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 UIEA2017072201265Fastener · looseNR 2 ENGINE NOSE COWL UPPER AREA FOUND WITH SEVERAL FASTENERS LOOSE. THE FASTENERS WERE TIGHTEN IAW AMM 20-11-00, REV 121.SDR UIEA2017070701122Structure · scratchedNR 1 ENGINE, RT CORE COWL EXTERIOR SURFACE FOUND WITH A SCRATCH. THE SCRATCH WAS SMOOTHENED AND FOUND WITHIN LIMIT AS IAW SRM 54-45-01-1A-1, FIG 101, DETAIL 2, REV 104.SDR UIEA2017070701123Structure · scratchedNR 1 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND WITH SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.SDR UIEA2017070701127Structure · scratchedNR 2 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.SDR UIEA2017070701128Door · damagedNR 2 ENGINE, LEFT CORE COWL FLIPPER DOOR FOUND DAMAGED. THE DOOR WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070101083Frame · wornNR 2 ENGINE, LT CORE COWL SECOND ZEE FRAME FROM FWD FOUND EXISTING REPAIR WORN. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062001046Stop · wornNR 1 ENGINE LEFT CORE COWL ATTACH STOP FOUND WORN. THE STOP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017062301059Seal · damagedNR 1 ENGINE LEFT CORE COWL FAIRING AFT UPPER EDGE STRIP SEAL FOUND DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017070101080Frame · chafedNR 2 ENGINE LEFT CORE COWL MOST AFT FRAME FOUND A CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR COEA2017072701816Panel · chafedLEFT ENGINE NACELLE INBOARD LATERAL PANEL LANDING HAS CHAFING AND CORROSION. REPAIRED IAW SRAS PCE-1570/17.SDR P5CA2017072600234Fitting · damagedNR 1 PYLON AFT STRUT UPPER LATERAL RESTRAINT FITTING INBD LOWER CORNER FOUND CONDUCTIVITY IS 37.6% IACS. THE RESTRAINT FITTING REPLACED IAW R1-54-00-11949, REV B.SDR P5CA2017072600235Panel · crackedNR 3 PYLON TOP PANEL 611GT INTERIOR VAPOR PANEL OTBD AND AFT CORNER FOUND CRACKED. REPAIRED IAW R1-57-41-11957, REV A.SDR P5CA2017072600236Panel · crackedLT PYLON TOP PANEL 511GT INTERIOR VAPOR PANEL OTBD AND AFT CORNER FOUND CRACKED. REPAIRED IAW R1-57-41-11956, REV A.SDR REXA2017072200852Retainer · crackedPYLON PANEL 433BB SEAL RETAINER CRACKED. REMOVED AND REPLACE THE SEAL RETAINER IAW SRM 51-42-06.SDR QXEA2017072000483Fitting · corrodedLEFT NACELLE EMS STRUT A3 ATTACHMENT FITTINGS HAS EVIDENCE OF CORROSION ON THE FWD ATTACHMENT FITTING (IB) AND AFT ATTACHMENT (IB & OB). REMOVED LIGHT SURFACE CORROSION IAW SRM 51-14-00, REPAIR 04. WITHIN LIMITS IAW DWG 85414543, REV C.SDR 2017FA0000286Web · crackedWHILE PERFORMING A STRUCTURAL REPAIR IAW 57-90-10 FOR THE RT NACELLE UPPER NS 80.87 LEADING EDGE RIB. ON REMOVING THE CRACK FROM THE RIB ASSY IAW SRM. A CRACK WAS DISCOVERED IN BEHIND THE RIB ON THE KEELS ON WEB. AFTER REMOVAL OF THE RIB SECTION. CRACK BESDR FDEA201706221750Door · damagedON AIRCRAFT ARRIVAL AT GATE, MX INFORMED CREW THAN THE NR 2 ENGINE PLATFORM FOR ACCESS ON ENGINE WAS OPEN. NO COCKPIT INDICATIONS, NO UNUSUAL FLIGHT CHARACTERISTIC DURING ANY PHASE OF FLIGHT. INSPECTED ALL DAMAGE TO THE NR 2 ENGINE PATIO DOORS AND WORK PLSDR COEA2017062101900Landing · chafedLEFT NACELLE OTBD REBATE LANDING FOR LATERAL PANEL 475AL IS CHAFED. REPAIRED IAW SRAS PCE-1147/17.SDR SCNA20170616094Fastener · looseNR 2 NACELLE, LOWER PANEL 422AB HAS LOOSE AND SHANKED OUT FASTENERS. INSTALLED NEW FASTENERS.SDR SWIA201743472Access Panel · damagedLEFT PYLON LOWER QD ACCESS PANEL 412DB HAD TWO DIVIDERS KNIFE EDGED. REMOVED AND REPLACED THE DIVIDERS IAW SRM.SDR SWIA201743471Access Panel · damagedRT ENGINE LOWER PYLON QD ACCESS PANEL 422BB TWO DIVIDERS ARE KNIFE EDGED. REMOVED AND REPLACED THE DIVIDERS IAW SRM.SDR SWIA201743434Structure · dentedINLET COWL OF RIGHT ENGINE INNER BARREL HAS NUMEROUSE DENTS. (C-CHECK) RO: 06/29/2017 REPAIRED 7 DENTS IN RH INLET ACOUSTIC INNER PANEL IAW SRM.SDR UIEA2017060800963Latch · corrodedNR 2 ENGINE, FAN COWL LATCHES CORRODED. THE LATCHES WERE CLEANED IAW MM 20-30-03.SDR UIEA2017060800965Seal · tornNR 2 ENGINE, RT FAN COWL HAS A TORN SEAL. THE FAN COWL ASSY WAS REPLACED IAW MM 71-11-04.SDR UIEA2017060800967Seal · tornNR 2 ENGINE RT FAN COWL HAD A TORN SEAL. THE SEAL REPLACED IAW MM 71-11-04.SDR UIEA2017060800973Rub Strip · looseNR 2 ENGINE INLET COWL AFT BULKHEAD RUBSTRIP HAS RIVETS MISSING AT 6 O'CLOCK POSITION. REPLACED THE RIVETS IAW MM 71-11-04.SDR UIEA2017060800981Bolt · missingNR 2 AND 1 ENGINES FAN COWLS SLING BOLTS MISSING. FAN COWLS MISSING SLING BOLTS REPLACED IAW MM 20-11-00.SDR UIEA2017060800982Bushing · wornNR 2 ENGINE, LT CORE COWL SUPPORT BOLT HAVE PLAY. THE BRACKET BUSHING & BOLTS REPLACED IAW AMM 71-11-11.SDR UIEA2017041700600Seal · crackedNR 2 ENGINE, LT CORE COWL UPPER AFT SPRING SEAL FOUND CRACKED. THE SPRING SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042000616Plate · wornNR 1 ENGINE, RT CORE COWL RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042000617Rivet · looseNR 1 ENGINE, LT CORE COWL EXTERIOR UPPER FWD AREA FOUND RIVET LOOSE. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042000620Plate · wornNR 2 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR FOUND TWO STRIKER PLATES WORN. THE STRIKER PLATES WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042400628Seal · wornNR 1 ENGINE, LT CORE COWL FLIPPER DOOR SEAL FOUND WORN. THE DOOR SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042400629Angle · crackedNR 1 ENGINE, LT CORE COWL INTERIOR AFT UPPER AREA ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042400631Seal · wornNR 1 ENGINE, LT CORE COWL FWD UPPER SEAL FOUND WORN. SEAL REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042400632Rub Strip · looseNR 2 ENGINE RT CORE COWL UPPER AFT AREA FOUND RUB STRIP WITH LOOSE RIVET. THE RUB STRIP RIVETS REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017042800670Plate · wornNR 2 ENGINE LT CORE COWL INTERIOR AREA 5TH AND 6TH SUPPORT FRAME, SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017050200690Frame · chafedNR 1 ENGINE RT CORE COWL LOWER AFT HAT FRAME FOUND CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017050800730Bracket · wornNR 1 ENGINE LT CORE COWL FWD UPPER BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017050900735Rod End · looseNR 2 ENGINE LT CORE COWL HOLD OPEN ROD , ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.SDR UIEA2017050900737Rod End · looseNR 1 ENGINE LT CORE COWL HOLD OPEN ROD, ROD END FOUND LOOSE. THE ROD END WAS REMOVED AND REPLACED IAW SRM 70-50-00, REV 120.SDR UIEA2017050900738Rod End · wornNR 1 ENGINE RT CORE COWL HOLD OPEN ROD, ROD END FOUND WORN. THE ROD END WAS REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.SDR UIEA2017051100769Rub Strip · crackedNR 2 ENGINE LT CORE COWL UPPER AFT RUB STRIP FOUND CRACKED. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017051100770Rub Strip · wornNR 1 ENGINE L/H CORE COWL EXTERIOR FWD RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017051100771Rub Strip · wornNR 2 ENGINE L/H CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIPS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR UIEA2017051100772Rub Strip · wornNR 1 ENGINE RT CORE COWL EXTERIOR AREA RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.SDR SWIA201743536Fairing · debondedLEFT ENGINE UPPER STANG FAIRING IS DISBONDED. INSTALLED A NEW FAIRING IAW SRM.SDR A6WA2017061245046Retainer · crackedSEAL RETAINER CRACKED ON PANEL 422BT. REPAIRED THE SEAL RETAINER IAW SUP 16-363.SDR AALA201706019034Attach Angle · corrodedLEFT ENGINE FAN CASE NOSE COWL ATTACH ANGLE HAS EVIDENCE OF CORROSION AT THE 4 O'CLOCK AND 5'OCLOCK POSITIONS. AIRCRAFT WAS GROUNDED. REMOVED AND REPLACED LEFT ENGINE IAW MCM 71-93-01, 71-95-22, 71-94-45, 71-94-03, AND 71-94-43. OPERATIONAL CHECK GOOD.SDR JR2R20170530198Gusset · crackedRIGHT NOSE COWL INTERNAL UPPER GUSSET CRACKED. REMOVED AND REPLACED THE GUSSETT IAW CMM 71-10-1H.
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