JASC 5411
Service difficulty reports · 1,454
Reports filed under 5411 · Nacelle/Pylon, Frame/Spar/Rib, 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 = '5411' 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 = '5411' 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 ASAA0945680Frame · gougedNR 2 PYLON TE FAIRING UPPER FWD ACCESS PANEL AFT ATTACHMENT AFT APERTURE FRAME GOUGED REMOVED AND REPLACED NR 2 PYLON AFT APERTURE FRAME.SDR SWIA200921944Frame · crackedRIGHT INBOARD NACELLE FRAME CRACKED. (C CHECK) REPAIRED PER SRM.SDR SWIA200922064Frame · corrodedENGINE PYLONS K-FRAME MOUNTS CORRODED. (C CHECK) REPLACED PER AMM.SDR F3LA2009043000083Frame · brokenDURING C4 C-CHECK, INSPECTION NOTED THAT THE LEFT PYLON HAS A BROKEN FRAME ON THE OUTBOARD SIDE NEAR AFT CORNER OF THE PRECOOLER. MAINTENANCE FABRICATED AND INSTALLED REPAIR EXTRUSION, REFERENCE SRM 51-42-11 AND 51-72-11.SDR CALA2009042400213Frame · damagedNR 1 PYLON NAC STA 285 O/B FRAME CHORD FOUND DAMAGED. NR 1 PYLON NAC STA 285 O/B FRAME CHORD REPLACED PER SRM 51-40-02.SDR DL76L090664Spar · crackedFOUND AT PSV, THE NR 2 PYLON UPPER SPAR WEB CRACKED AT THE CUTOUTS FOR HYDRAULIC DRAIN AND SUPPLY LINES, AND THE PRESSURIZED FUEL LINE.SDR TAMF20090025SFrame · crackedDURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-055 AND CV09-0833-04.SDR TAMF20090023SFrame · crackedDURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 2 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 54-054 AND CV09-0811-02.SDR TAMF20090022SFrame · crackedDURING C3 CHECK INSPECTION WAS FOUND A CRACK ON NR 1 ENGINE CORE COWL FRAME STA NAC 303.75. REPAIR ACCOMPLISHED IAW EWO 767 54-087 AND ROHR CV09-0810-03.SDR 2009FA0000226Rib · crackedDURING ACCOMPLISHMENT OF STC NR ST02664CH, INSTALLATION OF ENGINES, THE PYLONS REQUIRE DISASSEMBLY AND MODIFICATION. DURING DISASSEMBLY OF THE LT PYLON, THE AFT PYLON CENTER RIB WAS FOUND CRACKED AT THE LOWER STRINGER CUT-OUT. THE CRACK EMANATES FWD FROM THESDR 2009FA0000225Rib · crackedDURING ACCOMPLISHMENT OF STC ST02661CH, INSTALLATION OF ENGINES, THE PYLON REQUIRES DISASSEMBLY AND MODIFICATION. DURING DISASSEMBLY OF BOTH LT AND RT PYLONS, THE AFT PYLON CENTER RIB WAS FOUND CRACKED AT THE LOWER STRINGER CUT-OUT. THE CRACKS ARE EMANATING SDR DL757090427Spar · damagedNR 1 ENGINE PYLON AFT SPAR HAS HEAVY CHAF WEAR AT OTBD FLANGE. REPAIRED/COMPLIED WITH PER ERA 472310-14AD REV O.SDR TAMF20090008SFrame · chafedDURING C3 CHECK INSPECTION FOUND ENG NR2 RH CORE COWL NAC STA 303.75 FRAME AND STRAP WITH CHAFING. REPAIRED ACCOMPLISHED IAW EWO 767 54-048 AND ROHR CV 09-0629-01.SDR TAMF20090007SFrame · crackedDURING C3 CHECK INSPECTION FOUND ENG NR 2 RT CORE COWL NAC STA 275 FRAME CRACKED. REPAIR ACCOMPLISHED IAW EWO 767 54-049 AND ROHR CV 09-0629-01.SDR IPXA09M55146Rib · dentedINSPECTION TYPE:3C COMPLY WITH ATTACHED WAN 1373016 AND EO MD11-5480-28541-B PARA 4B AND PARA 6C. REMOVED, DRILLED AND INSTALLED NEW RIB FORMER IAW IPXA EO MD11-5480-28541-B.SDR SWIA200921835Frame · crackedC-CHECK, LEFT NACELLE FRAME NR 1 CRACKED. REPLACED PER SRM.SDR CA090220003Spar · cracked(CAN) DURING INSP IAW AWD 97-10-16 (A) CONTROL ROTOR PN 36209-3, SN 449. FOUND CRACKED AT LOWER BOLT HOLE .600 FROM END OF SPAR.SDR KCSA091009Frame · crackedNR 4 PYLON REAR ENG MOUNT BULKHEAD I/B FWD FRAME LOWER FASTENER HOLE CRACKED.SDR GLBA20090212AARib · wornMAJOR REPAIR - DURING SCHEDULED INSPECTION MAINTENANCE THE LEFT FORWARD INBOARD NACELLE KEEL RIB FLANGE WORN AT THE UPPER CORNER AREA AT APPROXIMATELY BL 91.75. MAINTENANCE REPAIRED THE LT FORWARD INBOARD KEEL RIB FLANGE AT THE UPPER CORNER AREA AT APPROXIMATSDR KCSA091006Rib · crackedNR 4 PYLON HAS A 4 INCH CRACK ON THE NAC STA 236 BULKHEAD INTERNAL RIB AT PYLON SHUTOFF VALVE INBOARD SUPPORT ROD MOUNT BRACKET.SDR DL76S091521Fitting · fracturedNR 2 PYLON INBOARD MIDSPAR FITTING WAS REPAIRED IAW ERA 472678-14. C/W 472678-14.SDR F3LA2009012600010Stringer · crackedINSPECTION NOTED NR 2 ENGINE UPPER PYLON RIB 06 FORWARD INBOARD STRINGER WAS CRACKED AT CORNER HOLE. MAINTENANCE PERFORMED REPAIR BY FABRICATING SUPPORT ANGLE AND INSTALLING PER SRM 51-42-11 AND 54-52-12.SDR SWIA200921283Frame · crackedC-CHECK, RIGHT HYD PACK FRAME CRACKED. REPLACED PER SRM.SDR SWIA200821275Frame · crackedLEFT NACELLE POWER & CONDITION LEVER PULLEY QUADRANT SUPPORT FRAME IS CRACKED (C CHECK). REPLACED PER SRM.SDR KCSA081611Rib · crackedNR 2 PYLON O/B RIB CRACKED 1.5 INCH AT NAC STA 267.SDR FDEA200812025049Spar · crackedNR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS 4 INCH CRACK, REFERENCE INSPECTION OF PYLON S177 WORKCARD 54X1201ALI-P2. COMPLIED WITH HFEC. VERIFIED NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS CRACKED INDICATION PER NDTSPM. REMOVED AND FABRICATED NEW WEB REF DWG SDR KCSA081608Rib · crackedNR 2 NAC STA 211 I/B RIB CRACKED 1 INCH, BELOW MIDSPAR.SDR AALA200810312Rib · crackedLEFT ENGINE PYLON, CRACK IN LOWER FORWARD END OF THE INBOARD RIB JUST ABOVE PANEL NUMBER 8111C. REPAIRED PER SRM 54-21-00 FIGURE 2 SHEET 1 AND 2, 54-01-00 FIGURE 2 SHEET 2 AND 51-60-00 FIGURE 1 SHEET 1.SDR GUUA11070802Keelbeam · crackedDURING SCHEDULED ROUTINE MAINT DISCOVERED LT NACELLE INBD KEEL HAS A 1.0 INCH CRACK FWD OF LANDING GEAR TRUNION BOLT. REMOVED AND REPLACED LT NACELLE INBD KEEL.SDR B62R20081107003Frame · crackedNR 1 & NR 2 ENG PYLON, STRUT AFT FAIRING HEAT SHIELD SPAR STRUCTURE, NR 5 FRAME P/N 313W3813-X HAS A 4.50 INCH CRACK ON THE LOWER AFT INBD CORNER. CRACK IS IN THE SAME LOCATION ON BOTH NR 1 & NR 2 ENG PYLON FRAMES. NR 2 ENG PYLON FRAMES NR 1 THRU NR 4, P/N'SSDR B62R20081106002Spar · corrodedNR 2 ENG PYLON STRUT, AFT FAIRING HEAT SHIELD LOWER SPAR STRUCTURE, PITTING CORROSION FOUND THROUGHOUT SPAR STRUCTURE, CHORDS, FRAMES 3, 4 & 5. EVIDENCE OF PITTING CORROSION AND HEAT DAMAGE ON LOWER SIDE OF WEBS. REF 54-51-71 PG 6. POSSIBLE CAUSE WAS AFT FASDR 08FDEA04585Spar · misinstalledNR 1 PYLON, WHEN THE 311N5220-52 BATHTUB FITTING WAS LOCATED AND DRILLED C/M TO THE INBD LOWER SPAR 3 HOLES WERE MISLOCATED CAUSING A MISALIGNMENT C/M TO THE LWR SPAR. REAMED OTBD HOLE "A' TO 0.3267 DIA AND INSTALLED 1 BACB30US5K(*) X BOLT. REAMED OTBD HOLE SDR 08FDEA04419Rib · wornNR 3 PYLON PANEL 489 AL HAS A WORN RIB. REMOVED & REPLACED RIB IN REF TO DAC DWG AUB 7107; REV " P '.SDR KCSA081505Frame · corrodedNR 3 PYLON NAC STA 221.9 BULKHEAD LT FWD FRAME WEB CORRODED. (K)SDR KCSA081504Frame · corrodedNR PYLON NAC STA 221.9 BULKHEAD RT FWD FRAME WEB CORRODED. (K)SDR KCSA081503Doubler · corrodedNR 3 PYLON NAC STA 221.9 BULKHEAD FWD FRAME WEB DOUBLERS CORRODED. (K)SDR KCSA081502Frame · crackedNR 3 PYLON NAC STA 221.9 BULKHEAD LT AFT FRAME WEB CRACKED. (K)SDR KCSA081501Frame · crackedNR 3 PYLON NAC STA 221.9, BULKHEAD RT AFT FRAME WEB CRACKED AT (2) SPOTS. 750 AND .250. (K)SDR 08FDEA04000Rib · chafedNR 3 PYLON PANEL 489 AL FWD RIB IS CHAFED. REMOVED & REPLACED RIB IAW DWG AUB 7107 & SRM 51-35-01.SDR 08FDEA03999Rib · chafedNR 1 PYLON PANEL 439 AL FWD RIB IS CHAFED THROUGH. REMOVED RIB IAW ARM 51-35-01; VOL II. LOCATED AND DRILLED THE NEW RIB P/N AUB 7107-39, PO 631193.2 IAW DWG AUB 7107; REV "P". INSTALLED NEW RIB IAW SRM 51-35-01; VOL II.SDR 08FDEA03874Spar · crackedFOUND ON LOWER SPAR OF PYLON NR 1 UPPER SURFACE CRACK IN CENTER STIFFENER AT RIB 10A. REPAIR PERFORMED BY CUT OUT THE CRACKED AREA AND INSTALLING A DOUBLER IAW DRAWING R546-10349, APPROVED BY RAS/70512822/010/2008 ISS A, APPROVED BY EA 6-5451-123098.SDR 08FDEA03873Longeron · wornFOUND ELONGATED HOLE ON AFT FAIRING ADAPTER LONGERON, PYLON NR 1. REPAIR PERFORMED BY WELDING THE LONGERON OVERSIZE FASTENER HOLE AND REDRILL THE FASTENER HOLE SAME AS ORIGINAL IAW RAS/ROHR/0776/2008 ISS A, APPROVED BY EA 6-5455-123139.SDR DL757081169Spar · damagedDURING CURRENT HMV, AN OVERSIZED HOLE WAS FOUND ON THE SPAR CHORD, NR 1 PYLON, DURING ACCOMPLISHMENT OF PYLON MOD. SUBJECT HOLE IS COMMON TO SIDE STRUT SKIN. BOEING WAS CONTACTED CONCERNING OVERSIZING SUBJECT HOLE, INSPECTING, AND INSTALLATION OF OVERSIZED FSDR CALA0800858Frame · crackedNR 1 ENGINE PYLON, AFT BULKHEAD CRACKED AT HOLE NR 19, REF EA 5440-01234 OP 11 STEP 4.3. COMPLIED WITH PPS205.65 NEW TORQUE BULKHEAD FITTING REMOVAL AND INSTALLATION REF ECRA 5450-01749.SDR 08FDEA03677Spar · corrodedCORROSION FINDINGS AROUND PYLON NR 2 SPIGOT BEARING HOLES, UPPER SPAR RIB 12-13. REPAIR PERFORMED BY CORRSOION REMOVAL, NDT FOR CORROSION FREE CONDITION AND SURFACE PROTECTION IAW. RAS/70512899/009/2008 ISS.A, APPROVED EA 6-5451-123134.SDR EIA2008032Frame · crackedPYLON NR 4 AFT ENG MOUNT, RT (1/B) AFT FRAME, 1 HOLE CRACKED PER NDT REPORT. MFGR NEW FRAME PER DRW NR 65B90310 INSTALLED PER 51-30-02 - 51-24-11 - BAL5119.SDR NWAA084066731Frame · crackedDURING L CHECK FOUND CRACK IN NR 4 PYLON REAR ENGINE MOUNT BULKHEAD FORWARD FRAME AT NAC STA 222.90. REPAIRED PER EA 67-213556.SDR KCSA081394Frame · crackedNR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 & .250 INCHES) AT 221.9, LBL 5, WL 150. (S)SDR KCSA081393Frame · crackedNR 3 PYLON REAR ENG MOUNT BULKHEAD LT AFT FRAME WEB IS CRACKED (.250 INCHES & .750 INCHES) AT 221.9, LBL 6, WL 148.5. (S)SDR KCSA081392Frame · crackedNR 2 PYLON REAR ENG MOUNT BULKHEAD LT FORWARD FRAME WEB IS CRACKED (.250 INCHES) AT 221.9, LBL 5, WL 148.5. (S)
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