JASC 5342

Service difficulty reports · 573

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR REXA2026101601945Drag Angle · crackedDURING (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.Sep 18, 2026 · N296PQ · Cndair CL6002D24SDR REXA2026101601944Drag Angle · crackedCRACKED 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.Sep 18, 2026 · N296PQ · Cndair CL6002D24SDR REXA2026101601943Drag Angle · crackedCRACKED 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.Sep 18, 2026 · N296PQ · Cndair CL6002D24SDR REXA2026102001962Drag Angle · crackedCRACKED 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.Sep 2, 2026 · N479PX · Cndair CL6002D24SDR REXA2026102001963Drag Angle · crackedCRACKED 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.Aug 27, 2026 · N479PX · Cndair CL6002D24SDR REXA2026091401827Drag Angle · crackedRH 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.Aug 8, 2026 · N549CA · Cndair CL6002D24SDR REXA2026091401826Drag Angle · crackedLH 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.Aug 8, 2026 · N549CA · Cndair CL6002D24SDR REXA2026091401825Drag Angle · crackedLH 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.Aug 8, 2026 · N549CA · Cndair CL6002D24SDR REXA2026091001786Drag Angle · crackedCRACK 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-A01Jul 29, 2026 · N478PX · Cndair CL6002D24SDR REXA2026091001785Drag Angle · crackedCRACK 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-A01Jul 29, 2026 · N478PX · Cndair CL6002D24SDR HNAA2026081400700Drag Angle · crackedVERTICAL STAB TO FUSELAGE RH SIDE FWD DRAG ANGLE HAS MULTIPLE CRACKS. RAR THE RH VERTICAL STABILIZER FWD DRAG ANGLE IAW EMB 145 SRM 51-40-02Jul 11, 2026 · N942LL · Emb EMB145LRSDR VNAA202608210008Drag Angle · crackedCRACK 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-A01Jul 2, 2026 · N544EA · Cndair CL6002C10SDR AALA202607106503Attach Fitting · corrodedAIRCRAFT 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.Jun 29, 2026 · N912AN · Boeing 737823SDR VNAA202608210006Drag Angle · crackedCRACK 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-A01Jun 28, 2026 · N544EA · Cndair CL6002C10SDR VNAA202608210004Drag Angle · crackedCRACK 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 WASJun 28, 2026 · N544EA · Cndair CL6002C10SDR SWAA2026072944661Lug · corrodedFOUND SURFACE CORROSION ON AFT FACE OF RT HORIZONTAL STAB CENTER SECTION LOWER LUG, AS PER EA 26-155-01728 THE CONFIGURATION IS ACCEPTABLE.Jun 25, 2026 · N494WN · Boeing 7377H4SDR SWAA2026072944812Lug · corrodedFOUND SURFACE CORROSION ON AFT FACE OF LT HORIZONTAL STAB CENTER SECTION LOWER LUG. AS PER EA 26-155-01709 THE CONFIGURATION IS ACCEPTABLE.Jun 23, 2026 · N494WN · Boeing 7377H4SDR VNAA20260623033Intercostal · corrodedHN00275235 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-A01Jun 23, 2026 · N518AE · Cndair CL6002C10SDR VNAA20260623031Intercostal · corrodedAVI 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.Jun 23, 2026 · N518AE · Cndair CL6002C10SDR SWIA2026061976763Drag Angle · crackedVERTICAL 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.Jun 19, 2026 · N719SK · Cndair CL6002C10SDR REXA2026082601654Drag Angle · crackedCRACKED 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 SRMJun 12, 2026 · N926XJ · Cndair CL6002D24SDR REXA2026082601653Drag Angle · crackedCRACKED 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 SRMJun 12, 2026 · N926XJ · Cndair CL6002D24SDR VNAA202607280002Drag Angle · crackedCRACK 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 DATUJun 11, 2026 · N552NN · Cndair CL6002D24SDR REXA2026072801191Drag Angle · crackedCRACK 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 Jun 10, 2026 · N929XJ · Cndair CL6002D24SDR REXA2026062900987Drag Angle · crackedTHERE 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 51-42-06-0Jun 9, 2026 · N153PQ · Cndair CL6002D24SDR SWIA2026060277686Drag Angle · crackedRIGHT 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-Jun 2, 2026 · N822SK · Cndair CL6002D24SDR SWIA2026060277631Drag Angle · crackedLEFT 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.Jun 2, 2026 · N822SK · Cndair CL6002D24SDR VNAA202607120004Drag Angle · crackedCRACK 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 Jun 1, 2026 · N607NN · Cndair CL6002D24SDR VNAA202607120003Drag Angle · crackedCRACK 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-A01Jun 1, 2026 · N607NN · Cndair CL6002D24SDR SWIA2026053177682Drag Angle · crackedRH 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-May 31, 2026 · N822SK · Cndair CL6002D24SDR SWIA2026052577625Drag Angle · crackedLEFT 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.May 25, 2026 · N822SK · Cndair CL6002D24SDR REXA2026052600612Drag Angle · crackedLH FWD DRAG ANGLE IS CRACKED. COMPLIED WITH CRJ900 SRM REPAIR 55-31-00-201-001-A01 ON L/H FWD DRAG ANGLE.May 23, 2026 · N919XJ · Cndair CL6002D24SDR SWIA2026051876877Drag Angle · crackedVERT 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.May 18, 2026 · N796SK · Cndair CL6002C11SDR SWIA2026051876876Drag Angle · crackedVERT 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 INSMay 18, 2026 · N796SK · Cndair CL6002C11SDR REXA2026060400927Drag Angle · crackedCRACK 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 ATMay 3, 2026 · N909XJ · Cndair CL6002D24SDR REXA2026060400926Drag Angle · crackedCRACK 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 May 3, 2026 · N909XJ · Cndair CL6002D24SDR SWIA2026042176430Drag Angle · crackedLH 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.Apr 21, 2026 · N770SK · Cndair CL6002C10SDR SWIA2026042176379Drag Angle · crackedRIGHT 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.Apr 21, 2026 · N770SK · Cndair CL6002C10SDR VNAA20260418004Drag Angle · crackedCRACK 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 Apr 18, 2026 · N605NN · Cndair CL6002D24SDR REXA2026042300310Drag Angle · crackedCRACK 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-9Apr 16, 2026 · N913XJ · Cndair CL6002D24SDR REXA2026051500591Drag Angle · crackedINITIAL 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 Apr 14, 2026 · N913XJ · Cndair CL6002D24SDR REXA2026051500590Drag Angle · crackedINITIAL 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 (TRACApr 14, 2026 · N913XJ · Cndair CL6002D24SDR HNAA2025052000424Drag Angle · crackedRIGHT VERTICAL STABILIZER DRAG ANGLE HAS POSSIBLE CRACK AT FRAME 78. REMOVED AND REPLACED RT VERTICAL TO FUSELAGE DRAG ANGLE IAW SRM 51-40-02.Apr 7, 2026 · N655AE · Emb EMB145LRSDR CALA2026040915240Lug · corrodedLEFT 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.Apr 7, 2026 · N53441 · Boeing 737924ERSDR REXA2026042300315Drag Angle · crackedINITIAL 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 DATMar 25, 2026 · N913XJ · Cndair CL6002D24SDR SWIA2026031677389Drag Angle · brokenVERTICAL 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-SKYMar 16, 2026 · N611SK · Cndair CL6002C10SDR REXA2026050700519Drag Angle · crackedCRACK 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- 001Mar 12, 2026 · N138EV · Cndair CL6002D24SDR REXA2026050700504Drag Angle · crackedCRACK 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-AMar 12, 2026 · N138EV · Cndair CL6002D24SDR REXA2026050700497Drag Angle · crackedCRACK 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- 0Mar 12, 2026 · N138EV · Cndair CL6002D24SDR REXA2026050500460Drag Angle · crackedCRACK 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-A01Mar 7, 2026 · N279PQ · Cndair CL6002D24
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