JASC 5410
Service difficulty reports · 4,119
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 C2XA01BT053Channel · crackedDURING C-CHECK INSPECTION FOUND RIGHTHAND LOWER NACELLE HAS THE LEFTHAND UPPER CHANNEL CRACKED. MAINTENANCE FABRICATED NEW EDGING IAW ATR42 SRM 54-12-61 FIGURE 106 AND REMOVED AND REPLACED IAW ATR42 SRM 51-25-03.SDR AU010295Fairing · missing(AUS) NR 2 ENGINE RT COLD STREAM C DUCT MISSING UPPER INBOARD DUCT TO STRUT FILLET FAIRING.SDR MALA010392Drag Strut · damagedDURING 4K INSPECTION IN CWA, MAINTENANCE FOUND ELONGATED HOLES WERE NOTED IN LT AND RT NACELLE, IB AND OB DRAG STRUTS AND FITTINGS. REF TO EO S54047. MAINTENANCE REPAIRED DRAG STRUTS AND FITTINGS IAW PROCEDURES CONTAINED IN SB340-57-027 AND SRS 340 SDS001219 SDR MWEA010511Intercostal · crackedRIGHT PYLON INTERCOSTAL AFT OF AFT SPAR HAS A CRACK ON UPPER END. REMOVED PYLON SKIN, FABRICATED TWO EACH REPAIR DOUBLERS, INSTALLED DOUBLERS AND SKIN.SDR MWEA010473Intercostal · crackedRIHT PYLON MOST INBOARD INTERCOSTAL AFT OF AFT SPAR HAS A SMALL CRACK ON UPPER FLANGE APPROXIMATELY 18 INCHES AFT OF AFT SPAR. FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR AWXA0001557Attach Angle · crackedNR 2 PYLON AFT BLKHD ATTACH ANGLE IS CRACKED AT PP STA 200. REMOVED ANGLE IAW SRM 51-40-02; FABBED REPLACEMENT ANGLE IAW DWG 311N5041; INSTALLED IAW SRM 51-40-02.SDR MWEA010387Stiffener · crackedRIGHT PYLON SUPPORT STIFFNER HAS A CRACK, LOCATED ABOVE 13TH STAGE AIR DUCT. REMOVED FASTENER, FABRICATED AND INSTALLED DOUBLER.SDR EIA2001129Angle · crackedFOUND NR 3 PYLON REAR ENGINE MOUNT BULKHEAD LEFT TOP LONGERON, REPAIR ANGLE ON FRAME TOP END CRACKED. NDT INSPECTED AREA, DEFECTIVE BRACKET REPLACED PER SRM 51-10-01. (M)SDR EIA2001119Structure · chafedMZJ-EAC - FOUND NR 4 PYLON LOWER EDGE CHAFED BELOW REPAIR DOUBLER AT RIGHT OUTBOARD SIDE, AFT OF AFT ENGINE MOUNT. REPAIRED NR 4 PYLON PER ECRA 3203-54-024-2. (M)SDR CNMA200100002Fitting · brokenDURING MAINTENANCE REMOVAL OF NR 2 ENGINE, THE LEFT AFT LIFTING FITTING WAS BROKEN CAUSING DAMAGE TO THE CENTER BOX STRUCTURE AT THE TOP OF THE ENGINE BAY OF NR 2 PYLON - ( REFERENCE DC10 IPC 54-12-02, PG 7). THE CAUSE OF THE FAILURE OF THE LIFTING FITTING HASDR MALA010341Duct · crackedFOUND DURING C-CHECK, LT COWL 453BR NACA DUCT HAS CRACKS. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00; NDT REQUIRED FOR FURTHER CRACKING. NDT PER FFVNDT006ED NO CRACKS. DAMAGE IS ACCEPTED AS IS AREA IS PRIMED AND TREATED REF SAAB SRM 340SDSSDR MALA010340Duct · crackedFOUND DURING C-CHECK, LT COWL 453AL NACA DUCT IS CRACKED. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00. NDT REQUIRED FOR FURTHER CRACKING. NDTPERFFVNDT006ED NO CRACKS PAST ROUT OUT. REPAIR IS ACCEPTABLE IAW SAAB DOCUMENT 340SDS001241.AREA IS SDR MALA010339Duct · crackedFOUND DURING C-CHECK, COWL 463AL NACA DUCT IS CRACKED. MAINTENANCE REMOVED CRACK BY ROUTING METHODS IAW SRM 51-70-00; NDT REQUIRED FOR FURTHER CRACKING. NDT PER FFVNDT006EC NO CRACKS PAST ROUTE OUT. REPAIR IS ACCEPTABLE IAW SAAB DOCUMENT 340SDS001241. AREA ISDR MALA010350Fastener · damagedFOUND DURING 4K-INSPECTION, CWA. LT NACELLE OB & IB FWD SKIN HAS FASTENERS PULLING THROUGH SKIN AROUND NACELLE STA 203. MX COMPLETED REPAIR IAW MAL EO S54049.SDR MWEA010352Stiffener · crackedRIGHT PYLON OUTER LOWER STIFFENER HAS A 1 INCH CRACK AT STATION 858. FABRICATED AND INSTALLED DOUBLER AND ANGLES.SDR EIA2001135Fitting · crackedHKG-HAECO - FOUND NR 1 ENGINE PYLON DIAGONAL BRACE AFT FITTING CRACKED FROM AFT LEFT ATTACH BOLT HOLE TO OUTBOARD AFT SIDE, AND LEFT 2ND FROM AFT BOLT HEAD BROKEN OFF. REPLACED DIAGONAL BRACE FITTING WITH TAPER SHIM INSTALLED PER BSB 57-2288, BSB 57A2308, BOESDR COMA0110062Stiffener · crackedDURING 2C CHECK TASK 5410-442-04I, THE RT NACELLE FRAME 10 STIFFENER ANGLE, WAS FOUND CRACKED. THE PART WAS REPLACED IN ACCORDANCE WITH EMB-120 SRM STANDARD PRACTICES.SDR C2XA01IA154Channel · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND CHANNEL ON THE LEFT HAND HALF MOON COWLING WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR C2XA01IA152Channel · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND ENGINE TOP COWL WAS FOUND TO HAVE A CRACKED LEFT HAND CHANNEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR MALA010320Hinge · crackedFOUND DURING C-CHECK, IN NASHVILLE, TN. LT ENGINE HINGE COWL 453BR NACA DUCT IS CRACKED. MAINTENANCE STOPPED DRILLED CRACK, FABRICATED DOUBLER REF EO340SDS001131. NO CRACKS NOTED IAW FFVNDT006, INSTALLED REPAIR DOUBLER.SDR MALA010319Duct · crackedFOUND DURING C-CHECK, IN NASHVILLE, TN. LT ENGINE COWL DUCT IS CRACKED. MAINTENANCE STOP DRILLED CRACK, FABRICATED DOUBLER. NO CRACKS NOTED IAW FFVNDT006. INSTALLED REPAIR DOUBLER IAW SAAB STATEMENT 340SDS001131.SDR RRXA10807Plate · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO WING L/E SHIM PLATE AT I/B NR3 ENG. PYLON, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW E.O.#01-006 WITH APPROVED 8110-3 DATED SDR UPS01235221Duct · crackedINSPECTION TYPE:C-CK, NR 2 ENG INLET S-DUCT INNER SKIN HAS APPROX 3 INCH CIRCUMFERENTIAL CRACK APPROX 104 INCHES FROM AFT EDGE AT 3 O''CLOCK. CUT OUT DAMAGE AREA. INSTALLED REPAIR.SDR MWEA010154Web · crackedVERTICAL WEB CRACKED IN RIGHT PYLON OUTBOARD OF 13TH STRINGER. BLEED NUT ACCESSIBLE THROUGH PANEL 8204A. FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR DL757010245Structure · crackedNR 1 PYLON CRACKED AT FWD INBOARD TORQUE BOX CUTOUT 443AR AT UPPER FWD EXT CORNER. REPAIRED PER SRM 54-51-01.SDR 20010209CW009Beam · crackedAC TOTAL TIME 4800 HRS , CRACK NOTED ON BOTH BEAMS RIGHT AND LEFT OUTBOARD SIDE OF EACH ENGINE. BOTH CRACKS APPROX 1.5 IN LONG. CRACKS IN RADIUS OF BEND OF TOP STRAP OF BEAM ASSEMBLY NEAR JUNCTION OF FORE AND AFT RUNNING ENGINE MOUNT BEAMS.SDR HNAA0100011Door · separatedNR 2 MLG FWD DOOR CAME OFF IN FLIGHT, DAMAGING SURROUNDING NACELLE STRUCTURE. REPLACED GEAR DOOR AND REPAIRED NACELLE STRUCTURE PER EO8-54-01-061.SDR UPS01434981Stiffener · crackedINSPECTION TYPE:C, NR 2 PYLON CRACK OTBD PYLON STIFFENER NAC 286. REPAIRED STIFFENER IAW SRM 54-14-03.SDR MWEA010070Angle · crackedLEFT HAND LOWER PYLON ATTACH ANGLE IS CRACKED AT STATION 980. REMOVED CRACKED ANGLE, LOCATED, DRILLED, AND INSTALLED NEW ANGLE.SDR CA011113017Support · cracked(CAN) FOUND THREE CRACKS DURING CHECKS. CRACKED AT FS 630 & 640, LT & RT BL 36 & 00.SDR C2XA01IA050Channel · crackedYYZ - DURING CONTINENTAL EXPRESS C-CHECK, THE RIGHT HAND ENGINE LOWER NACELLE WAS FOUND TO HAVE THE INBOARD CHANNEL CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED SECTION OF CHANNEL IN ACCORDANCE WITH ATR 42-320 SRM 54-12-60 & 51-25-03, AND THE AIRCRASDR C2XA01IA049Channel · crackedYYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT HAND ENGINE COWL (425AT) WAS FOUND TO HAVE A CRACKED CHANNEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IN ACCORDANCE WITH ATR42-320 SRM 54-12-61 AND 51-25-01, AND THE AIRCRAFT WAS APPSDR C2XA01IA047Structure · crackedYYZ - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT HAND ENGINE LOWER COWLING WAS FOUND TO HAVE A CRACKED EDGING. MAINTENANCE REMOVED AND REPLACED THE AFFECTED EDGING IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, AND 51-25-03, AND THE AIRCRAFT WAS APPRSDR C2XA01IA046Channel · crackedYYZ - DURING C-CHECK INSPECTION, THE LEFT HAND UPPER COWLING (425AT) WAS FOUND TO BE CRACKED AT THE LEFT HAND CHANNEL. MAINTENANCE REMOVED AND REPLACED THE AFFECTED CHANNEL IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, AND 51-25-01, AND THE AIRCRAFT WAS APPROVEDSDR PCAA0108103Rivet · looseDURING FLEET INSPECTION FOR NACELLE RIVETS BEING LOOSE AND MISSING, 2 RIVETS ON RIGHT NACELLE OUTBOARD END FOUND LOOSE JUST BELOW FLAP TRACK. LOOSE RIVETS REPLACED. AIRCRAFT RETURNED TO SERVICE.SDR AWXA0001194Angle · damagedLT WING O/B PYLON SKATE ANGLE HAS ELONGATED NR 3 FASTENER HOLE. REMOVED DAMAGE; FABED AND INSTALLED REPAIR AND INSTALLED SKATE ANGLE IAW SRM 51-40-02 AND 51-70-11; INSTALLED REPAIR ANGLES, 2 EA, AND 3 EA FILLERS IAW B737 SRM 51-70-11 AND 54-50-71; FABED ANGLESSDR DL757010074Structure · crackedNR 2 PYLON AFT CORNER PERMANENT REPAIR ACTL 3003-310854.SDR C2XA00TY015Structure · damagedTYS - DURING SCHEDULED MX, THE LEFT ENGINE FIRE EXTINGUISHER WAS INADVERTENTLY ACTIVATED. THE EXTINGUISHING AGENT OVER-PRESSURIZED THE LEFT ENGINE PYLON CAUSING STRUCTURAL DAMAGE TO THE TRAILING EDGE AND NUMEROUS RIBS AND STIFFENERS INTERNAL TO THE PYLON. MASDR C2XA00IA438Frame · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT LOWER NACELLE WAS FOND TO BE CRACKED ON THE INBOARD FORWARD FRAME. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE EC5410-01048, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA00IA439Frame · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE LEFT LOWER NACELLE WAS FOUND TO BE CRACKED ON THE INBOARD FORWARD FRAME. MAINTENANCE REPAIRED THE FRAME IAW CONTINENTAL EXPRESS ENGINEERING CHANGE EC5410-01048, AND THE AIRCRAFT WAS APPROVED FOR RETURN SDR C2XA00IA447Frame · crackedYUL - DURING CONTINENTAL EXPRESS C-CHECK INSPECTION, THE RIGHT BOTTOM NACELLE INBOARD FORWARD VERTICAL FRAME WAS FOUND TO BE CRACKED. MAINTENANCE PERFORMED A DOUBLER REPAIR IAW CONTINENTAL EXPRESS ENGINEERING CHANGE EC5410-01048, AND THE AIRCRAFT WAS APPROVEDSDR QXEA0003162Plate · chafedYXX-RIGHT HAND NACELLE, CHAFE DAMAGE TO NACELLE ACTUATOR MOUNT PLATE. REPAIRED IAW DHC-8 RD8-54-1052 AND SRM 51-20-16, PAGE 1-5, AND SRM 51-20-36, PAGE 1-8.SDR AALA20002025Structure · crackedTUL - HFEC INDICATES CRACK 1 INCH BY 1 INCH, ON UPPER CHORD ANGLE OUTBOARD AFT HOLE NR 1 ENGINE PYLON AT FORWARD ENGINE MOUNT FITTING. REPAIRED PER ESO 11697, DATED 11-22-2000. (M)SDR CALA0001798Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 ENGINE PYLON O/B TRAILING EDGE BRACKET. THE BRACKET WAS REMOVED AND A NEW BRACKET WAS INSTALLED IAW SRM 51-30-2, 51-10-2, 51-10-4, AND 51-10-3.SDR L1GA200000388Stiffener · crackedCRACKED L ANGLE RT ENGINE STRUT PANEL SUPPORT STIFFENER INSTALLED. STACKED ANGLE REPAIR.SDR MWEA001241Clip · crackedLEFT PYLON STRUCTURE AT CANTED STATION XN 34.5 HAS LOWER CLIP CRACKED. -- FABRICATED AND INSTALLED CLIP REPAIR.SDR MWEA001240Clip · crackedLEFT PYLON STRUCTURE AT CANTED STATION XN 34.5 HAS UPPER CLIP CRACKED. -- FABRICATED AND INSTALLED CLIP REPAIR.SDR MWEA001239Bracket · crackedANGLE BRACKET IN LEFT PYLON STRUCTURE AT CANTED STATION XN 34.5 IS CRACKED. -- FABRICATED AND INSTALLED ANGLE BRACKET REPAIR.SDR C2XAOOIA411Structure · crackedYUL-DURING C-CHECK INSPECTION, THE RH ENGINE BOTTOM COWLING UPPER FWD ATTACHMENT EDGE WAS FOUNMD TO BE CRACKED. MX REMOVED DAMAGED EDGE. FABRICATED AND INSTALLED A NEW EDGE IN ACCORDANCE WITH ATR42-320 SRM 54-12-61, 51-25-01 & 51-25-03 AND A/C WAS APPROVED FORSDR C2XAOOIA412Frame · crackedYUL-DURING C-CHECK INSPECTION THE RT ENG BOTTOM COWLING LT FWD FRAME (X1333) WAS FOUND TO BE CRACKED. MX PERFORMED A DOUBLER REPAIR IN ACCORDANCE WITH CONTINENTAL EXPRESS ENGINEERING CHANGE EC5410-01047 REF. ATR DRAWING 41S41R0031 AND A/C WAS APPROVED FOR RETU
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