JASC 5410
Service difficulty reports · 4,119
Reports filed under 5410 · Nacelle/Pylon, Main Frame, 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 = '5410' 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 = '5410' 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 JR2R20240307411Fitting · chafedRH PYLON OB WING MAIN BOX FITTING CHAFED ON FLANGE.SDR JR2R20240307387Retainer · chafed#1 LH AFT CORE COWL LOWER REAR SEAL FOUND SEAL RETAINER DAMAGED.SDR YENA2024030500323Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON RH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING IAW A320 SRM 54-51-12-283-002, A320 SRM 54-51-12-300-002, AND AMM 54-51-41-400-001-A TOOL USED: CALIPER: P/N: 500-197-30 S/N: A21043111, SDR YENA2024030500322Spigot · corrodedDURING HEAVY MAINTENANCE: CORROSION ON UPPER SPAR SPIGOT RECEPTACLE ON LH PYLON; REMOVED AND REPLACED SPIGOT LOWER FITTING ON LH PYLON IAW A320 SRM 54-51-12-283-002 AND A320 SRM 54-51-12-300-002. TOOL USED: DIGITAL CALIPER P/N: 500-197-30, S/N: A21043111, DUE SDR COEA2024030507734Panel · crackedDURING A SCHEDULED MAINTENANCE INSPECTION, CRACKS WERE DISCOVERED ON THE L/H ENGINE INBOARD PLENUM PANEL AFT SIDE BY THE UPPER MIDDLE STIFFENER. THIS IS THE SUPPLEMENTAL SDR FOR CORRECTIVE ACTION: WO 256404 NR 22, L/H ENGINE INBOARD PLENUM PANEL WAS REPLACED ISDR SWI2024042900326Latch · chafedR/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 4/26/2024) REPAIRED R/H UPPER TRANS COWL OUTER SKIN / FWD. DISHING AND COMPLIED WITH ALL STEPS OF NEW FINAL REO 670-54-21-1622, REV. --, 2024-03-28. COMPLIED WITH M-337 & SKY CARD 51-900-1SDR MTNA20240228001Door · missingUPON POST FLIGHT INSPECTION IN CHS, THE FO DISCOVERED THAT THE LEFT HAND ENGINE COWLING ON THE NUMBER 2 ENGINE WAS MISSING. BOTH PRE FLIGHT INSPECTIONS BY BOTH CREW MEMBERS CONFIRMED THAT THE COWLING WAS ATTACHED PRIOR TO FLIGHT. THE COWLING APPEARS TO HAVE BESDR SWAA2024030457110Acoustic Panel · peelingCREW REPORTS #1 ENGINE ACCOUSTICLE PANELPEELED UP AROUND 3 OR 4 OCLOCK POSITION<[01] REMOVED AND REPLACED #1 ENG AFT ACOUSTICAL PANEL 7-9 O?CLOCK POSITION PER AMM 72-23-02 REMOVED AND REPLACED #1 ENG 8 O?CLOCK POSITION STRUT PROFILE PER AMM 72-23-02SDR FDEA202402250241Shear Tie · cracked#2 PYLON AFT TORQUE BOX BULKHEAD INBOARD SHEAR TIE CRACKED. REMOVE AND REPLACED SHEAR TIE (313T3310-1155) USING 767 SRM REFERENCE 51-40-02-0G AND IPC 54-51-53-13C ALONG WITH BOEING DRW 313T3310-1155 & 313T3310 SH 91.SDR DU4R2024021900008Reinforcement · crackedDURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND #1 ENGINE PYLON O/B SIDE REINFORCEMENT PLATE CRACKED. S/O 634004 N/R 26173SDR DALA2024022102451Receptacle · corrodedSHIP 3271 DISC: PITTING CORROSION TRACES ON SPIGOT RECEPTACLE INNER BORE AT LH PYLON. C/A: REMOVED AND REPLACED LOWER SPIGOT FITTING ON PYLON LH AS PER A320 SRM 51-42-11-801, SRM 54-51-12-300-001, SRM 54-51-44-11 AND AMM54-41- 400-001-A. INSTALL SPIGOT BALL JOSDR CALA2024022200494Bracket · corrodedAN ANGLE SUPPORT BRACKET IS DAMAGED, LOCATED AT THE INTERIOR UPPER AFT CORNER OF 437BL ACCESS, OB SIDE IF NO 1 PYLON. REMOVED AND REPLACED BRACKET P/N 313T3380-133 IAW B767 SRM 51-40-02 PAR 7 AND PAR 9 AND BOEING DWG 313T3380. REF AMES (ILN) NRC167037-0400-0SDR AALA202402202506Sleeve · deformedAIRCRAFT IN BASE MAINTENANCE: RIGHT HAND PYLON FORWARD ATTACH FITTING OUTBOARD LOWER SLEEVE HAS DEFORMATION. REPLACED SLEEVE PER AMM 54-51-00.SDR SWAA2024021652072Nose Cowl · crackedSEVERAL AREAS AROUND INTERIOR OF #2 NOSE COWL INLET HAS ABRADABLE SHROUD CRACKED AND DELAMINATED<[01] C/W LOCAL RECONDITION ON #2 ENGINE ABRADABLE SHROUD IAW MT 772-21-05. SEE TTG8Q00RJMKC FOR WORK PERFORMED.SDR CALA2024021600436Heat Shield · cracked#1 PYLON HEAT SHIELD PAN ASSY UPPER WEB CRACKED NEAR DRAIN HOLE AND AT AFT END. REF AMES (ILN) NRC 166320-0400-0175. NEW WEB FABBED AND INSTALLED IAW AMES DOC # 47594FAB01 AND UNITED EC/RA 5456-01044. FORM# 46-0024 C/W. REF AMES (ILN) NRC 166320-0400-0175.SDR CALA2024021500425Plate · worn#2 I/B PYLON PANEL 447AL HAS WEAR MARK INTO PANEL AROUND 2 FWD HOLES. ALSO, FLAT SEAL IS NOT CORRECT SEAL. BULB SEAL SHOULD GO THE LENGTH OF THE PANEL. REF AMES (ILN) NRC 166320-0400-0050. #2 I/B PYLON PANEL 447AL BLENDED AND FOUND TO BE OUT OF LIMITS. PARTIALSDR DALA2024072907533Strake · missingSHIP 3276 DISC: NBR 1 ENGINE INB STRAKE MISSING. C/A: DEFER TO CDL 54-00-01C, PLACARD INSTALLED. (LP: 5451710)SDR VNAA2024021100024Cowling · chafedCHAFE ON R/H ENGINE UPPER FAN COWL INNER SURFACE ON INTERNAL DOUBLER NEAR FWD LATCH, MARKED WITH TAPE INSTALLED NEW R/H UPPER FAN COWL INTERNAL DOUBLER P/N CN622-0430-205 IAW CRJ900 SRM 51-42-13-001-001-A01 HN00130177 DISCREPANCY: CHAFE ON R/H ENGINE UPPER SDR CALA2024021200391Bracket · wornNO 2 ENG O/B FAN COWL HOLD OPEN ROD HAS EXCESSIVE PLAY AT STOWAGE BRACKET (REFERENCE STREAMER) FABRICATED NEW PLATE PN 314T3114-35 INSTALLED PLATE AMD GROMMET IAW B7567 SRM 51-40-02 PARA 7. REFERENCE NON-ROUTINE 167037-0400 -0203 FOR DETAAILSSDR AALA202404255009Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION MEASURING L= 13.571 IN, W= 1.343 IN. D= 0.002 IN. ON SPIGOT FITTING RECEPTACLE ON RIGHT PYLON, BETWEEN RIB 4 AND RIB 5. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR CALA2024021600437Angle · crackedNR 1 PYLON HEAT SHIELD PAN ASSY UPPER WEB STIFFENER ANGLE CRACKED ( ANGLE LOCATION IS JUST AFT OF DRAIN HOLE) REPORTED BY V921225 NEW ANGLE P/N 313T3355-315UAL WAS FABBED ON CRO WO# C/W. 166323-0400-0003. HOLES LOCATED AND WAS INSTALLED ON NR 0400-0162 AND 040SDR AALA202404251751Spigot · corrodedAIRCRAFT IN BASE MIANTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT HAND PYLON. REPLACED SPIGOT FITTING PER AMM 54-51-12-300-002.SDR NACA2024020400001Acoustic Panel · damagedLH ENGINE INLET ACOUSTIC PANEL DAMAGED AT 12 OCLOCK POSITION. DEFERRED PER DMI 72-00 ON 2/5/24 AT 0600Z IAW B767 AMM 72-00-00 TABLE 645.SDR COEA2024013004767Support Bracket · crackedWO 254814 NR 6 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED ON THE L/H NACELLE UNDER THE INERTIAL SEPERATOR MOUNTING POINT, INBOARD SIDE. LONGERON SUPPORT BRACKET. REPAIRED COWLING REINSTALLED IAW C408 MM 71-10-15.SDR AALA202401263656Spigot · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON STATIONS 6465 AND 7063, BETWEEN PYLON RIBS 3 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.SDR AALA202401261844Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT PYLON LOWER SPIGOT FITTING RECEPTACLE BETWEEN PYLON STATIONS 6465 AND 7063, BETWEEN PYLON RIBS 3 AND 5. REPLACED LOWER SPIGOT FITTING PER SRM 54-51-12.SDR N6WA2024020101Fairing · crackedRH ENGINE UPPER HINGE LINE FAIRING CRACKED. R&R CRACKED FAIRING ON RH ENGINE UPPER HINGE LINE IAW CRJ SRM 51-42-00, AMM 54-12-01SDR JJBA20240130059Cowling · crackedLH LOWER COWL, AFT LIP CRACKED. LH ENG LOWER COWL LIP REPLACEDSDR SWAA2024030543355Support Frame · cracked#1 ENGINE O/B FAN COWL FRAME SUPPORT NEXT TO OIL SERVICES DOOR IS CRACK<[01] REMOVED AND REPLACED #1 ENGINE O/B FAN COWL FRAME SUPPORT NEXT TO OIL SERVICES DOOR AS-PER SRM51-40-02-0G-0;[02] VERIFIED STEP 1SDR SWAA2024030543448Support Frame · cracked#2 ENGINE PNL#423 I/B FAN COWL SUPPORT FRAME NEXT TO OIL SERVICES DOOR IS CRACK<[01] REMOVED AND REPLACED #2 ENGINE PNL#423 I/B FAN COWL SUPPORT FRAME NEXT TO OIL SERVICES DOOR AS-PER SRM 51-40-02-0G-0;[02] VERIFIED STEP 1SDR IPXA2024013064738Panel · crackedPANEL 423BL HAS A CRACK ON THE UNDER SIDE INSTALLED DOUBLER AT COWL STRUCTURE 423BL I.A.W SRM 54-52-51 FIGURE 204. INSTALLED 2 EA SEALS AND 2 EA SEAL RETAINERS I.A.W SRM 51-40-21.SDR FXTA2040321119002Duct · chafedLH AND RH AFT ICE VANE DOOR FOUND TO BE CHAFING ON EXIT DUCT CAUSING A GROOVE TO BE WORN INTO THE SKIN WHEN ICE VANE SYSTEM IN THE NORMAL CONFIGURATION.SDR FXTA2040321119001Longeron · crackedBOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINSDR FXTA202403210095Longeron · crackedBOTH LH AND RH LOWER ENGINE COWLINGS HAVE STRUCTURE CRACKED UNDER THE ATTACHMENT OF THE ICE VANE DOOR LINKAGE CASTINGS. CRACKING WAS NOTICED COMING OUT FROM UNDER THE CASTINGS AND WHEN THE INSPECTION PANELS WERE OPENED TO LOOK AT THE STRUCTURE UNDER THE CASTINSDR SWAA2024020742762Door · cracked#1 ENGINE INBD FAN COWL WEB PANEL AFT OF OIL SERVICE DOOR IS CRACKED (MARKED)<[01] REMOVED AND REPLACED WEB PANEL PER SRM 51-10-02;[02] COMPLIED WITH INSPECTION; REMOVED AND REPLACED WEB PANEL PER SRM 51-10-02.SDR SWAA2024020642763Casting · cracked#2 ENGINE AFT PYLON AFT STRUT FAIRING AFT CASTING CRACKED<[01] REMOVED AND REPLACED PYLON AFT STRUT FAIRING AFT CASTING PER SRM 51-10-02;INSTALLED FASTENERS PER SRM 51-40-02.;[02] VERIFIED C/A #1 <BR>REMOVED AND REPLACED PYLON AFT STRUT FAIRING AFT CASTING PERSDR IPXA2024013128251Access Panel · crackedFAULT - CRACK - RIB, NO.1 PYLON INSIDE OF MID TORQUE BOX SUPPORT, CAN ACCESS FROM PANEL #436AR (REPLACE) REVIEWED REMOVED DAMAGE PARTS I.A.W SRM 51-40-02-0G REV.88.INSTALLED NEW PARTS I.A.W SRM 51-40-02-0G REV.88SDR ASAA2024011648001Support Fitting · gougedLESSOR ITEM: PYLON #2 - FWD SUPPORT - GOUGES AND FRETTING FOUND, IT HAS TO BE INSPECTED PRIOR TO ENGINE INSTALLATION. GROUNDED - YES. BLENDED OUT DAMAGE IAW A-320 SRM 51-73-00-001 AND FOUND BLEND OUTS TO BE WITHIN ALLOWABLE LIMITS IAW A-320 SRM 54-51-18-283-SDR IXXA20250115003Latch · gougedRH ENGING L/H FAN COWL AFT LATCH HOUSING HAS GOUGE. 8110-3 FVCI CONTROL NO. 25003-1.SDR IPXA2024011725517Doubler · crackedNR 1 ENGINE PYLON INBOARD EDGING ANGLE CRACK - PERFORM PERMANENT REPAIR FABRICATED DOUBLER IAW SRM 54-56-10. INSTALLED DOUBLER IAW SRM 54-56-10 CONFIG-1 PAGE 203. AT #1 ENG PYLON.SDR IPXA2024011626744Unknown · unknownCRACK IN #1 ENG AFT LOWER PYLON FAIRING. ALL STEPS COMPLETED PER SREO 32659-REQ001 APEND ASDR AALA202401179308Shroud · crackedAIRCRAFT IN BASE MAINTENANCE: RIGHT WING FUEL SHROUD IN OUTBOARD SIDE OF NUMBER 2 PYLON IS MISALIGNED AND CRACKING. REMOVED, REPLACED AND LEAK CHECKED RIGHT HAND WING FUEL SHROUD IN OUTBOARD SIDE OF NUMBER 2 PYLON.SDR IPXA2024012989730Fairing · crackedFAULT: L/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 INSTALLED NEW CHORD IAW SRM 51-40-02.SDR IPXA2024011289730Unknown · unknownL/H PYLON INBD STRUT AFT FAIRING HAS A SUPPORT CRACKED AT NAC STA 203.85 APPROVEDSDR COEA2024011201734Doubler · crackedWO 254211 NR 5 DISCREPANCY: DURING A SCHEDULED INSPECTION, A CRACK WAS DISCOVERED IN THE R/H ENGINE COWL AT THE LOWER SUPPORT STRINGER UNDER THE VAIN ACTUATOR MACHINED BRACKET. REPAIRS COMPLETED IAW SR-408-ATA54-42396 TO R/H ENGINE COWL AND INCORPORATED SDR IPXA2024032073868Frame · crackedNR 1 PYLON PRE-COOLER AERA STRUCTURE ANGLE FRAME HAS MULTIPLE CRACKED. 74-095 LOCATED DRILLED AND INSTALLED ANGLE AT #1 PYLON PRE-COOLER AREA PER REF MD-11 SRM 51-31-01-OG-0 AND 54-05-41-OG-0.SDR SWI202403110196Stand Off · crackedR/H UPPER TRANSCOWL INBD A BRACKET IS CRACKED (C-CHECK RO 3/10/2024) R/H UPPER TRANSCOWL I/B "A" BRACKET HAS BEEN REMOVED AND REPLACED REF REO# 670-54-21-971, REV B, DATED 11/28/23. REFER TO CONTINUATION SHEET FOR DETAILS. COMPLIED W/SKYCARD 51-900-1002 SSDR SWIA20240311011Transcowl · chafedR/H UPPER TRANSCOWL INBD SLIDER IS WORN/CHAFED (C-CHECK RO 3/10/2024) COMPLIED WITH ALL STEPS OF REO 670-54-21-1610 REV €“ DATED: 2024-01-26, DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE RH UPPER TRANSCOWL UPPER INBOARD SLIDER. COMPLIED WITH SKYWEST TASK CSDR DALA2024022302565Fairing · missingTHE #2 ENGINE WAS EXPERIENCING HIGH OIL CONSUMPTION. DURING THE INVESTIGATION, WHEN THE #2 ENGINE COWLS WERE OPENED, MAINTENANCE DISCOVERED THAT THE LOWER LEFT COMPRESSOR FAIRING WAS MISSING. EVIDENCE SHOWS THAT THE FAIRING ATTACHING INSERTS LOOKED TO BE "PULLSDR IPXA2024020831758Sleeve · damagedFAULT - # 1 ENGINE OBD FAN COWL LEADING EDGE INTERNAL SURFACE HAS MISSING SEVERAL FINGER SEAL . 89-139. INSTALLED 02 TRANSLATING SLEEVE EDGE PROTECTOR ON ENGINE #2 T/R, O/B IAW SRM51-40-21. REVIEWED
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