N532EA

Service difficulty reports · 92

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 = 'N532EA' 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 VNAA2026040215501Manifold · faultedHYD SYSTEM 3 FLUID LOST AS SOON AS WE REACH CRUISE. / REMOVED AND REPLACED HYD SYS 3 PRESSURE MANIFOLD ASSY IAW CRJ 700 AMM 29-12-09-000/400-801-A01, REMOVED AND REPLACED BOTH PUMP PRESSURE SWITCHES HYD SYS 3 IAW AMM 29-34-01-000/400-802-A01, REMOVED AND REPLApr 1, 2026 · N532EA · Cndair CL6002C10 · Hydraulic System, MainSDR VNAA202602080002Stringer · crackedWHILE PERFORMING SB670BA-53-040 FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE BS 280.00 TO 295 INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR FOUND A CRACK EXTENDING FROM BS 280 TO PAST 4TH FASTENER HOLE GOING AFT ON STRINGER 3L REFeb 8, 2026 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2026021080001Floor Support · mismanufacturedON DRILL UP OF LT PRESSURE BOX, FOUND TWO PILOT HOLES ON LBL 18 TO BE MISALIGNED. OVERSIZED MISALIIGNED HOLES IAW REO 670-53-41-797 REV--.Feb 8, 2026 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20240918002Skin · damaged620FH PERM REPAIR FOR DAMAGED SCREW HOLE TO THE VERTICAL STABILIZER RH SKIN BETWEEN RIB 2 & RIB 3 AND BETWEEN FRONT SPAR & STRG 1. C/W 620FH PERMANENT REPAIR FOR THE DAMAGED HOLE TO V-STAB RH SKIN BTW RIB 2 & RIB 3 AND BTW FRONT SPAR & STRG 1 (PERMANENT REPASep 18, 2024 · N532EA · Cndair CL6002C10 · Vertical Stabilizer, Plate/SkinSDR WRXR20240918001Slat Track · gougedL/H WING SLAT TRACK 3-3 ECCENTRIC ROLLERS, FOUND SLAT TRACK TO HAVE GROOVES ON EACH SIDE AND TOP AND BOTTOM OF TRACK. SLAT TRACK 3-3. COMPLIED WITH REO 670-57-42-1680 REV --, REMOVED AND REINSTALLED LH SLAT TRACK 3-3 PER CRJ700 AMM 27-81-41-000-803-A01 AND 27-Sep 18, 2024 · N532EA · Cndair CL6002C10 · Leading Edge DevicesSDR WRXR20240909003Skin · gougedGOUGE DAMAGE TO LH FIXED LEADING EDGE 621AT, ABOVE LANDING/TAXI LIGHT. SMOOTH AND BLENDED DAMAGED AREA IAW CRJ 900 SRM 57-41-01-201-001-A01, NDT COMPLIED WITH, AREA RE-FINISHED IAW REO 670-57-41-576.Sep 9, 2024 · N532EA · Cndair CL6002C10 · Wing, Plate/SkinSDR WRXR20240909002Skin · dented4X DENTS LOCATED ON LOWER SKIN UNDER PANELS 195DL AND 196DR APPROXIMATELY @FS 969 STRINGER 26L - 27. #1: .4 X .4 X .019. #2: .8 X .4 X .011. #3: 1.0 X .7 X .027. #4: 1.1 X 1.1 X .034. DAMAGE IS NOT ALLOWED IN THIS AREA PER CRJ700 SRM 53-51-01-101-003-A01. REPSep 9, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WRXR20240909001Intercostal · corrodedINTERCOSTAL C/T STRINGER 20R, BETWEEN FRAMES AT FS310.00 AND FS319.70, BELOW AND FORWARD OF THE SERVICE DOOR LOWER SILL (WL72.50), HAS LIGHT CORROSION ON THE UPPER FACE. 319.70 HAS ELONGATED HOLE THROUGH INTERCOSTAL AND DRILL START IN STRINGER. HOLE MEASURES: Sep 9, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20240831001Slat · scratchedFOUND SCRATCHES UNDER SEALANT ON RH SLAT #1 ACCESS FLANGE, 4TH OUTBOARD, BETWEEN WS92.20 TO WS102.43. REPAIRED IAW EA-A1-670-57-00046.Aug 31, 2024 · N532EA · Cndair CL6002C10 · Leading Edge DevicesSDR WRXR20240830001Skin · dented650FH PERM REPAIR - TEMPORARY DISPOSITION FOR DENT DAMAGE TO PYLON L/E SKIN, RHS. COMPLIED WITH REO M670-54-52-079 REV-- PERMANENT DISPOSITION FOR DENT & BLENDED DAMAGE TO PYLON L/E SKIN.Aug 30, 2024 · N532EA · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR WRXR20240829002Seat Track · corrodedFLOOR SEAT TRACK #58, LOCATED AT FS863.00 TO FS977.00, RBL9.00, HAS 6 AREAS OF MILD CORROSION FROM FS874.00 TO FS957.00. REMOVED AND REPLACED SEAT TRACK #58, LOCATED AT FS863.00 TO FS977.00, RBL9.00 WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAAug 29, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240829001Door Frame · scratchedLIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER EDGE FRAME OF THE AFT CARGO BAY DOOR. @ STRINGER 11-STRINGER 20 FS977-FS1051. LH SIDE SKIN PN: MM670-35116-007. SMOOTHED AND BLENDED LIGHT SCRATCHES FOUND IN MULTIPLE AREAS ON THE UPPER AND LOWER Aug 29, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, StructureSDR WRXR20240827009Cargo Track · corrodedCARGO TRACK #1 RBL27.00, LOCATED AT FS977.13 TO FS1005.13, HAS MILD CORROSION AT FS 989.00 AND FROM FS993.00 TO FS1005.13. REMOVED AND REPLACED SEAT TRACK CARGO TRACK #1 RBL27.00, LOCATED AT FS977.13 TO FS1005.13 WITH FABRICATED TRACK FROM EXTRUSION PN 20276-2Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827008Seat Track · corrodedCARGO TRACK #1 RBL9.00, LOCATED AT FS977.13 TO FS1005.13, HAS MILD CORROSION FROM FS994.00 TO FS1000.00 AND UPPER SURFACE CORROSION AT FS994.00. REMOVED AND REPLACED SEAT TRACK CARGO TRACK #1 RBL9.00, LOCATED AT FS977.13 TO FS1005.13 WITH FABRICATED TRACK FROAug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827006Cargo Track · corrodedCARGO TRACK #2, LOCATED AT FS988.25 TO 1005.13, LBL9.00, HAS MILD CORROSION ON UPPER SURFACE AT FS992.00, MILD CORROSION IN THE TRACK CHANNEL FROM FS992.00 TO 1005.13. REMOVED AND REPLACED CARGO TRACK #2, LOCATED AT FS988.25 TO 1005.13, LBL9.00 WITH FABRICATEDAug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827005Seat Track · corrodedFLOOR SEAT TRACK #54R, LOCATED AT FS677.00 TO FS863.00, RBL9.00, HAS 11 AREAS OF MILD CORROSION FROM FS678.00 TO FS863.00, A GOUGED LUG (I/B SIDE) AT FS812.00, AND GOUGES IN THE BOTTOM OF THE TRACK CHANNEL FROM FS764.00 TO FS775.00. REMOVED AND REPLACED SEAT TAug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827004Seat Track · corrodedFLOOR SEAT TRACK #57, LOCATED AT FS863.00 TO FS988.25, LBL9.00, HAS 5 AREAS OF MILD CORROSION FROM FS875.00 TO FS957.00, ONE GOUGED LUG AT FS956, AND A SECTION WITH GOUGES IN THE TRACK CHANNEL FROM FS926 TO FS936. REMOVED AND REPLACED SEAT TRACK #57, LOCATED AAug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827003Seat Track · corrodedFLOOR SEAT RAIL #54L, LOCATED AT FS677.00 TO FS863.00, LBL9.00, HAS 12 AREAS OF MILD CORROSION FROM FS677.00 TO FS862.00.Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827002Seat Track · corrodedFLOOR SEAT TRACK #56, LOCATED AT FS923.00 TO FS977.00, LBL27.00, HAS MILD CORROSION FROM FS969.00 TO FS974.00. : REMOVED AND REPLACED SEAT TRACK #56, LOCATED AT 923.00 TO FS977.00, LBL27.00, WITH FABRICATED SEAT TRACK FROM EXTRUSION PN 20276-288-0-0 IAW CRJ 70Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20240827001Cleat · corrodedCORROSION ON AREAS B, C ARE COMMON TO STRINGER 22R FS333. FRAME CLEAT PN:SH670-31253-3. : FABRICATED FRAME CLEAT C/T STRINGER 22 @FS333 FROM 2024T3-0.050 LOT#446842B7/1.16.1 PER BOMBARDIER DRAWING #:SH670-31253 REV. A, AND INSTALLED IAW CRJ700 SRM TASK 51-42-0Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2024082600633Stringer · corrodedSTRINGER 24R HAS MULTIPLE AREAS OF CORROSION BETWEEN FS310-FS349. REMOVED CORRODED STRINGER 24R FWD (FS280-FS333) AND AFT(FS333-FS349) AND WET INSTALLED NEW STRINGER 24R FWD AND AFT IAW CRJ700 SRM 51-42-06-001-001-A01. PERFORMED STRINGER SPLICE @349-364 IAW CRAug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNA202408260009Stringer · corrodedSTRINGER 23R HAS SEVERAL AREAS OF CORROSION FROM FS310-FS349. AREAS FROM FS319-FS349 ARE NO REPAIRS ALLOWED PER CRJ700 SRM 53-00-03-201-001-A01. REMOVED AND REPLACED CORRODED STRINGER 23R FWD(FS280-FS333)AND AFT(FS333-FS379) PER CRJ700 SRM 51-42-06-001-001-A0Aug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR WRXR20240826001Stringer · corrodedCORROSION FOUND ON STRINGER 22R PN:SH670-31210-2 AT FS.340-FS349. NO REPAIRS ALLOWED PER CRJ700 SRM TASK 53-00-03-201-001-A01. REMOVED CORRODED STRINGER 22R FWD(280-333) AND AFT(333-349) AND WET INSTALLED NEW STRINGER 22R FWD AND AFT IAW CRJ700 SRM 51-42-06-0Aug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR WRXR20240823001Seat Track · corrodedFLOOR SEAT RAIL #48, LOCATED AT FS350.00 TO FS485.00, RBL9.00, HAS 4 AREAS OF MILD CORROSION FROM FS356.00 TO FS469.00 AND GOUGES IN THE BOTTOM OF THE TRACK CHANNEL IN 2 SECTIONS FROM FS419.00 TO FS437.00 AND FS455.00 TO FS473.00. REMOVED AND REPLACED FLOOR SEAug 23, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR202408200001Skin · dentedPERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R. PERFORMED PERM REPAIR - SKIN, FUSELAGE - BETWEEN FS1031.00 AND FS 1051.30 AND STR 22R AND STR 25R IAW REO-670-53-61-2326 REV--.Aug 20, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WRXR20240813001Drain Line · corrodedPASSENGER DOOR SILL, MIDDLE DRAIN TUBE ASSY IS CORRODED. REMOVED DAMAGED DRAIN TUBE ASSY AND REPLACED WITH A NEW ASSY (SH670-31904-5) WITH PERMANENT FASTENERS IAW CRJ700 SRM TASK 51-42-20-001-001-A01. TOUCH UP PAINT AND FASTENERS IAW CRJ700 SRM TASK 51-25-01-0Aug 13, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WRXR20240812002Window Frame · gougedUPON REMOVING RH WINDSHIELD, SEVERAL GOUGES WERE FOUND IN THE FWD. LOWER SILL PN:CC670-33195-5. BLENDED DAMAGE ON RH LWR FWD SILL, ROTO-PEENED REWORKED AREA IAW CRJ700/900 SRM 51-24-11 PER REO 670-53-11-2000, REV--. USED TUNGSTEN CARBINE 9/16 X 1.25" DOUBLE ROAug 12, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, StructureSDR WRXR20240812001Window Frame · gougedUPON REMOVING COCKPIT RH SIDE WINDOW, TOOL MARKS/GOUGES WERE FOUND ON RH LOWER AFT SILL PN: CC670-33196-2. BLENDED DAMAGE ON RH LWR AFT SILL, ROTO-PEENED REWORKED AREA IAW CRJ700/900 SRM 51-24-11 PER REO 670-53-11-1999. USED TUNGSTEN CARBINE 9/16 X 1.25" DOUBLAug 12, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, StructureSDR WRXR20240806001Drain Line · corrodedPASSENGER DOOR SILL, AFT DRAIN TUBE ASSY (P/N SH670-31904-5) IS CORRODED AND HAS A LARGE HOLE ON THE BACKSIDE / RADIUS OF THE TUBE. - REMOVED AND REPLACED DRAIN TUBE ASSY (SH670-31904-5) AND INSTALLED NEW SOLID RIVETS (MS20470AD5-9) IAW CRJ700 SRM TASK 51-42-Aug 6, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202407260001Door Frame · gougedFWD, AFT BAGGAGE BAY TRACK P/N CC670-38809-1 ROLLER GUIDE, LOWER, FWD, DOOR SURROUND, HAS TWO GOUGES ON THE I/B SIDE OF THE OPENING ROUGHLY 0.60" LONG AND 0.050" WIDE. BLENDED IAW CRJ 700 SRM 51-12-00 USING A 20:1 RATIO. NOMINAL THICKNESS .080" AND MINIMUM THIJul 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202207189991Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODEDJul 18, 2022 · N532EA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202207079995Strap · corrodedAFT BELLY FAIRNING SUPPORT STRUCTURE FROM FS879 TO FS939 STR24R STRAP WITH NUTPLATES ATTACHED HAS SEVERAL AREAS OF CORROSION AROUND NUTPLATES ON BOTTOM SIDES.Jul 7, 2022 · N532EA · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA202207079994Intercostal · corrodedINTERCOSTAL 26L CORRODED BETWEEN FS 349 AND FS 364Jul 7, 2022 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202207079992Door Sill · corrodedAFT CARGO DOOR SILL IS CORRODEDJul 7, 2022 · N532EA · Cndair CL6002C10 · Cargo/Baggage DoorsSDR VNAA202207079991Intercostal · corrodedINTERCOSTAL 27L BETWEEN FS349 AND FS364 IS CORRODEDJul 7, 2022 · N532EA · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA202201271111Compressor · fodTAKING OFF OUT OF DCA THE RH ENGINE DID NOT ACHIEVE TAKEOFF POWER SO THE TAKEOFF WAS ABORTED. RH ENG LOW PWR ON TAKE OFF ROLL HIGH SPEED ABORT. REMOVED AND REPLACED FUEL METERING UNIT IAW 73-21-03-000/400-801-A01. OPS AND LEAK CHECK OF THE FMU GOOD AT THIS TIJan 25, 2022 · N532EA · Cndair CL6002C10 · Fuel Controlling SystemSDR VNAA202107251111Pcb · unserviceableHYD 1 LO PRESS CAUTION MSG ALONG WITH HYDRAULIC 1 SOV CLSD STATUS MSG AND ENGINE BOTTLE SWITCH LIGHTS ILLUMINATED AND LH ENG BLEED CAUTION MSG SHORTLY AFTER TAKEOFF. QRH WAS RAN AND MESSAGES CLEARED. ON CLIMB OUT HYD 1 LO PRESS CAUTION MSG ALONG WITH HYDRAULIJul 21, 2021 · N532EA · Cndair CL6002C10 · Fire Protection System WiringSDR VNAA2020062111102Battery Pack · inoperativeROW 16 OVERHEAD AND LOWER ROW 16AC EMERGENCY LIGHTS NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY BATTERY PACK IAW 33-51-17-400-801 OPS CHECK GOOD.Jun 20, 2020 · N532EA · Cndair CL6002C10 · Emergency LightingSDR SIMA20191011001Stringer · corrodedSTRINGER 27 IS CORRODED JUST AFT OF FRAME FS280. REMOVED AND REPLACED STRINGER 27 JUST AFT OF FS280.00 IAW SRM 51-42-06 AND SRM 51-42-20.Oct 11, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20191010003Skin · dentedDENTS ON LEFT INBOARD FLAP LOWER SIDE 17 INCHES FROM INBD EDGE 4 INCHES FROM THE TRAILING EDGE. -C/A-REPAIRED LH INBD FLAP LOWER SIDE IAW SRM 57-52-01-991-812.Oct 10, 2019 · N532EA · Cndair CL6002C10 · Trailing Edge FlapsSDR SIMA20191010002Skin · dentedRT WING INBOARD FLAP UNDER SIDE HAD FOUR DENTS. COMPLIED WITH REPAIR IAW ERS-CR-57MR-1173 01Oct 10, 2019 · N532EA · Cndair CL6002C10 · Trailing Edge FlapsSDR SIMA2019100492812Frame · corrodedFRAME AT FS 333.0 IS CORRODED FWD AND AFT SIDES BETWEEN STR 26R AND STR 27-C/A-COMPLETED THE FRAME REPAIR AT FS 333.00 IAW SRM 53-00-06 AND SRM 51-42-21Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20190928008Door Sill · corrodedSERVICE DOOR SILL HAS AREAS OF CORROSSION BETWEEN FS 319.70 ANS 349.00-C/A-REMOVED AND REPLACED SERVIE DOOR SILL ANGLE IAW SRM51-42-21 AND 51-42-06.Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20190928006Frame · corrodedFRAME AT FS 319.0 IS CORRODED FWD SIDE BETWEEN STR 26L & 26R-C/A-COMPLETED FRAME REPAIR IAW SRM 53-00-06Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA2019100194005Stringer · corrodedSTRINGER 26 LT WAS CORRODED BETWEEN BS 2800 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06 AND 53-21-03.Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20190924004Stringer · corrodedSTRINGER 26 RT IS CORRODED BETWEEN FS FRAME 280.00 AND FS FRAME 295.00-C/A-RAR STRINGER 26 RT BETWEEN FS280 AND FS333 IAW SRM 51-42-06.Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20190924001Stringer · corrodedSTRINGER 25 RT IS CORRODED BETWEEN FRAME FS280.00 AND FS295.00. C/A-R&R STRINGER 25R BETWEEN FS2800.00 AND FS295.00 IAW SRM 51-42-06.Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA2019100191007Bulkhead Web · corrodedLEFT SIDE LOWER BULKHEAD AT FS 280.00 HAS CORROSION. COMPLETED INSTALLATION OF THE LHS LOWER BULKHEAD WEB AND DOUBLER IAW SRM 53-11-10.Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20190915005Bulkhead · corrodedRIGHT SIDE LOWER BULKHEAD AT FS280.00 HAS CORROSION.-C/A-REMOVED AND REPLACED RH SIDE LOWER BULKHEAD AT FS-280.00 IAW SRM 53-11-10.Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20190915004Floorbeam · corrodedRIGHT FLOOR BEAM AT FS280.00 HAS NUMEROUS AREAS OF CORROSION ON UPPER SURFACE THERE IT IS LAYERED BETWEEN DRIP TRAY AND UPPER L ANGLE-C/A-REMOVED AND REPLACED RT FLOOR BEAM AT FS 280 IAW SRM 51-42-06 AND SRM 51-42-13.Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
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