JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 IPXA10559440Attach Angle · crackedINSPECTION TYPE:C1, WHILE WORKING CUSTOMER CARD NR 853032 FOUND THE LT AFT FAIRING STRUCTURE TO HAVE (2 EA) UNDER LYING ATTACHING ANGLES CRACKED, BEHIND THE AFT LOWER TE SKIN HEAT SHIELD PP5291.8, PN 313N5052-67 AND 313N5052-68. R & R IAW SRM 51-40-02-0G.SDR FDEA201004191226Structure · wornNR 2 ENG PYLON PANEL 457 CL UPPER LATCH CONTACT AREA IS WORN. REPAIRED AREA IAW SRM 54-32-01, VOL III AND SRM 51-35-01, VOL II. ALODINED AND PRIMED REPAIR IAW SRM 51-21-01, VOL II. WORK WAS COMPLETED IAW DWG AUB 7332.SDR 2010FA0000342Stiffener · crackedPYLON NR 1, INBD NR 3, STIFFENER CRACK.SDR 2010FA0000435Door · crackedNR 2 PYLON LT SIDE PRESSURE RELIEF DOOR CRACK (0.35 INCH).SDR DALA1318560171Pin · crackedREPLACEMENT OF CRACKED RT FUSE PINS IAW 01-059169-12, ME06.SDR DALA1011710661Fitting · damagedNR 2 PYLON LT SIDE LOWER CHORD AND FITTING AT STA 142 FOUND INCOMING HOLE WITH FREEZE PLUG INSTALLED. ACCOMPLISHED ER/A 481530-14, REV ORIGINAL REF NON ROUTINE 160664 (DL757101351).SDR DL76L100550Bushing · wornNR 2 PYLON LOWER SPAR FITTING BUSHINGS REPLACED IAW SRM 54-53-90 FIG 201 REPAIR 4SDR FDEA201003020591Latch · corrodedNR 2 ENGINE FAN COWL CENTER LATCH FITTING IS SEVERLY GOUGED. COMPLIED WITH EA 6-7110-136625.SDR DL76L100551Bushing · wornNR 1 PYLON LOWER SPAR FITTING BUSHINGS REPLACED IAW SRM 54-53-90 FIG 201 REPAIR 4.SDR UALA2010030200740Heater Blanket · burnedSHIELD ASSY NR 2 ENGINE BURNED AND FALLING APART. REPLACED HYD HEAT SHIELD BLANKET AND SECURED. ALL OKAY.SDR DL757100819Structure · damagedNR 2 PYLON LT SIDE HAS 3 EA INCOMMING HOLES OVERSIZED AT STA 143 TO 146. REPAIRED IAW ERA480018-14 REV ORIG AT SAA ON NRC 159256.SDR 22AA201000041Fairing · crackedDURING "C" CHECK, NR 1 ENGINE PYLON FWD FAIRING FWD SIDE FOUND WITH CRACK. NON-ROUTINE NR 224, CRACK AREA AT NR 1 ENGINE PYLON FWD FAIRING FWD SIDE AREA REPAIRED IAW EN 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3 DATED 26 FEB 2010.SDR 22AA201000039Fairing · crackedDURING "C" CHECK, NR 3 PYLON FWD FAIRING FOUND WITH CRACKED AT 02 LOCATIONS. NON-ROUTINE NR 227, 02 EACH CRACK LOCATIONS AT NR 3 ENGINE PYLON FWD FAIRING AREA REPAIRED IAW 1004-10 WORK INSTRUCTIONS AND FAA APPROVED FORM 8110-3, DATED 26 FEB 2010.SDR A6WA201040075Structure · crackedPYLON PANEL 412BT SEPARATOR CLIP IS CRACKED. R & R SEPARATOR CLIP PN 601-37003-183 IAW SRM 51-42-06.SDR FDEA201001250235Frame · crackedCRACK INDICATION FOUND APPROX 0.5" IN LENGTH DURING HFEC INSP ON THE NR 2 PYLON CARRY THRU STRUCTURE ACCESS PANEL NR 363ML CUTOUT. REPAIR CARRIED OUT IAW EA NR 1-5530-137547. THIS REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 109.SDR A6WA201040042Hinge Fitting · gougedRT ENGINE LWR TRANS COWL INNER INBD CTR HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO NR 601R-78-33-3922.SDR A6WA201040041Hinge Fitting · gougedRT ENGINE UPR TRANS COWL INNER INBD HINGE FITTING IS GOUGED. REPAIRED GOUGE IAW REO 601R-78-33-3923.SDR FDEA201001170165Bushing · misalignedSTRUT NR 1 DIAG BRACE WING FITTING OTBD BUSHING HAS MIGRATED. REMOVED BUSHINGS IAW SOPM 20-50-03. RECEIVED REPAIR BUSHINGS ON TRAV NR T9/811726. INSTALLED 2EA REPAIR BUSHINGS IAW EA F-5740-131560. CATEGORY "A". MAJOR REPAIR.SDR 2010F00004Nose Cowl · unsecureUPON CLIMBOUT THE PILOTS NOTICED THE LT UPPER NOSE COWLING WAS SLIGHTLY LIFTING FROM ITS MATING SURFACE. THE PILOTS REDUCED POWER DROPPED FLAPS AND GEAR DECLARED AND EMERGENCY AND TURNED BACK FOR THE AIRPORT. THE ACFT LANDED UNEVENTFULLY. UPON SHUTDOWN OUR MX SDR IXXA10WSAP018SFairing · delaminatedDURING ROUTINE C-CHECK INSP FOUND NR 2 PYLON V-FAIRING 447DB FWD AREA DELAMINATED. ACCOMPLISHED REPAIR IAW SRM 51-70-17, REV 101 AND SRM 51-21-10, REV 101.SDR SWIA200923178Structure · crackedLEFT ENGINE NACELLE CRACKED. (C-CHECK) REPAIRED PER SRM.SDR HYIA1376GLBEAMBeam · crackedDURING A ROUTINE SCHEDULED INSP, MX FOUND LT NACELLE INBD ENG CARRIER BEAM CRACKED. REPLACEMENT OF BEAM IN PROGRESS.SDR FDEA200911184010Nose Cowl · damagedNR 1 ENG NOSE COWL EXTERIOR SKIN AFT OF THE BULLNOSE IS DETERIORATED AROUND THE ENTIRE CIRCUMFERENCE. REPAIRED THE NR 1 ENG NOSE COWL EXTERIOR SKIN AFT OF THE BULLNOSE DETERIORATED AROUND CIRCUMFERENCE BY APPLYING FIBERGLASS EPOXY RESIN AND GRAPHITE CLOTH IAWSDR DL757100337Structure · damagedNR 2 PYLON RT SIDE APPROX STA 150 FOUND 6 EA OVERSIZED HOLES. ACCOMPLISHED ERA 478214-14 REV ORIG AT SAA SAT REF NON ROUTINE 136582.SDR DXTA2009111103853Structure · dentedPOSSIBLE BIRD STRIKE ON RT ENGINE AT 7 OCLOCK POSITION. DENT FOUND ON ENGINE LIP AND BLOOD WITH FEATHERS AROUND INTAKE.SDR A6WA200940772Seal · crackedON RT COWL TORQUE BOX 2 FWD SEALS (BOTTOM AND OTBD BOTTOM) FOUND CRACKED ON RT COWL TORQUE BOX 2 FWD SEALS REPLACED IAW SRM 51-42-12.SDR UIEA2009110300004Structure · damagedEO 4471A044, DURING THE A-CHECK INSP ON 11/3/2009, MX FOUND DAMAGE TO THE NR 2 ENG LT CORE COWL UPPER FWD CORNER. (DISPOSITION WAS MADE TO PERFORM A TIME LIMITED REPAIR AS DESCRIBED IN PART 1 WORK INSTRUCTIONS. SCHEDULE REPEAT INSPECTIONS AT EVERY A-CHECK AND SDR HALA2009103000496Structure · damagedETOPS SIGNIFICANT SYS -NR 1 ENG OTBD FAN COWL DAMAGE TOP, CAUGHT ON PYLON PANEL DAMAGE IS 2'' LONG AND 1/2 SPLIT. APPLIED SPEED TAPE TO DAMAGED AREA OF NR1 ENG OTBD FAN COWL IAW M105 FILE NR R0032. OK FOR SERVICE.SDR DL757100339Bushing · migratedNR 1 ENGINE MIDSPAR OTBD SIDE LOAD FITTING BUSHING MIGRATED. ACCOMPLISHED ERA 477160-14AD AT SAA SAT REF NON ROUTINE CARD 124460.SDR A6WA200940706Strip · corrodedLT ENGINE UPPER CORE COWL INNER WEAR STRIP ERRODED. LT ENGINE UPPER CORE COWL STRIP REPLACED IAW SHORTS CMM 71-12-01-300-820-A01.SDR FDEA200910263666Plate · gougedNUMBER 1 PYLON AFT STRUT FAIRING LOWER PLATE FOUND 2 GOUGED MARKS. REPAIR CARRIED OUT IN ACCORDANCE WITH EA NR F-5480-131057 EA. REPAIR IS CLASSIFIED AS MINOR AS PER GMM 6-2-100 CRITERIA.SDR A6WA200940732Strip · erodedLT ENGINE LWR CORE COWL AFT INNER WEAR STRIP ERODED. AFT INNER WEAR STRIP ON LT ENGINE LWR CORE COWL REPLACED IAW CMM 20-42-06. (K)SDR HALA2009102200474Bracket · brokenETOPS SIGNIFICANT SYSTEM - FOUND ON WALKAROUND BY MTC NBR 1 ENG ACOUSTICAL PANEL AT 4 O'CLOCK POSITION PULLED UP. REMOVED AND REPLACED BRACKETS AND ACOUSTICAL PANEL IAW 72-33-05. OK TO SERVICE.SDR BSYA2009054Fastener · looseAFTER DEPARTING ADS PILOT NOTICED A COUPLE OF FASTENERS POPPED LOOSE. RETURNED TO ADS, MAINTENANCE SECURED ALL FASTENERS, OK FOR CONTINUED FLIGHT.SDR DL757091655Structure · crackedNR 2 O/B PYLON UPPER CHORD CRACKED AT NAC STA. 136 / ACCOMPLISHED ER/A 477153-14 REV ORIG AT SAA SAT ON N/R CARD 141834SDR A6WA200940674Door · gougedLT ENGINE NOSE ACCESS COWL 432 AT LIPS FUND GOUGED OUT OF LIMITS (1" X 0.3" X 0.08"). REPLACED IAW CMM 71-14-01-300-814-401. (K)SDR RMV2009F00001Door · unsecureAFTER TAKEOFF, THE FLIGHT CREW NOTICED AIRFRAME VIBRATION. ACFT LANDED AT THE CLOSEST AIRPORT WITHOUT INCIDENT. A VISUAL INSPECTION OF THE RT COWLING SHOWED THAT THE FWD OTBD 2 LATCHES WERE UNLATCHED AND THE AFT OTBD LATCH WAS SECURED. THE UPPER AND LOWER CSDR FDEA200909273390Door Frame · chafedNR 2 ENGINE DOOR JAMB AREAS AT APPROX 5 O'CLOCK POSITION CHAFED. REPAIRED PER EA1-5450-133871 (MAJOR REPAIR).SDR KPVA200910001Structure · contaminatedLT NACELLE, AFT TAIL CONE, OUTBOARD SIDE HONEYCOMB HAS OIL CONTAMINATION. REMOVED APPROXIMATELY 750SQ/IN OF CONTAMINATED HONEYCOMB. REPLACED HONEYCOMB AND FIBERGLASS PLIES IAW BOMBARDIER RD 8-57-2752.SDR FDEA200909143296Shield · crackedNR 2 PYLON "Y" DUCT HEAT SHIELD IS CRACKED AT THE LR FLANGE. REMOVED AND INSTALLED HEAT SHIELD IAW SRM 51-40-21. MATERIAL ID 2024-T3 IAW SRM 51-70-10; PG 102. ALODINED AMD PRIMED DOUBLER IAW SRM 51-40-2; PARA 6. STOPPED DRILLED IAW SRM 51-70-10; PG 102.SDR CA090914002Washer · cracked(CAN) DURING A 600HRS INSPECTION, ONE OF THE WASHER P/N 204-030-913-005 WAS FOUND CRACKED. THE CRACK IS COMING INWARD FROM THE OUTTER CIRCONFERENCE OF THE WASHER. THIS IS THE THIRD TIME THAT THIS WASHER IS BEING REPLACED OVER A PERIOD OF JUST OVER A YEAR, THE SDR UIEA200900055Beam · severedNR 4 PYLON LT SPRING BEAM FORWARD JOURNAL END SEVERED. NR 4 ENGINE REMOVED FOR FERRY FLIGHT TO ROW. ALL REQUIRED INSPECTIONS ACCOMPLISHED. AS PER RECOMMENDATIONS AS PER SB 747-54A2214 AND SB 747-54A2182.SDR LR7A2009090900125Plenum · crackedDURING SCHEDULED C-9 CHECK PER JOB CARD HC7204, FOUND NR 3 ENGINE AFT NACELLE PLENUM CRACKED AT FS 535, WL 255, PPBL0. REPAIRED IAW LAC MEA 382-54-09-028.SDR LR7A2009090900124Plenum · crackedDURING SCHEDULED C-9 CHECK PER JOB CARD HC7204, FOUND NR 2 ENGINE AFT NACELLE PLENUM CRACK AT FS 535, WL 250.5, PP LBL9.5. REPAIRED IAW LAC MEA 382-54-09-027.SDR CA090901004Cowling · departedDURING TAKE-OFF PHASE, ACFT LOST THE LT FWD ENG COWLING.SDR CA090903002Access Door · separatedDURING ROUTINE FLIGHT REFUEL/DEFUEL ACCESS DOOR CAME OFF. ISAR Q123-2008-09 AND REPAIR DWG RD8-54-2335 AND IN-SERVICE MODSUM IS8Q5200012 WERE RAISED TO ADDRESS THIS ISSUE.SDR CA090825004Bracket · crackedTHE RT UPPER REAR CORNER BRACKET UNDER THE ENG DECK FOUND CRACKED.SDR UIEA201000176Fairing · crackedENG 3 OTBD CORE COWL UPPER AFT AREA FAIRING HAS A CRACK. ON THE AFT UPPER EDGE. DUE TO NO STOCK FOR THE PANEL, DISPOSITION WAS TO ACCOMPLISH A TIME LIMITED REPAIR BY WELDING THE CRACK IAW STANDARD PRACTICES AND REPLACEMENT OF FAIRING WITHIN THE NEXT 2A CHECK.SDR CA090807002Nacelle · dentedUPON ARRIVAL AT THE MX BASE, EVIDENCE OF A BIRD STRIKE WAS NOTICED ON THE RT WING L/E. UPON CLOSER EXAMINATION IT WAS FOUND THAT THE BIRD HAD IMPACTED ON THE FWD EDGE OF THE UPPER FWD ENG COWL (COMMONLY KNOWN AS THE HORSECOLLAR) AND SPLATTERED BACK ON TO THE SDR TRBACPCP20090018Structure · corrodedRIGHT INBOARD UNDERWING NACELLE BOX JUNCTION LINE HAS CORROSION. COMPLIED WITH ATR-72 SRAS DO/TS-4640/OS.3376.
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