JASC 5400
Service difficulty reports · 1,907
Reports filed under 5400 · Nacelle/Pylon 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 = '5400' 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 = '5400' 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 DL72S982487Angle · corrodedFOUND CORROSION ON HEAVYWEIGHT HUSH-KIT MOD ON RT NR 2 ENG AFT MOUNT SUPPORT CHORD ANGLE IN EXCEEDANCE OF MFG MINIMUM ALLOWABLE TOLERANCES. REPLACED RT CHORD ANGLE WITH NEW MFG PART.SDR QXEA9900087Shackle · corrodedPDX - SURFACE CORROSION ON FORWARD SHACKLES IN RIGHT-HAND STUB WING. REPAIRED IAW FOKKER SRM 51-10-4, PAGE 9, PARAGRAPH 5A (1).SDR ABXA9801089Angle · crackedDURING C-CHECK, FOUND VERTICAL ANGLE/BRACKET CRACKED ON OUTBOARD SIDE OF NR 2 PYLON, UNDER THROTTLE CONDUIT JAM NUT. REPLACED BRACKET/ANGLE IAW DC9 SRM.SDR ARWA981124Fasteners · misinstalledC-CHECK, NR 1 AND NR 2 PYLON'S HAVE WRONG FASTENERS INSTALLED IN PLANKS. OPENED REPLACEMENT HOLES TO .260 DIA AND INSTALLED PER EO DRAWING NR 98-014 ON 8110-3, DATED SEPT 28, 1998 UNDER WORK NR 1299.SDR ARWA981117Angle · crackedC-CHECK, 4.5 INCH CRACK TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN336. STOP DRILLED CRACK, INSTALLED REPAIR DOUBLER PER EO NR 98-0924-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.SDR ARWA981116Angle · crackedC-CHECK, 8 INCH CRACK IN RADIUS OF TOP O/B PYLON TO WING ATTACH ANGLE NR 3 ENGINE STA YN310. STOP DRILLED CRACK, INSTALLED DOUBLER PER EO NR 98-0926-06 ON 8110-3, DATED SEPT 24, 1998 UNDER WORK ORDER NR 1300.SDR MWEA981046Fitting · crackedCRACKS FOUND LEFT PYLON REAR SPAR UPPER CAP ATTACH FITTING. REMOVED AND REPLACED CRACKED FITTING.SDR DHL9872017DAngle · corrodedAT D CHECK, RT SIDE OF NR 2 ENGINE PYLON LOOK THROUGH ACCESS PANEL 35201 ANGLE IS CORRODED AND CRACKED. REMOVED ANGLE, INSTALLED NEW ANGLE PER SRM 54-10-2, 12 LONG, N/R 6778.SDR ABXA9801134Doubler · crackedLEFT WING NR 1 PYLON STUB WING LOWER SURFACE REPAIR DOUBLER CRACKED BETWEEN 2 RIVETS. REPAIRED IAW DC8 SRM 51-1-26.SDR SWAA982795Angle · crackedDURING SCHEDULED RON CHECK, FOUND NR 2 ENG O/B PYLON AFT MOUNT AREA ABOVE ENG TAILPIPE L-ANGLE INSIDE AT TOP FASTENER IS CRACKED. REPAIRED ANGLE PER BOEING SRM.SDR UPS98828216Fitting · corrodedINSPECTION TYPE-D, NR 1 PYLON THROUGH PANEL 197B FIRST RT VERTICAL STIFFENER LWR ATTACH FITTING CORRODED. REMOVED OLD FITTING, RCD NEW FITTING FROM MACHINE SHOP DRILLED HOLES AND INSTALLED IAW DC8 SRM 51-1-20D.SDR ABXA9800933Angle · crackedNR 3 ENGINE PYLON SUPPORT ANGLE CRACKED AT AFT OUTBOARD END. REPAIRED PYLON RIB, LOWER SECTION IAW ABX REA-D854-24337MR.SDR ABXA9800935Angle · crackedDURING C-CHECK, FOUND NR 2 PYLON TO FUSELAGE ATTACH ANGLE CRACKED BENEATH THE PYLON LEADING EDGE. REPLACED ANGLE IAW DC9 SRM 54-04.SDR P5CA9801575Angle · cracked#4 PYLON AFT BULKHEAD FWD SIDE HAS AN ANGLE STOP DRILLED AND CRACK APPEARS TO BE GOING BEYOND STOP DRILL. REPAIRED PER SRM 51-14-01 AND 51-30-02.SDR ABXA9801111Pylon · crackedWHILE COMPLYING WITH D-INSPECTION, FOUND NR 2 PYLON CRACKED INTERNALLY, JUST AFT OF THE AFT SPAR. REPAIRED CRACK IAW ABX REA D954-25253 AND ABX DWG K05159.SDR EIAA980333Spar · corrodedMZJ - DURING C4 CHECK, RIGHT PYLON FORWARD SPAR UPPER BEAVER TAIL HAS CORROSION. REPAIRED PER SRM 54-04 AND ECRA 945-54-025-2. (M)SDR CALA9801983Channel · crackedINSPECTION FOUND A 1 INCH CRACK IN NR 1 ENGINE LOWER PYLON PANEL NR 5107 AND A SMALL SECTION MISSING ON THE TRAILING END INNER FRAME U CHANNEL. THE U CHANNEL ON LOWER PYLON PANEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3, 51-30-2, 51-10-2 ANSDR CKSA98605Stiffener · corrodedNR 2 STIFFENER IN RT NR 1 PYLON HAS NUMEROUS AREAS OF CORROSION. NDT VERIFIED OUT OF LIMITS. REPAIRED IAW ASA CKF-PYL-017, CKF-PYL-029 & CKF-PYL-031 INCL ALL SUPP SHEETS. FOUND DURING ACCOMPLISHMENT OF C D AND CPCP AT BOEING WICHITA (KIAB). WORK ORDER NUMBSDR UPS98227943Web · crackedINSPECTION TYPE:C WEB OVER NR 2 ENGINE CRACKED AT BS 1376 RT. NEW WEB FABRICATED AND INSTALLLED IAW DRAWING 65-17555.SDR DL72W982079Angle · corrodedWHILE PERFORMING HUSH-KIT MOD, FOUND RT CHORD ANGLE ON NR 2 ENG SLOPING WEB CORRODED BEYOND MFG SPECS. REPLACED RT CHORD WITH NEW SCV CHORD.SDR SWAA982459Angle · crackedDURING SCHEDULED 1/2D CHECK, FOUND ATTACH ANGLE CRACKED AT UPPER SHELF PANEL NR 2 PYLON OTBD EDGE INBD OF NR 6 SPOILER. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982448Clip · crackedDURING SCHEDULED D CHECK, FOUND L-CLIP CRACKED, SUPPORT BRACKET TOP OF NR 1 PYLON. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982435Bracket · gougedDURING SCHEDULED D CHECK, FOUND NR 1 PYLON SPRING DOOR AND MOUNT BRACKET IS GOUGED. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982434Bracket · crackedDURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L BRACKET SUPPORT CRACKED AT UPPER OF FLAP CUTOUT ON AFT PANEL SUPPORT. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982433Angle · chafedDURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E L- ANGLE AND STIFFENER ARE CHAFFED AT LWR SIDE OF FLAP CUTOUT. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA982431Angle · crackedDURING SCHEDULED D CHECK, FOUND NR 1 PYLON I/B T/E LWR SIDE ANGLE SUPPORT CRACKED JUST FWD OF TAILCONE FITTING. REMOVED AND REPLACED PER BOEING SRM.SDR DL72W982078Angle · corrodedFOUND LT CHORD ANGLE ON NR 2 ENG SLOPING WEB WITH CORROSION BEYOND MFG SPECS. REPLACED CHORD ANGLE WITH NEW CHORD ANGLE.SDR CALA9801904Channel · crackedINSPECTION FOUND A 10 INCH CRACK IN AFT CHANNEL INSIDE NR 1 PYLON ABOVE LOWER AFT FAIRING. A NEW CHANNEL WAS INSTALLED IAW SRM 51-10-2.SDR ABXA9801048Angle · crackedCRACKED ANGLE ON NR 4 ENGINE PYLON, LOWER SIDE LEFT AFT OF PNEUMATIC DUCT OPENING. REPAIRED IAW ABX REA D854-24199 AND DC8 SRM 51-1-20D.SDR ABXA9801042Support · crackedNR 1 PYLON OUTBOARD SIDE AT STATION AND YOP 230, SUPPORT CRACKED. REPAIRED IAW DWG 44088012-1 AND DC8 SRM 51-1-20D.SDR DL76L982035Spar Web · crackedPYLON NR 1 ENGINE NACELLE STRUT, AFT UPPER SPAR WEB FS 222, LBL4, CRACK REPAIR. A .75 INCH LONG CRACK WAS FOUND EMANATING FROM THE AFT, OUTBD CORNER OF A CUTOUT IN THE AFT UPPER SPAR WEB OF THE NR 1 ENGINE NACELLE STRUT AT FS 222, LBL4. THE CRACK WAS ROUTESDR 9810296635Channel · crackedDURING PERIODIC CHECK, FOUND CRACK IN STIFFENER FLANGE ON NR 4 PYLON BL 0, FS 157. REPAIRED PER EA 66-160980, REV A.SDR 98UAL900463Brace · gougedA .060 INCH DEEP GOUGE IN PYLON NUMBER ONE DIAGONAL BRACE. THE GOUGE IS 40 INCHES FORWARD OF AFT END OF DIAGONAL BRACE AND 1.74 INCHES LONG BY .5 INCH WIDE. CAUSED BY CONTACT WITH STEEL PNEUMATIC LINE. PYLON NUMBER ONE DIAGONAL BRACE REPLACED BEFORE FURTHERSDR ABXA9801039Stiffener · crackedNR 4 ENGINE LOWER AFT PYLON FAIRING INTERNAL STRUCTURE VERTICAL STIFFENER IS CRACKED AT TOP LEFT RIVET HOLE. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 5643201.SDR CALA9801772Channel · crackedINSPECTION FOUND A 1.75 INCH CRACK IN NR 3 ENGINE PYLON UPPER FIXED COWL FORWARD END U-CHANNEL. THE CHANNEL WAS REMOVED AND A NEW CHANNEL WAS INSTALLED IAW SRM 51-40-3.SDR DL72W982217S-Duct · crackedAT HMV FOUND SKIN - BENT/CRACKED INSIDE S-DUCT APPROX 4FT FROM L/E OF INLET AT 12 O-CLOCK POSITION. CORR: MANUFACTURED REPAIR DBLR AND FILLER PER SRM 54-10-3 P.63 INSTLD PER SAME.SDR CALA9801748Web · crackedINSPECTION FOUND THREE 2 INCH CRACKS ON NR 1 ENGINE PYLON INTERNAL WEB AT STA 1065. THE CRACKS WERE STOP DRILLED IAW SRM 51-10-1. A REPAIR WAS INSTALLED IAW SRM 51-10-3 AND 54-01, FIGURE 2.SDR CALA9801720Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN RT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1213. THE ATTACH ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.SDR CALA9801719Angle · crackedINSPECTION FOUND A .5 INCH CRACK IN LEFT RIB TO SKIN ATTACH ANGLE AND A 2.5 CRACK IN RIGHT RIB TO SKIN ATTACH ANGLE OF CENTER ENGINE AIR DUCT HOUSING AT STA 1203. THE ATTACH ANGLES WERE REMOVED AND REPLACED IAW SRM 51-40-3 AND MM 51-20-11.SDR ABXA9800880Angle · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND A CRACK IN THE NR 1 ENGINE PYLON UPPER ATTACH ANGLE AT FS 980. REPAIRED CRACK IAW DC9 SRM CHAPTER 53-04.SDR DL72S981875Duct · bentDOGHOUSE AFT LIP, ON AIRINTAKE DUCT 360 DEGREES AREA, BENT AND DISTORTED. HEAVY ACCUMULATION OF SEALER. REMOVED DAMAGE DOUBLER, BEGAN DRILLING NEW DOUBLER. COMPLETED FABRICATION OF NEW DOUBLER PER SRM 54-10-3 FIG 13 D. OK TO INSTALL DOUBLER. INSTALLED REPSDR VJ9800314Seal · chafedNR 1 ENGINE SPRING SEAL ON LOWER SURFACE APRON HAS WEAR BEYOND LIMIT DUE TO CHAFING IAW DC9 SRM 53-01, FIG 1. LOCATED, DRILLED, DEBURRED AND INSTALLED NEW SPRING SEALS IAW DC9 SRM 51-10-4 AND 51-30-5.SDR SWAA981898Angle · damagedDURING SCHEDULED D-CHECK, FOUND NR 1 PYLON ANGLE LOWER EDGE OF I/B FLAP CUTOUT DAMAGED. REMOVED AND REPLACED PER BOEING SRM.SDR ABXA9800797Angle · crackedDURING C-CHECK, FOUND ANGLE CRACKED INSIDE NR 1 PYLON ABOVE AFT OUTBOARD CORNER OF PANEL 8105. REPLACED ANGLE IAW DC9 SRM 54-01 AND 51-30-2.SDR CALA9801489Casting · crackedINSPECTION FOUND NR 1 ENGINE PYLON PANEL LOWER SIDE NUT PLATE AREA CRACKED AND FOUND A 1 CRACK IN INBOARD FORWARD ATTACH CASTING. THE CASTING WAS REMOVED IAW SRM 51-30-2. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-40-3, 51-10-2, AND MM 51-20-11. SDR CALA9801466Fairing · crackedINSPECTION FOUND A 1 INCH CRACK ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 183.4. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2, 51-40-2, FIGURE 1, AND 51-30-2.SDR CALA9801465Fairing · crackedINSPECTION FOUND A 1 INCH CRACK AT FASTENER HOLE ON NR 1 ENGINE WING TO ENGINE UPPER FAIRING AT LOWER INBOARD CORNER, WS 181.0. THE CRACK WAS STOP DRILLED, AN EXTERNAL REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-2, FIGURE 2 AND 51-40-2, FIGURE 1SDR DL76L981678Shim · migratedA SHIM WAS FOUND MIGRATED .25 FROM BENEATH THE STRUT LOWER SPAR FITTING ON THE NR 1 PYLON. THE CONDITION IS DESCRIBED IN BAC S/B 767-54-0070. THE LOCAL FASTENERS WERE REPLACED AND THE MIGRATED SHIM WAS TRIMMED FLUSH PER THE TEMPORARY REPAIR INSTRUCTIONS OF TSDR RRXA98360Fastener · trappedDURING A MAINTENANCE VISIT, TRAPPED FASTENER UNDER DRAG ANGLE AND A FASTENER INTERFERS WITH REPLACEMENT OF FOOTSTOOL FITTING AT NR 3 PYLON. DELTED TRAPPED FASTENER FROM FOOTSTOOL, INSTALLED AND MODIFIED FOOTSTOOL TO AVOID INTERFERENCE IAW FAA APPROVED TIMCO DSDR RRXA98359Fastener · trappedDURING A MAINTENANCE VISIT, TRAPPED FASTENER UNDER DRAG ANGLE AND A FASTENER INTERFERS WITH REPLACEMENT OF FOOTSTOOL FITTING AT NR 2 PYLON. DELTED TRAPPED FASTENER FROM FOOTSTOOL, INSTALLED AND MODIFIED FOOTSTOOL TO AVOID INTERFERENCE IAW FAA APPROVED TIMCO D
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