# JASC 5730: Wing, Plate/Skin

- Type: JASC system/component code (FAA)
- ATA chapter: 57 Wings
- Title in the code table: WING, PLATES/SKINS
- Service difficulty reports: 27,210
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=54
- Page: https://openairdocs.org/jasc/5730

## What it covers

For reports of the exterior covering of the wing including the access covers, tip tank fillets, or fairings. Includes the leading edge and trailing edge skin and wing mounted fuel compartment panels.

## Service difficulty reports (27,210, newest 50)

- [SDR FDEA202610201614](https://openairdocs.org/sdr/FDEA202610201614), Oct 20, 2026: Doug MD11F. DOUBLER. CRACKED. LEFT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 764 FOUND CRACKED ABOUT 0.2 INCH. (N618FE)
- [SDR FDEA202610201613](https://openairdocs.org/sdr/FDEA202610201613), Oct 20, 2026: Doug MD11F. DOUBLER. CRACKED. RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 746 FOUND CRACKED ABOUT 0.2 INCH. (N618FE)
- [SDR FDEA202610201612](https://openairdocs.org/sdr/FDEA202610201612), Oct 20, 2026: Doug MD11F. DOUBLER. CRACKED. RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 740 FOUND CRACKED ABOUT 0.2 INCH. (N618FE)
- [SDR FDEA202610201611](https://openairdocs.org/sdr/FDEA202610201611), Oct 20, 2026: Doug MD11F. DOUBLER. CRACKED. RIGHT WING, LEADING EDGE COMPARTMENT BEADED DOUBLER AT XOS 728 FOUND CRACKED ABOUT 0.2 INCH. (N618FE)
- [SDR FDEA202610201610](https://openairdocs.org/sdr/FDEA202610201610), Oct 20, 2026: Doug MD11F. SKIN. CRACKED. RIGHT WING, NR 16 SLAT TRACK CUTOUT AT WS XOS 1005, FOUND CRACKED ABOUT 0.5". (N618FE)
- [SDR R61A2026101800305](https://openairdocs.org/sdr/R61A2026101800305), Oct 18, 2026: Emb ERJ170100SE. SKIN. CRACKED. FOUND CRACK ON RT WING LOWER SKIN, INBOARD OF RIB 17 AND AFT OF SPAR 1. PERFORMED PERMANENT REPAIR AT RT WING LOWER SKIN (N979RP)
- [SDR CALA2026102120497](https://openairdocs.org/sdr/CALA2026102120497), Oct 17, 2026: Boeing 757224. SKIN. CRACKED. RT WING SKIN UNDER ACCESS PANEL 643BB CRACKED AT HOLE 5. CRACK LOCATION IS AT THE 6 AND 12 0'CLOCK LOCATION. (FWD AND AF (N57111)
- [SDR FXGA202610140001](https://openairdocs.org/sdr/FXGA202610140001), Oct 14, 2026: Textrn 408. SKIN. CRACKED. 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  (N408RE)
- [SDR JR2R20261012532](https://openairdocs.org/sdr/JR2R20261012532), Oct 12, 2026: Emb ERJ170200LR. SKIN. CHAFED. RH WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIRED (N88359)
- [SDR JR2R20261012537](https://openairdocs.org/sdr/JR2R20261012537), Oct 12, 2026: Emb ERJ170200LR. SKIN. CHAFED. LEFT WING FIXED LEADING EDGE OVER PYLON HAS CHAFES. REPAIRED. (N88359)
- [SDR YENA2026101500971](https://openairdocs.org/sdr/YENA2026101500971), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450562. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURF (N588JB)
- [SDR YENA2026101500970](https://openairdocs.org/sdr/YENA2026101500970), Oct 11, 2026: Airbus A320232. SKIN. DAMAGED. DURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N558JB - SRM REPAIR SURVEY, DEFECT 4400 62-29919 ; "(RESOLVED O (N588JB)
- [SDR YENA2026101500969](https://openairdocs.org/sdr/YENA2026101500969), Oct 11, 2026: Airbus A320232. SKIN. CRACKED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDIN (N588JB)
- [SDR YENA2026101500968](https://openairdocs.org/sdr/YENA2026101500968), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING ); "(RESOL (N588JB)
- [SDR YENA2026101500967](https://openairdocs.org/sdr/YENA2026101500967), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING ); "(RESOLVED (N588JB)
- [SDR YENA2026101500966](https://openairdocs.org/sdr/YENA2026101500966), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450569. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURF (N588JB)
- [SDR YENA2026101500965](https://openairdocs.org/sdr/YENA2026101500965), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDIN (N588JB)
- [SDR YENA2026101500964](https://openairdocs.org/sdr/YENA2026101500964), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450551. CORROSION ON LH WING TOP SKIN OVERHANG LOWER SURF (N588JB)
- [SDR YENA2026101500962](https://openairdocs.org/sdr/YENA2026101500962), Oct 11, 2026: Airbus A320232. SKIN. CRACKED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING ); "REF AE (N588JB)
- [SDR YENA2026101500961](https://openairdocs.org/sdr/YENA2026101500961), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDIN (N588JB)
- [SDR YENA2026101500960](https://openairdocs.org/sdr/YENA2026101500960), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING ); "REF AEROM (N588JB)
- [SDR YENA2026101500959](https://openairdocs.org/sdr/YENA2026101500959), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDIN (N588JB)
- [SDR YENA2026101500958](https://openairdocs.org/sdr/YENA2026101500958), Oct 11, 2026: Airbus A320232. SKIN. CRACKED. DURING HEAVY MAINTENANCE, EA A26-876-01 WING / LH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 9-18 / CORROSION - P (N588JB)
- [SDR YENA2026101500954](https://openairdocs.org/sdr/YENA2026101500954), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, EA 26-872-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 13 / CORROSION - PERM (N588JB)
- [SDR YENA2026101500951](https://openairdocs.org/sdr/YENA2026101500951), Oct 11, 2026: Airbus A320232. SKIN. CORRODED. DURING HEAVY MAINTENANCE, EA 26-873-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 7 AND 13 / CORROSION  (N558JB)
- [SDR FDEA202610081495](https://openairdocs.org/sdr/FDEA202610081495), Oct 8, 2026: Doug MD11F. DOUBLER. CRACKED. RIGHT WING, FIXED LEADING EDGE RIB DOUBLER AT STATION XOS 667 FOUND CRACK ABOUT 0.2". (N610FE)
- [SDR FDEA202610081494](https://openairdocs.org/sdr/FDEA202610081494), Oct 8, 2026: Doug MD11F. DOUBLER. CRACKED. LEFT WING, FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.3". (N610FE)
- [SDR FDEA202610081493](https://openairdocs.org/sdr/FDEA202610081493), Oct 8, 2026: Doug MD11F. DOUBLER. CRACKED. LEFT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 682 FOUND CRACK ABOUT 0.2". (N610FE)
- [SDR FDEA202610081492](https://openairdocs.org/sdr/FDEA202610081492), Oct 8, 2026: Doug MD11F. DOUBLER. CRACKED. RIGHT WING - FIXED LEADING EDGE BEADED DOUBLER AT STATION XOS 705 FOUND CRACK ABOUT 0.2". (N610FE)
- [SDR COEA2026101212767](https://openairdocs.org/sdr/COEA2026101212767), Oct 7, 2026: Textrn 408. SKIN. CRACKED. DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK ON THE RT UPPER WING SKIN BETWEEN WS 224.32 AND WS 241.68. OPEN (N767FX)
- [SDR COEA2026101211767](https://openairdocs.org/sdr/COEA2026101211767), Oct 7, 2026: Textrn 408. SKIN. CRACKED. DURING A POST FLIGHT INSPECTION, DISCOVERED A CRACK IN THE LT UPPER WING SKIN BETWEEN WS 157.95 AND WS 142.30. OPEN (N767FX)
- [SDR UIEA2026100600955](https://openairdocs.org/sdr/UIEA2026100600955), Oct 7, 2026: Boeing 74745EF. SKIN. CRACKED. DURING LFEC INSPECTION AT LH WING FRONT SPAR UPPER SKIN BETWEEN WS621-WS637, FOUND 02 EA FASTENERS WITH CRACKED INDICATI (N486MC)
- [SDR UIEA2026100600956](https://openairdocs.org/sdr/UIEA2026100600956), Oct 7, 2026: Boeing 74745EF. SKIN. CRACKED. DURING LFEC INSPECTION AT RH WING FRONT SPAR LOWER SKIN BETWEEN WS540-WS560 FOUND 01 EA FASTENER WITH CRACK.(<P>REFER TO (N486MC)
- [SDR CALA2026100820218](https://openairdocs.org/sdr/CALA2026100820218), Oct 7, 2026: Airbus A319131. ACCESS PANEL. DAMAGED. DURING REMOVAL OF ACCESS PANEL 540KB, ACFT SKIN WAS DAMAGED. EXCEEDED LIMITS OF SRM 57-21-11-300-002, INTERIM REPAIR PER (N848UA)
- [SDR CALA2026101320350](https://openairdocs.org/sdr/CALA2026101320350), Oct 6, 2026: Boeing 757224. ACCESS PANEL. CRACKED. RIGHT WING INTERSPAR 2 EACH CRACKS NOTED WHILE ACCOMPLISHING EA5720-03647 (A) AT HOLES NR 6 & 27 AT PANEL ACCESS 643BB.  (N17126)
- [SDR JR2R20261006891](https://openairdocs.org/sdr/JR2R20261006891), Oct 6, 2026: Emb ERJ170200LL. PANEL. CHAFED. R/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM. (N85320)
- [SDR JR2R20261006890](https://openairdocs.org/sdr/JR2R20261006890), Oct 6, 2026: Emb ERJ170200LL. PANEL. CHAFED. L/H WING OVER PYLON L/E PANEL IS CHAFED. REPAIRED PER SRM. (N85320)
- [SDR DALA2026100605529](https://openairdocs.org/sdr/DALA2026100605529), Oct 4, 2026: Boeing 717200. VANE. DENTED. 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 (N978AT)
- [SDR SWAA2026100721957](https://openairdocs.org/sdr/SWAA2026100721957), Oct 3, 2026: Boeing 7378. WINGLET. DELAMINATED. UPPER SPLIT SCIMITAR WINGLET LEADING EDGE DELAMINATED. IAW SRM 57-30-01-2R-6, PROCEDURES BY COMPLETING REPAIR 6, TYPE 1. (N8793Q)
- [SDR R61A2026100100290](https://openairdocs.org/sdr/R61A2026100100290), Oct 1, 2026: Emb ERJ170200LR. SKIN. CRACKED. FOUND CRACK ON RT WING MAIN BOX, LOWER SKIN, AT SPAR II RIB 4A JUNCTION. REPAIRED PER ETD 2026-170-016493. (N208JQ)
- [SDR COEA2026100109708](https://openairdocs.org/sdr/COEA2026100109708), Sep 30, 2026: Textrn 408. SKIN. CRACKED. EVIDENCE OF A CRACK ON THE R/H WING AFT SIDE TOWARDS THE OUTBOARD PORTION OF THE FLAP. OPEN (N708FX)
- [SDR DALA2026100105450](https://openairdocs.org/sdr/DALA2026100105450), Sep 30, 2026: Boeing 717200. SKIN. GOUGED. GOUGES ON FIXED LEADING EDGE BTW XOS=390 TO XOS=410 AT LT WING, COMPLIED WITH ER/A 637059-14. (1841449) (AIRCRAFT GROUND (N991AT)
- [SDR IPXA2026100181758](https://openairdocs.org/sdr/IPXA2026100181758), Sep 29, 2026: Airbus A300F4622R. ACCESS PANEL. CRACKED. LEFT WING BELOW KRUGER FLAP ACCESS PANEL 513AB STRUCTURE (RING) CRACKED. INTERNAL DOUBLER WAS REMOVED AT LH WING BELOW K (N158UP)
- [SDR COEA2026100108708](https://openairdocs.org/sdr/COEA2026100108708), Sep 29, 2026: Textrn 408. PANEL. DENTED. DENT UNDER LT SPONSON PANEL. OPEN (N708FX)
- [SDR SCNA20261014425](https://openairdocs.org/sdr/SCNA20261014425), Sep 28, 2026: Boeing 7378F2. SKIN PANEL. CRACKED. INITIAL INSPECTION: CRACK WAS FOUND IN THE SKIN OF HOLE #6 SKIN AND COUNTERSINK BTW 12 O CLOCK POSITION AT LEADING EDGE  (N825SY)
- [SDR SCNA20261014424](https://openairdocs.org/sdr/SCNA20261014424), Sep 28, 2026: Boeing 7378F2. SKIN. CRACKED. CRACKS WERE FOUND IN THE SKIN OF HOLE #4 SKIN & COUNTERSINK BTW 10 O CLOCK POSITION AND HOLE #5 SKIN & COUNTERSINK BTW 1 (N825SY)
- [SDR SWIA2026092777276](https://openairdocs.org/sdr/SWIA2026092777276), Sep 27, 2026: Emb ERJ170200LL. SKIN. DENTED. LH WING TIP LEADING EDGE FOUND DENTED FILED CLOSEDDUE TO NO ALLOWABLE DENT DAMAGE TO THE WING TIP FIXED LEADING EDGE BEI (N85373)
- [SDR SWAA2026101619844](https://openairdocs.org/sdr/SWAA2026101619844), Sep 24, 2026: Boeing 7378H4. ACCESS PANEL. ELONGATED. ELONGATED HOLES ON THE LT WING ACCESS PANEL 561CB. REPAIRED THE ACCESS PANEL 561CB IAW SRM 51-70-04-2R-10, REPAIR 10. (N8306H)
- [SDR SWAA2026101639462](https://openairdocs.org/sdr/SWAA2026101639462), Sep 24, 2026: Boeing 7378H4. ACCESS PANEL. DAMAGED. ELONGATED HOLES ON LT WING ACCESS PANEL 561AB. REPAIRED THE ACCESS PANEL 561AB IAW SRM 51-70-04-2R-10, REPAIR 10. (N8306H)
- [SDR SWAA2026101639003](https://openairdocs.org/sdr/SWAA2026101639003), Sep 24, 2026: Boeing 7378H4. ACCESS PANEL. DAMAGED. ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR  (N8306H)

All 27,210: https://openairdocs.org/jasc/5730/reports.md

## Other codes in chapter 57

- [JASC 5700](https://openairdocs.org/jasc/5700): Wing Structure (2,401 reports)
- [JASC 5710](https://openairdocs.org/jasc/5710): Wing Main, Frame Structure (4,449 reports)
- [JASC 5711](https://openairdocs.org/jasc/5711): Wing Spar (5,579 reports)
- [JASC 5712](https://openairdocs.org/jasc/5712): Wing, Rib/Bulkhead (6,954 reports)
- [JASC 5713](https://openairdocs.org/jasc/5713): Wing, Longeron/Stringer (2,086 reports)
- [JASC 5714](https://openairdocs.org/jasc/5714): Wing, Center Box (1,451 reports)
- [JASC 5720](https://openairdocs.org/jasc/5720): Wing Miscellaneous Structure (13,614 reports)
- [JASC 5740](https://openairdocs.org/jasc/5740): Wing, Attach Fittings (3,003 reports)
- [JASC 5741](https://openairdocs.org/jasc/5741): Wing, Fuselage Attach Fittings (544 reports)
- [JASC 5742](https://openairdocs.org/jasc/5742): Wing, Nacelle/Pylon Attach Fittings (258 reports)
- [JASC 5743](https://openairdocs.org/jasc/5743): Wing, Landing Gear Attach Fittings (3,097 reports)
- [JASC 5744](https://openairdocs.org/jasc/5744): Wing, Control Surface Attach Fittings (2,713 reports)
- [JASC 5750](https://openairdocs.org/jasc/5750): Wing, Control Surfaces (1,157 reports)
- [JASC 5751](https://openairdocs.org/jasc/5751): Ailerons (5,077 reports)
- [JASC 5752](https://openairdocs.org/jasc/5752): Aileron Tabs (654 reports)
- [JASC 5753](https://openairdocs.org/jasc/5753): Trailing Edge Flaps (31,481 reports)
- [JASC 5754](https://openairdocs.org/jasc/5754): Leading Edge Devices (17,330 reports)
- [JASC 5755](https://openairdocs.org/jasc/5755): Spoilers (4,549 reports)
- [JASC 5797](https://openairdocs.org/jasc/5797): Wing System Wiring (81 reports)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.