JASC 5410
Service difficulty reports · 4,110
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 IPXA2026022687780Bracket · crackedFAULT - CRACK - BRACKET, NO.1 PYLON HYDRAULIC RESERVOIR VENT TUBE AT CENTER AREA. (REPLACE). FABRICATE BRACKET (P/N:313T2380-836) PER BOEING DWG NO.:313T2380 SH 105 REV."-";PL 313T2380-836 REV."A" AND ORIGINAL PART AS A SAMPLE I.A.W GMM-MTX CH 9.08 REV: 14 RESDR SWIA2026070676520Beam · chafedRIGHT ENGINE LOWER C DUCT, THE INBD INNER BEAM ARE CHAFED, WHERE IT MEETS THE FIRE SEAL. BLENDED CHAFE ON RT ENGINE LOWER C DUCT INBD INNER BEAM IAW SRM 51-12-00-001-001-A01L 16. NO DAMAGE ALLOWED IN THIS AREA. REPAIRED PER REO 690-54-22-122 REV--. SEE CONTSDR SWAA2026021770829Fan Cowl · crackedNUMBER 2 ENGINE INBD FAN COWL CRACKED ON FORWARD AND AFT FRAMES. REMOVED AND REPLACE NR 2 ENG. INBD COWLING IAW MM 71-11-04SDR SWAA2026021770727Fairing · crackedNUMBER 2 ENGINE PYLON, AFT FAIRING PLUME SUPPRESSOR CRACKED. PARTIALLY LOCATED AND DRILLED REPAIR STRAPS IAW SRM 54-50-70-2R-7. REPAIRED IAW SRM 54-50-70-2R-7, REPAIR 7.SDR SWAA2026021770998Fan Cowl · crackedNR 2 ENGINE INBD FAN COWL CRACKED ON FWD & AFT FRAMES. REMOVED AND REPLACED NR 2 ENG. INBD COWLING IAW MM 71-11-04, ON TASK TTG8Q01AF2EY.SDR IXXA202602164011Access Door · unsecurePANEL 195EL OPENED IN FLIGHT. RESECURED PANEL 195EL IN ACCORDANCE WITH BOEING SERVICE BULLETIN 767-25A0275.SDR ABXA20260213065Door · missingDURING MAINTENANCE INSPECTION, FOUND NR 2 ENGINE OTBD PYLON PANEL MISSING, 446BR. MAINTENANCE DEFERRED IAW CDL 54-53-2. PLACARDS INSTALLED. REDUCE TAKEOFF AND LANDING PERFORMANCE BY 600 LB. (272 KG) ENROUTE CLIMB BY 1400 LB. (635 KG) NO MX DEACTIVATION PROCEDSDR CALA2026022314023Plate · wornLEFT PYLON AT LOWER RIB 5 SPAR AND CHAFE STRIP IS WORN. LEFT PYLON LOWER RIB 5 SPAR CHAFED WAS BLENDED PER SRM 54-51-12-283-003, AREA OF CHAFE IS 1 INCH FWD OF FASTENER ROW AND 6 INCHES FROM INBD EDGE. POST BLENDING AREA MEASURES: D=0.010, W-0.500, L=0.250.SDR HNAA2026030400195Bracket · crackedLEFT PYLON FWD AND AFT PRECOOLER STUCTURE BRACKETS CRACKED. RAR BRACKETS IAW SRM 51-40-02SDR VNAA202602090018Landing · bentLH PYLON LANDING FOR PANEL 412DT IS BENT. MM670-37123-011 DOUBLERSDR HNAA2026022000145Seal · crackedNR 4 SPRING SEAL CRACKED OM RT UPPER COWL. R & R SPRING SEAL IAW SRM 51-40-02.SDR HNAA2026021900139Seal · crackedSPRING SEAL ON LT LWR COWL CRACKED. R & R SPRING SEAL IAW SRM 51-40-02.SDR IPXA2026022899828Beam · crackedCRACKED BEAM, NR 1 PYLON AFT FAIRING INNER INBD SIDE LWR BEAM. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 130, SB 767-54-0109, REV 1, DWG 313T2303, SHT 25, REV A, DWG 313T2303, SHT 27, REV A, DWG 313T2303, SHT 28, REV A, DWG 313T2303, SHT 29, REV A, SDR QXEA2026020900026Fairing · looseFLIGHT 2044, NR 2 ENGINE INBD, FWD FAIRING NOTED PARTIALLY UNSECURED IN FLIGHT. LANDING UNEVENTFUL. FOUND ON POST FLIGHT WALKAROUND. REMOVED FROM SERVICE. REMOVED PANEL 421AL, PERFORMED GVI OF PANEL AND SURROUNDING AREA. NO DAMAGE NOTED. INSTALLED PANEL 421ALSDR CALA2026020913632Hinge Fitting · gougedNR 2 ENG OTBD FAN COWL NR 3 HINGE HAS GOUGE FWD SIDE OF FITTING FROM CONTACT WITH ANTI ICE DUCT V-BAND CLAMP IAW AAR LCQ NR 9294106/3 8106. REMOVED GOUGES ON NR 2 ENG OTBD FAN COWL NR 3 HINGE FITTING FWD SIDE IAW SRM 54-02-00 REPAIR 012 TO A SMOOTH CONTOUR FISDR DALA2026021100978Strut · crackedFOUND RT STRUT FORWARD MID SPAR BEWTEEN STA 221 AND STA 237 CUTOUT CRACKED. REPAIRED AS PER PRI 631935-14. (1434806)SDR UIEA2026020500043Panel · missingLOWER EXHAUST PANEL MISSING ON THE #3 ENG INLET COWL, IAW AMM 05-51-58 PARTS DEPART THE AIRPLANE INSPECTED, NO ADDITIONAL DAMAGE FOUND. PERFORM EA-1971A256 PER NON-MEL 247237 & 247238 (SEE NEXT LP FOR DEFERRAL). TRANSFER TO DMI 247232 IAW MEL 30-21-01A CAT CSDR SWAA2026030266699Bracket · crackedNUMBER 2 ENGINE OTBD FAN COWL VERTICAL BRACKET, JUST BEHIND OIL SERVICE DOOR, CRACKED. NR 2 ENGINE FAN COWL REPLACED ON TTG8Q00S5HD9.SDR YENA2026020400122Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON SPIGOT LOWER FITTING ON LH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00037) REF AEROMAN NR 2025-682782 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON LH PYLON IAW SRM 54-51-283-002, SRM 51-44-11-801, SDR YENA2026020400121Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION IN THE SPIGOT LOWER FITTING ON RH PYLON; (RESOLVED ON W/O: 1420259 TASKCARD: NR-00038) REF AEROMAN NR 2025-682784 WP 2025-413/1. REMOVED AND REPLACED THE SPIGOT LOWER FITTING ON RHPYLON IAW SRM 54-51-283-002, SRM 51-44-11-80SDR DALA2026021000962Fitting · corrodedNR 1 ENGINE ATTACHMENT SPIGOT FITTING OUT OF LIMITS, LEVEL 2 CORROSION. REPLACED NR 1 PYLON LOWER SPIGOT FITTING IAW A319 SRM TASK 54-51-12-300-001. (LP 1443400)SDR CALA2026020213485Drain · missingON WALK AROUND, FOUND NR 2 ENGINE AFT PYLON CLAMP BLOCK MISSING WITH DAMAGE TO AFT LOWER PYLON LINE & SUPPORT ASSY INSPECTED NR 2 ENGINE AFT PYLON AND FOUND CLAMP BLOCK, SEVERE CHAFING TO LOWER PYLON DRAIN LINE & ELONGNATED DAMAGED TO SUPPORT ASSY. REF IPC 54SDR SCNA20260219090Fitting · damagedTWO ELONGATED HOLES ON THE NR 1 COWLING HINGE FITTING INBD & OTBD, NAC STA 158.1230 REPAIRED IAW ECTC ENG-54SCA-11809, & ETI-737-26-025, REV 6.SDR VNAA202601280002Cowling · damagedTEMPORARY REPAIR TO THE LH LOWER FORWARD CORE COWL INBOARD LOWER Z-DISHING AND FIRE SHIELD THE FOLLOWING TEMPORARY REPAIR IS VALID FOR A MAXIMUM OF 8000 FLIGHT HOURS FROM THE TIME OF INCORPORATION OF THIS REO AT REV -. LEFT LOWER FORWARD CORE COWL INBD LOWERSDR IXXA20260127001Frame · crackedNR 1 PYLON AFT TORQUE BOX OB VERTICAL FRAME CRACKED STA 285.45SDR VNAA20260329035Fire Seal · tornTORN FIRE SEAL OF AFT CORE COWL ALSO BENT SEAL RETAINER (7 O' CLOCK) AT LH ENGINE. FIRE SEAL OF AFT CORE COWL WAS REPLACED PER SRM 51-42-10-001-001-A01 AND SRM 51-42-13-001-001-A01, SEAL RETAINER (7 O' CLOCK) AT LT ENGINE WAS CONFORMED PER SRM 51-24-16-001-00SDR SWAA2026030264282Cowling · pulledNR 2 ENGINE OUTER LIP SKIN FOUR FASTENERS LOOSE & PULLED. REMOVED AND REPLACED THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01 AND TASK TTG8Q01A4JPY.SDR DALA2026012900702Receptacle · corrodedCORROSION BORE SPIGOT FITTING RECEPTACLE ON RT PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RT PYLON IAW SRM 54-51-12-300-001, & SRM 54-51-12-283-001. FOUND BEYOND LIMITS, MEASUREMENT OF CORRODED AREA: D: 0.0042 INCH & OF DIAMETER IS 4.348 INCH. (LP: 141796SDR YENA2026012600069Access Door · openFLT 995, MCO- SJO. AIRCRAFT DIVERTED TO FLL. PASSENGER RECORDED A VIDEO OF OPEN LOWER PANEL ON IMBOARD SIDE OF #1 ENGINE DURING FLIGHT. N606-FLT-MCO-SJO-DIVERSION THE A/C DIVERTED TO FLL, THE CREW REPORTED A PANEL WAS OPEN ON THE NBR 1 ENG AND SEEMED TO BE FSDR JR2R20260124397Beam · chafedNR 2 ENGINE OTBD TRANSCOWL LOWER BEAM STRUCTURE CHAFED. REPAIRED PER ETD.SDR VNAA20260329008Bonding Plate · missingMISSING SHIM (1EA) ON PYLON FS 1126.00 (UPPER SKIN) AT LH ENGINE. NEW SHIM (1EA) ON PYLON FS 1126.00 (UPPER SKIN) AT LH ENGINE WAS INSTALLED PER CRJ900 SRM 51-42-10-001-001-A01SDR FDEA202601190068Skin · corrodedNR 2 ENGINE UPPER NACELLE INTERNAL STRUCTURE OTBD SIDE PPS 134.76 CORRODED. THIS ITEM HAS BEEN ACCOMPLISHED ON EA # F-5430-T0386151 P1 TITTLE: NACELLES/PYLONS- SKIN/PLATES/PANELS- # 2 PYLON O/B SIDE SKIN-EXISTING REPAIR DOUBLER BETWEEN PP STA 174-190, WITHSDR JJBA20260114031Seal · tornRIGHT ENGINE PYLON UPPER FAIRING HAS SEAL TORN. REMOVED AND REPLACED SEAL ON RH ENGINE PYLON UPPER FAIRING.SDR SWAA2026011360923Fan Cowl · crackedAN APPROX 7 INCH CRACK FOUND ON THE NR 2 ENGINE COWLING OTBD, AT THE 4 O`CLOCK POSITION. R & R OTBD NR 2 ENG FAN COWL IAW 71-11-02.SDR DALA2026011500356Receptacle · corrodedENGINE NR 1 PYLON SPIGOT RECPTACLE AND SPIGOT BALL JOINT WITH CORROSION. REPLACED LOWER SPIGOT FITTING OF PYLON NR 1 IAW SRM TASK 54- 51-12-300-001, REV 155, AND REPLACED PYLON SPIGOT BALL JOINT IAW AMM TASK 54-51-41-000-001-A, PARAG 4C, AND TASK 54-51-41-400SDR DALA2026011200258Receptacle · corrodedNR 1 ENGINE PYLON SPIGOT RECPTACLE AND SPIGOT BALL JOINT CORRODED. REPLACED BALL AND RECEPTACLE IAW SRM 54-51-12-300-001 AND AMM 54 -51-41/400. (LP: 1397020)SDR DALA2026011200257Receptacle · corrodedNR 2 ENGINE, PYLON SPIGOT RECEPTACLE AND SPIGOT BALL JOINT CORRODED. REPLACED BALL AND RECEPTACLE IAW SRM 54-51-12-300-001 AND AMM 54 -51-41/400. (LP: 1397017)SDR IPXA2026011335756Web · crackedDURING REMOVAL OF #2 ENGINE INLET COWL AFT BLKHEAD COVER PLATE LH SIDE NEAR AMBIENT PRESS LINE MORE CRAKS FOUND AT UNDERNEATH. INSTALLED NEW WEB I.A.W. A300-600 NACELLE SRM 54-10-00. REVIEWEDSDR AALA202601154284Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. MAINTENANCE PERFORMED PERMANENT REPAIR ON LOWER SPIGOT FITTING LH PYLON IAW A319 SRM 54-51-12-300-002.SDR AALA202601159692Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. MAINTENANCE PERFORMED PERMANENT REPAIR ON LOWER SPIGOT FITTING RH PYLON IAW A319 SRM 54-51-12-300-002.SDR IXXA20260205001Bearing · galledGALLING, LIGHT CORROSION AND GOUGE AROUND BEARING FACESDR SWIA2026010675613Door · dentedADM# N726SK-8479 - 6 O'CLOCK POSITION LT ENGINE COWL FAN DOOR. 6 O"CLOCK POSITION LT ENGINE LOWER COWL FAN DOOR 3 INCH LONG DENT BY 1.5" WIDE. 0.020 DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDASDR AALA202602015622Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR IPXA2026011374486Splice Plate · crackedNR 2 ENGINE INLET COWL AFT BULKHEAD LH SIDE HAS A CRACK NEAR AMBIENT PRESSURE SENSOR LINE. INSTALLED NEW SPLICE PLATE I.A.W. A300-600 NACELLE SRM 54-10-00. REVIEWEDSDR SWIA2026030975454Fan Cowl · dentedLH ENGINE LOWER FAN COWL DOOR HAS SEVERAL EXTERIOR SKIN DENTS (MARKED) (C-CHECK RO 03/07/2026)REPAIRED LH ENGINE LOWER DAN COWL DOOR DENTS IAW DWG CN622-0201 REV. -L, CRJ550 SRM 51-42-06-001-001-A01 AND CRJ550 SRM 51-42-10-001-001-A01 REV. 38 - JUL 25/2020 ASDR AALA202602096527Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON SPIGOT FITTING RECEPTACLE. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR DALA2026010500058Shim · migratedSHIM MIGRATION INSIDE NR 1 PYLON SEEN THROUGH ACCESS PANEL 434AL AT LOWER INTERNAL BULKHEAD TO ENGINE MOUNT SURFACES BELOW BARREL NUTS AT I/B AND O/B SIDES. FABRICATED AND INSTALLED NEW SHIMS AT 191.861 BULKHEAD LOWER SURFACE IAW DWG 311N3160-6, SRM 51-40-0SDR AALA202601177014Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT SLEEVE OF RIGHT PYLON (L=7.570 IN). MAINTENANCE REPLACED SPIGOT SLEEVE ON RH PYLON IAW AMM 57-26-12-000-002-A AND AMM 57-26-12-400-002-A.SDR GTIA2025121839206Nut · corrodedREFERENCE T.C. AOT A57N025-25. FOUND CORROSION ON NR 1 ENG PYLON SPIGOT FITTING NUT.SDR GTIA2025121839203Nut · corrodedREFERENCE TC AOT A57N025-25, FOUND CORROSION ON NR 2 PYLON SPIGOT FITTING NUT. R & R PYLON SPIGOT NUT IAW AMM 57-26-12.
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