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 AALA202510135698Shackle · wornAIRCRAFT IN BASE MAINTENANCE: LEFT PYLON FORWARD INBOARD ATTACH FITTING SHACKLE WORN AT PYLON RIB 4. REPLACED SHACKLE PER AMM 54-51-17.SDR CALA2025100809800Plate · wornLEFT WING PYLON HYDRAULIC BULKHEAD FITTING PLATE IS WORN. REMOVED AND REPLACED LH WING HYDRAULIC BULKHEAD MOUNTING PLATE I AW A319 SRM 57-21-11-300-005.SDR VNAA20251111006Fairing · damaged1075FH PERM REPAIR - SPEED TAPE APPLIED - RH PYLON TRAILING EDGE FAIRING LOWER PANEL DAMAGE WITHIN 1075 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. RH PYLON TRAILING ESDR AALA202510029025Strut · crackedAIRCRAFT IN BASE MAINTENANCE: FOUND NUMBER 1 ENGINE STRUT PROFILE IN THE 5 O'CLOCK POSITION CRACKED. INSTALLED NEW ENGINE STRUT PROFILE. PER AMM 72-23-02.SDR SWAA2025102219054Web · crackedNUMBER 1 ENGINE INBOARD FAN COWL WEB AFT OF THE OIL SERVICE DOOR CRACKED. REMOVED AND REPLACED WITH TTG8Q00S5H1F.SDR R61A2025101900469Plate · chafed#1 ENGINE INBOARD T/R CENTER THERMAL BLANKET CHAFE PLATE CHAFED. REPAIRED PER REPUBLIC AIRWAYS 170EA-78-31-0004MR_1REV2SDR AALA202510305697Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR AALA202510242711Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURES OF CORROSION ARE: L: 13.000 IN, W: 1.368 IN, D: 0.003. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON IAW A320 SRM 54-51-12-300-002.SDR AALA202510211101Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURES OF CORROSION ARE L=13.386 IN, W= 1.350 IN, D= 0.059 IN. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE BTW STA6793/RIB 4 AND STA7063/RIB 5 ON RH PYLON I.A.W. A319 SRM-54-51-SDR AALA202510216557Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON MEASURES OF CORROSION ARE L= 13.386 IN, W= 1.350 IN, D= 0.059 IN. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE BTW STA6793/RIB 4 AND STA7063/RIB 5 ON LH PYLON I.A.W. A319 SRM-54-51SDR CALA2025092609311Fairing · inflt separationLEFT ENGINE FORWARD THUMBNAIL FAIRING MISSING UPON ARRIVAL. NO OBVIOUS DAMAGE NOTED. REF AMM TASK 05-51-59-202-001 PART DEPARTS THE AIRPLANE INSPECTION.SDR IPXA2025101500061Plate · crackedNR 2 PYLON OTBD SIDE AT RIB 3A HAD 2 CRACKS. REMOVED PLATE PYLON #2 O/B SIDE AT RIB 3A IAW A300-600 SRM 51-40-21. INSTALLED PLATE P\N A5461237120000 PYLON #2 O/B SIDE AT RIB 3A, IAW SRM 51-40-21. AND 54-52-21.SDR IPXA2025101660290Support Frame · crackedFAULT-STR-#1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL FWD SUPPORT FRAME CRACKED. REMOVE SUPPORT FRAME PYLON N.1 PANEL 413BL -ZONE400 IAW A300-600 SRM 51-40-21. ++INSTALLED FRAME SUPPORT WITH THE SAME FASTENER AT -#1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL FWD SDR IPXA2025101660368Support Frame · crackedNR 1 PYLON PANEL 413BL AFT SUPPORT FRAME LH SIDE END WORN THRU. REMOVED AFT SUPPORT FRAME LH SIDE #1 PYLON-ZONE400 IAW SRM 51-40-21. INSTALLED FRAME SUPPORT WITH THE SAME FASTENER AT #1 PYLON-ZONE400: NO.1 PYLON PANEL 413BL AFT IAW A300-600 SRM 51-40-21.SDR 2025FA0000657Inlet Screen · corrodedDISCOVERED GALVANIC CORROSION COMMON TO THE ENGINE SHREDDER SCREEN PLATE (P/N 101-910049-107) ON THE LOWER AFT ENGINE COWLING WHERE THE CRES SHREDDER SCREEN IS SECURED. NO BARRIER APPLIED (I.E. ALODYNE PRIMER, OR SEALER) BETWEEN THE DISSIMILAR METEALS. THE CORSDR EE4Y2025091723167Heat Shield · misrepairedDURING THE STRUCTURE INSPECTION, AN EXISTING REPAIR WAS FOUND INSTALLED WITHOUT RECORDS AT RH ENGINE PYLON HEAT SHIELD BAY #8. DUE TO THIS FACT, THE REPAIR WAS REMOVED. THIS CONDITION WAS REPORTED AND REPAIRED IAW ETD2025-190-926307 DTD AUG 08 2025 AND DOCUMENSDR SWAA2025110415026Inlet · pulledPULLED THROUGH FASTENERS 2 O' CLOCK POSITION ON RIGHT INLET COWL OUTER LIP SKIN. REMOVED AND REPLACED RT INLET COWL OUTER LIP SKIN IAW SRM 54-10-01-1A-2 AND SRM 51-40-02. ACCOMPLISHED NDI INSPECTION IAW NDTM PART 6; 51-00-00. REMOVED AND REPLACED NR 2 ENGISDR CALA2025091708996Web · damagedNR 1 ENGINE TOP OF PYLON HYDRAULIC LINE BRACKET WORE INTO BOW TIE STRAP ON TOP OF PYLON. REPAIRED UPPER PLYLON WEB REF ECRA 5450-03044.SDR DALA2025091506785Fitting · corrodedLEFT PYLON SPIGOT-RECEPTACLE FITTING CORRODED. REPLACED THE LOWER SPIGOT FITTING IAW SRM TASK 54-51-12-300- 001. (1198774).SDR DALA2025091506784Fitting · corrodedRIGHT PYLON SPIGOT-RECEPTACLE FITTING CORRODED. REPLACED LOWER SPIGOT FITTING IAW SRM TASK 54-51-12-300- 001. (1198763).SDR DALA2025091506767Spar · crackedPERFORMED OPEN HOLE INSPECTION ON THE FORWARD UPPER SPAR HIDDEN PORTION OF CHORD,FOUND 01 EA CRACK ON THE FASTENER HOLE ON THE INBORD UPPER SPAR AT NSTA221.25, THE CRACK FASTENER HOLE ON LH PYLON UPPER SPAR AT NSTA 221.25 REPAIRED AS PER PRI 582037-14 REV 0 (SDR DALA2025091306744Drag Fitting · damagedDURING DVI OF NR 1 PYLON DRAG FTG FASTENER HOLES 1-10 FOUND HOLE 2 HAS DAMAGE AND REQUIRES REAMED. REPLACED NBR 1 PYLON DRAG FITTING AND OVERSIZED HOLES PER ER/A 628602-14AD. (LP 1195915)SDR DALA2025091306743Drag Fitting · damagedDURING DVI OF NR 1 PYLON DRAG FTG FASTENER HOLES 1-10 FOUND HOLE 4 HAS DAMAGE AND REQUIRES REAMED. NR 1 PYLON DRAG FITTING FASTENER HOLE #4 WAS REAMED TO 2ND OVERSIZE .5938. HFEC HOLE SCAN WAS COMPLETED WITH NO DEFECTS NOTED. REAMED HOLE IAW B757-200 SRM 51-SDR COEA2025091108757Bracket · gougedDAMAGE FOUND ON THE LEFT ENGINE INBOARD AFT FIREWALL BEHIND ICE VANE ACT REAR BRACKET ASSY. MAINTENANCE INSPECTED AND APPLIED SURFACE TREATMENT PER SRM.SDR AALA202510301205Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 6. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR AALA202510068077Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON MEASURES ARE L:13.380 INCH, W: 1.328 INCH, D= 0.005INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE LOC. ON RH PYLON IAW A320 SRM 54-51-12-300-002.SDR AALA202509268562Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE, CORROSION ON UPPER BOLT AT AFT ATTACH FITTING ON LT PYLON L=0.017 INCH, W=0.033, INCH AND D=0.011 INCH. MAINTENANCE REPLACED BOLT.SDR FDEA202509071640Fitting · crackedWHILE ACCOMPLISHING F-5730-E034006 P13 OPEN HOLE INSPECTION OF THE #1 ENGINE DRAG LINK FITTING HOLE #13 HAS CRACKIN SKIN WORK ACCOMPLISHED ON FINAL EA 3F-5730-T0384587 PT1 REV DATE SEP 06, 2025, MAJOR REPAIR WINGS-PLATES & SKINS-LH WINGS, UPPER SKIN @ DRAGSDR FDEA202509071639Fitting · crackedWHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSPECTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #4 HAS CRACK IN FITTING LAYER. WORK ACCOMPLISHED ON FINAL EA # F-5730-T0384448 PT1 REV DATE SEP 06, 2025, WINGS- PLATES AND SKINS-RH WING, UPPER SKIN AT DRAGSDR FDEA202509071638Fitting · crackedWHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSEPCTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #2 HAS CRACKED IN SKIN. WORK ACCOMPLISHED ON FINAL EA #F-5730-T0384448 PT1 MAJOR REPAIR, WINGS-PLATES & SKINS-RH WING UPPER SKIN @ DRAG FITTING CRACK REPAIRSDR FDEA202509071637Fitting · crackedWHILE ACCOMPLISHING F-5730-E034006 P14 OPEN HOLE INSPECTION OF THE #2 ENGINE DRAG LINK FITTING HOLE #8 HAS CRACKIN SKIN/FITTING. WORK ACCOMPLISHED ON FINAL EA#F-5730-T0384448 PT1 REV DATE SEP 06, 2025, WINGS-PLATES AND SKINS-RH WING, UPPER SKIN AT DRAG FITSDR EE4Y2025090423050Rib · wornENGINE #1 PYLON ACCESS PANEL 431CL O/B SUPPORT STRUCTURE WITH WEAR, THE RIB ASSY P/N: 116A5502-5 AND P/N: 116A5502-6 MUST BE FABRICATED PER THE APPLICABLE DWG116A5502 INSTRUCTIONS AND BCS COO-COO-25-0019-01B SMAL REQUESTED. HOWEVER, COOPESA DO NOTHAVE THE CAPASDR EE4Y2025090423049Rib · wornRIB ASSY P/N: 116A5502-5 AND P/N: 116A5502-6 MUST BE FABRICATED PER THE APPLICABLE DWG 116A5502 INSTRUCTIONS AND BCS COO-COO-25-0019-01B SMAL REQUESTED. HOWEVER, COOPESA DO NOT HAVE THE CAPABILITIES TO COMPLY WITH THE CONVERSION COATING APPLICATION BY IMMERSIOSDR EE4Y2025090423046Fan Cowl · damagedDURING THE ACCOMPLISHMENT OF 737-70-812-02_P1-OP-UP-ENG NAC TASK CARD, IT WAS FOUND THE ENGINE #2, O/B FAN COWL P/N: 314-2200-18 BR, S/N: 9112001, WITH ELONGATED HOLES (2EA). COLLINS WAS CONTACTED ASKING FOR REPAIR INSTRUCTIONS AND FINAL APPROVAL. THE CONDITIOSDR DALA2025090106446Fitting · corrodedCORROSION ON BORE SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001 AND AS PER A319 SRM 54-51-12-283-001. (1175071).SDR DALA2025090106450Sleeve · crackedNICKS SLEEVE ON FWD SHACKLES ON LH PYLON. REPLACED SLEEVE ON FWD SHACKLES ON LH PYLON (1 EA) AS PER A320 FAM IPC 54-51-17-01. (1171788).SDR DALA2025090106449Sleeve · crackedSHIP 3152 CRACK SLEEVE UPPER POSITION AFT SHACKLES ON LH PYLON. CORRECTIVE ACTION: REPLACED SLEEVE UPPER POSITION AFT SHACKLES ON LH PYLON (1 EA) AS PER A320 FAM IPC 54-51-17-01. (1171780).SDR DALA2025090106439Fitting · corrodedCORROSION ON BORE SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-283-001, A319 SRM 54-51-12-300-001 AND A319 SRM 51-44- 11-801. (1171802).SDR VNAA202508280013Beam · gougedRIGHT UPPER C-DUCT INBOARD HINGE BEAM LUGS HAVE GOUGE / CHAFE DAMAGE. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-54-22-114 REV: -- DATED: 2025-07-01- REPAIR FOR DAMAGED BOLT HOLE AND BLENDED CHAFE DAMAGE TO RH UPPER THRUST REVERSER HINGE BEAM LUGS. REFERSDR FDEA202508281561Strut · corrodedENGINE #1 I/B NACELLE STRUT INTERNAL STRUCTURE AT APROX PPSTA 140.0 HAS CORROSION ON SIDE SKIN DISCRIPANCY WAS ACCOMPLISHED ON NR N00271.SDR HYIA20250829001Fitting · crackedDURING LIGHTED BORESCOPE INSPECTION (TEXTRON MEL54-02R3) TO SATISFY THE REQUIREMENT OF AD 2017-10-09, A CRACK WAS IDENTIFIED ON THE OUTBOARD SIDE OF THE LEFT HAND INBOARD NACELLE FITTING ( OEM: 5292029-21). THIS CRACK MEASURES APPROXIMATELY .287 INCHES LONG ANSDR NACA2025082300001Clamp · damagedNUMBER 1 ENGINE IDG CABLE HARNESS CLAMPS MISSING RUBBER INSULATORS (2 EA) AT APPROX 7 O'CLOCK POSITION. (RESOLVED ON W/O: 128197 TASKCARD: N/R-00048. REMOVED AND REPLACED # 1 ENG IDG CABLE HARNESS CLAMPS (2 EA) AT APPROX. 7 O'CLOCK POSITION IAW AMM SUBTASK 70SDR ABXA20250823188Panel · damagedDURING THE C-6 MAINTENANCE CHECK, THE NR 2 ENGINE PYLON PANEL ASSEMBLY WAS FOUND TO BE DAMAGED BEYOND REPAIR. MAINTENANCE FABRICATED A NEW PANEL. ACCORDING TO BAC DWG 313T2381 REQUIREMENTS, THE PIECES MUST BE PHOSPHORIC ANODIZED (PAA) AND PRIMED WITH BMS5-13SDR CALA2025082508087Rivet · missingSERVICE CHECK EXTERIOR WALK-AROUND PROCEDURE - 2, MISSING RIVETS ON CNA T/E, 12 CLOCK POSITION OF FWD ROW ON INNER SKIN SIDE. .NO OTHER RIVETS FELT OR LOOK LOOSE. REPLACED THE CNA AS PER EC/RA: 7811-01400 STEP: G.1. OKAY FOR 78-DIP FOR ENG 1 CNA TRAILING ESDR AALA202508259781Latch · wornAIRCRAFT WAS GROUNDED: AN EMERGENCY WAS DECLARED AND THE AIRCRAFT RETURNED TO ORD DUE TO THE FLIGHT CREW REPORTING THAT WHILE CLIMBING THRU FL250 THEY FELT AIRFRAME VIBRATION THAT LASTED ABOUT 20-30 SECONDS THAT COULD BE FELT ON THE RUDDER PEDALS. VIBRATION OCSDR NI6R202508200065Seal · leakingENROUTE TO THE BEULAH INCIDENT, APPROXIMATELY 30 MILES EAST OF HIF, THE PYLON 3 OVHT LIGHT ILLUMINATED ON THE MWP. THE ENGINES WERE SET TO CLIMB THRUST OF 800 TGT WHEN THE LIGHT CAME ON. WE COMPLETED THE QRH PROCEDURE FOR PYLON OVERHEAT AND TURNED TOWARD THE NSDR DALA2025082006234Panel · erodedNUMBER 1 ENGINE PYLON PANEL 414FR HAS EROSION DAMAGE. REPAIRED PER ER/A 628632-14. (7744524)SDR IXXA20250909003Attach Angle · cracked#2 PYLON, AFT FAIRING SUPPORT BULKHEAD ATTACH ANGLE IS CRACKED I/BSDR IXX2025F00020Shear Tie · cracked#2 PYLON, UNDER DOOR 447BR FWD SIDE BELOW FITTING, SHEAR TIE IS CRACKEDSDR SWAA2025090804969Skin · crackedCRACK ON INLET COWL ENGINE 1 AROUND 9 O CLOCK. FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00S712K;[02] FAULT RESOLVED ON OTHER FAULT SEE TTG8Q00S712K
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