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.

SDR DALA2025121109045Receptacle · corrodedCORRODED SPIGOT FITTING RECEPTACLE ON LT PYLON. REPLACED THE SPIGOT FITTING RECEPTACLE IAW SRM 54-51-12-300-001, AND SRM 54-51-12-283-001. (1345070).Dec 10, 2025 · N359NB · Airbus A319114SDR DALA2025121009024Drag Fitting · damagedCORROSION WAS FOUND ON OPEN HOLE AT RT ENG DRAG FTG CLAMP-UP & DIAG BRACE HOLE #16 CORROSION ON SKIN AND FITTING BTW 7 AND 9 O CLOCK POSITION, IN REF. (CARD 5720-01100-05B. JOB #138-0001. 6: HOLES AT RH ENG DRAG FTG CLAMP-UP & DIAG BRACE HOLES #3 AND #16 AT RHDec 9, 2025 · N822DX · Boeing 75726DSDR AALA202512302480Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT SLEEVE OF LEFT PYLON (L: 7.570 IN). MAINTENANCE REPLACED SPIGOT SLEEVE ON LH PYLON IAW AMM 57-26-12-400-002-A STEP 4.A.Dec 6, 2025 · N668AW · Airbus A320232SDR AALA202512162027Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT RECEPTACLE FITTING OF LEFT PYLON. MAINTENANCE REPLACED LOWER SPIGOT FITTING ON LH PYLON IAW A320 SRM 54-51-12-300-002.Dec 6, 2025 · N668AW · Airbus A320232SDR JR2R20251206654Beam · chafedWHILE PERFORMING LOWER DRAIN MAST SEAL REPLACEMENT ON NR 1 ENGINE INBD CORE COWL, FOUND DEEP CHAFE ON LOWER BEAM STRUCTURE. REPAIRED IAW ETD & TECHNICAL INSTRUCTION.Dec 6, 2025 · N88341 · Emb ERJ170200LRSDR SWAA2025120442497Acoustic Panel · delaminatedNR 2 ENGINE HAS TWO AFT ACOUSTICAL PANELS THAT ARE DELAMINATED LOCATED ABOVE AND BELOW THE 3 OCLOCK STRUT. REMOVED AND REPLACED THE AFT ACOUSTICAL PANELS IAW AMM 72-23-02.Dec 4, 2025 · N7739A · Boeing 7377BDSDR AALA202512044762Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT RECEPTACLE FITTING BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 51-51-12.Dec 3, 2025 · N668AW · Airbus A320232SDR SWAA2025121941613Support Web · crackedCRACK SUPPORT WEB LOCATED OUTBOARD FAN COWL ON ENGINE. REPLACED WEB AND FASTENERS LOCATED OUTBOARD FAN COWL ON ENGINE 2 IAW SRM 51-40-02, SRM 51-10-02, ITEM 9, AND CMM 71-13-30, REV 32, PAGE 10118, DETAIL P.Dec 1, 2025 · N459WN · Boeing 7377H4SDR VNAA20260205013Cowl Door · dentedDENT ON LOWER FAN COWL DOOR APPOX 6 O'CLOCK POSITION AL LH ENGINE. DRESSED BACK IAW 670-54-14-1012 REV. B AND REO 670-54-14-1332 REV. - -Nov 29, 2025 · N525AE · Bombdr CL6002D15SDR SIMA2025120906001Fitting · wornBEARING ON WING AT UPPER ATTACH POINT OF LT ENGINE UPPER LT PYLON LINK HAS EXCESSIVE PLAY REMOVED LT ENGINE PYLON UPPER ATTACH POINT OTBD FITTING ASSY PER SRM 51-40-08. INSTALLED THE NEW LT ENGINE PYLON UPPER ATTCH POINT OTBD FITTING ASSY IAW AMM 20-10-01, NE4Nov 26, 2025 · N257NN · Emb ERJ170200LRSDR CALA2025120211636Fan Cowl · gougedNUMBER 1 ENGINE OTBD FAN COWL INTERNAL SKIN AT 23 INCHES FROM FWD EDGE AND 33 INCHES FROM LOWER EDGE, FOUND MULTIPLE GOUGES. ACCOMPLISHED FAN COWL SKIN EXTERNAL REPAIR AT TWO FRAMES ON NR 1 ENG OTBD POSITION IAW SRM 54-20-01-2R-5 AND SRM 51-40-02-0G-0.Nov 26, 2025 · N14242 · Boeing 737824SDR SWAA2025120140002Inlet · pulledNUMBER 1 ENG COWL ASSY, INLET INNER SIDE AT 3 O'CLOCK POSITION OUTER BARREL HAS 15 PULLED FASTENERS AND CRACKED 5.5' LONG .IAW TTG8Q0192A5K. R & R NR 1 ENG INLET COWL IAW AMM 71-11-01.Nov 26, 2025 · N498WN · Boeing 7377H4SDR DALA2025112508583Drain Mast · missingNR 1 ENG DRAIN MAST MISSING. INSTALLED DRAIN AT AFT END OF DRAIN MAST IAW AMM 71-73, A/C OK FOR SVC. (LP: 8108788)Nov 22, 2025 · N366NW · Airbus A320212SDR DALA2025120308822Strut · crackedNR 2 NAC STRUT STA 204.50 I/B FITTING FOUND CRACK. CORRECTIVE ACTION: THE FITTING REMOVED AND REPLACED AS PER B767-400 SRM51-40-02 (1314415)Nov 21, 2025 · N840MH · Boeing 767432ERSDR UIEA2025111801310Cowl Door · corrodedCORROSION DAMAGED ON SKIN AND DOUBLER OF NO. 1 ENG LT CORE COWL, BETWEEN NAC STA 22.50 AND NAC STA 230.5 ON AFT SIDE OF PRECOOLER DUCT.(<P>1. ACCOMPLISHED EI NO: T2025A54M-2477 REV 2. 2. JOB COMPLETED AND CONDITION CHECK NORMAL.</P>)Nov 20, 2025 · N249BA · Boeing 747409SDR SWIA2026031075498Cowling · gougedRT ENG LOWER COWLING FWD LATCH HOUSING GOUGED (C-CHECK RO 03/08/2026)PERFORMED BLENDED OUT AND EVALUATED AREA ON RH ENG LOWER COWLING FWD LATCH HOUSING IAW SRM 51-12-00, REO 670-54-22-136 REV--.Nov 18, 2025 · N632SK · Cndair CL6002C10SDR SWAA2025120136235Shield · crackedNR 1 ENGINE, SHIELD CRACKED AT THE 2:00 POSITION AFT LOOKING FWD INBD CORE SIDE JUST UNDER AFT MOUNT. R & R HEAT SHIELD IAW AMM 70-51-00.Nov 17, 2025 · N8829Q · Boeing 7378SDR SWAA2025112036061Fitting · crackedNR 2 AFT PYLON STRUT FAIRING HAS A CRACKED FITTING. REMOVED CRACKED PYLON BRACKET FITTING IAW SRM 51-40-02. LOCATED AND DRILLED NEW END FITTING ASSY IAW SRM 51-40-02. C/W INSPECTION OF CA NR 2. INSTALLED NEW END FITTING ASSY IAW SRM 51-40-02.Nov 17, 2025 · N8510E · Boeing 7378H4SDR CALA2025111811305Door · missingDURING EPDSC WALKAROUBD FOUND MISSING NACELLE STRUT ACCESS DOOR ON INBOARD SIDE OF ENGINE 2. REPLACED ENGINE 2 NACELLE STRUT ACCESS DOOR REF IPC 54-52-01-01. NO OTHER DAMAGE NOTED UPON INSPECTION.Nov 16, 2025 · N644UA · Boeing 767322SDR FDEA202511102154Skin · crackedTAIL ENGINE INTAKE DUCT LEADING EDGE FOUND MULTIPLE CRACKS. #2 ENGINE NOSE COWL REMOVED AND REPLACED AS PER AMM 54-22-01-04, CARRIED OUT NOSE COWL ANTI-ICE SYSTEM FUNCTIONAL TEST AS PER AMM 30-22-00-700-804, FOUND SATISFACTORY. REPAIR CLASSIFIED AS MINOR ANov 10, 2025 · N574FE · Doug MD11FSDR AALA202512013407Plate · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING RETAINING PLATE PER SRM 54-51-12-300-002.Nov 9, 2025 · N831AW · Airbus A319132SDR AALA202511285111Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LT PYLON L= 4.340 INCH, W= 1.547 INCH D= 0.005 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE OF LT PYLON IAW A319 SRM 54-51-12-300-002.Nov 9, 2025 · N831AW · Airbus A319132SDR CALA2025111711272Fitting · crackedCRACK DAMAGE ON THE OTBD SIDE, FWD LOWER FLANGE OF MID BULKHEAD FITTING OF THE NR 2 STRUT ASSY AT PPS 174.30. THE CRACK EXTENDS FROM THE FWD EDGE OF FLANGE TO THE FWD FASTENER HOLE THROUGH ENTIRE MATERIAL THICKNESS.Nov 9, 2025 · N17128 · Boeing 757224SDR CALA2025111211163Structure · corrodedRIGHT PYLON SPIGOT BEARING INNER BORE HAS PITTING CORROSION. R & R NR 2 PYLON SPIGOT BEARING IAW AMM 54-51-41-000- 001-A, AND 54-51-41-400-001-A.Nov 8, 2025 · N877UA · Airbus A319132SDR CALA2025111211147Fitting · corrodedNUMBER 2 PYLON SPIGOT BEARING LOWER FITTING HAS PITTING CORROSION. REMOVED AND REPLACED THE NR 2 PYLON SPIGOT BEARING LOWER FITTING IAW SRM 54-51-12-300-002.Nov 7, 2025 · N877UA · Airbus A319132SDR CALA2025111211145Sleeve · corrodedNUMBER 2 ENGINE SPIGOT SLEEVE AND ATTACHING NUT HAVE PITTING CORROSION. RECEIVED AND REPLACED ENGINE 2 PYLON SPIGOT SLEEVE AND NUT IAW AMM 57-26-12-400-002-A.Nov 7, 2025 · N877UA · Airbus A319132SDR CALA2025111011098Fitting · crackedNUMBER 2 PYLON OTBD SIDE THROUGH ACCESS PANEL 443CR, LOWER CORNER OF PP STA 174 WITH EVIDENCE OF A CRACK. REPAIRED THE PYLON OTBD SIDE BULKHEAD FITTING IAW EA 757-5450-13-A4151 AND EC/RA 5450-03064 REV-.Nov 7, 2025 · N17128 · Boeing 757224SDR SWIA2026070676548Door · dentedADM# N813SK-7764 LEFT HAND ENGINE 6 O' CLOCK POSITION OF FAN COWL DOOR, SMALL DENT 3" WIDE, 1" LONG, .1" DEEP. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD ACFT PRACTICES (C-CHECK RO 07/02/2026)REMONov 6, 2025 · N813SK · Cndair CL6002D24SDR HYIA20251107002Crossbeam · chafedDURING MAINTENANCE CHAFING DAMAGE WAS VISUALLY IDENTIFIED ON THE FORWARD FACE OF THE LH CROSSOVER BEAM (OEM: 5654104-11). THIS CHAFE MEASURES APPROXIMATELY .700 LONG, .500 WIDE, WITH A DEPTH OF APPROXIMATELY .011. THIS BEAM HAS BEEN REPLACED.Nov 5, 2025 · N26156 · Cessna 402CSDR COEA2025110612738Panel · crackedNUMBER 2 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.Nov 3, 2025 · N738FX · Textrn 408SDR COEA2025110611738Panel · crackedWO 272105 NR 6 MINOR REPAIR/DISCREPANCY: #1 ENGINE OUTBOARD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. STOP DRILLED CRACK AND COVERED WITH SPEED TAPE IAW DQ428170M2. REPLACED THE PLENUM PANEL IAW MM 6-40-50 REV. 5 AND IPC 54-10-25-01 REV. 10.Nov 3, 2025 · N738FX · Textrn 408SDR COEA2025110610738Panel · crackedWO 272105 NR 5 MINOR: NR 1 ENGINE INBD PLENUM PANEL SKIN CRACKED AT AFT END OF TOP STIFFENER. REPLACED THE PLENUM PANEL IAW C408MM 6-40-50 REV.11Nov 3, 2025 · N738FX · Textrn 408SDR COEA2025110616759Link · corrodedWO 271980 NR 5 MINOR REPAIR/DISCREPANCY: RT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. REPLACED RT AFT INERTIAL SEPERATOR DOOR LINK ASSY REF IPC 30-20-05 FIG 1-5.Oct 30, 2025 · N759FX · Textrn 408SDR COEA2025110615759Link · corrodedWO 271980 NR 3 MINOR REPAIR/DISCREPANCY: LT ENGINE AFT DOOR LINK ASSY FRETTED AROUND CHAMBERED AREA. CORRECTIVE ACTION: REPLACED L/H AFT INERTIAL SEPERATOR DOOR LINK ASSY. REF IPC 30-20-05 FIG 1-5.Oct 30, 2025 · N759FX · Textrn 408SDR COEA2025110614759Link · crackedWO 271980 NR 2 MINOR REPAIR/DISCREPANCY: R/H ENGINE FWD DOOR LINK ASSY IS CRACKED. REPLACED FWD INERTIAL SEPERATOR DOOR LINK ASSY REF C408 IPC 30-20-05 FIG 1-5.Oct 30, 2025 · N759FX · Textrn 408SDR 2025F00252Attach Bracket · misinstalledLH ENGINE FIXED COWL FORWARD LOWER ATTACHMENT BRACKET INSTALLED INCORRECTLY (180 DEGREES/WRONG WAY AROUND).Oct 29, 2025 · N201CE · Gulstm GVISDR SWAA2025112029497Stiffener · crackedNR 2 ENGINE OTBD FAN COWL 424AR, SHELF STIFFENER CRACKED. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-02.Oct 28, 2025 · N8507C · Boeing 7378H4SDR DALA2025102707831Fitting · corrodedCORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. (1273360).Oct 26, 2025 · N363NB · Airbus A319114SDR E0YA2025110600081Cowling · unknownUPPER LEFT COWLING DEPARTED AIRCRAFT ON TAKEOFF. NO INDICATIONSOct 23, 2025 · N450RH · Bombdr CL6002D15SDR DALA2025102407777Fitting · corrodedCORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. (1268121).Oct 23, 2025 · N363NB · Airbus A319114SDR CALA2025102310433Doubler · crackedNR 1 PYLON UPPER FWD SPAR DOUBLER CRACKED AT LT SKIN. REPAIRED THE NR 1 PYLON UPPER FWD SPAR DOUBLER LT SKIN IAW SRM 54 -52-12-300-024.Oct 20, 2025 · N480UA · Airbus A320232SDR CALA2025102110325Fairing · crackedNUMBER 2 ENGINE AFT STRUT FAIRING POSSIBLE ON THE AFT BRACKET. REMOVED AND INSTALLED NR 2 ENGINE AFT STRUT FAIRING IAW SRM-51-40-02-0G-0, SRM 51-040-05-0G-0, SRM 51-40-08-0G-0, AIPC-54-52-04-02 ITEM 85, AMM 54-52-04-410-802.Oct 15, 2025 · N68805 · Boeing 737924ERSDR IPXA2025111264443Strut · crackedFOUND DURING DVI NR 1 PYLON OTBD SIDE HAS A CRACKED PANEL LANDING UNDER PANEL P/N 311N5049-139. INSTALL REPAIR DOUBLER, FILLERS 2 EACH /ALL REPAIR PARTS AT # 1 PYLON O/B SIDE IAW EA # 757-5450-01-B0589 STEP 17. ACCOMPLISH REPAIR PER VT-SAA EA 757-5450-01-B05Oct 14, 2025 · N456UP · Boeing 75724APFSDR CALA2025101410067Fairing · cracked#2 PYLON AFTER FAIRING WITH CRACK IN AFT AREA. REMOVED AND REPLACED NO. 2 PYLON AFTER FAIRING ASSY END, LOCATED DRILLED AND COUTERSUNK, APPLIED ALODINE, PRIMER, TOPCOAT PAINT IAW B737-900ER SRM 51-40-05-0G-0, SRM 51-40-02-0G-0,SRM51-40-08- 0G-0 SRM 51-21-72-3Oct 12, 2025 · N61898 · Boeing 737924ERSDR AALA202510249828Sleeve · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON AFT ATTACH FITTING UPPER SLEEVE WORN. REPLACED SLEEVE PER TASK CARD 26C41554028.Oct 11, 2025 · N188US · Airbus A321211SDR IPXA2025111094874Angle · crackedNR 2 ENG PYLON UPPER, ANGLE UNDER 423AL IS CRACKED IN TWO LOCATIONS, ACROSS BOLT HOLE AND FWD OF BOLTS. DOT #85/1018 CERTIFIED. REMOVED STRUCTURAL BEAM I.A.W. SRM 51-40-21.FABRICATED, LOCATED AND DRILLED NEW CROSSBEAM IAW A300-600 SRM 51-31-00 AND DWR# A53974Oct 10, 2025 · N129UP · Airbus A300F4622RSDR HYIA20251013001Beam · crackedDURING MAINTENANCE A CRACK WAS DISCOVERED ON THE INBOARD FACE OF THE RIGHT INBD ENGINE BEAM IN THE AREA OF THE VERTICAL ATTACH CHANNELS FOR THE CROSSOVER BEAM. THIS CRACK WAS DISCOVERED AFTER CHANGING THE CROSSOVER BEAM VERTICAL ATTACH BRACKET P/N: 5654107-15 Oct 9, 2025 · N548GA · Cessna 402CSDR CALA2025101309977Platform · missingNR 1 ENGINE OGV PLATFORM MISSING @ 5 O CLOCK PER AMM 72-23-00-211-804-G00. FAN FRAME MODULE INSPECTION H (23) OUTER PLATFORM OGV PERMITTED FOR ALL AREAS AND UP TO 3 PLATFORMS AFFECTED AND UP TO 2 CONSECUTIVE PLATFORMS.Oct 9, 2025 · N17566 · Boeing 7379SDR IPXA2025102162001Support · crackedRH PYLON PANEL 443KL SUPPORT STRUCTURE HAS (1EA) CRACK. REMOVED RH PYLON PANEL 443KL SUPPORT STRUCTURE IAW B757-200PF SRM 51-40-02. ++INSTALLED NWE SUPPORT AT RH PYLON IAW B757-200PF SRM 51-40-02. INSTALLED PANELS: 442AL, 443KL.Oct 8, 2025 · N457UP · Boeing 75724APFSDR AALA202510132947Shackle · wornAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON AFT ATTACH FITTING SHACKLE WORN AT PYLON RIB 10. REPLACED SHACKLE PER AMM 54-51-17.Oct 7, 2025 · N184US · Airbus A321211
Back to JASC 5410