JASC 5420

Service difficulty reports · 3,949

Reports filed under 5420 · Nacelle/Pylon Miscellaneous Structure, 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 = '5420'
  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 CA110801006Intercostal · crackedCRACKED INTERCOSTALS AT LOWER STRUCTURE OF BOTH NACELLES PN 85411581-103. PARTS REPLACED WITH NEW. ACFT RETURNED TO SERVICE.Jul 29, 2011 · Dhav DHC8311SDR FDEA201107293031Seal · wornPANEL 475CL FWD FINGER SEAL IS WORN APPROX 20 PERCENT ACROSS THE RT SIDE. REMOVED SEAL , FABRICATED NEW SEAL IAW SRM 51-40-44. INSTALLED NEW SEAL IAW SRM 51-40-21.Jul 29, 2011 · N435FE · Airbus A310203SDR KCSA111180Structure · crackedNR 2 PYLON STRUT CHORD HAS CRACK INDICATION IN AFT I/B LEFT HOLE.Jul 29, 2011 · N746CK · Boeing 747246FSDR UALA2011072703877Cover · unsecureMETAL CLIP HANGING DOWN BELOW RIGHT ENGINE. REMOVED LANYARD AND CLIP THAT HAD BROKEN OFF OF IDG OVERFLOW DRAIN COUPLING COVER, COVER STILL SECURE. SAMC REMARKS: CLOSED AND SECURED IDG ACCESS DOOR ON LEFT CORE COWL AFTER REMOVING LANYARD.Jul 26, 2011 · N669UA · Boeing 767322SDR IPXA11568363Shear Beam · crackedINSPECTION TYPE:C3, WHILE GETTING OK TO INSTALL ACCESS DOOR 445AL ON NR 2 PYLON FOUND SHEAR BEAM CRACKED AT NAC 203.85 AT UPPER INBD CORNER. R & R SHEAR BEAM IAW SRM 51-40-02-0G.Jul 26, 2011 · N401UP · Boeing 75724APFSDR IPXA11568328Angle · crackedINSPECTION TYPE:C3, WHILE INSPECTING FOR OK TO CLOSE ON NR 2 ENGINE PYLON PANEL 445CL, FOUND "L" ANGLE CRACKED AT INBD PYLON STRUCTURE WHERE PANEL ATTACHES TO PYLON. REMOVED, FABRICATED AND INSTALLED NEW "L" ANGLE-CLIP IAW SRM 51-30-01-0G, SRM 51-40-02-0G SRMJul 26, 2011 · N401UP · Boeing 75724APFSDR KCSA111175Rub Strip · wornOUTBOARD RUB STRIP WORN THROUGH JUST FWD OF UPPER AFT MOUNT APPROX NAC STA 221.Jul 26, 2011 · N700CK · Boeing 747246BSDR KCSA111174Rub Strip · wornINBOARD RUB STRIP WORN THROUGH JUST FWD OF UPPER AFT MOUNT APPROX NAC STA 221.Jul 26, 2011 · N700CK · Boeing 747246BSDR UIEA2011072500448Fuse Pin · crackedNR 4 PYLON UPPER LINK FWD MOUNT BOLT THREAD SEIZED AND NDT FOUND CRACKED AT THREAD ROOT AREA. FUSE PIN REPLACED IAW AMM 54-10-03.Jul 25, 2011 · N524MC · Boeing 7472D7BSDR IPXA11568362Attach Bracket · crackedINSPECTION TYPE:C3, WHILE WORKING CC 942638 (ENG 5072) FOUND BONDING STRAP ATTACH PLATE CRACKED ON NR 2 ENGINE AFT FAIRING ACCESS DOOR ATTACH STRUCTURE. REMOVED FABRICATED AND INSTALLED NEW BONDING STRAP ATTACH PLATE IAW SRM 51-4-02-0G, SRM 51-30-01-0G, SRM 5Jul 25, 2011 · N401UP · Boeing 75724APFSDR UALA2011072503777Fairing · bentBENT METAL ON NR 1 ENG PYLON LEFT SIDE ABOVE BURNER SECTION OF ENG, ADJUSTED LIP OF FAIRING.Jul 22, 2011 · N670UA · Boeing 767322SDR FDEA201107202845Support · crackedNR1 PYLON UPPER L/E AUX STRUCTURE WEB SUPPORT RT LIGHTNING HOLE HAS 3 EA CRACKS. COMPLIED WITH SB A300-54-6023, REV NR 1 DATED 02/27/02 BY REINFORCEMENT OF THE NR 1 PYLON CANTILEVER WEB BY ADDING A DOUBLER, COMPLIED WITH EA 6-5450-145606.Jul 20, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107192812Profile · crackedNR 2 PYLON UPPER L/E AUX STRUCTURE WEB SUPPORT LT LIGHTNING HOLE HAS 3EACH CRACKS. 1IN AND 1.5IN LONG (STA. 537 TO 551) INCORPORATED, SB 300-54-6023 REV NR 1 DATED 02/27/02 BY REINFORCEMENT OF THE NR 2 PYLON CANTILEVER WEB BY ADDING A DOUBLER IAW EA 6-5450-14Jul 19, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107182781Support · cracked3 INCH LONG CRACK ON WEB SUPPORT AT NR 1 PYLON INSIDE ACCESS 411CL BELOW FEEDER CABLE RIB 8 COMPLIED WITH SB A300-54-6023, REV NR 1 DATED 02-27-02 RE-ENFORCEMENT OF THE NR 1 PYLON CANTILEVER BUY ADDING DOUBLER UNDER THE HORIZ FIRE WALL AND ON THE LONGITUDIJul 18, 2011 · N654FE · Airbus A300F4605RSDR UALA2011071303510Heat Shield · chafedNR 2 PYLON EXHAUST HEAT SHIELDS (GATORBACKS) NR 2, 3, 4, 5 (FWD TO AFT), FWD EDGE OF SECTIONS HAVE WEAR FROM CHAFING OF GAP SEAL. THIS IS A MAJOR REPAIR REPORT REF: DOCK WU'S K7587X, Q7158E, Q7160E, Q7162E REPAIRED HEAT SHIELDS PER EVA 80988A. REINSTALLED.Jul 13, 2011 · N226UA · Boeing 777222SDR UALA2011071303509Heat Shield · chafedNR 1 PYLON EXHAUST HEAT SHIELDS (GATORBACKS) NR 2, 3, 4, 5 (FWD TO AFT), FWD EDGE OF SECTIONS HAVE WEAR FROM CHAFING OF GAP SEAL. THIS IS A MAJOR REPAIR REPORT REF: DOCK WU'S P5561F, P5563F, P5565F, P5567F. ACP'D REPAIR PER EVA 80987A.Jul 13, 2011 · N226UA · Boeing 777222SDR IPXA11568157Bracket · crackedINSPECTION TYPE:C3 RT BRACKET ON FAIRING 431AT BROKEN (CRACKED). REMOVED CRACKED RT BRACKET, FABRICATED NEW BRACKET AND INSTALLED IAW SRM 51-40-02, SRM 51-40-05, AMM 51-20-00, SRM 51-20-01 AND DRW 313N3100.Jul 13, 2011 · N401UP · Boeing 75724APFSDR AALA20110713AFW03Web · crackedLEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CUTOUT CRACKED. INSTALLED AN INTERNAL DOUBLER WITH SOME HARDWARE/MOUNTING BRACKET CHANGES FOR THE POWER FEEDER CABLES PER MAJOR EA B767-54-017977.Jul 13, 2011 · N376AN · Boeing 767323SDR FDEA201107122667Seal · chafedNR 2 ENGINE LT CORE COWL RAIN SEAL HAS CHAFED MARK TOP INNER AFT SIDE 1 IN LONG. R & R RAIN SEAL IAW SRM 51-72-10, PG 1,2 AND 3 DUE TO NO ALLOWABLE LIMITS.Jul 12, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107092619Shim · unknownWHILE COMPLYING SSIP MOD TO NR 1 STRUT ASSY STRUCTURE, CLEARANCE OF MORE THAN 0.040" SHIMS THICKNESS REQUIRED BETWEEN LOWER SPAR FITTING AND AFT BULKHEAD. ACCOMPLISHED E.A. F-5450-150743. REPAIR IS CLASSIFIED AS MAJOR.Jul 9, 2011 · N950FD · Boeing 757236SDR FDEA201107092629Stiffener · crackedNR 2 PYLON UPPER L/E ACCESS HOLE 424 AR LANDING AREA METAL SEAT CRACKED .5" LONG. REMOVED AND REPLACED STIFFENER IAW SRM 51-40-21 P 7.Jul 9, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107092628Support · cracked2 PYLON UPPER L/E WEB SUPPORT RT LIGHTNING HOLE HAS 4EA CRACKS, 2EA 1.5" LONG AND 2EA 1" LONG, STA 537 TO STA 551. COMPLIED WITH SB A300-54-6023 REV 1. COMPLIED WITH EA 6-5450-145606.Jul 9, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107092627Stiffener · crackedNR 2 PYLON UPPER L/E VERTICAL ANGLE HAS A CRACK 2" LONG AT LT SIDE ACCESS THRU 423AL AND STA 551. COMPLIED WITH SB A300-54-6023.Jul 9, 2011 · N654FE · Airbus A300F4605RSDR FDEA201107092626Angle · crackedNR 2 PYLON UPPER L/E VERTICAL ANGLE HAS CRACK 1.5" LONG RT SIDE ACCESS THRU 424 AR AT STA 551. COMPLIED WITH SB A300-54-6023 REV NR 1.Jul 9, 2011 · N654FE · Airbus A300F4605RSDR CALA2011070800469Fitting · crackedSUPPORT TASK NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD CRACKED. NR 2 PYLON NAC STA 285 TO STA 295 HORI TEE CHORD REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.Jul 7, 2011 · N68159 · Boeing 767224SDR EIAA2011087Structure · damagedNR 2 PYLON I/B SKIRT BENT AND TORN AT I/B DUCT HINGE POINTS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 488-54-041-2A.Jul 6, 2011 · N488EV · Boeing 747230BSDR EIAA2011086Structure · crackedNR 1 PYLON LOWER CENTER AND AFT MOUNT HOLES FOR PRECOOLER LOUVER ASSY CRACKED I/B SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 488-54-043-2.Jul 6, 2011 · N488EV · Boeing 747230BSDR EIAA2011085Structure · crackedNR 4 PYLON PRECOOLER EXHAUST DUCT CUTOUT LOWER AFT CORNER, LOWER ROW OF FASTENERS HOLES 1 EACH CRACKED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 488-54-049-2.Jul 6, 2011 · N488EV · Boeing 747230BSDR FDEA201107022557Angle · crackedNR 2 PYLON AFT TOP U ANGLE SUPPORT IS CRACKED 1 IN LONG THROUGH A FASTENER. HOLE R & R ANGLE IAW SRM 51-40-21, PARA 7.Jul 2, 2011 · N654FE · Airbus A300B4605RSDR K11A2011091291501Flange · cracked2 PYLON UPPER SURFACE TOP FLANGE CRACKED IN RADIUS.Jun 30, 2011 · N915CK · Doug DC915FSDR UALA2011070103273Support Bracket · crackedFOUND CRACKED HYD SUPPORT BRACKET AT NAC STA 180.8. REPLACED DAMAGED HYD SUPPORT BRACKET PER MM.Jun 28, 2011 · N589UA · Boeing 757222SDR LR7A2011063000220Pan · looseDURING SCHEDULED B-1 CHECK IAW JOB CARD HB5701. FOUND NR 3 ENGINE BREAD PAN AFT RT ATTACH STUD WITH LOOSE FIT. REPAIR BY REPLACEMENT ACCOMPLISHED IAW MEA 382-57-11-029.Jun 27, 2011 · N401LC · Lkheed 382GSDR FDEA201106272437Fairing · gougedNR 2 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN INBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 259.0. DAMAGED SKIN ON NR 2 STRUT AFT FAIRING LOWER PAN REPAIRED IAW EA F-5480-146471. REPAIR IS CLASSIFIED AS MAJOR.Jun 27, 2011 · N949FD · Boeing 757236SDR FDEA201106272436Fairing · gouged2 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN OTBD SIDE FOUND WITH PUNCTURE HOLE AT PP STA 259.0. GOUGED SKIN REPAIRED IAW EA F-5480-164671. REPAIR IS CLASSIFIED AS MAJOR.Jun 27, 2011 · N949FD · Boeing 757236SDR FDEA201106272435Fairing · gouged1 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN INBD SIDE FOUND WITH GOUGE MARK AT PP STA 259.0. GOUGE REPAIR CARRIED OUT IAW EA F-5480-146470. REPAIR IS CLASSIFIED AS MAJOR.Jun 27, 2011 · N949FD · Boeing 757236SDR FDEA201106272434Fairing · gougedNR 1 STRUT AFT FAIRING STRUCTURE LOWER PAN EXTERNAL SKIN OTBD SIDE FOUND GOUGED AT PP STA 259.0. GOUGED SKIN REPAIRED IAW EA F-5480-146470 ( LT PYLON AFT FAIRING PAN GOUGE REPAIR). REPAIR IS CLASSIFIED AS MAJOR.Jun 27, 2011 · N949FD · Boeing 757236SDR UALA2011062703148Angle · crackedNR 1 PYLON SUPPORT FOR FINGER SEAL WEAR ANGLE HAS CRACKS AT FASTENER HOLES ON BOTTOM OF PYLON. REMOVED FINGER SEAL ANGLE. PICK UP HOLES IN NEW ANGLE. STARTED TO INSTALL UPPER AFT ANGLE, LOWER SUPPORT WEB IN WORK AREA. COMPLETED INSTALLATIONJun 26, 2011 · N535UA · Boeing 757222SDR JR2R2011062600269Stand Off · crackedLEFT ENGINE LOWER TRANS COWL HAS BROKEN STANDOFF.Jun 26, 2011 · N908FJ · Cndair CL6002D24SDR JR2R2011062600268Stand Off · crackedLEFT ENGINE UPPER TRANS COWL HAS BROKEN STANDOFF.Jun 26, 2011 · N908FJ · Cndair CL6002D24SDR EIAA2011050Panel · corrodedNR 2 PYLON PANEL 462CL HAS CORROSION ON LOWER I/B SIDE OF PYLON IN EDGE RADIUS OF SPAR. REMOVED CORROSION AND REPAIRED PER ECRA 482-54-240-2.Jun 17, 2011 · N482EV · Boeing 747212BSDR A6WA201140709Strip · chafedRT ENG UPPER NOSE COWL AFT SEAL STRIP IS KNIFE EDGED. REMOVED UNSERVICEABLE AFT EDGE STRIP & REPLACED WITH SERVICEABLE AFT EDGE STRIP IAW CMM 71-14-01-300-814-A01.Jun 16, 2011 · N462AW · Cndair CL6002B19SDR K11A2012060616009Angle · crackedRIGHT PYLON MID SPAR WEB I/B LOWER ANGLE PREVIOUS REPAIR CRACKED (1 INCH).Jun 14, 2011 · N916CK · Doug DC933FSDR DALA1139030669Structure · crackedDURING HMV A CRACK WAS FOUND ON THE NR 2 PYLON UPPER CHORD RT SIDE FWD END. UPPER CHORD WAS REPAIRED IAW ERA 493120-14 REV ORIG.Jun 10, 2011 · N669DN · Boeing 757232SDR K11A2011080491504Angle · crackedNR 2 PYLON ANGLE CRACK, 1 INCH.Jun 9, 2011 · N915CK · Doug DC915FSDR K11A2011080491503Web · crackedNR 2 PYLON AFT MOUNT WEB CRACKED, .5 INCH CRACK.Jun 8, 2011 · N915CK · Doug DC915FSDR ABXR2011122200058Acoustic Liner · corrodedNR 1 ENGINE INLET COWL INNER BARREL ACOUSTIC LINER CORRODED AT 4 O'CLOCK POSITION. REPAIRED INNER ACOUSTIC BARREL PANEL ON CWO 23052-0001 IAW ROHR MM 71-11-16, REPAIR NR 15, REV 40, FEB 1/11.Jun 7, 2011 · N734AG · Boeing 76725DSDR IXXA11SMN078SAngle · crackedDURING ROUTINE C-CHECK INSP FOUND NR 4 PYLON INTERNAL ANGLE CRACKED AT STATION YN 321.397 AND STA XRS 495.665. REMOVED FASTENERS AS NEEDED TO PERFORM REPAIR. REMOVED DAMAGED AREA. PERFORMED NDT INSP. NO DISCREPANCY FOUND. FABRICATED REPAIR ANGLE, STRAP DOUBJun 6, 2011 · N830BX · Doug DC871FSDR A6WA201140442Retainer · crackedRT LWR PYLON PANEL 422DB SEAL RETAINER CRACKED. REMOVED UNSERVICEABLE SEAL RETAINER INSTALLED SERVICEABLE RETAINER AND SEAL.Jun 6, 2011 · N469AW · Cndair CL6002B19SDR DALA1138309861Web · crackedNR 2 PYLON AFT ENGINE MOUNT LWR SUPPORT STRUCTURE WEB AND EXISTING REPAIR CRACKED STA YN 174 VIEWED THRU ACCESS DOOR 8206A. NDT VERIFIED CRACK IN DOUBLER APPROX 2 INCHES LONG. REMOVED REPAIR DOUBLER PER DC9 SRM 51-30-2. STOP HOLE ON CRACK PER DC9 SRM 54-01Jun 6, 2011 · N770NC · Doug DC951SDR FDEA201106052123Fitting · corrodedNR2 PYLON SPIGOT RECEPTACLE FITTING HAS PITTING CORROSION ON UPPER PLATE. REMOVED NR 2 PYLON IAW AMM 54-50-00-4 REMOVED AND REPLACED UPPER AND LOWER SPIGOT FITTING IAW S/B 54-20-20 PAR. B(6) REINSTALLED NR 2 PYLON IAW AMM 54-50-00-4 COMPLIED WITH FEDEX EA 6Jun 5, 2011 · N817FD · Airbus A310304
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