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 HYIA20181003007Beam · crackedDURING MAINTENANCE A CRACK WAS FOUND ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11) THIS CRACK BEGINS AT THE UPPER INBOARD FASTENER HOLE COMMON TO THE TURBOCHARGER MOUNTING BRACKET, AND MEASURES APPROXIMATELY .371 INCHES LONG. THIS BEAM WSDR IPXA2018092864443Rod · not reportedNR 2 ENGINE FAN COWL SUPPORT ROD. R & R THE SUPPORT ROD IAW AMM 71-13-04-0401, OPS NORMAL.SDR IPXA2018100534697Fastener · looseNR 2 ENGINE INLET NOSE SKIN HAD LOOSE BLIND FASTENERS. REPAIRED IAW EA 011-7110-01-A7465, REV IR, AND EO MD11-7110-58061-B. MINOR.SDR HYIA20180914001Beam · crackedDURING NDT TESTING DONE TO SATISFY AD 2015-07-03, A CRACK WAS DISCOVERED ON THE LEFT NACELLE INBOARD ENGINE BEAM P/N: 5654109-6. THIS CRACK IS TRAVELING LEFT TO RIGHT ACROSS THE TOP OF THE BEAM ORIGINATING FROM A FASTENER HOLE ON THE TOP OF THE BEAM TRAVELLINGSDR HYIA20180827001Crossbeam · chafedDURING MAINTENANCE, CHAFING DAMAGE WAS FOUND ON THE RIGHT NACELLE CROSSOVER BEAM.SDR 2019F00062Cowling · erodedLEFT ENGINE LOWER COWLING DAMAGE (EROSION) ENGINEERING LETTER # DQ14437M1SDR P5CA201808220197Structure · erodedNR 1 ENGINE LT FAN COWL ERODED. REPAIRED THE AREA IAW CMM 71-13-21, REPAIR 9, REV 42.SDR P5CA201808220201Rivet · looseRIVETS ON THE NR 2 ENGINE RT CORE COWL AFT LOWER SIDE WERE FOUND LOOSE. REMOVED AND REPLACED THE DAMAGED RIVETS IAW SRM 51-40-02, REV 71, AND EI 72018A71M-4217, REV O.SDR REXA201808290741Fairing · crackedDURING REMOVAL OF THE NR 2 ENGINE PYLON TIE BAR K FRAME, FOUND THE UPPER, AFT HINGE LINE FAIRING TO BE CRACKED AT A SCREW HOLE. REMOVED & REPLACED THE FAIRING IAW SRM 51-42-06, AND 51-42-13.SDR ASOA2018082385178Bushing · wornLEFT ENGINE PYLON TIE-BAR ATTACH BUSHINGS AND BEARINGS WORN. REPLACED THE BUSHING AND BEARINGS IAW REO 670-54-22-002, REV NC, AND EC/TC REO 670-54-22-002.SDR DALA2018081505096Structure · damagedNR 1 ENGINE UPPER PYLON APRON CENTER SECTION MISSING AND AFT SECTION DAMAGED. R & R THE PYLON APRON CENTER AND AFT SECTIONS .SDR ASOA201808117146Yoke · crackedLEFT LOWER FORWARD YOKE CRACKED. REMOVED AND REPLACED YOKE.SDR DALA2018080804618Fairing · damaged(LOG 0686283) DURING INSPECTION FOUND BURNED MATERIAL OF FWD STRUT FAIRING ACCESS PANELS 431ER AND 441EL RH/LH ENGINE. ACCESS PANELS 431ER AND 441EL RH/LH WERE REPAIRED PER B-737-800 SRM 51-70-05 REPAIR 1.SDR V0XD20180809MD3Fire Seal · tornLEFT LOWER ENGINE COWLING DRAIN PAN FIRE SEAL WAS TORN. REPAIRED THE FIRE SEAL IAW REO 670-54-23-959, REV E, AND REO 670-54-23-1166.SDR IPXA2018081543824Door Frame · chafedNR 2 ENGINE RT FAN COWL DOOR FRAME HAD A WIDE SPREAD, DEEP CHAFE TO THE RUBSTRIP FROM TOP TO BOTTOM WITH DAMAGE TO UNDERLYING SKIN. REMOVED, FABRICATED AND INSTALLED THE RT FAN COWL DOOR FRAME AND RUBSTRIP IAW SREO MD11-5420-42847-A.SDR K11A2018112124012Structure · corrodedINNER CHORD ABOVE #2 ENGINESDR K11A2018112124011Structure · corrodedINNER CHORD ABOVE #2 ENGINE RIGHT SIDE HAS AREAS OF CORROSION.SDR K11A2018112124010Structure · corrodedOUTER CHORD ABOVE #2 ENGINE HAS CORROSIONSDR A8ZR20180823007Striker · out of limitsACCOMPLISHED RE-CONTOUR OF NR 2 ENGINE I/B COWL DOOR NACELLE STRIP-STRIKER FOR THE UPPER EDGE OF THE DOOR IAW EA 43-2018-083, REV A.SDR IPXA2018062983178Truss · gougedDURING A NR 3 PYLON INSPECTION, FOUND A GOUGE ON INBOARD TRUSS BEAM STRAP, OUTBORAD FACE. THE DAMAGE MEASURES 0.457 INCH LONG BY 0.17 INCH WIDE BY 0.055 INCH DEEP. REPAIRED IAW EO MD11-5410-69029-A, REV. AREA BLENDED OUT.SDR ASAA20180625177Panel · damagedWHILE ACCOMPLISHING TC 78472000 ON THE NR 2 ENGINE, FOUND FAN DUCT PANEL NR 12, AFT OTBD FASTENER PULLED THRU THE PANEL. ACFT GROUNDED. REMOVED AND REPLACED KEY-LOCKED INSERT FOR THE NR 12 FAN DUCT PANEL IAW SPM 70-42-13. INSTALLED THE FAN DUCT PANEL IAW SDR DALA2018062524187Rod End · corrodedNR 2 PYLON SUPPORT ROD IN THE THRUST REVERSER BAY ACCESS, JUST ABOVE, FWD AND AFT OF THE THRUST REVERSER LOCKOUT, HAD LOOSE HARDWARE AND RUSTED ROD ENDS. CLEANDED THE BEARINGS, ROD ENDS AND TIGHTEN LOCK NUTS IAW AMM 54-52-01.SDR REXA201806210522Nacelle · contaminatedAFTER ENGINE START AND DURING FLIGHT, A STRONG OIL ODOR FROM THE A/C PACKS, ODOR IN THE COCKPIT & AFT ROWS. RAN ENGINES IAW AMM 71-00-00. RAN PACKS IAW 21-51-00. OPENED THE ENGINE COWLS AND FOUND RESIDUAL OIL. CLEANED IAW SRM 51-26-00. NO DEFECTS FOUND. SDR IPXA2018062533972Rib · crackedNR 2 ENGINE PYLON WAS CRACKED, OTBD, AFT CORNER OF THE PRECOOLER AREA. REMOVED AND REPLACED THE RIB 8A IAW DWG A54612356, AND SRM 51-40-21.SDR DALA2018061103935Structure · dentedDURING A PREFLIGHT, FOUND SIGNIFICANT NOSE COWL DENTS AT 11:45 POSITION. REMOVED THE 1 ENGINE INLET COWL IAW PPBM 71-00 AND ERA 569353-14 AND INSTALLED SERVICEABLE INLET NOSE COWL.SDR SIMA20180606010Yoke · crackedLT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED UNSERVICEABLE AND INSTALLED NEW LT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.SDR SIMA20180606009Yoke · crackedRT PYLON ENGINE FORWARD LOWER YOKE CRACKED. (BEHIND LOWER FWD ENG MOUNT). REMOVED AND REPLACED RT PYLON ENGINE FORWARD LOWER YOKE IAW EO EM-54MR-386.SDR IPXA2018061830750Frame · crackedINTERNAL FRAME CRACKED INSIDE THE NR 2 PYLON LOWER AFT FAIRING. REMOVED, FABRICATED, AND INSTALLED A REPLACEMENT FRAME IAW DWG AVB7599, AND SRM 54-01-42.SDR IPXA2018062531013Skin · chafedNR 1 ENGINE. OTBD FAN COWL UPPER FWD DOOR HINGE FITTING WAS CHAFED. REPAIRED THE SKIN IAW EA 011-7110-01-A7299, REV I/R, AND EO MD11-7110-68797-A.SDR SWIA2018062644831Nose Cowl · dentedTWO DENTS ON THE LT ENGINE LIP SKIN AT THE 9 O'CLOCK POSITION. INSTALLED A NEW NOSE COWL ASSEMBLY IAW AMM.SDR REXA201805230405Support Bracket · crackedCRACKED SUPPORT BRACKET ON THE NR 1 ENGINE PYLON. REMOVED THE DAMAGED AND FABRICATED NEW AND INSTALLED IAW SRM 51-42-06.SDR ASAA2018051744649Case · corrodedDURING A NR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION. CORROSION FOUND ON 17 NUT PLATES FOR THE AFT ACOUSTICAL PANELS FROM APPROX 1:30 TO 10:30 O'CLOCK POSITIONS. AROUND BOTTOM OTBD SIDE OF CASE. ALSO FOUND THE NR 5 FAN FRAME AT 5 O'CLOCK POSITION SDR DALA201805153343Fairing · crackedRT PYLON AFT FIXED FAIRING CRACKED AT RIB 15. REPAIRED IAW AMDS 5450-01052-06B.SDR DALA2018051203342Fairing · crackedLT PYLON, AFT FIXED FAIRING WAS FOUND CRACKED AT RIB 15, REPAIRED IAW AMDS 5450-01052-06A.SDR UIEA201805160469Rub Strip · corrodedNR 2 ENGINE, RT CORE COWL EXTERIOR SURFACE FWD UPPER WEAR STRIP FOUND CORRODED. THE WEAR STRIPS WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 106.SDR UIEA201805160470Rub Strip · wornNR 2 ENGINE, RT CORE COWL UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160471Seal · tornNR 2 ENGINE, LT CORE COWL UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160472Shim · tornNR 1 ENGINE, RT CORE COWL MID & AFT HINGE ASSY ATTACH SHIMS FOUND TORN. THE SHIMS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160474Shim · tornNR 2 ENGINE, LT CORE COWL MID & AFT HINGE ASSY ATTACH SHIMS FOUND TORN. THE SHIMS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160494Rub Strip · wornNR 2 ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED SRM 51-40-02, REV 106.SDR UIEA201805160497Rub Strip · wornNR 1 ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160498Rub Strip · wornNR 1 ENGINE. LT CORE COWL FAIRING ASSY, INTERIOR SURFACE AFT UPPER AFT EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160499Rivet · damagedNR 1 ENGINE, RT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACH RIVETS FOUND DAMAGED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160500Rivet · damagedNR 2 ENGINE, LT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACH RIVETS FOUND DAMAGED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160501Seal · crackedNR 1 ENGINE, RT CORE COWL FAIRING ASSY UPPER EDGE AFT STRIP SEAL FOUND CRACKED. THE FAIRING ASSY SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160503Fastener · corrodedNR 2 ENGINE, RT CORE COWL INTERIOR SURFACE AFT SHEAR PLATE ATTACH FASTENERS FOUND RUSTY. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160502Seal · crackedNR 1 ENGINE, LT CORE COWL FAIRING ASSY. UPPER EDGE AFT STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160504Fastener · corrodedNR 2 ENGINE, RT CORE COWL MID AND AFT HINGE ATTACH FASTENERS FOUND RUSTY. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160636Adapter · wornNR 1 ENGINE, RT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER WAS FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.SDR UIEA201805160637Adapter · wornNR 2 ENGINE, RT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106.
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