# Service difficulty reports: N521AE

A list on [N521AE](https://openairdocs.org/aircraft/N521AE.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 3 · 138 reports

- [SDR VNAA2026041800011](https://openairdocs.org/sdr/VNAA2026041800011.md): Arm · gouged · Apr 15, 2026 · N521AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > GOUGE/DENT FOUND ON AFT INNER ARM OF FORWARD BAGGAGE BAY DOOR AFTER TROUBLESHOOTING TO DETERMINE CAUSE FOR DOOR TO BE DIFFICULT TO CLOSE AS REPORTED BY OPERATOR AT AIRCRAF ARRIVAL TO NQA FOR HEAVY CHECK. DETERMINED HARDWARE TO BE INCORRECTLY INSTALLED IN POSIT
- [SDR VNAA20262687185](https://openairdocs.org/sdr/VNAA20262687185.md): Access Panel · damaged · Apr 9, 2026 · N521AE · Cndair CL6002D24 · Wing, Plate/Skin
  > LEADING EDGE PRIMARY STRUCTURE 5771.25FH PERM REPAIR, PANEL 522CB
- [SDR VNAA2026041500007](https://openairdocs.org/sdr/VNAA2026041500007.md): Skin · damaged · Mar 31, 2026 · N521AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > TEMP TO PERM REPAIR: OVERSIZE FASTNER OF FWD BAGGAGE BAY DOOR DOUBLER AND SKIN.
- [SDR VNAA2026041500010](https://openairdocs.org/sdr/VNAA2026041500010.md): Shaft · worn · Mar 20, 2026 · N521AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > 1700FH PERM REPAIR - BAGGAGE DOOR SLEEK SHAFTS WORN WITHIN 1700 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES OR REPLACE PART.
- [SDR VNAA2026041500008](https://openairdocs.org/sdr/VNAA2026041500008.md): Skin Panel · scratched · Mar 13, 2026 · N521AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > 2650 FH PERM REPAIR - TEMPORARY REPAIR FOR SCRATCHES TO FUSELAGE SKIN PANEL BETWEEN STRG19L - STRG20L & BETWEEN FS333 - FS349 THIS TEMPORARY REPAIR IS VALID FOR 2650 FLIGHT HOURS FROM THE TIME OF INCORPORATION
- [SDR VNAA2026041500005](https://openairdocs.org/sdr/VNAA2026041500005.md): Skin · dented · Feb 7, 2026 · N521AE · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT 1 AND 2 HAVE DENT AT THE LEADING EDGE.
- [SDR VNAA2026041500004](https://openairdocs.org/sdr/VNAA2026041500004.md): Skin · dented · Feb 7, 2026 · N521AE · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT 1 AND 2 HAVE DENT AT THE LEADING EDGE.
- [SDR VNAA2026041500006](https://openairdocs.org/sdr/VNAA2026041500006.md): Skin · worn · Feb 6, 2026 · N521AE · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACKS HAVE WEAR AT SURFACES. SLAT 1 THROUGH 3 UPPER AND LOWER SURFACES.
- [SDR VNAA2026041500009](https://openairdocs.org/sdr/VNAA2026041500009.md): Skin · damaged · Feb 5, 2026 · N521AE · Cndair CL6002C10 · Leading Edge Devices
  > PERM REPAIR BEFORE 49,272.65 FH - LH IB SLAT WITHIN 6474.88 FHS FROM IR (BEFORE 49,272.65 FH), REPAIR, OR REPLACE THE DISCREPANT ITEM IN ACCORDANCE WITH APPROVED PROCEDURES. DURING VISUAL INSPECTION OF IB SLAT EDGE OF PREVIOUS TEMP REPAIR REF: EA 23-C7-57-00
- [SDR VNAA2026041500001](https://openairdocs.org/sdr/VNAA2026041500001.md): Bracket · cracked · Feb 5, 2026 · N521AE · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT BAGGAGE BAY DOOR INTERNAL HARNESS BRACKET IS CRACKED.
- [SDR VNAA2026041500002](https://openairdocs.org/sdr/VNAA2026041500002.md): Sleeve · chafed · Jan 22, 2026 · N521AE · Cndair CL6002C10 · Main Landing Gear Strut/Axle/Truck
  > LH MLG IB PISTON AXLE HAS CHIPPED METAL AT EDGE OF BRAKE UNIT ASSEMBLY BEARING SURFACE.
- [SDR VNAA2026041500003](https://openairdocs.org/sdr/VNAA2026041500003.md): Strut · scratched · Jan 21, 2026 · N521AE · Cndair CL6002C10 · Main Landing Gear Strut/Axle/Truck
  > RH MLG STRUT HAS 3 SCRATCHES ON REAR SIDE, ONE SCRATCH SHOWING BARE METAL.
- [SDR VNAA20250120003](https://openairdocs.org/sdr/VNAA20250120003.md): Web · corroded · Jan 19, 2025 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE REMOVING EXISTING L/H 280 LWR WEB REPAIR FOUND EXISTING STRUCTURE TO BE BEYOND REPAIR LIMITS. FULL R/H LWR WEB REPLACEMENT IS REQUIRED. FABRICATED, LOCATED, DRILLED AND INSTALLED LH LWR FS280 WEB AND DOUBLER IAW CRJ 700 SRM 53-11-10-201-004-A01.
- [SDR VNAA20250120002](https://openairdocs.org/sdr/VNAA20250120002.md): Web · corroded · Jan 19, 2025 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE REMOVING EXISTING R/H 280 LWR WEB REPAIR FOUND EXISTING STRUCTURE TO BE BEYOND REPAIR LIMITS. FULL R/H LWR WEB REPLACEMENT IS REQUIRED. REMOVED DAMAGED WEB AND PREVIOUS REPAIR IAW CRJ700 SRM 51-42-06-001-001-A01 AND COMPLIED WITH REPAIR #2 WEB REPLACEM
- [SDR VNAA2025F00004](https://openairdocs.org/sdr/VNAA2025F00004.md): Web · corroded · Jan 19, 2025 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE REMOVING EXISTING R/H 280 LWR WEB REPAIR FOUND EXISTING STRUCTURE TO BE BEYOND REPAIR LIMITS. FULL R/H LWR WEB REPLACEMENT IS REQUIRED. REMOVED DAMAGED WEB AND PREVIOUS REPAIR IAW CRJ700 SRM 51-42-06-001-001-A01 AND COMPLIED WITH REPAIR #2 WEB REPLACEME
- [SDR VNAA20250120001](https://openairdocs.org/sdr/VNAA20250120001.md): Floor Support · corroded · Jan 19, 2025 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL AT FS280 HAS CORROSION ON UPPER AND LOWER SURFACE. CORRECTIVE ACTION: REPAIRED CORROSION ON R/H FLOOR SILL IAW BOMBARDIER REO 670-53-21-139 REV. B DATED 2017-04-03
- [SDR VNAA2024121411101](https://openairdocs.org/sdr/VNAA2024121411101.md): Light · smoke · Dec 11, 2024 · N521AE · Cndair CL6002C10 · Flight Compartment Lighting
  > SMOKE FROM COLUMN ABOVE FO LIGHTING CONTROL PANEL AND STRONG ELECTRICAL SMELL. THE LOCATION OF THE SMOKE WAS IN THE COCKPIT, WHILE THE SOURCE WAS THE FO LIGHTING CONTROL PANEL. THE DURATION OF THE SMOKE EVENT WAS LESS THAN 10 MINUTES, AND NO MEDICAL ATTENTION
- [SDR VNAA2023110911102](https://openairdocs.org/sdr/VNAA2023110911102.md): Windshield · cracked · Nov 8, 2023 · N521AE · Cndair CL6002C10 · Flight Compartment Windows
  > AT CRUISE FL300 THE FO NOTICED THE WIND SHIELD CRACKING. WITHIN SECONDS THEY RECEIVED A RH WINDSHIELD HEAT CAUTION MESSAGE AND DECLARED AN EMERGENCY / REMOVED AND REPLACED RH WINDSHIELD IAW CRJ AMM 56-11-01-000/400-801-A01-PSA. OPS AND LEAK CHECK GOOD.
- [SDR VNAA202204049995](https://openairdocs.org/sdr/VNAA202204049995.md): Skin · corroded · Apr 4, 2022 · N521AE · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION ON SKIN REAR FUSELAGE FAIRING SEATLEMENT AREA BTW FS. 879 - 1015 (UNDER ACCESS 195AE, 195BB, 195DL, 196AR AND 196DR).
- [SDR VNAA202204049992](https://openairdocs.org/sdr/VNAA202204049992.md): Skin · corroded · Apr 4, 2022 · N521AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON EXTERNAL SKIN AT FWD FUSELAGE FAIRING SETTLEMENT AREA BTW. FS. 597 - FS. 693( UNDER ACCESS PANELS 191AB, 191BB, 192BB).
- [SDR VNAA202204049991](https://openairdocs.org/sdr/VNAA202204049991.md): Skin · none · Apr 4, 2022 · N521AE · Cndair CL6002C10 · Fuselage Structure (General)
  > WEAR ON SKIN BELOW DOUBLER AT POTABLE WATER FILL PANEL FS. 953 - FS. 969 BTW STRG. 23L AND STRG. 24L
- [SDR VNAA202204039995](https://openairdocs.org/sdr/VNAA202204039995.md): Floorbeam · corroded · Apr 3, 2022 · N521AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON UPPER FACE OF FLOOR SUPPORT BEAM AT LBL 9 BETWEEN FS. 581.00 AND FS. 597.00 AT PAX CABIN.
- [SDR VNAA202204039994](https://openairdocs.org/sdr/VNAA202204039994.md): Skin · worn · Apr 3, 2022 · N521AE · Cndair CL6002C10 · Fuselage Structure (General)
  > WEAR MARKS ON DOUBLER AND TRIPLER REPAIR FS. 969 -FS. 985 BETWEEN STRG. 26L AND 26R. CORRECTIVE ACTION:WEAR MARKS ON DOUBLER AND TRIPLER REPAIR FS
- [SDR VNAA202204039993](https://openairdocs.org/sdr/VNAA202204039993.md): Floorbeam · corroded · Apr 3, 2022 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR BEAM FS 333 AT STRG. 17 RBL FLOOR STRUCTURE PAX CABIN. CORRECTIVE ACTION:C
- [SDR VNAA202204039992](https://openairdocs.org/sdr/VNAA202204039992.md): Skin · corroded · Apr 3, 2022 · N521AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN FS. 1015- FS. 1031 ON STRG.24R AROUND DRAIN. CORRECTIVE ACTION: CORROSION ON EXTERNAL FUSELAGE SKIN BETWEEN FS. 1015- FS. 1031 ON STRG. 24R AROUND DRAIN. WAR REPAIRED PER EA 22-C7-53-192 REV.IR
- [SDR VNAA202204039991](https://openairdocs.org/sdr/VNAA202204039991.md): Skin · dented · Apr 3, 2022 · N521AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT ON FUSELAGE SKIN BTW FS. 533.00 TO FS. 549 ON STRG. 15LH. CORRECTIVE ACTION:DENT
- [SDR VNAA202105209991](https://openairdocs.org/sdr/VNAA202105209991.md): Angle · corroded · May 16, 2021 · N521AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS 280 TRANSVERSE BEAM, FWD COCKPIT FLOOR SUPPORT J ANGEL CORRODED. REMOVED AND REPLACED FS 280 J ANGLE PN CC670-33292-135 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR VNAA202102221111](https://openairdocs.org/sdr/VNAA202102221111.md): Circuit Breaker · tripped · Feb 20, 2021 · N521AE · Cndair CL6002C10 · Aileron Tab Control System
  > WHILE ENROUTE TO ELH, THE CA STATED THAT THE AILERON TRIM CIRCUIT BREAKER HAD POPPED. AFTER DISCUSSIONS WITH DISPATCH, THE CREW MADE THE DECISION TO RETURN TO FIELD FOR MAINTENANCE INSTEAD OF POSSIBLY STRANDING AN AIRCRAFT AT THE AIRPORT IN ELH. AN EMERGENCY W
- [SDR VNAA2020051511101](https://openairdocs.org/sdr/VNAA2020051511101.md): Smoke Warning · false activation · May 13, 2020 · N521AE · Cndair CL6002C10 · Smoke Detection
  > AFT LAV SMOKE MESSAGE WITH PAX IN LAV. NO DISCERNABLE SMOKE. MX PERFORMED OPS CHECK OF AFT LAV SMOKE DETECTOR IAW CRJ 700 AMM. OPS CHECK GOOD. SUSPECT PAX WAS VAPING.
- [SDR VNAA2020012761101](https://openairdocs.org/sdr/VNAA2020012761101.md): Wire · damaged · Jan 26, 2020 · N521AE · Cndair CL6002C10 · Light System Wiring
  > 3RD CEILING EMERGENCY FLOODLIGHT INOP. RE-CRIMPED 3RD CEILING EMERGENCY FLOODLIGHT GROUND WIRE IAW CRJ-700 ESPM 20-16-00 AND CRJ-700 AMM 33-51-09-000/400-801 [OPERATIONAL CHECK GOOD]
- [SDR VNAA201911221101](https://openairdocs.org/sdr/VNAA201911221101.md): Fire Bottle · false indication · Nov 21, 2019 · N521AE · Cndair CL6002C10 · Extinguishing System
  > ENGINE BOTTLE 2 LOW CAUTION MSG IN FLIGHT. C/W QRH. LANDED AT NEAREST SUITABLE AIRPORT.MX REMOVED AND REPLACED RH ENGINE FIRE BOTTLE. OPS CHECK GOOD.
- [SDR VNAA20191122102](https://openairdocs.org/sdr/VNAA20191122102.md): Connector · dirty · Nov 20, 2019 · N521AE · Cndair CL6002C10 · Fire Protection System Wiring
  > ENG BOTTLE 2 LO MESSAGE. APPROX. FL 340 WAS ON AND OFF FOR 4 MINUTES. RAN QRH AND LANDED AT NEAREST SUITABLE AIRPORT. REMOVED, CLEANED, & RE-SECURED CANNON PLUG ON #2 ENG FIRE BOTTLE IAW CRJ 700 AMM. OPS CHECK GOOD.
- [SDR VNAA2019070611101](https://openairdocs.org/sdr/VNAA2019070611101.md): Warning System · false activation · Jul 6, 2019 · N521AE · Cndair CL6002C10 · Landing Gear Position and Warning
  > GEAR DISAGREE WARNING MSG ILLUMINATED ON T/O. DEFERRED LANDING GEAR RETRACTION SYSTEM. MAINTENANCE PREFORMED SEVERAL GEAR SWINGS AND COULD NOT DUPLICATE THE PROBLEM, OPS CHECK GOOD. MEL CLEARED
- [SDR VNAA2019022411101](https://openairdocs.org/sdr/VNAA2019022411101.md): Relay · failed · Feb 24, 2019 · N521AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS STARTED CYCLING ON AND OFF DURING FLIGHT. REMOVED AND REPLACED RELAY K135 ON PCB5 IN JB11 IAW CRJ 700 ESPM 20-39-00 OPS CHECK GOOD
- [SDR VNAA2019021541101](https://openairdocs.org/sdr/VNAA2019021541101.md): Unknown · malfunctioned · Feb 14, 2019 · N521AE · Cndair CL6002C10 · Aileron Control System
  > ON APPROACH, CREW REPORTED LEFT WING DOWN. THEY TRIMMED THE A/C AND REPORTED THE CONDITION WORSENED AND THE AUTOPILOT DISCONNECTED. THEY DECLARED AN EMERGENCY AND LANDED IN CLT. UPON LANDING THE CREW REPORTED THEY HAD TO HOLD THE CONTROL WHEEL TO THE RIGHT TO
- [SDR SIMA201812282002](https://openairdocs.org/sdr/SIMA201812282002.md): Stringer · corroded · Dec 22, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > IN FWD AVIONICS BAY, STRINGER 25 RH HAS AREAS OF CORROSION BETWEEN FS 280.00 AND FS295.-C/A-RAR'D STRINGER 25R FROM FS 280.00-FS333.00 IAW SRM 51-42-06 AND SRM 51-42-20.
- [SDR SIMA2018122015002](https://openairdocs.org/sdr/SIMA2018122015002.md): Bulkhead Web · damaged · Dec 15, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > L/H COCKPIT BULKHEAD AFT LOWER WEB HAS OBLONGED RIVET HOLES. -C/A-REPAIRED L/H COCKPIT BULKHEAD LOWER WEB AT FS280.00 IAW SRM 53-11-10.
- [SDR SIMA20181215001](https://openairdocs.org/sdr/SIMA20181215001.md): Structure · dented · Dec 15, 2018 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DENT WITH CREASE FS1000-1015 STR 23L-24L, PERMANENT REPAIR. REPAIRED DENT IAW ERS-CR-53DF-3188 PTC AND ERS-CR-53MR-3331.
- [SDR SIMA20181213004](https://openairdocs.org/sdr/SIMA20181213004.md): Frame · corroded · Dec 13, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 319.00 FRAME IS CORRODED IN THE BELLY BETWEEN STRINGERS 26L AND 25R. INSTALLED NEW FRAME SECTION IAW SRM 51-42-06, AND 51-42-21.
- [SDR SIMA2018122112013](https://openairdocs.org/sdr/SIMA2018122112013.md): Floorbeam · corroded · Dec 12, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RT SIDE OF FLOORBEAM FS280.00 IS CORRODED BETWEEN BL0.00 AND THE OUTBD FLOOR SILL AND HAS A 1 INCH CRACK ON THE TOP FLANGE OUTBD OF RBL9.00. -C/A-RAR RT SIDE OF FLOORBEAM FS280.00 IAW SRM 51-42-06 AND SRM 51-42-13.
- [SDR SIMA2018122112014](https://openairdocs.org/sdr/SIMA2018122112014.md): Floorbeam · corroded · Dec 12, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LT SIDE OF FLOORBEAM FS280.00 IS CORRODED BETWEEN BL0.00 AND LBL27.00 AND HAS A 1 INCH CRACK BETWEEN RIVETS ON THE WEB OUTBD OF LBL9.00. -C/A-RAR L/H SIDE OF FLOORBEAM FS280.00 IAW SRM 51-42-06 SRM 51-42-13.
- [SDR SIMA20181220012](https://openairdocs.org/sdr/SIMA20181220012.md): Floorbeam · cracked · Dec 12, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > "L" ANGLE ON THE FWD SIDE OF FLOORBEAM FS280.00 JUST OUTBD OF THE STICKPUSHER ACTUATOR HAS A 1 INCH CRACK. -C/A-FABRICATED AND INSTALLED NEW "L" ANGLE ON FWD SIDE OF FLOORBEAM ON RH SIDE OF FS280.00 IAW ETN-CR-53-043, AND GPM 17-13.
- [SDR SIMA20181212011](https://openairdocs.org/sdr/SIMA20181212011.md): Floorbeam · cracked · Dec 12, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > "L" ANGLE ON THE AFT SIDE OF FLOORBEAM FS280.00 AT RBL 9.00 HAS 1.5 INCH CRACK. REMOVED AND REPLACED "L" ANGLE ASSEMBLY ON THE AFT SIDE OF FLOORBEAM FS280.00 AT RBL 9.00 IAW SRM 51-42-06.
- [SDR SIMA20181204006](https://openairdocs.org/sdr/SIMA20181204006.md): Stringer · corroded · Dec 4, 2018 · N521AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > IN FWD AVIONICS BAY, STRINGER 25R HAS AREAS OF CORROSION BETWEEN FS280-FS295. (AREAS MARKED IN RED GREASE PENCIL).-C/A-COMPLETE:RAR'D STR 25R FROM FS280-FS333 IAW SRM 51-42-06 AND SRM 51-42-20.
- [SDR SIMA20181204007](https://openairdocs.org/sdr/SIMA20181204007.md): Floor Support · corroded · Dec 4, 2018 · N521AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CPCP SSI 533009, LT OUTBD LONGITUDINAL FLOORBEAM AT FRAME FS1031.00 IS CORRODED. C/A-COMPLETE:REPAIRED FLOORBEAM AT FS1031.00 IAW ERS-CR-5300-3564.
- [SDR SIMA20180721003](https://openairdocs.org/sdr/SIMA20180721003.md): Light · inoperative · Jul 21, 2018 · N521AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS FOR LT OVER WING EXIT. TWO BULBS ARE BURNED OUT. REPLACED TWO BULBS FOR LT OVER WING EMERGENCY EXIT LIGHTS IN REFERENCE TO AMM 33-51-05. OPC GOOD.
- [SDR SIMA20180710001](https://openairdocs.org/sdr/SIMA20180710001.md): Pump · failed · Jul 10, 2018 · N521AE · Cndair CL6002C10 · Hydraulic Pump (Electric/Engine), Main
  > HYD 2 LOW PRESS IB FLT SPLRS IB SPOILERONS CAUTIONS MESSAGES DESCENDING THROUGH FL260. REMOVED AND REPLACED ENGINE DRIVEN PUMP (EDP) 2 IAW AMM 29-11-01. OPS CHECK GOOD. NO LEAKS NOTED AT THIS TIME PER FUEL AND OIL LEAK CHECK TASK 71-00-00-790-807.
- [SDR SIMA20180614001](https://openairdocs.org/sdr/SIMA20180614001.md): Light · inoperative · Jun 14, 2018 · N521AE · Cndair CL6002C10 · Emergency Lighting
  > DURING PS-1 CHECK FOUND CEILING EMERGENCY FLOOD LIGHT TO BE INOP AT ROW 16. R&R CEILING EMERGENCY FLOOD LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD.
- [SDR SIMA201805140005](https://openairdocs.org/sdr/SIMA201805140005.md): Wire · damaged · May 10, 2018 · N521AE · Cndair CL6002C10 · Equipment/Furnishings Wiring
  > AFT FA FLASHLIGHT NOT CHARGING. REPAIRED THE FLASHLIGHT SPLICE CONNECTION IAW ESPM 20-44-09. OPS CHECKED GOOD.
- [SDR SIMA20180311002](https://openairdocs.org/sdr/SIMA20180311002.md): Relay · failed · Mar 11, 2018 · N521AE · Cndair CL6002C10 · Emergency Lighting
  > EMER LTS CYCLING ON/OFF WHEN ARMED. FOUND RELAY K135 FAULTY USING WM 33-50-01. REMOVED AND REPLACED RELAY IAW MM 20-42-00 AND 24-06-11 OPS CKS OK.

Next page: https://openairdocs.org/aircraft/N521AE/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 = 'N521AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N521AE/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.