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 SWAA2024090332336Frame · crackedRIGHT ENGINE AFT PYLON AFT A-FRAME IS CRACKED. CRACK ORIGINATES AT FRAME DOUBLER AND CONTINUES THROUGH RADIUS FOR OVERALL LENGTH OF 1.2 INCHES. VERIFIED WITH NDT PART 6 PROCEDURE 23.<[01] 04 - REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPAIR- SDR SWAA2024082729482Frame · damagedRH PYLON FWD FRAME 313A2710-1 AND STIFFENER 313A2300-3 HAVE 2 EA ELONGATED HOLES ON THE I/B SIDE<[01] SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)SEE FAULT TTG8Q00VEVDL FOR FINAL DEPOSITION.;[02] C/WSDR JR2R20240818668Frame · chafedRH PYLON AFT FAIRING FWD FRAME LANDING CHAFED. REPAIREDSDR DALA2024080907966Spar · crackedSHIP 1817 #1 PYLON FWD UPPER SPAR WEB / NAC STA 221.25 - 237.5 / POWER FEEDER CABLE CUTOUT / CRACK. CORRECTIVE ACTION: ER/A 601117-14AD REV A SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 21,040 TOTAL FLIGHT CYCLES. (0486143)SDR UIEA2024062000562Frame · cracked#2 ENG L/H CORE COWL #2 FRAME (COUNT FROM FWD) FOUND CHAFING MARK.(<P>#2 FRAME CHAFING MARK AREA REPAIRED AS PER SRM 54-45-02-2R-1 REPAIR 1 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024062000563Frame · cracked#2 ENG L/H CORE COWL MOST AFT FRAME FOUND CRACK.(<P>FRAME CRACK AREA REPAIRED AS PER SRM 54-45-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR UIEA2024071400665Frame · chafedNUMBER 4 ENGINE RT CORE COWL FRAME NR 2 MID AREA FOUND CHAFING MARK, COUNT FROM FWD. FRAME REPAIRED IAW EA-1971A141 REV.0 DATE 01 JUL 24. NO FURTHER DEFECTS NOTED.SDR HNAA2024081300679Rib · corrodedE045282 CORROSION ON RH ENGINE UPPER COWLING CENTER RIB REINFORCEMENT 2 EACH. REMOVED AND REPLACED 2 CORRODED CENTER RIB REINFORCEMENTS (TRIANGLE GUSSETS) ON RH UPPER ENGINE COWLING IAW EMB 145 SRM 51-40-02, 51-20-01SDR DALA2024071507127Spar · gougedSHIP 3138 GOUGE UPPER SPAR ON WEB LOCATED AT RIB 8 TO RIB 9 INBOARD SIDE ON RH PYLON. CORRECTIVE ACTION: REPAIRED PER ER/A 619020-14. (0443580)SDR SWAA2024070501779Frame · cracked#2 ENG OUTBD COWL INTERNAL FRAME/GUSSET CRACKED AFT OF OIL SERVICE DOOR<[01] #2 ENGINE O/B FAN COWL BEING REPLACED ON FAULT TTG8Q00S5HAGSDR UIEA2024051000376Frame · chafedNO.2 ENG L/H CORE COWL #2 FRAME CHAFING (COUNT FROM FWD)(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201, NO FURTHER DEFECTS NOTED.</P>)SDR UIEA2024051000377Frame · chafedNO.3 ENG L/H CORE COWL #2 FRAME CHAFING (COUNT FROM FWD)(<P>FRAME REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.</P>)SDR SWAA2024061498230Frame · worn#2 ENGINE STRUT FORWARD FAIRING FRAME HAS WORN AREA (COMMON TO THUMBNAIL UPPER AFT LATCH)<[01] VERIFIED STEP 5 COMPLETE.;[02] VERIFIED STEPS 6 COMPLETE; STEP 7 IN PARTIAL.;[03] VERIFIED STEP 7 COMPLETE AND MEASUREMENT FIELD.;[04] VERIFIED RII STEP COMPLETE.;[0SDR DALA2024050304909Spar · crackedSHIP 1815 DURING CCK AT STAG, A CRACK WAS FOUND ON THE #1 ENGINE PYLON UPPER SPAR WEB BETWEEN NSTA221.25 AND 237.5. A REPAIR WAS INSTALLED PER ER/A 617659-14 SECTION I. CORRECTIVE ACTION: ACCOMPLISH ER/A 617659-14 SECTION II REPEAT INSPECTIONS (0321418)SDR YENA2024041600617Spar · crackedDURING HEAVY MAINTENANCE: CRACK AT I/B SPAR FITTING OF RH PYLON; REF: TOMX W/O 2527 N/R 00281 REPLACED PER EMB190 SRM 51-43-03 AND SRM 51-43-04 ETI-190-24-073 REV. I ETD2024-190-007640 REV A & EC 24-383-01.SDR YENA2024041600616Spar · crackedDURING HEAVY MAINTENANCE: CRACK AT INBD SPAR AFTER FITTING OF LH PYLON; REF: TOMX W/O 2527 NR-00282 REPLACED PER EMB190 SRM-51-43-03, SRM 51-43-04, ETI-190-24-074 REV. 1 ETD2024-190-007640 REV A& EC E24-384-01.SDR AALA202404101831Spar · wornAIRCRAFT IN BASE MAINTENANCE: LEFT HAND PYLON LOWER SPAR PLATE WORN AT RIB 5. REPLACED LOWER SPAR PLATE PER SRM 51-42-11.SDR JR2R20240329460Frame · chafedLH AFT PYLON FAIRING CENTER MOUNT BRACKETS CHAFED ON AFT PYLON FAIRING. REPAIREDSDR DALA2024032303687Rib · corrodedSHIP 3252 DISC: CORROSION RIB 8 ON REFORCING PLATE ON LH PYLON. C/A: COMPLIED WITH ER/A 616310-14AD REV.ORIGINAL. JOB COMPLETE. ASSOCIATED ER/A 00-616310 ADDED FOR AC 3252. (LP: 0251584)SDR YENA2024013000180Spar · crackedDURING HEAVY MAINTENANCE: AFTER REAMING OF AFT LUG BORE AT RH ENGINE PYLON INBD SPAR, CRACK WAS FOUND AND SPAR MUST BE REPLACED; REF TOMX WO# 2452 NR# 00431 RH ENGINE PYLON INBD SPAR WAS REPLACED PER SRM 51--43-03, SRM 51-43-04, & EMB ANNEX A RH & LH PYLON - ISDR IPXA2024013128280Rib · crackedFAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AL (REPLACE) C/W REVIEW REMOVED DAMAGE PART I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PART I.A.W SRM 51-40-02-0G REV.88SDR DALA2023122110449Unknown · unknownSHIP 0670 PYLON #1 / UPPER INBOARD SPAR CHORD / AT NAC STA. 136 / CRACK. CORRECTIVE ACTION: REF ERA 613979-14. (0117391)SDR DALA2023112909798Unknown · unknownSHIP 3120 CORROSION ON SPIGOT RECEPTACLE UPPER SPAR LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE UPPER SPAR LH PYLON AS PER A319 SRM 54-51-12-300-001. (0085856)SDR DALA2023112009545Unknown · unknownSHIP 3119 GOUGE WEB UPPER SPAR LOC. BTW RIB8 AND RI9 OUTBOARD SIDE LH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 612671-14 REV. ORIGINAL. (0072104)SDR GTIA2023112137634Spar · gougedDURING HMV FOUND GOUGE @ PYLON #1 SPAR. MDL 363MM MDW 30MM MDD 0.38MM OST 3.75MM RAF 329211302 CREATED. SDR REQUIRED.-VERIFIED NR #5001273510-0030 AND TC #1004125115-0010, REPAIR HAS BEEN ACCOMPLISHED IAW SPIRIT RAF-01 3292113-02. RE-INSPECTION REQUIRED INTERVSDR GTIA2023112137632Spar · gougedDURING HMV FOUND A GOUGE @ PYLON 2 SPAR. MDL 354MM MDW 28MM MDD 0.16MM OST 3.75MM. FINAL REPAIR DIMENSIONS W=100MM L=365MM. RAF 3292111-01. SDR ITEM.-VERIFIED NR #5001274888-0040 AND REPAIR HAS BEEN ACCOMPLISHED IAW SPIRIT RAF-01 3292111-01. RE-INSPECTION REQUSDR GTIA2023112137631Spar · gougedDURING HMV FOUND A GOUGE @ PYLON #2 SPAR. MDL 363MM MDW 30MM MDD 0.38MM OST 3.75MM FINAL REPAIR DIMENSIONS W=100MM L=365MM. RAF 3292110-02 CREATED. SDR ITEM.-VERIFIED NR #5001274370-0010 AND REPAIR WAS ACCOMPLISHED IAW RAF-01 3292110-02. RE-INSPECTION REQUIREDSDR YENA2023111701412Unknown · unknownDURING HEAVY MAINTENANCE: SECONDARY NRC IN REF NRC 00313: REPLACE INBD UPPER SPAR RH PYLON; (RESOLVED ON W/O: 1260255 TASKCARD: NR-00027 ) REF TOMX W/O# 2362, N/R # 00350. INBD UPPER SPAR RH PYLON WAS REPLACED PER EMB-190 SRM 51-43-03 SRM 51-43-04 AND SRM 51- SDR DALA2023110909236Unknown · unknownSHIP 192 #2 PYLON / FORWARD UPPER SPAR WEB / CRACK AT FUEL LINE PASS-THROUGH. CORRECTIVE ACTION: ERA 595324-14 REV A SECTION III FOLLOW-ON INSPECTIONS ARE REQUIRED WITHIN 12,000 FLIGHT CYCLES FROM SECTION I REPAIR EMBODIMENT. THEREAFTER, REPEAT SECTION III WITSDR DALA2023102008656Unknown · unknownSHIP 6811 MIGRATED BUSHING ON FORWARD UPPER SPAR FITTING ON LH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00117: BUSHINGS ON LH PYLON ATTACH FITTING WERE FABRICATED AND REPLACED PER B757-200 SRM 54-51-90. (0025613)SDR FDEA202310161768Frame · cracked#1 PYLON: NACELLE STA 329, MID-SPAR FRAME IS CRACKED AT THE INBOARD, UPPER CORNER REPAIRED #1 PYLON, NAC STA 329 FRAME IAW FEDEX EA # H-5450-T0376579-P1, RELEASED OCT 10, 2023, TITLED "NACELLES/PYLON - WING PYLON/STRUT - #1 PYLON NAC STA 329 FAIRING FRAME,SDR DU4R202310050037Rib · gougedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND R/H PYLON TO ENGINE FORWARD FITTING (PYRAMID) AT THE LOWER INBOARD AND OUTBOARD HOLES, JUNCTION TO RIB 1 AND LOWER SPAR HAS GOUGES AND CRACK INDICATIONS. S/O 339001 N/R 28478SDR DU4R202310040035Spar · corrodedDURING SCHEDULED INSPECTION, FOUND LT PYLON UPPER SPAR HAS CORROSION AT NUMEROUS LOCATIONS FWD OF PRE-COOLER BAY AND IN THE PRE-COOLER BAY. S/O 339001 N/R 28357SDR SWAA2023100205254Frame · cracked#1 ENGINE AFT PYLON HAS A CRACK IN THE AFT 'A' FRAME. CRACK IS 1 INCH LONG AND STOPS IN THE FRAME RADIUS.<[01] PERFORMED EA M-23-154-01884 (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- TIME LIMITED) TTG8Q00NPC7K;[02]SDR SWIA202309200010Unknown · wornREMOVED FRAME SPLICE @ FS 265 STR 23LH TO FOM REF CRJ 200 SRM 51-42-06. (FILED CLOSED) INSTALLED SAME SERVICEABLE FRAME SPLICE @ FS 265 STR 23LH TO FOM REF CRJ 200 SRM 51-42-06. COMPLETED 51-900-1003-SKY AND M-337.SDR DALA2023091107411Unknown · unknownSHIP 3274 GOUGE ON WEB LOC. UPPER PYLON BTW RIB08 TO RIB09 IB SIDE ON RH PYLON. CORRECTIVE ACTION: COMPLIED WITH ERA 611339-14 REV. ORIGINAL. (2963121)SDR GTIA2023082437437Spar · damagedDURING HMV FOUND A GOUGE @ PYLON #1 LOWER SPAR. MDL 337.13MM MDW 8.5MM MDD 0.49 OST 3.75MM RAF 3329127-01. OPEN SDR ITEM.-VERIFIED NR # 5001257255-0010 AND TC # 1004054607-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2333 REV 00 REINSPECTION REQUIRSDR GTIA2023082437436Spar · damagedDURING HMV FOUND A GOUGE @ PYLON #2 LOWER SPAR. MDL 340.45MM MDW 6.37MM MDD 0.31MM OST 3.75. RAF # 3329126-02 OPEN. SDR ITEM.-VERIFIED NR # 5001257257-0010 AND TC # 1004054608-0010. REPAIR HAS BEEN ACCOMPLISHED AS PER SPIRIT EA 5451-2334 REV. 00 REINSPECTION RSDR IPXA2023081293881Frame · crackedINSPECTION TYPE:CPANEL 485AL HAS A CRACKED FRAME FLANGE.FABRICATED NEW FLANGE IAW SRM 55-55-51.SDR IPXA2023062493505Spar · crackedINSPECTION TYPE:1CENGINE 1 I/B SIDE INLET COWL REAR SPAR HAS 1 EA CRACK AT 3 O'CLOCK POSITION.FABRICATED WEB SPAR AND REPLACED IAW SRM 51-40-21 AND P&W SRM 54-10-00.SDR CALA2023053101728Frame · crackedLH PYLON INBD NUMBER 3 FRAME (FROM FWD) LOWER AREA CRACKED. REPAIRED IAW ECRA 5452-01606 REF UARI-54-0009 REV 1. ECRA AUTHORIZES REPAIR OF DAMAGED FRAME PER SB 777-54-0044 ORIGIONAL REVISION WORK PACKAGE 2 AND AUTHORIZATION TO OMIT INSPECTION OF COUNTERSINKS.SDR IXXA2023052801Frame · damaged#2 PYLON L/E FRAME DAMAGEDSDR DALA2023042403161Unknown · unknownSHIP 184 FOUND NO.2 STRUT FWD UPR SPAR WEB CUTOUT CRACK AT NAC STA 188.00 AND 193.00. CORRECTIVE ACTION: THE CRACK AT NSTA 177 RBL 3, LENGTH 1.5" ; NSTA 175 RBL 1, LENGTH 0.5" AREA TRIMED OUT AND APPLY DOUBLER REPAIR WITH 2024T3 -0.125"CLAD ALUMINIUN SHEET AS SDR DALA2023032302237Unknown · unknownSHIP 199 FOUND NO.1 STRUT FWD UPPER SPAR WEB OB DRAIN HOLE CRACK AT NAC STA 157.00. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A606582-14 REV.ORIGINAL. (2675900)SDR DALA2023031701975Unknown · unknownSHIP 199 ERA 606582-14 ISSUED FOR CRACK FOUND ON THE #1 PYLON FORWARD UPPER SPAR WEB AT LH DRAIN HOLE. FOLLOW ON ACTI ON IS REQUIRED. CORRECTIVE ACTION: ERA 606582-14 SECTION II DUE AT 50000 TOTAL FLIGHT CYCLES (DUE I N 34276 FC), THEN EVERY 12,000 FC THEREAFTSDR DALA2023020700929Not Reported · not reportedSHIP 1821 FOUND OUT NO.1 PYLON TORQUE BOX UPPER SPAR CRACKED AT WIRE BUNDLE CUT OUT HOLE AT NAC STA 183. CORRECTIVE ACTION: TRIMED OUT THE DAMAGED AND PERFORMED DOUBLER REPAIR AS PER PRI: 605668-14 (2617927)SDR DALA2023020700928Not Reported · not reportedSHIP 1821 NO.2 PYLON TORQUE BOX UPPER SPAR HYD LINE CUT OUT HOLE FOUND CRACK. CORRECTIVE ACTION: TRIMED OUT THE DAMAGED AND PERFORMED DOUBLER REPAIR AS PER PRI: 605623-14 (2617902)SDR DALA2023020700919Not Reported · not reportedSHIP 1821 ER/A 605668-14, ER/A 605668-14 ISSUED FOR A CRACK TO PYLON #1 FWD UPPER SPAR WEB BETWEEN STA 221.25 AND 237.5. DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: DTA DTE DAMAGE TOLERANCE ANALYSIS REQUIRED ON OR BEFORE 02FEB2025. (26145SDR DALA2023020300851Spar · crackedERA 605623-14 ISSUED FOR CRACK TO #2 PYLON FWD UPPER SPAR WEB BE TWEEN STA 221.25 AND 237.5. DTA DTE DAMAGE TOLERANCE ANALYSIS IS REQUIRED. CORRECTIVE ACTION: PER ER/A 605623-14 REV A, DTE ANALYSIS FOR THE SECTION I REPAIR COMPLETED. DAMAGE TOLERANCE ASSESSMENSDR DALA2023011700336Frame · crackedCRACK ON FRAME NAC STA 200 ON INBOARD CORE COWL OF RH ENGINE. CORRECTIVE ACTION: SUMMARY OF NRC 00450: FRAME NAC STA 200 ON INBOARD CORE COWL OF RH ENGINE WAS REPAIRED PER DELTA CMM 71-11-73 PAGE D601 IN REFERENCE TO EA 06-476772-14 REV. B. (2581590)
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