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.

SDR CALA9700719Web · crackedINSPECTION FOUND A 2 INCH CRACK AT LOWER END OF WEB JUST FORWARD OF AFT ENGINE MOUNT, NR 2 PYLON. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-01, FIGURE 2.Apr 29, 1997 · N12507 · Doug DC932SDR 97ZZZX2993Nutplate Strip · brokenATW - NR 4 PYLON HORSESHOE PANEL (481AT) AFT NUTPLATE ATTACH STRIPS LT AND RT, BOTTOM 4 NUTPLATES NEED REPLACEMENT. ALSO, INBOARD AFT NUTPLATE STRIP IS BROKEN. REPAIRED ABOVE NUTPLATE STRIP PER BAE REPAIR HC546H9017 AND FAX DJR/RJ0378-97. PANEL 481AT IS NOWApr 29, 1997 · N610AW · Bag BAE146200ASDR ABXA9700947Angle · brokenDURING C-CHECK, FOUND THE NR 2 PYLON INTERIOR CANTED WEB LOWER ANGLE BROKEN OFF AT FORWARD CORNER IN ACCESS AREA 8206A. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-8.Apr 26, 1997 · N965AX · Doug DC941SDR CALA9700855Support · crackedINSPECTION FOUND A 6 INCH CRACK IN CHANNEL SUPPORT OF NR 2 ENGINE PYLON AFT FAIRING. THE CHANNEL SUPPORT WAS REMOVED, A REPLACEMENT CHANNEL SUPPORT WAS FABRICATED AND INSTALLED IAW SRM 51-31-01 AND 54-12-02.Apr 24, 1997 · N6857X · Doug DC1030SDR UPS97422835Chord · crackedINSPECTION TYPE-C, PYLON 3 FOUND DURING SB 747-54-2034 UNDER OLD DOUBLER CRACK 3.5 LONG RUNNING TO MID SPAR CHORD NAC STA 180 AND 3X HOLES DRILLED IN MID SPAR CHORD STA 184 EDGE MARGIN TOO SMALL. TRIMMED SKIN AND DOUBLER. INSTALLED FILLER, REWORKED MID SPAR Apr 22, 1997 · N681UP · Boeing 747121SDR 98ZZZX1696Former · crackedMULTIPLE CRACKS WERE FOUND IN FORMER WHICH IS LOCATED IN AREA ABOVE NR 2 ENGINE. FORMER IS A PART OF THE AFT PYLON STANG AREA.Apr 20, 1997 · N910SF · Doug DC1010SDR P5CA9700502Fairing · delaminatedDELAMINATION ON NR 3 PYLON SAIL BOAT FAIRING LEADING EDGE 2 BY 15. REPAIRED PER MA 5450-01:01.Apr 16, 1997 · N851FT · Boeing 747122SDR ABXA9700649Angle · crackedDURING C-CHECK, FOUND AN ANGLE CRACKED INSIDE THE RT PYLON AT THE AFT OUTBOARD CORNER OF PANEL NR 8206. REPLACED ANGLE IAW DC9 SRM 51-30-2.Apr 11, 1997 · N925AX · Doug DC914SDR EIAA970104Fitting · crackedHKG - DURING C5/D INSPECTION, FOUND NR 4 PYLON NAC STATION 215 FORWARD OF REAR ENGINE MOUNT B/HD BATHTUB FITTING CRACKED ACROSS BOTH BOLT HOLES. BATHTUB FITTING REPLACED AS PER SRM 51-10-01. (M)Apr 10, 1997 · N485EV · Boeing 747212BSDR HALA9750Closeout Rib · crackedFOUND .6875 VERTICAL CRACK ON NR 2 PYLON CLOSING RIB, ADJACENT TO FS 1167 BOTTOM OF LIGHTING HOLE. FABRICATED DOUBLER, STOP DRILLED CRACK AND INSTALLED DOUBLER PER DAC ACTION NR 327482 OR SRM 51-10-2. (M)Apr 9, 1997 · N709HA · Doug DC951SDR HAL9750Rib · cracked.6875 INCH VERTICAL CRACK ON NR 2 PYLON CLOSING RIB ADJACENT TO FS 1167 BOTTOM OF LIGHTING HOLE. FABRICATED DOUBLER, STOP DRILLED CRACK, AND INSTALLED DOUBLER PER DAC ACTION NR 327482 OR SRM 51-10-2. TOTAL TIME: 29,567 HOURS. TOTAL CYCLES, 73,626. (X)Apr 9, 1997 · N709HA · Doug DC951SDR UPS97822703Fitting · crackedINSPECTION TYPE-D, AFT END UPPER FITTING NR 1 PYLON IS CRACKED. REMOVED AND REPLACED FITTING IAW SRM 51-1-21.Apr 5, 1997 · N818UP · Doug DC873FSDR 97ZZZM582Angle · crackedDURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACH ANGLES, P/N'S 115921901-19 AND 115921901-20. THE ANGLES WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE.Mar 27, 1997 · N165G · Gulstm G1159ASDR 97ZZZM581Angle · crackedDURING AN 18 MONTH INSPECTION OF THE LEFT PYLON, 1 INCH CRACKS WERE FOUND IN THE LEADING EDGE ATTACH ANGLES, P/N'S 115921901-19 AND 115921901-20. THE ANGLES WERE REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Mar 27, 1997 · N165G · Gulstm G1159ASDR P5CA9700454Stiffener · crackedNR 1 PYLON RIGHT SIDE AFT SKIRT LOWER (INNER SIDE) STIFFENER BENT AND BRACKET CRACKED. REMOVED STIFFENER AND FABRICATED STIFFENER IAW BOEING SRM 51-40-01.Mar 24, 1997 · N859FT · Boeing 747123SDR CKSA97165Doubler · crackedDURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON ACCESS DOOR 407 DOUBLER CRACKED AT UPPER FASTENER HOLE. REPAIRED DAMAGE TO ACCESS DOOR DOUBLER IAW SKETCH AIA/E/2504, SRM 51-1-8, 51-1-20 EA 97-013A. CORROSION TASK CARD NUMBER 84-1-0551. NON-ROUTINE TASK CARD Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97163Spar Web · crackedDURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON UPPER SPAR WEB CRACKED UNDER DOUBLER OUTBOARD SIDE APPROXIMATELY STA YOP244. INSTALLED REPAIR AS PER AIA/E/2491 EA 97-013A. CORROSION TASK CARD NUMBER 81-1-0551. NON-ROUTINE TASK CARD NUMBER 93408.Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97159Spar Cap · crackedDURING CPCP CHECK INSPECTION, FOUND LEVEL 2 CORROSION NR 3 PYLON UPPER OUTBOARD SPAR CAP CRACKED AT STA YIP230. INSTALLED REPAIR TO UPPER OUTBOARD SPAR CAP IAW AIA SKETCH AIA/E/2519 EA 97-013. CORROSION TASK CARD NUMBER 83-1-0551. NON-ROUTINE TASK CARD NUMBMar 24, 1997 · N809CK · Doug DC855SDR CKSA97139Angle · crackedDURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON OUTBOARD UPPER SPAR CAP CRACKED APPROXIMATELY STA YOP223 VIEWED THROUGH PANEL 110. REMOVED AND INSTALLED NEW ANGLE AND HARDWARE PER SRM 51-1-0 AND 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551. NON-ROUTINE TASMar 24, 1997 · N809CK · Doug DC855SDR CKSA97135Web · crackedDURING C-2 CHECK INSPECTION, FOUND NR 4 PYLON STA YOP244 OUTBOARD SIDE WEB HAS A 3 INCH CRACK. STOP DRILLED CRACK, INSTALLED REPAIR IAW AIA SKETCH AIA/E/2522, SRM 51-1-82, SRM 51-1-20D, EA 97-017.B. C-1 CHECK INSPECTION WORK CARD NUMBER 2007. NON-ROUTINE TAMar 24, 1997 · N809CK · Doug DC855SDR CKSA97133Doubler · crackedDURING CPCP CHECK INSPECTION, FOUND NR 4 PYLON DOOR 412 CUTOUT CRACKED INNER AND OUTER DOUBLER STA YOP208 UPPER SPAR AREA, NR 4 PYLON UPPER OUTBOARD SPAR CAP CRACKED STA YOP206, NR 4 PYLON UPPER OUTBOARD SPAR CAP CRACKED STA YOP224. INSTALLED REPAIR DOUBLER NMar 24, 1997 · N809CK · Doug DC855SDR CKSA97132Spar Cap · crackedDURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON UPPER INBOARD SPAR CAP CRACKED PAST STOP DRILL AT UPPER AND APPROXIMATELY STA YOP254. INSTALLED REPAIR ON UPPER SPAR CAP IAW DC8 SRM 54-2-1 FIGURE 5. INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. CORROSION TASK CARDMar 24, 1997 · N809CK · Doug DC855SDR CKSA97131Bracket · crackedDURING CPCP CHECK INSPECTION, FOUND BRACKET INBOARD SIDE OF NR 1 PYLON AT SLOT ATTACH AREA CRACKED. INSTALLED BRACKET INBOARD SIDE NR 1 PYLON, SLOT ATTACH AREA, IAW DC8 SRM 51-1-0, INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97130Attach Plate · crackedDURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON CAP ATTACH PLATE INBOARD SIDE CRACKED TWO PLACES APPROXIMATELY STA YOP270. REMOVED AND REPLACED ATTACH PLATE INBOARD SIDE AS PER SRM 51-1-0. INSTALLED FASTENERS IAW SRM 51-1-20D AND 51-1-21. CORROSION TASK CARDMar 24, 1997 · N809CK · Doug DC855SDR CKSA97129Angle · crackedDURING CPCP CHECK INSPECTION, FOUND NR 1 PYLON CAP SUPPORT RIB OUTBOARD ATTACH ANGLE CRACKED APPROXIMATELY STA YOP212. REMOVED AND REPLACED OUTBOARD SUPPORT RIB AS PER SRM 51-1-0. INSTALLED FASTENERS IAW SRM 51-1-20D. CORROSION TASK CARD NUMBER 81-1-0551. NMar 24, 1997 · N809CK · Doug DC855SDR CKSA97128Skin · crackedDURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON CRACKED PYLON STUB WING LOWER SKIN DOUBLER AT XFS552.00 AND XFS454.00. REMOVED AND INSTALLED SKIN DOUBLER XFS552.00 AND XFS454.00 IAW DC8 SRM 51-1-0 AND INSTALLED HARDWARE IAW DC8 51-1-20D. C-1 CHECK INSPECTION WMar 24, 1997 · N809CK · Doug DC855SDR CKSA97126Bracket · crackedDURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON CRACKED PYLON BRACKET AT XFS542.50 AT FORWARD AND AFT END ALONG BENDS (2 EACH CRACKS APPROXIMATELY 1.0 INCHES AT AFT END AND 1 EACH CRACK APPROXIMATELY 2 INCHES FORWARD). REMOVED AND REPLACED PYLON BRACKET AT STA Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97125Fitting · crackedDURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON CRACKED PYLON STUB WING SIDE BRACE FITTING APPROXIMATELY 12.5 INCHES IN LENGTH. REMOVED AND REPLACED PYLON STUB WING SIDE BRACE IAW DC8 SRM 51-1-0 AND INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. C-1 CHECK INSPECTION Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97124Angle · crackedDURING C-1 CHECK INSPECTION, FOUND CRACKED ANGLE AT UPPER INBOARD STUB WING LEADING EDGE NR 1 PYLON. REMOVED AND INSTALLED ANGLE IAW DC8 SRM 51-1-0. INSTALLED HARDWARE IAW DC8 SRM 51-1-20D. C-1 CHECK INSPECTION WORK CARD NUMBER 1007. NON-ROUTINE TASK CARD Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97108Doubler · crackedDURING C-1 CHECK INSPECTION, FOUND NR 1 PYLON INNER DOUBLER, VERTICAL STIFFENER FORWARD PYLON TO LEADING EDGE SUPPORT ANGLE IS CRACKED. REMOVED AND INSTALLED DOUBLER VERTICAL STIFFENER FORWARD PYLON IAW DC8 SRM 51-1-0. INSTALLED HARDWARE IAW DC8 SRM 51-1-20DMar 24, 1997 · N809CK · Doug DC855SDR CKSA97104Brace · crackedDURING C-1 CHECK INSPECTION, FOUND LATERAL BRACE IN NR 2 PYLON JUST FORWARD OF WING FRONT SPAR HAS 1 INCH LONG CRACK AT INBOARD END. REPAIRED IAW DC8 SRM 54-2-1. C-1 CHECK INSPECTION WORK CARD NUMBER 7214. NON-ROUTINE TASK CARD NUMBER 93655.Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97087Bracket · crackedDURING CPCP CHECK INSPECTION, FOUND NR 3 PYLON STUB WING ATTACH OUTBOARD BRACKET CRACKED APPROXIMATELY STA YIP290 MARKED T6-58. FABRICATED NEW BRACKET IAW DC8 SRM 54-3-0 FIGURE 3D. INSTALLED NEW BRACKET IAW DC8 SRM 51-1-20D AND 51-3-0. CORROSION TASK CARD NMar 24, 1997 · N809CK · Doug DC855SDR CKSA97083Bracket · crackedDURING CPCP CHECK INSPECTION, FOUND NR 2 PYLON STUB WING UPPER OUTBOARD BRACKET CRACKED 6 INCHES LONG APPROXIMATELY STA YIP270. REMOVED CRACKED BRACKET, FABRICATED AND INSTALLED NEW BRACKET IAW SRM 53-1-0, 51-3-0, 51-1-21. CORROSION TASK CARD NUMBER 82-1-055Mar 24, 1997 · N809CK · Doug DC855SDR CKSA97078Angle · crackedDURING CPCP CHECK INSPECTION, FOUND NR 2 PYLON TO LEADING EDGE UPPER SUPPORT ANGLE CRACKED APPROXIMATELY STA YIP 232 AND WX244. REMOVED AND REPLACED UPPER SUPPORT ANGLE IAW SRM 51-1-0, 51-3-0 AND 51-1-21. CORROSION TASK CARD NUMBER 82-1-0551. NON-ROUTINE TAMar 24, 1997 · N809CK · Doug DC855SDR ABXA9700443Angle · crackedDURING C-CHECK, FOUND THE RIGHT PYLON UPPER SPAR TO WEB ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM.Mar 20, 1997 · N907AX · Doug DC931SDR 97FDEA00181Web · crackedN00735 N00736, 2 PYLON AFT LOWER SUPPORT STRUCTURE HAS 3 CRACKED WEBS/STIFFENER, FWD OF THE AFT ENGINE MOUNT AND ABOVE THE AFT ELECTRICAL HARNESS QD, NON ROUTINE. *S/D* REMOVED SUPPORT CAGE, REMOVED AND REPLACED DAMAGED SECTION PER SRM 53-00-01. INSTALLED SMar 19, 1997 · N307FE · Doug DC1030SDR ABXA9700445Angle · crackedDURING C-CHECK, FOUND THE LEFT PYLON TO FUSELAGE ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM.Mar 18, 1997 · N907AX · Doug DC931SDR ABXA9700444Angle · crackedDURING C-CHECK, FOUND LEFT PYLON LOWER SPAR TO WEB ATTACH ANGLE CRACKED. REPLACED ANGLE IAW SRM.Mar 18, 1997 · N907AX · Doug DC931SDR UPS97422429Doubler · misinstalledINSPECTION TYPE-C, PYLON 3 FOUND DURING SB54-2034R4 MODIFICATION THAT ALREADY DOUBLER WAS INSTALLED. ONLY DOUBLER IS NOT ACCORDING SB INSTALLED DOUBLER ON LT SIDE ACC, KLM DFX 97-046 REV 3 APPROVED EFN 747-54-0149R1.Mar 14, 1997 · N674UP · Boeing 747123SDR P5CA9700470Doubler · crackedNR 2 ENGINE PYLON OLD DOUBLER REPAIR BY G/B SLOT SEAL CORNER CRACKED. REMOVED AND REPLACED DOUBLER PER BOEING 51-30-02 AND 51-10-01 EDDY CURRENT IAW NTD 54-40-13 PART 6.Mar 14, 1997 · N854FT · Boeing 747122SDR CALA9700576Fitting · crackedINSPECTION FOUND NR 3 PYLON STRUT TO DIAGONAL BRACE ATTACH FITTING CRACKED. THE CRACK LENGTH WAS NOT IDENTIFIED. THE FITTING WAS REPLACED IAW ECRA 5447-01019.Mar 13, 1997 · N78019 · Boeing 747230BSDR CALA9700523Fairing · crackedINSPECTION FOUND A 4.5 INCH CRACK IN NR 2 ENGINE FAIRING TRAILING EDGE PANEL WITH SECTION MISSING, RT SIDE. THE TRAILING EDGE PANEL WAS REMOVED, A NEW PART WAS FABRICATED AND INSTALLED IAW SRM 54-32-02 AND 51-21-01.Mar 7, 1997 · N68041 · Doug DC1010SDR P5CA9700413Retaining Strip · crackedNR 3 PYLON O/B FWD BTM CORNER NUTPLATE RETAINING STRIP CRACKED AT NAC STA 180. REPAIRED PER BOEING SRM 51-10-01.Mar 6, 1997 · N859FT · Boeing 747123SDR CALA9700524Panel · crackedTHE NR 2 ENGINE NACELLE UPPER RT SKIRT PANEL WAS FOUND BENT AND TORN WITH A 6.5 CRACK. THE DAMAGED AREA WAS TRIMMED OUT, DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 54-20-00 AND 51-31-01.Mar 4, 1997 · N68041 · Doug DC1010SDR CA970421005Fitting · cracked(CAN) THE FITTING REFERRED TO IS MOUNTED AND COVERED WHICH PREVENTS IT FROM BEING CLEANED, INSPECTED OR TREATED FOR CORROSION. THIS CONDITION WAS FOUND DURING WINTER MAINTENANCE INSPECTION. FITTING WAS REPLACED.Mar 4, 1997 · Doug DC6BSDR AALA970456Support · wornTUL - BOLT HOLES 'A' AND 'B' IN SUPPORT HAVE GROOVES WORN IN THEM. REWORKED HOLES PER ESO 7349 DATED 3-4-97 AND INSTALLED BUSHING PER SAME ESO. TST: 61,615 HOURS. CYCLES: 20,785. (X)Mar 4, 1997 · N128AA · Doug DC1010SDR UPS97522219Fuse Pin · crackedINSPECTION TYPE:1C, FUSE PIN REPLACEMENT RIGHT HAND PYLON. REMOVED FUSE PIN, FOUND BOTH TO BE CRACKED, REPLACED BOTH FUSE PINS.Mar 3, 1997 · N416UP · Boeing 75724APFSDR UPS97822434Angle · crackedINSPECTION TYPE-C/CK, NR 1 PYLON I/B DRAG ANGLE CRACKED EXTENDING APPROX .25 INCH PAST STOP DRILL HOLE. STOP DRILL END OF CRACK .250 AND POLISH TO 32 MICRO INCH FINISH. VERIFIED AND MARKED END OF CRACK UTILIZING HFEC. STOP DRILLED CRACK AS MARKED BY NOT VERMar 2, 1997 · N804UP · Doug DC873FSDR CALA9700540Bracket · crackedINSPECTION FOUND A 1 INCH CRACK IN SUPPORT BRACKET OF NR 2 ENGINE PYLON LEADING EDGE. A NEW BRACKET WAS FABRICATED AND INSTALLED IAW SRM 54-04, 51-30-2, AND ECRA 5410-01169.Feb 28, 1997 · N17543 · Doug DC932SDR ABXA9700519Angle · crackedDURING C-CHECK, THE UPPER PYLON TO FUSELAGE ATTACH ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPLACED IAW DC9 SRM 51-30-5.Feb 28, 1997 · N947AX · Doug DC931
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