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.
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
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 FDKA200705244Angle · damagedLEFT UPPER COWLING, INBOARD ANGLE IS DAMAGED. THE DAMAGED ANGLE HAS BEEN REMOVED AND REPLACED.SDR UPS07649950Support · crackedINSPECTION TYPE:C1 NR 2 PYLON AFT VERTICAL PNL SUPPORT IS CHAFED FOR ACCESS PNL 447AL. FABRICATED NEW SPLICE PLATE PER SRM 51-40-05-06, SRM 51-30-01-06 AND SRM 51-40-08-05 AND GOODRICH ER 07-2526.SDR 07FDEA01863Bracket · crackedPYLON NR 1 AT AFT T/E LOWER SECTION LOWER FAIRING INNER "A" FRAME SUPPORT BRACKET HAS A CRACK (APPROX 3" LONG) VISIBLE THRU OPEN ACCESS NR 474DR AND BETWEEN RIB 20-21 THRU LIGHTENING HOLE. REMOVED AND REPLACED WEB IAW SRM 51-40-21. LOCATED AND DRILLED IAW SRSDR 07FDEA01712Bracket · crackedNR 3 PYLON HOLE "P" BRACKET CRACKED FWD OUTBD SEEN INSIDE PYLON AS PER STEP4. 2 ON W/C 7-5410-7-3304. REMOVED AND REPLACED ANGLE( 69-16917-2) IAW SRM 51-30-2 AND 51-10-4. NDT CHECKED "P" HOLE FOR CRACK AND NO CRACK NOTED IAW NTM 51-00-11.SDR 2007UALA01382Fitting · corrodedLIGHT CORROSION - BOTH DIAGONAL SIDE BRACE WING FITTING LUG BORE AT NR 4 PYLON. [SUP 05-29-07] ACCOMPLISHED BORING THE DUAL SIDE BRACE WING FITTING LUG BOTH HOLES PER COA 899993040 & SB 747-54A2218. FINAL HOLE DIA: INBD=2.2449, OUTBD=2.2750. A/C OK FOR RETUSDR 2007UALA01381Fitting · corrodedLIGHT CORROSION - RIGHT DIAGONAL SIDE BRACE STRUT FITTING LUG BORE AT NR 4 PYLON. [SUP 05-29-07] ACCOMPLISHED BORING OF THE STRUT DUAL SIDE BRACE FTG LUG OUTBD HOLE PER COA 899993040 AND SB 747-54A2218 FIG 8. FINAL HOLE SIZE = 2.2450". A/C OK FOR SERVICE. GSDR MASA200700238Angle · damagedLT PYLON WAS DAMAGED BY ENGINE FAILURE. REMOVED AND REPLACED PYLON ANGLES 601-37051-3 AND 601-37051-7.SDR NWAA071519751Web · crackedDURING SCHEDULED ENGINE CHANGE, FOUND CRACK IN LOWER EDGE OF RT PYLON CLOSURE WEB LIGHTENING HOLE AT STA YN 164. REPAIRED PER EA 97-208937.SDR DL76L070340Angle · crackedDURING ACCOMPLISHMENT OF INSPECTIONS OF THE NR 2 PYLON MIDSPAR FITTINGS AND CLOSEOUT ANGLE PER OPN 5281AD (01-074944-12). THE CLOSEOUT ANGLE WAS FOUND CRACKED IN THE TYPICAL LOCATIONS AT THE FASTENERS COMMON TO THE MIDSPAR FITTINGS. THE MID SPAR FITTINGS WERESDR DL76L070374Web · crackedNR 1 PYLON UPPER WEB WHERE WIRE HARNESS RUNS THROUGH, CRACKED 2 PLACES. INSTALLED NEW STIFFENER AND INSTALLED DOUBLERS AND FILLERS PER B767 SRM 54-53-02. ITEM WORKED DURING HMV IN GSO ON N/R CARD 20538.SDR HNAA0700058Stiffener · crackedSTIFFENER CRACKED ON TOP AFT NACELLE PANEL. REPLACED STIFFENER.SDR ABXA070147Angle · crackedANGLE CRACKED - PYLON AFT SPAR, AFT SIDE, LOWER STRAP, OUTBOARD END - JUST INBOARD OF AFT ENGINE MOUNT. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-5.SDR KCSA071079Angle · crackedNR 2 PYLON STA 219 ANGLE CRACKED .75 INCH.SDR COEA0705908Flange · damagedFRETTING DAMAGE FOUND ON LEFT NACELLE REBATE FLANGE COMMON TO PANEL 476AR. REMOVED REBATE PANEL. FABRICATED AND INSTALLED NEW REBATEPANEL IAW ATR SRM. (M)SDR DALA1104311401Heat Shield · unknownLT AND RT PYLON INBD STRUT FAIRING MID AND AFT PANEL HEAT SHIELD REPAIRED IAW EA 01-097116-03, ME01, ME02.SDR SWIA200717998Angle · crackedRT PYLON, THERE IS A CRACK IN THE LWR PYLON STRUCTURE AT FS 605, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED FORMED ANGLE REPAIR AT RT PYLON LOWER PYLON SECONDARY STRUCTURE SUPPORT ANGLE PER CRJ200 51-71-59 PG 2 SEC 2A.SDR UPS07449352Web · misrepairedINSPECTION TYPE:C NR 1 PYLON LWR WEB CRACK PREVIOUS REPAIR DOES NOT APPEAR TO COVER ENTIRE CONDITION. CRACK LENGTH .75 INCH. WEB REPAIRED PER SRM 54-10-03 FIG 2.SDR ABXA070058Angle · crackedCRACKS AT FASTENER HOLES LEFT AND RIGHT ON ANGLE INSIDE OF STRUT LOOKING UP THROUGH LIGHTNING HOLE ON AFT END. REMOVED AND REPLACED CRACKED ANGLE IAW B767 SRM 51-40.SDR ABXA070057Angle · crackedNR 1 PYLON TRAILING EDGE PANEL HAS CRACKED ANGLE ON INBOARD SIDE AND BROKEN NUT PLATE ON FORWARD OUTBOARD SIDE. REMOVED AND REPLACED ANGLE ON NR 1 PYLON TRAILING EDGE PANEL ON INBOARD SIDE AND REPLACED NUT PLATE IAW B767 SRM.SDR 07FDEA00430Support Bracket · damaged5 ELONGATED HOLES EXIST AT NR 2 ENGINE PYLON UNDERNEATH HYD SUPPORT BRACKET ACCESS PNL NR 483 CL. REPAIRED PYLON IAW 6-5450-106327.SDR 2007UALA00361Angle · crackedNR 2 PYLON MIDSPAR FITTING CLOSE-OUT ANGLE IS CRACKED, VERIFIED BY HFEC. STOPPED DRILLED CRACK AND INSTALLED STRAP REPAIR PER REO-G11942 REV C. PER UAL EVA-70073. MUST REPLACE CLOSE OUT ANGLE AT C-16-HMV VISIT. A/C RETURNED TO SERVICE. SUSPECT VIBRATION & HEASDR AWXA200700212Support Angle · crackedSAL - NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSION) CRACKED, RIB 8. REPLACED NR 2 PYLON SUPPORT ANGLE (OUTBOARD EXTRUSION), RIB 8 IAW A319 SRM 51-72-11.SDR SWIA200717943Support Angle · crackedENG BEAM RBL8.0 UPPER WEB SUPPORT ANGLE CRACKED, DISCOVERED DURING C-CHECK INSPECTION. INSTALLED NEW SUPPORT ANGLE AT RBL8.0 UPPER WEB PER CRJ200 SRM 51-42-06 PG 13.SDR HALA0700051Angle · crackedNR 2 ENGINE PYLON AFT FAIRING AFT SKIN OB STIFFENER FWD ANGLE IS CRACKED. REMOVED NR 2 PYLON FAIRING AFT SKIN O/B STIFFENER, FWD ANGLE (P/N 313T3080-69) AND FABRICATED REPLACEMENT ANGLE FROM .063 2034T3 IAW SRM 54-53-71-1A-1 AND SRM 51-70-11-0G-0. INSTALLED SDR HALA0700050Channel · crackedNR 2 ENGINE PYLON AFT FAIRING RT UPPER SUPPORT CHANNEL IS CRACKED AT FWD END. REMOVED DAMAGED RT UPPER SUPPORT CHANNEL O NR 2 ENGINE AFT FAIRING AND INSTALLED A NEW SUPPORT CHANNEL PER SRM 51-40-02.SDR HALA0700049Channel · crackedNR 2 ENGINE PYLON AFT FAIRING LT UPPER SUPPORT CHANNEL IS CRACKED AT FWD END. REMOVED DAMAGED LT SUPPORT CHANNEL ON THE NR 2 ENGINE AFT FAIRING AND INSTALLED A NEW SUPPORT CHANNEL PER SRM 51-40-02.SDR 2007UALA00256Web · damagedNR 1 NACELLE AFT FAIRING LWR WEB HAS 45 PERCENT IACS AT AREA NR 2. REPAIRED PER SRM 51-20-13. REPAIR COMPLETE. OK FOR RETURN TO SERVICE. SUSPECT PREVIOUS HEAT RELEASE INTO FAIRING DUE TO LEAKAGE.SDR 2007UALA00240Web · damagedNR 2 NACELLE AFT FAIRING LWR WEB HAS HEAT DAMAGE OF 44 PERCENT IACS AT AREA NR 3 & 4. REMOVED DAMAGED WEB BACK TO SECTION 5 AND INSTALLED NEW IAW SRM 51-70-13 REPAIR 4. READY FOR SERVICE. SUSPECT PREVIOUS HEAT RELEASE INTO FAIRING DUE TO LEAKAGE.SDR LR7A07007Web · crackedDURING SCHEDULED B 2 CHECK PER JOB CARD HB7201, FOUND NR 3 ENGINE NACELLE OB FAIRING WEB CRACKED AT FS497, WS220. REPAIRED WEB IAW SMP 583 57-40-11 AND LAC MEA 382-54-07-003.SDR USAA07009Skate Angle · crackedNR 1 PYLON O/B SIDE LOWER SKATE ANGLE AT FWD END CRACKED. REPAIRED ANGLES AND INSTALLED SKATE ANGLES IAW EA 98354, DEFECT SIZE: 1 INCH.SDR 0602769620Web · crackedDURING LINE CHECK, FOUND CRACK IN RT PYLON CLOSER WEB AT THE LIGHTENING HOLE LOWER EDGE STATION YN 164. REPAIRED PER EA 96-208511.SDR PIDA06122Strip · wornA WEAR STRIP WAS INSTALLED ON THE I/B SIDE OF THE LEFT ENGINE PYLON PER BOEING SB 737-54-1031 DUE TO WEAR MARKS JUST ABOVE THE THRUST REVERSER SLIDER.SDR 2006UALA02364Angle · crackedNR 2 PYLON MIDSPAR FITTING CLOSE OUT ANGLE, OUTBOARD SIDE, INBOARD FASTENER HAS CRACK INDICATION APPROX .75 INCH LONG LOCATED AFT SIDE. STOP DRILLED THE CRACK AND ACCOMPLISHED HIGH FREQ EDDY CURRENT INSP. CRACK CONTAINMENT CONFIRMED. FABRICATED REPAIR SPLISDR CA061123006Cap · cracked(CAN) CRACK NOTED AT LT NACELLE CANTED BULKHEAD CAP. CAP REPAIRED. (TC NR 20061123006)SDR DL757060963Bushing · migratedTHE NR 1 PYLON DIAGONAL BRACE WING FITTING OUTBOARD BUSHING IS MIGRATED. THE BUSHING WAS REMOVED AND THE HOLE INSPECTED. BUSHING WAS REINSTALLED.SDR DALA1133760682Link · damagedNACELLE STRUT UPPER LINK WING AND STRUT FITTING BUSHING REPLACED IAW EA 06-075079-03, ME01, ME02.SDR ABXA060303Stiffener · crackedSTIFFENER AT REAR OF NR 2 PYLON INBOARD SIDE CRACKED (DOUBLER ON STIFFENER). REMOVED AND REPLACED STIFFENER IAW B767 SRM 54-57-71 REF DWG 313T1380.SDR ABXA060302Stiffener · crackedSTIFFENER AT REAR OF NR 2 PYLON OUTBOARD SIDE CRACKED. REMOVED CRACKED STIFFENER. FABRICATED NEW STIFFENER IAW B767-200 DRAWING 313T3380. INSTALLED NEW ANGLE IAW B767-200 SRM 51-40-02.SDR QXEA200602903Beam · damagedC3 YYC - LEFT NACELLE UPPER LATCH BEAM, NEW DAMAGE FOUND AT PREVIOUS BLENDOUT LOCATION, NICKS. REPAIRED IAW REO670-54-21-697.SDR ASAA0671097Seal · damagedRIGHT NR 2 ENGINE UPPER PANEL 44 AT FWD INBOARD METAL SEAL IS DAMAGED. REPAIRED IAW SRM 51 40 02.SDR MALA060578Channel · crackedDURING COMPLETION OF AN E8 CHECK INSPECTION ON THIS AIRCRAFT, NOTED A CRACK IN THE LOWER CHANNEL OF THE RT ENGINE OB FORWARD COWLING. THE CRACK WAS NOTED IN CHANNEL PN 7271110-274 AND WAS APPROXIMATELY 12 INCHES LONG. CRACK WAS LOCATED IN THE APPROXIMATE CENTESDR HALA0600820Angle · crackedNR 2 PYLON FAIRING HEAT SHIELD INNER PAN INBD ANGLE CRACKED AT NAC STA 325.0. ON NR 2 PYLON FAIRING HEAT SHIELD INNER PAN INBD ANGLE, REMOVED CRACK DAMAGE TO A LENGTH OF .5". HFEC INSP REVEALED DAMAGE REMOVED AND NO CRACKS NOTED. FILLER AND DOUBLER (INTERNASDR KCSA061400Stiffener · chafedNR 1 PYLON AFT BULKHEAD AFT SIDE AT NAC STA 265.94 LEFT SIDE T-ANGLE CHAFED THRU AT ADP COMPENSATOR DUCT HOLE.SDR KCSA061395Web · crackedNR 2 PYLON LOWER MIDSPAR WEB AT NAC STA 221.9 HAS A HALF INCH CRACK JUST AFT OF INBOARD AFT ENGINE MOUNT LEG.SDR SWIA200617506Plate · corrodedRT ENGINE PYLON AFT END BONDING PLATES 3 HAVE CORROSION 2 ON TOP AND 1 ON THE BOTTOM, DISCOVERED DURING C-CHECK INSPECTION. REPLACED 2 TOP AND 1 BOTTOM RT ENGINE PYLON AFT END BONDING PLATE 3 WITH 2024T-3X .016" PO NR 71462, IAW DRAWING NR 601-37012 AND CRJ20SDR HALA0600758Angle · crackedUPON REMOVAL OF NR 2 ENGINE PYLON L-ANGLE CRACKED ON PYLON, 6" AFT OF THE DIAGONAL BRACE FWD ATTACH POINT, NAS STA 308. REMOVED AND REPLACED NR 2 ENG PYLON L-ANGLE 6" AFT OF DIAGONAL BRACE FWD ATTACH POINT NAS STA 308 IAW SRM 51-40-02-0G.SDR KCSA061350Stiffener · crackedNR 4 PYLON NAC STA 180 FORWARD SIDE OF BULKHEAD INBOARD VERTICAL STIFFENER IS CRACKED.SDR 06FDEA03331Bearing · corrodedPYLON NR 3, UPON REMOVAL OF AFT BEARING FOUND CORROSION ON THE BEARING BORE. REPAIR CARRIED OUT AS PER FEDEX EA 1-5410-100698, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR HALA0600757Vapor Barrier · crackedNR 2 PYLON VAPOR BARRIER JUST FWD OF MID SPAR FITTING IS CRACKED. REMOVED AND REPLACED CRACKED VAPOR BARRIER WITH NEW FABRICATED BARRIER, PER EA 311T308-126 AND SRM 51-40-05-0G-0.SDR 06FDEA03273Bearing · corrodedENGINE NR 3 PYLON AFT WING ATTACHMENT BEARING ASSEMBLY FOUND WITH CORROSION. REPAIR CARRIED OUT AS PER FEDEX EA NR 1-5410-100698, TITLE: "NACELLES AND PYLONS, NR 3 PYLON AFT BULKHEAD CORROSION, INTERIM (24 MONTH) REPAIR. REFER TO SNRM N01041 FOR WORK DETAI
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