JASC 5414

Service difficulty reports · 4,353

Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, 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 = '5414'
  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.

SDR FDEA202610191606Skin · corrodedNR 1ENGINE PYLON OUTB SIDE INTERNAL STRUCTURE SIDE SKIN CORRODED (PP STA 144.55 APROX.)Oct 19, 2026 · N923FD · Boeing 757204SDR JR2R20261015346Skin · chafed419KL HAS CHAFING ON INNER SURFACE.Oct 15, 2026 · N88359 · Emb ERJ170200LRSDR IPXA2026100503114Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 9 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.2", 18.2" FROM L/E, AT 9 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR Sep 30, 2026 · N354UP · Boeing 76734AFSDR IPXA2026100503125Skin · dentedFAULT - DENT - SKIN , NO.1 ENG NOSE COWL INLET AT 3 O'CLOCK POSITION. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.25", 20.5" FROM L/E, AT 3 O'CLOCK ON THE INNER BARREL OF NO.1 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FORSep 30, 2026 · N354UP · Boeing 76734AFSDR IPXA2026100603239Skin · dentedFAULT - DENT - SKIN , NO.2 ENG NOSE COWL INNER BARREL AT 8 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 8.2" FROM T/E, AT 8 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). FILL THE CUT OUT WITH ADHESIVE CURED AT 200°F FOR 1 Sep 30, 2026 · N354UP · Boeing 76734AFSDR IPXA2026100603252Skin · dentedDENTED SKIN , NR 2 ENG NOSE COWL INNER BARREL AT 5 O'CLOCK. CUT OUT THE DAMAGE AND CLEAN, MEASURE THE CUT OUT ( DIA : 0.3", 7" FROM T/E, AT 5 O'CLOCK ON THE INNER BARREL OF NO.2 ENG INLET COWL ). BOND THE SPACER WITH FILM ADHESIVE CURED AT 250°F FOR 2 HOURS Sep 30, 2026 · N354UP · Boeing 76734AFSDR CALA2026092919955Panel · missingNR 2 ENGINE HAS PYLON ACCESS PANEL 446AR MISSING. INSPECTED THE AREA FOR DAMAGE IAW AMM 05-51-59, NO DAMAGE FOUND. CDL 54BE REJECTION REPLACED THE MISSING PANEL IAW AMM 54-53-01-404-007. OK FOR SERVICE.Sep 27, 2026 · N68061 · Boeing 767424ERSDR IPXA2026101934070Skin · crackedPANEL 485AL FWD OUTER ARA, RH SKIN IS CRACKED.Sep 19, 2026 · N146UP · Airbus A300F4622RSDR SWAA2026092353287Skin · crackedNR 2 ENGINE PYLON HEAT SHIELD PLUME SUPPRESSOR SKIN CRACKED. CRACK LOCATION FROM AFT SKIN EDGE 28 INCHES; CRACK STOP FROM LEFT SKIN EDGE 0.500 INCHES. CRACK STOP FROM RIGHT SKIN EDGE 1.500 INCHES SRM 54-50-70-1A-3 CRACKS ARE NOT PERMITTED. ACCOMPLISHED INTSep 19, 2026 · N8749Q · Boeing 7378SDR IPXA2026100102793Panel · crackedPANEL 423BL EXTERNAL SURFACE WITH A CRACK. VERIFIED RECEIVED THE REPAIRED PANEL 423BL BY WELDING ON TRAVELER # T26/1879228, NOTE: THE INSTALLATION WILL BE ACCOMPLISED ON TASKCARD: T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622RSDR IPXA2026100102892Access Panel · crackedPANEL 413BL, EXTERNAL SURFACE WITH A CRACK DOT 53-024. RECEIVED THE REPAIRED PANEL 413BL BY WELDING ON TRAVELER # T26/1879227, NOTE: THE INSTALLASION WILL BE ACCOMPLISED ON TASK CARD T3F18E007EGD6.Sep 17, 2026 · N158UP · Airbus A300F4622RSDR JR2R20260914344Panel · chafedPANEL 429ML SPLICE CHAFED. REPAIRSep 14, 2026 · N88327 · Emb ERJ170200LRSDR JR2R20260914345Panel · chafedPANEL 429ML CHAFED AT SCREW HOLES, INTERNAL. REPAIRSep 14, 2026 · N88327 · Emb ERJ170200LRSDR JR2R20260914338Panel · chafedPANEL 419NR CHAFED AT SCREW HOLES, INTERNAL. REPAIRSep 14, 2026 · N88327 · Emb ERJ170200LRSDR DALA2026100705556Skin · delaminatedNR 2 ENGINE AFT COWL, INSIDE DELAMINATION AT 5 O'CLOCK POSITION. CLEANED AREA AND REPAIRED IAW SRM 54-30-01-2R, PROCEDURE 2, REPAIR 2. (9109242) AIRCRAFT WAS GROUNDEDSep 10, 2026 · N869DN · Boeing 737932ERSDR CALA2026091019359Access Door · missingINSTALLED NEW STRUT ACCESS DOOR ASSEMBLY REF AMM 54-53-01Sep 9, 2026 · N57862 · Boeing 75733NSDR IPXA2026092825914Skin · corroded***MAJOR REPAIR*** FAULT-400-STR- #2 ENGINE NACELLE PYLON STRUT, OUTBD INNER SKIN, FWD OF THE VENT PANEL OPENING HAS CORROSION AT SEAM OF FRAME, MAY BE UNDER THE PREVIOUS REPAIR. DOT 8-002. REMOVED EXISTING REPAIR DOUBLER AND REPAIR FILLER IN STR- #2 ENGINE NASep 7, 2026 · N444UP · Boeing 75724APFSDR IPXA2026091925377Skin · crackedENG 2 PYLON, CRACK AT LOWER T/E WEDGE. INSTALLED PANEL ASSY AT ENG 2 PYLON AT LOWER T/E WEDGE IAW SRM 51-40-02-0G-0.Sep 7, 2026 · N444UP · Boeing 75724APFSDR SWAA2026101409901Access Panel · delaminatedDELAMINATED ACCESS PANEL 444BR ON RT PYLON. REPAIRED THE ACCESS PANEL IAW SRM 51-70-04-2R-10, REPAIR 10.Sep 4, 2026 · N8656B · Boeing 7378H4SDR JR2R20260903326Skin · chafed429NR HAS DAMAGED, OVERSIZED SCREW HOLES ACROSS PANEL & CHAFING ON INNER SURFACE AROUND SCREW HOLES. REPAIRED.Sep 3, 2026 · N89357 · Emb ERJ170200LRSDR JR2R20260903327Skin · chafed419NR HAS DAMAGED, OVERSIZED SCREW HOLES ACROSS PANEL AND CHAFING ON INNER SURFACE AROUND SCREW HOLES. REPAIRED.Sep 3, 2026 · N89357 · Emb ERJ170200LRSDR JR2R20260903329Skin · chafed429ML HAS DAMAGED, OVERSIZED SCREW HOLES ACROSS PANEL & CHAFING ON INNER SURFACE AROUND SCREW HOLES. REPAIRED.Sep 3, 2026 · N89357 · Emb ERJ170200LRSDR SWAA2026092865103Cowling · damagedNR 1 ENGINE INLET COWL LIP SKIN HAVE LOOSE, PULLED, & SMOKING FASTENERS AT THE 3 O'CLOCK (2 EA), 5 O'CLOCK (4EA), 6 O'CLOCK (1EA), 10 O'CLOCK (2EA) AND 12 O'CLOCK (1EA) POSITIONS. REMOVED AND REPLACED THE NR 1 ENGINE INLET COWL IAW AMM 71-11-01.Sep 1, 2026 · N8548P · Boeing 7378H4SDR DALA2026090805019Skin · wornWEAR ON CUT-OUT STRUCTURE AT AREA ACCESS PANEL 446BL AT RT PYLON. COMPLIED WITH ER/A 636485-14. (1789727)(AIRCRAFT GROUNDED)Sep 1, 2026 · N195DN · Boeing 767332SDR UIEA2026081300755Skin Panel · crackedNR 1 PYLON NAC STA 228 INBD STRUT SKIN PANEL 452ER CUTOUT CRACKED. CAT C TIME LIMITED REPAIR. CARRIED OUT PERMANENT REPAIR IAW EO 1954A122 IAW SRM 54-50-01, REPAIR 2, & RI-54-50-18436, REV B. NO FURTHER DEFECTS NOTED.Sep 1, 2026 · N489MC · Boeing 747412FSDR UIEA2026082900821Cowling · crackedNR 3L CORE COWL MOST UPPER EDGE MID AREA FOUND CRACKED. REPAIRED IAW RI-71-13-18452 REV B. NO FURTHER DEFECTS NOTED.Sep 1, 2026 · N489MC · Boeing 747412FSDR IPXA2026090886672Panel · corrodedMAJOR REPAIR, NR 1 ENGINE INBD INSIDE PANEL 443JL FWD LOWER PYLON SURFACE HAS CORROSION. CUT & REMOVED THE DAMAGE PART OF PYLON SKIN IAW SRM 51-10-02-0G-0. ACCOMPLISHED REPAIR IAW EO-98556-REQ1 AND STE-MAE EA 757-5450-27-A4612, REV-.Aug 23, 2026 · N441UP · Boeing 75724APFSDR IPXA2026082877723Skin · dentedDENTED SKIN, NR 2 ENG NOSE COWL INNER BARREL NEAR 6:00 POS. CUT OUT DAMAGE AND CLEANED, MEASURE CUT OUT DIA 0.8", FROM FWD EDGE 27.5", AT 6 O'CLOCK ON INNER BARREL OF NR 2 ENG INLET COWL. BONDED THE SPACER WITH FILM ADHESIVE CURED AT 250 F FOR 2 HRS & FILLEDAug 20, 2026 · N393UP · Boeing 767316SDR DALA2026082004755Panel · crackedNR 2 PYLON, LATERAL PANELS, AREA OF FASTENERS NEAR UPPER EDGE OF THE EXTERNAL SURFACE OF THE RIGHT PYLON AT RIB 8 LEVEL FORWORD FASTENER FOUND CRACK. CORRECTIVE ACTION: REPAIRED PER A330 SRM 54-51-00-205-002. (1766235) AIRCRAFT WAS GROUNDED.Aug 20, 2026 · N803NW · Airbus A330323SDR DALA2026082004754Panel · crackedNR 1 PYLON, LATERAL PANELS, AREA OF FASTENERS NEAR UPPER EDGE OF THE EXTERNAL SURFACE OF THE LEFT PYLON AT RIB 8 LEVEL FORWORD FASTENER FOUND CRACKED. REPAIRED IAW SRM 54-51-00-205-002. (1766225) AIRCRAFT WAS GROUNDED.Aug 20, 2026 · N803NW · Airbus A330323SDR JR2R20260818112Panel · chafed429NR HAS BARE METAL SPOTS AND CHFING ON INNER SURFACE. REPAIRAug 18, 2026 · N86309 · Emb ERJ170200LRSDR IPXA2026081244447Cowling · dentedDENTED NR 2 ENG NOSE COWL INLET AT 7 & 5 O'CLOCK POSITIONS. CUT OUT THE DAMAGE & CLEAN, MEASURE THE CUT OUT ( (1) DIA : 1", 15.5" FROM FWD EDGE AT 7 O'CLOCK , (2) DIA : 1" , 15.3" FROM FWD EDGE AT 5 O'CLOCK ON THE INNER BARREL OF NR 2 ENG INLET COWL. BONDED TAug 6, 2026 · N331UP · Boeing 76734AFSDR SWAA2026082737942Skin · damagedNR 2 ENGINE INLET HAS PULLING FASTENERS AT 3 AND 9 O'CLOCK POSITIONS REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.Aug 3, 2026 · N8546V · Boeing 7378H4SDR SWAA2026082715244Skin · damaged#1 ENGINE INLET HAS PULLING FASTENERS AT THE 3 O'CLOCK POSITION REMOVED AND REPLACED NR 1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCEAug 3, 2026 · N8546V · Boeing 7378H4SDR JR2R20250803825Panel · chafedPYLON PANEL 419ML HAS MULTIPLE CHAFES ON INSIDE OF PANEL OUT OF LIMITS. REPAIREDAug 3, 2026 · N86311 · Emb ERJ170200LLSDR JR2R20250803828Panel · chafedPYLON PANEL 419NR HAS MULTIPLE CHAFES ON INSIDE OF PANEL OUT OF LIMITS. REPAIREDAug 3, 2026 · N86311 · Emb ERJ170200LLSDR JR2R20250801825Panel · chafedPYLON PANEL 419ML HAS MULTIPLE CHAFES ON INSIDE OF PANEL. REPAIREDAug 1, 2026 · N86311 · Emb ERJ170200LLSDR JR2R20250801828Panel · chafedPYLON PANEL 419NR HAS MULTIPLE CHAFES ON INSIDE OF PANEL. REPAIRED.Aug 1, 2026 · N86311 · Emb ERJ170200LLSDR SWAA2026082796842Skid Shoe · damaged#2 ENGINE INLET COWL LIP SKIN HAS 4 FASTENERS PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.Jul 23, 2026 · N8546V · Boeing 7378H4SDR SWAA2026082758386Skin · damaged#2 ENGINE INLET COWL LIP SKIN HAS 2 FASTENERS PULLING AT 9 O'CLOCK POSITION. REMOVED AND REPLACED #2 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q01DHKKQ FOR PARTS INFORMATION AND WORK PERFORMED.Jul 23, 2026 · N8546V · Boeing 7378H4SDR SWAA2026082780829Skin · damaged#1 ENGINE INLET COWL LIP SKIN HAS 1 FASTENER PULLING AT 3 O'CLOCK POSITION. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01. REFERENCE TTG8Q00S71UU FOR PARTS INFORMATION AND WORK PERFORMED. REMOVED AND REPLACED #1 ENGINE INLET COWL PER AMM 71-11-01.Jul 23, 2026 · N8546V · Boeing 7378H4SDR IPXA2026072249873Skin · crackedCRACKED SKIN, NR 1 ENG LT CORE COWL POSITION 9 O'CLOCK. REPAIRED DAMAGE AREA IAW SRM 54-45-01-2R-18, REV 95, AND EGAT WORK SHEET 60562.Jul 20, 2026 · N373UP · Boeing 767300SDR IPXA2026072249902Skin · crackedCRACK - SKIN , NO.1 ENG R/H CORE COWL LWR FWD LATCH AREA. PERFORMED THE HEAT TREATMENT FROM 2219-T31 TO T81 CONDITION. IAW EGAT WORK SHEET 60563 STEP 4.F.(1) (TABLE 201 PAGE 14 OF 14). REPAIR DAMAGE AREA I.A.W SRM 54-45-01-2R-12 REV. 95 AND EGAT WORK SHEETJul 20, 2026 · N373UP · Boeing 767300SDR IPXA2026072422572Skin · crackedCRACKED NR 2 PYLON FAIRING PANEL 447 ELX. ACCOMPLISH THE REPAIR IAW SRM 54-52-70-2R-4, REV 55, AND EGAT WORK SHEET 60557.Jul 18, 2026 · N363UP · Boeing 767346SDR SWAA2026072152275Skin · crackedON POST-DOCK WALK AROUND, FOUND CRACKED ON NR 2 ENGINE LOWER PYLON, ABOVE TAIL CONE. CRACK MEASURES ROUGHLY 14 IN LENGTH AND .080 WIDE AT ITS WIDEST.Jul 17, 2026 · N8746Q · Boeing 7378SDR 2026F00152Skin · corrodedMOVED 1 AREA OF CORROSION LOCATED AFT OF RH PYLON TRAILING EDGE, INBD AREA ON FUSELAGE SKIN IAW SRM 51-12-01 AND SRM 51-10-03. PER AQRD RFTS-117833 REV. 0. TITLED "N416QS (50500443) RT PYLON T/E FUSELAGE SKIN CORROSION" DATED 14JULY26. DAMAGE TOLERANCE: YES. TJul 17, 2026 · N416QS · Emb EMB505SDR IPXA2026082679985Skin · crackedPANEL 485AL HAS A CRACK ON THE FWD SIDE. INSTALLED SKIN PANEL ON PANEL 485AL FWD SIDE IAW SRM-51-40-21.Jul 15, 2026 · N136UP · Airbus A300F4622RSDR HNAA2026082700798Hinge · brokenNR 1 ENG START VALVE ACCESS PANEL HINGE BROKEN. R & R HINGE IAW SRM 51-40-02Jul 15, 2026 · N925AE · Emb EMB145LRSDR IPXA2026091160874Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (7EA) STEP 10 AND (1EA) STEP 1 AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.Jul 14, 2026 · N136UP · Airbus A300F4622RSDR IPXA2026091160860Skin · crackedNR 1 PYLON, PRECOOLER AREA, INTERNAL RT SKIN, AT RIB 4, WITH CRACK. INSTALLED RIVETS (8EA) AT NR 1 PYLON, PRECOOLER AREA, INTERNAL LT SKIN, AT RIB 4 IAW SRM 51-40-21-001.Jul 14, 2026 · N136UP · Airbus A300F4622R
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