# Service difficulty reports: JASC 5412

A list on [JASC 5412](https://openairdocs.org/jasc/5412.md).

Reports filed under 5412 · Nacelle/Pylon, Bulkhead/Firewall, newest first.

Page 1 of 22 · 1,086 reports

- [SDR IPXA2026090324513](https://openairdocs.org/sdr/IPXA2026090324513.md): Bulkhead · cracked · Aug 26, 2026 · N305UP · Boeing 76734AF
  > CRACKED 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 IPXA2026090305799](https://openairdocs.org/sdr/IPXA2026090305799.md): Firewall · cracked · Aug 25, 2026 · N441UP · Boeing 75724APF
  > NR 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 B757-2
- [SDR FDEA202608051085](https://openairdocs.org/sdr/FDEA202608051085.md): Bulkhead · corroded · Aug 5, 2026 · N613FE · Doug MD11F
  > NR 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 FDEA202607130918](https://openairdocs.org/sdr/FDEA202607130918.md): Bulkhead · misaligned · Jul 13, 2026 · N603FE · Doug MD11F
  > RIGHT 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-B
- [SDR FDEA202606030666](https://openairdocs.org/sdr/FDEA202606030666.md): Bulkhead · worn · Jun 3, 2026 · N617FE · Doug MD11F
  > #3 AFT PYLON BULKHEAD WORN REMOVED AND REPLACED AFT BULKHEAD.
- [SDR IPXA2026060875059](https://openairdocs.org/sdr/IPXA2026060875059.md): Bulkhead · cracked · Jun 2, 2026 · N161UP · Airbus A300F4622R
  > NR 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 IPXA2026060253330](https://openairdocs.org/sdr/IPXA2026060253330.md): Bulkhead · gouged · May 12, 2026 · N423UP · Boeing 75724APF
  > MAJOR 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 IPXA2026060903170](https://openairdocs.org/sdr/IPXA2026060903170.md): Bulkhead · cracked · May 3, 2026 · N156UP · Airbus A300F4622R
  > NR 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 SWAA2026042992805](https://openairdocs.org/sdr/SWAA2026042992805.md): Heat Shield · cracked · Apr 25, 2026 · N8718Q · Boeing 7378
  > CRACK 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 SE
- [SDR IPXA2026041035962](https://openairdocs.org/sdr/IPXA2026041035962.md): Bulkhead · cracked · Apr 4, 2026 · N313UP · Boeing 76734AF
  > CRACKED 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 IPXA2025101198719](https://openairdocs.org/sdr/IPXA2025101198719.md): Web · cracked · Sep 23, 2025 · N173UP · Airbus A300F4622R
  > ENG 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 AFT
- [SDR IXXA20250806001](https://openairdocs.org/sdr/IXXA20250806001.md): Bulkhead · cracked · Aug 6, 2025 · N241AZ · Boeing 767323
  > RIGHT PYLON FAIRING 447DB INTERNAL BULKHEAD IS CRACKED.
- [SDR KCSA202506261102](https://openairdocs.org/sdr/KCSA202506261102.md): Bulkhead Web · cracked · Jun 26, 2025 · N709CK · Boeing 7474B5
  > #1 PYLON STA 298.9 BULKHEAD WEB CRACKED WHERE HYDRAULIC LINE GOES THROUGH
- [SDR UIEA2025042400568](https://openairdocs.org/sdr/UIEA2025042400568.md): Strut · gouged · May 16, 2025 · N640GT · Boeing 7673S1
  > STRUT #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 FURTH
- [SDR IPXA2025041037198](https://openairdocs.org/sdr/IPXA2025041037198.md): Firewall · cracked · Mar 13, 2025 · N473UP · Boeing 75724APF
  > NR 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 ENGINE
- [SDR DALA2025022301388](https://openairdocs.org/sdr/DALA2025022301388.md): Heat Shield · damaged · Feb 23, 2025 · N355NW · Airbus A320212
  > SHIP 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 IXXA20250122010](https://openairdocs.org/sdr/IXXA20250122010.md): Bulkhead · cracked · Jan 19, 2025 · N571AZ · Boeing 767323
  > NO.1 PYLON, AFT FAIRING 437DB, INTERIOR FRAME IS CRACKED.
- [SDR JR2R20240928276](https://openairdocs.org/sdr/JR2R20240928276.md): Heat Shield · damaged · Sep 28, 2024 · N86311 · Emb ERJ170200LR
  > LH AFT PYLON FAIRING HEAT SHEILD HAS 1EA ELONGATED SCREW HOLE. REPAIR
- [SDR JR2R20240928277](https://openairdocs.org/sdr/JR2R20240928277.md): Heat Shield · damaged · Sep 28, 2024 · N86311 · Emb ERJ170200LR
  > LH AFT PYLON FAIRING HEAT SHEILD HAS 1EA ELONGATED SCREW HOLE. REPAIR
- [SDR EE4Y2024091020872](https://openairdocs.org/sdr/EE4Y2024091020872.md): Bulkhead · cracked · Sep 10, 2024 · N331NV · Airbus A319111
  > DURING 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 COEA2024071222708](https://openairdocs.org/sdr/COEA2024071222708.md): Bulkhead · cracked · Jul 11, 2024 · N708FX · Textrn 408
  > WO 259393 NR 3 DISCREPANCY: R/H ENGINE ACCESSORY PANEL BULKHEAD CRACKED. REPLACED THE BULKHEAD IAW CESSNA 408 SMR SMP.
- [SDR CALA2024061901873](https://openairdocs.org/sdr/CALA2024061901873.md): Fitting · worn · Jun 14, 2024 · N651UA · Boeing 767322
  > DURING 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 T
- [SDR VNAA20250820008](https://openairdocs.org/sdr/VNAA20250820008.md): Shield · chafed · Jun 12, 2024 · N633NN · Bombdr CL6002D15
  > LH 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 N
- [SDR VNAA202407090007](https://openairdocs.org/sdr/VNAA202407090007.md): Fireshield · chafed · May 29, 2024 · N584NN · Cndair CL6002D24
  > IN 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 FIRESH
- [SDR VNAA202407090006](https://openairdocs.org/sdr/VNAA202407090006.md): Fireshield · chafed · May 29, 2024 · N584NN · Cndair CL6002D24
  > IN 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 HNAA2024070500503](https://openairdocs.org/sdr/HNAA2024070500503.md): Firewall · cracked · May 18, 2024 · N649PP · Emb EMB145LR
  > E037246 RH PYLON CENTER FIREWALL CRACKED. RAR RH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0326
- [SDR HNAA2024070500502](https://openairdocs.org/sdr/HNAA2024070500502.md): Firewall · cracked · May 18, 2024 · N649PP · Emb EMB145LR
  > E037244 LH PYLON CENTER FIREWALL CRACKED. RAR LH PYLON CENTER FIREWALL IAW ETD-2024-145-014089 AND EO1-54-24-0327
- [SDR VNAA20240723002](https://openairdocs.org/sdr/VNAA20240723002.md): Fireshield · damaged · May 14, 2024 · N585NN · Bombdr CL6002D15
  > RH 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 HNAA202405140384](https://openairdocs.org/sdr/HNAA202405140384.md): Firewall · cracked · Apr 23, 2024 · N653AE · Emb EMB145LR
  > E034081 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 E
- [SDR HNAA2024051400383](https://openairdocs.org/sdr/HNAA2024051400383.md): Firewall · cracked · Apr 23, 2024 · N653AE · Emb EMB145LR
  > E034080 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 IPXA2023101658163](https://openairdocs.org/sdr/IPXA2023101658163.md): Bulkhead · cracked · Oct 12, 2023 · N411UP · Boeing 75724APF
  > *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 313N3052
- [SDR IPXA2023102690583](https://openairdocs.org/sdr/IPXA2023102690583.md): Bulkhead · gouged · Sep 27, 2023 · N425UP · Boeing 75724APF
  > MAJOR 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 IPXA2023102664541](https://openairdocs.org/sdr/IPXA2023102664541.md): Bulkhead · gouged · Sep 25, 2023 · N425UP · Boeing 75724APF
  > MAJOR 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 DALA2023052604197](https://openairdocs.org/sdr/DALA2023052604197.md): Unknown · unknown · May 24, 2023 · N672DL · Boeing 757232
  > SHIP 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 ABXA20230515105](https://openairdocs.org/sdr/ABXA20230515105.md): Vapor Barrier · damaged · Apr 10, 2023 · N219CY · Boeing 767383
  > DURING 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 2023FA0000112](https://openairdocs.org/sdr/2023FA0000112.md): None · none · Mar 5, 2023 · N571AZ · Boeing 767332
  > FOUND MULTIPLE DENTS BETWEEN 5-7 O'CLOCK ON ENGINE #2 INLET COWL ACOUSTIC PANEL.
- [SDR UIEA2022061900613](https://openairdocs.org/sdr/UIEA2022061900613.md): Bolt · broken · Jun 19, 2022 · N1409A · Boeing 767306
  > BOLT 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 FDEA202206171449](https://openairdocs.org/sdr/FDEA202206171449.md): Frame · cracked · Jun 17, 2022 · N131FE · Boeing 767300
  > #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 4
- [SDR DALA2022050903223](https://openairdocs.org/sdr/DALA2022050903223.md): Doubler · damaged · May 6, 2022 · N671DN · Boeing 757232
  > SHIP 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 I
- [SDR UIEA2022030300187](https://openairdocs.org/sdr/UIEA2022030300187.md): Skin · corroded · Mar 3, 2022 · N718BA · Boeing 7474H6
  > PITTING 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 DALA2021090705254](https://openairdocs.org/sdr/DALA2021090705254.md): Shim · migrated · Sep 3, 2021 · N692DL · Boeing 757232
  > SHIP 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.S
- [SDR ASAA2021052535014](https://openairdocs.org/sdr/ASAA2021052535014.md): Bulkhead · cracked · May 25, 2021 · N277AK · Boeing 737990ER
  > #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 IPXA2021052669861](https://openairdocs.org/sdr/IPXA2021052669861.md): Bulkhead · cracked · May 19, 2021 · N135UP · Airbus A300F4622R
  > INSPECTION 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 14
- [SDR IPXA2021052469768](https://openairdocs.org/sdr/IPXA2021052469768.md): Bulkhead · cracked · May 19, 2021 · N135UP · Airbus A300F4622R
  > INSPECTION 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 14
- [SDR UATA202101073315](https://openairdocs.org/sdr/UATA202101073315.md): Firewall · cracked · Dec 13, 2020 · N1331C · Casa C212CC
  > NR 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 SI
- [SDR FDEA2020082091939](https://openairdocs.org/sdr/FDEA2020082091939.md): Bulkhead · cracked · Aug 19, 2020 · N796FD · Boeing 757222
  > #2 PYLON HYDRAULIC BAY,AFT OF BULKHEAD THE OTBD LWR FWD CORNER ATTACH CLIP IS CRACKED REMOVED AND REPLACED CLIP PER BOEING DWG #313N3052
- [SDR FDEA2020080751771](https://openairdocs.org/sdr/FDEA2020080751771.md): Bulkhead · cracked · Aug 5, 2020 · N744FD · Airbus A300B4622R
  > NO.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 IPXA2020080558669](https://openairdocs.org/sdr/IPXA2020080558669.md): Bulkhead Web · worn · Aug 5, 2020 · N125UP · Airbus A300F4622R
  > NR 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 COEA2020100605805](https://openairdocs.org/sdr/COEA2020100605805.md): Firewall · cracked · Jun 22, 2020 · N805HC · Aerosp ATR42500
  > HATS 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 COEA2020101307805](https://openairdocs.org/sdr/COEA2020101307805.md): Firewall · cracked · Jun 2, 2020 · N805HC · Aerosp ATR42500
  > HATS 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.

Next page: https://openairdocs.org/jasc/5412/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/jasc/5412/reports

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