JASC 5342

Service difficulty reports · 578

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 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 CL6002D24SDR REXA2026050500459Drag Angle · crackedCRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER CRACK ON LH FWD AND AFT DRAG ANGLES ON 67.5% REAR SPAR DATUM AT VERTICAL STABILIZER WERE REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01Mar 7, 2026 · N279PQ · Cndair CL6002D24SDR REXA2026050400434Drag Angle · crackedCRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-A01Mar 6, 2026 · N676CA · Cndair CL6002D24SDR REXA2026050400433Drag Angle · crackedCRACK ON VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB RH FACE TO FUSELAGE FWD/AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER CRJ900 SRM 55-31-00-201-00Mar 6, 2026 · N676CA · Cndair CL6002D24SDR REXA2026050400428Drag Angle · crackedCRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED PER SRM 55-31-00-201-001-AMar 6, 2026 · N676CA · Cndair CL6002D24SDR REXA2026050400427Drag Angle · crackedCRACK ON VERTICAL STAB LH FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) VERTICAL STAB LT FACE TO FUSELAGE FWD. AFT DRAG ANGLE BTW STRG DATUM 37.81 & RS 23.11 (TRACE AT BL 0.00) WAS REPAIRED IAW SRM 55-31-00-201-001-Mar 6, 2026 · N676CA · Cndair CL6002D24SDR REXA2026042800392Drag Angle · crackedCRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). CRACKED FWD AND AFT DRAG ANGLE AT RIGHT STABILIZER TO FUSELAGE ATTACHMENT BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATFeb 26, 2026 · N297PQ · Cndair CL6002D24SDR SWAA2026031972305Fitting · corrodedCORRODED LOWER LUG FITTING, AFT FACE OF LT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING LOCATED AFT FACE POSITION LT HORIZONTAL STAB IAW 26-155-00498-WIP1, 26-155-00498-WIP2, 26-155-00498-WIP3, 26-155-00498-WIP4, 26-155-00498-WIP5, & EA 26-155-00498.Feb 19, 2026 · N463WN · Boeing 7377H4SDR SWAA2026031972306Fitting · corrodedCORRODED LOWER LUG FITTING, AFT FACE POSITION OF THE RT HORIZONTAL STAB. REPAIRED LOWER LUG FITTING ON THE RT HORIZONTAL STAB IAW 26-155-00499-WIP1, 26-155-00499-WIP2, 26-155-00499-WIP3, 26-155-00499-WIP4, AND EA 26-155-00499.Feb 19, 2026 · N463WN · Boeing 7377H4SDR SWIA2026021376161Drag Angle · crackedVERTICAL STAB LEFT DRAG ANGLE SHOWS SIGN OF POSSIBLE CRACK. REPAIRED LT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01.Feb 13, 2026 · N716SK · Cndair CL6002C10SDR VNAA202603130002Drag 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). CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATFeb 3, 2026 · N635NN · Cndair CL6002D24SDR VNAA2026031310001Drag 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). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM Feb 3, 2026 · N635NN · Cndair CL6002D24SDR VNAA20260304009Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT RH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) REPAIRED PER CRJ900 SRM 55-31-00-201-001-A01Jan 27, 2026 · N604NN · Bombdr CL6002D15SDR N6WA2026012803Mount · damagedHORIZONTAL STAB RT UPPER FITTING MOUNT HOLES ARE DAMAGED. REPAIRED RT UPPER FITTING MOUNT HOLES IAW EO-C550-55MR-007.Jan 26, 2026 · N688SK · Cndair CL6002C11SDR VNAA20260304001Drag Angle · crackedCRACK ON VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT LH DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) DRAG ANGLE WAS REPAIRED PER SRM 55-31-00-201-001-A01Jan 22, 2026 · N604NN · Bombdr CL6002D15SDR REXA2026030900202Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJan 13, 2026 · N272PQ · Cndair CL6002D24SDR VNAA20260303006Drag Angle · crackedCRACKED LT AFT DRAG ANGLE BETWEEN UNION OF FUSELAGE AND VERTICAL STABILIZER. 67.5% REAR SPAR DATUM. THE AFT DRAG ANGLE WAS REPAIRED IAW SRM 55-31-00-201-001-A01.Jan 11, 2026 · N602NN · Bombdr CL6002D15SDR SWIA2026011075991Drag Angle · crackedLT VERTICAL STAB AFT DRAG ANGLE SHOWS EVIDENCE OF CRACKING. REMOVED AND REPLACED L/H VERTICAL STAB AFT DRAG ANGLE WITH NEW DRAG ANGLE IAW CRJ 700 SRM 51-42-13-001-001-A01.Jan 10, 2026 · N795SK · Cndair CL6002C10SDR SWIA2026011075984Drag Angle · crackedRH VERTICAL STAB AFT DRAG ANGLE SHOWS EVIDENCE OF CRACKING. REMOVED AND REPLACED RT VERTICAL STAB AFT DRAG ANGLE WITH NEW DRAG ANGLE P/N AV670-21186-004 IAW CRJ 700 SRM 51-42-21-001-001-A01Jan 10, 2026 · N795SK · Cndair CL6002C10SDR SWIA2026030975469Drag Angle · crackedRH FUSELAGE - TO - VERTICAL STAB AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 03/07/2026)INSTALLED NEW RH AFT DRAG ANGLE REF CRJ700 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SRM 51-42-22-001-001-A01 AND DWG#BA670-35002 REV-F. COMPLIJan 6, 2026 · N779SK · Cndair CL6002C11SDR SWIA2026010675460Drag Angle · crackedLH FUSELAGE - TO - VERTICAL STAB AFT DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 03/07/2026)VERIFIED LH FUSELAGE TO VERTICAL STAB AFT DRAG ANGLE CRACKED. REMOVED LH AFT DRAG ANGLE REF CRJ700 51-42-21-001-001-A01, CRJ700 SRM 51-42-13-001-001-A01, CRJ700 SJan 6, 2026 · N779SK · Cndair CL6002C11SDR SWIA2026010675459Drag Angle · crackedLH FUSELAGE - TO - VERTICAL STAB FORWARD DRAG ANGLE POSSIBLE CRACK (MARKED) (C-CHECK RO 03/07/2026)VERIFIED VERTICAL STAB FORWARD DRAG ANGLE CRACK, REPAIRED REF CRJ 550 SRM CRJ550 SRM 55-31-00-201-001-A01 AND REO 670-55-31-203 REV -- DATE 2026-01-29. SEE CJan 6, 2026 · N779SK · Cndair CL6002C11SDR SWIA2025122876590Drag Angle · crackedRT VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE SHOWS POSSIBLE CRACK. REMOVED, CRACKED RIGHT, AFT DRAG ANGLE ON THE VERTICAL STAB, AND INSTALLED SERVICABLE DRAG ANGLE. SRM 51-42-21-001-001-A01 REV 38, SRM 51-42-13-001-001-A01 REV. 38, SRM 51-42-22-001-001-A01 REDec 28, 2025 · N813SK · Cndair CL6002D24SDR VNAA20260201006Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUMS. CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.62% STGR DATUM TO STGR DATUM TO 67.5%Dec 16, 2025 · N632NN · Bombdr CL6002D15SDR VNAA20260201005Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/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 SPARDec 16, 2025 · N632NN · Bombdr CL6002D15SDR VNAA20251216019Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BLO.00). DRAG ANGLE REPAIRED PER CRJ-900 SRM 55-31-00-201-001-A01Dec 16, 2025 · N634NN · Cndair CL6002D24SDR VNAA20251216018Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % REAR SPAR DATUM (TRACE AT BL 0). CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLES BTW 55.625 % STRG DATUM TO 67.5 % READec 16, 2025 · N634NN · Cndair CL6002D24SDR REXA2026052600664Drag Angle · crackedCRACK ON LEFT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LEFT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00)Dec 14, 2025 · N176PQ · Cndair CL6002D24SDR REXA2026052600663Attach Angle · crackedCRACK ON RIGHT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) RIGHT STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.Dec 14, 2025 · N176PQ · Cndair CL6002D24SDR VNAA20260125007Drag Angle · crackedCRACKED LEFT VERTICAL STAB TO AFT FUSELAGE ATTACHMENT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM. LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.625% STGR DATUM TO STGR DATUM TO 67.5% REAR SPAR DATUM WAS REDec 9, 2025 · N601EN · Bombdr CL6002D15SDR SWIA2026070676519Drag Angle · crackedLH VERTICAL STAB - TO - FUSELAGE AFT DRAG ANGLE POSSIBLE CRACK. REMOVED, CRACKED LEFT, AFT DRAG ANGLE ON THE VERTICAL STAB., AND INSTALLED SERVICABLE DRAG ANGLE. IAW SRM 51-42-21-001-001-A01, REV. 38, SRM 51-42-13-001-001-A01 REV. 38, SRM 51-42-22-001-001Nov 25, 2025 · N813SK · Cndair CL6002D24SDR SWIA2025112576494Drag Angle · crackedRIGHT VERTICAL STAB - TO - FUSELAGE FWD DRAG ANGLE POSSIBLE CRACK. REMOVED DAMAGE FROM THE RIGHT FORWARD VERTICAL STAB. DRAG ANGLE, FABRICATED AND INSTALLED REPAIR PARTS. REF. SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.Nov 25, 2025 · N813SK · Cndair CL6002D24SDR DALA2025112108504Skin · damagedNOTED DAMAGE TO SKIN AFT OF RUDDER (M)(P). SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 001-0233:2721-2001/001 00405 COMPLIED WITH PRI 629357 REV 0, 1, AND ERA 629357-14 REV B.Nov 19, 2025 · N133DU · Airbus BD5001A10SDR SWIA2025110675250Drag Angle · crackedRIGHT VERTICAL STAB TO FUSELAGE, AFT DRAG ANGLE HAS POSSIBLE CRACK AT THE AFT END. REPAIRED THE CRACKED DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY. NO DEFECTS NOTED.Nov 6, 2025 · N758EV · Cndair CL6002C10SDR REXA2025121201037Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUOct 31, 2025 · N292PQ · Cndair CL6002D24SDR REXA2025121201036Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00). RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DAOct 31, 2025 · N292PQ · Cndair CL6002D24SDR REXA2026051200539Drag Angle · crackedCRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM CRACK ON LH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUMOct 29, 2025 · N908XJ · Cndair CL6002D24SDR REXA2026051200538Attach Angle · crackedCRACK ON RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD & AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 61.56% STRG DATUM TO 67.5% REAR SPAR DATUM WAS REPAIRED PER CRJ-900 SRM Oct 29, 2025 · N908XJ · Cndair CL6002D24SDR VNAA20251204010Drag Angle · crackedCRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM. CORRECTIVE ACTION: CRACK ON RIGHT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SOct 29, 2025 · N629NN · Bombdr CL6002D15SDR VNAA20251204011Drag Angle · crackedCRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REAR SPAR DATUM DATUM. CORRECTIVE ACTION: CRACK ON LEFT VERTICAL STABILIZER TO FUSELAGE ATTACHMENT FWD/AFT DRAG ANGLE BTW 55.625% STGR DATUM TO 67.5% REOct 27, 2025 · N629NN · Bombdr CL6002D15SDR REXA2025110600980Drag Angle · crackedLEFT AFT DRAG ANGLE APPEARS CRACKED. REMOVED SURFACE FINISH IAW SRM 51-26-01-001-001-A01 & TS012487A. ON FURTHER EVALUATION FOUND LT AFT DRAG ANGLE TO BE CRACKED & REQUIRES REPAIR OR REPLACED. REMOVED DAMAGED LT AFT DRAG ANGLE IAW SRM 51-42-13-001-001-A01. SOct 26, 2025 · N915XJ · Cndair CL6002D24SDR REXA2025110600979Drag Angle · crackedLEFT FWD DRAG ANGLE APPEARS TO BE CRACKED. INSTALLED REPAIR PARTS ON LT FWD DRAG ANGLE AND COMPLIED WITH ALL STEPS OF CRJ900 SRM 55-31-00-201-001-A01Oct 26, 2025 · N915XJ · Cndair CL6002D24SDR HNAA2025112500823Drag Angle · crackedVERTICAL STABILIZER LH FWD DRAG ANGLE CRACKED. REMOVED AND REPLACED CRACKED VERTICAL STABILIZER LH FWD DRAG ANGLE IAW EMB145 SRM 51-40-02 AND INFORMATION CONTAINED IN SRM 53-31-01RE, ITEM 11, FIG 219.Oct 24, 2025 · N906AE · Emb EMB145LRSDR VNAA20251015050Drag Angle · crackedVERTICAL STAB RH DRAG ANGLE IS CRACKED (PREVIOUSLY REPAIRED AREA) CORRECTIVE ACTION: REPAIRED RH DRAG ANGLE IAW MHIRJ REO 670-55-31-188 REV -- DATED: 2025-03-04 AND BOMBARDIER REO 670-55-31-018 REV -A DATED: 2016-11-10.Oct 16, 2025 · N501BG · Cndair CL6002C10SDR HNAA2025112000770Drag Angle · crackedF077360 VERTICAL STABILIZER LH DRAG ANGLE HAS POSSIBLE CRACK AT FR 76. REMOVED CRACKED VERTICAL STABILIZER LH DRAG ANGLE AT FR 76 IAW EMB145 SRM 51-40-02 AND SRM 51-20-03 AND INSTALLED SERVICEABLE VERTICAL STABILIZER LH DRAG ANGLE AT FR 76. IAW EMB 145 SRM 53Oct 12, 2025 · N900AE · Emb EMB145LRSDR SWIA202512261004Drag Angle · crackedLEFT FWD VERTICAL STAB DRAG ANGLE CRACKED. PERFORMED REPAIR ON LT FWD VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY.Oct 4, 2025 · N820SK · Cndair CL6002D24
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