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.

SDR UIEA2017040200457Seal · tornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200456Seal · tornLEFT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200463Frame · crackedRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE UPPER SECOND FRAME FROM AFT, FOUND CRACKED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200465Frame · wornLEFT ENGINE, RT CORE COWL AFT ZEE FRAME HAS ONE EXISTING REPAIR ANGLE DOUBLER WORN, LOCATED 12 INCHES FROM LOWER EDGE. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200467Rub Strip · wornLEFT ENGINE, RT CORE COWL INTERIOR SURFACE UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200470Structure · damagedLEFT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT CHANNEL. REPAIRED IAW SRM 51-40-02 , REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200472Frame · damagedRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE AFT LOWER CORNER FOUND FASTENER HOLE ELONGATED ON SUPPORT TEE & HAT FRAME. REAMED TO NEXT SIZE AND A NEW FASTENER INSTALLED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200473Rub Strip · wornLEFT ENGINE, RT CORE COWL FAIRING ASSY AFT UPPER EDGE STRIP SEAL FOUND CRACKED. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200474Rub Strip · wornLEFT ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUBSTRIP FOUND WORN. THE RUBSTRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200477Frame · wornRT ENGINE, LT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD ONE EXISTING REPAIR ANGLE DOUBLER FOUND WORN. FRAME REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200478Frame · wornRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE SECOND ZEE FRAME FROM FWD FOUND WORN. THE AREA WAS CLEANED UP AND FOUND WITHIN LIMIT IAW SRM 54-42-02-1A-1, FIG 101, NOTE B, DETAIL 1, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200480Longeron · wornRIGHT ENGINE, RT CORE COWL INTERIOR SURFACE LOWER MOST AFT LONGERON FOUND WORN. LONGERON REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200482Longeron · wornRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE LOWER AFT LONGERON FOUND WORN. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200483Retainer · crackedNR 2 ENGINE, RT FAN COWL INTERIOR SURFACE UPPER AFT EDGE SEAL RETAINER FOUND CRACKED. THE SEAL RETAINER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200487Adapter · wornNR 2 ENGINE, RT FAN COWL INTERIOR SURFACE HOLD OPEN ROD STOW PIN ADAPTER AND FITTING FOUND WORN, LOCATED AT FWD LOWER SECTION. REMOVED AND REPLACED IAW SRM 51-40-02 REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040300493Seal · tornNR 2 ENGINE, RT FAN COWL LOWER EDGE MOST FWD AND SECOND FROM FWD SEALS FOUND TORN. REMOVED AND REPLACED IAW AMM 70-50-00, REV 120.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040400515Structure · erodedNR 2 ENGINE, RT FAN COWL FOUND ERODED. THE NR 2 ENGINE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040400514Structure · erodedNR 2 ENGINE, LT FAN COWL FOUND ERODED. THE FAN COWL WAS REPAIRED IAW SRM 54-22-01, REPAIR 4, REV 103.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040300504Door · wornRIGHT ENGINE, RT CORE COWL PRESSURE RELIEF DOOR SKIN INTERIOR EDGES FOUND WORN. RELIEF DOOR REMOVED AND REPLACED IAW AMM 71-11-09, REV 120. LATCH CHECK CARRIED OUT IAW AMM 71-11-09, REV 120. FOUND SATISFACTORY.Apr 5, 2017 · N1217A · Boeing 767375SDR UIEA2017040200481Channel · crackedRIGHT ENGINE, RT CORE COWL FAIRING AFT UPPER SECTION CHANNEL FOUND CRACKED. CHANNEL REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 3, 2017 · N1217A · Boeing 767375SDR UIEA2017040200486Housing · damagedRT ENGINE, LT CORE COWL AFT KEEPER HOUSING PIN ATTACHING HOLE FOUND ELONGATED & PIN WORN. REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.Apr 3, 2017 · N1217A · Boeing 767375SDR IPXA2017042316388Fairing · chafedINSPECTION TYPE: 3C, NR 2 ENGINE LT FAN COWL DIVERTER FAIRING CHAFE DAMAGE. REPAIRED NOTED CHAFE DAMAGE IAW EA 011-5440-01-A6747 REV IR, AND EO MD11-7110-64008-A.Apr 2, 2017 · N260UP · Doug MD11FSDR R61A201703310304Hinge · crackedMAINTENANCE REPORTED A CRACK ON THE NR 1 ENGINE THRUST REVERSER LATCH ACCESS PANEL HINGE. MAINTENANCE REMOVED AND REPLACED LATCH ACCESS PANEL HINGE IAW SRM 51-42-02, & 51-41-02.Mar 31, 2017 · N647RW · Emb ERJ170100SESDR A6WA2017033044900Louver · crackedRIGHT ENGINE LOWER COWL 442AB LOUVERS CRACKED AT SEVERAL PLACESMar 28, 2017 · N469AW · Cndair CL6002B19SDR IPXA2017041716180Torque Box · corrodedINSPECTION TYPE: D2, CORROSION ON THE NR 2 PYLON RT TORQUE BOX STRUCTURE AT NAC STA 305. REPAIR IAW SRID 3-3851609808.Mar 27, 2017 · N579UP · Boeing 74745ESDR JJBA20172403017Rib · crackedNR 1 NACELLE UPPER AFT DECK SECOND TO LAST RIB CRACKED IN THE CENTER. CRACKED RIBS REMOVED AND NEW ONES FABRICATED AND INSTALLED IAW SRM 51-10-00.Mar 24, 2017 · N359PH · Dhav DHC8202SDR SWIA201743206Latch · chafedRIGHT LOWER TRANSCOWL LATCH DOOR COAMING AND DOUBLER ARE CHAFED AT THE SPIGOT HOLE. PERFORMED PERMANENT REPAIR IAW REO.Mar 20, 2017 · N765SK · Cndair CL6002C10SDR SWIA201743203Fairing · crackedRIGHT ENGINE PANEL 443BB HAS A TWO INCH CRACK AT AFT BOLT HOLE. INSTALLED REPLACEMENT HINGE LINE FAIRING SKIN IAW SRM.Mar 19, 2017 · N765SK · Cndair CL6002C10SDR HALA2017031700111Rib · crackedDURING H CHECK, FOUND LEFT ENGINE PYLON INBOARD RIB 8A CRACKED. REPAIRED THE RIB IAW SRM 54-52-12 C4, FIGURE 208.Mar 17, 2017 · N383HA · Airbus A330243SDR FDEA201703150888Bearing · brokenNR 3 ENGINE PYLON AFT BEARING FOUND BROKEN. COMPLIED WITH EA 1-5450-T0332277, PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.Mar 15, 2017 · N589FE · Doug MD11FSDR DALA2017031301977Bracket · corrodedRT PYLON AFT WEB BRACKET WORN INTO INBD STRUCTURE AT NAC STA 454. REPLACED THE BRACKET IAW SRM 54-52-71.Mar 10, 2017 · N864DA · Boeing 777232SDR DALA2017031301976Structure · corrodedLT PYLON INBD STRUCTURE CORRODED AT NAC STA 39, AND 405. REPAIRED IAW SRM 54-52-71.Mar 10, 2017 · N864DA · Boeing 777232SDR DALA2017031301975Web · corrodedRT PYLON AFT WEB HAS CORROSION AT NAC 375 ON LOWER SURFACE. REPLACED THE WEB IAW SRM 54-52-71.Mar 10, 2017 · N864DA · Boeing 777232SDR DALA2017031301973Bracket · wornRT PYLON AFT WEB BRACKET WORN INTO OTBD STRUCTURE AT NAC STA 454. REPLACED THE BRACKET IAW SRM 54-52-71.Mar 10, 2017 · N864DA · Boeing 777232SDR HYIA20170828002Fitting · crackedDURING A ROUTINE INSPECTION, A CRACK WAS DISCOVERED IN THE RT INBOARD NACELLE FITTING. THE CRACK WAS FOUND ON THE OUTBOARD SIDE OF THE FITTING, JUST FORWARD OF THE SPAR STRAP. THE CRACK IS APPROXIMATELY 1.208 INCHES IN LENGTH. OPENMar 8, 2017 · N36911 · Cessna 402CSDR WVER2017030393803Fastener · missingRIGHT LOWER TRANS COWL HAS A ROW OF MISSING AND LOOSE FASTENERS ON EXTERIOR SKIN AT FWD OTBD ENDMar 3, 2017 · N938LR · Cndair CL6002D24SDR IPXA2017031915293Hinge Fitting · wornINSPECTION TYPE: 3C, NR 3 ENGINE INBD FAN COWL, AFT HINGE FITTING IS WORN. REPAIRED THE HINGE FITTING IAW EA 011-7110-01-A7610, REV. I/R, AND EO MD11-7110-63629-A.Feb 27, 2017 · N287UP · Doug MD11FSDR UIEA2017030300279Frame · damagedNR 1 ENG CORE COWL NR 2 FRAME FOUND DAMAGED. THE FRAME WAS REPAIRED IAW EO 197A116PART 1.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300280Door · damagedL4 AFT FAIRING STRUT DOOR SCREW HOLE ELONGATED. THE STRUT DOOR WAS REPAIRED IAW RI-54-56-11765 REV A.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300282Door · chafedL3 AFT FAIRING STRUT DOOR INNER SURFACE FOUND CHAFED. THE STRUT DOOR WAS REPAIRED IAW RI-54-56-11770 REV A.Feb 27, 2017 · N492MC · Boeing 74747UFSDR UIEA2017030300284Door · crackedL1 AFT FAIRING STRUT DOOR INNER SURFACE FOUND CRACK. STRUT DOOR REPAIRED IAW RI RI-54-56-11740, REV A.Feb 27, 2017 · N492MC · Boeing 74747UFSDR IPXA2017032115384Inlet · gougedINSPECTION TYPE: 3C, NR 2 ENGINE INTAKE LIP HAS SEVERAL GOUGES. REPAIRED INTAKE LIP ASSY IAW EA 011-5430-01-A6713, REV I/R, AND EO MD11-5430-63643-A.Feb 26, 2017 · N287UP · Doug MD11FSDR ABXA2017224017Beam · crackedNR 2 HYD BAY OTBD LOWER BEAM IS CRACKED AT FORWARD SIDE OF 1ST DOOR LATCH FITTING. REMOVED AND REPLACED THE NR 2 PYLON DOOR BEAM IAW SRM 51-40-02. AIRCRAFT WAS GROUNDED.Feb 24, 2017 · N769AX · Boeing 767281SDR IPXA2017022214330Structure · chafedINSPECTION TYPE : C, FOUND CHAFING ON THE NR 1 NACELLE CORE COWL EXTERNAL AFT UPPER CHAFED.Feb 22, 2017 · N343UP · Boeing 76734AFSDR IPXA2017031315050Fitting · damagedINSPECTION TYPE: 3C, RT NR 4 BANJO FITTING CARRY THROUGH CAP HAS A SHEARED FASTENER. REPAIRED THE FITTING IAW MD11-5530-46641-A.Feb 18, 2017 · N287UP · Doug MD11FSDR FDEA201702180586Doubler · crackedNR 3 PYLON UPPER WEB AT YN338, FEED THROUGH HOLE FOR GENERATOR LEAD INSULATOR BOOT, ATTACH FLANGE IS CRACKED AT OTBD SCREW HOLE. REMOVED AND REPLACED DOUBLER IAW SRM 51-31-01,V2. AND DWG AUB 7031.Feb 18, 2017 · N319FE · Doug MD1030FSDR F3LA2017031300090Bushing · corrodedNR 2 PYLON TO WING INBD SHACKLE FITTINGS PRESSED BUSHINGS CORRODED. REMOVED THE NR 2 PYLON TO WING INBD SHACKLE FITTING PRESSED BUSHING AND INSTALLED AND LINE HONED NEW FABRICATED BUSHING IAW TD 802729958-006-2017 AND EA A2-57R-33669.Feb 17, 2017 · N223FR · Airbus A320214SDR IPXA2017030914919Hinge · chafedINSPECTION TYPE: 3C, NR 3 ENGINE FAN COWL ASSY FWD HINGE ASSY HAS THREE AREA OF CHAFE DAMAGE. REPAIRED THE HINGE ASSY IAW EA 011-7110-01-A6683, REV I/R, AND EO MD11-7110-63533-A.Feb 17, 2017 · N287UP · Doug MD11FSDR SWIA201743087Channel · chafed435AB LOWER CORE COWL HAS A CHAFE ON INNER CHANNEL. PERFORMED PERMANENT REPAIR IAW CMM.Feb 11, 2017 · N932EV · Cndair CL6002B19SDR UIEA2017020800168Structure · damagedDURING INBOUND INSPECTION, FOUND NR 1 NACELLE DAMAGED. INSTALLED NACELLE STRUCTURE IAW AMM 71-11-01.Feb 8, 2017 · N780BA · Boeing 747409
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