# Service difficulty reports: JASC 5730

A list on [JASC 5730](https://openairdocs.org/jasc/5730.md).

Reports filed under 5730 · Wing, Plate/Skin, newest first.

Page 1 of 545 · 27,219 reports

- [SDR ERKR2026102200890](https://openairdocs.org/sdr/ERKR2026102200890.md): Access Panel · corroded · Oct 22, 2026 · N677NK · Airbus A321231
  > FUEL TANK ACCESS PANEL 540HB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES
- [SDR ERKR2026102200889](https://openairdocs.org/sdr/ERKR2026102200889.md): Access Panel · corroded · Oct 22, 2026 · N677NK · Airbus A321231
  > FUEL TANK ACCESS PANEL 540NB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES.
- [SDR 2026FA0000888](https://openairdocs.org/sdr/2026FA0000888.md): Access Panel · corroded · Oct 22, 2026 · N677NK · Airbus A321231
  > FUEL TANK ACCESS PANEL 540QB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES
- [SDR ERKR2026102200887](https://openairdocs.org/sdr/ERKR2026102200887.md): Access Panel · corroded · Oct 22, 2026 · N667NK · Airbus A321231
  > FUEL TANK ACCESS PANEL 540KB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES.
- [SDR ERKR2026FA0000886](https://openairdocs.org/sdr/ERKR2026FA0000886.md): Access Panel · corroded · Oct 22, 2026 · N677NK · Airbus A321231
  > FUEL TANK ACCESS PANEL 540LB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES/
- [SDR ERKR2026102200885](https://openairdocs.org/sdr/ERKR2026102200885.md): Access Panel · corroded · Oct 22, 2026 · N677NK · Airbus A321231
  > PANEL RACK FUEL TANK ACCESS PANEL 540JB HAS EVIDENCE OF CORROSION ON THE FASTENER HOLES.
- [SDR FDEA202610201614](https://openairdocs.org/sdr/FDEA202610201614.md): Doubler · cracked · Oct 20, 2026 · N618FE · Doug MD11F
  > LEFT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 764 FOUND CRACKED ABOUT 0.2 INCH.
- [SDR FDEA202610201613](https://openairdocs.org/sdr/FDEA202610201613.md): Doubler · cracked · Oct 20, 2026 · N618FE · Doug MD11F
  > RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 746 FOUND CRACKED ABOUT 0.2 INCH.
- [SDR FDEA202610201612](https://openairdocs.org/sdr/FDEA202610201612.md): Doubler · cracked · Oct 20, 2026 · N618FE · Doug MD11F
  > RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 740 FOUND CRACKED ABOUT 0.2 INCH.
- [SDR FDEA202610201611](https://openairdocs.org/sdr/FDEA202610201611.md): Doubler · cracked · Oct 20, 2026 · N618FE · Doug MD11F
  > RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 728 FOUND CRACKED ABOUT 0.2 INCH.
- [SDR FDEA202610201610](https://openairdocs.org/sdr/FDEA202610201610.md): Skin · cracked · Oct 20, 2026 · N618FE · Doug MD11F
  > RIGHT WING, NR 16 SLAT TRACK CUTOUT AT WS XOS 1005, FOUND CRACKED ABOUT 0.5".
- [SDR R61A2026101800305](https://openairdocs.org/sdr/R61A2026101800305.md): Skin · cracked · Oct 18, 2026 · N979RP · Emb ERJ170100SE
  > FOUND CRACK ON RT WING LOWER SKIN, INBOARD OF RIB 17 AND AFT OF SPAR 1. PERFORMED PERMANENT REPAIR AT RT WING LOWER SKIN RIB 17 IAW ETD2026-170-017594, REV A.
- [SDR CALA2026102120497](https://openairdocs.org/sdr/CALA2026102120497.md): Skin · cracked · Oct 17, 2026 · N57111 · Boeing 757224
  > RT WING SKIN UNDER ACCESS PANEL 643BB CRACKED AT HOLE 5. CRACK LOCATION IS AT THE 6 AND 12 0'CLOCK LOCATION. (FWD AND AFT)
- [SDR FXGA202610140001](https://openairdocs.org/sdr/FXGA202610140001.md): Skin · cracked · Oct 14, 2026 · N408RE · Textrn 408
  > FOUND 2 CRACKS ON LT WING UPPER SKIN. 1ST CRACK 2.3" LONG BETWEEN RIBS AT LBL 142.3 & 157.95, APPROXIMATELY 17.5 INCHES FORWARD OF WING TRAILING EDGE. 2ND CRACK 4.5" LONG BETWEEN RIBS AT LBL 157.95 & 173.6, APPROXIMATELY 14.25 INCHES FORWARD OF WING TRAILING E
- [SDR JR2R20261012532](https://openairdocs.org/sdr/JR2R20261012532.md): Skin · chafed · Oct 12, 2026 · N88359 · Emb ERJ170200LR
  > RH WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIRED
- [SDR JR2R20261012537](https://openairdocs.org/sdr/JR2R20261012537.md): Skin · chafed · Oct 12, 2026 · N88359 · Emb ERJ170200LR
  > LEFT WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIRED.
- [SDR YENA2026101500971](https://openairdocs.org/sdr/YENA2026101500971.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450562. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 7 ( CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00043) REF AEROMAN WO# 2026-228/1. NR# 2026-450562. ACCOMPLI
- [SDR YENA2026101500970](https://openairdocs.org/sdr/YENA2026101500970.md): Skin · damaged · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N558JB - SRM REPAIR SURVEY, DEFECT 4400 62-29919; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00047) REF AEROMAN WO 2026-228/1 NR # 2026-450636 COMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER
- [SDR YENA2026101500969](https://openairdocs.org/sdr/YENA2026101500969.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00049) REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SK
- [SDR YENA2026101500968](https://openairdocs.org/sdr/YENA2026101500968.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00050) REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWE
- [SDR YENA2026101500967](https://openairdocs.org/sdr/YENA2026101500967.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00051) REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH
- [SDR YENA2026101500966](https://openairdocs.org/sdr/YENA2026101500966.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450569. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 13 PLUS 3 INCHES. (CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00052) REF AEROMAN WO# 2026-228/1. NR# 2026-45
- [SDR YENA2026101500965](https://openairdocs.org/sdr/YENA2026101500965.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00053) REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKI
- [SDR YENA2026101500964](https://openairdocs.org/sdr/YENA2026101500964.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450551. CORROSION ON LH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 PLUS 16 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00054) REF AEROMAN WO# 2026-228/1. NR# 2026-450551. ACCOMPLISH
- [SDR YENA2026101500962](https://openairdocs.org/sdr/YENA2026101500962.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROMAN E
- [SDR YENA2026101500961](https://openairdocs.org/sdr/YENA2026101500961.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORD
- [SDR YENA2026101500960](https://openairdocs.org/sdr/YENA2026101500960.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROM
- [SDR YENA2026101500959](https://openairdocs.org/sdr/YENA2026101500959.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TE OH LOWER SURFACE RIB 9-18 IN ACCORDAN
- [SDR YENA2026101500958](https://openairdocs.org/sdr/YENA2026101500958.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, EA A26-876-01 WING / LH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 9-18 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500954](https://openairdocs.org/sdr/YENA2026101500954.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, EA 26-872-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 13 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500951](https://openairdocs.org/sdr/YENA2026101500951.md): Skin · corroded · Oct 11, 2026 · N558JB · Airbus A320232
  > DURING HEAVY MAINTENANCE, EA 26-873-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 7 AND 13 / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR FDEA202610081495](https://openairdocs.org/sdr/FDEA202610081495.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F
  > RIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED RIB DOUBLER AT STATION XOS 667 REMOVED AND INSTALLED WITH FABRICATED RIB DOUBLER AS PER MD-11 SRM 51-31-01-0G.RIB DOUBLER FABRICATE
- [SDR FDEA202610081494](https://openairdocs.org/sdr/FDEA202610081494.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F
  > LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MAJ
- [SDR FDEA202610081493](https://openairdocs.org/sdr/FDEA202610081493.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F
  > LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2". LEFT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 682 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS MA
- [SDR FDEA202610081492](https://openairdocs.org/sdr/FDEA202610081492.md): Doubler · cracked · Oct 8, 2026 · N610FE · Doug MD11F
  > RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2". RIGHT WING FIXED LEADING EDGE CRACKED BEADED DOUBLER AT STATION XOS 705 CARRIED OUT REPAIR AS PER MD-11 SRM 57-40-02-2R REPAIR 15 FIGURE 203. REPAIR CLASSIFIED AS
- [SDR COEA2026101212767](https://openairdocs.org/sdr/COEA2026101212767.md): Skin · cracked · Oct 7, 2026 · N767FX · Textrn 408
  > DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPEN
- [SDR COEA2026101211767](https://openairdocs.org/sdr/COEA2026101211767.md): Skin · cracked · Oct 7, 2026 · N767FX · Textrn 408
  > DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPEN
- [SDR UIEA2026100600955](https://openairdocs.org/sdr/UIEA2026100600955.md): Skin · cracked · Oct 7, 2026 · N486MC · Boeing 74745EF
  > DURING LFEC INSPECTION AT LH WING FRONT SPAR UPPER SKIN BETWEEN WS621-WS637, FOUND 02 EA FASTENERS WITH CRACKED INDICATIONS.(<P>REFER TO EN 3800-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2026100600956](https://openairdocs.org/sdr/UIEA2026100600956.md): Skin · cracked · Oct 7, 2026 · N486MC · Boeing 74745EF
  > DURING LFEC INSPECTION AT RH WING FRONT SPAR LOWER SKIN BETWEEN WS540-WS560 FOUND 01 EA FASTENER WITH CRACK.(<P>REFER TO EN#3799-26 REV 0 FOR WORK PERFORMED. NO FURTHER DEFECTS NOTED.</P>)
- [SDR CALA2026100820218](https://openairdocs.org/sdr/CALA2026100820218.md): Access Panel · damaged · Oct 7, 2026 · N848UA · Airbus A319131
  > DURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PERFORMED TO FUEL ACCESS PANEL 540KB IAW PART 1 OF ECRA 5721-01445. ACCOMPLISH PERMINATE REPAIR AT LT WING BOTTOM FUEL ACCESS PANEL 540KB HO
- [SDR CALA2026101320350](https://openairdocs.org/sdr/CALA2026101320350.md): Access Panel · cracked · Oct 6, 2026 · N17126 · Boeing 757224
  > RIGHT WING INTERSPAR 2 EACH CRACKS NOTED WHILE ACCOMPLISHING EA5720-03647 (A) AT HOLES NR 6 & 27 AT PANEL ACCESS 643BB. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5720-03684 AND ST ENGINEERING EA757-5720-13-A4616 WITH NO DEVIATIONS. DIP REQUIR ED AS FOLL
- [SDR JR2R20261006891](https://openairdocs.org/sdr/JR2R20261006891.md): Panel · chafed · Oct 6, 2026 · N85320 · Emb ERJ170200LL
  > R/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM.
- [SDR JR2R20261006890](https://openairdocs.org/sdr/JR2R20261006890.md): Panel · chafed · Oct 6, 2026 · N85320 · Emb ERJ170200LL
  > L/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM.
- [SDR DALA2026100605529](https://openairdocs.org/sdr/DALA2026100605529.md): Vane · dented · Oct 4, 2026 · N978AT · Boeing 717200
  > DENT ON LOWER SURFACE OF RT FWD MOVABLE VANE WAS FOUND AT RT WING. WD MOVABLE VANE AT RT WING WAS REPAIRED IAW SRM 57-53-01-2R, PROCEDURE 1, REPAIR 1. AND SRM 51-70-02-0G. (1848375) AIRCRAFT WAS GROUNDED.
- [SDR SWAA2026100721957](https://openairdocs.org/sdr/SWAA2026100721957.md): Winglet · delaminated · Oct 3, 2026 · N8793Q · Boeing 7378
  > UPPER SPLIT SCIMITAR WINGLET LEADING EDGE DELAMINATED. IAW SRM 57-30-01-2R-6, PROCEDURES BY COMPLETING REPAIR 6, TYPE 1. TEMPORARY REPAIR FOR RT WINGLET EROSION TAPE. ENGINEERING CONCURS WITH SRM.
- [SDR R61A2026100100290](https://openairdocs.org/sdr/R61A2026100100290.md): Skin · cracked · Oct 1, 2026 · N208JQ · Emb ERJ170200LR
  > FOUND CRACK ON RT WING MAIN BOX, LOWER SKIN, AT SPAR II RIB 4A JUNCTION. REPAIRED PER ETD 2026-170-016493.
- [SDR COEA2026100109708](https://openairdocs.org/sdr/COEA2026100109708.md): Skin · cracked · Sep 30, 2026 · N708FX · Textrn 408
  > EVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPEN
- [SDR DALA2026100105450](https://openairdocs.org/sdr/DALA2026100105450.md): Skin · gouged · Sep 30, 2026 · N991AT · Boeing 717200
  > GOUGES ON FIXED LEADING EDGE BTW XOS=390 TO XOS=410 AT LT WING, COMPLIED WITH ER/A 637059-14. (1841449) (AIRCRAFT GROUNDED).
- [SDR IPXA2026100181758](https://openairdocs.org/sdr/IPXA2026100181758.md): Access Panel · cracked · Sep 29, 2026 · N158UP · Airbus A300F4622R
  > LEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW A300-600 SRM 51-40-21-001. INSTALLED INTERNAL DOUBLER ON LH WING BELOW KRUGER FLAP ACCESS PANEL 513AB IAW
- [SDR COEA2026100108708](https://openairdocs.org/sdr/COEA2026100108708.md): Panel · dented · Sep 29, 2026 · N708FX · Textrn 408
  > DENT UNDER LT SPONSON PANEL. OPEN

Next page: https://openairdocs.org/jasc/5730/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 = '5730'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5730/reports

---
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