# Service difficulty reports: N518AE

A list on [N518AE](https://openairdocs.org/aircraft/N518AE.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 · 160 reports

- [SDR VNAA2026062920303](https://openairdocs.org/sdr/VNAA2026062920303.md): Windshield · unserviceable · Jun 26, 2026 · N518AE · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > RIGHT WINDSHIELD HEAT CAUTION, BURNING SMELL ASSOCIATED WITH MSG, PERFORMED INSTALLATION OF THE RT WINDSHIELD IAW AMM 56-11-01-400-801-A01-PSA. PERFORMED AN OPERATIONAL TEST OF THE WINDSHIELD/SIDE WINDOW TEMPERATURE CONTROLLER IAW AMM 30-41-06-710-801-A01.
- [SDR VNAA20260623048](https://openairdocs.org/sdr/VNAA20260623048.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STR 27R AND STR 26L. REMOVED DESCREPANT INTERCOSTAL, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01.
- [SDR VNAA20260623047](https://openairdocs.org/sdr/VNAA20260623047.md): Angle · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT BS 280 CORROSION CAP ANGLE TO BE CRACKED AND TO HAVE ELONGATED, OVERSIZE HOLES. INSTALLED NEW SERVICEABLE LT BS 280 CORROSION CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR VNAA20260623046](https://openairdocs.org/sdr/VNAA20260623046.md): Angle · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT BS 280 CORROSION CAP ANGLE TO BE CRACKED AND TO HAVE ELONGATED, OVERSIZE HOLES. INSTALLED NEW SERVICEABLE RT BS 280 CORROSION CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR VNAA20260623045](https://openairdocs.org/sdr/VNAA20260623045.md): Web · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT BS 280 LOWER WEB IS HAS EXFOLIATION CORROSION AT INBD EDGE. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE RT BS 280 LOWER REPAIR SPLICE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-
- [SDR VNAA20260623044](https://openairdocs.org/sdr/VNAA20260623044.md): Bulkhead Web · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LEFT BS 280 LOWER BULKHEAD WEB HAS EXFOLIATION CORROSION AT INBD EDGE. FABRICATED, LOCATED AND DRILLED NEW SERVICEABLE FS280 REPAIR LOWER WEB IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-01, 51-42-13-001-001-A01, 51-42-21-001-001-A01 AND 51-42-22-001-001-A0
- [SDR VNAA20260623043](https://openairdocs.org/sdr/VNAA20260623043.md): Floor Support · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND 7 CORROSION SPOTS ON FLOOR SUPPORT RBL 9 BETWEEN BS 847 - 909. REO 670-53-00-811 REV -.
- [SDR VNAA20260623042](https://openairdocs.org/sdr/VNAA20260623042.md): Crossbeam · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT FS 280 CROSSBEAM IS CORRODED. INSTALLED NEW SERVICEABLE RT BS 280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR VNAA20260623041](https://openairdocs.org/sdr/VNAA20260623041.md): Crossbeam · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT BS 280 CROSSBEAM IS CORRODED. INSTALLED NEW SERVICEABLE LH FS280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, 51-42-21-001-001-A01, AND 51-42-22-001-001-A01.
- [SDR VNAA20260623040](https://openairdocs.org/sdr/VNAA20260623040.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > HN00287189 DISCREPANCY: RH SIDE SEAT RAIL FROM FS 379-483 IS GOUGED AND CORRODED AT MULTIPLE LOCATIONS. CORRECTIVE ACTION: INSTALLED NEW SEAT RAIL PN SH670-32233-3 PO# 5-64583 AT FS379-483 RH IAW CRJ-700 AMM 53-00-49-400-801-A03 SH670-32233-3
- [SDR VNAA20260623039](https://openairdocs.org/sdr/VNAA20260623039.md): Bracket · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > NOTED THAT (7) FITTINGS, GUSSETS, AND CLIPS AROUND THE FWD AVI ACCESS DOOR SURROUND STRUCTURE HAVE CORROSION AND CHAFE MARKS. REPLACEMENT REQ. LOCATED, DRILLED, AND INSTALLED NEW SERVICEABLE BRACKET AT INTERSECTION OF F.S.364 AND STGR 25L IAW SRM 51-42-06-00
- [SDR VNAA20260623038](https://openairdocs.org/sdr/VNAA20260623038.md): Floorbeam · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > :CROSS BEAM IS CORRODED AT BS 1047 AND BETWEEN RBL 27 TO RBL 36. REPAIRED IAW REO 670-53-61-2641 REV--.
- [SDR VNAA20260623037](https://openairdocs.org/sdr/VNAA20260623037.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK RBL.9 APPROX BS 830 TO 977 HAS SIGNS OF CORROSION. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801(CONFIGA03).
- [SDR VNAA20260623036](https://openairdocs.org/sdr/VNAA20260623036.md): Doubler · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > ANTENNA DOUBLER IS CORRODED BETWEEN BB 295 TO 310, STR 26L TO STR 26R. INSTALLED NEW SERVICEABLE LOWER TCAS CHANNEL IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01.
- [SDR VNAA20260623035](https://openairdocs.org/sdr/VNAA20260623035.md): Frame · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 349 FRAME IS CORRODED BETWEEN STGR 26L TO STGR 26R. REMOVED DAMAGED FS 349 LOWER FRAME SEGMENT IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01, AND 51-42-21-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE FS 349 FRAME LOWER SEGMENT IAW SRM 51-42-06-001
- [SDR VNAA20260623034](https://openairdocs.org/sdr/VNAA20260623034.md): Frame · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 364 FRAME IS CORRODED BETWEEN STR 26R TO STR 25R. INSTALLED NEW SERVICEABLE 364 FRAME IAW SRM 51-42-06-001-001-A01, 51-23-00-001-001-A01, 51-42-21-001-001-A01.
- [SDR VNAA20260623033](https://openairdocs.org/sdr/VNAA20260623033.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > HN00275235 DISCREPANCY: AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27R AND STGR 26L CORRECTIVE ACTION: REMOVED DESCREPANT INTERCOSTAL, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE P/N(SH670-32075-3S) INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01
- [SDR VNAA20260623032](https://openairdocs.org/sdr/VNAA20260623032.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVI DOOR INTERCOSTAL IS CORRODED BETWEEN STGR 27R AND STGR 26R. REMOVED DISCREPANT INTERCOSTAL, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE INTERCOSTAL IAW CRJ700 SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01.
- [SDR VNAA20260623031](https://openairdocs.org/sdr/VNAA20260623031.md): Intercostal · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > AVI DOOR INTERCOSTAL IS CORRODED AT STGR 26R. REMOVED DESCREPANT DIAPHRAM, LOCATED, DRILLED, SEALED AND INSTALLED NEW SERVICEABLE. DIAPHRAM IAW SRM 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-23-00-001-001-A01.
- [SDR VNAA20260623030](https://openairdocs.org/sdr/VNAA20260623030.md): Angle · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > BS 280 FWD J ANGLE WAS CORRODED. REPLACED WITH NEW SERVICEABLE J-ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA20260623029](https://openairdocs.org/sdr/VNAA20260623029.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK FS 684 - 835 SEGMENT IS CORRODED. REMOVED DISCREPANT SEAT TRACK AND INSTALLED NEW SERVICABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623028](https://openairdocs.org/sdr/VNAA20260623028.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK BS 581 - 684 SEGMENT IS CORRODED. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED A NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623027](https://openairdocs.org/sdr/VNAA20260623027.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK BS 485 - 581 SEGMENT IS CORRODED. REMOVED CORRODED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623026](https://openairdocs.org/sdr/VNAA20260623026.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK FS 485 - 581 SEGMENT IS CORRODED. REMOVED CORRODED SEAT TRACK FROM LBL9, FS 485 - 581 IAW AMM 53-00-49-000-801-A03. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623025](https://openairdocs.org/sdr/VNAA20260623025.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL9 SEAT TRACK FS 349 - 485 SEGMENT IS CORRODED. REMOVED RBL9 SEAT TRACK AT FS 349-485 IAW AMM 53-00-49-000-801-A03. INSTALLED RBL9 SEAT TRACK IAW AMM 53-00-49-400-801-A03
- [SDR VNAA20260623024](https://openairdocs.org/sdr/VNAA20260623024.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK FS 861 - 969 SEGMENT IS CORRODED. RT SIDE SEAT TRACK BETWEEN FS 861AND FS 969 WAS REMOVED AND REPLACED IAW AMM 53-00-49-400-801 (CONFIG A03).
- [SDR VNAA20260623023](https://openairdocs.org/sdr/VNAA20260623023.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK FS 785 - 861 SEGMENT IS CORRODED. NEW RT SIDE SEAT TRACK BETWEEN FS 785 AND 861 WAS INSTALLED IAW AMM 53-00-49-400-801 (CONFIG A03).
- [SDR VNAA20260623022](https://openairdocs.org/sdr/VNAA20260623022.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK FS 713 - 761 SEGMENT IS CORRODED. NEW RT SIDE SEAT TRACK BETWEEN FS713 AND FS761 INSTALLED IAW TASK 53-00-49-400-801(CONFIGA03).
- [SDR VNAA20260623021](https://openairdocs.org/sdr/VNAA20260623021.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK BS 675 - 713 SEGMENT IS CORRODED. REMOVED CORRODED SIDE SEAT TRACK RT FS 675 - 713 IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623020](https://openairdocs.org/sdr/VNAA20260623020.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK FS 573 - 675 SEGMENT IS CORRODED. REMOVED RT SIDE SEAT TRACK AT FS 573 - 675 IAW AMM 53-00-49-000-801-A03. INSTALLED SERVICEABLE RT SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623019](https://openairdocs.org/sdr/VNAA20260623019.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK FS 675-713 SEGMENT IS CORRODED. REMOVED CORRODED SEAT TRACK AT FS675-713 LH SIDE IAW AMM 53-00-49-000-801-A03. INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623018](https://openairdocs.org/sdr/VNAA20260623018.md): Bracket · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > L/H WHEEL WELL HYD LINE BRACKET IS CORRODED BETWEEN W.S. 0.00 TO W.S. 29.00. REMOVED AND INSTALLED NEW SERVICEABLE HYDRAULIC LINE BRACKET IN LT WHEEL WELL BETWEEN W.S. 0.00 TO W.S 29.00 IAW SRM 51-41-02-001-001-A01 AND AMM 20-22-00-910-801-A01.
- [SDR VNAA20260623017](https://openairdocs.org/sdr/VNAA20260623017.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL9 SEAT TRACK BETWEEN BS 985 - BS 1000 FOUND TO BE CORRODED. REMOVED UNSERVICEABLE LBL 9 SEAT TRACK, BTWN BS 985- 1000 IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SERVICABLE LBL9 SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623016](https://openairdocs.org/sdr/VNAA20260623016.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK BS 713 - 761 SEGMENT IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623015](https://openairdocs.org/sdr/VNAA20260623015.md): Fitting · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > WHILE PERFORMING INSPECTION OF LT THRUST FITTING IAW AMM 71-22-01-400-801-A01 STEP 4.A.(1). FOUND FRETTING CORROSION ON LT PYLON OUTBD RIB THRUST FITTING HOUSING. REPAIRED LT PYLON OUTBOARD RIB REO 670-54-51-089, REV -.
- [SDR VNAA20260623014](https://openairdocs.org/sdr/VNAA20260623014.md): Fitting · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Structure
  > WHILE PERFORMING INSPECTION OF LH THRUST FITTING IAW AMM 71-22-01-400-801-A01 STEP 4.A.(1) FOUND EVIDENCE OF FRETTING CORROSION ON INTERFACE (MATING SURFACE) OF THRUST FITTING AND DAMAGE FOUND AROUND THE TABS OF THE THRUST FITTING ON THE INTERFACE. (MATING SUR
- [SDR VNAA20260623013](https://openairdocs.org/sdr/VNAA20260623013.md): Skin · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN IS CORRODED BETWEEN BS 517 TO 533 AT STR 27 (UNDER ADF ANTENNA). REPAIRED FUSELAGE SKIN IAW REO 670-53-31-1127, REV -.
- [SDR VNAA20260623012](https://openairdocs.org/sdr/VNAA20260623012.md): Floor Support · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT IS CORRODED BETWEEN BS 1000 TO BS 1031. REPAIRED FLOOR SUPPORT IAW SRM 53-0041-201-001-A01, FIGURE 53-00-41-991-830.
- [SDR VNAA20260623011](https://openairdocs.org/sdr/VNAA20260623011.md): Floorbeam · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL 27 FLOORBEAM IS CORRODED BETWEEN BS 1000 TO 1031. REPAIRED FLOORBEAM IAW SRM 53-0041-201-001-A01, FIGURE 53-00-41-991-830.
- [SDR VNAA20260623010](https://openairdocs.org/sdr/VNAA20260623010.md): Cargo Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 27 FLOOR SEAT TRACK IS CORRODED BETWEEN BS 985 TO 1000. INSTALLED NEW SERVICEABLE CARGO TIE DOWN FLOOR TRACK ON IAW REO 670-53-00-812 REV -.
- [SDR VNAA20260623009](https://openairdocs.org/sdr/VNAA20260623009.md): Stringer · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R CORRODED BETWEEN BS 985 TO BS 1000. COMPLIED WITH REPAIR OF STR 26R BY INCORPORATING REO 670-53-61-2626 REV-.
- [SDR VNAA20260623008](https://openairdocs.org/sdr/VNAA20260623008.md): Frame · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 1000 FRAME IS CORRODED BETWEEN S26R TO S25R. REPAIRED CORRODED AREA OF FRAME IAW REO 670-53-61-2626 REV. P1.
- [SDR VNAA20260623007](https://openairdocs.org/sdr/VNAA20260623007.md): Door Sill · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Structure
  > AFT CARGO DOOR SILL IS CORRODED BETWEEN BS 1031 TO 1047. INSTALLED NEW SERVICABLE AFT CARGO DOOR SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.
- [SDR VNAA20260623006](https://openairdocs.org/sdr/VNAA20260623006.md): Floor Support · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SILL IS CORRODED BETWEEN BS 364 TO 379. REPAIRED RIGHT FLOOR SILL IAW REO 670-53-00-390 REV -.
- [SDR VNAA20260623005](https://openairdocs.org/sdr/VNAA20260623005.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL.9 APPROX BS 830 TO 985 HAS SIGNS OF CORROSION. INSTALLED NEW SEAT TRACK BETWEEN IAW 53-00-49-400-801(CONFIGA03).
- [SDR VNAA20260623004](https://openairdocs.org/sdr/VNAA20260623004.md): Frame · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Main, Frame
  > BS 333 FRAME IS CORRODED BETWEEN STR 27 TO STR 25L. REMOVED, FABRICATED NEW FRAME SECTOR FROM FRAME IAW 670-53-21-277 REV-. LOCATED AND DRILLED IAW SRM 51-40-11-001-001-A01, AND INSTALLED A NEW FRAME SECTOR IAW REO 670-53-21-2779 REV —, AND SRM 51-42-21-001-
- [SDR VNAA20260623003](https://openairdocs.org/sdr/VNAA20260623003.md): Angle · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR SILL MID CAP ANGLE IS CORRODED. REMOVED AND REPLACED PASSENGER DOOR SILL MID CAP ANGLE IAW SRM 51-42-13-001-001-A01 AND 51-42-02-001-001-A01.
- [SDR VNAA202606230002](https://openairdocs.org/sdr/VNAA202606230002.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK FS861-969 SEGMENT IS CORRODED. REMOVED LT SIDE SEAT TRACK AT FS861-969 IAW AMM 53-00-49-000-801-A03 AND INSTALLED NEW SERVICEABLE LH SIDE SEAT TRACK AT FS861-969 IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA20260623001](https://openairdocs.org/sdr/VNAA20260623001.md): Seat Track · corroded · Jun 23, 2026 · N518AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK FS785-861 SEGMENT IS CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE SEAT TRACK IAW AMM 53-00-49-400-801-A03.
- [SDR VNAA2024031511101](https://openairdocs.org/sdr/VNAA2024031511101.md): Manifold · faulted · Mar 14, 2024 · N518AE · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MESSAGE AFTER GEAR RETRACTION / REMOVED AND REPLACED #3 HYDRAULIC SYSTEM PUMP PRESSURE SWITCHES IAW CRJ 700 AMM 29ˆ’34ˆ’01ˆ’000/400ˆ’802. OPS CHECK AND LEAK CHECK GOOD. REMOVED AND INSTALLED NOSE WHEEL STEERING MANIFOLD IAW CRJ 700 AM

Next page: https://openairdocs.org/aircraft/N518AE/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 = 'N518AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N518AE/reports

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