# Service difficulty reports: JASC 5342

A list on [JASC 5342](https://openairdocs.org/jasc/5342.md).

Reports filed under 5342 · Fuselage, Stabilizer Attach Fittings, newest first.

Page 1 of 12 · 573 reports

- [SDR REXA2026101601945](https://openairdocs.org/sdr/REXA2026101601945.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24
  > 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 61.56% STGR DATUM (LT SIDE) AT VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2026101601944](https://openairdocs.org/sdr/REXA2026101601944.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24
  > CRACKED FWD DRAG ANGLE BTW 55.62% STR DATUM TO 61.56% STGR DATUM (LT SIDE) ON THE VERTICAL STABILIZER TO FUSELAGE. THE FWD DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2026101601943](https://openairdocs.org/sdr/REXA2026101601943.md): Drag Angle · cracked · Sep 18, 2026 · N296PQ · Cndair CL6002D24
  > CRACKED AFT DRAG ANGLE BTWN 55.62% STR DATUM TO 61.56% STR DATUM ON THE VERTICAL STABILIZER TO FUSELAGE. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2026102001962](https://openairdocs.org/sdr/REXA2026102001962.md): Drag Angle · cracked · Sep 2, 2026 · N479PX · Cndair CL6002D24
  > CRACKED VERTICAL STABILIZER TO FUSELAGE RT AFT DRAG ANGLE BTW, 55.62% DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2026102001963](https://openairdocs.org/sdr/REXA2026102001963.md): Drag Angle · cracked · Aug 27, 2026 · N479PX · Cndair CL6002D24
  > CRACKED VERTICAL STABILIZER TO FUSELAGE LT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM. THE VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.
- [SDR REXA2026091401827](https://openairdocs.org/sdr/REXA2026091401827.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24
  > RH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED R/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR REXA2026091401826](https://openairdocs.org/sdr/REXA2026091401826.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24
  > LH VERTICAL STAB AFT DRAG ANGLE IS CRACKED REMOVED CRACKED DRAG ANGLE AND LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE L/H VERT. STAB AFT DRAG ANGLE P/N AV670-21186-003 IAW CRJ-900 SRM 51-40-11-001-001-A01, AND 51-42-13/21/22-001-001-A01.
- [SDR REXA2026091401825](https://openairdocs.org/sdr/REXA2026091401825.md): Drag Angle · cracked · Aug 8, 2026 · N549CA · Cndair CL6002D24
  > LH VERTICAL STAB FWD DRAG ANGLE IS CRACKED REPAIRED L/H VERTICAL STAB FWD DRAG ANGLE BY COMPLYING WITH ALL PERMANENT REPAIR STEPS PROVIDED IN CRJ-900 SRM 55-31-00-201-001-A01.
- [SDR REXA2026091001786](https://openairdocs.org/sdr/REXA2026091001786.md): Drag Angle · cracked · Jul 29, 2026 · N478PX · Cndair CL6002D24
  > 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 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR REXA2026091001785](https://openairdocs.org/sdr/REXA2026091001785.md): Drag Angle · cracked · Jul 29, 2026 · N478PX · Cndair CL6002D24
  > 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 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01
- [SDR HNAA2026081400700](https://openairdocs.org/sdr/HNAA2026081400700.md): Drag Angle · cracked · Jul 11, 2026 · N942LL · Emb EMB145LR
  > VERTICAL STAB TO FUSELAGE RH SIDE FWD DRAG ANGLE HAS MULTIPLE CRACKS. RAR THE RH VERTICAL STABILIZER FWD DRAG ANGLE IAW EMB 145 SRM 51-40-02
- [SDR VNAA202608210008](https://openairdocs.org/sdr/VNAA202608210008.md): Drag Angle · cracked · Jul 2, 2026 · N544EA · Cndair CL6002C10
  > CRACK ON FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). FWD DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE) WAS REPAIRED PER CRJ 700 SRM 55-31-00-201-001-A01
- [SDR AALA202607106503](https://openairdocs.org/sdr/AALA202607106503.md): Attach Fitting · corroded · Jun 29, 2026 · N912AN · Boeing 737823
  > AIRCRAFT IN BASE MAINTENANCE: VERTICAL STAB AFT MOUNT O/B FWD ATTACH FITTING HAS PITTING CORROSION. MAINTENANCE REPLACED VERTICAL STAB AFT MOUNT O/B FWD ATTACH FITTING IAW AARD 51-00-05-1.
- [SDR VNAA202608210006](https://openairdocs.org/sdr/VNAA202608210006.md): Drag Angle · cracked · Jun 28, 2026 · N544EA · Cndair CL6002C10
  > CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE). AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (RH SIDE).WAS REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01
- [SDR VNAA202608210004](https://openairdocs.org/sdr/VNAA202608210004.md): Drag Angle · cracked · Jun 28, 2026 · N544EA · Cndair CL6002C10
  > CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE). CRACK ON AFT DRAG ANGLE APPROX 43.75% MID SPAR DATUM AT VERTICAL STABILIZER (LH SIDE) WAS REPAIRED PER CRJ-700 SRM 55-31-00-201-001-A01. PAX DOOR HINGE PN 601R318073-5 WAS
- [SDR SWAA2026072944661](https://openairdocs.org/sdr/SWAA2026072944661.md): Lug · corroded · Jun 25, 2026 · N494WN · Boeing 7377H4
  > FOUND SURFACE CORROSION ON AFT FACE OF RT HORIZONTAL STAB CENTER SECTION LOWER LUG, AS PER EA 26-155-01728 THE CONFIGURATION IS ACCEPTABLE.
- [SDR SWAA2026072944812](https://openairdocs.org/sdr/SWAA2026072944812.md): Lug · corroded · Jun 23, 2026 · N494WN · Boeing 7377H4
  > FOUND SURFACE CORROSION ON AFT FACE OF LT HORIZONTAL STAB CENTER SECTION LOWER LUG. AS PER EA 26-155-01709 THE CONFIGURATION IS ACCEPTABLE.
- [SDR VNAA20260623033](https://openairdocs.org/sdr/VNAA20260623033.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10
  > HN00275235 DISCREPANCY: AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27R AND STGR 26L CORRECTIVE ACTION: REMOVED DESCREPANT INTERCOSTAL, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE P/N(SH670-32075-3S) INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR VNAA20260623031](https://openairdocs.org/sdr/VNAA20260623031.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10
  > AVI DOOR INTERCOSTAL IS CORRODED AT STGR 26R. REMOVED DESCREPANT DIAPHRAM, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE. DIAPHRAM IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01.
- [SDR SWIA2026061976763](https://openairdocs.org/sdr/SWIA2026061976763.md): Drag Angle · cracked · Jun 19, 2026 · N719SK · Cndair CL6002C10
  > VERTICAL STAB. RT FWD DRAG ANGLE HAS A POSSIBLE CRACK. EVALUATED AND PERFORMED REPAIR AT VERTICAL STAB. RT FWD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH 51-900-1002-SKY.
- [SDR REXA2026082601654](https://openairdocs.org/sdr/REXA2026082601654.md): Drag Angle · cracked · Jun 12, 2026 · N926XJ · Cndair CL6002D24
  > CRACKED AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM
- [SDR REXA2026082601653](https://openairdocs.org/sdr/REXA2026082601653.md): Drag Angle · cracked · Jun 12, 2026 · N926XJ · Cndair CL6002D24
  > CRACKED AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. AFT DRAG ANGLE AT RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM
- [SDR VNAA202607280002](https://openairdocs.org/sdr/VNAA202607280002.md): Drag Angle · cracked · Jun 11, 2026 · N552NN · Cndair CL6002D24
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATU
- [SDR REXA2026072801191](https://openairdocs.org/sdr/REXA2026072801191.md): Drag Angle · cracked · Jun 10, 2026 · N929XJ · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ900 SRM
- [SDR REXA2026062900987](https://openairdocs.org/sdr/REXA2026062900987.md): Drag Angle · cracked · Jun 9, 2026 · N153PQ · Cndair CL6002D24
  > THERE IS A POSSIBLE CRACK IN THE RIGHT-HAND VERTICAL STABILIZER DRAG ANGLE. STRIPPED PAINT FROM FWD DRAG ANGLE IAW CRJ900 SRM 51-26-01-001-001-A01. FOUND FWD DRAG ANGLE TO BE VISUALLY CRACKED 2.35"L, REMOVED FASTENERS FOR ACCESS FOR REPAIR IAW SRM 51-42-06-0
- [SDR SWIA2026060277686](https://openairdocs.org/sdr/SWIA2026060277686.md): Drag Angle · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24
  > RIGHT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED MX32369431 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01 SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CARD 51-
- [SDR SWIA2026060277631](https://openairdocs.org/sdr/SWIA2026060277631.md): Drag Angle · cracked · Jun 2, 2026 · N822SK · Cndair CL6002D24
  > LEFT SIDE VERTICAL STABILIZER LOWER FWD DRAG ANGLE IS CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER FWD DRAG ANGLE REPAIR IAW SRM 55-31-00-201-001-A01. COMPLIED WITH SKY CARD 51-900-1003-SKY.
- [SDR VNAA202607120004](https://openairdocs.org/sdr/VNAA202607120004.md): Drag Angle · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FW/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. (ET) HFEC INSPECTION WAS PERFORMED 01 CRACK WAS FOUND ON AFT DRAG ANGLE AND FWD DRAG ANGLE NO CRACKS WERE FOUND. IAW NDT
- [SDR VNAA202607120003](https://openairdocs.org/sdr/VNAA202607120003.md): Drag Angle · cracked · Jun 1, 2026 · N607NN · Cndair CL6002D24
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. REPAIRED PER SRM 55-31-00-201-001-A01
- [SDR SWIA2026053177682](https://openairdocs.org/sdr/SWIA2026053177682.md): Drag Angle · cracked · May 31, 2026 · N822SK · Cndair CL6002D24
  > RH SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACK MX32358189 C-CHECK RO 10132026PERFORMED REPAIR AT RIGHT SIDE VERTICAL STABILIZER LOWER AFT DRAG ANGLE REF CRJ900 SRM 55-31-00-201-001-A01 SEE CONTINUE CARD FOR DETAILS COMPLIED WITH TASK CARD 51-
- [SDR SWIA2026052577625](https://openairdocs.org/sdr/SWIA2026052577625.md): Drag Angle · cracked · May 25, 2026 · N822SK · Cndair CL6002D24
  > LEFT SIDE VERTICAL STABILIZER LOWER DRAG ANGLE HAS SUSPECT CRACKED. COMPLIED WITH LT SIDE VERT STAB LOWER AFT DRAG ANGLE REPAIR IAW SRM 55-31-00-201-001-A01. COMPLIED WITH TASKCARD 51-900-1002-SKY.
- [SDR REXA2026052600612](https://openairdocs.org/sdr/REXA2026052600612.md): Drag Angle · cracked · May 23, 2026 · N919XJ · Cndair CL6002D24
  > LH FWD DRAG ANGLE IS CRACKED. COMPLIED WITH CRJ900 SRM REPAIR 55-31-00-201-001-A01 ON L/H FWD DRAG ANGLE.
- [SDR SWIA2026051876877](https://openairdocs.org/sdr/SWIA2026051876877.md): Drag Angle · cracked · May 18, 2026 · N796SK · Cndair CL6002C11
  > VERT STAB LH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AT VERT STAB LH AFT DRAG ANGLE IAW BOMBARDIER REO 670-55-31-018, REV -A, DATE: 2016-11-10.
- [SDR SWIA2026051876876](https://openairdocs.org/sdr/SWIA2026051876876.md): Drag Angle · cracked · May 18, 2026 · N796SK · Cndair CL6002C11
  > VERT STAB RH AFT DRAG ANGLE IS CRACKED (C-CHECK RO 08/17/2026)PERFORMED REPAIR AFT DRAG ANGLE AT RH VERT STAB IAW BOMBARDIER REO 670-55-31-018 DATE: 2016-11-10, CRJ550 SRM 51-26-01, NDT PERFORMED BY BARON NDT, LLC FAA CRS# 5NDR545D REPORT# S072326-2 DATE INS
- [SDR REXA2026060400927](https://openairdocs.org/sdr/REXA2026060400927.md): Drag Angle · cracked · May 3, 2026 · N909XJ · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT
- [SDR REXA2026060400926](https://openairdocs.org/sdr/REXA2026060400926.md): Drag Angle · cracked · May 3, 2026 · N909XJ · Cndair CL6002D24
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE
- [SDR SWIA2026042176430](https://openairdocs.org/sdr/SWIA2026042176430.md): Drag Angle · cracked · Apr 21, 2026 · N770SK · Cndair CL6002C10
  > LH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED LT FUSELAGE TO VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026042176379](https://openairdocs.org/sdr/SWIA2026042176379.md): Drag Angle · cracked · Apr 21, 2026 · N770SK · Cndair CL6002C10
  > RIGHT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK IN THE RADIUS AREA. REPAIRED RT FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.
- [SDR VNAA20260418004](https://openairdocs.org/sdr/VNAA20260418004.md): Drag Angle · cracked · Apr 18, 2026 · N605NN · Cndair CL6002D24
  > CRACK ON LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LH VERTICAL STABILIZER TO FUSELAGE AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) WAS REPAIRED PER
- [SDR REXA2026042300310](https://openairdocs.org/sdr/REXA2026042300310.md): Drag Angle · cracked · Apr 16, 2026 · N913XJ · Cndair CL6002D24
  > CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-9
- [SDR REXA2026051500591](https://openairdocs.org/sdr/REXA2026051500591.md): Drag Angle · cracked · Apr 14, 2026 · N913XJ · Cndair CL6002D24
  > INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT RH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE
- [SDR REXA2026051500590](https://openairdocs.org/sdr/REXA2026051500590.md): Drag Angle · cracked · Apr 14, 2026 · N913XJ · Cndair CL6002D24
  > INITIAL INSPECTION: CRACKED AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). AFT DRAG ANGLE AT LH STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRAC
- [SDR HNAA2025052000424](https://openairdocs.org/sdr/HNAA2025052000424.md): Drag Angle · cracked · Apr 7, 2026 · N655AE · Emb EMB145LR
  > RIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.
- [SDR CALA2026040915240](https://openairdocs.org/sdr/CALA2026040915240.md): Lug · corroded · Apr 7, 2026 · N53441 · Boeing 737924ER
  > LEFT HORIZONTAL STAB LWR AFT ATTACH POINT LUG AFT FACE HAS CORROSION AROUND BUSHING AT THE 6 O'CLOCK POSITION. ATTACH POINT K. REPAIRED THE LT STAB ATTACH POINT K AND REPLACED BUSHINGS IAW REO-G25884 REV IR AND ECRA 5510-03355.
- [SDR REXA2026042300315](https://openairdocs.org/sdr/REXA2026042300315.md): Drag Angle · cracked · Mar 25, 2026 · N913XJ · Cndair CL6002D24
  > INITIAL INSPECTION: CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DATUM. LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD AND AFT DRAG ANGLE BTW 61.56% STGR DATUM TO 67.5% REAR SPAR DAT
- [SDR SWIA2026031677389](https://openairdocs.org/sdr/SWIA2026031677389.md): Drag Angle · broken · Mar 16, 2026 · N611SK · Cndair CL6002C10
  > VERTICAL STAB RT AFT DRAG ANGLE HAS WORKING FASTENER. REMOVED AND REPLACED FASTENER ON VERTICAL STAB RT AFT DRAG ANGLE REF REO 670-55-31-209 REV -A DATED 2026-05-28COMPLIED WITH 51-900-1002-SKY
- [SDR REXA2026050700519](https://openairdocs.org/sdr/REXA2026050700519.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. COMPLETE: LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER SRM 55-31-00-201- 001
- [SDR REXA2026050700504](https://openairdocs.org/sdr/REXA2026050700504.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24
  > CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 001-A
- [SDR REXA2026050700497](https://openairdocs.org/sdr/REXA2026050700497.md): Drag Angle · cracked · Mar 12, 2026 · N138EV · Cndair CL6002D24
  > CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM. RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM 55-31-00-201- 0
- [SDR REXA2026050500460](https://openairdocs.org/sdr/REXA2026050500460.md): Drag Angle · cracked · Mar 7, 2026 · N279PQ · Cndair CL6002D24
  > 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 ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01

Next page: https://openairdocs.org/jasc/5342/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 = '5342'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5342/reports

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