JASC 5410
Service difficulty reports · 4,114
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 SWAA2024091637923Heat Shield · cracked#2 ENGINE STRUT AFT HEAT SHIELD SKIN HAS A LARGE CRACK #2 ENGINE STRUT AFT HEAT SHIELD SKIN HAS A LARGE CRACK REF. SRM 54-50-70-1A-3 ALLOWABLE DAMAGE LIMITS 4(B)<[01] REPAIRED #2 ENG AFT FAIRING PLUME SUPPRESSOR PER SRM 54-50-70-2R-7. DVI REQUIRED EVERY 30 DAYSDR DALA2024091609068Fitting · corrodedSHIP 3133 CORROSION SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE BORE ON LH PYLON AS PER AIRBUS A319 SRM 54-51-12-300-001. AND A320 FAM AMM 54-51-41-400- 001-A. (0556699)SDR HYIA20240911001Beam · crackedDURING MAINTENANCE A CRACK WAS VISUALLY IDENTIFIED ON THE AFT SIDE OF THE LEFT NACELLE CROSSOVER BEAM (P/N: 5654104-11). THIS CRACK MEASURES APPROXIMATELY 1.316 INCHES IN LENGTH, AND BEGINS AT THE TOP INBOARD TURBO BRACKET MOUNTING HOLE ON THE AFT FACE OF THE SDR CALA2024091002406Fairing · crackedNO.2 ENGINE AFT FIXED FAIRING AFT EDGE CRACKED REF AAR N/R 9904799.SDR DALA2024090908819Support Bracket · corrodedSHIP 3148 CORROSION ON SUPPORT BRACKET AFT ATTACH FITTING ON AFT FIXED FAIRING LH PYLON. CORRECTIVE ACTION: REPLACED SUPPORT BRACKET AFT ATTACH FITTING ON AFT FIXED FAIRING LH PYLON PER AMDS CARD 5450-6010-LTSDR SWAA2024091135177Fitting · cracked#1 ENGINE PYLON AFT STRUT FAIRING ASSEMBLY FITTING IS CRACKED AND REQUIRES PERMANENT REPAIR OR REPLACEMENT.<[01] REMOVED AND REPLACED #1 ENGINE PYLON AFT STRUT FAIRING ASSEMBLY P/N 313A2752-1 PER SRM 51-40-02.SDR DALA2024090908807Fitting · corrodedSHIP 3144 CORROSION SPIGOT FITTING RECEPTACLE BORE ON RH PYLON. CORRECTIVE ACTION: REPLACED LOWER SPIGOT FITTING LH PYLON AS PER A319 SRM 54-51-12- 300-001. (0542779)SDR DALA2024090608781Fitting · corrodedSHIP 3148 CORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR ON LH PYLON. CORRECTIVE ACTION: REPLACED NEW SPIGOT RECEPTACLE FITTING UPPER SPAR ON LH PYLON AS PER A319 SRM 51-42-11 AND AS PER A319 SRM 54-51-12-300-001. (0540982)SDR DALA2024090308642Fitting · corrodedSHIP 3144 CORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR AT LH PYLON. CORRECTIVE ACTION: REPLACED LOWER SPIGOT FITTING LH PYLON AS PER A319 SRM 54-51-12- 300-001. (0535655)SDR SWAA2024090433223Inlet · crackedFOUND 8 CRACKED OR MISSING RIVETS AND POSSIBLE CRACKED SHEETMETAL ON RH SIDE OF ENG #2 INLET COWL<[01] 01 - REMOVED AND REPLACED PER [AMM 71-11-01-400-802-F00-NG (INSTALL THE INLET COWL (SLING AND OVERHEAD HOIST) - PERMANENT)SDR AALA202411201541Receptacle · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON RIGHT HAND PYLON. REPLACED SPIGOT FITTING RECEPTACLE PER A321 SRM 54-51-12.SDR AALA202410103577Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT HAND PYLON. REPLACED SPIGOT FITTING PER A319 SRM 54-51-12-300-001.SDR AALA202409202160Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN PYLON RIBS 4 AND 5. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR SWAA2024090332338Fairing · cracked#2 ENGINE AFT PYLON HAS A CRACK IN THE AFT A-FRAME THAT STARTS AT A PREVIOUSLY DOCUMENTED CRACK. IT BEGINS IN THE FRAME RADIUS AND ENDS IN THE SAME RADIUS. CRACK IS .150 LONG. SEE PREVIOUS WRITE UP. SEE ORIGINAL WRITE UP TTG8Q00VK0GY.<[01] 04 - REPAIRED PER [ESDR UIEA2024082800857Bolt · missingENGINE 1, NEAR TO FORWARD ENGINE MOUNT, LH SIDE, FIREWALL PROTECTION, MISING BOLTS.(<P>ENG 1, NEAR TO FORWARD ENGINE MOUNT, LH SIDE, FIREWALL PROTECTION, BOLTS WERE INSTALLED CORRECTLY IAW AMM 54-54-03-404-002</P>)SDR AALA202410100380Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LOWER SPAR FITTING BORE OF SPIGOT RECEPTACLE OF RIGHT WING. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-002.SDR IXXA20241003004Fan Cowl · delaminated#1 END INBD FAN COWL LOWER FWD LANDING HAS PAINT WORN OFF EXPOSING COMPOSITE. HAECO WO 320008 NON ROUTINE 40562SDR IXXA20241003002Fan Cowl · eroded#2 ENG OB FAN COWL LEADING EDGE IS ERRODED. HAECO WO 320008 NON ROUTINE 40568SDR SWIA202412240827Drag Fitting · crackedSUSPECTED CRACK ON THE RIGHT SIDE FWD DRAG FITTING. (C-CHECK RO 12/21/2024) (FILED CLOSED)PERFORMED REPAIR OF RH FWD DRAG ANGLE FITTING REF BOMBARDIER R.E.O. 670-55-31-018 REV. -A DATED 2016-11-18. COMPLIED WITH 51-900-1002-SKYSDR AALA202409065305Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN WS 3758 AND WS 4067, BETWEEN RIBS 7 AND 8. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR AALA202409061200Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON LEFT HAND PYLON SPIGOT FITTING RECEPTACLE BETWEEN WS 3758 AND WS 4067, BETWEEN RIBS 7 AND 8. REPLACED SPIGOT FITTING PER SRM 54-51-12.SDR YENA2024082701176Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON PYLON SPIGOT FITTING AT RH PYLON; (RESOLVED ON W/O: 1301603 TASKCARD: NR-00043) REF AEROMAN WO#2024-50/1 NR# 2024- 216663 REMOVED AND REPLACED SPIGOT FITTING LOC ON PYLON RH SIDE IAW A320 SRM 54-51-12-300-002. THIS REPAIRSDR YENA2024082701175Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION ON PYLON SPIGOT FITTING AT LH PYLON; (RESOLVED ON W/O: 1301603 TASKCARD: NR-00045) REF AEROMAN WO: 2024-050/1NR 2024-210650. REMOVED AND REPLACED SPIGOT FITTING LOC. ON LH PYLON LH SIDE IAW A320 SRM 54-51-12-300-002. THIS RESDR AALA202408278305Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON RIGHT-HAND PYLON. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR AALA202408277155Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SPIGOT FITTING RECEPTACLE ON LEFT-HAND PYLON. REPLACED SPIGOT FITTING PER SRM 54-51-12-300-001.SDR SWAA2024100431333Fastener · looseLT ENGINE NOSE COWL INLET LIP SKIN FASTENER AT 6:00 O'CLOCK NOT COMPLETELY SEATED. 124-001<[01] L/H INLET NOSE COWL BEING REPLACED UNDER TTG8Q00S70ZP;[02] L/H INLET NOSE COWL BEING REPLACED UNDER TTG8Q00S70ZPSDR SWAA2024082628177Fairing · cracked#1 AFT STRUT FAIRING CRACKED.<[01] 04 - REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPAIR- CRACK; #1/#2 ENGINE PYLON AFT STRUT SUPPORT FAIRING ASSY- REPAIR REFERENCE)];[02] VERIFIED REPAIRED PER [EA M-23-154-01884-REPREF (737-700/-800 - SWA-REPSDR DALA2024081908249Fitting · corrodedSHIP 3148 CORROSION ON SPIGOT RECEPTACLE FITTING UPPER SPAR ON RH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT RECEPTACLE FITTING UPPER SPAR ON RH PYLON AS PER A319 SRM 54-51-12-300-001. (0508887)SDR 2024F00191Door · erodedTHE R/H LOWER COWLING HAS LARGE CHIPS OF PAINT COMING OFF ON THE FWD. AREA WHICH IS EXPOSING THE COMPOSITE AREA, MULTIPLE AREAS OF COMPOSITE HAVE ERODED AWAY.SDR SWAA2024082127079Fairing · cracked#1 PYLON AFT WEDGE FWD WEB HAS A CRACK EXTENDING 1.6 INCHES FROM FWD WEB OVERLAP ACROSS RADIUS TO O/B FRAME.<[01] REMOVED AFT WEDGE FAIRING PER SRM 51-40-02.;[02] REPLACED AFT WEDGE FAIRING PER SRM 51-40-02.SDR CALA2024082000468Intake · damagedBIRDSTRIKE, EXCEPT AT ENGINE INLET ACPED BIRD STRIKE INSP REF GNMM 05-51-18 OK TO CONTINUE SEVICE.SDR SWAA2024081926183Fairing · crackedRIGHT # 2 ENGINE NACELLE STRUT FAIRING AFT CASTING CRACKED MARKED VERIFIED PER NDT PART 6 51-00-00 PROCEDURE 23<[01] ACCOMPLISHED TIME LIMITED REPAIR PER EA M-23-154-01884;[02] INSPECTION C/W.ACCOMPLISHED TIME LIMITED REPAIR PER EA M-23-154-01884SDR R61A2024081700360Frame · crackedPOSSIBLE CRACK FOUND ON OB PYLON UPPOR CHORD AT RH ENG BLKHD. MX PYLON WAS (MAJOR) REPAIRED ON RO#018175-2024 AND ETD2024-019502, AND 2024-020044. PYLON WAS SHIPPED BACK TO YQG FOR INSTALL.SDR YENA2024081301121Fitting · corrodedDURING HEAVY MAINTENANCE: CORROSION SPIGOT FITTING ON RH PYLON (1 EA); (RESOLVED ON W/O: 1301446 TASKCARD: NR-00051) REF AEROMAN WO # 2024-51/1 NR # 2024-371044 REPLACED LOWER SPIGOT FITTING IAW A320 SRM 54-51-12-300-002 STEP 2.A(3) TO (9).SDR IXXA2024081200001Fan Cowl · wornWEAR BEYOND LIMITS. LOWER FWD INNER EDGE WORN THROUGH EDGE PROTECTOR AND 1 PLY OF CARBON FIBER THAT MEASURED 16.75 INCHES X 1.2 INCHES.SDR IXXA2024081202Angle · cracked#2 ENGINE AFT O/B PYLON HYDRAULIC BAY DOOR CRACKEDSDR CALA2024081200401Access Door · missingPDA 2 NACELLE STRUT ACCESS DOOR ( PANEL #436AR ) MISSING, INBOARD OF ENG 1 PYLON. UPDATED WITH PICTURE. UPDATED WITH SUBMITTED ESDR REPORT. UPON LANDING WITH NO REPORTED EMERGENCY REPORTED, FOUND #1 ENG INBD NACELLE ACCESS DOOR 436AR MISSING UPON ROUTINE WALK SDR HNAA2024091700827Yoke · damagedRH PYLON YOKE FWD AND AFT FASTENER HOLES REQUIRE REAMING. REPAIRED IAW EO1-54-24-0497SDR IXXA2024080702Attach Angle · crackedNUMBER 1 ENGINE AFT STRUT I/B AFT HYDRAULIC DOOR BULB SEAL RETAINER UPPER ATTACH ANGLE IS CRACKEDSDR CALA2024080802179Access Panel · damagedREF AMES NON ROUTINE 173487-0400-0033.GENERATING ITEM:19-5400- 1-2009.#1 PYLON UPPER ACCESS 432AL, O/B UPPER SKIN CHAFED DUE TO HYD LINE BLOCK CLAMP WORKING FWD & AFT, TAG 10145,WORK WITH N/R 0400-0032.SDR UIEA2024072600754Fairing · cracked#4 ENG NOSE COWL LIP FAIRING AT INNER SIDE 12 O`CLOCK EXTERIOR SURFACE FOUND CRACK(<P>LIP SKIN CRACK AREA REPAIRED AS PER SRM 54-15-01-2R-20 REPAIR 20 FIG 201. NO FURTHER DEFECTS NOTED</P>)SDR IPXA2024091406896Skin · dented(STR) #2 ENG AIR INTAKE INSIDE AREA 6 O'CLOCK POS SURFACE SKIN HAS A DEEP DENT AS MARKED. 74-004 ATA CODE 71. ACCOMPLISHED EO-91273-REQ1 AND EA 011-5510-01-B0266 I/R. REVIEWED.SDR VNAA202508200026Door · abnormalPREVIOUS REPAIR WHITOUT TRACKING FOR PSA ON LOWER FAN COWL DOOR AT LH ENGINE BTWN 5 AND 6 O´CLOCK POSITION. PREVIOUS REPAIR WHITOUT TRACKING FOR PSA ON LOWER FAN COWL DOOR AT LH ENGINE BTWN 5 AND 6 O´CLOCK POSITION WAS REMOVED AND WAS REPAIRED PER REO 690-54SDR VNAA20250820005Door · dentedDENTS ON LOWER FAN COWL DOOR BTWN 4 TO 6´OCLOCK POSITION (5 EAS) AT LH ENGINE. DENTS ON LOWER FAN COWL DOOR BTWN 4 TO 6´OCLOCK POSITION (5 EAS) AT LH ENGINE WERE REPAIRED PER REO 690-54-14-774. REV-.SDR SWAA2024082922314Panel · cracked#1 ENGINE INBD FAN COWL DEFLECTOR WEB PANEL CRACKED JUST INSIDE OF OIL SERVE DOOR (MARKED)<[01] REMOVED AND REPLACED #1 ENG INBD FAN COWL PER AMM 71-11-02<BR>REF TTG8Q00S5GN8 FOR WORK ACCOMPLISHED.;[02] C/W INSPECTIONSDR SWAA2024082720185Inlet · corroded#2 ENGINE INLET COWL LIPSKIN WITH SURFACE CORROSION THROUGHOUT.<[01] #2 ENGINE INLET COWL WAS REPLACED ON BARCODE TTG8Q00UZ8YG;[02] FINAL INSPECTION; VERIFIED STEP #1.SDR SWAA2024082320509Fairing · cracked#1 ENGINE PYLON AFT FAIRING TRAILING EDGE WEDGE CRACKED. REFER TO EA M-23-154-01884-TLD; TTG8Q00TR5AV.<[01] LOCATED AND DRILLED UP NEW TRAILING EDGE WEDGE IAW SRM 51-40-02.;[02] VERIFIED LOCATED AND DRILLED UP NEW TRAILING EDGE WEDGE IAW SRM 51-40-02.;[03] COUSDR CALA2024080100345Door · missingPDA 1 #1 ENG NACELLE STRUT PRESSURE RELIEF DOOR MISSING. PICTURE UPDATE TOMC NOTIFIED. NO VISUAL DAMAGE.SDR UIEA2024072400737Fairing · damaged#2 PYLON UPPER CAVITY FWD L/E FAIRING SEVERAL SCREW HOLE FOUND ELONGATED(<P>#2 PYLON UPPER CAVITY L/E FAIRING FABRICATION AND REPLACEMENT IAW RI-57-31-17019 REV A. NO FURTHER DEFECTS NOTED.</P>)SDR SWAA2024073019852Strut · crackedWORKING MT 7256-I-14342-NG FOUND CRACK ATSTRUT 15 LOCATION C-1 MEASURING .750<[01] OK TO CONTINUE PER EA 7256-I-14342 AND TSR 2024005238
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