N519AE

Service difficulty reports · 155

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N519AE' AND registry_match = 'registration'
  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 VNAA2026041315901Selector Valve · faultedGEAR DISAGREE WARNING AFTER HANDLE SELECTED UP. GEAR NEVER MOVED, STAYED DOWN WITH 3 GREEN. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW CRJ 700 AMM 32-32-10-000/400-801-A01. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS FAULT.Apr 9, 2026 · N519AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2025102411101Light · odorELECTRICAL BURNING ODOR IN BETWEEN SEAT 3 AND 8 DF / REMOVED AND REPLACED SIDE WALL LIGHT SEAT 8AC AND 9AC IAW SWPM 20-16-00 AND AMM 33-21-07-000/400-801-A01 OPERATIONAL TEST GOOD. NO BURNING ODOR NOTICED.Oct 21, 2025 · N519AE · Cndair CL6002C10 · Passenger Compartment LightingSDR VNAA20250127007Drag Angle · crackedCRACK ON LH/RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AT BL0.00) LH/RH VERTICAL STABILIZER TO FUSELAGE ATTACHMENT AFT DRAG ANGLE BTW 55.62% STGR DATUM TO 67.5% REAR SPAR DATUM (TRACE AJan 7, 2025 · N519AE · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR VNAA20250127023Attach Angle · corrodedCORROSION ON LOWER ATTACH ANGLE LH / RH AND CENTER, FS 939.00, SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE FAIRING LOWER ATTACH ANGLE LH / RH ON FS 939.00, SUPPORT STRUCTURE, AFT WING-TO-FUSELAGE FAIRING WAS RE-INSPECTED PER CRJ/700 NDTM PART 01 TASK 51-20-009-Jan 6, 2025 · N519AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA20250127012Hinge · corrodedCORROSION ON HINGE AT PASSENGER DOOR, STEP TOP 832ET AND SEVERAL DAMAGES ON FRONT COVER OF THE SAME STEP. PLATE LOGO PAX DOOR AND HINGE AT PASSENGER DOOR, STEP TOP 832ET WERE REPLACED PER CRJ700 SRM 51-41-02-001-001-A01.Jan 6, 2025 · N519AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA20250127006Seat Track · looseIN REFERENCE TO RC TRFKE0065KKK: 670-53-11-210-RH_REV-D-TEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS CAPT/FO'S SEAT TRACKS WERE REPAIRED PER REO 670-53-11-210 REV -D.Jan 6, 2025 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127046Stringer · corrodedCORROSION ON STGR 21RH BTW FS349.00 TO FS379.00 WAS FOUND. ORROSION ON STGR 21RH BTW FS349.00 TO FS379.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-006-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01Dec 27, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127045Stringer · corroded"AFTER REMOVAL OF STGR 26L BTW FS280 TO FS333, CORROSION ON JOINT PIECE STGR WAS FOUND. JOINT PIECE STGR WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01"Dec 27, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127044Floorbeam · crackedN REFERENCE TO RC TRFKE00840RM': EA72-2020-093-SDIR-COCKPIT FLOOR BEAM AND FLOOR WEB - FS250, RBL26.00 ACCOMPLISH A HIGH FREQUENCY EDDY CURRENT (HFEC) INSPECTION FOR CRACK INDICATIONS IN THE AREA OF THE REPAIR PER NDTM PART 1, 51-20-006. T HE COCKOIT FLOOR Dec 23, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20250127043Hinge · wornWEAR ON PAX DOOR HINGE LUG LAND (FUSELAGE SIDE) PAX DOOR HINGE LUG LAND (FUSELAGE SIDE) WAS REPAIRED PER REO 670-53-21-582 REV. - F. ADDITIONAL SPECIFIC AIRWORTHINESS LIMITATIONS (DETAILED VISUAL INSPECTION) ARE NEEDED FOR REPAIR TYPE IV EVERY 5,700 THRESHODec 19, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA20250127042Lug · cracked"CRATCHED ON BORE OF LUG L5 AT LH AILERON. LUG L5 AT LH AILERON WAS REPAIRED PER REO 670-57-61-107 REV - B PAR. 6"Dec 18, 2024 · N519AE · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA20250127040Crossbeam · corroded"CORROSION ON CROSS BEAM UPPER FACE FS1000.00 RBL41 AND CROSS BEAM FS1051.30 RBL40 AT AFT CARGO COMPRTMENT CROSS BEAM UPPER FACE FS1000.00 RBL41 AND CROSS BEAM FS1051.30 RBL40 AT AFT CARGO COMPRTMENT WERE REPAIRED PER REO 670-53-61-2442 REV -- AND REO 670-53-Dec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127039Floor Support · corrodedCORROSION ON FLOOR SILL RH/LH BTW FS969.00 TO FS 1088.20 AT AFT BAGGAGE BAY. CORROSION ON FLOOR SILL RH/LH BTW FS969.00 TO FS 1088.20 AT AFT BAGGAGE BAY WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WERE EVALUATED WITHIN LIMITS PER CRJ700 SRM 53-00-45Dec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127038Floorbeam · corrodedCORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 CORROSION ON FLOOR PANEL SUPPORT ANGLE UPPER FACE AT FS280.00 BTW RBL 9.00 AND LBL 9.00 WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHIN LIMITS PDec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20250127037Seat Track · corrodedCORROSION ON SEAT RAIL LBL9 AND RBL9 (02 SEGMENTS) BTW FS 837.00 TO FS 1005.00 AT PASSENGER CABIN. SEAT RAIL LBL9 AND RBL9 (02 SEGMENTS) BTW FS 837.00 TO FS 1005.00 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-51-49-101-001-A01 AND WERE Dec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127036Seat Track · corrodedORROSION ON LEFT SIDE SEAT RAIL, (1 SEGMENT) BTW FS485 TO FS565, STGR15, LH SIDE SEAT RAIL, (1 SEGMENT) BTW FS485 TO FS565, STGR15, LH WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-31-49-101-001-A01 AND WAS REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03)Dec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127035Seat Track · corrodedCORROSION ON SEAT RAIL (4 SEGMENTS) SEVERAL LOCATIONS RBL / LBL 9.00'' BTW FS581 TO FS830 AT PASSENGER CABIN. SEAT RAIL (4 SEGMENTS) RBL / LBL 9.00'' BTW FS581 TO FS830 AT PASSENGER CABIN WERE EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-51-49-101-001-A01 ANDDec 12, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127034Stringer · corrodedCORROSION ON STGR 24R BTW FS280.00 TO FS310.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 24R BTW FS280.00 TO FS310.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND REPLACED PER CRJ700 SRM 51-42-06-001Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127033Stringer · corrodedCORROSION ON STGR 23R/23L BTW FS280.00 TO FS310.00 AT MAIN AVIONICS COMPARTMENT AREA ON STGR 23L BTW FS280 TO FS295 WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND CORROSION WAS NOT FOUND. CORROSION ON STGR 23L BTW FS295.00 TO FS310.00 AT MAIN AVIONICS CODec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127032Stringer · corrodedCORROSION ON STGR 26L/26R BTW FS280.00 TO FS295.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 26L/26R BTW FS280.00 TO FS295.00 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PER CRJ700 SRM 51-21-06-001-001-A01, EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127031Stringer Splice · corrodedCORROSION ON STGR 25R AND SPLICE (1EA) BTW FS280.00 TO FS364.00 AT MAIN AVIONICS COMPARTMENT. STRINGER 25RH BTW FS 280 TO FS 310 WAS CLEANED PER CRJ700 SRM 51-26-00-001-001-A01 AND AREA WAS INSPECTED PER CRJ700 NDTM 51-20-009-210-A01 AND NO DAMAGES WERE FOUDec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127030Stringer · corrodedCORROSION ON STGR 27 BTW FS280.00 TO FS295.00 AT MAIN AVIONICS COMPARTMENT. CORROSION ON STGR 27 BTW FS280.00 TO FS295.00 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-03-101-002-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-0Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20250127029Intercostal · corrodedCORROSION ON INTERCOSTALS (2EAS) BTW FS349.00 TO FS364.00 AND BTW STGR 26L TO STGR 27 AT MAIN AVIONICS COMPARTMENT. TERCOSTAL (1EA) BTW FS349.00 TO FS364.00 AND STGR 27 AT MAIN AVIONICS COMPARTMENT WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-23-101-003Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127028Joint · corrodedCORROSION ON CIRCUMFERENTIAL JOINT INTERNAL FS280.00 TO FS282.86, BELOW WL72.50, BTW STGR 22L TO 23L, 26L TO 24R, 20R TO 22R AND 17R TO 18R. CORROSION ON CIRCUMFERENTIAL JOINT INTERNAL FS280.00 TO FS282.86, BELOW WL72.50, BTW STGR 22L TO 23L, 26L TO 24R, 20Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127027Seat Track · corrodedCORROSION ON SEAT RAIL LBL 9.00 BTW FS 379 TO FS 485 AT PASSENGER CABIN. SEAT RAIL LBL 9.00 BTW FS 379 TO FS 485 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-21-49-101-001-A01 AND WAS REPLACED PER CRJ700 AMM 53-00-49 (CONFIG A03)Dec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127026Support Fitting · corrodedCORROSION ON RH JACK FITTING SUPPORT BTW FS=265.00 AND FS=280.00 AT MAIN AVIONICS COMPARTMENT. RROSION ON RH JACK FITTING SUPPORT BTW FS=265.00 AND FS=280.00 AT MAIN AVIONICS COMPARTMENT WAS REMOVED PERCRJ700 SRM 51-21-06-001-001-A01 AND WAS EVALUATED WITHINDec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127025Seat Track · corrodedCORROSION ON SEAT RAIL SEVERAL LOCATIONS RBL 9.00 BTW FS485 TO FS581 AT PASSENGER CABIN. SEAT RAIL RBL 9.00 BTW FS485 TO FS581 AT PASSENGER CABIN WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-51-49-101-001-A01 AND WAS REPLACED PER CRJ700 AMM 53-00-49 CONFIDec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127024Floor Support · corroded"CORROSION ON FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL19'' TO RBL 37'' AND LBL 21'' AT FUSELAGE FLOOR STRUCTURE. FLOOR SUPPORTS (4EAS) LOCATED BTW FS=280 TO FS=295 AND RBL19'' TO RBL 37'' AND LBL 21'' AT FUSELAGE FLOOR STRUCTURE WERE EVALUDec 11, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127022Bracket · corrodedCORROSION ON BRACKETS, MACHINED (4EAS) AND PLATE (1E/A) LBL 3.4 OF INTERNAL STRUCTURE AT FWD CARGO MACHINED BRACKETS (4EAS) OF INTERNAL STRUCTURE AT FWD CARGO COMPARTMENT WERE EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-32-58-101-001-A01 AND REPLACED PER CRJ7Dec 10, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127014Counterbalance · damagedNICKS AND WEAR AT FWD/AFT INNER COUNTERBALANCE ARMS OF THE FORWARD BAGGAGE BAY DOOR FWD/AFT INNER COUNTERBALANCE ARMS OF THE FORWARD BAGGAGE BAY DOOR WERE REPAIRED PER REO 670-52-35-289 REV.-ADec 10, 2024 · N519AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA20250127047Plate · corrodedCORROSION ON CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19), HYD PLATES (2EAS) ON LH/RH MAIN WHEEL WELL AND RH MLG HYDRAULIC LINES SUPPORT PLATE (IN BK, LG EXT, LG RET). CORRECTIVE ACTION: CONNECTORS SUPPORT PLATES LH/RH (PX33, PX17, PX34, PX19) MAINDec 8, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127021Door Sill · crackedCORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1051.00, BTW STGR 17LH AND STGR 18LH ORROSION ON AFT CARGO COMPARTMENT DOOR SILL BTW FS 1000.00 TO FS 1051.00, BTW STGR 17LH AND STGR 18LH WAS EVALUATED OUT LIMITS THEREFORE WAS REPLACED PER Dec 8, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127020Support · crackedCRACK ON LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND RBL35/LBL35 AT LH/RH MLG WHEEL WELL LH/RH FAIRING SUPPORT DIAPHRAGM IN STA. FS= 797 TO FS= 807 AND RBL35/LBL35 AT LH/RH MLG WHEEL WELL WERE REPLACED PER CRJ700 SRM 51-41-02-001-001-A01Dec 8, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127019Web · corrodedCRACK ON PREVIOUS REPAIR OF ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00. PREVIOUS REPAIR OF ELECTRICAL BAY FLOOR WEB RIGHT SIDE (BELOW ADG SUPPORT DOUBLER) FS193.00 WAS REPLACED PER CRJ700 SRM 53-11-43-201-001-A01Dec 8, 2024 · N519AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20250127018Door Frame · corrodedCORROSION ON INTERNAL SURROUND STRUCTURE SETTLEMENT AREA OF THE MAIN AVIONICS COMPARTMENT DOOR. INTERNAL SURROUND STRUCTURE SETTLEMENT AREA OF THE MAIN AVIONICS COMPARTMENT DOOR WAS REPAIRED PER REO 690-53-21-032 REV. --.Dec 8, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127017Skin · bulgedPROTUBERANCE ON EXTERNAL SKIN RH SIDE BTW FS202.75 TO FS 210.00 AND STRG 13A TO STRG 12A AT FORWARD FUSELAGE. PROTUBERANCE ON EXTERNAL SKIN RH SIDE BTW FS202.75 TO FS 210.00 AND STRG 13A TO STRG 12A AT FORWARD FUSELAGE WAS EVALUATED PER CRJ700 SRM 53-00-01-Dec 7, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20250127016Landing · crackedCRACK ON RH / LH DOOR LANDING STRUCTURE FS 188.00 (LATCH CUT OUT OF ACCESS DOOR 212AR AND 211AL) RH DOOR LANDING STRUCTURE FS 188.00 WAS REPLACED PER CRJ700 SRM 51-42-10-001-001-A01 AND LH DOOR LANDING WAS FABRICATED AND REPLACED PER DWG CC670-33151 REV-D ADec 6, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA20250127015Access Panel · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB CORROSION ON SETTLEMENT AREA OF ACCESS PANEL 195AB WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-82-55-101-002-A02 AND WAS REPLACED PER CRJ700 SRM 51-42-13-001-001-A01Dec 6, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20250127013Skin · dentedDESCRIPTION: DENT ON FUSELAGE SKIN BTW FS 1069.75 TO FS 1088.20 AND BTW STGR 17RH-16RH AT REAR FUSELAGE. DENT ON FUSELAGE SKIN BTW FS 1069.75 TO FS 1088.20 AND BTW STGR 17RH-16RH AT REAR FUSELAGE WAS REPAIRED PER REO 670-51-00-085 REV - A AND PER REO 670-53Dec 6, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20250127011Skin · erodedERROSION ON SLATS 2,3 AT RH WING. SLAT 3 AT RH WING WAS REPAIRED PER REO 670-57-42-1899 REV. --. SLAT 2 WOULD BE REPLACED UNDER NRC 00030.Dec 5, 2024 · N519AE · Cndair CL6002C10 · Leading Edge DevicesSDR VNAA20250127010Skin · nickedSEVERAL NICKS ON INBOARD FLAP OF INNER FACE AT RH AND LH WING BTWN FLS 15.00/FLS 77.00. SEVERAL NICKS ON INBOARD FLAP OF INNER FACE AT RH AND LH WING BTWN FLS 15.00/FLS 77.00 WERE BLEND OUT PER CRJ700 SRM 51-12-00-001-001-A01 AND WERE EVALUATED WITHINN LDec 5, 2024 · N519AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA20250127009Housing · wornWEAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR. EAR ON EXTERNAL HANDLE HOUSING AT AFT BAGGAGE BAY DOOR WAS REPAIRED PER REO 670-52-31-031 REV. -BDec 5, 2024 · N519AE · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA20250127008Skin · dentedDENT ON OUTER SKIN LOWER AREA AT FWD GALLEY SERVICE DOOROUTER SKIN LOWER AREA AT FWD GALLEY SERVICE DOOR WAS REPAIRED PER REO 670-51-00-085 REV - A AND REO 670-52-41-119 REV - .Dec 5, 2024 · N519AE · Cndair CL6002C10 · Service DoorsSDR VNAA20250127001Seat Track · damagedCAPTAIN SEAT TRACK AFT WEAR STRIP RIVET DAMAGE CAPTAIN SEAT TRACK WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 51-40-11-001-001-A01 AND REPLACED PER CRJ700 SRM 51-42-21-001-001-A01 AND EA A1-670-53-00023 REV -- SECTION III - PERMANENT REPAIR.Dec 5, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127005Skin · dentedDENT DAMAGE TO FUSELAGE SKIN IN RVSM AREA AT FS202.75 AND BETWEEN STRINGER 15R AND 16R DENT DAMAGE TO FUSELAGE SKIN IN RVSM AREA AT FS202.75 AND BETWEEN STRINGER 15R AND 16R WAS REPAIRED PER REO 670-53-11-2072 REV.-ADec 4, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20250127004Bracket · crackedAIR WATER SPRAYER SYSTEM BRACKET RAM AIR WATER SPRAYER SYSTEM BRACKET WAS REPAIRED PER EA 23-C7-21-0435 REV.IR SECTION III - PERMANENT REPAIR AND PER PER REO 670-53-61-2443 REV --. SPECIFIC AIRWOTHINESS LIMITATIONS ARE NEEDED. THE AIRCRAFT MUST NOT BE OPERATEDDec 4, 2024 · N519AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR VNAA20250127003Seat Track · damagedREFERENCE TO RC TRFKE0065KKK: 670-53-11-210-RH_REV-D-TEMP/PERM REPAIR FOR MISSING, LOOSE, OR DAMAGED ALIGNMENT RIVETS AT CAPT/FO'S SEAT TRACKS CAPT/FO'S SEAT TRACKS WERE REPAIRED PER REO 670-53-11-210 REV -D.Dec 4, 2024 · N519AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA20250127002Skin · dentedDENTS ON AFT LOWER FUSELAGE SKIN BTW FS1162.00-55.63% REAR SPAR DATUM AND BTW STR22L-STR22R. DENTS ON AFT LOWER FUSELAGE SKIN BTW FS1162.00-55.63% REAR SPAR DATUM AND BTW STR22L-STR22R WERE REPAIRED PER REO 670-53-71-095 REV. - - AND EA A1-670-53-00054 REV CDec 4, 2024 · N519AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20250127041Lug · corrodedCORROSION ON LUG´S R1, R2, R5 AND R6 AT RH AILERON LUG´S R1, R2, R5 AND R6 AT RH AILERON WERE REPAIRED PER REO 670-57-61-107 REV - B PAR. 6Nov 8, 2024 · N519AE · Cndair CL6002C10 · Wing, Control Surface Attach FittingsSDR VNAA202306051111Light · inoperativeWARDROBE LIGHT HAS A CHAFED WIRE CAUSING A SHORT & CBP1P4 BREAKER TO POP. / REMOVED AND REPLACED WARDROBE LIGHT ASSY IAW CRJ 700 VCMM 25-29-06 FOR THE CHAFFED WIRE. BREAKER STILL POPPED. UPON FURTHER INSPECTION FOUND WIRE TO NOT BE CHAFFED. REMOVED AND REPLACEJun 3, 2023 · N519AE · Cndair CL6002C10 · Passenger Compartment Lighting
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