JASC 5412
Service difficulty reports · 1,086
Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, 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 = '5412' 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 = '5412' 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 IPXA2026090324513Bulkhead · crackedCRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL 437DD, INNER AREA. REMOVED DAMAGE BULKHEAD IAW SRM 51-40-02-0G, REV. 96. INSTALLED NEW BULKHEAD IAW SRM 51-40-02-0G, REV 96 AND DWG 313T3360, SHT 15, REV B.SDR IPXA2026090305799Firewall · crackedNR 1 ENG OTBD T/R INTERNAL TOP METALLIC PLATE IS CRACKED. REMOVED INTERNAL TOP METALLIC PLATE DAMAGED AND REMOVED SEAL RETAINER (FOR ACCESS). #1 ENG O/B T/R. IAW B757-200PF SRM 51-40-02-0G-0. INSTALLED INTERNAL TOP METALLIC PLATE AND SEAL RETAINER. IAW B757-2SDR FDEA202608051085Bulkhead · corrodedNR 1 ENG PYLON AFT BULKHEAD LUG BORE HOLE FOUND WITH CORROSION AFTER SPHERICAL. BEARING REMOVED. CORROSION AT NR 1 ENG PYLON AFT BULKHEAD LUG BORE HOLE CARRIED OUT REPAIR IAW EA 1-5440-T0388257, PART 1. INSPECTION FINDINGS, THIS EA DEVIATES FROM EO 1-5440- SDR FDEA202607130918Bulkhead · misalignedRIGHT ENGINE #3 PYLON AFT BULKHEAD FOUND LUG BORE HOLE MISALIGN.YWN 418. RIGHT ENGINE #3 PYLON AFT BULKHEAD LUG BORE HOLE MISALIGN HOLE REWORKED AS PER EA #1-5440-T0387700 PART1.TITLE: NACELLES/PYLON - ATTACH /MOUNT/HINGE - NO 3 PYLON AFT BULKHEAD - MD11-BSDR FDEA202606030666Bulkhead · worn#3 AFT PYLON BULKHEAD WORN REMOVED AND REPLACED AFT BULKHEAD.SDR IPXA2026060875059Bulkhead · crackedNR 1 ENG O/B NOSE COWL AFT BULKHEAD HAS A CRACK. INSTALLED NEW WEB AND SPLICE IAW SRM 51-40-21 AND SRM 54-10-00 REPAIR NO. 14.SDR IPXA2026060253330Bulkhead · gougedMAJOR REPAIR, NR 2 PYLON AFT BULKHEAD LT SIDE REINFORCMENT FITTING IS GOUGED COMPLIED WITH EO-97567-REQ1 AND VT-MAE EA 757-5453-27-A4500, REV.-SDR IPXA2026060903170Bulkhead · crackedNR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION WITH CRACK APPROX 2 INCHES LONG. INSTALLED NEW WEB IN ZONE 400 NR 1 ENG, INLET INTAKE, AFT BULKHEAD AT 3 O'CLOCK POSITION. IAW SRM 54-10-00 REPAIR NR 14, PAGE 201, AND SRM 51-40-21-001.SDR SWAA2026042992805Heat Shield · crackedCRACK MEASURING 14.5 INCHES LONG ON NR 2 AFT LOWER PYLON HEAT SHEILD LOCATED 28 INCHES FWD OF AFT EDGE. LT OF CRACKED STOPS .312 AWAY FROM NEAREST FASTENER; RIGHT SIDE OF CRACK STOPS .33 AWAY FROM NEAREST FASTENER. COMPLIED WITH EA 26-154-01126 AND APPLIED SESDR IPXA2026041035962Bulkhead · crackedCRACKED BULKHEAD, NR 1 PYLON AFT FAIRING PANEL NR.437DB INNER NEW AREA. INSTALL NEW BULKHEAD IAW SRM 51-40-02-0G, REV 94, AND DWG 313T3360, SHT 42, REV E.SDR IPXA2025101198719Web · crackedENG NR 2 NOSE COWL BULKHEAD AREA LH SIDE, HAS 2 CRACKS (9 O'CLOCK POSITION). REMOVE PART ENG #2 NOSE COWL BULKHEAD AREA LH SIDE IAW SRM 51-40-21. INSTALLED PART ENG NR 2 NOSE COWL BULKHEAD AREA LT SIDE, IAW SRM 54-10-00 AND SRM 51-40-21. PART FABRICATED AFTSDR IXXA20250806001Bulkhead · crackedRIGHT PYLON FAIRING 447DB INTERNAL BULKHEAD IS CRACKED.SDR KCSA202506261102Bulkhead Web · cracked#1 PYLON STA 298.9 BULKHEAD WEB CRACKED WHERE HYDRAULIC LINE GOES THROUGHSDR UIEA2025042400568Strut · gougedSTRUT #2 AFT BUKLHEAD, SIDE LINK WITH GOUGES.(<P>SIDE LINK WITH GOUGES, REWORKED AREA AND PROTECTIVE TREATMENT WAS PERFORMED IAW TRE 6754213, LINK INSTALLATION WAS PERFORMED IAW 8017-0292_A-54-404-00-02_POWER PLANT STRUT - #2, TASK CARD WAS PERFORMED. NO FURTHSDR IPXA2025041037198Firewall · crackedNR 1 ENG LP COMPRESSOR INNER CASE AFT BULKHEAD FIREWALL WITH CRACK BTW 8-9 O'CLOCK. INSTALLED ENGINE#1 LH CENTER COMPRESSOR FAIRING OF LP COMPRESSOR INNER CASE. I.A.W AMM 72-03-01-424-006-R00. ACCOMPLISHED STEP 15 OF EO 535-7200-14571. INSTALLATION OF ENGINESDR DALA2025022301388Heat Shield · damagedSHIP 3255 DISC: REPAIR INSTALLED PER E/RA 624412-14 REV. ORIG. PRI REV. "0", "1" DOES NOT MATCH FINAL ERA 624412-14 REV ORIG. C/A: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 006-0001:2100-2096/007 00010 ENSURED ALL E/SDR IXXA20250122010Bulkhead · crackedNO.1 PYLON, AFT FAIRING 437DB, INTERIOR FRAME IS CRACKED.SDR JR2R20240928276Heat Shield · damagedLH AFT PYLON FAIRING HEAT SHEILD HAS 1EA ELONGATED SCREW HOLE. REPAIRSDR JR2R20240928277Heat Shield · damagedLH AFT PYLON FAIRING HEAT SHEILD HAS 1EA ELONGATED SCREW HOLE. REPAIRSDR EE4Y2024091020872Bulkhead · crackedDURING ACCOMPLISHMENT OF THE ALLEGIANT WORK 711000-C1-1-001, ENGINE # 1 AIR INTAKE COWL AFT BULKHEAD I/B SECTION AT 9 O´CLOCK WEB CRACKED AROUND ANCHOR NUT WAS FOUND. REPAIRED ENGINE # 1 AIR INTAKE COWL BULKHEAD I/B SECTION AT 9 O´CLOCK IAW GOODRICH CMM 71-11-SDR COEA2024071222708Bulkhead · crackedWO 259393 NR 3 DISCREPANCY: R/H ENGINE ACCESSORY PANEL BULKHEAD CRACKED. REPLACED THE BULKHEAD IAW CESSNA 408 SMR SMP.SDR CALA2024061901873Fitting · wornDURING C-CHECK, AMES MAINT DISCOVER ED 2 FASTENER HOLES ON NR 2 PYLON BULKHEAD FITTING WAS WORN & ELONGATED. BOTH INBD & OTBD FASTENER HOLES MEASURED 0.3125" DIA WITH DISTANCE BETWEEN HOLES MEASURING NG 0.250". ATTACHING ANGLE WAS CRACKED & REPLACED. AS TSDR VNAA20250820008Shield · chafedLH ENG FIRE SHIELD WITHIN 2140.41 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. ENGINEERING COMMENTS: LH ENG FIRE SHIELD REPAIR AS PER SRM TASK 54-23-00-201-005-A01. IF NSDR VNAA202407090007Fireshield · chafedIN REF. TRFKE00BY829:670-54-23-1164. 1500FH PERM REPAIR - SPEED TAPE APPLIED - CHAFE DAMAGE TO FWD CORE COWL FIRESHIELD PERMANENT REPAIR CORE COWL DUE TO DENT/CHAFE DAMAGE, SEE W.O. OR L.B. AND 670-54-23-1164 FOR DETAILS. CHAFE DAMAGE TO FWD CORE COWL FIRESHSDR VNAA202407090006Fireshield · chafedIN REF. TRFKE00BMX8D:EA A1-690-54-00008.1265FH PERM REPAIR - RH CORE COWL FIRE SHIELD CHAFE DAMAGE WITHIN 1265 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART. RH CORE COWL SDR HNAA2024070500503Firewall · crackedE037246 RH PYLON CENTER FIREWALL CRACKED. RAR RH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0326SDR HNAA2024070500502Firewall · crackedE037244 LH PYLON CENTER FIREWALL CRACKED. RAR LH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0327SDR VNAA20240723002Fireshield · damagedRH ENGINE LWR FWD CORE COWL FIRE SHIELD WITHIN 2,566.78 FLIGHT HOURS FROM IR (BEFORE 19,384.43FH) REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. FIRESHIELD LWR FWD CORE COWL RH ENGINE WAS REPAIRED PER REO 690-54-23-384 REV - -SDR HNAA202405140384Firewall · crackedE034081 RH ENGINE PYLON FIREWALL CRACKED AT TWO LOCATIONS. REMOVED DAMAGED RH ENGINE PYLON FIREWALL, PERFORMED CUTOUT OF NEW FIREWALL, FABRICATED SPLICE, AND INSTALLED NEW FIREWALL SECTIONS AND SPLICE IAW ETD2024-145-012367 REV "A", EMB 145 SRM 51-40-02 AND ESDR HNAA2024051400383Firewall · crackedE034080 LH ENGINE PYLON FIREWALL IS CRACKED 2 EACH. ERFORMED CUTOUT OF DAMAGED AREA ON L/H ENGINE PYLON FIREWALL IAW ETD2024-145-012367 REV "A". DRILLIED NEW L/H ENGINE PYLON FIREWALL, FABRICATED SPLICE AND INSTALLED REPAIR IAW ETD2024-145-012367 REV "A" AND SDR IPXA2023101658163Bulkhead · cracked*SUPPLEMENTAL SDR* R\H PYLON, HYD BAY, AFT SIDE OF PYLON BULKHEAD, UPPER SUPPORT ANGLE, I\B SIDE, HAS AN 1 1\2 INCH CRACK. VERIFIED HEAT TREATMENT PER NDTM, PART 4, 51-00-10. COMPLETED INSTALLATION PER DRAWING 313N3052SDR IPXA2023102690583Bulkhead · gougedMAJOR REPAIR, #2 ENG PYLON AFT I/B LWR CORNER REINFORCEMENT PANEL HAS A CRACK. VERIFIED ACCOMPLISHMENT PER UPS EO-88456-REQ 1 AND VTMAE EA 757-5453-27-A3388 REV-,WITHOUT ANY DEVIATION.SDR IPXA2023102664541Bulkhead · gougedMAJOR REPAIR, LOWER O/B EDGE OF AFT BULKHEAD ON #1 PYLON IS GOUGED DOT 06951-101. JOB WAS ACCOMPLISHED PER UPS EO-88455-REQ1 AND VT MAE EA # 757-5453-27-A3387 REV -, WITHOUT ANY DEVIATION.SDR DALA2023052604197Unknown · unknownSHIP 672 WEAR ON BULKHEAD STA 201.02 OF THE LH PYLON IN REF. NRC # 00354. CORRECTIVE ACTION: SUMMARY OF NRC 00746: WEAR ON BULKHEAD STA 201.02 OF THE LH PYLON WAS REPAIRED PER ER/A 607985-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2781481)SDR ABXA20230515105Vapor Barrier · damagedDURING C21 MAINTENANCE CHECK AT HAECO AMERICAS, MAINTENANCE FOUND NO. 1 PYLON OUTBOARD VAPOR BARRIER WEB APPROXIMATELY AT NAC STA. 230 DAMAGED AT THE D4044J MOUNT (CUTOUT). THE D4044J MOUNT WAS PULLED-OUT FROM THE WEB. THE SUBJECT BARRIER IS SUBJECT TO SB-767-SDR 2023FA0000112None · noneFOUND MULTIPLE DENTS BETWEEN 5-7 O'CLOCK ON ENGINE #2 INLET COWL ACOUSTIC PANEL.SDR UIEA2022061900613Bolt · brokenBOLT IS BROKEN FOR CLAMP LOCATED ON #2 ENG R/H SIDE AFT OF HEAT EXCHANGER. INSTALLED BOLT AS PER B767-300 AMM 70-50-00. OPS CHECK GOOD</P>)SDR FDEA202206171449Frame · cracked#2 PYLON DOOR 447BR LOWER BULKHEAD CRACKED AT NAC STA 329.50 REPAIRED #2 PYLON MID-SPAR FRAME IAW B767 SRM 54-52-71-2R, REPAIR 4SDR DALA2022050903223Doubler · damagedSHIP 671 AWR WORN PREVIOUS REPAIR ON OUTBD WEB AT NCA STA 100 APRROX AT LH PYLON IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00300: PREVIOUS REPAIR DOUBLER ON OUTBD WEB AT NCA STA 100 APRROX AT LH PYLON WAS REPLACED PER ER/A 567740-14 REV ORIGINAL SECTION ISDR UIEA2022030300187Skin · corrodedPITTING CORROSION - SKIN, NO. 1 PYLON AFT STRUT FAIRING FWD BULKHEAD(<P>BLENDED OUT THE DAMAGED AREA IAW SRM 51-10-02 REV. 50. PERFORM NDT INSPECTION, REFER TO JOB CARD ATTACHING SHEET NO. 0305381. MEASURED REWORK AREA DEPTH = 0.001" LENGTH = 1", WIDTH = 0.8" SDR DALA2021090705254Shim · migratedSHIP 692 MIGRATED SHIM BTW AFT BULKHEAD AND AFT ENGINE MOUNT (OUTBD SIDE) OF THE ENG. #2, NAC.STA. 198. (GET ACCESS THRU ACCESS PANEL 444AR). CORRECTIVE ACTION: SUMMARY OF NRC 00164: SHIM BTW AFT BULKHEAD AND AFT ENGINE MOUNT (OUTBD SIDE) OF THE ENG. #2, NAC.SSDR ASAA2021052535014Bulkhead · cracked#2 PYLON AFT STRUT FAIRING AFT BULKHEAD CRACKED. GROUNDED - YES. REMOVED & REPLACED #2 PYLON AFT STRUT FAIRING IAW B737-900 SRM 51-40-02-00-0.SDR IPXA2021052669861Bulkhead · crackedINSPECTION TYPE:SEG31 ENG NOSE COWL AFT BULKHEAD LH SIDE 9 O'CLOCK POSITION HAS CRACK AT THE ELBOW CUTOUTINSTALLED REPAIRED PART# 221-4050-523 S/N 0746001 ON #1 ENG. NOSE COWLK IAW P/W SRM 54-10-00 REPAIR 14SDR IPXA2021052469768Bulkhead · crackedINSPECTION TYPE:SEG#2 ENGINE NOSE COWL AFT BULKHEAD LH SIDE AT 9 O'CLOCK POSITION HAS A CRACK AT THE DRAIN ELBOW ON AFT BULKHEAD WEB.REPAIRED NOSE COWL AFT BULKHEAD WEB PER PW SRM 54-10-00 REPAIR 14SDR UATA202101073315Firewall · crackedNR 1 AND 2 ENGINE AFT SIDE OF FIREWALL LOWER DOUBLERS FOUND CRACKED NEAR OUTER EDGE OF BOTH LEFT AND RIGHT LOWER MOUNT FITTINGS. REPAIRED BOTH LT AND RT CRACKED DOUBLERS ON BOTH ENGINE FIREWALLS BY INSERTION OF NEW DOUBLER SECTIONS OF SIMILAR THICKNESS AND SISDR FDEA2020082091939Bulkhead · cracked#2 PYLON HYDRAULIC BAY,AFT OF BULKHEAD THE OTBD LWR FWD CORNER ATTACH CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BOEING DWG #313N3052SDR FDEA2020080751771Bulkhead · crackedNO.1 ENG INLET, O/B SIDE, AFT BULKHEAD CRACKED AROUND SENSE LINE ELBOW. REPAIRED #1 ENG INLET, O/B SIDE, AFT BULKHEAD AT SENSE LINE PER P&W SRM 54-10-00 FIG. 201.SDR IPXA2020080558669Bulkhead Web · wornNR 1 ENGINE INLET COWL, OTBD SESE LINE BULKHEAD FITTING HOLE IN WEB WAS WORN, AND ENLARGED. REMOVED & REPLACED THE WEB IAW SRM 54-10-00, FIG 201.SDR COEA2020100605805Firewall · crackedHATS WO 176998 NR00502, EMPIRE WO 211916 HEAVY CHECK. HATS/MAJOR REPAIR: RIGHT ENGINE UPPER FIREWALL HAS A CRACK AT APPROXIMATELY AREA 3. CORRECTIVE ACTION: REPAIRED PER SRAS ES-3628/18, 13303 ISSUE B, DATED 8/25/2020.SDR COEA2020101307805Firewall · crackedHATS WO 176998 NR00522, WO 211916 HEAVY CHECK HATS/MAJOR REPAIR. LEFT ENGINE UPPER FIREWALL HAS CRACK AT APPROXIMATELY AREA 3. CORRECTIVE ACTION: REPAIRED PER SRAS ES_0120973_01 16585 ISSUE B, DATED 8/26/2020.
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