# JASC 5324: Fuselage Fixed Partitions

- Type: JASC system/component code (FAA)
- ATA chapter: 53 Fuselage
- Title in the code table: FUSELAGE FIXED PARTITIONS
- Service difficulty reports: 40
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=48
- Page: https://openairdocs.org/jasc/5324

## What it covers

For reports of the fixed partitions which are part of the fuselage structure.

## Service difficulty reports (40)

- [SDR AALA202505162244](https://openairdocs.org/sdr/AALA202505162244), Apr 22, 2025: Boeing 737823. BRACKET. CORRODED. AIRCRAFT IN BASE MAINTENANCE: CORROSION ON APU COMPARTMENT BRACKET AT BS 1088, LBL 2. REPLACED BRACKET PER AARD 51-00-05 (N966AN)
- [SDR R61A2025010600026](https://openairdocs.org/sdr/R61A2025010600026), Jan 6, 2025: Emb ERJ170100SE. BEAM. CORRODED. DURING HEAVY CHECK AFT PASSENGER DOOR (747YX) CUTOUT LOWER BEAM FOUND CORRODED. L2 DOOR LOWER BEAM REPAIRED IAW ETD2024- (N747YX)
- [SDR A6WA202303298542](https://openairdocs.org/sdr/A6WA202303298542), Mar 29, 2023: Cndair CL6002B19. ANGLE. CORRODED. PAX DOOR SILL ANGLE HAS SMALL SPOTS OF CORROSION ALL ALONG THE UPPER TRIM ANGLE. AC REMOVED FROM SERVICE. REMOVED AND RE (N423AW)
- [SDR A6WA202301168522](https://openairdocs.org/sdr/A6WA202301168522), Jan 16, 2023: Cndair CL6002B19. FITTING. CORRODED. CORROSION ON FLOOR SUPPORT PN 601R38673-43 AT FS349.00 AND LBL38 TO LBL44. **********AIRCRAFT REMOVED FROM SERVICE****** (N466AW)
- [SDR A6WA202210218352](https://openairdocs.org/sdr/A6WA202210218352), Oct 21, 2022: Cndair CL6002B19. CHANNEL. CORRODED. L/H SILL BETWEEN FS 349.00 AND FS364.00 IS CORRODED ******AIRCRAFT REMOVED FROM SERVICE**** REMOVED AND INSTALL NEW FLOO (N456ZW)
- [SDR A6WA202210148340](https://openairdocs.org/sdr/A6WA202210148340), Oct 14, 2022: Cndair CL2151A10. NONE. CORRODED. LH SIDE SEAT RAIL, APPROX. FS364.00 THRU FS409+16 HAS MULTIPLE AREA'S OF CORROSION. FLAGGED ***AIRCRAFT REMOVED FROM SER (N456ZW)
- [SDR A6WA202209088315](https://openairdocs.org/sdr/A6WA202209088315), Sep 8, 2022: Cndair CL2151A10. PLATE. CORRODED. CORROSION ON FWD GALLEY SUPPORT PLATE AT FS 321 TO FS 327 AND RBL 4 TO RBL 8 AT WL 73.5. *******************AIRCRAFT REM (N460AW)
- [SDR A6WA202208238294](https://openairdocs.org/sdr/A6WA202208238294), Aug 23, 2022: Cndair CL2151A10. CLEAT. CORRODED. CLEAT ATTACHED TO FS313.56 FRAME 601R318086-1 IS CORRODED ***AIRCRAFT REMOVED FROM SERVICE **** INSTALLED NEW CLEAT IAW  (N452AW)
- [SDR A6WA202208188286](https://openairdocs.org/sdr/A6WA202208188286), Aug 18, 2022: Cndair CL2151A10. SEAT TRACK. CORRODED. CORROSION NOTED ON R/H FLOOR SEAT RAIL AT RBL9 AND APPROX. BETWEEN FS364.00-FS398] ****AIRCRAFT REMOVED FROM SERVICE *** (N452AW)
- [SDR A6WA202208188285](https://openairdocs.org/sdr/A6WA202208188285), Aug 18, 2022: Cndair CL6002B19. SEAT TRACK. CORRODED. CORROSION NOTED ON L/H FLOOR SEAT RAIL AT LBL9 AND APPROX. BETWEEN FS364.00-FS398 ****AIRCRAFT REMOVED FROM SERVICE **** (N452AW)
- [SDR A6WA202208178284](https://openairdocs.org/sdr/A6WA202208178284), Aug 17, 2022: Cndair CL6002B19. NONE. DAMAGED. LBL 9 FLOOR BEAM PART # 601R31113-124 COMMON TO THE FS 280 CLIP HAS OVERSIZE FASTENERS HOLES ****AIRCRAFT REMOVED FROM S (N452AW)
- [SDR A6WA202208068263](https://openairdocs.org/sdr/A6WA202208068263), Aug 6, 2022: Cndair CL6002B19. CROSSBEAM. CORRODED. CORROSION NOTED AT 280 CROSSBEAM BETWEEN LBL9-RBL9 ***AIRCRAFT REMOVED FROM SERVICE **** FS 280 BULKHEAD WEB AND FLOOR S (N452AW)
- [SDR A6WA202207308306](https://openairdocs.org/sdr/A6WA202207308306), Jul 30, 2022: Cndair CL2151A10. NONE. CORRODED. CORROSION ON EDGE OF CABIN FLOOR FRAME AT FS 349 AND RBL42 AND CORROSION ON FRAME SUPPORT ANGLE P/N: 601R38783-13 AT FS  (N457AW)
- [SDR A6WA202207308299](https://openairdocs.org/sdr/A6WA202207308299), Jul 30, 2022: Cndair CL2151A10. NONE. CORRODED. L/H FLOOR SEAT TRACK FROM FS 364 TO FS 409+8 RBL 9.5 HAS SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON L/H  (N457AW)
- [SDR A6WA202207298254](https://openairdocs.org/sdr/A6WA202207298254), Jul 29, 2022: Cndair CL6002B19. FLOOR SUPPORT. CORRODED. LH WINDSCREEN OTBD MOUNTING POINT SHOWS SIGNS OF EXFOLIATING CORROSION. ***AIRCRAFT REMOVED FROM SERVICE **** REMOVED AN (N448AW)
- [SDR A6WA202112288170](https://openairdocs.org/sdr/A6WA202112288170), Dec 28, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. RH SIDEWALL SEAT TRACK FROM FS364 TO FS409.00 + 16 HAS SURFACE CORROSION. ****AIRCRAFT REMOVED FROM SERVICE ***** REMOVE (N426AW)
- [SDR A6WA202112238042](https://openairdocs.org/sdr/A6WA202112238042), Dec 23, 2021: Cndair CL6002B19. NONE. CORRODED. CORROSION DAMAGE LOCATED ON R/H FLOOR SILL WEB AT FS 349 TO FS 349+12.5" AND RBL 42 TO RBL 44. DIMENSIONS ARE: (P1) = FS (N435AW)
- [SDR A6WA202102038094](https://openairdocs.org/sdr/A6WA202102038094), Dec 15, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. R/H SIDEWALL SEAT TRACKS FROM FS 364.00 TO FS 559.79 HAVE SEVERAL AREAS OF SURFACE CORROSION. EVALUATED CORROSION ON R/H (N438AW)
- [SDR A6WA202111017947](https://openairdocs.org/sdr/A6WA202111017947), Sep 27, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. SEAT TRACK P/N: 20276-144-0-0 AT FS 364.00 TO FS 409+18 L/H SIDE HAS NUMEROUS SPOTS OF CORROSION AND WEAR. ***AIRCRAFT R (N439AW)
- [SDR A6WA202110187909](https://openairdocs.org/sdr/A6WA202110187909), Sep 27, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. SEAT TRACK PN 20276-144-0-0 AT FS364.00 Ï¿½ FS409.00 + 18Ï¿½ HAS CORROSION AT NUMEROUS LOCATIONS. ***AIRCRAFT REMOVED FR (N439AW)
- [SDR A6WA202111087953](https://openairdocs.org/sdr/A6WA202111087953), Sep 3, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. CORROSION AT MULTIPLE LOCATIONS ON LH SIDEWALL SEAT TRACKS AT FS364, FS386, FS394, FS409, FS409+8, FS409+16, FS409+32, F (N427ZW)
- [SDR A6WA202110217918](https://openairdocs.org/sdr/A6WA202110217918), Aug 17, 2021: Cndair CL6002B19. SEAT TRACK. CORRODED. CORROSION AT MULTIPLE LOCATIONS ON R/H SIDEWALL SEAT TRACKS AT FS379, FS401, FS409+8, FS409+24, FS409+32, FS409+48, FS40 (N427ZW)
- [SDR RAIA2020011620002](https://openairdocs.org/sdr/RAIA2020011620002), Jan 12, 2020: Emb EMB145LR. FLOOR SUPPORT. CORRODED. LAV RH FLOOR SILL HAS CORROSION AROUND NUT PLATE HOLE- R&R LAV RH FLOOR SILL. (N835HK)
- [SDR A6WA201910246952](https://openairdocs.org/sdr/A6WA201910246952), Oct 8, 2019: Cndair CL6002B19. SEAT TRACK. CORRODED. L/H SIDE WALL SEAT TRACK IS CORRODED BETWEEN F.S.364 TO F.S.409. (N409AW)
- [SDR RAIA2019100292001](https://openairdocs.org/sdr/RAIA2019100292001), Sep 22, 2019: Emb EMB145LR. FLOOR SUPPORT. CRACKED. MAIN CABIN CENTER OMEGA BEAM IS CRACKED AND CORRODED AROUND FASTNER HOLE AT FR 59 & 61. R&R CENTER LAV OMEGA BEAM FROM F (N836HK)
- [SDR SWAA2019062634154](https://openairdocs.org/sdr/SWAA2019062634154), Jun 15, 2019: Boeing 7377H4. FLOOR PANEL. PEELING. PASSENGER CABIN FLOOR BOARD PANEL 232CF UPPER SURFACE HAD AREAS OF FIBERS PEELING, BETWEEN BS. 420 TO BS. 480. / REPAIRE (N285WN)
- [SDR SWAA2022012801304](https://openairdocs.org/sdr/SWAA2022012801304), Jun 30, 2017: Boeing 7377H4. WEB. DELAMINATED. (COSTOMER REQEST) 663 L/H LOWER EXISTING REPAIR IS DELAMINATED / INSTALLED REPAIR IN 3 BAYS IAW SRM 57-10-10-2R-2 IN BAY (N781WN)
- [SDR SWAA2022012527571](https://openairdocs.org/sdr/SWAA2022012527571), May 16, 2017: Boeing 7377H4. BULKHEAD. CRACKED. INSIDE A/C BAY DOOR 192CL AT STA. 663 BULKHEAD WALL 1.5 INCH CRACK IN WALL BELOW HYD. LINES. (MARKED). / INSTALLED PERMA (N283WN)
- [SDR A6WA201744921](https://openairdocs.org/sdr/A6WA201744921), Apr 2, 2017: Cndair CL6002B19. BEAM. CRACKED. 1014186-1000-0014 - 280 BEAM IS CRACKED AT THE LOWER SIDE NEXT TO THE MLG MANUAL RELEASE CABLE PULLEY BRACKET, O/B OF LB (N463AW)
- [SDR ASOA20130128250](https://openairdocs.org/sdr/ASOA20130128250), Jan 28, 2013: Emb EMB145LR. DOUBLER. CORRODED. DURING C-CHECK, CORROSION WAS FOUND ON THE LT WALL DOUBLER AT FRAME 61. MX R & R THE LT DOUBLER IAW SRM 51-40-02. (N13903)
- [SDR IPXA11166226](https://openairdocs.org/sdr/IPXA11166226), Apr 12, 2011: Airbus A300F4622R. FLOORBOARD. DELAMINATED. INSPECTION TYPE:10YR, MAIN CABIN FLOORBOARD NR 241SH IS DELAMINATED. ACCOMPLISHED REPAIR ON MAIN CABIN FLOORBOARD NR 241 (N133UP)
- [SDR SWAA050667](https://openairdocs.org/sdr/SWAA050667), Mar 6, 2005: Boeing 7373H4. SKIN. CRACKED. DURING SCHEDULED RON CHECK, FOUND FUSELAGE SKIN CRACKED AT BS 506, STR 16L. REPAIRED SKIN PER SWA EA. (N310SW)
- [SDR 249TR0069](https://openairdocs.org/sdr/249TR0069), Dec 22, 2004: Boeing 7372K5. CHANNEL. CORRODED. AFT LAVATORY FORWARD PARTITION BOTTOM CHANNEL HAS CORROSION. REPLACED CHANNEL PER SRM 51-10-1 AND SRM 51-30-0. (N249TR)
- [SDR SWAA030246](https://openairdocs.org/sdr/SWAA030246), Jan 28, 2003: Boeing 7373H4. WINDOW FRAME. CRACKED. DURING SCHEDULED SPECIAL VISIT, FOUND WINDOW FRAMES CRACKED (2 EA) AT LT WINDOW NR 7 AND RT WINDOW NR 11. REMOVED AND RE (N326SW)
- [SDR C2XA02TY144](https://openairdocs.org/sdr/C2XA02TY144), Sep 18, 2002: Emb EMB145. STRINGER. GOUGED. TYS DURING A SCHEDULED 2-C INSPECTION MAINT. FOUND GOUGES ON STRINGER 19L AND 19R AT STA. 17727.0. MAINT. BLENDED AND ND (N14974)
- [SDR COMA0260448](https://openairdocs.org/sdr/COMA0260448), Jul 22, 2002: Cndair CL6002B19. ANGLE. CRACKED. THE ANGLES AT BL 27 LH AND RH AND INTERCOSTAL AT RBL 36 AT FS 484 WERE FOUND CRACKED.REMVOED DISCREPANT PARTS, FABRICATE (N713CA)
- [SDR COMA0160352](https://openairdocs.org/sdr/COMA0160352), Mar 26, 2001: Cndair CL6002B19. POST. CRACKED. INBOARD AND OUTBOARD POSTS AT RBL 9 AND LBL 9 AT FS 559 ARE CRACKED AT APPROXIMATELY WL 45. CAUSE UNKNOWN. DAMAGED AREAS (N943CA)
- [SDR DHL9872138D](https://openairdocs.org/sdr/DHL9872138D), Jul 11, 1998: Boeing 727228. PANEL. CRACKED. AT D-CHECK, LOWER FWD CARGO COMPT RT FLOOR TO SIDE WALL PANEL CRACKED BS 720 STR 26. INSTALLED PANEL PER SRM 51-10-1, 2' (N721DH)
- [SDR DHL9872136D](https://openairdocs.org/sdr/DHL9872136D), Jul 11, 1998: Boeing 727228. SIDE WALL. CRACKED. AT D-CHECK, LOWER FWD CARGO FLOOR TO SIDE WALL PANEL CRACKED AT BS 600 STR 26L. REMOVED SIDE WALL PANEL PER 25-52-2. INS (N721DH)
- [SDR CA971223001](https://openairdocs.org/sdr/CA971223001), Dec 11, 1997: Bell 204B. CAP ANGLE. BROKEN. (CAN) UPPER CAP ANGLE FOUND BROKEN AND A CRACK HAD DEVELOPED IN THE MAIN PANEL. CRACK APPROX 2 INCHES TO 2.50 INCHES IN 

## 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 (38,407 reports)
- [JASC 5311](https://openairdocs.org/jasc/5311): Fuselage Main, Frame (61,504 reports)
- [JASC 5312](https://openairdocs.org/jasc/5312): Fuselage Main, Bulkhead (20,041 reports)
- [JASC 5313](https://openairdocs.org/jasc/5313): Fuselage Main, Longeron/Stringer (36,267 reports)
- [JASC 5314](https://openairdocs.org/jasc/5314): Fuselage Main, Keel (2,917 reports)
- [JASC 5315](https://openairdocs.org/jasc/5315): Fuselage Main, Floor Beam (44,152 reports)
- [JASC 5320](https://openairdocs.org/jasc/5320): Fuselage Miscellaneous Structure (215,699 reports)
- [JASC 5321](https://openairdocs.org/jasc/5321): Fuselage Floor Panel (49,299 reports)
- [JASC 5322](https://openairdocs.org/jasc/5322): Fuselage Internal Mounting Structure (12,746 reports)
- [JASC 5323](https://openairdocs.org/jasc/5323): Fuselage Internal Stairs (98 reports)
- [JASC 5330](https://openairdocs.org/jasc/5330): Fuselage Main, Plate/Skin (79,225 reports)
- [JASC 5340](https://openairdocs.org/jasc/5340): Fuselage Main, Attach Fittings (22,382 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 (573 reports)
- [JASC 5343](https://openairdocs.org/jasc/5343): Fuselage, Landing Gear Attach Fittings (1,946 reports)
- [JASC 5344](https://openairdocs.org/jasc/5344): Fuselage, Door Hinge (2,418 reports)
- [JASC 5345](https://openairdocs.org/jasc/5345): Fuselage, Equipment Attach Fittings (813 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 (66,268 reports)
- [JASC 5350](https://openairdocs.org/jasc/5350): Aerodynamic Fairings (6,107 reports)
- [JASC 5397](https://openairdocs.org/jasc/5397): Fuselage Main, Bulkhead Fuselage wiring (67 reports)

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