N526EA

Service difficulty reports · 112

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 = 'N526EA' 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 VNAA2026050417103Hinge · misinstalledGEAR DISAGREE WARNING MSG. T/S & FOUND ALL 3 GEAR TO CYCLE PROPERLY WITH THE NLG AFT DOOR DISCONNECTED UPON FURTHER INVESTIGATION FOUND NLG AFT DOOR LT UPPER HINGE LUG (AIRFRAME SIDE) TO BE INSTALLED UPSIDE DOWN WHICH CAUSED THE HINGE BUSHINGS TO CRACK/BREAK Apr 29, 2026 · N526EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202509260016Drag Angle · damagedELONGATE HOLES ON VERTICAL STABILIZER UNDER RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM. RH FWD DRAG ANGLE BTW 55.62% STGR DATUM TO 61.56% STGR DATUM WAS REPAIRED PER REO 670-55-31-196 REV.-ASep 4, 2025 · N526EA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous StructureSDR VNAA202509250011Hinge · not reportedPERM REPAIR - PASSENGER DOOR SURROUND STRUCTURE - HINGE REPLACEMENT REPLACE THE PASSENGER DOOR HINGE IN ACCORDANCE WITH CRJ700 SRM TASK 53-21-23-201-007- A01. PIANO HINGE OF PASSENGER DOOR WAS REPLACED PER CRJ700 SRM 53-21-23-201-007-A01Sep 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202509260014Frame Angle · corrodedAFTER ANGLE REINFORCING REMOVAL IN REF NRC 00238, CORROSION ON ANGLE REINFORCING OF FRAME FS879 WAS FOUND. CORROSION WAS REMOVED ON ANGLE REINFORCING OF FRAME FS879 PER CRJ-700 SRM 51-21-06-001-001-A01, EVALUATED OUT LIMTS PER CRJ-700 SRM 53-51-06-101-003-A01Aug 23, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202509260018Crossbeam · corrodedCORROSION WAS FOUND ON LH CROSSBEAM AT FS 280.00. LH CROSSBEAM AT FS280.00 WAS EVALUATED OUT OF LIMITS PER CRJ700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ700 SRM 51-42-06-001-001-A01, SRM 51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01.Aug 15, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202509260013Frame · corrodedAFTER DUCTS REMOVAL IN REF NRC 00236, CORROSION ON FRAME FS969 BTW STGR 26L TO 26R AT INTERNAL FUSELAGE. FRAME FS969 BTW STGR 26L TO 26R AT INTERNAL FUSELAGE. WAS REPLACED PER CRJ 700 SRM 51-42-06-001-001-A01 . AND SRM 51-42-21-001-001-A01.Aug 15, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202509260010Stringer · wornWEAR ON STGR 8 BTW FS1144 TO FS1162 AT AFT EQUIPMENT BAY. WEAR ON STGR 8 BTW FS1144 TO FS1162 AT AFT EQUIPMENT BAY WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-61-03-101-004-A01 AND WAS REPAIRED PER CRJ-700 SRM 53-00-03-201-002-A01.Aug 15, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202509260007Hinge Fitting · wornNICKS ON LUGS OF AILERON HINGE 2 (INB/OUTB LUGS) AND HINGE 3 (INB LUG) AT LH WING REAR SPAR. DAMAGED LUGS OF AILERON HINGE 2 (INB/OUTB LUGS) AND HINGE 3 (INB LUG) AT LH WING REAR SPAR WERE REPAIRED PER REO 670-57-51-629 REV - -.Aug 15, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260012Fitting · corrodedAFTER REMOVAL OF CROSSBEAM, CORROSION WAS FOUND ON FLOOR FITTING BTW INTERCOSTAL RBL 15 - RBL 17 AND BTW FS 280 -295. DUE TO EXCESSIVE DAMAGE ON FLOOR FITTING BTW INTERCOSTAL RBL 15 - RBL 17 AND BTW FS 280 -295 WAS FOUND OUT OF LIMITS PER CRJ700 SRM 53-00-00-Aug 14, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202509260011Hinge Fitting · damagedSTANDARD BUSHING FITS FREELY BORE LUG L5 CENTER HINGE AT LH AILERON ASSY. BORE LUG L5 CENTER HINGE AT LH AILERON ASSY WAS REPAIRED PER REO 670-57-61-237 REV. - -Aug 14, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260008Hinge Fitting · corrodedCORROSION ON BORE LUGS: L1 AND L2 CENTER HINGE 2 AT LH AILERON ASSY. BORE LUGS: L1 AND L2 CENTER HINGE 2 AT LH AILERON ASSY WERE REPAIRED PER REO 670-57-61-237 REV. - -Aug 14, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260006Bushing · wornAFTER REMOVAL BUSHINGS, WEAR ON OUTBOARD FACE OF LUGS R5, R6 OF CENTER HINGE FITTING AT RH AILERON. WEAR ON OUTBOARD FACE OF LUGS R5, R6 OF CENTER HINGE FITTING AT RH AILERON. WERE REPAIRED PER REO. 670-57-61-237 REV - -Aug 14, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260005Hinge Fitting · corrodedCORROSION ON BORE LUG # R1, R2, R4, R5, R6 OF CENTER HINGE FITTING AT RH AILERON. BORE LUG # R1, AND R4, WERE CLEANED PER CRJ700 SRM 51-26-00-001-001-A01, NO CORROSION WAS FOUND AND BORE LUG # R2, R5 AND R6 OF CENTER HINGE FITTING AT RH AILERON WERE REPAIRED Aug 14, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260004Hinge Fitting · corrodedCORROSION ON NLG DOOR INTERNAL HOLES OF HINGE FITTINGS (2EAS) LH/RH AT FUSELAGE STRUCTURE WAS FOUND. CORROSION ON NLG DOOR INTERNAL HOLES OF HINGE FITTINGS (2EAS) LH/RH AT FUSELAGE STRUCTURE WERE EVALUATED OUT OF LIMITS PER CRJ-900 SRM 51-10-06-001-001-A01 ANAug 14, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA202509250018Skin · corrodedCORROSION ON SETTLEMENT AREA OF ACCESS 832FL, 832EL, 832DL, 832CL, 832BL, 832AL, 832AR, AT PASSENGER DOOR. SETTLEMENT AREA ON ACCESS PANELS 832EL, 832DL, 832CL, 832BL, 832AL, 832AR WERE BLEND OUT, MEASURED WITHIN LIMITS PER CRJ-700 SRM 52-11-01-101-001-A01, 5Aug 14, 2025 · N526EA · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202509260003Hinge Fitting · gougedAFTER AILERON REMOVAL IN REF CARD 57-60-203_R/H-JIC, GOUGES ON LUG R4 CENTER HINGE FITTING AT RH AILERON. GOUGES ON LUG R4 CENTER HINGE FITTING AT RH AILERON. WERE REPAIRED PER REO 670-57-61-451 REV. - -Aug 13, 2025 · N526EA · Cndair CL6002C10 · AileronsSDR VNAA202509260002Brake · corrodedDURING REMOVAL OF MLG RH SHOCK STRUCT IN REFERENCE TASK CARD:32-079-003-19-RH CORROSION WAS FOUN ON BRAKE TAKE OUT RINK MLG RH. PIN, BRAKE TORQUE TAKE-OUT MLG RH WAS VERIFIED (P/N:49231-3 S/N: ACR110787) PER CRJ 700 IPC 32-11-39 AND MUST BE INSTALLED WITH JOBAug 12, 2025 · N526EA · Cndair CL6002C10 · Landing Gear Brake SystemSDR VNAA202509260001Skin · mechanic errorLH PYLON ACCESS PANEL 412HB MISDRILLED. GENERATE NEW RFTS REQUEST AND PROVIDE A DETAILS DAMAGE REPORT REQUESTING PERMANENT DISPOSITION. LT PYLON ACCESS PANEL 412HB MISDRILL WAS REPAIRED PER REO 670-54-51-084 REV.--Aug 12, 2025 · N526EA · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR VNAA202509260019Floorbeam · corrodedAFTER REMOVAL OF FLOOR PANEL SUPPORT ANGLE, CORROSION WAS FOUND ON RH CROSSBEAM AT FS 280.00. CORROSIÓN ON RH CROSSBEAM AT FS 280 ITS OUT OF LIMITS PER CRJ-700 SRM 53-00-01-101-001-A01 AND WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 SRM 51-42-10-001-0Aug 11, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202509260017Seat Track · corrodedCORROSION ON SEAT RAIL AT RBL9 (02) SEGMENTS: (01) FS679 - FS863. (02) FS863 - FS1005. OF THE PAX CABIN. SEAT RAILS (2EAS) AT RBL9 FS=679 TO FS=1005. OF THE PAX CABIN WERE EVALUATE OUT LIMITS PER CRJ 700 SRM 53-41-49-101-001-A01 AND CRJ 700 SRM 53-51-49-101-0Aug 11, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509260015Support Channel · damagedELONGATE HOLES ON LOWER CHANNEL FOUND AT RH RUDDER-PEDAL FRONT PIVOT SUPPORT STRUCTURE. LOWER CHANNEL AT RH RUDDER-PEDAL FRONT PIVOT SUPPORT STRUCTURE WAS REPAIRED PER REO 670-53-11-2175 REV.-Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250033Crossbeam · corrodedCORROSION ON CROSS BEAM ON FS1051.30 BTW LBL28 TO LBL39 AT BAGGAGE BAY FLOOR STRUCTURE. CROSS BEAM ON FS1051.30 BTW LBL28 TO LBL39 AT BAGGAGE BAY FLOOR STRUCTURE WAS REPAIRED PER REO 670-53-61-2549 REV -Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250032Floor Support · corrodedCORROSION ON FLOOR BEAM BTW FS985.00 TO FS1088.20 AND LBL27 AT AFT BAGGAGE BAY FLOOR STRUCTURE. DUE TO NO DAMAGE IS ALLOWED ON FLOOR BEAM BTW FS 1008 TO FS 1080 AND LBL 27 AT AFT BAGGAGE BAY FLOOR STRUCTURE WAS REPLACED PER SRM 53-61-43-101-001-A01 AND SRM 5Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250031Floor Support · corrodedCORROSION ON FLOOR BEAM BTW FS985.00 TO FS1088.20 AND LBL9 AT AFT BAGGAGE BAY FLOOR STRUCTURE. DUE TO NO DAMAGE IS ALLOWED ON FLOOR BEAM BTW FS 985.00 TO FS 1088.20 AND LBL 9 AT AFT BAGGAGE BAY FLOOR STRUCTURE WAS REPLACED PER CRJ700 SRM 53-61-43-101-001-A01Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250030Frame · corrodedCORROSION ON FRAME BTW FS909 STGR 26R TO STGR 26L AT INTERNAL FUSELAGE. CORROSION ON FRAME BTW FS909 STGR 26R TO STGR 26L AT INTERNAL FUSELAGE WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01. AND AREA OUT LIMITS PER CRJ-700 SRM 53-00-00-101-001-A01 AND WAS Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Structure (General)SDR VNAA202509250029Frame · corrodedCORROSION ON FRAME BTW FS 879 STGR 26R TO STGR 26L AT INTERNAL FUSELAGE. CORROSION ON FRAME BTW FS 879 STGR 26R TO STGR 26L AT INTERNAL FUSELAGE WAS EVALUATE OUT OF LIMITS PER CRJ-700 SRM 53-51-06-101-003-A01 AND REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202509250028Static Wick · corrodedCORROSION AT STATIC DICHARGER BASE, ACCESS PANEL 343BR. STATIC DICHARGER BASE ON ACCESS PANEL 343BR WAS REPLACED PER CRJ700 AMM 55-00-28-960-801 (CONFIG A01) AND SRM 51-42-06-001-001-A01Aug 7, 2025 · N526EA · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202509250027Frame · corrodedCORROSION ON FRAME BTW FS 863 STGR 26R TO STGR 26L AT INTERNAL FUSELAGE. FRAME BTW FS 863 STGR 21R TO STGR 21L AT INTERNAL FUSELAGE WAS EVALUATED OUT LIMITS PER CRJ-700 SRM 53-00-00-101-001-A01 AND FRAME WAS REPLACED PER CRJ/700 SRM 51-42-21-001-001-A01 AND Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202509250026Floor Support · crackedCRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE (FLIGHT COMPARTMENT FLOOR STRUCTURE BELOW WL79.50). CRACK ON FLOOR BEAM RBL 12.0 BTW FS 221.73 TO FS 229.00 AT FWD FUSELAGE INTERNAL STRUCTURE WAS REPAIRED PER 670-53-1Aug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250025Floor Support · corrodedCORROSION ALONG EXTERNAL FACE OF FLOOR SILL BTW FS1000-FS1051.30 AT SURROUND STRUCTURE OF AFT BAGGAGE-BAY DOOR. DUE TO EXCESSIVE CORROSION MUST BE REPLACED PER CRJ 700 SRM 51-21-06-001-001-A01 AND SILL, LOWER BTW FS1000-FS1051.30 AT SURROUND STRUCTURE OF AFTAug 7, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250038Support Angle · crackedCRACK ON SUPPORT ANGLES OF PANEL 542AZ/642AZ AT LH/RH MLG SHOCK STRUT BAY. SUPPORT ANGLES OF PANEL 542AZ/642AZ AT LH/RH MLG SHOCK STRUT BAY WERE REPLACED PER CRJ-700 SRM 51-42-21-001-001-A01.Aug 6, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250034Seat Track · corrodedCORROSION AT SEAT RAIL LBL 9 (02) SEGMENTS: (01) FS679 - FS863. (02) FS863 - FS1005. AT PAX CABIN. CORROSION AT SEAT RAIL LBL 9 (02) SEGMENTS: (01) FS679 - FS863. (02) FS863 - FS1005. AT PAX CABIN WAS EVALUATED OUT OF LIMITS PER PER CRJ-700 SRM 53-41-49-101-0Aug 6, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509250024Hinge Fitting · excess playDURING INSPECTION OF TASK CARD :55-30-203-JIC GVI OF THE VERTICAL STABILIZER INTERNAL AREA AROUND RUDDER POWER CONTROL UNIT WAS FOUND FREEPLAY ON BEARING OF LOWER HINGE FITTING AT REAR SPAR OF VERTICAL STABILIZER. HINGE FITTING #3 (P/N: AV670-21081-013 ) WAS Aug 6, 2025 · N526EA · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202509250022Seat Track · corrodedCORROSION AT SEAT RAIL LBL 9 (03) SEGMENTS: (01) FS375 - FS485. (02) FS485 - FS581. (03) FS581 - FS677. AT PAX CABIN. SEAT RAILS LBL 9 (03) SEGMENTS: (01) FS375 - FS485. (02) FS485 - FS581. (03) FS581 - FS677. AT PAX CABIN. WERE EVALUATES OUT LIMITS PER CRJ 7Aug 6, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509250021Seat Track · corrodedCORROSION ON RH SIDE SEAT RAIL (STRG 15R) (05) SEGMENTS: (01) FS573 - FS661. (02) FS679 - FS704. (03) FS704 - FS763. (04) FS783 - FS861. (05) FS861 - FS969. AT PAX CABIN. RH SIDE SEAT RAIL STRG 15R (FS573 - FS661) WAS CLEANED PER CRJ-700 SRM 51-26-00-001-001-Aug 6, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509250020Seat Track · corrodedCORROSION ON LH SIDE SEAT RAIL (STRG 15L) 04 SEGMENTS: (01) FS573 - FS679. (02) FS679 - FS704. (03) FS704 - FS763. (04) FS783 - FS861. AT PAX CABIN. CORROSION ON LH SIDE SEAT RAIL (STRG 15L) 04 SEGMENTS: (01) FS573 - FS679. (02) FS679 - FS704. (03) FS704 - FSAug 6, 2025 · N526EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202509250010Access Panel · damagedPYLON ACCESS PANEL 412HB DAMAGED FASTENER LOCATION WITHIN 1193.53 FLIGHT HOURS AFTER COMPLETION OF SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT LOCATION IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART// ENGINEERING COMMENTS. PYLON ACCESS PANEAug 6, 2025 · N526EA · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR VNAA202509250039Intercostal · corrodedCRACK ON INTERCOSTALS OF TIRE BURST SUPPORT STRUCTURE (SUPPORT FOR 542AZ/642AZ) AT LH/RH MLG SHOCK STRUT BAY. INTERCOSTALS OF TIRE BURST SUPPORT STRUCTURE (SUPPORT FOR 542AZ/642AZ) AT LH/RH MLG SHOCK STRUT BAY WERE REPLACED PER CRJ-700 SRM 51-42-06-001-001-AAug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250037Angle · corrodedCORROSION ON ANGLE MID CAP BTW FS310.00 TO FS349.00 AT PASSENGER SURROUND STRUCTURE. ANGLE MID CAP BTW FS310.00 TO FS349.00 AT PASSENGER SURROUND STRUCTURE WAS EVALUATED OUT OF LIMTS PER CRJ-700 SRM 53-00-00-101-001-A01 AND IT WAS REPLACED PER CRJ-700 SRM 51-Aug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250036Fitting · corrodedCORROSION ON SUPPORT OF ACTUATOR ROD ASSEMBLY BTW FS310.00 TO FS319.70 AND STGR18LH AT LOWER SURROUND STRUCTURE OF PASSENGER DOOR. SUPPORT OF ACTUATOR ROD ASSEMBLY BTW FS310.00 TO FS319.70 AND STGR18LH (FITTING) AT LOWER SURROUND STRUCTURE OF PASSENGER DOOR WAug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA202509250014Stringer · corrodedCORROSION ON STGR 26RH BTW FS 349-364 AT MAIN AVIONICS BAY. CORROSION ON STGR 26RH BTW FS 349-364 AT MAIN AVIONICS BAY DUE TO EXCESS DAMAGE WAS EVALUATED OUT OF LIMITS PER CRJ-700 SRM 53-21-03-101-006-A01 AND REPLACED PER CRJ 700 SRM 51-42-21-001-001-A01 AND Aug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202509250013Frame · corrodedCORROSION ON FRAME FS 319.70 BTW STGR 20LH TO 21LH AT MAIN AVIONICS BAY. CORROSION ON FRAME FS 319.70 BTW STGR 20LH TO 21LH AT MAIN AVIONICS BAY. WAS REMOVED PER CRJ-700 SRM 51-21-06-001-001-A01 AND EVALUATE WITHIN LIMITS PER CRJ-700 SRM 53-21-06-101-002-A01Aug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202509250012Floorbeam · corrodedCORROSION ON POST LOWER CORNER OF FS 280 STGR 25LH OF AT MAIN AVIONICS BAY. POST BTW FS 280/ STGR 25LH WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01 STEP 6.C, SRM 51-42-10-001-001-A01 STEP 8.C AND SRM 51-42-21-001-001-A01 STEP 6.CAug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202509250008Skin · scratched3250FH PERM REPAIR - SCRATCH DAMAGE ON FUSELAGE SKIN BETWEEN FS1031.00-FS1051.30 THE SUBJECT CONDITION IS STRUCTURALLY ACCEPTABLE FOR 3250 FLIGHT HOURS FROM TIME OF INCORPORATION OF THIS REO AT REV -. ENGINEERING COMMENTS: COMPLY WITH STEP 5 OF REO 670-53-61-2Aug 5, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202509250035Floorbeam · corrodedCORROSION AND WRONG INSTALLED FASTENERS (4EAS) ON FLOOR PANEL SUPPORT ANGLE AT FS280. FLOOR PANEL SUPPORT ANGLE AT FS280.00 WAS REPLACED PER CRJ-700 SRM 51-42-06-001-001-A01. AND SRM 51-42-21-001-001-A01.Aug 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA202509250007Floor Support · corrodedCORROSION ON FLOOR SUPPORTS (2EAS), PLATE (1EA), BRACKET MACHINED (2EAS) BTW FS 533 TO FS 581 STGR 26LH TO STGR 21LH AT FWD CARGO COMPARTMENT. CORROSION ON FLOOR SUPPORTS (2EAS), PLATE (1EA), MACHINED BRACKET (2EAS) BTW FS 533 TO FS 581 STGR 26LH TO STGR 21LHAug 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250006Web · gougedGOUGES ON WEB FROM THE FWD EDGE AND LOWER EDGE AT DOOR SURROUND STRUCTURE AT FWD BAGGAGE BAY. GOUGES ON WEB FROM THE FWD EDGE AND LOWER EDGE AT DOOR SURROUND STRUCTURE AT FWD BAGGAGE BAY WERE BLENDED OUT PER CRJ-700 SRM 51-12-00-001-001-A01 AND EVALUATED WITHAug 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250005Web · mechanic errorMISDRILL ON LOWER SURROUND STRUCTURE OF FWD COMPARTENT DOOR. REPAIRED PER REO 670-53-31-1078 REV --Aug 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202509250004Skin · wornWEAR ON LOWER SKIN OF AFT FUSELAGE ON FS970.00 TO FS 977.00 AND STG 27. LOWER SKIN OF AFT FUSELAGE ON FS970.00 TO FS 977.00 AND STG 27 WAS REPAIRED PER REO 670-53-00-789 REV.--Aug 4, 2025 · N526EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA202509250017Drag Angle · crackedCRACK ON FWD AND AFT RH DRAG ANGLE BTW UNION OF VERTICAL STABILIZER AND FUSELAGE (67.5% REAR SPAR DATUM). FWD AND AFT DRAG ANGLE WERE REPAIRED PER CRJ700 SRM 55-31-00-201-001-A01Aug 3, 2025 · N526EA · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
Back to N526EA