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 IPXA2026032610990Clamp · damagedDAMAGED CLAMP, NR.2 PYLON AFT FAIRING DOOR SUPPORT ROD. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T2303, SH 135, REV -.SDR IPXA2026032611804Plate · crackedCRACKED PLATE, NR 1 ENG LT CORE COWL INNER AFT LWR SIDE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-23, REV 47.SDR IPXA2026040197859Duct · chafedCHAFED DUCT, NR 2 ENG R/H CORE COWL PRECOOLER OULET DUCT (REPLACE). INSTALL PRECOOLER DUCT FOR ACCESS I.A.W SRM 51-40-02-0G REV.94 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV. 50. C/W REVIEWSDR ABXA20260320122Cowl Door · missingDURING MAINTENANCE INSPECTION, FOUND PANEL 446AL ON #2 ENG I/B PYLON MISSING. REPLACED PANEL 446AL IAW AMM 54-53-01. THIS CLOSES DI# 71620. PLACARD REMOVED. NO MX ACTIONS TO C/W REF LP 39398-16/2. AIRCRAFT RETURNED TO SERIVCE.SDR AALA202603201358Cowl Door · inflt separationAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETRUNED TO MIA DUE TO THE FLIGHT CREW REPORTING THAT DURING CLIMB OUT PASSENGERS AND FLIGHT ATTENDANTS REPORTED A COWLING DEPARTED THE AIRCRAFT ON TAKEOFF. THE AIRCRAFT LANDED SAFELY AT MIASDR AALA202605083174Hinge Fitting · wornAIRCRAFT IN BASE MAINTENANCE: #1 ENGINE INBOARD FAN COWL FORWARD HINGE FITTING MOUNTED ON THE PYLON IS WORN ALLOWING BUSHING HAS MIGRATED. MAINTENANCE REPLACED THE HINGE FITTING PER AMM 71-13-11.SDR IPXA2026032331814Clamp · brokenBROKEN CLAMP , NR 1 PYLON AFT FAIRING INNER HOLD OPEN ROD SUPPORT BRACKET AREA. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, & DWG 313T3349, SH 2, REV B.SDR IPXA2026032332844Beam · crackedCRACKED BEAM , NR 2 NACELLE AFT LOWER FAIRING RT UPPER UNDER THE 4TH LATCH FITTING AT NAC STA 373. INSTALLED A NEW BEAM IAW SRM 51-40-02-0G, REV 94 AND DWG 313T2380, SH. 10, REV K, 313T2380, SH 9, REV G, 313T2380, SH 22, REV F, & SERVICE BULLENTIN 767-54-010SDR IPXA2026032092047Adapter · chafedCRACKED BRACKET , NR 2 ENGINE LT CORE COWL HOLD OPEN ROD STOW ADAPTER. INSTALL A NEW BRACKET I.A.W SRM 51-40-02-0G REV.94 AND CMM IPL 71-13-23 REV 47.SDR IPXA2026032091714Clamp · crackedCRACKED CLAMP, NR 2 PYLON AFT FAIRING DOOR HOLD OPEN SUPPORT ROD STOW CLAMP. REMOVED DAMAGE CLAMP I.A.W SRM 51-40-02-0G REV.94. INSTALLED A NEW CLAMP IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3349, SH 2, REV B.SDR SWAA2026041385063Cowling · corrodedON THE NR 2 OTBD FAN COWL; THE FWD HOLD OPEN ROD STOWAGE POINT HAS EVIDENCE OF CORROSION AROUND THE CENTER ATTACH POINT AND THE CENTER POINT SPINS. REMOVED AND REPLACED #2 O/B FAN COWL PER MM 71-11-02. REFERENCE TTG8Q01BDEQR FOR PARTS INFORMATION AND TTG8Q01SDR ABXA20260315110Door · missingDURING MAINTENANCE INSPECTION, FOUND RIGHT ENG OUTBD NACELLE STRUT ACCESS DOOR MISSING (446AR). MAINTENANCE DEFERRED MISSING NACELLE STRUT DOOR PER CDL 54-53-2 MX ACTIONS C/W PLACARD INSTALLED MBCB C-CHECK, FOR INSPECTION SEE LP 39404-50/1. A/C RETURNED TOSDR SWIA2026031477514Anchor Nut · mechanic errorMISSED DRILLED ANCHOR NUT ON LH ENGINE UPPR FWD TORQUE BOX BEAM FAN COWL ATTACHMENT HN00301025 MARKED HN00301025 C-CHECK RO 09302026FABRICATED AND INSTALLED REPAIR FITTING TO THE LH ENGINE UPPER TRUST REVERSER REF REO 670-54-22-166 REV -- 2026-07-22 AND REO 6SDR SWIA2026031477510Skin · puncturedPUNCTURE DAMAGE ON UPPER FAN COWL DOOR. REPAIRED DAMAGE ON UPPER FAN COWL DOOR OUTER SKIN IAW REO 670-54-14-1342, REV -.SDR ABXA20260314109Door · missingDURIING MAINTENANCE INSPECTION, FOUND LT ENG INBOARD NACELLE STRUT ACCESS DOOR MISSING (436AR). MAINTENANCE DEFERRED L ENG INBOARD NACELLE STRUT ACCESS DOOR IAW CDL 54-53-2. MX PROCEDURES C/W. PLACARDS INSTALLED. DOOR REMOVED. MBCB NEXT C-CHECK. C/W VISUAL INSDR SCNA20260317127Cowl Door · unlatchedABNORMAL ACFT VIBRATION AFTER TAKEOFF. ACFT REQUIRED SUBSTANTIAL RT AILERON TO MAINTAIN WINGS LEVEL. RETURNED TO LAL. POST FLT REVEALED NR 1 ENG COWL UNLATCHED INFLT. ACFT INSPECTED & REPAIRED EXCEPT FOR NR 42 & 43. COMPONENTS REPLACED: NR 2 FUEL HOSE, NR 3 HSDR FDEA202603130344Beam · crackedNUMBER 2 PYLON OUTBD SIDE SKIRT BEAM IS CRACKED AT THE AFT NUTPLATE HOLE. MARKED WITH TAPE, 2026-03-13] TECHNICIANS FOUND A CRACK ON THE #2 PYLON FAIRING OUTBD LATCH BEAM NEAR NAC STA 370 (P/N 313T2380- 1190). THERE ARE NO PUBLISHED REPAIRS FOR THIS TYPESDR IPXA2026031646305Door · blownDURING WALK AROUND FOUND A BLOW OUT PANEL DAMAGED ON THE RIGHT ENGINE PYLON R & R STRUT RELIEF AND ACCESS DOOR PER AMM 54-53-01SDR HYIA20260313001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK MEASURES APPROXIMATELY 1.25 INCHES IN LENGTH, AND BEGINS AT THE TOP INBOARD TURBO BRACKET MOUNTING HOLE ON THE AFT FACE OF THE BSDR IXXA20230327001Strut · crackedNR 1 NACELLE STRUT FAIRING, I/B U FRAME CRACKED. XTREME AVIATION NON ROUTINE 856SDR VNAA202604110024Cowling · crackedCRACK OUTER SKIN OF RH AFT CORE COWL, PYLON INTERFACE AREA. SKIN OF RH AFT CORE COWL, PYLON INTERFACE AREA WAS REPAIRED PER REO 690-54-13-254 REV. - -SDR IPXA2026031086246Cover · chafedCHAFED COVER, NR 3 ENG R/H CORE COWL INNER AFT LATCH AREA. INSTALL NEW COVER I.A.W SRM 51-40-02-0G REV.106 AND GOODRICH AEROSTRUCTURES CMM IPL 71-13-24 REV.50.SDR IPXA2026031886249Bracket · chafedNR 4 ENG LT CORE COWL HOLD OPEN ROD SUPPORT BRACKET CHAFING. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G REV.106 AND CMM IPL 71-13-23 REV.47SDR IPXA2026031686662Bracket · gougedGOUGED BRACKET, NR 2 ENG RT CORE COWL HOLD- OPEN ROD RECIVER BRACKET. REMOVED DAMAGE BRACKET IAW SRM 51-40-02-0G REV.106. INSTALLED NEW BRACKET IAW SRM 51-40-02-0G ,REV.106 AND CMM IPL 71-13-24 REV.50.SDR IPXA2026031363475Receiver · missingMISSING BUSHING, NR 2 ENGINE LT FAN COWL, LWR MID BRACKET. INSTALLED A NEW RECEIVER ASSY IAW SRM 51-40-02-0G, REV 94, AND CMM IPL 71-13-21 REV.47.SDR CALA2026031114508Acoustic Liner · damagedON WALKAROUND FOUND DAMAGE TO NR 2 ENGINE ACOUSTIC LINER BETWEEN 2 AND 3 O CLOCK POSITION. REMOVED FAN CASE OGV FAIRING PER AMM 72-21-03. REQUIRES INSTALLATION OF THREE OGV FAIRING ASSMEBLY PANELS. SEE PICTURES BELOW. INSTALLED OGV FAIRINGS AT POSITION 8 AND SDR IPXA2026031247725Plate · wornWORN PLATE, NR 1 ENG LT CORE COWL INNER AFT FRAME LOWER PLATE. INSTALLED A NEW PLATE IAW SRM 51-40-02-0G, REV 94, & CMM IPL 71-13-23 REV 47.SDR IPXA2026031247676Hinge · wornWORN HINGE, NR 1 PYLON STRUT PRESSURE RELIEF DOOR 434AR UPPER HINGE. INSTALLED NEW HINGE IAW SRM 51-40-02-0G, REV 94, DWG 311T1064, SHT 1, REV G , & DWG 311T1064, SHT 2, REV E.SDR IPXA2026031329791Rod · wornWORN RECEIVER , NR 1 ENG LT CORE COWL HOLD OPEN ROD. REMOVED DAMAGE RECEIVER IAW SRM 51-40-02-0G REV.94 2.INSTALL NEW RECEIVER IAW SRM 51-40-02-0G REV.94 AND AEROSTRUCTURES CMM IPL 71-13-23 REV.47 3.SDR IXXA202604060011Support Bracket · crackedSTRUT NR 1, LT AT NAC 295.09 SUPPORT BRACKET WITH CRACK. REF XTREME AVIATION NRC 732SDR DALA2026030801579Fitting · damagedENGINE NR 2 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACED ENGINE # 2 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. REPLACED #2 PYLON LOWER SPIGOT FITTIN G IAW A319 SRM TASK 54-51-12-300-001 REV 155 DATED 17 NOV 2SDR DALA2026030801578Fitting · damagedENGINE NR 1 PYLON FOUND SPIGOT LOWER FITTING AND SPIGOT BALL JOINT DAMAGE. REPLACE ENGINE NR 1 PYLON SPIGOT LOWER FITTING AND SPIGOT BALL JOINT IAW SRM 54-51-12. (LP: 1477390)SDR VNAA202604110008Inlet · wornWEAR ON AFT EDGE OF INLET COWL IN SETLEMENT AREA OF FAN COWL 3:00 O' CLOCK POSITION AT LH ENGINE. ON AFT EDGE OF INLET COWL IN SETLEMENT AREA OF FAN COWL 3:00 O' CLOCK POSITION AT LH ENG WAS REPAIRED PER REO 690-54-11-607 REV. - -SDR IPXA2026031784226Angle · crackedNR 1 ENG AFT PYLON FARING SUPPORT ANGLE L BRACKET ON INBD SIDE IS CRACKED. REMOVED BRACKET ON NR 1 ENGINE AFT PYLON FARING IAW SRM 51-40-02. INSTALLED A NEW L ANGLE IAW SRM 51-40-02.SDR IPXA2026030647430Seal · brokenBROKEN - SPRING SEAL, PNL NO. 446CR (REPLACE) 1.REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV.94. INSTALL NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 16 REV.-.SDR CALA2026030314232Structure · crackedLEFT ENGINE NACELLE, FWD TORQUE BOX UPPER SURFACE, AROUND DRAIN HOLE FOUND TWO CRACKS. INTERIM REPAIR ACCOMPLISHED IAW ECRA 5450-03104, PART 1, STEP 1 WITHOUT DEVIATION.SDR CALA2026030314230Structure · crackedNR 2 ENGINE NACELLE, FWD TORQUE BOX UPPER SURFACE INBD SIDE, AROUND DRAIN HOLE FOUND TWO CRACKS, & OTBD SIDE ARROUND DRAIN HOLE FOUND TWO CRACKS. INTERIM REPAIR WAS ACCOMPLISHED IAW ECRA 5450-03106, PART 1, STEP 1, WITHOUT DEVIATION.SDR IPXA2026030633793Seal · brokenBROKEN SPRING SEAL, PNL NO.446CL (REPLACE). REMOVED DAMAGE SEAL I.A.W SRM 51-40-02-0G REV.94 INSTALL NEW SEAL I.A.W SRM 51-40-02-0G REV 94 AND BOEING DWG NO:311T2570 SH 16 REV -.SDR SWAA2026032380585Fastener · shearedRIGHT INLET COWL LIP SKIN HAS SHEARED FASTENERS HEAD AT 2; 3 AND 10 O'CLOCK POSITIONS; MARKED<[01] COMPLETED STEP 1;[02] REMOVED AND REPLACED RH INLET COWL IAW AMM 71-11-01-400-802-F00 LEAK TEST GOOD;[03] VERIFIED CORRECTIVE ACTION 2.;[04] VERIFIED STEPS 2 ANDSDR IPXA2026030612569Seal · brokenBROKEN SEAL , NO. 1 PYLON AFT FAIRING PNL 436CL SPRING SEAL AREA. REMOVED DAMAGE SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 2. INSTALL NEW SEAL STRIP I.A.W SRM 51-40-02-0G REV.94 AND BOEING DWG NO:311T2570 SH 16 REV.- 3. JOB COMPLETEDSDR SWAA2026030274512Cowl Door · pulledNR 2 ENG INLET COWL HAS TWO PULLED THRU FASTENERS AND ONE MISSING FASTENER ON AFT BULKHEAD AT 3 O`CLOCK POSITION VIEWING AFT FACING FWD. R & R THE NR 2 ENGINE INLET COWL IAW AMM 71-11-01.SDR DALA2026022701379Fitting · corrodedCORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001 AND AS PER A319 SRM 54-51-12-283-001 PARAGRAPH 2. FIGURE 001 SHEET 1 AND 2. FOUND BEYOND OUT MEASURED OF LIMITS TOOL USED CALIPER SDR SWIA2026022477507Door · gougedGOUGE ON INTERIOR AND PROTRUDING DENT ON EXTERIOR ON LOWER RT FAN COWL DOOR, 8 O`CLOCK. PERFORMED A CUT OUT OF DAMAGE IAW SRM 54-14-00-201-001-A01, FABRICATED, LOCATED, DRILLED, AND INSTALLED DOUBLER IAW SRM 54-14-00-201-001-A01, SRM 54-14-00-201-001-A01.SDR SWAA2026033074076Strut · crackedNR 1 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 1 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-05, DWG 313A2400, REV A, & DWG 313A2700, REV-.SDR SWAA2026033074077Strut · crackedNUMBER 2 NACELLE AFT FAIRING STRUCTURE CRACKED AT AFT END. REMOVED & REPLACED THE NR 2 NACELLE STRUT AFT FAIRING TRAILING EDGE ASSY IAW SRM 51-40-02, DWG 313A2400, REV A, AND DWG 313A2700, REV-.SDR AALA202603257929Wedge · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT ENGINE AFT STRUT FAIRING TAIL SECTION WEDGE, INBOARD SKIN LOWER SIDE. REPLACED WEDGE PER SRM 54-50-70.SDR SWAA2026022472838Suppressor · crackedNR 2 ENGINE PYLON AFT FAIRING PLUME SUPPRESSOR CRACKED. REPAIRED THE AFT FAIRING PLUME SUPPRESSOR IAW SRM 54-50-70-2R-7.SDR IPXA2026030825078Longeron · damagedNR 2 ENG-PANEL RACK-485AL FWD O/B TOP LONGERON 1ST 2 HOLES HAVE WEAR -109-101-VWV. UPPER LONGERON REMOVED AND REPLACED IAW A300-600, SRM51-40-21-001, SRM 51-72-10-001.SDR IPXA2026022604702Rub Strip · gougedGOUGED WEAR STRIP, NR 2 ENG RT CORE COWL T/E INNER SIDE UPPER PLATE. INSTALLED A NEW WEAR STRIP IAW SRM 51-40-02-0G, REV 94 AND CMM IPL 71-13-24 REV.50.SDR IPXA2026022606029Latch · wornWORN OUT - LATCH 3 EA, NO.1 ENG R/H FAN COWL OIL TANK ACCESS DOOR. (REPLACE). INSTALL NEW LATCH I.A.W SRM 51-40-02-0G REV.94 AND BOEING AIPC 71-11-10-51 REV. 141.
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