# Service difficulty reports: N515AE

A list on [N515AE](https://openairdocs.org/aircraft/N515AE.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 · 165 reports

- [SDR VNAA2026070220803](https://openairdocs.org/sdr/VNAA2026070220803.md): Sensor · unserviceable · Jul 1, 2026 · N515AE · Cndair CL6002C10 · Door Warning System
  > PASSENGER DOOR MASTER WARNING IN FLIGHT FOLLOWED BY PROX 1 FAULT. HANDLE POPPED OUT OF STOWED POSITION, FOUND WX CURTAIN INTERFERING WITH DOOR CLOSURE. MOVED CURTAIN. DEFERRED PAX DOOR PER MEL 52-21-01 CAT A. VERIFIED DOOR IND OPERATIVE PER MEL INSTRUCTIONS.
- [SDR VNAA202512020057](https://openairdocs.org/sdr/VNAA202512020057.md): Floorbeam · cracked · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RT FLIGHT COMPARTMENT FLOORBEAM CRACKED ON THE FWD SIDE OF THE BS 280
- [SDR VNAA202512020056](https://openairdocs.org/sdr/VNAA202512020056.md): Stringer · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 27 IS CORRODED BETWEEN BS 265 TO 250.
- [SDR VNAA202512020055](https://openairdocs.org/sdr/VNAA202512020055.md): Beam · gouged · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > LEFT UPPER C-DUCT LATCH BEAM NR 1 LUG IS GOUGED ON THE INBOARD SIDE.
- [SDR VNAA202512020054](https://openairdocs.org/sdr/VNAA202512020054.md): Hinge · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO COMPARTMENT STEP PLATE HAS CORRODED HINGE MARKED WITH RED TAPE. HEM670-35623-003 HINGE
- [SDR VNAA202512020053](https://openairdocs.org/sdr/VNAA202512020053.md): Stiffener · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > WHILE ACCESSING FOR REPAIR OF THE L/H FS280 LOWER BULKHEAD, FOUND THE STIFFENER AT LBL 26 TO BE CRACKED AT THE BOTTOM HOLE. DAMAGE IS OUT OF LIMITS IAW CRJ-700 SRM 53-00-00-101-001-A01. FS280 BULKHEAD FWD STIFFENER AT LBL 26.00 REQUIRES REPLACEMENT.
- [SDR VNAA202512020052](https://openairdocs.org/sdr/VNAA202512020052.md): Floorbeam · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > WHILE ACCESSING FOR REPAIR OF LT FS280 LOWER WEB, FOUND THE LT BS 280 FLOORBEAM TO HAVE DEEP PITTING CORROSION WITH THE DEEPEST DAMAGE BEING.048 AT LBL12 WHICH IS OUT OF LIMITS IAW CRJ-700 SRM 53-00-00-101-001-A01. LT BS 280 FLOORBEAM REQUIRES REPLACEMENT.
- [SDR VNAA202512020051](https://openairdocs.org/sdr/VNAA202512020051.md): Floorbeam · cracked · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LBL9 COCKPIT FLOOR BEAM PANEL SUPPORT ANGLE P/N: CC670-33199-3 HAS ONE EACH CRACK PROPOGATED FROM HOLE @ AFT END OF ANGLE. CC670-33199-3S PANEL SUPPORT BRACKET
- [SDR VNAA202512020050](https://openairdocs.org/sdr/VNAA202512020050.md): Washer · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Structure (General)
  > F.S 280 LH LOWER BULKHEAD @ LBL 9 HAS SEVERE INTERGRANULAR CORROSION CAUSING LOWER WEB CLOSE OUT ANGLE TO BE PUSHED OUT. 670-53-11-594-1 WEB
- [SDR VNAA202512020049](https://openairdocs.org/sdr/VNAA202512020049.md): Washer · damaged · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Structure (General)
  > RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00557371, SO# 400382749 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7 WASHER
- [SDR VNAA202512020048](https://openairdocs.org/sdr/VNAA202512020048.md): Washer · damaged · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Structure (General)
  > PER CUSTOMER REQUEST, SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00557370, SO# 400382748 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7). CC670-10635-7 WASHER
- [SDR VNAA202512020047](https://openairdocs.org/sdr/VNAA202512020047.md): Trunnion · corroded · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Hydraulic System, Main
  > FOUND FOUR TRUNNION BODIES CORRODED ON LT FLS 24.00, 65.50, 102.90, AND FLS 40.40 THAT REQUIRE FABRICATION. MHI601R14261-601R14261 REV NC.
- [SDR VNAA202512020046](https://openairdocs.org/sdr/VNAA202512020046.md): Bracket · cracked · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FOUND CRACK ON MOUNTING BRACKET FOR HYDRAULIC ACCUMULATOR ON LT SIDE OF TRU BAY.
- [SDR VNAA202512020045](https://openairdocs.org/sdr/VNAA202512020045.md): Bracket · damaged · Dec 5, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > INDICATIONS NOTED AT THE REAR SPAR LATERAL BEAM SIDE STAY BRACKET LHS OUTBD. AFT BORE APPROX..500" IN LENGTH AND 80% F.S.H FAILING NDT SH670-35627. WINDSHIELD FWD LOWER SILL
- [SDR VNAA202512020044](https://openairdocs.org/sdr/VNAA202512020044.md): Fitting · damaged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HSTA SCREW JACK FITTING HAD DAMAGE AND REQ REPAIR.
- [SDR VNAA202512020043](https://openairdocs.org/sdr/VNAA202512020043.md): Window Frame · gouged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > WHILE CLEANING COCKPIT DISCOVERED THERE TO BE A GOUGE IN RH BELOW WINDSHIELD SILL SUPPORT STRUCTURE
- [SDR VNAA202512020042](https://openairdocs.org/sdr/VNAA202512020042.md): Hinge Fitting · gouged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Spoilers
  > NR 1 SIDE OF INBD MULTI FUNCTIONAL SPOILER ATTACHMENT HINGE FITTING IS GOUGED.
- [SDR VNAA202512020041](https://openairdocs.org/sdr/VNAA202512020041.md): Lug · chafed · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STABILIZER OTBD LUG FITTINGS HAVE CHAFING DAMAGE FROM CONTACT WITH THE ANTI-ROTATION DEVICES.
- [SDR VNAA202512020040](https://openairdocs.org/sdr/VNAA202512020040.md): Skin · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > PITTING CORROSION LOCATED ON THE EXTERIOR OF FUSELAGE BETWEEN F.S 501 AND F.S 517 AT STRINGER 27. REQUIRES EVALUATION. SH670-33202 SKIN
- [SDR VNAA202512020039](https://openairdocs.org/sdr/VNAA202512020039.md): Skin · damaged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND TWO ELONGATED FASTENER HOLES ON SKIN AT FS 986 STGR 27.
- [SDR VNAA202512020038](https://openairdocs.org/sdr/VNAA202512020038.md): Window Frame · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT WINDSHIELD POST SHOWS SIGNS OF CRACKING ON UPPER SIDE.
- [SDR VNA2025F00043](https://openairdocs.org/sdr/VNA2025F00043.md): Window Frame · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT WINDSHIELD POST SHOWS SIGNS OF CRACKING ON UPPER SIDE.
- [SDR VNAA202512020037](https://openairdocs.org/sdr/VNAA202512020037.md): Window Frame · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT WINDSHIELD POST SHOWS EVIDENCE OF CRACKING ON UPPER SIDE.
- [SDR VNAA202512020036](https://openairdocs.org/sdr/VNAA202512020036.md): Ring · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > CORROSION FOUND IN RT ENGINE RING AT A4 ATTACHMENT BOLT HOLE (1EA) MARKED WITH ZIP TIE THROUGH DISCREPANT BOLT HOLE.
- [SDR VNAA202512020035](https://openairdocs.org/sdr/VNAA202512020035.md): Web · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Rudder Structure
  > RUDDER LOWER WEB HAS AREAS OF CORROSION ON INNER SURFACE. CC670-22135-3 LOWER WEB
- [SDR VNAA202512020034](https://openairdocs.org/sdr/VNAA202512020034.md): Web · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD WEB FOUND TO BE CRACKED.
- [SDR VNAA202512020033](https://openairdocs.org/sdr/VNAA202512020033.md): Web · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT WEB FOUND TO BE CRACKED. REQUIRES REPLACEMENT.
- [SDR VNAA202512020032](https://openairdocs.org/sdr/VNAA202512020032.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK IS CORRODED BETWEEN F.S. 985 TO F.S. 1000.
- [SDR VNAA202512020031](https://openairdocs.org/sdr/VNAA202512020031.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 18 SEAT TRACK IS CORRODED BETWEEN BS 939 - 985.
- [SDR VNAA202512020030](https://openairdocs.org/sdr/VNAA202512020030.md): Frame · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND CORROSION ON BS 379 RT FRAME BETWEEN S20R AND S25R.
- [SDR VNAA202512020029](https://openairdocs.org/sdr/VNAA202512020029.md): Plate · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR KICKPLATE ANGLE CORRODED OUTBOARD SIDE, FWD TO AFT.
- [SDR VNAA202512020028](https://openairdocs.org/sdr/VNAA202512020028.md): Mount Bracket · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Exterior Lighting
  > LEFT PYLON LOGO LIGHT MOUNTING STRUCTURE HAS CORROSION IN MULTIPLE PLACES. MM 670-37285-S0201 LOGO LIGHT MOUNTING PLATE.
- [SDR VNAA202512020027](https://openairdocs.org/sdr/VNAA202512020027.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT RAIL BETWEEN CS 860 AND 969 IS CORRODED.
- [SDR VNAA202512020026](https://openairdocs.org/sdr/VNAA202512020026.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK LBL 9, BS 517 - 549 IS CORRODED.
- [SDR VNAA202512020025](https://openairdocs.org/sdr/VNAA202512020025.md): Bracket · chafed · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Main Landing Gear
  > RIGHT MLG SIDE STAY BRACKET IS CHAFED.
- [SDR VNAA202512020024](https://openairdocs.org/sdr/VNAA202512020024.md): Angle · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID CAP ANGLE IS CORRODED.
- [SDR VNAA202512020023](https://openairdocs.org/sdr/VNAA202512020023.md): Mount Fitting · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > GALLEY MOUNT FITTING IS CORRODED BETWEEN F.S. 280 TO F.S. 295 AND BETWEEN RBL 9 TO RBL 18.
- [SDR VNAA202512020022](https://openairdocs.org/sdr/VNAA202512020022.md): Striker · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > GALLEY SERVICE DOOR LOWER SEAL STRIKER IS CORRODED ON THE AFT SIDE AROUND SCREW HOLES.
- [SDR VNAA202512020020](https://openairdocs.org/sdr/VNAA202512020020.md): Intercostal · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL IS CORRODED BETWEEN F.S. 319 TO F.S. 333.
- [SDR VNAA202512020019](https://openairdocs.org/sdr/VNAA202512020019.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 FLOOR SEAT TRACK IS CORRODED BETWEEN F.S. 349 TO F.S. 469
- [SDR VNAA202512020018](https://openairdocs.org/sdr/VNAA202512020018.md): Post · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > FLIGHT COMPARTMENT RBL 9 ENTRY POST ARE CORRODED AT F.S. 280.
- [SDR VNAA202512020017](https://openairdocs.org/sdr/VNAA202512020017.md): Floorbeam · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLIGHT COMPARTMENT LBL 9 ENTRY POST ARE CORRODED AT F.S. 280. 5-32993.
- [SDR VNAA202512020016](https://openairdocs.org/sdr/VNAA202512020016.md): Web · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > NOSE JACK FITTING RT WEB IS CORRODED.
- [SDR VNAA202512020015](https://openairdocs.org/sdr/VNAA202512020015.md): Web · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > NOSE JACK FITTING LT WEB IS CORRODED.
- [SDR VNAA202512020014](https://openairdocs.org/sdr/VNAA202512020014.md): Hinge · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > LEFT MLG DOOR ATTACHMENT FITTINGS FWD AND AFT ARE CORRODED. DWG CC670-10552 HINGE.
- [SDR VNAA202512020013](https://openairdocs.org/sdr/VNAA202512020013.md): Skin · cracked · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > RIGHT FUSELAGE SKIN IS CRACKED AROUND THE AFT TRU DOOR LATCH. TRU BAY DOOR LANDING
- [SDR VNAA202512020012](https://openairdocs.org/sdr/VNAA202512020012.md): Seat Track · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAL TRACK AT RBL9 BETWEEN BS 349 - 485 HAS EVIDENCE OF CORROSION SH670-32159-1.
- [SDR VNAA202512020011](https://openairdocs.org/sdr/VNAA202512020011.md): Seat Track · damaged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > PASSENGER SEAT TRACK AT LBL 9 BETWEEN BS 379 - 485 HAS HEAVY CORROSION SH670-32249-3.
- [SDR VNAA202512020010](https://openairdocs.org/sdr/VNAA202512020010.md): Retainer · damaged · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER SEAL RETAINER IS DAMAGED.
- [SDR VNAA202512020009](https://openairdocs.org/sdr/VNAA202512020009.md): Frame · corroded · Dec 4, 2025 · N515AE · Cndair CL6002C10 · Aerodynamic Fairings
  > WING TO FUSELAGE FAIRING FRAME IS CORRODED AT STGR 27.

Next page: https://openairdocs.org/aircraft/N515AE/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 = 'N515AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N515AE/reports

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