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 SWAA981605Bracket · crackedDURING SCHEDULED C2 CHECK, FOUND NR 6 CANOE/PYLON AREA O/B SIDE ANGLE BRACKET CRACKED. REPAIRED PER BOEING SRM.SDR P5CA9801234Fairing · delaminatedNR 3 PYLON NAC STA 320 SAIL BOAT RT FAIRING 474D HAS OUTER SKIN DELAMINATION. HOT BOND REPAIR PER SRM 51-40-06 FIG 13.SDR CALA9801382Strap · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 PYLON TRAILING EDGE PANEL DOUBLER STRAP. A NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 54-30-0.SDR CALA9801380Angle · crackedINSPECTION FOUND A CRACK IN NR 1 PYLON TRAILING EDGE PANEL INTERCOSTAL ATTACH ANGLE. A NEW ATTACH ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-3, AND 51-00.SDR ABXA9801098Angle · crackedRADIUS CRACK AT NR 1 PYLON ATTACH ANGLE. REPAIRED IAW ABX REA D854-23442MR.SDR 98ZZZX3229Bolt · shearedDURING PERFORMANCE OF C-CHECK INSPECTION, TASK ON LEFT INBOARD FORWARD NACELLE FITTING ASSY P/N 120-00361-001, FOUND ALL OUTER BOLTS P/N MS21134-04005 SHEARED AND AFT INNER BOLT LOOSE.SDR MWEA98822Angle · crackedFOUND CRACK ON LEFT PYLON LOWER AFT BOX CORNER ANGLE. MTC FABRICATED AND INSTALLED REPAIR ANGLE.SDR SWAA981517Chord · crackedDURING SCHEDULED BC1 CHECK, FOUND OUTBOARD PYLON CHORD CRACKED AT NAC BS 319. REPAIRED PER SWA RA NR 1-354-192.SDR P5CA9801204Fairing · delaminatedNR 3 PYLON V FAIRING DELAMINATED. REPAIRED PER SRM 51-30-07.SDR P5CA9801201Fairing · delaminatedNR 4 PYLON V FAIRING DELAMINATED. REMOVED AND REPLACED FAIRING SRM 51-10-01 AND 51-30-02.SDR SWAA981416Support · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR1 PYLON 'L' ANGLE SUPPORT ON I/B AFT SIDE ON LWR SIDE OF FLAP CUTOUT IS GOUGED BEYOND LIMITS. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981415Support · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON LWR AFT END L SUPPORT ON I/B SIDE OF PYLON. REMOVED AND REPLACED PER BOEING SRM.SDR SWAA981414Bracket · crackedDURING SCHEDULED D CHECK, FOUND CRACKED NR 1 PYLON UPR AFT END, L BRACKET ON I/B SIDE OF SUPPORT BETWEEN ACCESS PANELS 5735L AND 5736L AND AFT SIDE PANEL SUPPORT AT THE AFT END OF ACCESS PANEL 5736L. REMOVED AND REPLACED PER BOEING SRM.SDR AALA981473Angle · corrodedTUL - FOUND CORROSION ON LOWER FLANGE OF RIB 14A UPPER PYLON TO WING PANEL SUPPORT. INSTALLED NEW FLANGE PER SRM 51-72-10-0. (M)SDR DHL9872169DS-Duct · corrodedAT D-CHECK, NR 2 ENGINE INLET DUCT AFT END HAS PULLED RIVETS AND SKIN CRACKED. CUT OUT DAMAGED AREA AT 12 O'CLOCK AFT END. CUT OUT DAMAGED SECTION OF INTERNAL STRAP AT TOP OF AFT END, 12 INCHES LONG. FABRICATED AND INSTALLED FILLER AND DOUBLER 7 X 4 PER SRMSDR TWAA9812011Angle · crackedDURING OP 15 MAINT CHECK, FOUND LOWER ATTACH ANGLE AT FUSELAGE CRACKED 1.5 IN AT FWD END OF NR 1 PYLON. REMOVED CRACKED ANGLE AND FABRICATED NEW ANGLE FROM 177PH STEEL, .040 IN. INSTALLED WITH MONEL RIVETS REF DWG 5923062.SDR SCNA98525Web · wornDURING HEAVY CHECK, THE NUMBER 1 PYLON LEFT HAND SIDE INTERNAL STATION YN187 PYLON WEB LOWER CAP WAS FOUND WORN TO A KNIFE EDGE, FROM CHAFING AGAINST THE CABLE HOUSING VISIBLE THROUGH PANEL 437AL. ADJUSTED BRACKET AND REINSTALLED PER SRM 513101, REPAIRED IAWSDR 99ZZZM594Structure · wornNR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH HOLES WORN AND SLOPPY AT SHOULDER COWL STRUCTURE. REPAIR PER RI HC710H9033. REPAIRED NR 3 PYLON SHOULDER COWL AFT LORD MOUNT ATTACH STRUCTURE HOLES IAW BAE REPAIR DRAWING HC710H9003. (M)SDR 98ZZZX2957Plank · crackedPYLON PLANK HAS CRACK LOCATED AT 19.5 INCHES AFT FROM YN190. SUSPECT CAUSE OF THE CRACK WAS VIBRATION.SDR 98ZZZX2956Plank · crackedPYLON PLANK CRACK LOCATED AT YN226. SUSPECT CAUSE OF THE CRACK IS VIBRATION.SDR CALA9801222Angle · crackedINSPECTION FOUND NR 2 ENGINE PYLON INBOARD VERTICAL ATTACH ANGLE FORWARD OF WIRE BUNDLE CRACKED AT LOWER END. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-10-3, 51-30-5, 54-04, FIGURE 10, AND MM 51-20-11.SDR ABXA9800607Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON STRUCTURE CRACKED AT STATION 1033 OUTBOARD OF PANEL 8206 BOTTOM OF PYLON. REPLACED ANGLE IAW DC9 SRM 51-30-2.SDR P5CA9801132Brace · chafedNR 2 ENGINE PYLON DIAGONAL BRACE FORWARD LOWER END HAS CHAFE MARKS. BLENDED PER SRM 54-40-01 FIG 3. TREATED/PAINT PER SRM 51-10-02.SDR C2XA98IA234Support · crackedIAH - DURING C-CHECK INSPECTION, FOUND LEFT NACELLE FLAP OUTBOARD RIB LOWER SKIN SUPPORT CRACKED. MAINTENANCE STOP DRILLED THE CRACK AND INSTALLED A REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR MWEA98755Channel · crackedFOUND CRACK ON RIGHT PYLON 2 CHANNEL FORWARD OF AFT ENGINE MOUNT. MTC FABRICATED AND INSTALLED REPAIR DOUBLERS.SDR 98ZZZM591Keel Web · damagedAT SCHEDULED INSPECTION DETERMINED THE RIGHT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART 2. VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNTSDR 98ZZZM590Keel Web · damagedAT SCHEDULED INSPECTION, DETERMINED THE LEFT NACELLE INBOARD KEEL ASSEMBLY TO FAIL CONDUCTIVITY TEST PER RAYTHEON SERVICE BULLETIN 54-3071 PART 2, VISUAL INSPECTIONS PROVED SATISFACTORY PER PART 1 OF SAME BULLETIN. SCHEDULED REPETITIVE VISUAL INSPECTIONS UNTISDR ABXA9800569Shear Tie · crackedWHILE COMPLYING WITH C-INSPECTION, FOUND THE LEFT ENGINE PYLON SHEAR-TIE CRACKED AT LONGERON 14 LEFT AND FS 1041. REPLACED SHEAR-TIE IAW DOUGLAS DC9 SRM CHAPTERS 53-12-3, 51-30-1, 51-30-2 AND 51-30-5.SDR AALA981191Rib · corrodedTUL - RIB 16A HAS CORROSION ON LANDING SURFACE. REPLACED RIB ASSY PER SRM 51-72-10-0. (M)SDR UPS98227023Web · crackedINSPECTION TYPE: C, CRACK ON WEB ABOVE NR 2 ENG HORIZONTAL FIREWALL RT SIDE AT STA 1381. WEB FABRICATED AND INSTALLED IAW DRAWING 65-17555.SDR DL72S981268Skin · crackedRIVETS LOOSE .25 INCH CRACK IN DORSAL FIN OUTER SKIN RT SIDE BELOW PANEL 9516. REPAIR PER M/M 54-30-0 FIG 801.SDR IXXA9800118Angle · crackedDURING ROUTINE C-CHECK INSPECTION, CRACKS WERE DETECTED ON THE NUMBER ONE AND FOUR INBOARD PYLON ATTACH ANGLE STIFFENERS. REPAIR ACCOMPLISHED REMOVAL OF THE DAMAGED ANGLES, FABRICATION AND INSTALLATION OF TWO NEW ANGLES IN ACCORDANCE WITH DOUGLAS DRAWING 5756SDR CALA9801034Fairing · crackedINSPECTION FOUND A 2 CRACK IN NR 1 PYLON LT FAIRING. THE FAIRING WAS REMOVED. A NEW FAIRING WAS FABRICATED AND INSTALLED IAW SRM 51-35-02.SDR MWEA98649Spar · damagedTHE LEFT PYLON UPPER SPAR CAPS WERE FOUND DAMAGED. REMOVED AND REPLACED SPAR CAPS USING APPROVED DATA.SDR MWEA98648Angle · damagedTHE LEFT PYLON FWD SPAR AFT INBOARD SURFACE HAS A IMPROPER REPAIR. MAINTENANCE REMOVED DAMAGED AREA INSTALLED REPLACEMENT PARTS USING APPROVED DATA.SDR DL72S981224S-Duct · crackedS-DUCT LEADING EDGE ROLLED OVER AND CRACKED JUST AFT OF NOSE COWL AT 12 O'CLOCK POSITION. REMOVED DAMAGED AREA AND FABRICATED REPAIR PER SRM 54-10-3 FIG 13. OK TO INST REPAIR. INSTALLED REPAIR PER SRM 54-10-3 FIG 13. OK TO CLOSE. CLOSED OUTER SKIN.SDR QXEA9800836Drain Line · crackedPDX - LEFT STUBWING NR 2 DRAIN LINE IS LOOSE AND CRACKED AT NACELLE FIREWALL BELOW AND OUTBOARD OF NR 1 SILENCER. REPAIRED IAW HORIZON AIR EA 4-54-38 AND 54-54-38A.SDR UPS98827026Angle · crackedINSPECTION TYPE:D, THE NR 1 PYLON OUTBOARD ANGLE DOUBLER AT THE FRONT SPAR IS CRACKED. REMOVED FABRICATED AND REPLACED ANGLE IAW DWG 5803961 AND SRM 51-1-20D AND 51-3-0.SDR ABXA9800485Angle · crackedDURING C-CHECK, FOUND NR 1 ENGINE PYLON TRAILING EDGE INTERIOR ANGLE CRACKED AT AFT OUTBOARD CORNER. REPLACED ANGLE IAW DC9 SRM 51-30-2, 51-30-5 AND DACO DWG 9915555.SDR QXEA9800811Heatshield · wornNR 1 ENGINE NACELLE HEATSHIELD ASSEMBLY INBOARD SIDE HAS HOLE WORN THROUGH APPROXIMATELY STATION 228.0. REPAIRED IAW HORIZON AIR EA 9-54-160 AND CONAIR EO 1995.SDR SWAA980904Angle · crackedDURING SERVICE CHECK, FOUND NR 2 PYLON I/B AND O/B ACCESS CUTOUT PANEL SUPPORT ANGLE CRACKED. REMOVED AND REPLACED PER BOEING SRM.SDR CKSA98307Brace · wornDURING ACCOMPLISHMENT OF AD 95-10-16, FOUND NR 1 PYLON DIAGONAL BRACE DAMAGED BEYOND LIMITS, .240 WIDE .405 LONG .085 DEEP, .090 AWAY .190 WIDE .400 LONG .040 DEEP. REPLACED DIAGONAL BRACE IAW MM 54-10-03 AND SECURED HOLD OPEN STRUT. NON-ROUTINE TASK CARD NSDR SWAA980878Doubler · damagedDURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM.SDR SWAA980877Doubler · damagedDURING SERVICE CHECK, FOUND DAMAGED DOUBLER ON THE NR 2 0/B PYLON SKIN AT THE WING LEADING EDGE INTERFACE. REPAIRED PER BOEING SRM.SDR DL72S981034S-Duct · cracked3 INCH SECTION OF S DUCT INNER SKIN DAMAGED/BENT BACK 3 FT. AFT OF INLET AT 1 OCLOCK POSITION, ERA 364794-14 DOUBLER.SDR ABXA9800924Rib · crackedNR 4 PYLON UPPER RIB HAD CRACK AT END. REPAIRED IAW DC8 SRM.SDR 99ZZZM444Rib · crackedNR 2 PYLON BOX STRUCTURE HAS A CRACK IN THE LOWER OUTBOARD FLANGE OF RIB NR 5 THAT IS APPROX .5 INCH LONG. NR 2 PYLON CRACK OF APPROX .5 INCH LONG IS ACCEPTABLE AND HAS BEEN REPORTED TO BAE RDO PER P/C HC646H9018. GENERATED W/C FOR REINSPECTION. (M)SDR 98FDEA00341Bolt · looseSNRM N 00874, A/C 304, FOUND 9 EA BOLTS LOOSE AT BOTTOM OF PYLON FWD MOUNT. REMOVE, INSPECTED AND INSTALLED 9 EA BOLTS PER M/M 20-50-0212.SDR ABXA9800456Angle · crackedDURING C-CHECK, THE LEFT UPPER PYLON ATTACH ANGLE WAS FOUND CRACKED. REPAIRED IAW DC9 SRM 54-04.SDR QXEA9800694Strut · damagedNR 2 THRUST STRUT IS DAMAGED APPROXIMATELY 10 AFT OF NACELLE TO STUB WING FEED THROUGH. REPAIRED IAW FOKKER MM 54-40-03, PAGE 201 TO 203, AND HORIZON AIR EA 4-71-81.
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