED OUT, NDT INSPECTED, REPAIRED IAW BOEING TELEXS. (M)SDR C2XA99IA456Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND RT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINENTAL EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA455Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND LEFT NACELLE FRAME NR 1 CRACKED. REMOVED AND REPLACED FRAME NR 1 IAW CONTINENTAL EXPRESS EC5410-01033. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR QXEA9901591Frame · corrodedPDX - NACELLE FRAME UNDER MAIN LANDING GEAR RETRACTION ACTUATOR FITTING HAS FRETTING CORROSION. REPAIRED IAW HORIZON AIR EA 9-54-203.SDR AU990749Frame · cracked(AUS) ENGINE MOUNT FRAME CRACKED IN THE AREA AT THE TOP OF THE CLUSTER GUSSET ON THE LEFT SIDE. CRACK LENGTH 13 MM (0.51 INCH). FOUND DURING INSPECTION IAW AD/CESSNA180/4 (ITEM IS NOT PART OF THIS INSPECTION).SDR 99T64R241ARFrame · crackedNR 0762 - 6 INCH CRACK IN NR 3 PYLON CAP FORMER (HORSE COLLAR) FORWARD SECTION STA YN161. FABRICATED REPLACMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR - ARWA. (X)SDR UPS99429694Frame · crackedINSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED, FWD END OF DIAG BRACE FWD ATTACH FITTING, O TB SIDE, APPROX PYLON STA 292. THE CRACK IS APPROX 1.5 INCH LONG, FROM BOTTOM END OF FRAME.SDR UPS99429693Frame · crackedINSPECTION TYPE:N/A, NR 3 PYLON FRAME CRACKED FWD END OF DIAG BRACE FWD ATTACH FITTING, I/B SIDE APPROX PYLON STA 292, APPROX 2 INCH LONG, FROM BOTTOM END OF FRAME. *S/D* REMOVED DAMAGED RIB (P/N 65B90411-604) AND REPLACED WITH RIB (P/N 65B90411-604) AND BONSDR 99T64R371ARFrame · crackedFOUND 5 INCH CRACK IN NR 1 PYLON CAP NUT PLATE FORMER (HORSE COLLAR) YN 161. FABRICATED AND INSTALLED NEW FORMER IAW EO99-061. (M)SDR EIA990263Rib · crackedMZJ - DURING C-CHECK, A 6 INCH CRACK WAS FOUND ON THE RIGHT TRAILING EDGE PYLON 2ND RIB INBOARD. REPAIRED BY TRIMMING RIB AND INSTALLING NEW SPLICE AND REPAIR DOUBLERS PER ECRA 942-55-020-2. (M)SDR 99T64R236ARFrame · crackedNR 0164 - 5 INCH CRACK IN PYLON CAP FORMER 2ND SECTION NR 1 PYLON STA YN 190. FABRICATED REPLACEMENT PART PER EO 99-061 WITH APPROVED FAA FORM 8110-3 DATED 6-14-99. INSTALLED IAW DC-8 SRM 51-1-21. REF: ARROW AIR, ARWA. (X)SDR ASOA99042Frame · crackedDURING C-CHECK INSPECTION, FOUND LEFT AND RIGHT ENGINE NACELLE FRAME NR 1 TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME IN LEFT AND RIGHT ENGINE NACELLES. (M)SDR ASOA99036Frame · crackedDURNG C-CHECK INSPECTION, NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES WERE FOUND TO HAVE CRACKS. REMOVED AND REPLACED NR 1 FRAME ON LEFT AND RIGHT ENGINE NACELLES. (M)SDR 99ZZZX1967Frame · crackedDURING ROUTINE MAINTENANCE CHECKS, CRACKS WERE FOUND ON BOTH ENGINE NACELLE NR 1 FRAMES. ON THE LT FRAME, THE CRACK IS LOCATED ON THE LOWER SIDE OF THE STIFFENING WEB BETWEEN THE TOP OUTBOARD MOUNTING BOLT HOLE AND THE OUTBOARD EDGE OF THE FRAME. ON THE RT FSDR C2XA99IA235Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT REAR NACELLE FRAME CRACKED ABOVE REAR SPAR. FABRICATED AND INSTALLED REPAIR DOBLERS IAW SRM 51-70-05 AND 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR C2XA99IA161Frame · crackedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE FRAME CRACKED AT OUTBOARD COWL STAY FITTING. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER REPAIR IAW SRM 51-70-05 AND SRM 51-40-02. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)
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