# Service difficulty reports: N532EA

A list on [N532EA](https://openairdocs.org/aircraft/N532EA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 92 reports

- [SDR VNAA2026040215501](https://openairdocs.org/sdr/VNAA2026040215501.md): Manifold · faulted · Apr 1, 2026 · N532EA · Cndair CL6002C10 · Hydraulic System, Main
  > HYD 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 REPL
- [SDR VNAA202602080002](https://openairdocs.org/sdr/VNAA202602080002.md): Stringer · cracked · Feb 8, 2026 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > WHILE 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 RE
- [SDR VNAA2026021080001](https://openairdocs.org/sdr/VNAA2026021080001.md): Floor Support · mismanufactured · Feb 8, 2026 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ON 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--.
- [SDR WRXR20240918002](https://openairdocs.org/sdr/WRXR20240918002.md): Skin · damaged · Sep 18, 2024 · N532EA · Cndair CL6002C10 · Vertical Stabilizer, Plate/Skin
  > 620FH 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 REPA
- [SDR WRXR20240918001](https://openairdocs.org/sdr/WRXR20240918001.md): Slat Track · gouged · Sep 18, 2024 · N532EA · Cndair CL6002C10 · Leading Edge Devices
  > L/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-
- [SDR WRXR20240909003](https://openairdocs.org/sdr/WRXR20240909003.md): Skin · gouged · Sep 9, 2024 · N532EA · Cndair CL6002C10 · Wing, Plate/Skin
  > GOUGE 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.
- [SDR WRXR20240909002](https://openairdocs.org/sdr/WRXR20240909002.md): Skin · dented · Sep 9, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > 4X 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. REP
- [SDR WRXR20240909001](https://openairdocs.org/sdr/WRXR20240909001.md): Intercostal · corroded · Sep 9, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTERCOSTAL 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:
- [SDR WRXR20240831001](https://openairdocs.org/sdr/WRXR20240831001.md): Slat · scratched · Aug 31, 2024 · N532EA · Cndair CL6002C10 · Leading Edge Devices
  > FOUND SCRATCHES UNDER SEALANT ON RH SLAT #1 ACCESS FLANGE, 4TH OUTBOARD, BETWEEN WS92.20 TO WS102.43. REPAIRED IAW EA-A1-670-57-00046.
- [SDR WRXR20240830001](https://openairdocs.org/sdr/WRXR20240830001.md): Skin · dented · Aug 30, 2024 · N532EA · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > 650FH 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.
- [SDR WRXR20240829002](https://openairdocs.org/sdr/WRXR20240829002.md): Seat Track · corroded · Aug 29, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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 IA
- [SDR WRXR20240829001](https://openairdocs.org/sdr/WRXR20240829001.md): Door Frame · scratched · Aug 29, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Structure
  > LIGHT 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
- [SDR WRXR20240827009](https://openairdocs.org/sdr/WRXR20240827009.md): Cargo Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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 20276-2
- [SDR WRXR20240827008](https://openairdocs.org/sdr/WRXR20240827008.md): Seat Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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 FRO
- [SDR WRXR20240827006](https://openairdocs.org/sdr/WRXR20240827006.md): Cargo Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CARGO 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 FABRICATED
- [SDR WRXR20240827005](https://openairdocs.org/sdr/WRXR20240827005.md): Seat Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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 T
- [SDR WRXR20240827004](https://openairdocs.org/sdr/WRXR20240827004.md): Seat Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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 A
- [SDR WRXR20240827003](https://openairdocs.org/sdr/WRXR20240827003.md): Seat Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT RAIL #54L, LOCATED AT FS677.00 TO FS863.00, LBL9.00, HAS 12 AREAS OF MILD CORROSION FROM FS677.00 TO FS862.00.
- [SDR WRXR20240827002](https://openairdocs.org/sdr/WRXR20240827002.md): Seat Track · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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 70
- [SDR WRXR20240827001](https://openairdocs.org/sdr/WRXR20240827001.md): Cleat · corroded · Aug 27, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > CORROSION 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 51-42-0
- [SDR VNAA2024082600633](https://openairdocs.org/sdr/VNAA2024082600633.md): Stringer · corroded · Aug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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 CR
- [SDR VNA202408260009](https://openairdocs.org/sdr/VNA202408260009.md): Stringer · corroded · Aug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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-A0
- [SDR WRXR20240826001](https://openairdocs.org/sdr/WRXR20240826001.md): Stringer · corroded · Aug 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 51-42-06-0
- [SDR WRXR20240823001](https://openairdocs.org/sdr/WRXR20240823001.md): Seat Track · corroded · Aug 23, 2024 · N532EA · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR 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 SE
- [SDR WRXR202408200001](https://openairdocs.org/sdr/WRXR202408200001.md): Skin · dented · Aug 20, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PERM 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--.
- [SDR WRXR20240813001](https://openairdocs.org/sdr/WRXR20240813001.md): Drain Line · corroded · Aug 13, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER 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 51-25-01-0
- [SDR WRXR20240812002](https://openairdocs.org/sdr/WRXR20240812002.md): Window Frame · gouged · Aug 12, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Structure
  > UPON 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 RO
- [SDR WRXR20240812001](https://openairdocs.org/sdr/WRXR20240812001.md): Window Frame · gouged · Aug 12, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Structure
  > UPON 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" DOUBL
- [SDR WRXR20240806001](https://openairdocs.org/sdr/WRXR20240806001.md): Drain Line · corroded · Aug 6, 2024 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER 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-
- [SDR VNAA202407260001](https://openairdocs.org/sdr/VNAA202407260001.md): Door Frame · gouged · Jul 26, 2024 · N532EA · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD, 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 THI
- [SDR VNAA202207189991](https://openairdocs.org/sdr/VNAA202207189991.md): Door Sill · corroded · Jul 18, 2022 · N532EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR SILL IS CORRODED
- [SDR VNAA202207079995](https://openairdocs.org/sdr/VNAA202207079995.md): Strap · corroded · Jul 7, 2022 · N532EA · Cndair CL6002C10 · Aerodynamic Fairings
  > AFT BELLY FAIRNING SUPPORT STRUCTURE FROM FS879 TO FS939 STR24R STRAP WITH NUTPLATES ATTACHED HAS SEVERAL AREAS OF CORROSION AROUND NUTPLATES ON BOTTOM SIDES.
- [SDR VNAA202207079994](https://openairdocs.org/sdr/VNAA202207079994.md): Intercostal · corroded · Jul 7, 2022 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL 26L CORRODED BETWEEN FS 349 AND FS 364
- [SDR VNAA202207079992](https://openairdocs.org/sdr/VNAA202207079992.md): Door Sill · corroded · Jul 7, 2022 · N532EA · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR SILL IS CORRODED
- [SDR VNAA202207079991](https://openairdocs.org/sdr/VNAA202207079991.md): Intercostal · corroded · Jul 7, 2022 · N532EA · Cndair CL6002C10 · Fuselage Main, Frame
  > INTERCOSTAL 27L BETWEEN FS349 AND FS364 IS CORRODED
- [SDR VNAA202201271111](https://openairdocs.org/sdr/VNAA202201271111.md): Compressor · fod · Jan 25, 2022 · N532EA · Cndair CL6002C10 · Fuel Controlling System
  > TAKING 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 TI
- [SDR VNAA202107251111](https://openairdocs.org/sdr/VNAA202107251111.md): Pcb · unserviceable · Jul 21, 2021 · N532EA · Cndair CL6002C10 · Fire Protection System Wiring
  > HYD 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 HYDRAULI
- [SDR VNAA2020062111102](https://openairdocs.org/sdr/VNAA2020062111102.md): Battery Pack · inoperative · Jun 20, 2020 · N532EA · Cndair CL6002C10 · Emergency Lighting
  > ROW 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.
- [SDR SIMA20191011001](https://openairdocs.org/sdr/SIMA20191011001.md): Stringer · corroded · Oct 11, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR SIMA20191010003](https://openairdocs.org/sdr/SIMA20191010003.md): Skin · dented · Oct 10, 2019 · N532EA · Cndair CL6002C10 · Trailing Edge Flaps
  > DENTS 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.
- [SDR SIMA20191010002](https://openairdocs.org/sdr/SIMA20191010002.md): Skin · dented · Oct 10, 2019 · N532EA · Cndair CL6002C10 · Trailing Edge Flaps
  > RT WING INBOARD FLAP UNDER SIDE HAD FOUR DENTS. COMPLIED WITH REPAIR IAW ERS-CR-57MR-1173 01
- [SDR SIMA2019100492812](https://openairdocs.org/sdr/SIMA2019100492812.md): Frame · corroded · Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 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 51-42-21
- [SDR SIMA20190928008](https://openairdocs.org/sdr/SIMA20190928008.md): Door Sill · corroded · Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE 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.
- [SDR SIMA20190928006](https://openairdocs.org/sdr/SIMA20190928006.md): Frame · corroded · Sep 28, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS 319.0 IS CORRODED FWD SIDE BETWEEN STR 26L & 26R-C/A-COMPLETED FRAME REPAIR IAW SRM 53-00-06
- [SDR SIMA2019100194005](https://openairdocs.org/sdr/SIMA2019100194005.md): Stringer · corroded · Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Structure
  > STRINGER 26 LT WAS CORRODED BETWEEN BS 2800 AND 295. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06 AND 53-21-03.
- [SDR SIMA20190924004](https://openairdocs.org/sdr/SIMA20190924004.md): Stringer · corroded · Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR SIMA20190924001](https://openairdocs.org/sdr/SIMA20190924001.md): Stringer · corroded · Sep 24, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 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.
- [SDR SIMA2019100191007](https://openairdocs.org/sdr/SIMA2019100191007.md): Bulkhead Web · corroded · Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LEFT SIDE LOWER BULKHEAD AT FS 280.00 HAS CORROSION. COMPLETED INSTALLATION OF THE LHS LOWER BULKHEAD WEB AND DOUBLER IAW SRM 53-11-10.
- [SDR SIMA20190915005](https://openairdocs.org/sdr/SIMA20190915005.md): Bulkhead · corroded · Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RIGHT 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.
- [SDR SIMA20190915004](https://openairdocs.org/sdr/SIMA20190915004.md): Floorbeam · corroded · Sep 15, 2019 · N532EA · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT 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.

Next page: https://openairdocs.org/aircraft/N532EA/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N532EA/reports

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