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 IPXA201408083889Intercostal · crackedINSPECTION 4C, APPOXIMATELY ONE INCH LONG CRACK AT NR 2 LOWER PYLON REAR CENTER SPAR TO REAR SPAR LOWER INTERCOSTAL. ACCOMPLISHED DOUBLER REPAIR IAW SRM-55-30-02, FIG 204, REPAIR 7.Jul 18, 2014 · N255UP · Doug MD11FSDR IXXA20140718019Beam · crackedNUMBER 1 PYLON INBOUND LOWER BEAM INSIDE ACCESS DOOR 437BL IS WORN THROUGH AT FWD END & FASTENER HOLES ARE WORN. NR 1 PYLON INBOUND LOWER BEAM R & R IAW DWG 313T1380.Jul 18, 2014 · N791AX · Boeing 767281SDR DALA2014071604118Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE ON RT FORWARD PYLON OTBD SIDE BETWEEN RIB 5-RIB 6 CANTILEVER STRUCTURE. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE ON RT FORWARD PYLON OTBD SIDE BETWEEN RIB 5-RIB 6 CANTILEVER STRUCTURE IAW SRM 54-52-12.Jul 15, 2014 · N323US · Airbus A320211SDR DALA2014071604116Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE ON LT FORWARD PYLON INBD SIDE BETWEEN RIB 5-RIB 6 CANTILEVER STRUCTURE. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE ON LT FORWARD PYLON INBD SIDE BETWEEN RIB 5 TO RIB 6 CANTILEVER STRUCTURE IAW SRM 54-52-12, PARJul 15, 2014 · N323US · Airbus A320211SDR SWIA201438769Support Bracket · crackedCRACKED SUPPORT BRACKET, LT ENGINE, AFT OF NOSE COWL AT 12 O`CLOCK. C-CHECK, REMOVED SUPPORT BRACKET AND INSTALLED REPAIRED BRACKET IAW REO.Jul 14, 2014 · N937SW · Cndair CL6002B19SDR FDEA201407121753Stiffener · crackedNUMBER 3 ENG PYLON AFT LOWER FAIRING HAS CRACK ON LAST TWO STIFFENERS. REMOVED CRACKED RIBS TWO EACH IAW SRM VOL II 51-31-01. GENERATED & REVISED EA 8-5480-T0309537 P1. WELDED CRACKS ON TRAVELER'S T14 1079877 & T14 1079876. LOCATED, DRILLED & INSTALLED TWOJul 12, 2014 · N315FE · Doug MD1030FSDR A6WA201441754Retainer · crackedPYLON PNL 422BT SEAL RETAINER IS CRACKED.Jul 11, 2014 · N444ZW · Cndair CL6002B19SDR FDEA201407101691Intercostal · crackedNR 2 ENG INTERCOSTAL FOUND CRACKED UNDER 363GL. INTERCOSTAL PN AJC7644-33. INSTALLED DOUBLER & FILLER IAW SRM 55-0-00 FIG 5 & EA 8-5530-T0309468.Jul 10, 2014 · N358FE · Doug MD1010FSDR A6WA201441753Retainer · crackedPYLON PNL 412DB SEAL RETAINER IS CRACKED.Jul 9, 2014 · N444ZW · Cndair CL6002B19SDR SWIA201438733Stiffener · crackedLEFT NACELLE FLAP INNER OTBD SIDE STIFFENER CRACKED. C-CHECK, NEW STIFFENER INSTALLED LT NACELLE FLAP INNER OTBD SIDE IAW SRM.Jul 8, 2014 · N271YV · Emb EMB120ERSDR SWIA201438953Support · crackedRT NACELLE BLUE HYDRAULIC SYS HYDRAULIC PACK LOWER SUPPORT FRAME IS CRACKED. C-CHECK, REPLACED LOWER SUPPORT FRAME FOR RT NACELLE BLUE HYDRAULIC PACK.Jul 7, 2014 · N576SW · Emb EMB120ERSDR CALA2014071191433Structure · crackedNUMBER 1 PYLON AS SEEN THROUGH ACCESS PANEL 432BL, WIRE BUNDLE CUT OUT CRACKED. STOP DRILLED CRACK ENDS & FABRICATED THE -12 DOUBLER & -13, -14 & -15 FILLERS & INSTALLED IAW SRM 54-53-02 REPAIR 2. IAW SRM THIS IS A CAT A & SUPPLEMENTAL INSPECTIONS ARE COVEREJul 5, 2014 · N667UA · Boeing 767322SDR YENA20140701121Bearing · wornACFT RETURN TO DEPARTURE DUE TO VIBRATION FELT DURING INITIAL CLIMB. VIBRATION STOPPED WHEN ACFT CLEAN, HAD SLIGHT VIBRATION WHILE CONFIGURING LANDING. PERFORM TSM TASK 27-64-00-810-801A. FOUND UPPER SPHERICAL BEARING ON LINK AT ENG NR 1 PYLON FAIRING, MOVABJul 1, 2014 · N760JB · Airbus A320232SDR USAA2014070200014Shear Pin · looseRON, DURING ACCOMPLISHMENT OF EO 5414P124 THE RT PYLON INBD LOWER LINK FITTING ASSEMBLY WAS FOUND LOOSE. RE-TORQUED & SAFETIED THE LOWER LINK FITTING ASSEMBLY IAW EO 5414P124.Jun 28, 2014 · N961UW · Emb ERJ190100IGWSDR CALA2014063091364Heat Shield · wornNUMBER 2 HEAT SHIELD LE WAS WORN ON NR 2 PYLON. INTERIM REPAIR ON HEAT SHIELD WAS ACCOMPLISHED. VISUAL INSPECTION OF REPAIR AT INTERVAL OF 375 DAYS WITH THRESHOLD OF 6 JULY 2015. AFTER 29 JULY 2017 THE GENERATED CF ITEM CAN BE CLEARED IF INSPECTION OUTLINEDJun 28, 2014 · N224UA · Boeing 777222SDR USAA2014063000035Lock Nut · looseTHE RT PYLON LOWER LINK OTBD FITTING SHEAR PIN LOCKNUT WAS FOUND LOOSE WITH A MIGRATED BUSHING. ACCOMPLISHED A RE-TORQUE OF THE LOCKNUT & INSTALLED THE PROPER SAFETIES.Jun 27, 2014 · N944UW · Emb ERJ190100IGWSDR HYIA20140624001Beam · crackedDURING VISUAL INSPECTION OF NACELLE STRUCTURE AT TURBOCHARGER REMOVAL FOR OTHER MAINTENANCE, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT TURBOCHARGER MOUNT BRACKET ATTACH HOLE AFT SIDE OF BEAM. CORRECTIVE ACTION WILL BE TO R & R BEAM WITH NEW OEMJun 23, 2014 · N4652N · Cessna 402CSDR FDEA201406201493Mount Fitting · corrodedLEFT ENG FWD MOUNT FITTING OTBD SIDE AFT ATTACHED HOLE UPPER SPOT FACE & HOLE FOUND CORROSION. COMPLIED WITH SRM54-51-81-101 PARA 4 A & EA 6-545-T0308811 PT 1 REPAIR LT ENG FWD MOUNT FITTING OTBD SIDE AFT ATTACHED HOLE.Jun 20, 2014 · N660FE · Airbus A300F4605RSDR REXA2014061600618Heat Shield · damagedTASK CARD 900-54-430-301 LT ENG LOWER CORE HEAT SHIELD CORNER PULLING UP ITEM 40 IPC 54-23-01. REPAIRED LT ENG LOWER CORE HEAT SHIELD CORNER IAW EA CRJ954-02663.Jun 16, 2014 · N929XJ · Cndair CL6002D24SDR SIMA20140616004Support Bracket · crackedAFT PIPE SUPPORT CRACKED IN TWO PLACES, INBD CRACK APPROX 10MM IN LENGTH EXTENDING INTO RIVET EAR OTBD CRACK APPROX 25MM ON FOLD OF SUPPORT BRACKET IAW IPC 54-51-00 FIG 21A ITEM 1. REPLACED AFT PIPE SUPPORT BRACKET IAW SRM 51-40-02.Jun 16, 2014 · N626AE · Emb EMB145LRSDR CALA2014061691293Rub Strip · chafedNUMBER 2 PYLON LOWER RUB STRIP FOUND CHAFFED AT RIBS 5 & 10. REPAIRED LOWER SPAR PLATE CNA ANTI- CHAFE IAW SRM54-51-12 P 207 REPAIR 5 BA REQUIRES INSPECTION IAW SRI 54-51-12-2-001-00. INITIAL INSPECTION THRESHOLD TO BEGIN AT 102297 PTT 66543PTC.Jun 15, 2014 · N490UA · Airbus A320232SDR CALA2014061691292Rub Strip · chafedNUMBER 1 PYLON LOWER RUB STRIP CHAFED BETWEEN RIB 5 & RIB 10. REPAIRED LOWER SPAR PLATE CNA ANTI-CHAFE IAW SRM54-51-12 P207 RPR 5 BA. REQUIRES INSPECTION. INITIAL THRESHOLD TO BEGIN AT 102297 PTT 66453 PTC.Jun 15, 2014 · N490UA · Airbus A320232SDR DALA14035613221Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE OF THE RT FORWARD PYLON CANTILEVER STRUCTURE INBD SIDE AT LEVEL RIB 5. REPAIRED SUPPORT ANGLE IAW SRM 54-52-12.Jun 13, 2014 · N321US · Airbus A320211SDR IXXA20140612001Support Angle · crackedNUMBER 2 NACELLE INSIDE PANEL 445AR-BR, OTBD OF DIAGONAL BRACE FWD ATTACH POINT. SUPPORT ANGLE AT FWD CHORD, CRACKED AT FASTENER HOLE TO EDGE. CRACK APPROX 1/4 INCH VERIFIED BY HFEC. CRACK LENGTH .6 INCHES, LOCATION NAC STATION 206.00 TO N/A. PART NAME BRACJun 12, 2014 · N557CM · Boeing 7572B6SDR UIEA2014060900227Attach Angle · crackedNUMBER 1 PYLON AFT FAIRING SUPPORT FRAME LT ATTACH ANGLE FOUND CRACKED. NR 1 PYLON AFT FAIRING SUPPORT FRAME LT ATTACH ANGLE REPLACED & INSTALLED IAW SRM 51-10-02.Jun 9, 2014 · N644GT · Boeing 7673JHFSDR DALA14034343221Support Angle · crackedDURING INSPECTION, FOUND CRACK ON SUPPORT ANGLE OF THE LT UPPER PYLON INBD SIDE AT LEVEL RIB 5 CANTILEVER STRUCTURE. PERFORMED PERMANENT REPAIR ON SUPPORT ANGLE OF THE LT UPPER PYLON INBD SIDE AT LEVEL RIB 5 CANTILEVER STRUCTURE IAW SRM 54-52-12 PARA 5N, FIJun 9, 2014 · N321US · Airbus A320211SDR SWAA2014070129555Support Angle · crackedRIGHT PYLON ACCESS PANEL SUPPORT ANGLE CRACKED. R & R ANGLE IAW SRM.Jun 5, 2014 · N515SW · Boeing 7375H4SDR SWAA2014062329332Support Angle · crackedNUMBER 1 ENG STRUT TORQUE BOX INBD SUPPORT ANGLE CRACKED AT INTERNAL AREA ACCESS PANEL N5758L. R & R ANGLE IAW SRM & DWG.Jun 5, 2014 · N515SW · Boeing 7375H4SDR SWAA2014062329331Support Angle · crackedNUMBER 1 ENG STRUT TORQUE BOX SUPPORT ANGLE CRACKED AT INTERNAL AREA ACCESS PANEL N5757L. R & R ANGLE IAW SRM & DWG.Jun 5, 2014 · N515SW · Boeing 7375H4SDR SWAA2014062329330Support Angle · crackedRIGHT PYLON SUPPORT ANGLE CRACKED AT INTERNAL AREA OF STRUT TORQUE BOX AT ACCESS PANEL 5857R INBD SIDE. R & R ANGLE IAW SRM & DWG.Jun 5, 2014 · N515SW · Boeing 7375H4SDR SWAA2014061629077Angle · crackedNUMBER 2 PYLON LOWER SUPPORT STRUCTURE OF ACCESS PANEL 5858R ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.Jun 5, 2014 · N646SW · Boeing 7373H4SDR SWAA2014061629071Fitting · crackedRIGHT PYLON FWD UPPER STRUT STRUCTURE SUPPORT OF ACCESS PANEL 5847R CLIP CRACKED. R & R CLIP IAW SRM & DWG.Jun 5, 2014 · N515SW · Boeing 7375H4SDR CALA2014060991229Angle · crackedNR 2 PYLON HAS A CRACKED ANGLE OTBD SIDE NEAR RIB 6. CUT OUT CRACKED SPAR OTBD SIDE NEAR RIB 6 IAW SRM 54-52-12 FIG 211 SH 2. FABRICATED REPAIR SPLICE & INSTALLED SPLICE REPAIR IAW SRM 54-52-12. THIS REPAIR DOES NOT REQUIRE SRI INSPECTIONS IAW ABOVE SRM.Jun 5, 2014 · N844UA · Airbus A319131SDR ABXA20140604192Splice Plate · crackedCANOE PANEL 447DB ATTACH POINT TO NACELLE LT SIDE NUTPLATE CHORD CRACKED 1.25 INCHES BETWEEN NUTPLATES AT LOWER END. ORIGINAL NR 4788O-0000-0365 WRITTEN FOR CHAFE IN SAME AREA. PAINT & NUTPLATES TO BE REINSTALLED ON THIS NR AFTER REPAIR. CRACK CONFIRMED WITJun 4, 2014 · N790AX · Boeing 767281SDR R61A201405290731Stiffener · crackedDURING HEAVY CHECK, RT PYLON STIFFENER ON OTBD SIDE CRACKED, MX R & R STIFFENER IAW SRM 51-43-02, 51-41-02.May 29, 2014 · N807MD · Emb ERJ170100SUSDR AALA20140524004Stiffener · crackedRIGHT PYLON STIFFENER CRACKED 2 INCHES AFT OF INBD FRAME CHORD AT STATION 285.450. R & R STIFFENER IAW SRM 51-10-02-0G, 51-40-02-0G & DWG 311T2400.May 24, 2014 · N371AA · Boeing 767323SDR QXEA2014050300441Angle · brokenRT NACELLE, STARBOARD SIDE AFT STIFFENING ANGLE HAS A PIECE BROKEN. COMPLETED STEPS 1-3 OF EO 54-L02645. PERFORMED ET INSP ON RT NACELLE STBD SIDE AFT STIFFENING ANGLE CUT OUT IAW EO 54-L02645 AND NDTM PT.1 51-00-06, REV 10 DATED 6/5/13. NO DEFECTS NOTED. C/W May 23, 2014 · N400QX · Bombdr DHC8402SDR R61A201405230716Stiffener · crackedDURING HEAVY CHECK, LT ENGINE AFT PYLON INBD STIFFENER IS CRACKED. MX R & R STIFFENER IAW SRM 51-42-01.May 23, 2014 · N813MA · Emb ERJ170100SUSDR CALA2014052700656Latch · unsecureTWO PYLON LATCHES ON TOP OF NR 2 ENG CAME UP ON ROTATION ON TAKEOFF, AS REPORTED BY EXIT ROW PAX. AIR RETURN TO GUAM INSPECTED THUMBNAIL FAIRING. FOUND TWO EACH LOOSE LATCH HANDLES, LATCH KEEPERS FOUND SECURED. ADJUSTED LATCH HANDLES IAW MM 54-52-01.May 23, 2014 · N24736 · Boeing 737724SDR SWAA2014052828382Fitting · damagedRIGHT PYLON STRUT FITTING OTBD LUG BORE DAMAGED AT ENG MOUNT CROSSBEAM ATTACH POINT. REPAIRED FITTING IAW EA.May 22, 2014 · N359SW · Boeing 7373H4SDR SWAA2014052228275Bracket · crackedRIGHT WING NR 6 FLAP CRACKED ANGLE BRACKET INSIDE RT AFT NACELLE AT NACELLE STATION 267 INBD OF NR 6 FLAP TRANS. R & R BRACKET IAW SRM.May 21, 2014 · N694SW · Boeing 7373T5SDR HYIA2014052303Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE INBD ENG BEAM WAS FOUND TO BE CRACKED AT INBD AFT FACE. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL NEW RT NACELLE INBD ENG BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTMay 20, 2014 · N290CA · Cessna 402CSDR HYIA20140523001Beam · crackedDURING ROUTINE SCHEDULED INSPECTION, THE RT NACELLE CROSSOVER BEAM WAS FOUND TO BE CRACKED AT LWR U CHANNEL. CORRECTIVE ACTION WILL BE TO REMOVE & INSTALL RT NACELLE CROSSOVER BEAM IN ITS ENTIRETY. A SUPPLEMENT TO THIS SDR HAS BEEN SUBMITTED TO FURTHER OUTLIMay 20, 2014 · N290CA · Cessna 402CSDR IPXA2014061383287Tee Fitting · chafed4C INSPECTION, NR 2 ENGINE PYLON ACCESS PANEL 458AR AFT FAIRING TEE FITTING FOUND CHAFED. FABRICATED AND REPLACED TEE FITTING IAW EA 011-5450-01-A5397, REV I/R AND EO 5450-54528-A.May 17, 2014 · N279UP · Doug MD11FSDR SWAA2014071530023Strip · crackedNUMBER 2 PYLON ACCESS PANEL 58720 CRACKED NUTPLATE STRIP OTBD SIDED. REPAIRED STRIP IAW EA.May 16, 2014 · N521SW · Boeing 7375H4SDR SWAA2014060328632Angle · crackedNR 1 ENG SUPPORT STRUT ACCESS 5757L ANGLE CRACKED. R & R ANGLE IAW SRM & DWG.May 10, 2014 · N386SW · Boeing 7373H4SDR REXA2014051400091Stiffener · damagedELONGATED FASTENER HOLE ON THE LT PYLON UPPER STIFFENER WITH A FASTENER HOLE NOMINAL DIAMETER OF .215”. REPAIRED IAW EA CRJ254-02532.May 10, 2014 · N8918B · Cndair CL6002B19SDR A6WA201441534Retainer · crackedLEFT PYLON PANEL 412BT SEAL RETAINER IS CRACKED. REMOVED CRACKED SEAL RETAINER & INSTALLED A NEW SERVICEABLE SEAL RETAINER IAW SRM 51-42-06, 20-40-11 & 51-23-00.May 9, 2014 · N446AW · Cndair CL6002B19SDR ABXA20140508155Channel · crackedNUMBER 2 PYLON OTBD SIDE BEHIND PANEL OPENING 447 ERX IN HYD BAY A CHANNEL IS CRACKED AT APPROXIMATELY NAC STATION 310, CRACK IS 3 INCHES. R & R AFT FAIRING OTBD BEAM IAW DWG 313T 2380 & SRM 51-40-02. CRACKED LENGTH IS 3 INCHES, PN 313T1380-242, PART NAME AFMay 8, 2014 · N785AX · Boeing 767281SDR SWAA2014061128927Grounding Strap · corrodedNR 2 ENG STRUT FWD GND STRAP CORRODED. R &R STRAP IAW DWG & SRM.May 6, 2014 · N557WN · Boeing 737790
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