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 DALA2025052203944Fitting · corrodedSHIP 3162 ENGINE #1 PYLON SPIGOT RECEPTACLE FITTING BEARING WITH CORROSION. CORRECTIVE ACTION: REPLACED #1 PYLON SPIGOT BALL JOINT IAW A319 AMM TASK 54-51-41- 000-001-A. (0978242).May 21, 2025 · N362NB · Airbus A319114SDR DALA2025052203942Fitting · corrodedSHIP 3162 ENGINE #2 PYLON SPIGOT RECEPTACLE FITTING BALL JOINT WITH CORROSION. CORRECTIVE ACTION: REPLACED #2 PYLON SPIGOT BALL JOINT IAW A319 AMM TASK 54-51-41- 00-001-A. (0978117).May 21, 2025 · N362NB · Airbus A319114SDR UIEA2025052100651Latch · faulted#2 ENGINE NACELLE STRUT, TWO LATCHES CHECK FOR OPERATION ON WALL ARROUND, FOUND BOTH PARTIAL OPEN.(<P>REMOVED AND REPLACED 2EA DEFECTIVE LATCHES AT #2 ENG NACELLE STRUT IAW B767 SRM 51-40-02. OPS CHECK GOOD.</P>)May 21, 2025 · N664GT · Boeing 76731BSDR UIEA2025052100652Bracket · cracked#1 ENGINE PYLON I/B DOOR OPEN ROD DAMAGE & BRACKET CRACKED.(<P>LOCATED, DRILLED, AND INSTALLED NEW HOLD OPEN ROD SUPPORT BRACKET IAW B767 SRM 51-40-02 & 51-40-05. INSTALLED NEW HOLD OPEN ROD IAW B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)May 21, 2025 · N664GT · Boeing 76731BSDR UIEA2025052100656Rod · damaged#1 ENGINE INBOARD, HOLD OPEN ROD, CORE COWL LH DAMAGE WON'T LOCK.(<P>REMOVED AND REPLACED #1 ENG INBOARD HOLD OPEN ROD COWL LH AS REQUIRED IAW B767 AMM 71-11-11 AND 20-11-00. NO FURTHER DEFECTS NOTED.</P>)May 21, 2025 · N664GT · Boeing 76731BSDR UIEA2025052100658Latch · worn#2 ENG PYLON STRUT TWO LATCH WORN OUT. NEED TO BE REPLACED R/H ACCESS PANEL.(<P>REMOVED DAMAGED LATCHED AT LHS ACCESS PANEL AT #2 ENGINE PYLON STRUT, LOCATED, CLEANED, PREPARED, SECURED AND INSTALLED NEW LATCHES AS REQUIRED AT #2 ENGINE PYLON STRUT ACCESS PANEMay 21, 2025 · N664GT · Boeing 76731BSDR SWAA2025052072057Fairing · cracked#1 ENG PYLON AFT STRUT SUPPORT FAIRING CRACKED<[01] REMOVED AND REPLACED CRACK #1 ENG PYLON AFT STRUT SUPPORT FAIRING PER SRM 51-40-02.May 17, 2025 · N439WN · Boeing 7377H4SDR UIEA2025041700530Bushing · wornENG 1, STRUT UPPER LINK, LOWER FITTING, BUSHINGS WITH WEAR.(<P>BUSHING WAS REPLACED AND INSTALLED IAW SRM 54-52-90-2R-2 REV 128. NO FUTHER DEFECTS NOTED.</P>)May 16, 2025 · N640GT · Boeing 7673S1SDR UIEA2025041700532Bushing · corrodedSTRUT 2 UPPER LINK LOWER ATTACHMENT FITTING INBOARD/OUTBOARD LUG BUSHINGS WITH CORROSION.(<P>BUSHINGS WERE REPLACED IAW SRM 54-52-90-2R-2 REV 128. NO FURTHER DEFECTS NOTED.</P>)May 16, 2025 · N640GT · Boeing 7673S1SDR UIEA2025041700533Bushing · corrodedSTRUT 1 DIAGONAL BRACE FWD BUSHINGS WITH CORROSION.(<P>BUSHINGS WERE REPLACED IAW SOPM 20-50-03 REV 127 & CMM 54-50-21. NO FURTHER DEFECTS NOTED.</P>)May 16, 2025 · N640GT · Boeing 7673S1SDR UIEA2025041700534Bushing · corrodedSTRUT 2 DIAGONAL BRACE FWD BUSHINGS WITH CORROSION.(<P>BUSHINGS WERE REPLACED IAW SOPM 20-50-03 REV 127 & CMM 54-50-21. NO FURTHER DEFECTS NOTED.</P>)May 16, 2025 · N640GT · Boeing 7673S1SDR SWAA2025051971257Fairing · cracked#2 ENGINE PYLON AFT STRUT FAIRING NAC STA. 315; 1 INCH CRACK VISIBLE IN FITTING.<[01] ADDED 'AFT STRUT FAING' TO FAULT HEADING.;[02] REPAIRED REF M-23-154-01884;[03] ENG 02) CFM56-7B24/3 ENGINE (PN: CFM56-7B24/3; SN: 802895);[04] C/W M-23-154-01884.;[05] ADDEDMay 14, 2025 · N926WN · Boeing 7377H4SDR CALA2025051304645Door · missingPDA 2 #1 ENGINE IDG SERVICE DOOR MISSING UPON LANDING AT SFO. A SDR REPORT MUST BE ACCOMPLISHED PDA CAT 2 # 1 ENGINE IDG DOOR WAS FOUND MISSING UPON LANDING AT SFO. OUR BELIEVE IS WHEN AIRCRAFT DEPARTING FROM EWR (FLT 1475) THE IDG DOOR WAS NOT FULLY LATCHED May 12, 2025 · N14107 · Boeing 757224SDR VNAA2025050800032Latch · chafedHN00194545 DISCREPANCY: LH UPPER TRANSCOWL HAS CHAFING UNDER LATCH PANEL. CORRECTIVE ACTION: UPON FURTHER EVALUATION, FOUND DAMAGE TO BE LOCATED ON L/H UPPER TRANSCOWL LATCH DOOR COAMING P/N CN624-2060-205. EVALUATED CHAFE DAMAGE ON THE L/H UPPER TRANSCOWL LATMay 8, 2025 · N502AE · Cndair CL6002C10SDR SWAA2025050566699Inlet · pulled#2 ENGINE INLET HAS 17 FASTENERS PULLED THRU ON OUTBOARD SIDE 3OCLOCK POSITION.<[01] REMOVED #2 ENGINE INLET REF AMM 71-11-01;[02] 01 - REMOVED AND REPLACED PER [AMM 71-11-01-401-NG (INLET COWL - REMOVAL/INSTALLATION - PERMANENT)]May 2, 2025 · N417WN · Boeing 7377H4SDR AALA202506058712Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION FLOOR BEAM +Y1732 LOCATED BTW FR65 AND FR66 AT LEVEL OF STR 23L AT AFT GALLEY AREA L=0.531 INCH, W=0.667INCH, D=0.040 INCH. MAINTENANCE REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON I.A.W A319 SRM-54-51-12-300-001.May 1, 2025 · N762US · Airbus A319112SDR IPXA2025051593375Doubler · crackedENG 1 CORE COWL O/B EXTERNAL AREA HAVE EVIDENCE OF CRACK AND 4 FASTENERS MISSING DOT 07-030. INSTALLED DOUBLER AND FILLER IAW B757 SRM 54-41-01-2R-1.Apr 28, 2025 · N415UP · Boeing 75724APFSDR 2025FA0000321Fairing · damagedFOUND DAMAGE TO NO. 2 PYLON INBOARD CORE COWL AND SKIRT FAIRING PANEL (CF680C2), NAC STA 294.51 TO 304.4.Apr 27, 2025 · N29383 · Boeing 7673Q8SDR SWAA2025052864520Cowl Door · cracked#1 ENGINE INBOARD FAN COWL; PANEL 414; WEB AFT OF OIL SERVICE DOOR CRACKED. REMOVED AND REPLACE #1 ENG I/B FAN COWL IAW AMM 71-11-02.Apr 26, 2025 · N8687A · Boeing 7378H4SDR SWAA2025052864522Cowl Door · cracked#2 ENGINE OUTBOARD FAN COWL; PANEL 424; WEB AFT OF THE OIL SERVICE DOOR CRACKED.<[01] REMOVED AND REPLACED #2 ENGINE OUTBOARD FAN COWL PER AMM 71-11-02 AND MT# 7111-E-17063-NG. REFERENCE TTG8Q00S5H19 FOR WORK ACCOMPLISHED AND PARTS INFORMATION.;[02] INSPECTED Apr 26, 2025 · N8687A · Boeing 7378H4SDR AALA202505272497Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING LOWER ON RH PYLON MEASURE OF THE DAMAGE ARE: L= 13.50 INCH, W= 1.335 INCH, D= 0.006 INCH. MAINTENANCE REPLACED SPIGOT FITTING LOWER ON RH PYLON BTW SRA 679 TO SRA 829 A319 SRM 54-51-12-300-001.Apr 25, 2025 · N819AW · Airbus A319132SDR AALA202504290492Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON MOUNTED CENTER HINGE FITTING FOR THE OUTBOARD THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 54-57-17.Apr 25, 2025 · N172US · Airbus A321211SDR DALA2025042203154Drag Fitting · damagedSHIP 6710 A.A.//A.D. DISCREPANCIES ON OPEN HOLES FROM LH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE # 3 CORROSION ON FITTING 9 O CLOCK POSITION, HOLE # 7 CORROSION ON FITTING BTW 9-10 O CLOCK POSITION (IN REF: CARD 5720-01100-04A JOB # 151-0001 STEP 14.C.). CORRECTApr 20, 2025 · N6710E · Boeing 757232SDR AALA202504294368Sleeve · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON FORWARD SHACKLE SLEEVE CRACKED. REPLACED SLEEVE PER TASK CARD 26L40054002.Apr 19, 2025 · N177US · Airbus A321211SDR UIEA2025032800400Access Door · worn#2 PYLON I/B ACCESS DOOR #462ER FOUND 2EA SCREW HOLES WORN(<P>PANEL FABRICATED AS PER RI-54-50-17522 REV A . NO FURTHER DEFECTS NOTED</P>)Apr 18, 2025 · N493MC · Boeing 74747UFSDR KCSA2025041716Nacelle · damagedLANDING HARD ENGINE POD STRICK #4. FOUND DAMAGE ON ENGINE 4 INBOARD FAN COWL AND THRUST REVERSER, OUTBOARD FAN AND THRUST REVERSER INSPECTED ENGINE 4 IAW B747-400 AMM 05-51-06 NO OTHER DAMAGE FOUND. REPAIRED AND COMPLIED WITH DAMAGE FOUND IAW 500 14052 AND SRApr 17, 2025 · N768CK · Boeing 747481FSDR SWIA2025082500416Drag Angle · crackedTHE RH VERTICAL FWD DRAG ANGLE IS CRACKED. (C-CHECK RO 8/21/2025) REPAIRED RH VERTICAL FORWARD DRAG ANGLE BY INSTALLING -3 DOUBLER ANGLE AND -4 ANGLE FILLER ON VERTICAL STABILIZER TO FUSELAGE FWD ATTACHMENT PER REF CRJ 900 SRM 55-31-00-201-001-A01. COMApr 16, 2025 · N804SK · Cndair CL6002D24SDR SWI2025F00662Support Beam · failed inspENGINE SUPPORT BEAM RBL27.50 CLOSE OUT ANGLE AT FS625.30 & WL111.09 HAS AN INDICATION .75" LONG BY 100% FSH PROPERGATING FROM THE LOWER FASTENER HOLE. FAILED NDT INSPECTION. (C-CHECK RO 05/27/2025)REMOVED UNSERVICEABLE RH ENG SUPPORT BEAM CLOSE OUT ANGLE (P/Apr 16, 2025 · N930SW · Cndair CL6002B19SDR SWIA20250527416Support Beam · failed inspENGINE SUPPORT BEAM LBL27.50 CLOSE OUT ANGLE AT FS625.30 & WL119.12 HAS AN INDICATION .3" LONG BY 100% FSH PROPERGATING FROM THE UPPER FASTENER HOLE. FAILED NDT INSPECTION. (C-CHECK RO 05/27/2025)REMOVED UNSERVICEABLE LH ENG SUPPORT BEAM CLOSE OUT ANGLE (P/N:Apr 16, 2025 · N930SW · Cndair CL6002B19SDR SWAA2025042124890Flange · crackedUPON REMOVAL OF #2 ENGINE EXHAUST PLUG FOUND ENGINE FLANGE ASSY FLANGE CRACKED AT MULTIPLE LOCATIONS.Apr 15, 2025 · N924WN · Boeing 7377H4SDR KC8A20250418002Cowl Door · inflt separationDURING CRUISE, RIGHT ENGINE UPPER AND LOWER RIGHT COWLING DEPARTED AIRCRAFT. 'THIS IS A RE-SUBMISSION DUE TO MISSING REGISTRATION NUMBER NOT LISTED IN 1. (C).Apr 15, 2025 · N229CK · Amd FALCON20SDR KC8A20250418001Cowl Door · inflt separationDURING CRUISE. RIGHT ENGINE UPPER AND LOWER RIGHT COWLING DEPARTED AIRCRAFT.Apr 15, 2025 · N200MV · Amd FALCON20SDR SWAA2025051957377Support Web · crackedCRACK SUPPORT WEB LOC INBOARD FAN COWL ON ENGINE 1 2025-250482<[01] REPLACED SUPPORT WEB LOC INBOARD FAN COWL ON ENGINE 1 IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G PARAGRAPH 9 AND GOODRICH AEROSTRUCTURES CMM 71-13-30 REV 31; IPL FIGURE 4; SHEET 5.;[02] REPApr 13, 2025 · N7747C · Boeing 7377BDSDR AALA202504115219Shim · migratedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND ENGINE STRUT TORQUE BOX UPPER OUTBOARD ATTACHED CHORD AT AFT END, SUPPORT BRACKET SHIM MIGRATED. TREIMMED AND RETIGHTENED SHIMTO 45 IN LB WITH NO FASTENER ROTATION. SHIM IS TIGHT AND CANNOT BE REMOVED.Apr 10, 2025 · N924NN · Boeing 737823SDR CALA2025041403753Fairing · crackedNO-2 PYLON AFT LOWER FIXED FAIRING AFT INTERNAL SUPPORT RIB CRACKED REF AAR N/R 9948452 REMOVED AND REPLACED T/E ASSY AFT FAIRING AT #2 PYLON AFT FIXED FAIRING AS PER SRM 51-40-02-0G-0 AND DWG# 313A2700. ESFR COMPLETED REMOVED AND REPLACED T/E ASSY AFT FAIRApr 9, 2025 · N86534 · Boeing 737824SDR 2025FA0000236Skin · unknownREPAIR EVALUATION - #2 ENGINE INLET COWL INNER SKIN EXISTING REPAIRS.Apr 6, 2025 · N475CM · Boeing 767300SDR DALA2025040802734Fitting · corrodedSHIP 685 A.D.//A.A. DISCREPANCIES ON OPEN HOLES FROM LH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE # 2 CORROSION AND SCRATCHES ON FITTING AND SKIN BTW 8-11 O CLOCK POSITION, HOLE # 3 CORROSION ON FITTING AND SKIN BTW 1-4 O CLOCK POSITION, HOLE # 4 CORROSION ON FITTApr 5, 2025 · N685DA · Boeing 757232SDR DALA2025040802733Drag Fitting · corrodedSHIP 685 A.D.//A.A. DISCREPANCIES ON OPEN HOLES FROM LH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE # 11 CORROSION ON FITTING AND SKIN BTW 4-7 O CLOCK POSITION, HOLE # 12 CORROSION ON FITTING AND SKIN BTW 8-11 O CLOCK POSITION, HOLE # 13 CORROSION ON FITTING BTW 9- Apr 5, 2025 · N685DA · Boeing 757232SDR UIEA2025032300377Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BL, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BL WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEApr 5, 2025 · N1381A · Boeing 767316SDR UIEA2025032300378Retainer · corrodedCORROSION ON THE PLATE LOCATED IN THE FRAME UPPER PART (INNER STRUCTURE) WHICH IT IS SUPPORTING THE ACCESS PANEL 447BR, RIGHT ENGINE, AFT NACELLE STRUT FAIRINGS.(<P>PLATE OF THE ACCESS PANEL 447BR WAS REPLACED IAW SRM 51-10-02-0G-0 PAR 9 REV 52. NO FURTHER DEFApr 5, 2025 · N1381A · Boeing 767316SDR SWI2025F00810Structure · corrodedS/N 0462BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX), THEIRS A FUEL LINE THAT LEAKED AND AREA HAS CORROSION. FLAGGED (C-CHECK RO 06/29/2025)REMOVED CORROSION BETWEEN FS1069.75 AND FS1088.20 INTERNAL OF LH PYLON (LUNCH BOX) PER CRJ900 SRM Apr 3, 2025 · N800SK · Cndair CL6002D24SDR EE4Y2025040322130Inlet · dentedDURING THE STRUCTURE INSPECTION IT WAS FOUND THE ENGINE #1 AIR INLET MODULE P/N: 341-1010-509A, S/N: 0069001 INNER BARREL SKIN WITH SMALL DENTS. THE DENTS WERE EVALUATED AS PER SRM 71-61-01 AD53 AND SOME OF THEM WERE FOUND OUT LIMITS DUE TO THE DISTANCE BETWEEApr 3, 2025 · N238BJ · Emb ERJ190100IGWSDR EE4Y2025040322128Inlet · dentedDURING THE STRUCTURE INSPECTION IT WAS FOUND THE ENGINE #2 AIR INLET MODULE (REF /B/) INNER BARREL LOWER SKIN WITH SMALL DENTS LOCATED BETWEEN 5.0 AND 7.0 O’CLOCK. THE DENTS WERE EVALUATED AS PER SRM 71-61-01 AD53 AND WERE FOUND OUT LIMITS DUE TO THE DISTANCE Apr 3, 2025 · N238BJ · Emb ERJ190100IGWSDR AALA202505020671Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BORE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.Apr 2, 2025 · N176UW · Airbus A321211SDR AALA202505026407Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON LOWER SPIGOT FITTING RECEPTACLE BORE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.Apr 2, 2025 · N176UW · Airbus A321211SDR AALA202504070960Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. MAINTENANCE REPLACED SERVICEABLE LOWER SPIGOT FITTING RECEPTACLE ON LH PYLON IAW A319 SRM 54-51-12-300-002.Apr 2, 2025 · N820AW · Airbus A319132SDR VNAA20250524005Fitting · damagedTOOL MARK ON FITTING OF SPRING CONTRABALANCE AT LH NACELLE. FITTING OF SPRING CONTRABALANCE AT LH NACELLE WAS REPAIRED PER REO 670-54-20-003 REV --Apr 1, 2025 · N514AE · Bombdr CL6002D15SDR AALA202504299895Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON MOUNTED AFT HINGE FITTING FOR THE INBOARD THRUST REVERSER HAS EXCESSIVE PLAY. REPLACED HINGE FITTING PER AMM 54-57-17.Mar 29, 2025 · N172US · Airbus A321211SDR AALA202504081519Pin · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON INBOARD ATTACH FITTING LOWER SLEEVE / PIN THREADS WORN AT PYLON RIB 4. REPLACED SLEEVE / PIN PER TASK CARD 26C41554028.Mar 27, 2025 · N172US · Airbus A321211SDR AALA202504081692Pin · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND FORWARD PYLON INBOARD ATTACH FITTING UPPER SLEEVE / PIN THREADS WORN AT PYLON RIB 4. REPLACED SLEEVE / PIN PER TASK CARD 26C41554028.Mar 27, 2025 · N172US · Airbus A321211
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