JASC 5415
Service difficulty reports · 1,305
Reports filed under 5415 · Nacelle/Pylon, Attach Fittings, 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 = '5415' 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 = '5415' 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 A6WA2017010245532Attach Fitting · crackedNR 1 PYLON LE ACCESS ATTACH FLANGE IS CRACKED ON THE LOWER PYLON.SDR SIMA20171122004Fitting · crackedL/H PYLON LOWER FWD ENGINE YOKE FITTING CRACKED-C/A-REMOVED AND REPLACED L/H PYLON LOWER FWD ENGINE YOKE FITTING IAW EO EM-54MR-386.SDR DALA2017110808047Bushing · chafedNR 1 PYLON FWD UPPER LINK FITTING BUSHINGS FOUND CHAFED. NEW BUSHINGS INSTALLED IAW SRM 54-52-90.SDR SWAA2022011938284Fairing · cracked**FOR DELAY PURPOSES ONLY**#2 ENGINE LOWER AFT PYLON T/E WEDGE FAIRING IS CRACKED; #8 SLAT IS DELAMINATED; #7 SLAT HAS DENTS / FOR DELAY CODING ONLYREPLACED #2 ENG LOWER AFT T/E WEDGE FAIRING C/W EA FOR SLAT DENTS AND DELAMSDR HYIA20171017001Fitting · crackedWHILE CONDUCTING SID 57-10-16 INSPECTION, TWO CRACKS WERE DISCOVERED ON THE OUTBOARD SIDE OF THE INBOARD FITTING, JUST FORWARD OF THE SPAR STRAP. THE FITTING WAS REPLACED.SDR UIEA2017090801619Tee Fitting · brokenNR 2 ENGINE, LT CORE COWL MOST AFT HAT CHANNEL LOWER ATTACH TEE FOUND BROKEN. THE TEE FITTING WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 29.SDR EE4Y2017100504646Mount Fitting · corrodedDURING THE STRUCTURAL INSPECTION AT THE ENGINE NR 2 PYLON AREA, WAS FOUND THE NR 2 PYLON AFT ENGINE MOUNT FITTING WITH CORROSION. THE DAMAGED AREA WAS REPAIRED PER AIRBUS INSTRUCTIONS UNDER REF 80356610 AND EOD 32S-54-0180-R00 AND APPROVED UNDER RDAS 80356610/SDR QXEA2017091500566Bushing · migratedRIGHT NACELLE INBD FWD ATTACH FITTING AFT LUG BUSHING MIGRATED FWD. REMOVED THE BUSHING IAW RD84-54-1978. REAMED THE FITTING AND A FRAME IAW RD84-54-1978. NDT CARRIED OUT IAW NDTM 6, 51-00-08-250-801. PROTECTED THE BORE IAW RD84-54-1978. INSTALLED & SEALED SDR SIMA20170812002Support · crackedLT ENGINE PYLON FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD LOWER YOKE IAW EO EM-54MR-386.SDR IPXA2017071319248Bushing · corrodedINSPECTION TYPE: SEG2, NR 2 PYLON TWO UPPER LINK BUSHINGS AT THE FWD END CORRODED. REMOVED AND REPLACED.SDR HYIA20170705002Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, A CRACK WAS IDENTIFIED IN THE RT INBOARD NACELLE FITTING.SDR HYIA20170705001Fitting · crackedWHILE PREPPING THE LOWER NACELLE SKIN FOR SID 57-10-16 NDT INSPECTION, TWO CRACKS WERE IDENTIFIED IN THE LT OUTBOARD NACELLE FITTING.SDR RAIA201706140001Yoke · crackedRIGHT PYLON FWD YOKE CRACKED. REMOVED AND REPLACED THE RT PYLON FWD YOKE.SDR HYIA20170828016Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .123 IN LENGTH.SDR HYIA20170828011Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED ON THE LT OUTBOARD FITTING. THE CRACK AS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .102 IN LENGTH.SDR IPXA2017053117737Truss Fitting · gougedINSPECTION TYPE: 1C, RT WING NR 3 PYLON ENGINE MOUNT, LT TRUSS FITTING HAS TWO GOUGES. REPAIRED THE TRUSS FITTING IAW EA 011-5410-01-A6811 REV I/R, AND EO MD11-7120-64408-A.SDR HYIA20170828010Fitting · crackedDURING A SID 57-10-16 INSPECTION, A CRACK WAS DISCOVERED IN THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .145 IN LENGTH.SDR HYIA20170828009Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .098 IN LENGTH.SDR SWAA2022011490263Access Panel · delaminated#1 ENGINE PYLON ACCESS PANEL 431AR IS DELAMINATED / REMOVED AND REPLACED #1 ENG PYLON ACCESS PANEL 431AR ASSY LOCATED NEW FASTENER HOLES AND COUNTERSINKED; ATTACHED FIRE SEAL PER SRM 51-40-02-OG-0; SRM 51-40-08-00-00 & DRAWING 313A2200SDR HYIA20170828008Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE LT OUTBOARD NACELLE FITTING. THESE CRACKS WERE DISCOVERED ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACKS MEASURED .088, .097, AND .155 IN LENGTH.SDR HALA2017031600106Support · crackedDURING H CHECK, FOUND THE RIGHT PYLON SUPPORT STRUCTURE ON INBOARD SIDE FOR RIB 8 CRACKED. REPAIRED THE SUPPORT IAW SRM 54-52-12, FIGURE 208.SDR GTIA2017031601821Fitting · nickedNICK FOUND ON THE NR 1 ENGINE PYLON TO WING FITTING. REPAIRED IAW EO 5451-1704.SDR HYIA20170828001Fitting · crackedWHILE CONDUCTING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS APPROXIMATELY 1.208 INCHES IN LENGTH.SDR HYIA20170828006Fitting · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THERE WAS ONE CRACK IN THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS .108 IN LENGTH. THE OTHER CRACK WAS DISCOVERED ON THE OUTBOARD SIDE OSDR HYIA20170828005Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS FOUND ON THE LT OUTBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK WAS MEASURED AT .191 IN LENGTH.SDR REXA2017022200287Attach Bracket · crackedLEFT LOWER HINGE LINE FAIRING ATTACH BRACKET BROKEN. REMOVED AND REPLACED THE ATTACH BRACKET IAW SRM-51-42-21.SDR HYIA20170828013Fitting · crackedDURING A SID 57-10-16 NDT INSPECTION, FOUR CRACKS WERE FOUND IN THE LT OUTBOARD FITTING. TWO OF THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .143 AND .129 IN LENGTH. THE OTHER TWO CRACKS WERE FOUND OSDR A6WA201744798Bracket · crackedSTANDOFF BRACKET AT 7 O'CLOCK POSITION ON RH ENGINE NOSE INLET COWLSDR QXEA2017013000825Mount · crackedRT FWD EXHAUST DUCT HAD 1 EA TIE BAR MOUNT CRACKED. WELDED RT FWD EXHAUST DUCT TIE BAR MOUNT USING .025" FILLER METAL WITH TITANIUM WELD ROD PER SRM 54-45-25 REPAIR-26 PG 202 STEP 7(C,D,E AND F). TRIMMED AWAY CRACKED AREA OF RT FWD EXHAUST DUCT TIE BAR MOUNT PSDR QXEA2017013000824Mount · crackedLT FWD EXHAUST DUCT HAS 1 EA TIE BAR MOUNT CRACKED. WELDED LT FWD EXHAUST DUCT TIE BAR MOUNT USING .025" FILLER METAL WITH TITANIUM WELD ROD PER SRM 54-45-25 REPAIR-26 PG 202 STEP 7(C,D,E AND F). TRIMMED AWAY CRACKED AREA OF LT FWD EXHAUST DUCT TO BAR MOUNT PESDR HYIA20170828007Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND ON THE RT OUTBOARD NACELLE FITTING. TWO OF THE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. MEASURED .050 AND .090 IN LENGTH. THE THIRD CRACK WAS FOUND ON THE OUTBOASDR HYIA20170828017Fitting · crackedDURING A ROUTINE INSPECTION, TWO CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. THESE CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .119 AND .146 IN LENGTH.SDR HYIA20170828015Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS FOUND IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK MEASURED .049 IN LENGTH.SDR HYIA20170828012Fitting · crackedDURING A ROUTINE INSPECTION, THREE CRACKS WERE FOUND IN THE RT OUTBOARD NACELLE FITTING. TWO CRACKS WERE FOUND ON THE INBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THEY MEASURED .161 AND .088 IN LENGTH. THE THIRD CRACK WAS FOUND ON THE OUTBOARSDR HYIA20170828014Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE LT INBOARD NACELLE FITTING. THE CRACK WAS DISCOVERED ON THE OUTBOARD SIDE, JUST FORWARD OF THE SPAR STRAP. CRACK LENGTH IS .117.SDR HYIA12062016002Fitting · crackedDURING A ROUTINE INSPECTION, CRACKS WERE IDENTIFIED AT RT OB NACELLE FITTING P/N 5292029-10. JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5 CURRENTLY AT REVISION 2 AND SERVICE KIT SK402-47A/B). THE MAJORITY OF THIS NACELLE FITTING IS NOT ACCESSIBLE FOSDR HYIA12062016001Fitting · brokenDURING A ROUTINE INSPECTION, A CRACK WAS IDENTIFIED AT RT IB ENGINE BEAM ASSEMBLY P/N 5654109-7 AND THE BEAM WAS REMOVED. AT REMOVAL, THE RT NACELLE IB FITTING P/N 5292029-12 WAS FOUND TO BE BROKEN IN HALF JUST FWD OF LWR FWD WING SPAR STRAP (REFERENCE MEB02-5SDR SIMA20161119006Fitting · crackedDURING IMBV INSPECTION, QC FOUND LT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED LT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFSDR SIMA20161118009Fitting · crackedDURING IMBV INSPECTION, QC FOUND RT ENGINE FWD LOWER YOKE FITTING CRACKED. AIRCRAFT WAS REMOVED FROM SERVICE FOR IMBV INSPECTION AND WILL BE RETURNED TO SERVICE AFTER INSPECTION. REMOVED AND REPLACED RT ENGINE FWD LOWER YOKE FITTING IAW EO-EM-54MR-386. AIRCRAFSDR SIMA20161115001Fitting · crackedLT ENGINE FWD LOWER YOKE CRACKED. REMOVED AND REPLACED LT FWD PYLON LOWER YOKE IAW EO EM-54MR-386.SDR FDEA201611124006Mount · corrodedNR 2 PYLON FWD MOUNT CORRODED. REPAIRED IAW SRM 54-51-81. MAJOR REPAIR.SDR FDEA201611124005Mount · corrodedCORROSION ON NR 1 PYLON FWD MOUNT. REPAIRED BY INSTALLATION OF BUSHINGS IAW SRM 54-51-81 MAJOR REPAIR .SDR DALA2016102507621Torque Box · crackedLEFT NACELLE STRUT FWD TORQUE BOX FWD ACCESS DOOR 432AL CRACKED CUTOUT. REPAIRED IAW ERA 551278-14.SDR KCSA201610141088Attach Fitting · crackedNR 2 PYLON I/B MIDSPAR FITTING CLIP HAS AN APPROX 1.5" CRACK IN THE RADIUS OF THE PART.SDR ABXA20161011167Angle · crackedANGLE CRACKED ON OUTBOARD PYLON JUST ABOVE AND FORWARD OF STRUT ACCESS DOOR. REMOVED AND REPLACED THE ANGLE IAW DRAWING 313T3310 AND SRM 51-40-02 PAR 7.SDR IPXA2016092108498Truss Fitting · chafedINSPECTION TYPE: 3C, RIGHT WING PYLON ENGINE MOUNT TRUSS FITTING CHAFED AT YWN 200.2. REPAIRED THE TRUSS FITTING IAW EA 011-5440-01-A6431 REV. I/R AND EO MD11-5440-61822-A.SDR ASOA20160811046Fitting · crackedDURING NR 2 ENGINE CHANGE THE LOWER FORWARD ENGINE YOKE LINKAGE FITTING WAS FOUND CRACKED, L=.245. MAINTENANCE REPLACED THE NR 2 ENGINE FORWARD YOKE LINKAGE FITTING IAW STS EA 26-2014-063.SDR A6WA201644072Bracket · brokenLEFT NOSE COWL PDU WIRE HARNESS BRACKET BROKEN. REPLACED BRACKET IAW CMM 20-42-06.SDR FDEA201606091914Fitting · damagedNR 1 PYLON OTBD AFT TR FITTING LOWER AFT HOLE DAMAGED. COMPLIED WITH EA F-5450-T0325811 P1 OF NR 1 PYLON OB AFT TR FITTING LOWER AFT HOLE.SDR SWAA2016060652389Mount Bracket · crackedRIGHT ENGINE AFT STRUT MOUNT BRACKET CRACKED ON BULKHEAD, EXTERNAL AREA OF LOWER SPAR OTBD SIDE. R & R BRACKET IAW SRM & DWG.
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