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 FDKA200705244Angle · damagedLEFT UPPER COWLING, INBOARD ANGLE IS DAMAGED. THE DAMAGED ANGLE HAS BEEN REMOVED AND REPLACED.May 25, 2007 · N831MJ · Emb EMB145LRSDR 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.May 23, 2007 · N318UP · Boeing 76734AFSDR 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 SRMay 21, 2007 · N432FE · Airbus A310203SDR 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.May 7, 2007 · N465FE · Boeing 727225SDR 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 RETUMay 3, 2007 · N104UA · Boeing 747422SDR 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. GMay 3, 2007 · N104UA · Boeing 747422SDR MASA200700238Angle · damagedLT PYLON WAS DAMAGED BY ENGINE FAILURE. REMOVED AND REPLACED PYLON ANGLES 601-37051-3 AND 601-37051-7.Apr 24, 2007 · N17337 · Cndair CL6002B19SDR 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.Apr 21, 2007 · N751NW · Doug DC941SDR 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 WEREApr 20, 2007 · N182DN · Boeing 767332SDR 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.Apr 17, 2007 · N183DN · Boeing 767332SDR HNAA0700058Stiffener · crackedSTIFFENER CRACKED ON TOP AFT NACELLE PANEL. REPLACED STIFFENER.Apr 12, 2007 · N331EN · Dhav DHC8311SDR 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.Apr 6, 2007 · N903AX · Doug DC932SDR KCSA071079Angle · crackedNR 2 PYLON STA 219 ANGLE CRACKED .75 INCH.Mar 23, 2007 · N701CK · Boeing 747236BSDR 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)Mar 7, 2007 · N908FX · Aerosp ATR42300SDR DALA1104311401Heat Shield · unknownLT AND RT PYLON INBD STRUT FAIRING MID AND AFT PANEL HEAT SHIELD REPAIRED IAW EA 01-097116-03, ME01, ME02.Mar 2, 2007 · N140LL · Boeing 767332SDR 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.Feb 16, 2007 · N412SW · Cndair CL6002B19SDR 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.Feb 15, 2007 · N683UP · Boeing 747121SDR 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.Feb 13, 2007 · N793AX · Boeing 767281SDR 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.Feb 12, 2007 · N793AX · Boeing 767281SDR 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.Feb 9, 2007 · N407FE · Airbus A310203SDR 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 & HEAFeb 8, 2007 · N643UA · Boeing 767322SDR 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.Feb 2, 2007 · N831AW · Airbus A319132SDR 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.Jan 31, 2007 · N869AS · Cndair CL6002B19SDR 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 Jan 31, 2007 · N584HA · Boeing 767300SDR 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.Jan 31, 2007 · N584HA · Boeing 767300SDR 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.Jan 31, 2007 · N584HA · Boeing 767300SDR 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.Jan 29, 2007 · N217UA · Boeing 777222SDR 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.Jan 29, 2007 · N217UA · Boeing 777222SDR 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.Jan 17, 2007 · N402LC · Lkheed 382GSDR 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.Jan 3, 2007 · N501UW · Boeing 737301SDR 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.Dec 18, 2006 · N620NW · Doug DC932SDR 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.Dec 14, 2006 · N737DX · Boeing 737400SDR 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 SPLIDec 11, 2006 · N657UA · Boeing 767322SDR CA061123006Cap · cracked(CAN) CRACK NOTED AT LT NACELLE CANTED BULKHEAD CAP. CAP REPAIRED. (TC NR 20061123006)Nov 20, 2006 · Cessna 414SDR DL757060963Bushing · migratedTHE NR 1 PYLON DIAGONAL BRACE WING FITTING OUTBOARD BUSHING IS MIGRATED. THE BUSHING WAS REMOVED AND THE HOLE INSPECTED. BUSHING WAS REINSTALLED.Nov 13, 2006 · N629DL · Boeing 757232SDR DALA1133760682Link · damagedNACELLE STRUT UPPER LINK WING AND STRUT FITTING BUSHING REPLACED IAW EA 06-075079-03, ME01, ME02.Nov 8, 2006 · N682DA · Boeing 757232SDR 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.Nov 7, 2006 · N783AX · Boeing 767281SDR 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.Nov 6, 2006 · N783AX · Boeing 767281SDR QXEA200602903Beam · damagedC3 YYC - LEFT NACELLE UPPER LATCH BEAM, NEW DAMAGE FOUND AT PREVIOUS BLENDOUT LOCATION, NICKS. REPAIRED IAW REO670-54-21-697.Oct 21, 2006 · N601QX · Cndair CL6002C10SDR ASAA0671097Seal · damagedRIGHT NR 2 ENGINE UPPER PANEL 44 AT FWD INBOARD METAL SEAL IS DAMAGED. REPAIRED IAW SRM 51 40 02.Oct 18, 2006 · N607AS · Boeing 737790SDR 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 CENTEOct 13, 2006 · N427XJ · Saab 340BSDR 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 (INTERNAOct 12, 2006 · N585HA · Boeing 767300SDR KCSA061400Stiffener · chafedNR 1 PYLON AFT BULKHEAD AFT SIDE AT NAC STA 265.94 LEFT SIDE T-ANGLE CHAFED THRU AT ADP COMPENSATOR DUCT HOLE.Oct 5, 2006 · N709CK · Boeing 747132SDR 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.Oct 4, 2006 · N709CK · Boeing 747132SDR 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 CRJ20Oct 2, 2006 · N957SW · Cndair CL6002B19SDR 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.Sep 26, 2006 · N586HA · Boeing 767300SDR KCSA061350Stiffener · crackedNR 4 PYLON NAC STA 180 FORWARD SIDE OF BULKHEAD INBOARD VERTICAL STIFFENER IS CRACKED.Sep 21, 2006 · N709CK · Boeing 747132SDR 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.Sep 15, 2006 · N580FE · Doug MD11SDR 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.Sep 13, 2006 · N586HA · Boeing 767300SDR 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 DETAISep 13, 2006 · N580FE · Doug MD11
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