# JASC 5342: Fuselage, Stabilizer Attach Fittings

- Type: JASC system/component code (FAA)
- ATA chapter: 53 Fuselage
- Title in the code table: FUSELAGE, STABILIZER ATTACH FITTINGS
- Service difficulty reports: 573
- FAA code table: https://www.faa.gov/sites/faa.gov/files/JASC_Code.pdf#page=48
- Page: https://openairdocs.org/jasc/5342

## What it covers

For reports of the fittings on the fuselage used for the attachment of the stabilizers

## Service difficulty reports (573, newest 50)

- [SDR REXA2026101601945](https://openairdocs.org/sdr/REXA2026101601945), Sep 18, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. DURING (ET) HFEC INSPECTION ON DRAG ANGLE IAW NRC 252, A CRACK WAS FOUND ON THE AFT DRAG ANGLE BTW 55.62% STR DATUM TO 6 (N296PQ)
- [SDR REXA2026101601944](https://openairdocs.org/sdr/REXA2026101601944), Sep 18, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED FWD DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) ON THE VERTICAL STABILIZER TO FUSELAGE. THE F (N296PQ)
- [SDR REXA2026101601943](https://openairdocs.org/sdr/REXA2026101601943), Sep 18, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED AFT DRAG ANGLE BTWN 55.62% STR DATUM TO 61.56% STR DATUM ON THE VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG AN (N296PQ)
- [SDR REXA2026102001962](https://openairdocs.org/sdr/REXA2026102001962), Sep 2, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED VERTICAL STABILIZER TO FUSELAGE RT AFT DRAG ANGLE BTW, 55.62% DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABI (N479PX)
- [SDR REXA2026102001963](https://openairdocs.org/sdr/REXA2026102001963), Aug 27, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL S (N479PX)
- [SDR REXA2026091401827](https://openairdocs.org/sdr/REXA2026091401827), Aug 8, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. RH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED R/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REP (N549CA)
- [SDR REXA2026091401826](https://openairdocs.org/sdr/REXA2026091401826), Aug 8, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. LH VERTICAL STAB AFT DRAG ANGLE IS CRACKED REMOVED CRACKED DRAG ANGLE AND LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE (N549CA)
- [SDR REXA2026091401825](https://openairdocs.org/sdr/REXA2026091401825), Aug 8, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. LH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REP (N549CA)
- [SDR REXA2026091001786](https://openairdocs.org/sdr/REXA2026091001786), Jul 29, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. RH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67 (N478PX)
- [SDR REXA2026091001785](https://openairdocs.org/sdr/REXA2026091001785), Jul 29, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67 (N478PX)
- [SDR HNAA2026081400700](https://openairdocs.org/sdr/HNAA2026081400700), Jul 11, 2026: Emb EMB145LR. DRAG ANGLE. CRACKED. VERTICAL STAB TO FUSELAGE RH SIDE FWD DRAG ANGLE HAS MULTIPLE CRACKS. RAR THE RH VERTICAL STABILIZER FWD DRAG ANGLE IAW  (N942LL)
- [SDR VNAA202608210008](https://openairdocs.org/sdr/VNAA202608210008), Jul 2, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. CRACK ON FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). FWD DRAG ANGLE APPROX 43.75% MID  (N544EA)
- [SDR AALA202607106503](https://openairdocs.org/sdr/AALA202607106503), Jun 29, 2026: Boeing 737823. ATTACH FITTING. CORRODED. AIRCRAFT IN BASE MAINTENANCE: VERTICAL STAB AFT MOUNT O/B FWD ATTACH FITTING HAS PITTING CORROSION. MAINTENANCE REPLACED (N912AN)
- [SDR VNAA202608210006](https://openairdocs.org/sdr/VNAA202608210006), Jun 28, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). AFT DRAG ANGLE APPROX 43.75% MID  (N544EA)
- [SDR VNAA202608210004](https://openairdocs.org/sdr/VNAA202608210004), Jun 28, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE). CRACK ON AFT DRAG ANGLE APPROX 43 (N544EA)
- [SDR SWAA2026072944661](https://openairdocs.org/sdr/SWAA2026072944661), Jun 25, 2026: Boeing 7377H4. LUG. CORRODED. FOUND SURFACE CORROSION ON AFT FACE OF RT HORIZONTAL STAB CENTER SECTION LOWER LUG, AS PER EA 26-155-01728 THE CONFIGURA (N494WN)
- [SDR SWAA2026072944812](https://openairdocs.org/sdr/SWAA2026072944812), Jun 23, 2026: Boeing 7377H4. LUG. CORRODED. FOUND SURFACE CORROSION ON AFT FACE OF LT HORIZONTAL STAB CENTER SECTION LOWER LUG. AS PER EA 26-155-01709 THE CONFIGURA (N494WN)
- [SDR VNAA20260623033](https://openairdocs.org/sdr/VNAA20260623033), Jun 23, 2026: Cndair CL6002C10. INTERCOSTAL. CORRODED. HN00275235 DISCREPANCY: AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27R AND STGR 26L CORRECTIVE ACTION: REMOVED DESCRE (N518AE)
- [SDR VNAA20260623031](https://openairdocs.org/sdr/VNAA20260623031), Jun 23, 2026: Cndair CL6002C10. INTERCOSTAL. CORRODED. AVI DOOR INTERCOSTAL IS CORRODED AT STGR 26R. REMOVED DESCREPANT DIAPHRAM, LOCATED, DRILLED, SEALED AND INSTALLED NEW SE (N518AE)
- [SDR SWIA2026061976763](https://openairdocs.org/sdr/SWIA2026061976763), Jun 19, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. VERTICAL STAB. RT FWD DRAG ANGLE HAS A POSSIBLE CRACK. EVALUATED AND PERFORMED REPAIR AT VERTICAL STAB. RT FWD DRAG ANGL (N719SK)
- [SDR REXA2026082601654](https://openairdocs.org/sdr/REXA2026082601654), Jun 12, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. (N926XJ)
- [SDR REXA2026082601653](https://openairdocs.org/sdr/REXA2026082601653), Jun 12, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACKED AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. (N926XJ)
- [SDR VNAA202607280002](https://openairdocs.org/sdr/VNAA202607280002), Jun 11, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% RE (N552NN)
- [SDR REXA2026072801191](https://openairdocs.org/sdr/REXA2026072801191), Jun 10, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM  (N929XJ)
- [SDR REXA2026062900987](https://openairdocs.org/sdr/REXA2026062900987), Jun 9, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. THERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ90 (N153PQ)
- [SDR SWIA2026060277686](https://openairdocs.org/sdr/SWIA2026060277686), Jun 2, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. RIGHT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED MX32369431 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT S (N822SK)
- [SDR SWIA2026060277631](https://openairdocs.org/sdr/SWIA2026060277631), Jun 2, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. LEFT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER FWD DRAG ANGLE REPA (N822SK)
- [SDR VNAA202607120004](https://openairdocs.org/sdr/VNAA202607120004), Jun 1, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% (N607NN)
- [SDR VNAA202607120003](https://openairdocs.org/sdr/VNAA202607120003), Jun 1, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% R (N607NN)
- [SDR SWIA2026053177682](https://openairdocs.org/sdr/SWIA2026053177682), May 31, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. RH SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACK MX32358189 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT S (N822SK)
- [SDR SWIA2026052577625](https://openairdocs.org/sdr/SWIA2026052577625), May 25, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. LEFT SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER AFT DRAG ANGLE (N822SK)
- [SDR REXA2026052600612](https://openairdocs.org/sdr/REXA2026052600612), May 23, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. LH FWD DRAG ANGLE IS CRACKED. COMPLIED WITH CRJ900 SRM REPAIR 55-31-00-201-001-A01 ON L/H FWD DRAG ANGLE. (N919XJ)
- [SDR SWIA2026051876877](https://openairdocs.org/sdr/SWIA2026051876877), May 18, 2026: Cndair CL6002C11. DRAG ANGLE. CRACKED. VERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBAR (N796SK)
- [SDR SWIA2026051876876](https://openairdocs.org/sdr/SWIA2026051876876), May 18, 2026: Cndair CL6002C11. DRAG ANGLE. CRACKED. VERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBAR (N796SK)
- [SDR REXA2026060400927](https://openairdocs.org/sdr/REXA2026060400927), May 3, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM  (N909XJ)
- [SDR REXA2026060400926](https://openairdocs.org/sdr/REXA2026060400926), May 3, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (N909XJ)
- [SDR SWIA2026042176430](https://openairdocs.org/sdr/SWIA2026042176430), Apr 21, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. LH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED LT FUSELAGE TO VERTICAL  (N770SK)
- [SDR SWIA2026042176379](https://openairdocs.org/sdr/SWIA2026042176379), Apr 21, 2026: Cndair CL6002C10. DRAG ANGLE. CRACKED. RIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VE (N770SK)
- [SDR VNAA20260418004](https://openairdocs.org/sdr/VNAA20260418004), Apr 18, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0 (N605NN)
- [SDR REXA2026042300310](https://openairdocs.org/sdr/REXA2026042300310), Apr 16, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM (N913XJ)
- [SDR REXA2026051500591](https://openairdocs.org/sdr/REXA2026051500591), Apr 14, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR  (N913XJ)
- [SDR REXA2026051500590](https://openairdocs.org/sdr/REXA2026051500590), Apr 14, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR  (N913XJ)
- [SDR HNAA2025052000424](https://openairdocs.org/sdr/HNAA2025052000424), Apr 7, 2026: Emb EMB145LR. DRAG ANGLE. CRACKED. RIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG A (N655AE)
- [SDR CALA2026040915240](https://openairdocs.org/sdr/CALA2026040915240), Apr 7, 2026: Boeing 737924ER. LUG. CORRODED. LEFT HORIZONTAL STAB LWR AFT ATTACH POINT LUG AFT FACE HAS CORROSION AROUND BUSHING AT THE 6 O'CLOCK POSITION. ATTACH PO (N53441)
- [SDR REXA2026042300315](https://openairdocs.org/sdr/REXA2026042300315), Mar 25, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. INITIAL INSPECTION: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM  (N913XJ)
- [SDR SWIA2026031677389](https://openairdocs.org/sdr/SWIA2026031677389), Mar 16, 2026: Cndair CL6002C10. DRAG ANGLE. BROKEN. VERTICAL STAB RT AFT DRAG ANGLE HAS WORKING FASTENER. REMOVED AND REPLACED FASTENER ON VERTICAL STAB RT AFT DRAG ANGLE R (N611SK)
- [SDR REXA2026050700519](https://openairdocs.org/sdr/REXA2026050700519), Mar 12, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. COMPLETE:  (N138EV)
- [SDR REXA2026050700504](https://openairdocs.org/sdr/REXA2026050700504), Mar 12, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. LEFT VERTI (N138EV)
- [SDR REXA2026050700497](https://openairdocs.org/sdr/REXA2026050700497), Mar 12, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. RIGHT VER (N138EV)
- [SDR REXA2026050500460](https://openairdocs.org/sdr/REXA2026050500460), Mar 7, 2026: Cndair CL6002D24. DRAG ANGLE. CRACKED. CRACK ON RH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER CRACK ON RH FWD AND AFT DRAG ANGLES  (N279PQ)

All 573: https://openairdocs.org/jasc/5342/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 (38,407 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 5324](https://openairdocs.org/jasc/5324): Fuselage Fixed Partitions (40 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 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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