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.
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
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 YENA20160404278Ball Joint · corrodedCORROSION ON PYLON NR 2 SPIGOT BALL JOINT, REPLACED SPIGOT BEARING IAW AMM 54-51-41-400-001.SDR DALA2016040302558Pylon · damagedNR 1 ENGINE PYLON INBD SIDE BS 102, STRUCTURE HAS A CHAFE AFT SIDE OF STRUCTURE. CUT OUT DAMAGE AREA IAW EA 06-462518-14. FABRICATED DOUBLER REPAIR AND FILLER IAW EA 06-462518-14. INSTALLED REPAIR IAW EA 06-462518-14.SDR DALA2016111808963Fairing · corrodedCORROSION ON MOVABLE FAIRING OF HORIZONTAL WEB INTERNAL AREA ON LT PYLON . REPLACED IAW SRM.SDR IPXA2016033101446Rib · crackedINSPECTION TYPE :1C,2C, NR 2 PYLON PANEL 424CR HAS A CRACK ON RIB, REPAIRED PANEL IAW SRM 54-52-51.SDR SIMA20160325005Yoke · crackedLEFT FWD PYLON LOWER YOKE CRACKED. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386. FOUND DURING INSPECTION WC 54-200-00.SDR WVER2016032500001Transcowl · dentedDURING HEAVY CHECK INSPECTION, A DENT WAS DISCOVERED ON THE LT LOWER TRANSCOWL, LOWER OTBD AREA, MEASURING APPROXIMATELY 2" W X 2" L X .020" D. DENT WAS REPAIRED IAW BSC EO CL600-2D24-71-L03954.SDR IPXA2016042002400Frame · chafedINSPECTION TYPE: 2C, NR 2 ENGINE RT CORE COWL AFT FRAME CHAFE DAMAGE AND ELONGATED FASTENER HOLES REPAIRED CORE COWL IAW EA 011-5420-01-A6204 REV. IR AND EO MD11-7110-60463-A.SDR DALA2016031802067Web · crackedNR 1 PYLON CRACKED UPPER WEB AT NUTPLATE FOR FEEDER CABLE GROMMET BETWEEN TRS. REPAIR C/W IAW ERA 544764-14, REV 0.SDR IPXA2016031500746Shackle · corrodedINSPECTION TYPE:10YR, NR 1 PYLON RIB 18 FWD AND AFT SHACKLE HAVE CORROSION, NICKS, AND CHAFING. REPLACED SHACKLE.SDR IPXA2016031500747Shackle · corrodedINSPECTION TYPE: 10 YR, NR 1 PYLON RUB 18 FWD AND AFT SHACKLES HAVE CORROSION, NICKS, AND SCRATCHES. REPLACED SHACKLE.SDR DALA2016031001830Firewall · wornNR 2 PYLON UPPER FWD OTBD FIRE WALL , OTBD T/R FWD VERTICAL SPRING STEEL STRIKER WEAR PLATE IS EXCESSIVELY WORN. REF N/R 327, ACCOMPLISH SRM 54-51-02, FIG 201, REPAIR OF DAMAGE. ACCOMPLISHED REPAIR IAW SRM 54-51-02, FIG 201, REPAIR 1, ON NR 327.SDR DALA2016030401633Hinge Fitting · damagedELONGATED HOLES ON HINGE FITTING YN=83, 2 EA, YN=111, 2EA, YN=154, 1EA, YN=184, 1EA AND YN=214, 1EA AT LT NACELLE APRON. FITTING BS YN=83 LWR/UPPER, YN=111 UPPER, YN=154 UPPER, YN=214 UPPER WERE REPAIRED IAW CMM 71-10-10 AND ERA 228793-14 AND FITTING BS YN=1SDR N6WA201602280001Structure · damagedDAMAGE FOUND TO LT ENGINE COWLING AT THE 6 O CLOCK POSITON. PERFORMED MAJOR REPAIR IAW REO 670-54-14-1129.SDR FDEA201602270700Web · crackedNR 3 ENG PYLON, UPPER SPAR WEB, RT SIDE AT F HOLE HAS INDICATION UNDER STIFFENER. OLD WEB WAS R & R BECAUSE OF EXCESSIVE CRACKS FOUND ON THE BOTTOM SIDE OF WEB.SDR HNAA2016022200049Fitting · crackedNR 2 ENGINE HOSE COLLAR AFT FLANGE IS CRACKED IN 2 LOCATIONS, BOTH 1" LONG LOCATED 3.5" TO LT OF CENTER BOTH VERTICAL ROWS OF RIVETS. R & R RIVETS AND DAMAGED RADIUS IAW RD8-54-3774.SDR KCSA201602181005Fireshield · chafedNR 2 ENGINE PYLON INBD FIRE SHIELD CHAFED BETWEEN NAC BS 180 TO BS 221.5.SDR ASAA2016021115431Acoustic Panel · wornREF T/C 78472000, NR 2 ENGINE AFT ACOUSTICAL PANEL, 7-8 O`CLOCK ALF, FWD CENTER FASTENER WORN THROUGH PANEL. ACFT GROUNDED. R & R NR 2 ENGINE AFT ACOUSTICAL PANEL 7-8 O`CLOCK POSITION REF AMM 72-23-02.SDR 2016FA0000081Cowl Door · departedTHE LT ENGINE LOWER COWL SEPARATED SHORTLY AFTER TAKEOFF. POST FLIGHT INSPECTION REVEALED THE THREE MOST INBD FORWARD FASTENERS MISSING. ALL OTHER FASTENERS REMAINED INSTALLED IN THEIR RECEPTACLES AFTER SEPARATION WITH THE EXCEPTION OF TWO RANDOM MISSING FASSDR SWIA201641908Panel · chafedPYLON PANEL 443BB CHAFE AT THE AFT END. INSTALLED NEW PANEL 443BB IAW SRM.SDR P5CA2016020400022Frame · chafedNR 1 LEFT CORE COWL NR 2 FRAME FOUND CHAFING NR 1 LT CORE COWL NR 2 FRAME CHAFING MARK AREA REPAIRED IAW NR; RE 71-13-11226, REV A, EO 44TSA.61 REV 0.SDR SIMA20160130002Yoke · crackedRIGHT FWD PYLON LOWER YOKE CRACKED ON THE FWD FLANGE. REMOVED & INSTALLED SERVICEABLE YOKE IAW EO EM-54MR-386.SDR ASAA2016012314970Panel · looseNR 1 ENGINE FAN DUCT PANEL NR 2 HAS LOOSE FASTENERS. ACFT GROUNDED. RESECURED FAN DUCT PANEL IAW AMM 72-23-07-400-801-F00.SDR WVER2016011950201Bracket · crackedBRACKET JUST AFT OF THE FWD LATCH ON THE LT UPPER TRANSCOWL IS CRACKED.SDR KO0R201601060030Failsafe · corrodedNR 1 PYLON HAS EVIDENCE OF CORROSION ON UPPER SPAR LOWER SURFACE AFT OF NACELLE BS 302, BULKHEAD AROUND MULTIPLE FASTENERS.SDR DALA2016011200211Structure · gougedNR 2 CORE COWL AFTER RUB STRIP WAS REMOVED A 4" GOUGE WAS FOUND IN COWL MATERIAL. REMOVED NR 2 ENGINE INBD CORE COWL IAW AMM 71-11-06-004-037-P00. FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 54-41-01, PG 1.0 DETAIL III. INSTALLED A SERVICEABLE CORE COWL IAW AMSDR U2RA201512110002Fairing · dentedNR 3 PYLON OTBD HYDRAULIC ACCESS BAY DOOR HAS 1 DENT. DENT LENGTH 3". ACCOMPLISHED MAJOR REPAIR IAW ASI SOLUTIONS EO 5410ERO2105, REV IR.SDR P5CA2015121400204Strut · crackedCRACK REPAIR ON STRUT NR 2 INBD SIDE SKIN PANEL, NAC BS 221.25 TO 237.5, REF NRC M0538, REPAIR PERFORMED IAW REA MF01084R0148, REV NEW, DATED 29 OCT 15, REA MF0108R0148, REV A, DATED 15 NOV 15 AND AS INSTRUCTED BY SR 4-3029397194, MESSAGE.SDR P5CA2015121100193Hinge Fitting · damagedHINGE FITTING ASSY, WEAR DAMAGE REPAIR ON ENGINE'S NR1 FAN COWL BS 188.2, REPAIR PERFORMED IAW REA MF01084R0071, REV A DATED 13OCT15.SDR CA151221018Fastener · missing(CAN) - DURING ROUTINE MAINTENANCE, OPERATOR FOUND 5 LOCK FASTENERS WERE FOUND MISSING ON THE UPPER SIDE OF THE LT ENGINE PYLON IN SERVICE. - P/N OF MISSING FASTENER : PIN SHEAR HST11AG-8-4 - THE LOOSE COLLARS OF THE FASTENERS WERE FOUND INSIDE THE PYLON AREASDR DALA2015120407485Panel · detachedCLIMBING OUT OF 400' ON TAKEOFF, CAP FAIRING ON LT ENGINE SEPARATED FROM ACFT. DISCOVERED PANEL 431AT DEPARTED ACFT PERFORMED VISUAL INSPECTION OF AREA AFT PANEL 431AT, WING, FUSELAGE, TAIL IAW AMM 05-51-59 INSTALLED SERVICEABLE PANEL 431AT IAW AMM 54-52-01. SDR ABXA20151110207Beam · crackedNUMBER TWO STRUT INTERIOR STRUCTURE IS CRACKED WHERE PANEL 447ERX ATTACHES AT LOWER EDGE. R & R NR 2 PYLON HYD BAY OTBD BEAM WHERE PANEL 447ERX ATTACHES IAW SRM 51-40-02. CRACKED 1.0", PN 313T1380-242, PART NAME BEAM, AFT FAIRING OTBD, SN NSN, STRINGER & WS SDR HYIA11072015001Beam · crackedDURING SCHEDULED INSPECTION THE LT NACELLE CROSSOVER BEAM ASSEMBLY WAS FOUND TO BE CRACKED AT OTBD LOWER U CHANNEL. REMOVAL OF CROSSOVER BEAM ASSEMBLY, DETAILED VISUAL INSPECTION OF SURROUNDING STRUCTURE FOR ADDITIONAL DEFECTS & INSTALLATION OF NEW BEAM ASSEMSDR R61A201510300805Screw · corrodedDURING HEAVY CHECK, AFT PYLON FAIRING, AFT INBD SIDE HARDWARE IS CORRODED ON BONDING JUMPER. MAINTENANCE R & R AFT PYLON FAIRING, AFT INBD SIDE HARDWARE IAW AMM 20-13-21. PN NAS1861-3-9, SCREW.SDR UHLA201510260823Attach Fitting · crackedLT PYLON, INBD AFT ATTACH LINK LUG IS CRACKED. CUTOUT DAMAGE SECTION OF RT CHORD ASSY AND SPLICED IN NEW SECTION OF CHORD ASSY INTO PYLON IAW ETD2015-170-098790.SDR DALA2015103006598Hinge · wornFREEPLAY ON UPPER HINGES OF HARDWARE ON YN=80, NR 1, YN=100 NR 2, YN=184 NR 3 AND YN=214 NR 4, LT APRON PYLON. UPPER HINGES ON BS YN=80, YN=184, AND YN=214 AT LT APRON PYLON WERE REPAIRED AND HARDWARE REPLACED AND FREE PLAY WAS CORRECTED IAW CMM 71-10-10 AND SDR DALA2015102506491Structure · chafedRT NACELLE OTBD SIDE CHAFE ON FIRE SEAL BULKHEAD NAC STA 102, EXISTING REPAIR IS CHAFED. REMOVED DAMAGED DOUBLER AT RT PYLON IAW SRM 51-40-03 ON FIRE SEAL BULKHEAD BS 102, FABRICATED DOUBLER USING TI-6AL-AV-063, PO 6714Q-00039 DIM 8" X 6" IAW EA 06-462518-14 SDR SWIA201541558Structure · chafedRIGHT ENGINE UPPER CORE COWL INNER T/E CHAFED. R & R NEW RT ENGINE UPPER CORE COWL IAW SRM.SDR DALA2015101806340Fitting · corrodedCORROSION ON FORWARD/AFT FITTING BUSHING ON AFT CONEBOLT AT LEFT PYLON. NEW BUSHING INSTALLED IAW DWG 5965645, REV B.SDR KCSA201510161050Fireshield · chafedNR 1 PYLON OTBD FIRESHEILD AT NAC BS 199-212 IS SEPARATED, BENT AND CHAFED.SDR KCSA201510161049Fireshield · chafedNR 4 PYLON INBD LOWER INSIDE EDGE APPROXIMATELY NAC BS 221 HAS WORN RIVETS AND METAL.SDR DXTR2015110902Inlet · dentedDENT ON THE L/E OF THE LT ENGINE NACELLE MEASURING 2.250" X .750" X .100 D AT THE 5 O'CLOCK POSITION WHEN VIEWED LOOKING AFT. COMPLETED REPAIR AS REQUIRED AND REASSEMBLED INLET IAW AQRD ERO-791084-01, REV 1R TITLED "LT ENGINE INLET L/E DENT REPAIR" AND THE SRSDR FDEA201510083119Stiffener · crackedNR 1 PYLON SPAR STIFFENER, FOUND CRACKED BETWEEN RIB 9 & 10 DURING NDT. REPAIRED IAW EA 6-5450-T0320597 P1. MAJOR REPAIR IAW GMM 6-2-100.SDR IPXA2015101694873Plate · corrodedINSPECTION TYPE: 10YR, NR 1 ENGINE PYLON SPHERICAL SPIGOT BEARING PLATE HAS PITTING CORROSION. R & R BEARING PLATE IAW TC 545017-01-3M-471.SDR IPXA2015101694866Bearing · corrodedINSPECTION TYPE:10YR, NR 1 ENGINE PYLON SPHERICAL SPIGOT BEARING HAS PITTING CORROSION. R & R SPIGOT BEARING REF AMM 54-51-78.SDR ASAA2015100613373Panel · looseNR 1 ENGINE INLET AND FAN BLADES DETAILED INSPECTION FOUND NR 1 FAN FRAME PANEL AT RT 12 O'CLOCK POSITION AND NR 5 FAN FRAME PANEL HAS ONE FASTENER LOOSE AND HAS DAMAGED THE PANEL. ACFT GROUNDED. REPLACED FAN DUCT PANEL AT RT 12 O'CLOCK, IAW AMM 72-23-07.SDR ASOA20151005056Yoke · crackedDURING MAINTENANCE THE NR 1 ENGINE FORWARD LOWER YOKE FITTING WAS FOUND TO BE CRACKED. MAINTENANCE REPLACED THE NR 1 ENGINE YOKE FITTING IAW STS EA26-2014-063.SDR R61A201510020750Fastener · corrodedDURING HEAVY CHECK, WIRE HARNESS MOUNTING BRACKET AT SPAR 3 AFT PYLON FAIRING T/E FASTENERS ARE CORRODED. MAINTENANCE R & R WIRE HARNESS MOUNTING BRACKET AT SPAR 3 AFT PYLON FAIRING T/E FASTENERS IAW AMM 20-10-07, PN NAS1801-08-8, SCREW.SDR DALA2015093005883Latch · corrodedNR 1 ENG OTBD FAN COWL HAS COMPOSITE DAMAGE AROUND AFT LATCH. REPAIRED NR 1 ENGINE OTBD FAN COWL IAW PRI 536955-14, REV 0, AND ER/A 536955-14, REV. ORIGINAL.SDR UHLA201509250746Link · corrodedNR 1 ENGINE PYLON OTBD LOWER LINK INBOARD SURFACE HAS CORROSION FOUND UNDER FAIL SAFE ANGLE WHILE PERFORMING CRACKED LOWER LINK REPAIR. PERFORMED ROTO PEAN AND FINAL REPAIR IAW ETD2015-170-085250.SDR DALA2015091505662Stiffener · crackedACFT HAS CRACKED STIFFENER, 11 O`CLOCK POSITION, CRACKED CLIP, 8 O`CLOCK POSITION. SHEARED FASTENERS, 2 O`CLOCK POSITION AND MISSING FASTENER AT 7 O`CLOCK POSITION AT RT ENGINE NOSECOWL. FWD BULKHEAD AFT FACE. CRACKED STIFFENER 11 O`CLOCK, CRACKED CLIP 8 O`C
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