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 AU991015Rod · worn(AUS) FOLLOWING REMOVAL OF THE RT PYLON BOAT FAIRING FOR REPAIR THE FOLLOWING DEFECTS WERE FOUND: 1. RT ENGINE DRIVEN HYDRAULIC PUMP PRESSURE AND SUPPLY LINE ELBOW JAM NUTS BACKED OFF AND ELBOW FRETTING IN PYLON RECEPTACLES2S. 2. INBOARD VERTICAL STRAKESDR UF6A990945Modular · crackedSBN - LEFT MODULAR 7 AFT INBOARD DIAPHRAGM IS CRACKED. MAINTENANCE STOP DRILLED CRACK AND REPAIRED. ALL WORK WAS DONE IAW BAE ATP SRM 53-10-02 AND 51-30-01. (M)SDR DL72S992116Skin · crackedTPA LTR CHK D-2 9/21/99, 1 CRACK ON S-DUCT HOUSING RT SIDE AT UPPER END OF PANEL 9524. REPAIRED PER MM 54-30-0.SDR TWAA9917404Clip · brokenDURING OP 16 MAINT CHECK AT STA 944, THE LOWER SIDE OF NUMBER 2 PYLON DOUBLER ANGLE CLIP WAS BROKEN. REPLACED DOUBLER PER SPM 6-70-01.SDR DL767992171Brace · corrodedMIGRATED/ROTATED BUSHINGS WERE FOUND IN THE FORWARD LUGS OF THE NR 1 AND NR 2 PYLON DIAGONAL BRACES DURING PYLON INSTALLATION. MINOR CORROSION DAMAGE AND FRETTING DAMAGE WAS FOUND IN THE BORES UPON BUSHING REMOVAL.SDR COMA9960507Angle · chafedPANEL 411AL CHAFED BY FASTENER MID FRAME OUTBOARD EDGE LEFT HAND ENGINE PYLON. PERFORMED MAJOR REPAIR SMOOTHED CHAFE ON (P/N 601-37004-133) AND FABED NEW SUPPORT ANGLE 601-37004-57 AS PER SAMPLE USING 2024-T3.040 PO NR 4206/1 AND INSTALLED IAW WVAC EO NR 601RSDR DL72S992010Skin · cracked.5 INCH CRACK ON DUCT HOUSING SKIN AT PANEL 9524 RT SIDE. REPAIR PER MM 54-30-0.SDR ABXA9900699Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON LEADING EDGE INBOARD LOWER ATTACH ANGLE CRACKED. REPLACED ANGLE IAW DC9 SRM 54-04.SDR ABXA9900696Angle · crackedDURING C-CHECK, FOUND RIGHT PYLON HAD CRACKED WEB AT LOWER ATTACH ANGLE. REPLACED ANGLE IAW DC9 SRM 51-30-2 AND 51-30-5.SDR DL76S992061Fitting · corrosionI/B LUG OF THE NR 1 ENGINE PYLON MIDSPAR O/B FITTING FOUND WITH CORROSION AND WEAR DAMAGE. DAMAGE FOUND ON FACE OF LUG AND IN BORE, ERA 333570-14 REV A.SDR DL72W992014Angle · corrodedDURING HUSH-KIT MOD, FOUND NR 2 AFT MOUNT SUPPORT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED OLD ANGLE WITH ONE OF NEW MFG.SDR ABXA9900711Angle · crackedDURING C-CHECK, FOUND THE NR 2 PYLON UPPER ATTACH ANGLE CRACKED AT FORWARD END. REPAIRED ANGLE IAW DC9 SRM 54-04.SDR CALA9901117Web · crackedINSPECTION FOUND A 5 INCH CRACK AT FORWARD WEB OF NR 2 PYLON AFTER REMOVING VERTICAL FIN. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-31-01.SDR UIEA99071Strap · crackedNR 1, 2, 3, 4, PYLONS EXTERIOR RIGHT PRE-COOLER EXHAUST CUTOUT FOUND WITH CRACK,AND NR 3 STIFFENER CRACK. REPAIRS CARRIED OUT IAW BOEING TELEXS AND SB 747-54-2163 R1 AND SB 747-54A2158 R2. THE SB REVS HAVE BEEN APPROVED ALTERNATE METHOD OF COMPLIANCE. (M)SDR UIEA99070Strap · cracksNR 4 PYLON INTERIOR, LEFT BULKHEAD STRAP AT NAC STATION 286 FOUND CRACKED. REPAIRED IAW BOEING TELEXS, TO BE RE-INSPECTED EVERY C-CHECK NOT TO EXCEED 18 MONTHS OR 1000 FLTS. (M)SDR UIEA99069Fitting · oversizeNR 1 AND NR 4 PYLONS FOUND FASTENER HOLE SIZE TO EXCEED TOLERANCE PER SB 747-54A2152 IN SPRINGBEAM SUPPORT FITTINGS IN 3 HOLE LOCATIONS. HOLES WERE OVERSIZED, NDT PERFORMED TO VERIFY NO CRACKS. NO INSURANCE CUT WAS PERFORMED AND FASTENERS INSTALLED. THIS ISSDR UIEA99065Doubler · crackedNR 1 PYLON CAP SKIN MOD MO 54-0074 AREA FOUND WITH EXISTING DOUBLER, BULKHEAD FRAME CRACK AT STATION 270. THE CRACKED FRAME FLANGE WAS TRIMMED TO REMOVED DAMAGE, NDT PERFORMED TO VERIFY NO OTHER CRACKS. NEW REPAIR ANGLES AND NEW DOUBLER INSTALLED IAW BOEING SDR MWEA99550Web · crackedCRACK AT RIGHT PYLON VERTICAL WEB U-CHANNEL OUTBOARD OF STATION 859. MTC FABRICATED AND INSTALLED DOUBLERS.SDR MWEA99544Stiffener · crackedLEFT PYLON 2 CHANNEL STIFFENER HAS A CRACK ON OUTBOARD END. MTC FABRICATED AND INSTALLED DOUBLER AND TRIPLER.SDR DHL9972743CS Duct · crackedAT C CHECK, NR 2 ENGINE S DUCT HOUSING LT OUTER SKIN AT BS 1216 HAD 2 INCH CRACK JUST RIGHT UP OF ACCESS PANEL 9523. REMOVED ACCESS PANEL 9523 TO GAIN ENTRY REMOVED ATTACH RING PER SRM 51-30-2 AND REMOVED PREVIOUS REPAIR. STOP DRILLED CRACK IAW SRM 51-10-1. SDR DHL9972757CBracket · crackedAT C-CHECK, NR 1 PYLON FWD IND END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED AND REPLACED BRACKET PER SRM 51-30-2, 9 X 4 N/R 6338.SDR DHL9972752CBracket · crackedAT C CHECK, NR 1 ENG PYLON FWD I/B END VERTICAL BRACKET CRACKED AT UPPER I/B END ACCESS PANEL 5407. REMOVED THRUST REV SHUTOFF VALVE. REMOVED 6 BOLTS FROM QUADRANT DISCONNECTED THRUST REV QUADRANT DRUM FOR SM ACCESS PER MM 71-11-21. REMOVED AND REPLACED BRASDR UF6A990815Modular 5 · damagedSBN - RIGHT MODULAR 5 IS PUNCTURED ON TOP AND DELAMINATING. MAINTENANCE REPAIRED DAMAGE. ALL WORK WAS DONE IAW BAE ATP SRM 54-10-01. (M)SDR UF6A990609Modular 6 · crackedSBN - LEFT MODULAR 6 IS CRACKED AT THE AFT FAIRING. MAINTENANCE REPAIRED CRACK. ALL WORK WAS DONE IAW BAE ATP SRM. (M)SDR 99FDEA00328Bolt · crackedNR 190 NR 3 PYLON AFT SPHERICAL BEARING, THROUGH BOLT FOUND WITH CRACK IND DURING MAGNAFLUX INSP. INSTALL NEW NR 3 PYLON AFT BEAR THROUGH BOLT PER EO 8-5410-7-430734 PART 4 STEP 12 AND 13.SDR UPS99830448Doubler · crackedINSPECTION TYPE:C3, NR 1 PYLON LWR FWD EXTERNAL HORSE SHOE DOUBLER IS CRACKED. FABRICATED AND INSTALLED DOUBLER, MATERIAL ID PO NR 22463 7075-T6.080 IAW DC8 SRM 57-2-1A.SDR 99ZZZX3196Stiffener · crackedDURING CONTINENTAL EXPRESS C-CHECK, FOUND LT MLG WHEELWELL AFT BULKHEAD, OUTBOARD STIFFENER CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 54-20-04. AIRCRAFT APPROVED FOR RETURN TO SERVICE. TAT: 20,512.5 HOURS. TAC: 27,506. (X)SDR UPS99830459Fairing · crackedINSPECTION TYPE:C3, NR 4 PYLON NOZZLE FAIRING HAS CRACKED FORMER. FABRICATED AND INSTALLED REPAIR IAW TIMCO REO NR 06674, HEAT TREATED REPAIR ANGLE AND CLIP IAW DAC DWG 9756774 GEN NOTE 23 AND TIMCO REO NR 0667 4, DC8 SRM 51-1-21.SDR UF6A990777Module · wornSBN - THE MODULAR 6 TITANIUM TUBE HAS A HOLE IN IT AND IS WORN DEEPLY ON BOTH SIDES. MAINTENANCE ROUTED OUT THE HOLE AND SMOOTHED THE EDGES. THE CHAFFED AREAS WRE BLENDED OUT SMOOTH. ALL WORK WAS DONE IAW WITH ENGINEERING REPORT NR 99-131. (M)SDR AU990808Nacelle · fod(AUS) RIGHT ENGINE FIRE DECK FOD. A SCREWDRIVER WAS FOUND DURING THE PRE-FLIGHT INSPECTION.SDR MWEA99456Angle · crackedUPPER AND LOWER RIB ANGLES AT STATION XN 61-410 IN LEFT PYLON IS CRACKED. MAINTENANCE FABRICATED AND INSTALLED REPAIR ANGLES.SDR UIEA99059Tee Chord · crackedDURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-SDR 99ZZZX3052Tee Chord · crackedDURING ROUTINE INSPECTION OF NR 1 AND NR 4 PYLONS, CRACKS WERE DISCOVERED IN THE RT UPPER TEE CHORD, FORWARD HORIZONTAL FLANGE, NACELLE STA 270. CRACK LENGTH IN NR 1 PYLON WAS 2.25 INCHES, NR 4 PYLON WAS 1.25 INCHES. REPAIRS ACCOMPLISHED IAW KLM DATA FAX 99-SDR USAA990710Channel · crackedCLT - DURING Q-4 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK FORWARD OUTBOARD ACCESS CUTOUT PYLON CHANNEL. INSTALLED DOUBLER PER TR 54-30-07. (M)SDR F3LA99102Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)SDR F3LA99101Fairing · crackedDEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)SDR CA990719038Heat Shield · damaged(CAN) REFERENCE: IPC FIG 82 ITEMS 23, 29, AND 57. DURING 50 HR INSPECTION FOUND SHIELD P/N 41604-01 WITH 6 CHERRY MAX RIVETS PULLED OUT WHICH SECURES HEAT SHIELD TO SKIN P/N 41667-08 AND ANGLE P/N 40667-1 ON RT NACELLE. HEAT SHIELD SHOWS TO HAVE BEEN EITHESDR UPS99230107Clevis · crackedINSPECTION TYPE:C, ENGINE NR 2 STRUTS ABOVE NR 2 HORIZONTAL FIRE WALL, CLEVIS CRACKED ON LOWER END OF LOWER STRUT. CLEVIS REPLACED IAW DWG 65-17553.SDR EIA990248Pan · wornHKG - DURING C/D CHECK, NR 3 PYLON FORWARD STRUT CLOSURE PAN, RT REAR CORNER SKIN WORN. CLOSURE PAN TRIMMED AND REPAIRED PER RS-R-71-90-34115. (M)SDR EIA990243Spar · crackedHKG - DURING C/D CHECK, NR 1 PYLON LOWER SPAR WEB CRACKED AT NAC 221.5 BL 0, DURING EO ACCOMPLISHMENT. REPAIRED PER SRM 54-10-03 FIG 2. (M)SDR EIA990235Fitting · nickedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225 HAS SEVERAL BAD NICKS. REPAIRED PER RS-R-54-54-34111 AND SRM 54-40-01 FIG 1, 8110-3. (M)SDR EIA990234Fitting · corrodedHKG - DURING C/D CHECK, NR 4 PYLON UPPER FRONT SPAR FITTING AT STATION 225, CORROSION FOUND IN BUSHING BORE. REPAIRED BUSHING BORE IAW SB 747-54-2164 FIG 2, INSURANCE CUT TO FINAL SIZE 2.360 INCH AND RS-R-54-34085, 8110-3. (M)SDR HNAA9900092Angle · chafedNR 1 ENG HORSE COLLAR CHAFED ON INBOARD SIDE, FWD ANGLE DOUBLER. PART OF MONOCOQUE STRUCTURE OF NAC CAUSE BY BONDING STRAP DEPTH= .016. BLENDED AREA IAW EO8-54-99-727.SDR A6WA9900084Bolt · failedNR 2 ENGINE PYLON TO WING, OUTBOARD LOWER BOLT HAD IS SHEARED OFF. REPLACED LOWER OUTBOARD WING TO PYLON BOLT IAW MM 54-52-00. (X)SDR EIA990215Block · scratchedHKG - DURING C/D CHECK, NR 3 NACELLE STRUT FORWARD UNIVERSAL BLOCK FOUND DEEP SCRATCH MARKS IN BUSHING BORE AREA. REPLACED FORWARD MOUNT UNIVERSAL BLOCK ASSEMBLY PER MM 71-21-02. (M)SDR ABXA9900555Angle · crackedDURING C-CHECK, FOUND NR 1 PYLON LEFT LOWER ATTACH ANGLE CRACKED AT STATION 990. REPAIRED ANGLE IAW DC9 SRM 54-04.SDR EIA990201Fitting · corrodedHKG - DURING C/D CHECK, NR 2 PYLON DIAGONAL BRACE AFT WING FITTING HAS 2 BOLT HOLES WITH CORROSION IN BORES. NR 2 PYLON DIAGONAL BRACE AFT WING FITTING BOLT HOLE CORROSION REMOVED BY OVERSIZING. HOLE SIZES TO MAX LIMIT PER SB 54-2159. (M)SDR EIA990199Pan · wornHKG - DURING C/D CHECK, NR 1 PYLON FORWARD STRUT CLOSURE PAN LEFT AND RIGHT SKIN WORN. STRUT CLOSURE PAN REPAIRED PER RS-R-71-90-34116, 8110-3. (M)SDR DL72L991467Angle · corrodedON HUSH-KIT MOD, FOUND RT NR 2 AFT MOUNT CHORD ANGLE CORRODED BEYOND MFG SPECS. REPLACED RT CHORD ANGLE WITH ONE OF NEW MFG.SDR CALA9900729Support · crackedINSPECTION FOUND A 3 INCH CRACK IN NR 1 ENGINE DIAGONAL FRAME SUPPORT AT NACELLE STA 315 ON RT SIDE. THE DIAGONAL FRAME SUPPORT WAS REPLACED IAW SRM 51-40-02.
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