JASC 5410
Service difficulty reports · 4,114
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 AALA202406177940Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON SPIGOT FITTING LOWER PLATE AT PYLON RIB 6. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR CALA2024061401799Door · missingPDA 1 #2 ENG OIL SERVICE DOOR MISSING ON ARRIVAL TO DENVER HINGE IS MISSING PIC CHECKED BONDING BETWEEN COWL HINGE AND PYLON FOR NEW COWL OIL SERVICE DOOR MEASURES 20.5 IN X 18.5 IN INSTALL PER AMM 20-28-00. WITHIN LIMTS. REF LOGPAGE 8256271 OIL SVC DOOR MISSISDR COEA2024061219708Torque Tube · wornWO 258062 NR 3 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION OF THE R/H LOWER COWL INERTIAL SEPERATOR TORQUE TUBE ASSYS, PLAY AND WEAR WAS DISCOVERED ON THE FWD TORQUE TUBE TO OUTBOARD SHAFT FITTING, THE AFT TORQUE TUBE TO R/H ARM ASSY AND THE FWD TORSDR COEA2024061218708Torque Tube · wornDURING A SCHEDULED MAINTENANCE INSPECTION OF THE L/H LOWER COWL INERTIAL SEPERATOR TORQUE TUBE ASSY'S, PLAY AND WEAR WAS DISCOVERED ON THE FWD TORQUE TUBE TO INBOARD SHAFT FITTING, THE FWD TORQUE TUBE TO R/H ARM ASSY AND THE FWD TORQUE TUBE TARGET ARM. REPLASDR COEA2024080223738Latch · excess playL/H LOWER AFT COWLING FWD ICE VANE DOOR R/H LEVER TO CLEVIS ASSY ATTACHMENT HAS PLAY. REPAIRED IAW C408 SPM 20-10-65 AND 20-40-30.SDR CALA2024060301667Panel · missingPDA 2 ON ETOPS WALKROUND FOUND PANEL 446BR MISSING. PYLON PANEL 446BR FITTED, AMM REF 54-53-01-404-007 FOR INSTALLATION. PARTS USED: 76-5453-3-0063,QTY :1SDR MK1Y20240602001Strut · damagedREPAIR - ENG #2, STRUT CORE COWL HINGE #2 L/H, AT STA 201.25, BORES OUT OF DESIGN LIMIT.SDR VNAA202407090003Fireshield · wornIN REF. TRFKE0095XD2:EA22-C9-54-0939. PERM REPAIR - LH ENGINE FWD CORE COWL FIRE SHIELD WITHIN 4270.48 FLIGHT HOURS FROM IR (BEFORE 19,075.18 FH'S) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. REPAIRED PER REO.NO .690-54-23-3SDR COEA2024080529738Separator · crackedWO 258209 NR 1 DISCREPANCY: L/H COWL, NACELLE, INERTIAL SEPARATOR MOUNTING STRUCTURE HAS CRACKS. CORRECTIVE ACTION: REPAIRED PER SR-408-ATA54-42396 REV. C.SDR VNAA202407020005Fireshield · wornRIGHT FWD CORE COWL FIRE SHIELD ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. R/H FWD CORE COWL FIRE SHIELD WAS REPAIRED PER REO N° 690-54-23-382 REV.--SDR JJBA20240611027Yoke · crackedRH PYLON SPAR II YOKE AFT RIVET HOLE CRACKED. CRACKED HOLE ON RH PYLON SPAR II YOKE AFT RIVET HOLE REPAIREDSDR UIEA2024052400434Fastener · looseNO.2 ENG R/H CORE COWL FOUND SEVERAL FASTENER LOOSE(<P>#2 ENG RH CORE COWL FASTENER REPLACED IAW EA -1971A101 REV 0 AND SRM 51-40-02 REV 100 DATE 20 FEB 2024. NO FURTHER DEFECTS NOTED. </P>)SDR UIEA2024052500444Structure · cracked#2 ENG R/H CORE COWL EXHAUST AREA FOUND SEVERAL FASTNER HOLE CRACKED(<P>REPAIRED IAW SRM 54-41-01-2R-3 REPAIR 3 AND EA-1971A104. NO FURTHER DEFECTS NOTED.</P>)SDR CALA2024052901608Access Door · missingNACELLE STRUT ACCESS DOORS INBOARD (446AL ) AT ENG 2 MISSING. PERFORMED REQUEST CDL 54BE. CDL FOLLOWED AND INOP. STICKED INSTALLED 150 SQUARE INCHES) IAW GMM 02-30-95 PARAGRAPH H TABLE 1. GVI INSPECTION NO DAMAGES FOUND. NSU AT GRU. PARTS INFORMED. CONFIRMSDR DALA2024052805538Ball Joint · corrodedSHIP 3132 CORROSION SPIGOT BEARING BALL JOINT ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT BALL JOINT ON LH PYLON AS PER A320 FAM AMM 54-51 -41-400-001-A. (0363367)SDR AALA202406118942Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR CALA2024052901626Door · missingPDA 2 PDA : LEFT ENGINE PYLON OUTBOARD NACELLE STRUT PRESSURE RELIEF DOOR MISSING {B767-51-3-6003}. PERFORMED GVI AND IT WAS NOT FOUND ANY DAMAGES ON THE NACELLE INSTALLED. CDL COMPLIED, STICKER INSTALLED. STRUCT AREA, RELEASED CDL 54D DUE NO PARTS AT GRU. STISDR MK1Y2024052200378Acoustic Panel · dentedFOUND SEVERAL FILLING REPAIRES AND DENTS ON ENGINE (PW4060-3) #1 INLET COWL ACOUSTIC PANELSSDR HYIA20240521001Crossbeam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE RIGHT HAND CROSSOVER BEAM (OEM P/N: 5654104-12) OF N678JG. THIS CRACK IS LOCATED ON THE AFT FACE OF THE BEAM, COMMON TO THE TOP OUTBOARD BOLT HOLE FOR THE TURBOCHARGER SUPPORT BRACKET. THIS CRACK MEASURSDR SWAA2024061487783Rub Strip · debonded#1 ENGINE PYLON UPPER WEB PANEL CUT OUT RUB STRIP DISBONDED (COMMON TO PANEL 433AT)<[01] UPDATED MEASUREMENTS.;[02] REMOVED AND REINSTALLED #1 ENGINE PANEL 433AT CUT OUT RUB STRIP PER AMM 51-51-00-340-803.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2; CARD COMPLESDR SWAA2024061487788Rub Strip · debonded#1 ENGINE PYLON UPPER WEB PANEL CUT OUT RUB STRIP DISBONDED (COMMON TO PANEL 433BT)<[01] UPDATED MEASUREMENTS.;[02] REMOVED AND REINSTALLED #1 ENGINE PANEL 433BT CUT OUT RUB STRIP PER AMM 51-51-00-340-803.;[03] VERIFIED CORRECTIVE ACTION ITEMS 1-2; CARD COMPLESDR SWAA2024060787399Support Angle · crackedTHE #2 ENGINE INBD FAN COWL HAS A CRACK NOTED ON A SUPPORT ANGLE AT APPROXIMATELY 7 INCHES BELOW PANEL 423AL AND 14 INCHES FROM THE FWD EDGE. (MARKED)<[01] VERIFIED NO CRACK INDICATION ON BRACKET PER NDT PART 6 51-00-00 PROCEDURE 23.;[02] REINSTALLED T CLIP PESDR SWAA2024062587264Panel · peelingPANEL 431DL INNER SURFACE IS PEELING<[01] REPAIRED INNER SURFACE PANEL 431DL. AS PER; SRM 51-70-14-2R-3.;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024061487063Web · cracked#1 INBD FAN COWL HAS CRACKED WEB NEXT TO PANEL 414AR.<[01] 03 - SERVICED STRUT (X-DIMENSION CHECK REQUIRED) PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] REMOVED AND REPLACED #1 INBD FAN COWL WEB (SHIESDR COEA2024052917708Longeron · crackedWO 257747 NR 6 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE L/H NACELLE INBOARD SIDE LONGERON UNDER THE ICE VANE ATTACH POINT SHOWS SIGNS OF CRACKED STARTING. REPLACED THE L/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. MM 71-10-05 AND SDR COEA2024052916708Longeron · crackedWO 257747 NR 5 DISCREPANCY: DURING A SCHEDULED MAINTENANCE INSPECTION, THE R/H NACELLE OUTBOARD SIDE LONGERON IS CRACKED IN BEND RADIUS UNDER THE ICE VANE ACTUATOR ATTACH POINTS. REPLACED THE R/H LOWER AFT COWLING AND FORWARD INTAKE COWLING REF. C408 MM 71-1SDR SWAA2024061486974Rub Strip · debonded#2 ENGINE PYLON UPPER WEB RUBSTRIP DISBONDED COMMON TO PANEL 443CT CUT OUT<[01] INSTALLED SERVICEABLE RUB STRIP ON #2 ENGINE PYLON PANEL 443CT CUT OUT PER AMM 51-51-00-340-803 STEPS 3. D. (2)(A). ADHESIVE APPLIED AT 15:05 UTC.;[02] INSTALLED SERVICEABLE RUB STSDR DALA2024052205420Panel · missingSHIP 1201 ON WALK AROUND FOUND PANEL MISSING BEHIND N1 FAN ON THE LEFT ENG . CORRECTIVE ACTION: C/W SECTION II PERMANENT REPAIR PER ERA 618914-14 REV B. OK TO CLOSE MONITOR LOG. A/C OK FOR SVC. (5628162)SDR IXXA2024051602Attach Angle · cracked#1 PYLON FRAME ATTACH ANGLE COMMON TO THE OTBD SIDE LOAD FITTING IS CRACKED ACCESS THROUGH PANEL 436ALSDR SWAA2024062586007Panel · damagedRIGHT INLET COWL OUTER LOWER PANEL 422AB TWO EACH FASTENER HOLES ELONGATED<[01] THIS INLET COWL WILL BE REPLACED ON WORK CARD TTG8Q00S71JJ;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR SWAA2024062586015Panel · damagedLEFT INLET COWL OUTER LOWER PANEL 412AB ONE EACH FASTENER HOLE ELONGATED<[01] LEFT INLET COWL IS BEING REPLACED ON TASK CARD # TTG8Q00S71JJ;[02] VERIFIED STEP 1<BR>AUDIT C/W PER MPM 52.02.02SDR R61A2024061200251Fitting · crackedDURING EXIT INSPECTION FOUND LH PYLON I/B AFT ATTACH LUG FITTING CRACKED. REPAIRED IAW SB170-54-0018 AND ETD2024-170-016196. ALSO REF SWO-000497-2024 FOR WORK PERFORMED.SDR AALA202405305151Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLO SPIGOT FITTING RECEPTACLE BETWEEN WS 679 AND WS 706, BETWEEN RIB 4 AND RIB 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR A6WA202405118746Fitting · crackedCRACKED FITTING ON UPPER TRANSLATING COWLING DOOR. ACFT REMOVED FROM SERVICE. REMOVED & REPLACED FITTING INTERLOCK RH ON UPPER TRANSLATING COWLING DOOR, IAW SRM 51-42-28 REV. 39 DATE 2024-05-08. ALL WORK PERFORMED UNDER WORK ORDER 004309. NO. 20124,SDR DALA2024051005114Fairing · crackedSHIP 178 #2 PYLON LWR AFT FAIRING HAS VERTICAL CRACK ON I/B SIDE FWD OF T /E REMOVABLE PANEL. CORRECTIVE ACTION: REPAIRED REF B767 SRM 54-53-01-2R-7 (0334681)SDR NACA2024050700006Torque Box · crackedFOUND RH PYLON FWD TORQUE BOX UPPER SKIN OB DRAIN HOLE CRACK. THE CRACK LENGTH IS 2.7", REPAIRED AS PER DRAFT EO 767-54-0006SDR NACA202405070003Bolt · failedFOUND #2 ENG CORE COWL HINGE BOLT COULD NOT SELF LOCK. REPLACED #2 ENG CORE COWL HINGE BOLT IAW 767-300 AMM 71-11/SDR IXXA2024050603Support Angle · cracked#1 STRUT FAIRING LONGERON SUPPORT ANGLE IS CRACKED AT NAC 364SDR DALA2024050704997Structure · crackedSHIP 1815 FOUND LH NACELLE STRUT FWD UPR SPAR CUTOUT CRACK AT NAC STA 230. CORRECTIVE ACTION: THE CRACK ON LH NACELLE STRUT FWD SPAR CUTOUT AT NAC STA 230 REPAIRED AS PER PRI 617659-14, COMPARED AND COMPLIED WITH ER/A 617659-14 (0326995)SDR SWIA2024071000504Door · dentedRIGHT ENGINE NACELLE UPPER FAN COWL DOOR FOUND DENTED ADJACENT TO UPPER FORWARD INLINE FAIRING (C-CHECK RO 7/9/2024) DENT ON R/H UPR FAN COWL DOOR ELIMINATED WITH CUTOUT REPAIR CRJ 900 SRM 54-14-00-201-005-A01 COMPLIED WITH M337 AND COMPLIED WITH SKYWESDR SWAA2024052081097Web · crackedA225 022 #2 ENGINE OTBD FAN COWL OIL ACCESS DOOR INTERNAL AFT WEB CLOSEOUT CRACKED<[01] REMOVED AND REPLACED WEB IAW SRM 51-40-02-0G-0 USING PART NUMBER 314-2269-4 A TAG A237806 VERIFIED TO BE CORRECT REPLACEMENT PART IAW CMM 71-13-30.SDR FDEA202404300531Drag Fitting · crackedC/W EA F-5730-T0378682 WING - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SKIN HOLES REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-15 OF EA TF-5730-T0378682 PT1 WINGS - PLATES AND SKIN - RHW PYLON DRAG FITTING TO SKSDR FDEA202404300527Drag Fitting · crackedCW EA F-5730-T0378768 WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TO SKIN HOLES - REINSPECTION OF PREVIOUS REPAIRS AND APPROVAL. COMPLIED WITH AND COMPLETED ALL STEPS 1-13 OF EA TF-5730-T0378768 PT1. WINGS - PLATES AND SKIN - LHW PYLON DRAG FITTING TOSDR SWAA2024042979791Cowling · cracked#1 ENGINE INBOARD FAN COWL CRACKED<[01] R/R FAN COWL PER AMM 71-11-02SDR HYIA20240426001Fitting · crackedDURING MAINTENANCE A CRACK WAS IDENTIFIED ON THE OUTBOARD LEG OF THE RIGHT HAND INBOARD NACELLE FITTING, (P/N: 5292029-22) THIS CRACK MEASURES APPROXIMATELY .100 INCHES LONG AND WAS DISCOVERED USING THE LIGHTED BORESCOPE INSPECTION PROCEDURE AS OUTLINED IN TEXSDR AALA202405171441Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING LOCATED BETWEEN RIB 4 AND RIB 5 ON RIGHT-HAND PYLON. REPLACED SPIGOT FITTING PER SRM 51-42-11-801SDR AALA202405167975Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING BETWEEN PYLON RIBS 3 AND 4. REPLACED SPIGOT FITTING PER SRM 51-42-11.SDR AALA202405134579Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT-HAND PYLON SPIGOT FITTING RECEPTACLE BORE LOCATED BETWEEN WS 679 AND WS 706 AND RIB 4 TO RIB 5 ON LEFT-HAND PYLON. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12-300-002.SDR WX0A2024050832036Fairing · cracked(DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0011: REAR KEEL FAIRING CRACK ON R/H PYLON AFT LOWER FAIRING. / REAR KEEL FAIRING CRACK ON R/H PYLON AFT LOWER FAIRING REPAIRED IAW S.R.M. 54-56-11-283-013 PARA. (5) REV. 148. THIS REPAIR TASK ISDR WX0A2024050832035Fairing · cracked(DISCREPANCY DISCOVERED DURING AIRCRAFT HEAVY MX VISIT) NRC 4000-0010: REAR KEEL FAIRING CRACK ON L/H PYLON AFT LOWER FAIRING. / REAR KEEL FAIRING CRACK ON L/H PYLON AFT LOWER FAIRING REPAIRED IAW S.R.M. 54-56-11-283-013 PARA. (5) REV. 148. THIS REPAIR TASK I
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