JASC 5414

Service difficulty reports · 4,361

Reports filed under 5414 · Nacelle/Pylon, Plate/Skin, newest first.

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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"

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SDR UIEA200600073Pylon · wrinkledNR 2 PYLON FOUND WITH WRINKLE SKIN ON RHS FWD OF PYLON VALVE MANUAL CRANK AREA. WRINKLE SKIN INSPECTION CARRIED OUT IAW BOE MSG NUMBER: 1-167645228-9, FOUND SATISFACTORY. REPEAT DETAIL VISUAL INSP EVERY C-CHK, NOT TO EXCCED 18 MONTHS.Apr 3, 2006 · N540MC · Boeing 747243BSDR CA060407008Access Panel · missing(CAN) THE AIRPLANE LANDED AT IT`S DESTINATION WHEN CREW EXITED THE PLANE, THEY NOTICED THAT THE AFT RT BELLY ACCESS PANEL WAS MISSING. NOTHING WAS NOTICED BY CREW WHILE IN FLIGHT (VIBRATIONS). (TC NR 20060407008)Mar 31, 2006 · Bombdr BD7001A10SDR QXEA200600868Skin · crackedPDX - C4 THERE IS A CRACK IN THE RIGHT HAND NACELLE, AT THE FORWARD OUTBOARD CORNER OF THE FORWARD GEAR DOOR CUT OUT. REPAIRED IAW RD 8-54-873.Mar 29, 2006 · N354PH · Dhav DHC8202SDR QXEA200601023Rivet · looseYYC - C4 LEFT NACELLE, UPPER SURFACE, OUTBOARD WING LEADING EDGE TO NACELLE FILLER FAIRING HAS LOOSE RIVETS. REPAIRED IAW DHC-8-200 SRM TASK 20-34-11-370-801.Mar 25, 2006 · N353PH · Dhav DHC8202SDR NACA20060030Panel · gougedLT O/B NACELLE REBATE PNL IS CHAFFED. CLEANED DAMAGED AREA. FOUND GOUGE LWR FWD CORNER .046' DEEP MAX AND CHAFFING .015 DEEP MAX. ORIG THICKNESS OF PART IS .079" PER SRM 54-31-61 FIG 101. MAX ALLOWABLE DAMAGE PER ATR 42 SRM 51-10-10 TBL NR 1 IS .004, FOUND Mar 22, 2006 · N42NC · Aerosp ATR42300SDR NACA20060029Panel · gougedRT NACELLE O/B REBATE PNL IS CHAFFED. CLEANED DAMAGED AREA TO ASSESS DAMAGE. FOUND GOUGE AT LWR FWD CORNER .024" DEEP MAX AND CHAFFING .033" DEEP MAX. ORIG THICKNESS OF PART IS .079" PER ATR 42 SRM 54-31-61 FIG 101 IT#5. MAX ALLOWABLE DAMAGE PER ATR 42 SRM Mar 22, 2006 · N42NC · Aerosp ATR42300SDR NACA20060028Panel · gougedLT NACELLE I/B REBATE PNL GOUGED ON LWR FLANGE. CLEANED DAMAGE AREA TO ACCESS DAMAGE. FOUND GOUGE LWR FWD CORNER .079" DEEP MAX AND CHAFFINGS .036" DEEP MAX. ORIG THICKNESS OF PART IS .079 PER ATR SRM 54-31-61 FIG 101 ITEM 5 REV 76. MAX ALLOWABLE DAMAGE PMar 22, 2006 · N42NC · Aerosp ATR42300SDR NACA20060027Panel · gougedRT NACELLE I/B REBATE PANEL IS GOUGED ON THE LOWER FLANGE. CLEANED DAMAGED AREA TO ASSESS DAMAGE. FOUND GOUGE AT LWR FWD CORNER TO BE .065" DEEP MAX AND CHAFFING TO BE .018" DEEP MAX. ORIGINAL THICKNESS OF PART IS .079" PER ATR 42 SRM CHAPTER 54-31-61 FIG 1Mar 22, 2006 · N42NC · Aerosp ATR42300SDR CALA0600093Skin · crackedINSPECTION FOUND A .5 INCH CRACK IN NR 1 PYLON SKIN AT UPPER FORWARD O/B PANEL, NAC STA 224. A DOUBLER WAS INSTALLED IAW ECRA 5430-01230.Mar 22, 2006 · N14320 · Boeing 7373T0SDR 06FDEA1147Skin · crackedENGINE NR 2 - INLET COWL LIP SKIN WITH 2 CRACKS (3 INCH) AND (.75 INCH) ZONE 05:00 HOURS. REPAIRED IAW CMM 71-11-05, FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Mar 18, 2006 · N801FD · Airbus A310324SDR UIEA200600053Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 291.5 (ACCESS PANEL 453AL). ACCESS PANEL 453AL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9, DATED 15 MARCH 2006 TO CONDUCT DETAIL VISUAL INSPECTIMar 16, 2006 · N540MC · Boeing 747243BSDR UIEA200600054Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 248 (ACCESS PANEL 452DL). ACCESS PANEL 452DL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9, DATED 15 MARCH 2006 TO CONDUCT DETAIL VISUAL INSPECTIONMar 16, 2006 · N540MC · Boeing 747243BSDR UIEA20060053Access Panel · crackedNR 1 PYLON ACCESS PANEL CUT-OUT FOUND CRACKED AT LOWER AFT SIDE FWD OF NAC STA 291.5. (ACCESS PANEL 453AL). ACCESS PANEL 453AL CUT-OUT CRACK REPAIRED AS PER BOEING MSG, NR 1-167526498-2 AND FAA FORM 8100-9 DATED 15 MARCH 2006, TO CONDUCT DETAIL VISUAL INSPECTMar 16, 2006 · N540MC · Boeing 747243BSDR 06FDEA1026Skin · crackedACCOMPLISH MAINTENANCE B-CHECK. NR 2 ENG SMALL CRACKS FOUND ON AIR INLET EXTERIOR SKIN SURFACE AT ZONE BETWEEN NR 5 AND NR 6 HOURS (LIP INLET). REPAIRED PER CMM 71-11-05 FIG 603. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.Mar 13, 2006 · N802FD · Airbus A310324SDR IXXA06SMN098SPanel · crackedDURING ROUTINE C CHECK, RT WING NR 4 PYLON PANEL CRACKED, YN 321.000. PERFORMED MAJOR REPAIR IAW DC8-70 SB 54-93 CONDITION V. REMOVED FASTENERS IAW SB 54-93 PAGE 11 FIG 2 DC8 SRM 51-3-0, DC8 SRM 51-1-21. PERFORMED VISUAL INSPECTION TO PYLON ADAPTER PANEL FOR Mar 9, 2006 · N602AL · Doug DC873FSDR CALA0600082Skin · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 2 PYLON O/B ACCESS PANEL 5824R AT FORWARD UPPER CORNER OF PANEL. A PERMANENT REPAIR WAS PERFORMED IAW ECRA 5430-01204.Mar 7, 2006 · N12313 · Boeing 7373T0SDR QXEA200600635Panel · chafedPDX - C4 CHECK, RIGHT ENGINE NACELLE APERTURE FOR PANEL 422CT IS CHAFED. REPAIRED IAW SRM 54-00-11, SRM 51-00-16 AND SRM 51-20-11.Feb 21, 2006 · N349PH · Dhav DHC8202SDR UIEA200600006Panel · missingON WALKAROUND FOUND NR 1 ENGINE LOWER ACCESS PANEL MISSING.Feb 14, 2006 · N528MC · Boeing 7472D7BSDR CALA0600059Skin · crackedINSPECTION FOUND A .5 INCH CRACK AT FORWARD UPPER CORNER OF NR 2 ENGINE PYLON O/B ACCESS PANEL. AN INTERIM REPAIR HAD BEEN INSTALLED PREVIOUSLY AND THE ITEM WAS PLACED ON DIP. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01204.Feb 13, 2006 · N14324 · Boeing 7373T0SDR HNAA0600011Collar · departedNR 1 HORSE COLLAR CAME UNSECURED DURING FLIGHT. AIRCRAFT WAS ON REPOSITION FLIGHT FROM ROC TO PHL WHEN CAPTAIN NOTICED SPARKS COMING FROM THE NR 1 PROP AREA. DECLARED AN EMERGENCY AND LANDED AT SYR. NR 1 HORSE COLLAR REMAINED IN PLACE UNTIL AIRCRAFT WAS TAXFeb 10, 2006 · N814EX · Dhav DHC8102SDR P5CA0601442Skin · chafedNR 3 PYLON INBOARD SIDE ACCESS PANEL 473BL INTERIOR SKIN AT CUTOUT FORWARD SIDE CHAFING MARKS. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A186.Feb 6, 2006 · N534MC · Boeing 7472F6BSDR P5CA0601441Skin · chafedNR 4 PYLON ACCESS PANEL 483BL CUTOUT, FORWARD INTERNAL SKIN CHAFING MARKS. REPAIRED PER BOEING 8100-9 DATED 24JAN2006 PER EO-4754A186.Feb 6, 2006 · N534MC · Boeing 7472F6BSDR UPS06446219Skin · crackedINSPECTION TYPE:C NR 4 PYLON - SKIN / DOUBLER CRACKED FOUND 3EA FASTENER HOLES ON LEFT LWR EDGE BESIDE AFT UPPER ENG MOUNT FITTING NAC STA 220, (CRACK LENGTH .5 INCH). NR 4 PYLON LEFT LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24. AFTER STOP HOLES DRILFeb 2, 2006 · N522UP · Boeing 747200SDR MALA060047Skin · chafedDURING 4K CHECK IN BNA FOUND RT NACELLE IS CHAFED AT THE 3:00 POSITION INSIDE THE INTAKE OPENING AND HAS BEEN REPAIRED IAW MESABA EO S54146.Feb 1, 2006 · N425XJ · Saab 340BSDR QXEA200600309Skin · chafedYYC - C3 RIGHT HAND NACELLE AFT CORE COWL HAS TWO STRIPS OF CHAFING DAMAGE ON INBOARD SIDE. REPAIRED IAW REO 71-11-525 AND HORIZON AIR EA R-71-133.Jan 21, 2006 · N606QX · Cndair CL6002C10SDR USAA060093Skin · crackedFOUND CRACK NR 1 ENGINE PYLON I/B SIDE AROUND ACCESS HOLE 5724. DOUBLER INSTALLED IAW TR 54-30-10, DEFECT SIZE: 1".Jan 18, 2006 · N775AU · Boeing 7374B7SDR USAA060080Skin · crackedFOUND CRACK NR 1 ENGINE PYLON I/B SIDE AROUND ACCESS HOLE 5724. DOUBLER INSTALLED IAW TR 54-30-10, DEFECT SIZE: 1".Jan 18, 2006 · N775AU · Boeing 7374B7SDR TAMF20060001ODuct · delaminatedDURING WEEKLY CHECK, FOUND DELAMINATION ON NR 1 ENGINE RT T/R (FAN COWL DUCT) INNER SKIN (DAMAGE MEASUREMENT IS 34 BY 13.5 INCH), CAUSED BY LIBERATION OF 2 OUTLET VANES ON IDG AIR/OIL COOLER ASSY P/N 35E38-5. FAN REVERSER P/N 683L136G08 WAS REMOVED AND TEMPORJan 16, 2006 · N770QT · Boeing 767200SDR CALA0600002Skin · crackedINSPECTION FOUND A 0.35 INCH CRACK IN NR 1 ENGINE UPPER PYLON PANEL (SKIN) 5727L. THE CRACK WAS STOP DRILLED AND A REPAIR DOUBLER WAS INSTALLED IAW ECRA 5430-01230, REV B.Jan 8, 2006 · N69311 · Boeing 7373T0SDR 0601048Skin · elongatedREPLACED RT WING TO NR 2 ENGINE AFT FAIRING IB SKIN PANEL DUE TO ELONGATED HOLES.Jan 6, 2006 · N767TW · Boeing 737230CSDR UPS06246087Skin · crackedINSPECTION TYPE:C&SI ENG, NR 1 PYLON SKIN CRACKED AT LEADING EDGE INBOARD SIDE. REPAIR OR REPLACE SKIN. ON REMOVAL OF NR 1 PYLON AND BULLNOSE SEAL IAW SRM 51-30-02 IT WAS NOTED THAT THE ADJACENT FUSELAGE SKIN PANEL WAS DAMAGED BETWEEN BS 1183 AND 1133 S12 REJan 5, 2006 · N938UP · Boeing 727173CSDR 06FDEA0013Skin · chafedFOUND SECTION SKIN IS CHAFED ABOVE RT LWR RAIN GUTTER, BS 1351. REPAIRED SKIN CHAFE OVER RT LWR RAIN GUTTER, BS 1351 PER SRM 54-30-3.Jan 3, 2006 · N191FE · Boeing 72722SDR 2005UALA01495Bushing · corrodedNR 1 PYLON UPPER LINK FITTING, OUTBOARD LUG REQUIRES REWORK DUE TO INBOARD LUG REWORKED. BUSHING REPLACEMENT DUE CORRODED BUSHING. BOTH LUGS MUST BE REWORKED AS A PAIR. REWORKED AND BUSHINGS WERE REPLACED DUE TO CORROSION. BUSHINGS WERE REPLACED PER SRM 54Dec 20, 2005 · N644UA · Boeing 767322SDR 2005UALA01494Skin · crackedNR 1 PYLON INBOARD FWD STRUT SKIN CRACKED AT PANEL 416BR CUTOUT RADIUS. IT WAS PROBABLY CAUSED BY FATIGUE. THE SKIN WAS REPAIRED PER SRM 54-53-01 WITH -1 AND -2 DOUBLERS.Dec 20, 2005 · N644UA · Boeing 767322SDR 05FDEA04382Skin · crackedRIGHT WING UPPER SURFACE PANEL LANDINGS ABOVE NR 2 PYLON BENT & CRACKED. REMOVED AND REPLACED CLOSING RIB NR 8 IAW DWG A572-45361 AND A310-200 SRM 51-40-21. REMOVED AND REPLACED 2 ANGLE LANDINGS IAW A310-200-40-21.Dec 20, 2005 · N450FE · Airbus A310222SDR VNAA0512026Access Panel · missingAFTER FLIGHT THE RT ENGINE NOSE COWL UPPER ACCESS PANEL WAS DISCOVERED MISSING. MAINTENANCE INSTALLED A SERVICEABLE PANEL AND THE AIRCRAFT WAS RELEASED FOR SERVICE.Dec 16, 2005 · N229PS · Cndair CL6002B19SDR USAA051550Skin · crackedLOCATION: IB SIDE OF NR 1 ENGINE PYLON. INSTALLED DOUBLER IAW TR 54-50-07, DEFECT SIZE: .250 IN.Dec 14, 2005 · N591US · Boeing 737301SDR 2005UALA01450Bushing · wornNR 1 PYLON UPPER LINK FITTING, INBOARD LUG, OUTBOARD BUSHING LIP FRETTED. NR 1 PYLON UPPER LINK FITTING, INBD LUG, OUTBD BUSHING LIP FRETTED. IT WAS PROBABLY CAUSED BY TOLERANCE BUILD UP. BUSHING WAS REPLACED PER SRM 54-51-93.Dec 13, 2005 · N644UA · Boeing 767322SDR 2005UALA01449Bushing · rotatedNR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBOARD AND OUTBOARD BUSHINGS HAS EVIDENCE OF ROTATION IN THE BORE. NR 1 PYLON DIAGONAL BRACE FITTING AT STRUT ATTACH, FWD INBD AND OUTBD BUSHINGS HAVE EVIDENCE OF ROTATION IN THE BORE. MIGRATION CAUSE IS Dec 13, 2005 · N644UA · Boeing 767322SDR AU510002179Fairing · missing(AUS) NR 2 ENGINE UPPER LT (A) FRAME FAIRINGS PN UL27562 AND PN UL27561 DAMAGED/MISSING. UPPER HALF DAMAGED AND LOWER HALF MISSING. (CASA NR 510002179)Dec 12, 2005 · Boeing 747438SDR AU510002178Panel · missing(AUS) NR 4 ENGINE VIGV ACCESS PANEL MISSING. INVESTIGATION ALSO FOUND THE LP COMPRESSOR ACOUSTIC LINING DAMAGED AT THE 6 O`CLOCK POSITION WITH A HOLE APPROXIMATELY 150MM BY 100MM (6IN BY 4IN) IN THE SKIN. VIGV CONTROLLER PANEL SUPPORT STRUCTURE ALSO DAMAGED. (Dec 12, 2005 · Boeing 747338SDR AU510002163Panel · missingNR 3 ENGINE IB STRUT ACCESS PANEL MISSING.Dec 12, 2005 · Boeing 74748ESDR AU510002058Panel · missing(AUS) NR4 ENGINE LOWER (A) FRAME SEALING FAIRING UPPER PANEL MISSING AND LOWER FAIRING SLIGHTLY DAMAGED ON THE AFT CORNER. SEE ATTACHMENT FOR INVESTIGATION DETAILS. (CASA NR 510002058)Dec 12, 2005 · Boeing 747438SDR AU510001870Skin · crackedRT ENGINE STRUT INBOARD SKIN CRACKED FROM UPPER AFT RADIUS OF 442AL ACCESS PANEL CUTOUT THROUGH RIVET HOLE. CRACK IS LOCATED IN INTERNAL DOUBLER AS WELL. CRACK WAS CONFIRMED USING NDT. CRACK LENGTH APPROXIMATELY 63.5MM (2.5IN).Dec 12, 2005 · Boeing 767338SDR AU510001564Panel · separated(AUS) NR 2 ENGINE IB SAILBOAT FAIRING HYDRAULIC VALVE ACCESS PANEL MISSING. SUSPECT PANEL INCORRECTLY SECURED. IMPACT DAMAGE CAUSED TO LEADING EDGE OF LT HORIZONTAL STABILIZER.Dec 12, 2005 · Boeing 747*SDR 05FDEA04061Repair · unknownPREVIOUS REPAIR INSTALLED ON NR 1 PYLON LT SIDE OB AFT LWR FAIRING EXTERNAL DOUBLER AT RIB 20, NEEDS EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR FOUND NOT TO BE I/A/W A310-200 SRM 54-54-51 FIG 203. REMOVED EXISTING REPAIR I/Dec 1, 2005 · N423FE · Airbus A310203SDR UPS05M45812Skin · crackedINSPECTION TYPE:N/A NR 1 ENGINE OUTBOARD PYLON HAS 1.5 INCH CRACK THRU A RIVET. REPAIRED PER SRM 54-00-01.Nov 19, 2005 · N277UP · Doug MD11FSDR IXXA05RNG096SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON ON UPPER SKIN AT PYLON NR 2 LEADING EDGE UPPER SKIN, LT. CORROSION WAS REMOVED IAW DC8 SRM 51-1-8 PAGE 20, THICKNESS MEASUREMENT WAS PERROMED IAW ASTME 797-01 AND IT WAS FOUND OUT OF LIMITS IAW DC8 SRM 57-2-0 PAGENov 3, 2005 · N721CX · Doug DC872SDR QXEA200501612Skin · gougedYYC DURING C3 CHECK, RIGHT NACELLE AFT CORE COWL HAS NUMEROUS GOUGES ON INBOARD SIDE (LOWER EXTERNAL). MAINTENANCE REMOVED DAMAGE IAW CRJ-700 SRM 51-12-00-001-001-A01. RESTORED FINISH.Oct 31, 2005 · N603QX · Cndair CL6002C10SDR IXXA05RNG093SSkin · corrodedDURING INSPECTION CHECK WAS FOUND A CORROSION ON THE UPPER SKIN AT OB PYLON NR 4-RT. DAMAGED AREA WAS CLEANED AND REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-2-1 FIG 38 AND EWO ATI 57-058.Oct 28, 2005 · N721CX · Doug DC872
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