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 CALA2025120911939Frame · gouged(B737-06-3-0443) NO.2 ENG PYLON FWD STRUT FAIRING, BOTTOM SIDE OF FRAME IS GOUGED FROM PANEL 441AT AFT UPPER LATCH. FABRICATED AND INSTALLED REPAIR IAW SRM 54-50-71-2R-4 .SDR DALA2025120908988Spar · crackedCRACKS WERE FOUND ON THE NR 1 PYLON FWD UPPER SPAR WEB. ACCOMPLISH ER/A 630407-14AD. (1335822)SDR DALA2025120908982Spar · crackedLEFT STRUT, LT FORWARD UPPER SPAR VERTICAL FLANGE CRACKED NSTA 221.25. ABRICATED THE UPPER SPAR AND REMOVED AND REPLACED THE UPPER SPAR CHORD IAW ER/A 630536-14. (1331241)SDR JJBA20251204013Rib · crackedRH ENGINE UPPER COWLING, FWD RIB AT XN810 FOUND CRACKED. ON RH ENGINE UPPER COWLING, FWD RIB AT XN810 REMOVED AND REPLACED.SDR DALA2025110608104Spar · crackedFOUND NO.2 PYLON FWD UPPER SPAR WEB CRACK AT NSTA 221.25 TO NSTA 237.5 FUEL LINE CUTOUT. THE NO.2 PYLON FWD UPPER SPAR WEB CRACK AREA REPAIRED AS PER PRI 629978-14 (1281183)SDR EE4Y2025103123400Spar · crackedDURING ACCOMPLISHMENT OF ALLEGIANT TASK A32X-54-481-002 , NACELLES/PYLON AFT FIXED FAIRING RHS UPPER SPAR AT SEALING RIB 15 O/B AREA WITH CRACK INDICATION.AFT FIXED FAIRING UPPER SPAR WAS REPARED FOLLOW REPAIR INSTRUCTIONS PER ALLEGIANT ENGINEERING ORDER A32X-SDR DALA2025101507552Spar Web · crackedDURING H CHECK AT STAG, A CRACK WAS NOTED ON THE NR 2 PYLON FWD UPPER SPAR WEB. A REPAIR WAS INSTALLED PER ER/A 629501-14 SECT. I. ACCOMPLISH ER/A 629501-14 SECT. II INSPECTION NOT TO EXCEED 25,783 TOTAL A/C FLIGHT CYCLES, THEN AT 12,000 FLIGHT CYCLE INTERSDR DALA2025101507550Spar · crackedNR 2 NACELLE STRUT FWD TORQUE BOX UPPER SPAR HYD TUBE CLAMP FASTENER HOLE FOUND CRACKED. REPAIRED AS PER PRI629500-14 REV.0. THE PRI629500- 14 REV.0 COMPARED AND COMPLIED WITH ER/A629500-14. (1251312)SDR CALA2025101410075Spar · crackedNO.2 PYLON UPPER FWD SPAR DOUBLER HAS CRACKED AT R/H SKIN. GENER ATED BY V919150 ON HAECO LCQ NR 9298226/40226. ESFR INFORMATION UPDATE REPAIR AREA ON #2 PYLON UPPER FWD SPAR DOUBLER AT RT SKIN IAW A3 20 SRM 54-52-12-300-036. ACMP BY V901914SDR EE4Y2025100723298Spar · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-54-471-002, LH ENGINE PYLON AFT FIXED FAIRING UPPER SPAR WITH CRACK AT RIB 15 WAS FOUND.PERFORMED REPAIR IN ACCORDANCE WITH REPAIR INSTRUCTION R54512052 ISSUE F FIG 201 AND DIAGRAM A SRM PERMANENT REPAIR 54-54-1SDR EE4Y2025100723297Spar · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT TASK A32X-54-481-002, RH ENGINE PYLON AFT FIXED FAIRING UPPER SPAR WITH CRACK AT RIB 15 WAS FOUND.PERFORMED REPAIR IN ACCORDANCE WITH REPAIR INSTRUCTION PER R54512052 ISSUE F (FIG 201 AND DIAG SRM PERMANENT REPAIR 54-54-1SDR IPXA2025101599994Rib · crackedPYLON NR 2 UPPER SURFACE AT RIB 3A HAVE A CRACK. RIB 3A REMOVED IN IAW SRM 51-40-21, WELDED. RE-INSTALLED RIB 3A AT PYLON NR 2 UPPER SURFACE, IAW SRM 51-40-21.SDR IPXA2025101599805Rib · crackedPYLON #2 I/B SIDE AT RIB 3A HAVE A CRACK. DOT 90-080. RIB 3A REMOVED IN IAW A300-600 SRM51-40-21, READY TO WELD. ++RE-INSTALLED RIB 3A AT PYLON #2 UPPER SURFACE, IAW A300-600 SRM 51-40-21.SDR IPXA2025091662750Frame · crackedNR 1 ENGINE PPANEL 475AL I/B SIDE #7 STRINGER FROM FRONT CRACKED DT 1/042 INSTALLED FRAME #7 AT 475AL USING FASTNERS IAW SRM-51-40-21SDR IPXA2025091662589Frame · crackedNR 2 ENGINE PANEL 485AL HAS CRACK ON I/B SIDE #7 FRAME FROM FRONT. INSTALLED FRAME #7 AT 485AL USING FASTENERS IAW A300-600-SRM-51-40-21SDR IPXA2025100821478Frame · crackedNUMBER 2 ENG PYLON, UPPER SIDE, BETWEEN PANEL 423AL TO 423BL, SUPPORT ARC SHAPE FRAME HAS CRACKS. REMOVED SUPPORT UPPER SIDE IN RIBS 3 #2 ENG PYLON. AFTER FURTHER EVALUATIONS 02 CRACKS FOUND OUT OF LIMITS. IAW AIRBUS A300-600 SRM 54-52-51 PAG.2 FIG.1 AND SRM SDR JR2R20250811861Frame · chafedLEFT HAND PYLON FAIRING, FRAME 5, BOTH MOUNTING LUGS ARE CHAFED OUT OF LIMITS. REPAIREDSDR DALA2025081105959Spar · crackedPERFORMED OHEC INSPECTION OF THE FORWARD UPPER SPAR HIDDEN PORTIONS OF CHORD-CF6-80C STRUT,FOUND 01EA CRACK ON THE INBOARD FASTENER HOLE OF THE WEB AT NSTA221.25. REPAIRED AS PER PRI 581786-14.SDR DALA2025080505851Spar · crackedRIGHT PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 FOUND CRACKED AROUND WIRE CUTOUT. THE R/H PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 POWER FEEDER CABLE CUTOUT CRACK AREA REPAIRED IAW PRI 628061-14 REV 0, .COMPARED AND COMPLIED WITHSDR CALA2025090108313Spar · gougedRIGHT PYLON UPPER SPAR UPPER SURFACE AT RIB 4-RIBS HAS GOUGE AREA. ACCOMPLISHED PART 1, INTERIM REPAIR PER REO-L25512 REV IR. PER EC 5451-0500. ACCOMPLISH A PERMANENT REPAIR AT RH PYLON REAR UPPER SPAR UPPER SURFACE BETWEEN RIBS 4 & 5 PER PART 3 IAW ECRA 54SDR DALA2025080105781Spar · crackedRIGHT PYLON UPPER SPAR BETWEEN NAC STA221.25 AND NAC STA237.5 FOUND CRACK AROUND HYD CASE DRAIN LINE CUTOUT. DAMAGED AREA REPAIRED PER ER/A 00-628062-14.SDR DALA2025080105782Spar Web · damagedERA 628061-14 SECTION I ISSUED FOR REPAIR TO #2 PYLON FWD UPPER SPAR WEB AT POWER FEEDER CABLE CUTOUT. DAMAGED AREA REPAIRED PER ER/A 00-628061.SDR UIEA2025070900881Frame · crackedNR 4 ENG NACELLE LT CORE COWL FRAME NR 2 FOUND CHAFED. FRAME CHAFE AREA REPAIRED IAW SRM 54-45-02-2R-1 REPAIR FIG 201. NO FURTHER DEFECTS NOTED.SDR UIEA2025070900883Frame · cracked#4 ENG R/H CORE COWL FRAME #5 (COUNT FROM FWD) FOUND CRACKED. FRAME CRACK AREA REPAIRED AS PER SRM 54-41-02-2R-2 REPAIR 2 FIG 201. NO FURTHER DEFECTS NOTED.SDR IPXA2025072822969Frame · brokenNUMBER 2 PYLON, INSIDE 485AL OTBD SIDE 5TH FRAME FWD FROM AFT END HAS BROKEN STIFFENER ON LOWER END. CLIP AND FRAME WAS INSTALLED IAW A300/600 SRM 51-40-21.SDR IXXA20250529002Frame · gougedO/B CORE COWL #1 ENG 2ND FRAME SUPPORT STRUCTURE FROM FWD HAS GOUGESDR IXXA20250429003Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 4TH FRAME FROM FWDSDR IXXA20250429002Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 2ND FRAME FROM FWDSDR IXXA20250429001Frame · gouged#2 ENG I/B CORE COWL HAS GOUGE ON 3RD FRAME FROM FWDSDR SWAA2025031404422Frame · pulled#1 ENG AFT STRUT FAIRING O/B SIDE FWD STIFFENER HAS PULLED THRU HILOCS <[01]. REPLACED FRAME SECTION AS REQUIRED REF SRM 51-40-05 AND DWG313A2700.SDR CALA2025021000324Spar · crackedRII INSPECTION REQUIRED DURING DVI OF STRUT #2 FIRE SEAL AND FIREWALL - TOP SURFACE INSPECTION WAS OBSERVED CRACK ON NACELLE STRUT FWD UPPER SURFACE. ACCOMPLISHED ALL EC/RA# 5451-01467 STEPS.SDR IXXA20250117006Frame · crackedNO. 2 PYLON, AFT FAIRING 447DB, INTERIOR FRAME IS CRACKED.SDR IPXA2025020521932Rib · crackedFAULT-STR-Z400-#2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL CHANNEL CRACKED-DOT 139/21-MR/139. INSTALLED BLEED AIR PRECOOLER IAW AMM 36-11-15-0401. INSTALLED SPLICE BRACKET AT #2 ENG PYLON TOP AREA RIB 8 LH LATERAL PANEL IAW SRM 51-40-21. REVIEWEDSDR IXXA20250128001Frame · worn#1 ENGINE, OUTBOARD CORE COWL, INNER SUPPORT STRUCTURE IS WORN. REF HAECO WO 320010 NON ROUTINE 30227SDR DALA2024122311927Rib · crackedSHIP 3308 LH PYLON LAPF LH SUPPORT NO.8 RIB CRACKED. CORRECTIVE ACTION: STOP-DRILLED AT THE END OF CRACK AT NO.8 LH RIB AND QPPLY DOUBLER REPAIR AS PER PW 51A702 CMM 54-56-11 REPAIR 13 REV 22. (0724726)SDR DALA2024121711798Pylon · crackedSHIP 1819 DURING CCK AT STAG, A CRACK WAS NOTED ON THE #2 PYLON FWD UPPER SPAR WEB. A REPAIR WAS PERFORMED PER ER/A 622989-14AD. CORRECTIVE ACTION: REVISE ER/A 622989-14AD BY 12DEC2026 TO INCORPORATE STAGE 2/3 APPROVAL WITH DTE, AND AMOC TO AD 2021-10-19. (071SDR WRXR20241211002Frame · gougedBARE METAL AND NICKS ON TOP SIDE OF PYLON FRAME PN: MM670-37223-001 COMMON TO PYLON LEADING EDGE PANEL 411AT. REMOVED O/B NUTPLATE ON FLANGE, SMOOTH AND BLENDED DAMAGED AREA IAW CRJ700 SRM 51-12-00-001-001-A01. PERFORMED REPAIR ON BARE METAL AND NICKS ON TOP SSDR SWAA2024112759044Frame · cracked#2 ENGINE AFT STRUT FAIRING SUPPORT FRAME FOR AFT FAIRING PANEL CRACKED BOTH SIDES OF FLANGE (PIC ATTACHED)<[01] REMOVED AFT STRUT FAIRING SUPPORT FRAME AND DRILLED NEW FRAME # 313A2752-1 PER SRM 51-10-02. OK TO INSTALL;[02] C/W INSPECTION AS REQUIRED C/A #1;[SDR DALA2024111110810Spar · gougedSHIP 3160 GOUGE UPPER SPAR CANTILEVER OUTBOARD SIDE BTW RIB8 AND RIB9 ON RH PYLON. CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTION ON UPPER SPAR CANTILEVER OUTBOARD SIDE BTW RIB8 AND RIB9 ON RH PYLON ASPER ER/A 621023-14 REV ORIGINAL SECTION I HAS BEEN COMPLIESDR HNAA2024121101184Rib · corrodedF005232 CORROSION ON #2 ENGINE UPPER COWLING ON 3 PROFILE REINFORCEMENTS AT CNT RIB. RAR REINFORCEMENTS IAW SRM 51-40-02SDR IPXA2024112967766Rib · crackedPYLON #1 RIB 18, PANEL 475AL SUPPORT O/B HAS A CRACK.SDR IPXA2024102465947Frame · cracked-#1 PYLON- PANEL 475AL I/B 1ST STIFFENER (FWD) HAS 1' CRACK BETWEEN RIVETS- DOT 109-067-VWV.REMOVED FRAME BRACKET BROKEN FROM PYLON #1 475AL I/B IAW A300-600 SRM 51-40-21.INSTALLED NEW FRAME BRACKET P/N 221-0081-192, BATCH 0003973110 IAW A300-600 SRM 51-40-21SDR AALA202410181445Spar · wornAIRCRAFT IN BASE MAINENANCE: #2 ENGINE PYLON SPAR WORN AT CNA SPRING SEAL CONTACT POINT AND PYLON RIB 5. REPAIRED SPAR PER SRM 54-51-12-283-003 AND EA 358940.SDR DALA2024100909863Spar · crackedSHIP 1806 LH PYLON FORWARD UPPER SPAR IDG POWER FEEDER CABLE CUTOUT CRACKED. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER ER/A 621135-14. (0597890)SDR DALA2024100909864Spar · crackedSHIP 1806 2 CRACKS WERE FOUND ON THE #1 ENGINE PYLON UPPER SPAR WEB BETWEEN NSTA221.25 AND 237.5. CORRECTIVE ACTION: REPAIRED DAMAGED AREA PER ACCOMPLISH ER/A 621135-14 SECTION II REPEAT INSPECTIONS BEFORE THE A/C REACHES 25,505 TOTAL FLIGHT CYCLES (0596820)SDR DALA2024100309655Rib · damagedSHIP 3359 L/H PYLON O/B SIDE SKIN RIB 8 EXISTING REPAIR. CORRECTIVE ACTION: COMPLIED WITH DELTA WORK CARD 5100-01848-07A AND ERA 613791-14. OK FOR CONTINUED SERVICE. (0587988)SDR IPXA2024101104287Rib · crackedPANEL 423AL HAS A CRACK (BETWEEN 3" TO 4" LONG) DOT 129-001 (GE-129) INSTALLED RIB AT PYLON #2 WITH EXISTING FASTENERS IAW A300-600 SRM 51-40-21.SDR IPXA2024101122648Rib · crackedPYLON #1 UPPER AREA PRESSURE RELIEF DOOR AFT BOLT SIDE HAS 2 POINTS WITH CRACKS 34-023. INSTALLED RIB AT PYLON #1 IAW A300-600 SRM 51-40-21 USING EXSISTING FASTENERS.SDR DALA2024090908850Spar · crackedSHIP 1805 REFER LOG #1503452, FOUND NO.1 PYLON I/B SIDE MID SPAR AFT WEB CRACK AT NAC 290. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A620276-14 (0541998)SDR DALA2024090908851Spar · damagedSHIP 1805 ERA 620276-14 ISSUED FOR REPAIR TO #1 PYLON AFT MIDSPAR WEB DTE DTA IS REQUIRED. CORRECTIVE ACTION: DAMAGED AREA REPAIRED PER ER/A 00-620276 (0541019)
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