# Service difficulty reports: N500AE

A list on [N500AE](https://openairdocs.org/aircraft/N500AE.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 4 · 181 reports

- [SDR VNAA2026082123301](https://openairdocs.org/sdr/VNAA2026082123301.md): Pin · failed · Aug 21, 2026 · N500AE · Cndair CL6002C10 · Turbine Engine Compressor Section
  > RT ENGINE HIGH VIBE IN FLIGHT. REMOVED AND REPLACED RH FAN BLADE PINS IAW CRJ7 AMM 72-21-02-000/400-801-A01-PSA.
- [SDR VNAA202604010031](https://openairdocs.org/sdr/VNAA202604010031.md): Floor Support · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT IS CORRODED BETWEEN FS 1031 AND FS 1088. REPAIRED FLOOR BEAM IAW MHIRJ REO 670-53-61-2531 REV--.
- [SDR VNAA202604010030](https://openairdocs.org/sdr/VNAA202604010030.md): Post · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Structure
  > F.S.280 BULKHEAD DOOR POST AND ATTACHING ANGLE AT LBL11 IS CORRODED AT WL 79.5 COMPLIED WITH F.S. 280 BULKHEAD DOOR POST AND ATTACHING ANGLE AT LBL11 AT WL 79.5 IAW CRJ 700 SRM 53-11-10-201-006-A01. CC670-34142-2
- [SDR VNAA202604010032](https://openairdocs.org/sdr/VNAA202604010032.md): Door · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Emergency Exits
  > THE STRAP BELOW THE RH OVER-WING EMERGENCY EXIT DOOR IS CORRODED. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-=53-41-749 REV – DATED 2025-07-18. - DISPOSITION FOR BLENDED CORROSION DAMAGE TO RH OVERWING EMERG. EXIT SURROUND STRUCTURE LOWER INNER STRAP B
- [SDR VNAA202604010029](https://openairdocs.org/sdr/VNAA202604010029.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS879-FS915 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01. SH670-37543-3
- [SDR VNAA202604010028](https://openairdocs.org/sdr/VNAA202604010028.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL AT FS 714-FS761 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01. SH670-37509-1
- [SDR VNAA202604010033](https://openairdocs.org/sdr/VNAA202604010033.md): Strap · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Aerodynamic Fairings
  > RBL 45 FAIRING SUPPORT STRAP IS CORRODED AT FS 847. REMOVED AND REPLACED FS 847 RBL 45 FAIRING SUPPORT STRAP PN# SH670-39166-5 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-45-00-001-001-A01 & 51-23-00-001-001-A01.
- [SDR VNAA202604010027](https://openairdocs.org/sdr/VNAA202604010027.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00250420 DISCREPANCY: RH SIDE SEAT RAIL AT FS 785 TO FS 838 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT RAIL PN (SH670-36260-3) IAW CRJ-700 AMM 53-00-49-400-801-A01. FINISHED IAW CRJ-700 SRM 53-00-49-201-002-A01 STEP 3,D. REFERENCE BARCODE HN00
- [SDR VNAA202604010034](https://openairdocs.org/sdr/VNAA202604010034.md): Strap · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CORROSION ON STRAP AT LBL45 AROUND FASTENER HOLES AT F.S.847. REMOVED AND REPLACED NEW FS 847 LBL 45 FAIRING SUPPORT STRAP PN# SH670-39166-5 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-45-00-001-001-A01 & 51-23-00-001-001-A01.
- [SDR VNAA202604010035](https://openairdocs.org/sdr/VNAA202604010035.md): Strap · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LOWER STRAP ATTACHED TO LOWER SUPPORT WEB AT F.S.879 HAS SURFACE CORROSION BETWEEN LBL45 AND RBL45. FOUND THE L/H & R/H FS 879 FAIRING SUPPORT STRAPS BETWEEN LBL45 & RBL 45 TO BE OUT OF LIMITS IAW CRJ-700 SRM 53-82-55-101-002-A01 DUE TO THE AMOUNT / DEPTH OF
- [SDR VNAA202604010026](https://openairdocs.org/sdr/VNAA202604010026.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RH SIDE SEAT RAIL AT FS 863 TO FS 915 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01. SH670-37543-3
- [SDR VNAA202604010036](https://openairdocs.org/sdr/VNAA202604010036.md): Angle · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Aerodynamic Fairings
  > ANGLE IS CORRODED ATTACHED TO LOWER FAIRING SUPPORT WEB AT F.S.939 BETWEEN RBL2 AND LBL28. REMOVED UNSERVICEABLE FS939 BL0 SUPPORT ANGLE (P/N: SH670-39189-1) AND LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE FS939 BL0 SUPPORT ANGLE (P/N: SH670-39189-1) IAW
- [SDR VNAA202604010025](https://openairdocs.org/sdr/VNAA202604010025.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00250423 DISCREPANCY: RH SIDE SEAT RAIL AT FS 915 TO FS 969 IS CORRODED. CORRECTIVE ACTION: REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01. SH670-37543-3
- [SDR VNAA202604010037](https://openairdocs.org/sdr/VNAA202604010037.md): Skin · chafed · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Elevator, Plate/Skin
  > UNDERSIDE OF LH ELEVATOR INTERFACE IS CHAFED. REMOVED CHAFING IAW SRM 51-12-00-001-001-A01. PERFORMED U.T. THICKNESS ON L/H ELEVATOR LEADING EDGE REWORK AREAS IAW NDTM PART 01 51-20-004-270-A01. LOWEST REMAINING THICKNESS TO BE.043" OR GREATER. MEASUREMENTS
- [SDR VNAA202604010024](https://openairdocs.org/sdr/VNAA202604010024.md): Flange · cracked · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Engine Thrust Reverser
  > NDT FOUND FULL SCREEN INDICATION ON LOWER TORQUE BOX CASCADE ATTACHMENT FLANGE AT NUTPLATE HOLE MID FLANGE AND MARKED ON THE PART. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-54-22-123 REV -- DATED 2025-09-05 - TEMPORARY REPAIR FOR CRACK TO CASCADE ATTA
- [SDR VNAA202604010038](https://openairdocs.org/sdr/VNAA202604010038.md): Hinge Fitting · gouged · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Spoilers
  > RH OB GROUND SPOILER IB HINGE FITTING IS GOUGED. REMOVED EDGE DAMAGE AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW CRJ 700 SRM 57-71-02-101-A01. RESTORED FINISH IAW CRJ 700 SRM 51-25-01-001-001-A01.
- [SDR VNAA202604010039](https://openairdocs.org/sdr/VNAA202604010039.md): Guide Fitting · chafed · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR UPPER AND LOWER GUIDE FITTINGS HAVE CHAFING DAMAGE AT AFT FRAME F.S.578.36. REMOVED DAMAGE ON FORWARD CARGO DOOR UPPER AND LOWER GUIDE FITTINGS AT AFT FRAME F.S.578 IAW CRJ 700 SRM 53-31-23-201-002-A01. EVALUATED REWORKED AREA ORIGINAL THI
- [SDR VNAA202604010040](https://openairdocs.org/sdr/VNAA202604010040.md): Floor Support · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SILL MID CAP ANGLE IS CORRODED AROUND FASTENER HOLES BETWEEN FS310 AND FS349. LOCATED, DRILLED AND INSTALLED NEW SERVICABLE PART [P/N SH670-31825-3] IAW CRJ 700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA202604010023](https://openairdocs.org/sdr/VNAA202604010023.md): Spar · damaged · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Ailerons
  > FOUND RH AILERON WING AFT SPAR MOST I/B BUSHING LUG BORE TO BE PREVIOUSLY OVERSIZED. CORRECTIVE ACTION: PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-57-51-632, REV -- DATED 2025-08-29 - REPAIR FOR DAMAGE TO BORE OF RH AILERON HINGE FITTING NO 1, INBD LUG,
- [SDR VNAA202604010041](https://openairdocs.org/sdr/VNAA202604010041.md): Skin · dented · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN DENTED BETWEEN FS333 AND FS349 STGR 5R. FUSELAGE DENT WAS REPAIRED IAW REO 670-53-21-2658 REV.-- DATED 2025-10-06.
- [SDR VNAA202604010042](https://openairdocs.org/sdr/VNAA202604010042.md): Hinge Fitting · damaged · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > EA23-C7-52-0463 (PERM REPAIR BEFORE 50,492.99 FH - PAX DOOR PIANO HINGE ROLL PIN) WITHIN 3813.87 FHS FROM IR (BEFORE 50,492.99 FH), REPAIR, REPAIR OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. REPLACED THE PASSENGER DOOR FUSELAGE SID
- [SDR VNAA202604010022](https://openairdocs.org/sdr/VNAA202604010022.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN FS 581 AND FS 683.00. INSTALLED NEW SERVICEABLE SEAT TRACK AT RBL 9 FLOOR BETWEEN FS 581 AND FS 683.00 IAW CRJ700 AMM 53-00-49-400-801(CONFIGA01)
- [SDR VNAA202604010043](https://openairdocs.org/sdr/VNAA202604010043.md): Handle · chafed · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR OUTER HANDLE CUTOUT IS CHAFED. BURNISHED CHAFED AREA SMOOTH IAW CRJ 700 SRM 51-12-00-001-001-A01. MAX CHAFED AREA LENGTH.300, WIDTH.070, AND DEPTH.020 WITHIN ALLOWABLE LIMITS IAW REO 670-52-31-031 REV -B DATED 2016-12-07 STEP 1. PERFORMED E
- [SDR VNAA202604010021](https://openairdocs.org/sdr/VNAA202604010021.md): Angle · cracked · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON RH COCKPIT FLOOR SUPPORT ANGLE. REMOVED AND REPLACED FLOOR SUPPORT ANGLE IAW CRJ-700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-40-11-001-001-A01.
- [SDR VNAA202604010044](https://openairdocs.org/sdr/VNAA202604010044.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS572-FS645 IS CORRODED. (LOCATION IS APPROXIMATE). FABRICATED, LOCATED, AND DRILLED NEW SERVICEABLE SEAT RAIL FROM RAW STOCK MATERIAL (PN- 20276-288-0-0A) IAW CRJ700 SRM 51-40-11-001-001-A01 AND BOMBARDIER REO 670-53-00-343. REV -M, DAT
- [SDR VNAA202604010020](https://openairdocs.org/sdr/VNAA202604010020.md): Hinge · damaged · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > HN00269920 DISCREPANCY: WHILE PERFORMING REPLACEMENT OF PASSENGER DOOR HINGE FUSELAGE SIDE, FOUND PREVIOUSLY INSTALLED FREEZE PLUG ON SKIN SIDE AT FS333.00 TO BE DAMAGED BEYOND USE. REQUIRES REPLACED. CORRECTIVE ACTION: COMPLIED WITH CRJ 700 MHIRJ REO 670-53-2
- [SDR VNAA202604010045](https://openairdocs.org/sdr/VNAA202604010045.md): Frame · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME 295 FLANGE IS CORRODED BETWEEN STR24R AND STR25R REPAIRED FRAME 295 FLANGE AT STGR 24R AND 25R BY COMPLYING WITH REPAIR IAW CRJ 700 SRM 53-00-06-201-004-A01 SECTION 6 REPAIR PROCEDURES
- [SDR VNAA202604010019](https://openairdocs.org/sdr/VNAA202604010019.md): Floorbeam · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > L/H COCKPIT FLOOR PANEL SUPPORT CAMLOC ANGLE ASSY P/N(CC670-33199-3) FOUND TO BE CRACKED AT RIVET NEAR F.S.280.00 DOOR POST. INSTALLED NEW L/H COCKPIT FLOOR PANEL SUPPORT CAMLOC ANGLE ASSY P/N(CC670-33199-3) IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-
- [SDR VNAA202604010047](https://openairdocs.org/sdr/VNAA202604010047.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK FROM FS364 TO FS485 IS CORRODED. REMOVED 2EA. SEAT TRACK SEGMENTS BETWEEN F.S.364 TO F.S.485. INSTALLED NEW SERVICEABLE SEAT TRACK SEGMENT PN SH670-32249-951 AND INSTALLED FABRICATED SEAT TRACK SEGMENT PN SH670-32120-955
- [SDR VNAA202604010048](https://openairdocs.org/sdr/VNAA202604010048.md): Doubler · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > ONE NUTPLATE DOUBLER IS CORRODED FOR THE FWD WING-TO-FUSELAGE FAIRING, LOCATED BETWEEN FS 597 AND FS 613, BETWEEN STGR 27 AND STGR 26L. REMOVED CORRODED DOUBLER. FABRICATED AND INSTALLED NEW DOUBLER IAW CRJ 700 SRM 51-23-00-001-001-A01 AND CRJ 700 SRM 51-42-
- [SDR VNAA202604010018](https://openairdocs.org/sdr/VNAA202604010018.md): Stringer · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 23 LEFT IS CORRODED AT THE AFT END F.S.333 AND REQUIRES REPAIR OR REPLACEMENT. REMOVED AND REPLACED LH STRINGER 23 AT FS. 333-280 WITH SERVICEABLE PN: SH670-31211-3U IAW CRJ700 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND MHIRJ REO 670-53-21-2
- [SDR VNAA202604010049](https://openairdocs.org/sdr/VNAA202604010049.md): Bracket · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FWD CARGO MACHINED BRACKET IS CORRODED BETWEEN FS 549 AND FS 565, BETWEEN STGR 25R AND STGR 24R. REMOVED AND REPLACED FWD CARGO BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202604010050](https://openairdocs.org/sdr/VNAA202604010050.md): Bracket · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Structure (General)
  > FWD CARGO MACHINED BRACKET IS CORRODED AT FS 533, BETWEEN STGR 27 AND STGR 26L. REMOVED AND REPLACED FWD CARGO BRACKET IAW CRJ 700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202604010017](https://openairdocs.org/sdr/VNAA202604010017.md): Stringer · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND STR 20L @ FS. 280 LAP JOINT TO BE CORRODED. REMOVED CORRODED STRINGER. LOCATED, DRILLED AND INSTALLED NEW SERVICEABLE STRINGER PN SH670-31554-5S IAW CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA202604010051](https://openairdocs.org/sdr/VNAA202604010051.md): Floor Support · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LH FLOOR SILL IS CORRODED BETWEEN FS 923 AND FS 969. BLENDING OVER FASTENERS IS NOT PERMITED, (18) EACH BLIND NUTPLATE RIVETS WERE R&R AND BLENDED AREAS WERE ALODINED PRIMED AND PAINTED IAW CRJ700 SRM 51-42-15-001-001-A01, 51-21-11-001-001-A01, 51-25-06-001-
- [SDR VNAA202604010016](https://openairdocs.org/sdr/VNAA202604010016.md): Stringer · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > RH FS349 STGR2R CEILING PANEL SUPPORT BRACKET IS CRACKED. REMOVED AND REPLACED SUPPORT BRACKET IAW CRJ-700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR VNAA202604010052](https://openairdocs.org/sdr/VNAA202604010052.md): Floor Support · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT SIDE FLOOR SILL HAS AN AREA OF CORROSION AT F.S.281 RH SIDE FLOOR SILL HAD NOMINAL CORROSION DAMAGE AROUND SOLID RIVET HEADS (4) EACH. RIVETS WERE REMOVED, PAINT, AND CORROSION WAS REMOVED UP TO (0.018") DEEP. PART IS WITHIN LIMITS IAW CRJ700 SRM 51-42
- [SDR VNAA202604010053](https://openairdocs.org/sdr/VNAA202604010053.md): Floorbeam · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AVI BAY FLOOR SUPPORT ANGLE IS CORRODED AT F.S.280 FRAME BETWEEN STRINGERS 25L AND 25R. REMOVED AND REPLACED AVI BAY FLOORBOARD SUPPORT ANGLE AT FS 280 P/N CC670-34256-3 IAW CRJ 700 SRM 51-42-21-001-001-A01 AND 51-42-06-001-001-A01
- [SDR VNAA202604010015](https://openairdocs.org/sdr/VNAA202604010015.md): Doubler · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > ANTENNA DOUBLER BETWEEN FS 295 AND FS 310 AT BL0 IS CORRODED. REMOVED AND REPLACED DOUBLER IAW CRJ-700 SRM 51-42-06-001-001-A01. SH670-32364-7
- [SDR VNAA202604010054](https://openairdocs.org/sdr/VNAA202604010054.md): Floorbeam · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RBL 9 FLOOR BEAM IS CORRODED BETWEEN FS 1031 AND FS 1069. UPON FURTHER INVESTIGATION, FOUND RBL9 FLOOR BEAM BETWEEN FS1031 - FS1069 TO BE OUT OF LIMITS DUE TO NO DAMAGE ALLOWED IAW CRJ700 SRM 53-61-43-101-001-A01. REMOVED CORROSION IAW CRJ700 SRM 51-21-06-00
- [SDR VNAA202604010014](https://openairdocs.org/sdr/VNAA202604010014.md): Stringer · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR25R IS CORRODED BETWEEN FS295 AND FS310. BLENDED DEEP PITTED CORROSION ON STGR 25R. EVAL NDT RESULTS (NOTE:P/N(SH670-31212-2) STGR 25R IN LOCATION OF FS295.00-FS310.00 MANUFACTURED THICKNESS IS (0.061") REF CRJ700 SRM 53-21-03-101-002-A01 (THE REMOVED DA
- [SDR VNAA202604010013](https://openairdocs.org/sdr/VNAA202604010013.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS 379-FS445 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01.
- [SDR VNAA202604010055](https://openairdocs.org/sdr/VNAA202604010055.md): Support Strap · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 45 FAIRING SUPPORT STRAP IS CORRODED AT FS 847. REMOVED AND REPLACED FS 847 RBL 45 FAIRING SUPPORT STRAP PN# SH670-39166-5 IAW CRJ 700 SRM 51-42-06-001-001-A01, 51-45-00-001-001-A01 & 51-23-00-001-001-A01.
- [SDR VNAA202604010056](https://openairdocs.org/sdr/VNAA202604010056.md): Channel · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > U CHANNEL IS CORRODED BETWEEN FS 581 AND FS 597, BETWEEN STGR 27 AND STGR 26R.. CORRECTIVE ACTION: COMPLIED WITH REPAIR TO "U" CHANNEL BETWEEN FS 581 AND FS 597, BETWEEN STGR 27 AND STGR 26R BY REPLACING UNSERVICEABLE "U" CHANNEL (P/N: SH670-33272-3) AND INSTA
- [SDR VNAA202604010057](https://openairdocs.org/sdr/VNAA202604010057.md): Bracket · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > THE FWD CARGO MACHINED BRACKET IS CORRODED AT FS 533, BETWEEN STGR 27 AND STGR 26L. CORRECTIVE ACTION: PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-32-145 REV – DATED 2025-07-25.
- [SDR VNA2026F00007](https://openairdocs.org/sdr/VNA2026F00007.md): Bracket · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > THE FWD CARGO MACHINED BRACKET IS CORRODED AT FS 533, BETWEEN STGR 27 AND STGR 26L. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-32-145 REV – DATED 2025-07-25.
- [SDR VNAA202604010012](https://openairdocs.org/sdr/VNAA202604010012.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS 445-FS572 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01. SH670-32234-3
- [SDR VNAA202604010058](https://openairdocs.org/sdr/VNAA202604010058.md): Joint · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > F.S. 477 CIRCUMFERENTIAL JOINT IS CORRODED BETWEEN STGR 25L AND STGR 24R. PERFORMED REPAIR BY COMPLYING WITH MHIRJ REO 670-53-21-2657 REV – DATED 2025-07-25. - DISPOSITION FOR BLENDED CORROSION DAMAGE TO FS477.40 BUTTSTRAP BETWEEN STR 25L AND STR 24R. THE AI
- [SDR VNAA202604010011](https://openairdocs.org/sdr/VNAA202604010011.md): Seat Track · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS 712-FS761 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01.
- [SDR VNAA202604010010](https://openairdocs.org/sdr/VNAA202604010010.md): Seat Spring · corroded · Apr 1, 2026 · N500AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT RAIL AT FS785-FS838 IS CORRODED. REMOVED AND REPLACED SIDE SEAT RAIL IAW CRJ-700 AMM 53-00-49-400-801-A01.

Next page: https://openairdocs.org/aircraft/N500AE/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 = 'N500AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N500AE/reports

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