JASC 5414
Service difficulty reports · 4,360
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 SWAA2022011981542Plate · brokenBROKEN SEAL PLATE LOCATED STRUT ACCESS PANEL #441AL ON ENGINE 2 / REPLACED SEAL PLATE LOCATED STRUT ACCESS PANEL #441AL ON ENGINE 2 IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02SDR AALA201705159002Skin · damagedELONGATED HOLE ON LEFT PYLON LOWER BOTTOM SKIN AT MOUNTING PLATE. REPLACED MOUNTING PLATE PER D57251216200.SDR UIEA2017040200466Skin · wornRIGHT ENGINE, LT CORE COWL FAIRING SKIN UPPER AFT CUTOUT SECTION INTERIOR SURFACE FOUND WORN. THE SKIN WAS REPAIRED IAW SRM 54-423-01-2R-5, REPAIR 5 , REV 103.SDR UIEA2017040200471Skin · crackedRIGHT ENGINE, LT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. THE SKIN CUTOUT WAS REPAIRED IAW SRM 54-423-01-2R-4, REPAIR 4, REV 103.SDR UIEA2017040200475Skin · crackedRIGHT ENGINE, RT CORE COWL SKIN UPPER AFT CUTOUT SECTION FOUND CRACKED. REPAIRED IAW SRM 54-42-01-2R-4, REPAIR 4, REV 103.SDR UIEA2017040200476Rivet · looseRIGHT ENGINE, LT CORE COWL INTERIOR SURFACE AFT UPPER PLATE FOUND RIVET LOOSE. THE LOOSE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 103.SDR IPXA2017041616166Skin · crackedINSPECTION TYPE: 3C, NR 2 ENGINE INLET COWL LIP SKIN HAS 13 CRACKS. REPAIRED THE INLET COWL LIP SKIN IAW SRM 54-10-01, REPAIR 4 .SDR UIEA2017040200469Skin · wornRIGHT ENGINE, RT CORE COWL FAIRING SKIN UPPER AFT CUTOUT SECTION INTERIOR SURFACE FOUND WORN. REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, REV 103.SDR WVER2017032905Fastener · looseDURING ACCOMPLISHMENT OF EO 7/9-54-400, FASTENERS WERE FOUND TO BE LOOSE ON BOTH LT AND RT PYLONS. LEFT HAND SIDE-7 LOWER / 4 UPPER. RIGHT HAND SIDE-5 LOWER / 3 UPPER. REPAIRED IAW REO 670-54-51-034 REV-A 2016/04/20.SDR AALA20170419002Skin · corrodedLEFT PYLON CORRODED ON THE RIGHT SIDE OF THE PRESSURE REGULATING AND SHUTOFF VALVE ACCESS PANEL LANDING. REPAIRED IAW SRM 51-10-02-0G AND EA 268826.SDR FDEA201703271182Skin Panel · damagedNR 2 ENGINE LEFT LOWER FORWARD FAN COWL LAND A/C SIDE. A PREVIOUS REPAIR IS DAMAGED AND COMING APART. REPLACED DAMAGED SKIN PANEL NR 2 ENGINE LEFT LOWER FORWARD FAN COWL LAND PER DAC DWG AJC7415, IAW SRM 51-31-01 FIG 11 VOL 2.SDR AALA20170425003Skin · corrodedAIRCRAFT WAS IN BASE MAINTENANCE. LEFT ENGINE PYLON INBOARD SKIN CORRODED AFT OF THE LOWER CHORD FLANGE. REPAIRED IAW EA 268963.SDR DALA2017032302359Skin · crackedNR 2 PYLON LT FWD TORQUE BOX FWD ACCESS DOOR 442AL CUTOUT AREA SKIN FOUND CRACK. REPAIRED PER ERA 555730-14.SDR UIEA2017032200372Panel · corrodedFOUND THE NR 4 NACELLE PANEL CORRODED. ACCOMPLISHED EI Y2017A54M-490 REV 1.SDR DALA2017031702210Skin · crackedNR 2 PYLON RT FWD TORQUE BOX FWD ACCESS DOOR 426BR CUTOUT AREA SKIN FOUND CRACKED. REPAIRED IAW SRM 54-53-01.SDR IPXA2017032415456Skin · crackedINSPECTION TYPE: C10, CRACK ON INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIRED THE PYLON IAW SR 3-3822893601 AND EO B767-5430-63695-A.SDR DALA2017031002058Skin · corrodedSKIN CORRODED ON LIP INLET COWL ON THE NR 1 ENGINE. REMOVED CORROSION IAW SRM.SDR YENA201703070186Skin · damagedDURING HEAVY CHECK MAINTENANCE, FOUND THE NR 1 ENG AFT SECTION OF PYLON BOTTOM WING SKIN PANEL NR 3 SYSTEM MOUNTING PLATE AND GREEN HYD LINE DAMAGED. REPAIRED.SDR IPXA2017031315085Skin · crackedINSPECTION TYPE: 1C, NR 1 PYLON 4 HAS A CRACK ON INTERIOR. REPAIRED IAW SRM 54-52-51SDR ASOA201702221274Skin · dentedPANEL 432 AT IS DAMAGED ALONG FORWARD HINGE LINE AREA (BENT EDGE) LT UPPER. REDRESSED THE SKIN TO ORIGINAL FORM PER ECTC REO 670-54-14-1012.SDR REXA2017021900274Panel · crackedPYLON PANEL 412DB CRACKED THROUGH FASTENER HOLE. A NEW PANEL WAS LOCATED & DRILLED IAW SRM 51-40-11.SDR DALA2017020801055Skin · crackedNR 2 ENGINE RT CORE COWL SKIN HAS A 10 INCH CRACK AT THE TE. REPLACED THE COWL ASSY IAW AMM 71-11-06.SDR IPXA2017022814517Panel · chafedINSPECTION TYPE: 3C, NR 1 PYLON PANEL 437BL CHAFED ON INNER SURFACE. REPAIRED IAW EA 011-5450-01-A6638, REV. IR, AND EO MD11-5450-63262-A.SDR 7C7A2017013100279Skin · crackedLEFT NACELLE FWD DOOR CUT OUT FWD INBD CORNER CRACKED.SDR U2RA201706130003Skin · chafedDURING A D CHECK INSPECTION, FOUND THE NR 4 ENGINE OTBD CORE COWL WITH WEAR GROOVE AT PRE-COOLER EXHAUST DUCT OPENING. REPAIRED IAW EO MAS-J217-N919CA-004.SDR DALA2017012700698Skin Panel · crackedNR 2 PYLON I/B SKIN PANEL: CRACK AT FASTENER. ALSO, ADJACENT FASTENERS ARE LOOSE. C/W REPAIR PER PRI 554683-14, REV1 AND ERA 554683-14 REV ORIGINAL.SDR AN0R2017403006Skin · delaminatedAREAS OF DAMAGE EXIST COMMON TO THE C DUCT BONDED ASSEMBLY, FWD AND AFT SKIN AND FWD INBOARD OUTER SIDEWALL SKIN. THE FWD CENTER INNER SKIN. THE MID CENTER INNER SKIN. THE FWD INBD INNER SIDEWALL SKIN.SDR DALA2017011900476Panel · damagedSEVERAL FASTENERS PULLED THROUGH THE LEFT PYLON FAIRING, LOWER FWD EDGE. REPAIRED THE PANEL IAW 54-00-00 REP 2. FIG 201.SDR QXEA2017011600014Panel · departedON CLIMBOUT FLIGHT ATTENDANT CALLED AND NOTIFIED US THAT A PASSENGER ADVISED THEM A PART FELL OFF THE AIRPLANE AFTER TAKEOFF ON NUMBER NR 2 NACELLE. RETURNED TO FIELD. LANDING UNEVENTFUL. IDENTIFIED MISSING PART AS NR 2 ENGINE FWD SIDE DOOR 422AL. INSTALLED SESDR P5CA2017011200019Skin · dentedNR 2 ENG NOSE COWL INNER BARREL LOWER SIDE IS DENTED. CUT OUT THE DENT SKIN DIA: 0.5" AT 5 O' CLOCK POS OF LOWER ACOUSTIC PANEL AND CLEAN INSTALLED THE SPACER INTO THE HOLE CURED AT 250 FAHRENHEIT FOR 2 HOURS. FILLED THE HOLE WITH ADHESIVE CURED AT 200 FAHRENHSDR DALA2017012500620Fairing · crackedFOUND A CRACK AT RT ENG STRUT AFT PYLON FARING TIME LIMITED REPAIR. ACCOMPLISHED ERA554357-14 TIME LIMITED REPAIR.SDR IPXA2017011912934Skin · crackedINSPECTION TYPE: C10, FOUND A CRACK ON THE INBD SIDE SKIN AND DOUBLER OF THE NR 2 PYLON. REPAIR IAW SR 4-3618994436 AND EO B767-5430-62924-A.SDR IPXA2017013113517Skin · damagedINSPECTION TYPE: 3C, NR 2 PYLON LT LOWER SKIN HAS DAMAGED FASTENERS. REPAIRED THE SKIN IAW EA 011-5450-01-A6588 REV. I/R AND EO MD11-5430-63001-A.SDR DALA2017010700203Skin · crackedCRACKED LT PYLON UPPER SKIN. TRAILING EDGE PYLON LH WAS REMOVED AND INSTALLED IAW SRM 51-30-1. HFEC INSPECTION WAS ACCOMPLISHED.SDR FDEA201612294573Panel · delaminated#2 ENGINE INLET (PICKLE BARREL) PANEL AJC7068 IS DELAMINATED. REPAIRED IAW SRM 51-71-00 VOL 2.SDR SCNA20161222338Plate · wornNR 1 PYLON PANEL 431AT, THUMBNAIL, AFT LOCATOR PLATES ARE WORN. REPLACED THE LOCATOR PLATE.SDR SCNA20161222337Plate · wornNR 2 PYLON PANEL 441AT AFT LOCATOR PLATES WORN. REPLACED THE PLATES.SDR ASOA201712151034Skin · damagedDURING C CHECK, FOUND LOWER FORWARD CORE COWL INNER SKIN DAMAGED RIGHT ENGINE. COMPLIED WITH REPAIR IAW REO 670-54-23-959, & EC/TC REO 670-54-23-959SDR CALA2016120200993Skin · crackedNR 2 PYLON LT SIDE ACCESS PANEL OPENING 446BL, SKIN CRACKED AT UPPER FWD CORNER. REPAIRED IAW SRM 54-53-01 FIG 201,SDR CALA2016120200990Access Panel · crackedNR 2 PYLON INBD SURFACE ACCESS PANEL 446BL FWD UPPER CUT-OUT HAS EVIDENCE OF CRACK. STOP DRILLED CRACK IAW SRM 54-53-01. FABRICATED A REPAIR IAW SRM 54-53-01. INSTALLED THE REPAIR IAW SRM 54-53-01.SDR UIEA2016113000927Skin · chafedNR 2 PYLON SKIN CHAFING LT SIDE. SKIN REPLACED IAW SRM 51-40-02.SDR UIEA2016113000924Skin · chafedNR 1 PYLON INBD UPPER RUB STRIP SKIN CHAFED RT SIDE. REPLACED IAW SRM 51-40-02SDR DALA2016112709383Skin · crackedNR 2 NACELLE STRUT SIDE SKIN PANEL AT FORWARD TORQUE BOX ACCESS HOLE CRACKED AND REPAIRED IAW ERA 271983-14.SDR DALA2016112709382Skin · crackedNR 1 NACELLE STRUT SIDE SKIN PANEL AT FORWARD TORQUE BOX ACCESS HOLE CRACKED. COMPLIED WITH EAR 360779-14.SDR QXEA2016113000764Stiffener · corrodedRIGHT NACELLE PANEL 424AR HAS A FOUR BY FOUR INCH CHAFE ON STIFFENER. REPLACED THE STIFFENER IAW SRM 51-42-05-02-01 AND DWG 85414014, REV E.SDR SWIA201642930Skin · dentedRIGHT UPPER TRANS COWL HAS MULITPLE DENTS. REPLACED RT NACELLE TRANS COWL IAW CMM.SDR KCSA201611141095Fireshield · damagedDAMAGE FIRE-SHIELD ON LOWER EDGE SKIN O/B SIDE OF NR 4 PYLON AT NAC STA 223.0 - 227.0.SDR DALA2016102607721Skin · crackedDURING H CHECK, A CRACK WAS FOUND ON THE NR 1 PYLON ACCESS DOOR CUTOUT. A REPAIR WAS PERFORMED IAW ER/A 551278-14.SDR SWIA201642832Skin · wornRIGHT NACELLE CORE COWL HAS WEAR AT LATCH AREA CAUSED BY BLOCKER DOOR. FABRICATED AND INSTALLED REPAIR PLATE IAW CMM. BLENDED NR 6 BLOCKER DOOR TO OBTAIN THE CORRECT CLEARENCE IAW CMM, CLEARANCE CHECKED GOOD.SDR DALA2016101907570Skin · crackedNR 1 NACELLE STRUT UPPER SPAR O/B WATER DRAIN HOLE FOUND WITH CRACK. C/W ERA 544564-14.
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