# JASC 5330: Fuselage Main, Plate/Skin

- Type: JASC system/component code (FAA)
- ATA chapter: 53 Fuselage
- Title in the code table: FUSELAGE MAIN, PLATE/SKIN
- Service difficulty reports: 79,216
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=48
- Page: https://openairdocs.org/jasc/5330

## What it covers

For reports of the exterior covering of the fuselage including access covers.

## Service difficulty reports (79,216, newest 50)

- [SDR DALA2026101905723](https://openairdocs.org/sdr/DALA2026101905723), Oct 18, 2026: Boeing 717200. SKIN. DAMAGED. FOUND A DISCREPANT FASTENER HOLE WAS IDENTIFIED AT THE INTERSECTION OF FRAME Y503 AND LONGERON L1, AT THE FOURTH FASTENE (N980AT)
- [SDR IXXA20261016001](https://openairdocs.org/sdr/IXXA20261016001), Oct 16, 2026: Boeing 767323. SKIN. CRACKED. PERFORM REPLACEMENT OF THE FOLLOWING DAMAGE SECTION 43 FUSELAGE STRUCTURE FROM STA. 654 TO STA 785.9 (N443AZ)
- [SDR IXXA20261015007](https://openairdocs.org/sdr/IXXA20261015007), Oct 15, 2026: Boeing 767323. SKIN. MECHANIC ERROR. MISSDRILLED HOLES AT R/H SKIN TEAR STRAP LOCATIONS FROM STA 654+44 TO STA 654+88 BETWEEN S-13R & S-9R AND FROM STA 654+1 (N443AZ)
- [SDR JR2R20261015724](https://openairdocs.org/sdr/JR2R20261015724), Oct 15, 2026: Emb ERJ170200LL. SKIN. CORRODED. FWD CARGO SCUFF PLATE EXTERNAL SKIN LOCATED AT FR24-FR27 HAS MULTIPLE SPOTS OF CORROSION. REPAIRED PER ETD. (N88359)
- [SDR IXXA20261015001](https://openairdocs.org/sdr/IXXA20261015001), Oct 15, 2026: Boeing 767323. TEAR STRAP. MECHANIC ERROR. MISRILLED HOLES AT LT SKIN TEAR STRAP (N443AZ)
- [SDR AALA202610160189](https://openairdocs.org/sdr/AALA202610160189), Oct 14, 2026: Airbus A321253NX. SKIN PANEL. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON FUSELAGE SKIN PANEL AROUND THE VACUUM GENERATOR EXHAUST BETWEEN FR 67 AND FR  (N464AA)
- [SDR SIMA20261014002](https://openairdocs.org/sdr/SIMA20261014002), Oct 14, 2026: Emb ERJ170100SE. SKIN. CORRODED. CORROSION ON FORWARD EDGE OF LAV DRAIN BOX AFT SIDE OF FRAME 88 BETWEEN STRINGERS 29R-28R. (LEVEL 2 CORROSION) REPAIRED  (N774JG)
- [SDR IXXA202610140002](https://openairdocs.org/sdr/IXXA202610140002), Oct 14, 2026: Boeing 767323. BUTTSTRAP. DAMAGED. CIRCUNFERENTIAL BUTT SPLICE STA 654+22 BETWEEN S-13L AND S-14L AN OVERSIZE RIVET HOLE NOTED WITH A .281" DIAMETER APROX (N443AZ)
- [SDR IXXA20261014001](https://openairdocs.org/sdr/IXXA20261014001), Oct 14, 2026: Boeing 767323. SKIN. OUT OF LIMITS. L/H WINDOW B/S 654+33 AFT EDGE GAP IS OUT OF LIMITS AT .193 MAX LIMIT BEING .160 (N443AZ)
- [SDR DALA2026101605689](https://openairdocs.org/sdr/DALA2026101605689), Oct 13, 2026: Boeing 737932ER. SKIN. DAMAGED. LEFT FUSELAGE SKIN HAS DAMAGE ABOVE HORIZONTAL STAB NEAR SLIDING SEAL. STA 1088 AND 1104. REF ERA 6374949-14. (9153550)  (N923DZ)
- [SDR N6WA2026101506](https://openairdocs.org/sdr/N6WA2026101506), Oct 13, 2026: Cndair CL6002C11. SKIN. CORRODED. EVALUATE POSSIBLE CORROSION ON SKIN FUSELAGE AT PANEL 195DR. REMOVED CORROSION ON SKIN FUSELAGE IN SEVERAL POINTS IAW SR (N581GJ)
- [SDR N6WA2026101505](https://openairdocs.org/sdr/N6WA2026101505), Oct 13, 2026: Cndair CL6002C11. SKIN. SCRATCHED. EVALUATE SCRATCHES ON SKIN FUSELAGE LEFT BETWEEN BS 939 - 1115 AT PANEL 195DL. REMOVED SCRATCHES ON SKIN AT PANEL 195DL  (N581GJ)
- [SDR N6WA2026101504](https://openairdocs.org/sdr/N6WA2026101504), Oct 13, 2026: Cndair CL6002C11. SKIN. DAMAGED. FOUND 2EA DAMAGED AREAS ON LOWER FUSELAGE SKIN AT FS977. PERFORMED PERMANENT REPAIR AT AFT FUSELAGE SKIN FS 977, STR 27  (N581GJ)
- [SDR AALA202610152437](https://openairdocs.org/sdr/AALA202610152437), Oct 12, 2026: Airbus A319132. SKIN. CRACKED. AIRCRAFT IN BASE MAINTENANCE: FASTIGUE CRACK RADIATING FROM FASTENER HOLE BETWEEN FR13-FR14 AND BETWEEN Z+780-Z+950ON LH (N807AW)
- [SDR CALA2026101520382](https://openairdocs.org/sdr/CALA2026101520382), Oct 11, 2026: Boeing 737824. SKIN. CRACKED. FOUND A CRACK AT FUSELAGE EXTERNAL SKIN WASTE VENT BS 917 STR 21 - 22. PERFORMED PERMANENT REPAIR ON FUSELAGE EXTERNAL S (N14219)
- [SDR DALA2026101305626](https://openairdocs.org/sdr/DALA2026101305626), Oct 10, 2026: Boeing 717200. SKIN. DENTED. FOUR DENTS IDENTIFIED COMMON TO AFT INSTALLATION DOUBLER BETWEEN L2R AND L3R FRAME Y541 TO Y560. REPAIRED PER ER/A 63724 (N961AT)
- [SDR UIEA2026100900973](https://openairdocs.org/sdr/UIEA2026100900973), Oct 10, 2026: Boeing 767375. SKIN. CRACKED. DURING EO 6753A070 (SB 767-53A0100 R3/AD 2012-09-04 TERMINATING ACTION) OPEN-HOLE HFEC AT STA 955 R/H, A CRACK INDICATIO (N649GT)
- [SDR DALA2026101305625](https://openairdocs.org/sdr/DALA2026101305625), Oct 9, 2026: Boeing 717200. SKIN. CRACKED. DENT AND CRACK FUSELAGE SKIN STA Y=370-389, L-29R & L-30. REPAIRED PER ER/A 610692-14. (1857452) AIRCRAFT WAS GROUNDED. (N978AT)
- [SDR DALA2026101205599](https://openairdocs.org/sdr/DALA2026101205599), Oct 9, 2026: Boeing 717200. SKIN. MECHANIC ERROR. DRILL START INDENTATIONS AT CABIN CEILING BS 927, BTWN STRINGER 3R & 4R. REPAIRED PER ER/A 637414-14. (1856706) AIRCRAFT (N920AT)
- [SDR UIEA2026092100889](https://openairdocs.org/sdr/UIEA2026092100889), Oct 9, 2026: Boeing 74748EF. DOUBLER. NO DISCREPANCY. SECT 41 LAP JOINT INSP: EXISTING DOUBLERS (06 EA) ON S-14L STA 140-160, S-44L STA 240-260, S-44R STA 240-260, S39R STA 3 (N419MC)
- [SDR UIEA2026100500952](https://openairdocs.org/sdr/UIEA2026100500952), Oct 9, 2026: Boeing 74748EF. DOUBLER. MISINSTALLED. SEC 42 LAP JOINT INSP OF EXISTING DOUBLERS (02 EA) ON S39L, STA 940-960 AND S39R, STA 920-960; FOUND THE REPAIR NOT CONF (N419MC)
- [SDR UIEA2026100600964](https://openairdocs.org/sdr/UIEA2026100600964), Oct 9, 2026: Boeing 74748EF. DOUBLER. MISINSTALLED. SECT 46 LAP JOINT INSP OF EXISITNG DOUBLERS (05 EA), STRINGER 14L, BS 1980-2020, S12L, BS 1720-1740, S12L, STA 2140-2160 (N419MC)
- [SDR SWIA2026100877552](https://openairdocs.org/sdr/SWIA2026100877552), Oct 8, 2026: Emb ERJ170200LL. SKIN. DENTED. DENTED FWD FUSELAGE LT SKIN JUST BEHIND THE LI DOOR BTWN FRAMES 21-22, STRINGERS 15L-16L. THE TOTAL AREA OF THE IS 4 INC (N304SY)
- [SDR DALA2026101205589](https://openairdocs.org/sdr/DALA2026101205589), Oct 8, 2026: Boeing 737932ER. SKIN. CRACKED. DURING HFEC INSP. ON CUT OUT OF UPPER SKIN. STRINGER 2ND HOLE FROM CUT OUT IS CRACKED. ALSO CUT OUT ON STRINGER 24 CUT O (N808DN)
- [SDR DALA2026101205588](https://openairdocs.org/sdr/DALA2026101205588), Oct 8, 2026: Boeing 737932ER. SKIN. PUNCTURED. DTE, ER/A 637291-14 REV A FOR SKIN REPAIR OF PUNCTURE AT STA 203.8 AND STR24L. REF ERA 637291-14. (1855311) AIRCRAFT WAS (N808DN)
- [SDR AALA202610094763](https://openairdocs.org/sdr/AALA202610094763), Oct 8, 2026: Boeing 737823. SKIN. CORRODED. AIRCRAFT IN BASE MAINTENANCE: AFT CARGO SKIN CORROSION AT BS 767-807, STR 27R. ACCOMPLISHED REPAIR DOUBLER INSTALL AND R (N810NN)
- [SDR DALA2026101305608](https://openairdocs.org/sdr/DALA2026101305608), Oct 7, 2026: Boeing 757232. SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN BS 328, 348, 360, AND 391. REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853249)(AIRCRA (N6707A)
- [SDR DALA2026101305607](https://openairdocs.org/sdr/DALA2026101305607), Oct 7, 2026: Boeing 757232. SKIN. DAMAGED. LIGHTNING STRIKE ON FUSELAGE SKIN BS 328 - 348, 360, & 391, REPAIRED IAW SRM 53-00-01-2R, PROCEDURE 6. (1853238)(AIRCRAF (N6707A)
- [SDR UIEA2026093000932](https://openairdocs.org/sdr/UIEA2026093000932), Oct 7, 2026: Boeing 74745EF. SKIN. GOUGED. DURING INSPECTION OF THE LOWER LOBE FWD CARGO DOOR STRINGER 34R SKIN LAP SPLICE, A GOUGE WAS FOUND C/T UPPER SKIN. WORK  (N486MC)
- [SDR AALA202610108075](https://openairdocs.org/sdr/AALA202610108075), Oct 6, 2026: Airbus A321211. SKIN PANEL. CRACKED. AIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL FASTENER HOLE AT FR 14 AND S11R - REPAIRED FUSELAGE SKIN PANEL (N174US)
- [SDR AALA202610071210](https://openairdocs.org/sdr/AALA202610071210), Oct 6, 2026: Airbus A321211. SKIN PANEL. CRACKED. AIRCRAFT IN BASE MAINTENANCE: CRACKED FUSELAGE SKIN PANEL AT FR 14 AND S11L - REPAIRED SKIN PANEL PER EA 379757 (N174US)
- [SDR CALA2026100720187](https://openairdocs.org/sdr/CALA2026100720187), Oct 6, 2026: Boeing 777224. SKIN. CRACKED. ONE HOLE FOUND CRACKED ON RT FUSELAGE SKIN LAYER UNDER LONGERON FITTING. REPAIRED IAW EA 5310-07557, OP 007. (N78008)
- [SDR QMLA2026100620076](https://openairdocs.org/sdr/QMLA2026100620076), Oct 6, 2026: Urocop EC135P2. DOUBLER. CRACKED. DURING INSPECTIONS FOUND REAR DOUBLER CRACK. ALSO NEXT TO THAT THE INSIDE REINFORCEMENT CRACKED (N138LN)
- [SDR JR2R20261006187](https://openairdocs.org/sdr/JR2R20261006187), Oct 6, 2026: Emb ERJ170200LL. SKIN. CORRODED. UPON REMOVAL OF FWD LOWER DRAIN MAST, EXTERNAL SKIN FOUND CORRODED. REPAIRED PER ETD. (N85320)
- [SDR AALA202610089601](https://openairdocs.org/sdr/AALA202610089601), Oct 5, 2026: Boeing 737823. SKIN. CORRODED. AIRCRAFT IN BASE MAINTENANCE: LH RAM AIR FWD DOOR INTERNAL SKIN CORRODED. REMOVED AND REPLACED LH RAM AIR FWD DOOR MODUL (N819NN)
- [SDR 9WGA2026100754501](https://openairdocs.org/sdr/9WGA2026100754501), Oct 5, 2026: Doug MD11F. SKIN. GROUND DAMAGE. AT STATION NSY, DURING CARGO LOADING, ONE PALLET FELL OFF THE K-LOADER AND HIT THE FUSELAGE ABOVE WATER SERVICING PANEL  (N9WGA)
- [SDR IPXA2026101280317](https://openairdocs.org/sdr/IPXA2026101280317), Oct 3, 2026: Boeing 75724APF. SKIN. CORRODED. AFTER REMOVAL OF ADF ANTENNA FOUND UPPER FUSELAGE SKIN WITH DEEP PITTING CORROSION AND TOOLING MARKS. (N402UP)
- [SDR ABXA20261003452](https://openairdocs.org/sdr/ABXA20261003452), Oct 3, 2026: Boeing 767341. SKIN. DAMAGED. DURING C 6 CHECK IN AT KALITTA MTX FOUND CROWN SKIN DAMAGED AT BS 1467 LBL 12. TT04. MTX ACCOMPLISHED REPAIR OF CROWN SK (N760CK)
- [SDR SWAA2026101500242](https://openairdocs.org/sdr/SWAA2026101500242), Oct 2, 2026: Boeing 7378H4. DOUBLER. CRACKED. EGPR SURROUND DOUBLER CRACKED AT LOWER FLANGE. ACCOMPLISHED REPAIR ON EGPR SURROUND DOUBLER LOWER FLANGE IAW SRM 53-10-1 (N8697C)
- [SDR DALA2026100505510](https://openairdocs.org/sdr/DALA2026100505510), Oct 2, 2026: Boeing 717200. SKIN. DAMAGED. FUSELAGE SKIN FS 294-351 S-28R TO S-27L DAMAGED. REPAIRED PER ER/A 590835-14. (1845326) AIRCRAFT WAS GROUNDED. (N998AT)
- [SDR DALA2026100505499](https://openairdocs.org/sdr/DALA2026100505499), Oct 2, 2026: Airbus BD5001A11. WASTE BOX. CORRODED. LAVATORY WASTE BOX FWD RIGHT HAND CORNER (DOOR SEAL AREA) HAS CORROSION. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUM (N322DU)
- [SDR CALA2026100520095](https://openairdocs.org/sdr/CALA2026100520095), Oct 2, 2026: Boeing 777224. SKIN. CRACKED. ONE HOLE FOUND CRACKED AT LONGERON AREA. THE FUSELAGE SKIN AT BS 993-1035, S35R-37R WAS REPAIRED IAW EA 5310-07557, REV  (N78008)
- [SDR CALA2026100520092](https://openairdocs.org/sdr/CALA2026100520092), Oct 2, 2026: Boeing 777224. SKIN. CRACKED. TWO HOLES FOUND CRACKED ON RT UNDERWING LONGERON AREA. FUSELAGE SKIN AT BS 993-1035, S35-37R REPAIRED IAW EA 5310-07557, (N78008)
- [SDR CALA2026100520090](https://openairdocs.org/sdr/CALA2026100520090), Oct 2, 2026: Boeing 777224. SKIN. CRACKED. LEFT UNDERWING LONGERON FUSELAGE SKIN FOUR FASTNER HOLES FOUND CRACKED. FUSELAGE SKIN REPAIRED AT BS 993 - 1035, S35L TO (N78008)
- [SDR HNAA202610070954](https://openairdocs.org/sdr/HNAA202610070954), Oct 1, 2026: Emb EMB145LR. SKIN. DENTED. DENT AND SCRATCH ON EXTERNAL SKIN AT BTW FR12A-13 BTW STR 6-8L. REPAIRED IAW SRM 53-10-01 (N653AE)
- [SDR DALA2026100105449](https://openairdocs.org/sdr/DALA2026100105449), Oct 1, 2026: Boeing 717200. REPAIR. DENTED. DENTS ON PREVIOUS FLUSH REPAIR BTW BS 218-256 BTW LONG 17LT TO 18 LT, R & R FLUSH REPAIR PER SRM 53-00-01-2R. (1841666)  (N978AT)
- [SDR CALA2026101320344](https://openairdocs.org/sdr/CALA2026101320344), Sep 30, 2026: Boeing 737824. SKIN. DENTED. THREE DENTS FOUND ON UPPER FUSELAGE SKIN BETWEEN BS 500B - 500C, STRINGER 1 & 2L. DENTS INTERFERE WITH FWD STARLINK ANTE (N73299)
- [SDR Y2PA2026100126023](https://openairdocs.org/sdr/Y2PA2026100126023), Sep 30, 2026: Doug MD88. SKIN. DAMAGED. ON 29AUG2026, THE SUBJECT AIRCRAFT WAS INVOLVED IN AN ENGINE CHANGE INCIDENT WHICH RESULTED IN DAMAGE TO THE FUSELAGE SK (N832US)
- [SDR IXXA20260930002](https://openairdocs.org/sdr/IXXA20260930002), Sep 30, 2026: Boeing 767323. SKIN. CRACKED. MAIN CARGO COMPARTMENT BETWEEN STRINGER 17L TO STRINGER 18L AND STATION 654+44 TO STATION 654+55 A CRACK WAS FOUND ON TH (N443AZ)
- [SDR IXXA20260930001](https://openairdocs.org/sdr/IXXA20260930001), Sep 30, 2026: Boeing 767323. SKIN. CRACKED. SEC 43 FUSELAGE SKIN FROM S-17R AND BETWEEN S-18R & S-19R AND STATION 654+44 TO STATION 654+66 A CRACK WAS FOUND. (N443AZ)

All 79,216: https://openairdocs.org/jasc/5330/reports.md

## Other codes in chapter 53

- [JASC 5300](https://openairdocs.org/jasc/5300): Fuselage Structure (General) (8,203 reports)
- [JASC 5301](https://openairdocs.org/jasc/5301): Aerial Tow Equipment (18 reports)
- [JASC 5302](https://openairdocs.org/jasc/5302): Rotorcraft Tail Boom (965 reports)
- [JASC 5310](https://openairdocs.org/jasc/5310): Fuselage Main, Structure (38,379 reports)
- [JASC 5311](https://openairdocs.org/jasc/5311): Fuselage Main, Frame (61,498 reports)
- [JASC 5312](https://openairdocs.org/jasc/5312): Fuselage Main, Bulkhead (20,038 reports)
- [JASC 5313](https://openairdocs.org/jasc/5313): Fuselage Main, Longeron/Stringer (36,262 reports)
- [JASC 5314](https://openairdocs.org/jasc/5314): Fuselage Main, Keel (2,916 reports)
- [JASC 5315](https://openairdocs.org/jasc/5315): Fuselage Main, Floor Beam (44,127 reports)
- [JASC 5320](https://openairdocs.org/jasc/5320): Fuselage Miscellaneous Structure (215,617 reports)
- [JASC 5321](https://openairdocs.org/jasc/5321): Fuselage Floor Panel (49,215 reports)
- [JASC 5322](https://openairdocs.org/jasc/5322): Fuselage Internal Mounting Structure (12,743 reports)
- [JASC 5323](https://openairdocs.org/jasc/5323): Fuselage Internal Stairs (98 reports)
- [JASC 5324](https://openairdocs.org/jasc/5324): Fuselage Fixed Partitions (40 reports)
- [JASC 5340](https://openairdocs.org/jasc/5340): Fuselage Main, Attach Fittings (22,372 reports)
- [JASC 5341](https://openairdocs.org/jasc/5341): Fuselage, Wing Attach Fittings (489 reports)
- [JASC 5342](https://openairdocs.org/jasc/5342): Fuselage, Stabilizer Attach Fittings (571 reports)
- [JASC 5343](https://openairdocs.org/jasc/5343): Fuselage, Landing Gear Attach Fittings (1,944 reports)
- [JASC 5344](https://openairdocs.org/jasc/5344): Fuselage, Door Hinge (2,417 reports)
- [JASC 5345](https://openairdocs.org/jasc/5345): Fuselage, Equipment Attach Fittings (812 reports)
- [JASC 5346](https://openairdocs.org/jasc/5346): Fuselage, Powerplant Attach Fittings (921 reports)
- [JASC 5347](https://openairdocs.org/jasc/5347): Fuselage, Seat/Cargo Attach Fittings (66,237 reports)
- [JASC 5350](https://openairdocs.org/jasc/5350): Aerodynamic Fairings (6,105 reports)
- [JASC 5397](https://openairdocs.org/jasc/5397): Fuselage Main, Bulkhead Fuselage wiring (67 reports)

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