JASC 5414
Service difficulty reports · 4,361
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.
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
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 CALA0001994Angle · crackedINSPECTION FOUND A 1 INCH CRACK AT AFT END UPPER SURFACE OF NR 1 PYLON ANGLE. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-1, AND 51-30-5.SDR CALA0001938Skin · crackedINSPECTION FOUND A 1/4 INCH CRACK IN NR 2 OB PYLON SKIN AFT OF UPPER T/R ABOVE PANEL 5824R. A DOUBLER AND FREEZE PLUGS WERE INSTALLED IAW SRM 5450-01330 AND ECRA 5430-01204.SDR AT0000511Pylon · crackedFOUND NR 2 ENGINE PYLON LOWER AND UPPER TRAILING EDGE PANEL HAS LOOSE AND MISSING FASTENERS. REMOVED AND REPLACED NR 2 ENGINE TRAILING EDGE PANEL UPPER AND LOWER SKINS. REMOVED AND REPLACED WEDGE, REMOVED AND REINSTALLED NR 2 ENGINE PYLON TRAILING EDGE ASSEMSDR AU001163Panel · separated(AUS) RT STRUT TRUNNION ACCESS PANEL SEPARATED FROM AIRCRAFT. THE PANEL CAUSED IMPACT DAMAGE TO THE RT HORIZONTAL STABILISER LEADING EDGE AND TOP SKIN. FOLLOWING REMOVAL OF THE REMAINS OF THE DEPARTEDPANEL THE HOLDING TORQUE ON THE ANCHOR NUTS WAS CHECKED WITHSDR 20001120SH043Fairing · crackedNR 2 ENGINE LOWER LOW DRAG FAIRING NAC STA 290.91 HAD A SKIN CRACK BETWEEN MOUNTING HOLES. REPAIRED PER ECRA 621-53-0008. (X)SDR EISA20000225Skin · puncturedPUNCTURE AT NR 2 ENGINE NOSE COWL AFT OF INLET RING. CORRECTIVE ACTION: CUT OUT PUNCTURED SKIN, FABRICATED, FILLER, AND DOUBLER, ALODINED, PRIMED, AND INSTALLED REPAIR IAW SRM 51-10-2, 51-40-2 FIG. 1, 54-30-3 FIG.5, 54-30-2, 51-30-2.SDR EIAA2000300Doubler · crackedJFK - DURING SCHEDULED NR 3 ENGINE CHANGE, INSPECTION FOUND CRACK ON NR 3 PYLON, INBOARD SIDE ON DOUBLER ABOVE AFT MOUNT. REMOVED CRACKED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER PER SRM 54-10-03 AND SRM 53-30-03. (X)SDR COMA0010402Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-IR, 7-25-99.SDR COMA0010401Skin · chafedUPON COMPLANCE OF 2C INSPECTION TASK 5410-432-04I THE LT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1,IR,7-25-99.SDR COMA0010400Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR COMA0010399Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I THE RT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED I/A/W EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7-25-99.SDR UPS00434316Skin · damagedINSPECTION TYPE:C, NR 1 PYLON DAMAGE TO PYLON SKIN LWR SHIRT AREA INBOARD OF REAR ENGINE MOUNT AND FWD OF ENGINE MOUNT. REPAIR CARRIED OUT IAW SRM 54-30-03 FIG 36.SDR 20001120SH059Skin · corrodedDURING 100-HOUR INSPECTION, AIRCRAFT NACELLE AREA FOUND THE UPPER ENGINE MOUNT ATTACH STRUCTURE STEEL STRAPS HEAVILY CORRODED. UPON REMOVAL OF THE UPPER NACELLES ON THE LEFT AND RIGHT SIDES OF THE AIRCRAFT, FOUND HEAVY PITTING AND WIDE SPREAD CORROSION OVER TSDR USAA001785Skin · crackedCLT - FOUND SKIN AND DOUBLER CRACKED 1 INCH, NR 1 PYLON AT ACCESS PANEL 5728L. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR ABXA000472Doubler · crackedFOUND 12 INCH CRACK ON NR 4 INBOARD SIDE OF PYLON SKIN STATION YOP 220. *S/D* REPAIRED IAW DC8 SRM 54-2-1 AND REA D854-38893-MR.SDR AU001221Panel · cracked(AUS) LT PYLON PANEL 5727L REPAIR DOUBLER CRACKED. DOUBLER WAS FITTED IAW SB 7737-54-1035.SDR 20010125SG019Skin · corrodedDURNIG C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WASSDR 20010125SG018Skin · corrodedDURING C-CHECK AT ALITALIA, THE FITTING ELEMENT INSIDE THE AIR INTAKE DUCT ON THE NR 2 ENGINE SKIN PANEL ATTACHED TO BANJO''S 1, 2, 3 STRUCTURE IS CORRODED. REPAIRED IAW EO CH-00-015, BOEING TLX CAC-FCO 00-00008H, AND DRAWING AJC 7998. AN FAA FORM 8110-3 WASSDR DHL2000715011Panel · damagedNR 3 ENGINE PYLON FIXED COWL PANEL DAMAGED UPPER SIDE AFT OF 2ND VERTICAL LATCH CUTOUT. REPAIR PER SRM 51-10-1. SIZE OF REPAIR 23 X 4 INCHES.SDR USAA001673Skin · crackedCLT - Q-4, SKIN CRACKED .50 INCH AT RIGHT AFT CORNER ACCESS PANEL AT NAC STA 225. INSTALLED FILLER AND DOUBLER PER TR 54-30-07. (X)SDR EIAA2000050Plate · crackedKJFK - FLT EIA 328 - ON POST-FLIGHT WALKAROUND, FOUND 5.75 INCHES VERTICAL CRACK ON NR 3 PYLON, INBOARD SIDE BELOW PYLON VLV PLATE. REMOVED AND REPLACED NR 3 ENGINE TO FACILITATE PYLON REPAIR. STOP DRILLED CRACK, FABRICATED DOUBLER. REPAIRED AND INSTALLED PSDR DHL2000708020Panel · crackedPANEL 5512 MOUNT HOLE CRACK. REPLACED PANEL 12 X 25 INCH PER SRM 51-30-2.SDR DHL200072005CSkin · crackedDURING C CHECK, FOUND NR 1 ENGINE AFT FIXED COWL LOWER FWD SKIN CUTOUT CRACK AT EDGE. INSTALLED DOUBLER PER B727 SRM 54-10-3, SIZE OF REPAIR 5 X 6 INCHES.SDR USAA001383Skin · crackedCLT - FOUND SKIN PYLON CRACKED 1.5 INCHES, NAC STATION 212 PANEL ACCESS 5727L. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR USAA001302Skin · crackedCLT - FOUND SKIN AND DOUBLER CRACKED .5 INCH, RIGHT PYLON PANEL CUTOUT 5824R. FABRICATED AND INSTALLED DOUBLER PER EA 67781 AND TR 54-50-07. (M)SDR RIVA0000026Skin · dentedPSM, THE NR 3 ENG NACELLE NOSE COWL IS DENTED BEYOND LIMITS AT NAC STA 63.5 AT THE 5 O''CLOCK POS. REPAIRED THE AREA BY INSTALL OF A FLUSH TYPE REPAIR. REMOVED THE DAMAGED AREA IAW SRM 54-30-3 FIG 2. FABRICATED THE FILLER, DOUBLER AND SHIMS IAW SRM 54-30-3 SDR RIVA0000025Skin · dentedPSM, NR 1 ENG NOSE COWL IS DENTED BEYOND ALLOWABLE LIMITS AT NAC STA 98 AT THE 9 O''CLOCK POS. REP THE AFFECTED AREA BY THE INSTALL OF A FLUSH TYPE REP. ALL WORK WAS ACCOM IAW BY THE FOLLOWING: 1) REMOVED THE DAMAGED AREA IAW THE SRM 54-30-3 FIG 2. FABRICATSDR CA001004016Panel · missing(CAN) ON WALKAROUND FOUND PANEL MISSING ON INBOARD SIDE OF RIGHT HAND ENGINE STRUT. NIL PART AVAILABLE, PLACED ON MEL 54-51-0100. NEW PANEL INSTALLED.SDR USAA001220Skin · crackedCLT - FOUND PYLON SKIN CRACKED 1 INCH, STATION 260, WL 132 INBOARD PYLON SKIN PANEL 5724L. INSTALLED DOUBLER PER TR 54-50-07, EA 67725 AND EA 67746. (M)SDR C2XA00IA247Panel · missingCLL - FLT 3463 - DURING POST-FLIGHT INSPECTION, THE CREW REPORTED THAT THE RIGHT HYDRAULIC SERVICE DOOR WAS MISSING. MAINTENANCE REPLACED THE RIGHT HYDRAULIC SERVICE DOOR, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR USAA001072Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, RIGHT ACCESS CUTOUT OUTBOARD EDGE PANEL 5828R. INSTALLED EXTERNAL DOUBLER PER TR 54-30-07. (M)SDR USAA001071Skin · crackedCLT - FOUND SKIN CRACKED .5 INCH, RIGHT PYLON ACCESS HOLE CUTOUT AT OUTBOARD EDGE. INSTALLED EXTERNAL DOUBLER PER TR 54-30-07. (M)SDR USAA001091Skin · crackedCLT - FOUND PYLON SKIN CRACKED 1 INCH, LOWER AFT CORNER OF 5724L. INSTALLED DOUBLER PER TR 54-50-07. (M)SDR CALA0001152Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN LT ENGINE PYLON TOP CUTOUT PANEL NR 5727. AN INTERIM REPAIR WAS PERFORMED IAW ECRA 5430-01230. A DIP WAS INITIATED TO REINSPECT THE SKIN AND DOUBLER FOR CRACK GROWTH EVERY 150 FLIGHT CYCLES UNTIL TIP OF CRACK REACHES PRODUCSDR F3LA00155Panel · crackedDEN - DURING C-2 CHECK INSPECTION, FOUND 4 CRACKS IN NR 2 ENGINE PYLON PANEL NR 5824R IN UPPER FORWARD CORNER OF ACCESS HOLE. MAINTENANCE REPAIRED DAMAGED AREA PER EA 54-737-015A. (M)SDR DHL200070921CSkin · crackedNR 3 ENG COWLING O/B SIDE AFT SECTION CLOSE TO HORIZONTAL LATCH SKIN IS CRACKED. INSTALLED DOUBLER REPAIR ON AFFECTED AREA PER SRM 51-40-2.SDR DHL200070917CSkin · corrodedNR 1 LOWER COWLING CLOSE TO FIRE ACCESS, SKIN IS CORRODED ON PREVIOUS REPAIR. REMOVED OLD REPAIR PER SRM 51-30-2. CUT OUT DAMAGED SECTION OF SKIN (18 X 5.5 INCH)PER SRM 54-10-3. INSTALLED DOUBLER REPAIR PER SRM 54-10-3 FIG 5. ALL REPAIR PARTS WERE TREATED SDR ASAA0040090Fairing · chafedSEA - DURING SCHEDULED C-CHECK, NR 1 ENGINE INBOARD BULLNOSE FAIRING WAS FOUND TO BE CHAFED AND GOUGED. REPAIRED PER EA 5430-01069. (M)SDR C2XA00IA176Skin · crackedIAH - DURING C-CHECK INSPECTION, THE RIGHT THRUST REVERSER WAS FOUND TO BE CRACKED WITH SHEARED RIVETS ABOVE AND FORWARD OF PANEL 426SL. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A DOUBLER REPAIR. (M)SDR COMA0010210Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STURCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, IR, 7/25/99.SDR COMA0010213Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-1, IR, 7/25/99.SDR COMA0010212Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE RIGHT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-IR, 7/25/99.SDR COMA0010211Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB-120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT #3364-1, IR, 7/25/99.SDR USAA000972Access Panel · crackedPIT - FOUND CRACKED ACCESS PLATE CRACKED 1 INCH, 5727L NR 1 ENGINE PYLON. DOUBLER INSTALLED PER TYP REPAIR 54-30-07. (M)SDR 20000620SH028Skin · chafedNR 4 PYLON INBOARD SIDE LOWER EDGE OF THE SKIN DAMAGED (CHAFED). FOUND DURING ENGINE CHANGE. SUBMITTER SUGGESTED FREQUENT INSPECTION OF AREA WHEN COWLING IS REMOVED. REPAIRED PER EAC ECRA N855FT-54-001-EAC. (X)SDR 0002146718Skin · crackedDURING M-CHECK, FOUND CRACK IN THE NUMBER 4 INBOARD PYLON SKIN, AT SLOT SEAL, NACELLE STATION 180. REPAIRED PER EA 67-175573.SDR COMA0010200Skin · chafedUPON COMPLIANCE OF2C INSPECTION TASK 5410-432-04I, THE LEFT NACELLE OUTBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR COMA0010199Skin · chafedUPON COMPLIANCE OF 2C INSPECTION TASK 5410-442-04I, THE LEFT NACELLE INBOARD INNER SKIN WAS FOUND TO BE CHAFED. THE DAMAGED PART WAS REPLACED IAW EMB 120 STRUCTURAL REPAIR MANUAL STANDARD PRACTICES AND AERODESIGN REPORT NR 3364-1, REV IR, 7-25-99.SDR CALA0000851Skin · crackedINSPECTION FOUND TWO 1 INCH CRACKS IN NR 1 ENGINE PYLON I/B SIDE ACCESS DOOR PANEL NR 5724L CUTOUT. A DOUBLER WAS INSTALLED IAW ECRA 5430-01204.SDR RRXA002776Skin · cutDURING A MAINTENANCE VISIT FOUND SEVERAL CUTS IN NR 4 ENG O/B T/R INTER RING COWL, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. RECEIVED REPAIR AND INSTALLED IAW EO NR 00-107 WITH APPROVED 8110-3 DATE
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