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 KCSA201404081038Fireshield · damagedNR 2 PYLON INBD INNER SURFACE, FIRE SHIELD, APPROXIMATELY NAC. STA 223 HAS DAMAGE.SDR CA140402011Shield · failed(CAN) DURING APPROACH, THE FLIGHT CREW NOTICED A HIGHER THAN USUAL T5 INDICATION THAT LIMITED THE NR 2 ENGINE TORQUE. THE ACFT LANDED WITHOUT INCIDENT. A 5" X 3" PIECE OF SHEET METAL FOUND IN THE ENGINE INLET COMPARTMENT. AREA INSPECTED AS WAS DISCOVERED THSDR SWIA201438011Blowout Door · looseRT LOWER COWL BLOW OUT DOOR HAS PLAY AT HINGES. C-CHECK, REPLACED INBD SIDE IAW SRM.SDR SWIA201438010Blowout Door · looseRT LOWER COWL BLOW OUT DOOR HAS PLAY AT HINGES. C-CHECK, REPLACED OTBD SIDE IAW SRM.SDR A6WA201441346Louver · crackedLEFT LOWER NOSE COWL 432AB ACCESS PANEL 432AC VENT LOUVER HAS CRACK ON INBD & OTBD ENDS TWO EACH SLATS. REMOVED CRACKED VENT LOUVER & INSTALLED NEW SERVICEABLE LOUVER IAW SRM 51-42-06, 51-40-11 & 51-25-16.SDR SWIA201438121Latch · wornRT ENGINE LOWER COWL BLOW OUT DOOR LATCH CATCH WORN. C-CHECK, R & R DOOR LATCH CATCH IAW SRM.SDR SWIA201438016Latch · wornLT ENGINE LOWER COWL BLOW OUT DOOR LATCH CATCH WORN. C-CHECK, REPLACED IAW SRM.SDR SPUY201403310037Latch · crackedNR 1 ENGINE, UPPER COWLING FITTING LATCH ATTACHMENT CRACKED ONE INCH.SDR CALA2014033190739Seal · damagedNR 1 PYLON FIRE SEAL DAMAGED. APPLIED SEALANT TO E1 FWD PYLON FIRE SEAL IAW SOPM 20-60-04.SDR DALA14019370984Structure · crackedCRACK FOUND DURING HFEC 06-10-01-001 ON NR 2 PYLON. REPAIRED IAW ERA 524353-14, REV ORIG.SDR CA140407013Gear · wrong part(CAN) WHILE ATTEMPTING TO RIG A NACELLE VENT DOOR, IT WAS DISCOVERED THAT THE ACTUATOR HAD A DIFFERENT GEAR RATIO THAN IS REQUIRED. INVESTIGATION REVEALED THAT THE ACTUATOR, PN 85891-02, CAME FROM THE MFG WITH DIFFERENT MODEL NUMBERS THAT DENOTE DIFFERENT GEASDR DALA14016430670Structure · dentedSMALL DENT IN NR 2 NOSE COWL, AT 7 O`CLOCK POSITION. REMOVED DAMAGE IAW SRM 54-11-01. INSTALLED REPAIR IAW SRM 54-11-01.SDR DALA14016743723Nacelle · damagedAFTER TAKEOFF A SLIGHT VIBRATION WAS FELT. PASSENGER REPORTED DAMAGE TO RT ENGINE COWLING. TOWER REPORTED POSSILBLE BIRD STRIKE. ACFT RETURNED TO DEPARTURE. MAINTENANCE INSPECTED ACFT IAW ERA 523786-14. DAMAGE WAS FOUND ON RT ENGINE COWLING, PYLON, WING ANSDR ASAA2014030807116Acoustic Panel · damagedFOUND NR 6 AFT ACOUSTICAL PANEL FWD INBD FASTENER ATTACHMENT DAMAGED. ACFT GROUNDED. INSTALLED NEW NR 6 AFT ACOUSTICAL PANEL ON NR 2 ENGINE IAW AMM TASK 72-23-02-400-801-F00.SDR ASOA20140302042Yoke · crackedNR 2 PYLON LOWER FORWARD YOKE CRACKED. R & R YOKE.SDR ASOA20140302041Yoke · crackedNR 1 PYLON LOWER FORWARD YOKE CRACKED. R & R YOKE.SDR KCSA201402261015Fireshield · damagedNR 2 PYLON FIRE SHIELD INBD SIDE AT APPROX BS 231 IS DAMAGED.SDR ASAA2014021206839Strut · wornWHILE ACCOMPLISHING ENGINE INLET INSPECTION ON NR 2 ENGINE T/C 78472000. FOUND OTBD UPPER AND LOWER FASTENERS MISSING ON NR 4 FAN FRAM STRUT, 3 O`CLOCK LOOKING FORWARD, FAN DUCT PANEL NR 5 WITH A FASTENER THAT WILL NOT TIGHTEN, AND FAN DUCT PANELS NR 1 AND NSDR GTIA201402071161Structure · damagedNR 2 ENGINE-DENT/SCRATCH FOUND ON ENGINE UP DURING WALK AROUND PERFORMED DIMENSION CK, DENT IS 2.7500" X 1 " AND J04 DEEP. OUT OF LIMITS REQUIRES NOSE COWL CHANGE. REMOVED DAMAGED COWL, INSTALLED ROBBED PART FROM A/C 522 IAW AMM 71-11-11, NEEDS OPS TEST, ACCOSDR SCNA20140210022Panel · corrodedPANEL 441DR UNDER SIDE HAS MULTIPLE AREAS WITH SURFACE CORROSION. REPAIRED PANEL 441DR.SDR HNAA2013123100648Flange · crackedLEFT NACELLE COLLAR FLANGE IS CRACKED AT FORWARD END. R & R FORWARD ANGLE ON LT COLLAR IAW AMM 54-40-04, 54-40-06 AND EO8-54-13-0696.SDR HNAA2013123100647Flange · crackedCOLLAR FLANGE IS CRACKED ON RT NACELLE, INBD FORWARD SIDE. REMOVED CRACKED SECTION IAW RD8-54-3449. HFEC INSPECTION WAS DONE. NO CRACKS FOUND. REPAIRED RT NACELLE IAW AMM 20-14-01 AND EO8-54-13-0728.SDR ABXR2013122000004Cowling · crackedNR 2 ENGINE INBD CORE COWL CRACKED AT TOP MID POINT. REPAIRED IAW SRM.SDR DALA13071650182Liner · puncturedTWO SMALL PUNCTURES ON NR 1 ENGINE INNER LINER AT 10 O`CLOCK POSITION, REPAIRED IAW SRM 54-00-01.SDR ASAA2013121596889Panel · damagedDURING NR 2 ENGINE INLET AND FAN BLADE DETAILED INSPECTION, FOUND NR 1, AT 12 O`CLOCK POSITION AFT, FAN DUCT PANEL HAS DAMAGED FASTENER HOLE, AFT INBD FASTENER (M). ACFT GROUNDED. FAN DUCT PANEL NR 1 AT NR 12 POS AFT. R & R IAW AMM 72-30-07-400-801-00.SDR ASAA2013120596854Panel · crackedACCESS PANEL 5815 CRACKED. INSTALLED NEW ACCESS PANEL.SDR ASAA2013120596855Structure · chafedNR 1 PYLON, OTBD MID-FAIRING SIDE LINK MISSING ONE NUTPLATE. STRUCTURE UNDER NUTPLATE FOUND TO HAVE CHAFING AND IS OUT OF LIMITS. LOCATED AND DRILLED NEW NUTPLATE IAW SRM 54-50-71-1A-1, FIG 101, 51-40-05-0G-0 AND AMM 51-21-21-307-014.SDR DALA13064516303Doubler · crackedNR 1 PYLON OTBD STRUT T/E DOOR FWD LOWER AREA EXITING DOUBLER FOUND CRACKED. REPLACED DOUBLER IAW EA 63-82067, REV A, SECTION II AND HFEC INSPECTION, NO CRACK FOUND IAW NDTM PART 5 51-00-00, PROCEDURE 11 OR 16.SDR FDEA201311132759Fairing · damagedFOUND NR 3 ENGINE PYLON AFT BOAT TAIL DAMAGED. FWD LOWER SECTION DEPARTED ACFT. DAMAGE TO AFT CENTER BODY AND TAIL CONE. DAMAGE TO EXHAUST NOZZEL AROUND TAIL CONE AT 12 O`CLOCK POSTION.SDR FDEA201311102724Bushing · migratedNR 1 PYLON LOWER SPAR FITTING BUSHING MIGRATED. REPAIRED IAW SRM 54-50-90 REPAIR 5, FIG 201, PROCEDURE III, REV.110. MAJOR REPAIR.SDR FDEA201311102723Bushing · migratedNR 2 PYLON LOWER SPAR FITTING BUSHING MIGRATED. REPAIRED PER SRM 54-50-90 REV 110 REPAIR 5. REPAIR CLASSIFIED AS MAJORSDR GTIA201311091031Door · departedAIR RETURN DUE LOOSING RT ENGINE INBD AND OTBD COWLINGS, DECLARING EMERGENCY. LANDED SAFELY. INSPECTIONS REVEAL DAMAGES TO THE SECONDARY PYLON STRUCTURES AND IN THE VERTICAL L/E STABILIZER PANEL. REPAIR OF THE SECONDARY PYLON STRUCTURES IN PROCESS AND VERTISDR DALA13059723212Receptacle · corrodedDURING INSPECTION, FOUND CORROSION ON LT PYLON SPIGOT RECEPTACLE FITTING. REPLACED LT PYLON SPIGOT RECEPTACLE IAW SRM 54-51-12 PARAGRAPH 5.A FIG 201, DWG R54612042, & R54612043.SDR DALA13060185640Bushing · migratedNR 1 PYLON UPPER LINK FITTING BUSHING MIGRATED. REMOVED, INSPECTED AND REPAIRED IAW SRM 54-51-90.SDR A6WA201310314M308Structure · damagedLT ENG LOWER CORE COWL ALIGNMENT HOLES ELONGATED. FABRICATED 2 EA DOUBLERS FOR ELONGATED HOLES ON LT ENG LOWER CORE COWL.SDR 2013FA0000657Shroud · crackedRT UPPER EDUCTOR SHROUD CRACKED AT FORWARD CIRCUMFERENTIAL FLANGE; BEYOND LIMITS IAW SRM. REPAIRED IAW REPAIR STATEMENT 340SDS034475.SDR R61A201310281069Bolt · corrodedDURING HEAVY CHECK, LT PYLON 419DT HAS SEVERAL SCREWS ALONG TOP OF PANEL THAT ARE CORRODED. MX R & R CORRODED SCREWS ON LT PYLON PANEL 419DT IAW AMM 54-50-21.SDR R61A201310221078Structure · corrodedDURING HEAVY CHECK, RT AFT PYLON ADEL CLAMPS, STANDOFFS,AND HARNESS CLAMPS CORRODED. MX R & R CORRODED STANDARDS IAW SRM 51-42-00, SWPM 20-51-00 AND AMM 20-10-03.SDR KCSA201310170104Fireshield · chafedNR 3 PYLON INBD FIRESHIELD FWD OF AFT ENGINE MOUNT IS CHAFED APPROX. NAC STA 218.SDR KCSA201310170103Fireshield · chafedNR 3 PYLON INBD SIDE OF FIRESHIELD JUST AFT OF REAR ENGINE MOUNT CHAFED APPROX. NAC STA 223.SDR KCSA201310170102Fireshield · chafedNR 2 PYLON INBD FIRESHIELD JUST FWD OF ENGINE MOUNT IS CHAFED APPROX. NAC STA 219.SDR KCSA201310170101Bracket · chafedNR 2 PYLON NAC STA 196 LOWER WEB, BLEED AIR DUCT ANTI-ROTATION BRACKET CHAFED.SDR KCSA201310170100Fireshield · chafedNR 2 PYLON APPROX. NAC STA 263 I/B AFT FIRESHIELD CHAFED.SDR R61A201310151041Clamp · corrodedDURING HEAVY CHECK, RT ENGINE PYLON HAS SURFACE CORROSION ON ADEL CLAMPS, TWO PLACES LOWER WING CONDUIT BRACKET. MX R & R TWO ADEL CLAMPS AT NR 2 ENGINE AFT PYLON LOWER WING AND CONDUIT BRACKET IAW AMM 20-10-01.SDR REXA2013101102054Fairing · gougedRT ENGINE LOWER AFT HINGE LINE FAIRING 443BB GOUGED. FABRICATED NEW HINGE LINE FAIRING IAW SRM 51-24-21 AND SRM 51-40-11.SDR REXA2013100902167Plate · wornRT ENGINE LOWER CORE COWL BLOW OUT DOOR STRIKER PLATE WORN. R & R STRIKER PLATE IAW SRM 51-42-06.SDR REXA2013100902103Panel · damagedPANEL 433BB CRACKED & GOUGED. REMOVED & INSTALLED PIECES TO NEW PANEL IAW SRM 51-42-06 & SRM 51-42-13. FABRICATED NEW PANEL IAW SRM 51-24-21. NEW MATERIAL ID IS .0632024-T3.SDR REXA2013100902095Pad · wornRT AFT CORE COWL RUB PAD MOUNT BLOCK WORN. R & R RT AFT CORE COWL RUB PAD MOUNT BLOCK AND RUB INSULATING PAD IAW SRM 54-13-00.SDR REXA2013100902085Access Panel · gougedACCESS PANEL 443BB IS GOUGED ON AFT END. FABRICATED NEW ACCESS PANEL IAW SRM 51-24-21 AND SRM 51-40-41.SDR REXA2013100902084Access Panel · gougedACCESS PANEL 443BT IS GOUGED ON AFT END. FABRICATED NEW ACCESS PANEL IAW SRM 51-24-21 AND SRM 51-40-11.
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