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 CALA9900871Skin · crackedINSPECTION FOUND A 1 CRACK IN NR 1 ENGINE PYLON SKIN AT PANEL CUTOUT 5727L (NAC STA 213). THE CRACK WAS STOP DRILLED AND A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.SDR UF6A990759Skin · crackedSBN - THE NR 2 MOD 6 IS CRACKED AT APPROX THE 7 O'CLOCK POSITION. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED A PARTIAL SKIN REPLACEMENT. ALL WORK WAS DONE IAW DER REPORT NR 99-131. (M)SDR UPS99830158Skin · crackedINSPECTION TYPE:N/A ON POST FLIGHT, ENGINEER AND MECHANIC VERIFIED A SMALL CRACK ON NR 2 PYLON. ACCOMPLISHED EO DC8-5430-11626-A APPENDIX B INTERIM REPAIR NR 2 PYLON OUTBOARD RAMP AT THE ENGINE FAN EXHAUST OUTLET. TRANSFERRED TO DMI LIST C/N D-175661 ASSIGNESDR UF6A990744Skin · burnedSBN - LIGHTNING STRIKE DAMAGE OUTBOARD SIDE OF NR 2 NACELLE. MAINTENANCE REPAIRED DAMAGE IAW BAE ATP SRM 51-60-01, FIG 1. (M)SDR QXEA9901590Skin · crackedPDX - LEFT NACELLE LOWER INBOARD FORWARD CORNER CUTOUT IS CRACKED. REPAIRED IAW DHC-8 RD 8-54-724.SDR UF6A990724Skin · looseSBN - SEVERAL WORKING RIVETS ON MOD 4 SKIN OUTBOARD SIDE. MAINTENANCE REPLACED SKIN AND REPAIRED IAW BAE SRM 51-10-03 AND 51-10-06. (M)SDR MWEA99384Skin · crackedLEFT PYLON UPPER SKIN STIFFENER IS CRACKED ABOVE 13TH STAGE BLEED DUCT INSIDE PANEL 8103A. MTC FABRICATED AND INSTALLED DOUBLER REPAIR.SDR CALA9900784Skin · crackedINSPECTION FOUND A 2 INCH CRACK IN NR 2 ENGINE PYLON SKIN WITH LOOSE FASTENERS ON PYLON FIN. THE SKIN WAS REPAIRED IAW SRM 54-20-00, FIGURE 6 AND FASTENERS WERE REPLACED IAW SRM 51-31-00.SDR UPS99630006Panel · crackedRT ENG OTBD SIDE PYLON PANEL CRACKED. PANEL IS FIRST FWD OF HYDRAULI C ACCESS DOOR. CRACK IS 2 INCH LONG RADIATING FROM AFT EDGE. PANEL NUMBER 447ERX REF MM 06-43-00 PG 213. PERFORMED INTERIM REPAIR PER EO B767-5450-11458-A AS ISSUED BY UPS ENGINEERING. ASDR AT9900577Panel · corrodedDURING SCHEDULED INSPECTION AT TIMCO, FOUND PANEL NR 8105A ON THE LEFT LOWER PYLON CORRODED. REMOVED AND REPLACED PANEL NR 8105A IAW DC9 SRM 51-30-1, 54-02, 51-10-3.SDR UIEA9940Skin · crackedPYLON SKIN CRACKED NAC 235 R/S. EDGE OF PRE-COOLER EXHAUST DUCT OPENING EDGE. STIFFENER NR 3 RT SIDE. REPAIRED PER TLS BKK-99-0069RE, 99-0064RE, 99-0063RE. 8130-3 ISSUED. (X)SDR F3LA99087Skin · crackedDEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3. (M)SDR MWEA99449Skin · crackedTHE LEFT ENGINE PYLON UPPER SKIN TRAILING EDGE HAS A CRACK AT STATION 886. MAINTENANCE FABRICATED AND INSTALLED DOUBLER.SDR C2XA99BT047Skin · damagedBTV - DURING 5A INSPECTION, FOUND FUSELAGE DAMAGE ON RIGHT SIDE UNDER NR 2 ENGINE AS MARKED. MAINTENANCE REPAIRED SKIN AS PER EMB145 SRM NR 53-31-01. PRESSURE CHECKED AIRCRAFT GOOD. (M)SDR DL757991218Skin · crackedTHE NR 2 ENG NACELLE STRUT SKIN WAS FOUND WITH MULTIPLE CRACKS IN THE RT SIDE SKIN PANEL. REPAIRED PER ERA 333163-14, REV A.SDR DL757991214Skin · crackedTHE NR 1 ENG NACELLE STRUT SKIN WAS PREVIOUSLY FOUND CRACKED AND REPAIRED. ADDITIONAL CRACKING WAS FOUND DURING THE CURRENT VISIT. THE NEW CRACK WAS APPROX 1 INCH IN LENGTH. REPAIRED PER ERA 333162-14, REV A.SDR SIMA991402Skin · chafedABI - DURING MBV INSPECTION, FOUND CHAFE ON THE LEFT INBOARD NACELLE OUTER SKIN PANEL. CUTOUT PUNTURE AREA OF CHAFE AND BLENDED THE REMAINING CHAFED AREA. PERFORMED AN EDDY CURRENT INSPECTION OF THE REWORK AREA WITH NO CRACK INDICATIONS NOTED. RESTORED PROTSDR ABXA9900500Skin · crackedNR 4 PYLON UPPER SKIN TRAILING EDGE CRACKED AT STATION XFS 532. REPAIRED IAW ABX REA NR D857-27903MR.SDR CALA9900555Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 2 ENGINE PYLON SKIN AT PANEL NR 5824 AND A .5 INCH CRACK WAS FOUND IN PANEL NR 5828. REPAIRS WERE INSTALLED IAW ECRA 5430-01230.SDR ABXA9900490Skin · crackedLEFT WING NR 2 PYLON LEADING EDGE SKIN CRACKED AT STATION XS 250 UNDER THE UPPER SLOT DOOR. REPAIRED IAW DC8 SRM 57-3-3.SDR AT9900479Panel · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL. FOUND THE LEFT PYLON PANEL NR 8103 CORRODED AROUND CAMLOCKS AND BACK SIDE OF THE PANEL. MECHANICALLY REMOVED CORROSION FROM PANEL, FOUND PANEL BEYOND REPAIR. ORDERED NEW PANEL IAW DC9 SRM 51-10-3, AND 54-02 FIG 3SDR AT9900392Panel · corrodedSCHEDULED INSPECTION AT TIMCO LAKE CITY, FL, FOUND THE RIGHT PYLON PANEL NR 8204 CORRODED AROUND CAMLOCKS AND ON THE BACK SIDE. FABRICATED, LOCATED, DRILLED, DEBURRED THREE EACH REPAIRS, PRIMED, AND INSTALLED IAW DC9 SRM 51-10-3, 51-30-2, 54-01 FIG 1, 54-30-0SDR UF6A990513Skin · chafedSBN - RIGHT MODULE THREE HAS SEVERAL HOLES CHAFED IN BOTTOM FIRE SKIN. MAINTENANCE REPAIRED DAMAGE BY FABRICATION OF DOUBLER IAW BAE ATP SRM 54-10-03 AND 51-60-01 FIGURE ONE. (M)SDR DHL9980205CSkin · crackedC CHECK, NONROUTE ENG #4 INSIDE CENTER PYLON SECTION GENERATOR FEEDER CABLE SUPPORT HAD CRACK DAMAGE ON SURFACE. REMOVED GENERATOR FEEDER CABLE SUPPORT AS PER DC8 MM 20-50-1. CUT OUT CRACKED AREAS FROM PANEL AT NR 4 PYLON CENTER AREA IAW DC8 SRM 3-2-0 FIG 23SDR 99T64R115ARAnchor Nut · missingNR 0525 - ONE EACH ANCHOR NUTPLATE MISSING, NR 1 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)SDR 99T64R114ARAnchor Nut · missingNR 0524 - 2 EACH, ANCHOR NUTPLATES MISSING NR 2 PYLON REMOVABLE PLANK. INSTALLED JO-BOLTS IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)SDR 99T64R113ARAnchor Nut · missingNR 0523 - ONE EACH, ANCHOR NUTPLATES MISSING NR 3 PYLON REMOVABLE PLANK. INSTALLED JO-BOLT IAW EO 99-026 WITH APPROVED FAA FORM 8110-3 DATED 2-9-99. REF: ARROW AIR, ARWA. (X)SDR SIMA991121Skin · chafedABI - DURING MBV INSPECTION A CHAFE WAS DISCOVERED ON THE LEFT NACELLE INBOARD OUTER SKIN AT FILLET SEAL CONTACT. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. RESTORED PROTECTIVE TREATMENT INCLUDING THE POLYURETHANE TOP COAT. FABRICATEDSDR SIMA991102Skin · chafedABI - DURING A MBV INSPECTION, A CHAFE WAS DISCOVERED ON RIGHT NACELLE INBOARD INNER SKIN PANEL. BLENDED OUT THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS. FABRICATED A DOUBLER .025 THICK. APPLIED FAY SEALANT TO THE CONTSDR AALA990562Skin · damagedTUL - FOUND 4 HOLES THROUGH SKIN ELONGATED AND OVERSIZED. INSTALLED DOUBLER PER ESO 11697, DATED 4-8-99. (M)SDR SIMA991097Skin · chafedABI - DURING A MBV INSPECTION A CHAFE WAS DISCOVERED ON THE RIGHT NACELLE INBOARD OUTER SKIN PANEL AT FILLET FAIRING SEAL CONTACT POINT. BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. CUT OUT AREA AROUND PUNCTURE AND APPLIED PROTECTIVE TREATMESDR SIMA991092Skin · chafedABI - DURING A MBV INSPECTION A CHAFE WAS DISCOVERED ON THE LEFT NACELLE INBOARD OUTER SKIN PANEL AT THE FILLET FAIRING SEAL CONTACT POINT. BLENDED THE CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A DOUBLER AND A TRIPLER .050 THICK. FABRSDR CALA9900423Skin · crackedINSPECTION FOUND THE NR 2 ENGINE RT O/B PYLON SKIN CRACKED AT FORWARD UPPER CORNER AND AFT LOWER CORNER AT ACCESS PANEL NR 5824. THE CRACKS WERE .5 AND 2 INCH LONG. REPAIRED IAW ECRA 5430-01204.SDR QXEA9900555Skin · damagedYXX - NR 2 NACELLE HAS RIVETS PULLED THROUGH SKIN AT NACELLE STATION 134.68 AT LOWER LONGERON OUTBOARD SIDE. REPAIRED IAW SRM 51-20-16.SDR SIMA990901Skin · chafedABI - DURING MBV INSPECTION, FOUND CHAFE ON THE RIGHT NACELLE INBOARD OUTER SKIN PANEL BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. RESTORED PROTECTIVE TREATEMENT TO THE BLENDED AREA INCLUDING POLYURETHANE TOP COSDR SIMA990892Skin · chafedABI - DURING A MBV INSPECTION, FOUND CHAFE ON THE LEFT NACELLE OUTBOARD INNER SKIN. BLENDED THE CHAFE AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT DOUBLER .025. APPLIED SEALANT TO THE CONTACT SURFACSDR DHL9970149DPanel · puncturedAT D-CHECK, PANEL TOP OF NR 2 ENGINE TORQUE BOX HAS A HOLE PUNCHED THROUGH. FABRICATED NEW PANEL 21 X 7.5 PER SRM 51-10-2.SDR CALA9900331Panel · crackedINSPECTION FOUND A 3 INCH CRACK ON NR 3 PYLON PANEL NR 487ER. THE PANEL WAS REPLACED IAW SRM 51-30-00.SDR DLL13990665Panel · damagedFOUND ON WALKAROUND, NR 1 ENG PYLON PANEL 451FT DAMAGED. FABRICATED NEW PANEL PER ERA 367054-14.SDR CALA9900325Skin · crackedINSPECTION FOUND A 1 CRACK IN NR 3 PYLON SKIN. A DOUBLER REPAIR WAS INSTALLED IAW ECRA 5450-01212. A DIP WAS ISSUED TO CHECK BLIND FASTENERS FOR SECURITY EVERY 1000 CYCLES UNTIL A PERMANENT REPAIR IS INSTALLED WITHIN 400 DAYS.SDR SIMA990787Skin · chafedABI - DURING MBV INSPECTION, FOUND CHAFE ON RT NACELLE INNER SKIN. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED A REINFORCEMENT DOUBLER .025 INCH THICK. APPLIED SEALANT TO THE CONTACT SURFACE OF THE DOUBLERSDR SIMA990785Skin · chafedABI - DURING MBV INSPECTION, FOUND CHAFE ON RT NACELLE INBOARD OUTER SKIN PANEL. BLENDED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO INDICATIONS OF CRACKS. FABRICATED AN EXTERNAL DOUBLER .050 INCH THICK. APPLIED SEALANT TO THE CONTACT SURFACE OF TSDR SIMA990772Skin · chafedABI - DURING MBV INSPECTION, A CHAFE WAS DISCOVERED ON THE RT NACELLE INBOARD SKIN PANEL FROM WING FILLET FAIRING SEAL. CUT OUT AND BLENDED THE DAMAGED AREA AND PERFORMED AN EDDY CURRENT INSPECTION WITH NO CRACK INDICATIONS NOTED. RESTORED PROTECTIVE TREATMESDR AT9900197Skin · crackedSCHEDULED INSPECTION AT AERO CORP, FL. FOUND THE NR 1 PYLON TRAILING EDGE PANEL LOWER SIDE SKIN REPAIR DISBONDED AND CORNERS CRACKED OFF AT BS 1030 TO 1076. REMOVED SKIN, FABRICATED NEW SKIN, DRILLED, DEBURRED, COUNTERSUNK, TREATED, PRIMED, AND INSTALLED IAWSDR 99T64R380ARFastener · missingNR 0557 - NR 2 PYLON LOWER SURFACE 2 EACH FASTENERS MISSING OUTBOARD SIDE ABOVE TAILPIPE. YN 219 AND YN 300. REAMED HOLES TO -197/-199 DIAMETER. INSTALLED MS21141 - V06 FASTENER PER EO 99-036 WITH APPROVED FAA FORM 8110-3 DATED 2-24-99. REF: ARROW AIR, ARSDR SIMA990671Skin · chafedABI - DURING MBV INSPECTION, A CHAFE WAS DISCOVERED ON THE RT NACELLE FILLET FAIRING SEAL CONTACT AREA. BLENDED CHAFED AREA AND PERFORMED AN EDDY CURRENT INSPECTION. FABRICATED A REPAIR DOUBLER AND TRIPLER BOTH .050 INCH THICK. APPLIED PROTECTIVE TREATMENT SDR QXEA9900534Skin · damagedYXX - NR 1 NACELLE OUTBOARD LOWER CORNER AT FORWARD GEAR DOOR CUTOUT OUTER SKIN DAMAGED. REPAIRED IAW DHC-8 RD 8-54-1043.SDR C2XA99IA169Skin · chafedDURING CONTINENTAL EXPRESS C-CHECK INSPECTION, FOUND LEFT NACELLE INBOARD SIDE DENTED AT FRAME 2. INSTALLED DOUBLER REPAIR IAW SRM 51-70-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR DL733990386Skin · crackedCRACK IN NR 1 PYLON STRUT SKIN AT THE ACCESS OPENING 5727L. ACTION TAKEN, 332810-14.SDR QXEA9900526Skin · chafedYXX - NR 1 NACELLE AFT FINGERNAIL DECK SKIN CHAFED AT STA 236. REPAIRED IAW DHC-8 RD 8-54-376, 8-54-1032 AND DHC-8 SRM 51-40-00.
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