# Service difficulty reports: N522AE

A list on [N522AE](https://openairdocs.org/aircraft/N522AE.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 · 156 reports

- [SDR VNAA2026081922901](https://openairdocs.org/sdr/VNAA2026081922901.md): Skin · dented · Aug 17, 2026 · N522AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT DAMAGE AT FS280.00 AND S24R, PERFORMED ALL WORK USING STEPS AND DRAWINGS LISTED IN REO 670-53-11-2357.
- [SDR VNAA2026072521101](https://openairdocs.org/sdr/VNAA2026072521101.md): Window · cracked · Jul 22, 2026 · N522AE · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT SIDE WINDOW CRACKED WITH ASSOCIATED RT WINDOW HEAT CAUTION MESSAGE. REMOVED AND INSTALLED RT SIDE WINDOW IAW AMM 56-12-01-400-801-A01. OPS TEST OF WINDOW TEMP CONTROLLER GOOD. NO LEAKS PRESENT AT THIS TIME.
- [SDR 1Q2R2026061000001](https://openairdocs.org/sdr/1Q2R2026061000001.md): Skin · gouged · May 26, 2026 · N522AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > AFT BAGGAGE BAY DOOR FUSELAGE SKIN GOUGED AT FS1000.00 BETWEEN STGR 15 AND STGR 16. PERFORMED REPAIR TO AREA IN ACCORDANCE WITH REO NO. 670-53-61-2717 REV. --, DATED MAY 4TH, 2026.
- [SDR 1Q2R2026061100001](https://openairdocs.org/sdr/1Q2R2026061100001.md): Latch · nicked · May 22, 2026 · N522AE · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > RIGHT HAND TRANS COWL NICKED/DENTED ON THE LATCH DOOR BELOW THE FORWARD LATCH. DAMAGE MEASURED 3/8"L X 1.0"W. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH MHI RJ REO 670-54-21-1816 REV. --, DATED MAY 5TH, 2026, AND REPLACED LATCH.
- [SDR 1Q2R2026061000002](https://openairdocs.org/sdr/1Q2R2026061000002.md): Skin · damaged · May 22, 2026 · N522AE · Cndair CL6002C10 · Wing, Plate/Skin
  > LEFT-HAND WING LEADING EDGE DAMAGED AT RIB SS64.46, 5TH FASTENER HOLE FROM BOTTOM. PERFORMED REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-41-695 REV. --, DATED APRIL 27, 2026.
- [SDR 1Q2R2026061000003](https://openairdocs.org/sdr/1Q2R2026061000003.md): Access Panel · damaged · May 20, 2026 · N522AE · Cndair CL6002C10 · Wing, Plate/Skin
  > RIGHT HAND INBOARD FLAP INNER UPPER SKIN DAMAGED AT FLS 24.00 AND 2IN FROM VANE CRADLE ACCESS PANEL. PERFORMED REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-52-352 REV. --, DATED MARCH 28, 2017.
- [SDR 1Q2R202606100004](https://openairdocs.org/sdr/1Q2R202606100004.md): Panel · dented · May 15, 2026 · N522AE · Cndair CL6002C10 · Trailing Edge Flaps
  > LEFT INBOARD LEADING EDGE FLAP SKIN DENTED BETWEEN ST 29.00 AND 60.50. PERFORMED PERMANENT REPAIR IAW REO 670-57-52-658, REV--.
- [SDR 1Q2R2026042700001](https://openairdocs.org/sdr/1Q2R2026042700001.md): Fitting · temp repair · Apr 23, 2026 · N522AE · Cndair CL6002C10 · Wing Main, Frame Structure
  > 2-OFF AREAS OF BLENDED CHAFE DAMAGE TO MAIN LANDING GEAR SIDE STAY FITTING (DWG: CC690-10608, AL ALY 7050-T7452, 0.310" +/- 0.010" NOMINAL THICKNESS, REF), RHS. TEMPORARY REPAIR PREVIOUSLY PERFORMED UNDER PSA AIRLINES EA NO: 57-2025-0371 REV --, DATED 2025-03-
- [SDR 1Q2R2026061200001](https://openairdocs.org/sdr/1Q2R2026061200001.md): Skin · gouged · Apr 17, 2026 · N522AE · Cndair CL6002C10 · Leading Edge Devices
  > EA 57-2025-0380 FOR SLAT PANEL 622EZ REQUIRED PERMANENT REPAIR. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH MHI RJ REO 670-57-42-2470 REV. --, DATED APRIL 13, 2026.
- [SDR VNAA2025061711102](https://openairdocs.org/sdr/VNAA2025061711102.md): Unknown · noise · Jun 15, 2025 · N522AE · Cndair CL6002C10 · Standard Practices/Structures
  > AFTER TAKEOFF LOUD ELECTRIC CRACKLING/BUZZING NOISE FROM FO SIDE OF FLIGHT DECK / INSPECTED NOSE COMPARTMENTS/AVIONICS BAY FOR ANY LOOSE ITEMS. PRESSURIZED PLANE IAW CRJ700 AMM 21-31-00-910-801-A01-PSA TO ~4.0 DELTA AND USED RADIOS TO CONTACT TOWER. OPS CHECK
- [SDR VNAA2025050111101](https://openairdocs.org/sdr/VNAA2025050111101.md): Controller · faulted · Apr 30, 2025 · N522AE · Cndair CL6002C10 · Fuel Indicating System
  > DESPITE BOTH ENGINES INDICATING SIMILAR FUEL BURN FUEL WAS DEPLETING FROM LEFT TANK AT TWICE THE EXPECTED RATE. / TROUBLESHOT IAW CRJ 700 FIM 28-41-22-810-804-A01-PSA. NO FAULT CODES AT REFUEL/DEFUEL PANEL. SHOT WIRES ALL WIRES SHOT GOOD. REMOVED AND REPLACED
- [SDR VNAA2025032711101](https://openairdocs.org/sdr/VNAA2025032711101.md): Control Panel · faulted · Mar 25, 2025 · N522AE · Cndair CL6002C10 · Cabin Pressure Control System
  > AUTO PRESSURE CAUTION MSG IN FLIGHT / REMOVED AND REPLACED CABIN PRESSURE CONTROL PANEL IAW AMM 21-33-01-000/400-801-A01-PSA. OPS TEST GOOD AT THIS TIME IAW AMM 21-33-01-710-801-A01. PRESSURIZED AIRCARFT IAW AMM 21-31-00-910-801-A01-PSA FAULT DID NOT RE-OCCUR.
- [SDR VNAA202302161111](https://openairdocs.org/sdr/VNAA202302161111.md): Actuator · unserviceable · Feb 14, 2023 · N522AE · Cndair CL6002C10 · Stabilizer Control System
  > PITCH FEEL FAULT STATUS MSG / COMPLIED WITH MIPM FOR PITCH FEEL FAULT. REMOVED AND REPLACED THE LINEAR PITCH-FEEL ACTUATOR IAW CRJ 700 AMM 27-31-23-000-801-A01.
- [SDR VNAA202206151113](https://openairdocs.org/sdr/VNAA202206151113.md): Sensor · fault message · Jun 12, 2022 · N522AE · Cndair CL6002C10 · Brake
  > EN ROUTE TO PHL THE CREW FOR 5349 GOT A BRAKE TEMP OVERHEAT MASTER WARNING MESSAGE. THEY RAN THE QRH AND GOT THE MESSAGE TO RESET AND CONTINUE DIRECT TO PHL. THEY MADE THE DECISION TO DECLARE A EMERGENCY AND EMERGENCY VEHICLES DID ROLL BUT WERE NOT NEEDED. THE
- [SDR VNAA202205261112](https://openairdocs.org/sdr/VNAA202205261112.md): Light · wrong part · May 24, 2022 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY FLOOR PATH LIGHTING APPEARS TO BE WRONG EFFECTIVITY / REMOVED IMPROPER FLOOR-PATH MARKING AND PARTIALLY INSTALLED CORRECT FLOOR-PATH MARKING THAT WAS AVAILABLE FROM GALLEY TO SEAT 3FD ON RIGHT SIDE. ON LEFT SIDE INSTALLED FROM GALLEY TO SEAT 3A IAW C
- [SDR VNAA202205131111](https://openairdocs.org/sdr/VNAA202205131111.md): Galley · odor · May 12, 2022 · N522AE · Cndair CL6002C10 · Air Distribution Fan
  > FA SMELLED SMOKE IN GALLEY, CA CONFIRMED SMELL OF SMOKE WHILE/AFTER BOARDING. CALLED MX BUT SMELL DISSIPATED BEFORE MX ARRIVED, MX COULD NOT REPLICATE, OR FIND SOURCE OF SMELL.. SMELL OF SMOKE IN FWD GALLEY BIN / C/W CRJ 700 FIM 21-22-00-810-806-A01. C/W CRJ 7
- [SDR VNAA2022032799914](https://openairdocs.org/sdr/VNAA2022032799914.md): Frame · corroded · Mar 26, 2022 · N522AE · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 1015.00 BTW STGR 25RH AND STGR 26RH. CORRECTIVE ACTION:
- [SDR VNAA2022032799913](https://openairdocs.org/sdr/VNAA2022032799913.md): Floorbeam · corroded · Mar 26, 2022 · N522AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON FLOORBEAM FS 985.00 TO FS 1098 27LBL AFT BAGGAGE BAY. CORRECTIVE ACTION:
- [SDR VNAA2022032799911](https://openairdocs.org/sdr/VNAA2022032799911.md): Stringer · corroded · Mar 26, 2022 · N522AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON SKIN SPLICE FS STA 281 BETWEEN STRINGERS 24L TO 24R AT MAIN AVIONICS COMPARTMENT. (E/E). CORRECTIVE ACTION:
- [SDR VNAA2022032799910](https://openairdocs.org/sdr/VNAA2022032799910.md): Angle · weak · Mar 26, 2022 · N522AE · Cndair CL6002C10 · Passenger/Crew Doors
  > WEAR ON FORWARD ANGLE SUPPORT BTW FS 320 FS 311, (NEAR ACCESS PANEL 832AL OF PASSANGER DOOR. CORRECTIVE ACTION:
- [SDR VNAA202203249991](https://openairdocs.org/sdr/VNAA202203249991.md): Floorbeam · corroded · Mar 24, 2022 · N522AE · Bombdr CL6002D15 · Fuselage Main, Floor Beam
  > CORRISION ON FLOORBEAM, 27RBL. IN FS STA-985.00 TO FS STA 1098 AFT BAGGAGE BAY. REPAIRED PER EA 22-C7-53-0193 REV.IR SECTION III, PERMANENT REPAIR
- [SDR VNAA202203219994](https://openairdocs.org/sdr/VNAA202203219994.md): Floorbeam · corroded · Mar 21, 2022 · N522AE · Bombdr CL6002D15 · Fuselage Structure (General)
  > CORROSION ON FLOOR BEAM 9RBL AT FS STA=985.00 TO FS =1098 AT AFT BAGGAGE BAY..CORRECTIVE ACTION: REPAIRED PER EA 22-C7-53-0194 REV. IR SECTION III, PERMANENT REPAIR.
- [SDR VNAA202203219992](https://openairdocs.org/sdr/VNAA202203219992.md): Rib · cracked · Mar 21, 2022 · N522AE · Bombdr CL6002D15 · Wing, Rib/Bulkhead
  > CRACK ON RIB LEADING EDGE SS58.41 AT LEFT WING LEADING EDGE. CORRECTIVE ACTION: CRACK ON RIB LEADING EDGE SS58.41 AT LEFT W
- [SDR VNAA202203219991](https://openairdocs.org/sdr/VNAA202203219991.md): Stringer · corroded · Mar 21, 2022 · N522AE · Bombdr CL6002D15 · Fuselage Main, Longeron/Stringer
  > SB SB 670BA-25-112-REQ-GENERAL. CORROSION ON STGR 27 BTE FS310 TO FS319 AT E/E COMPARTMENT. CORRECTIVE ACTION: -25-112-REQ-GENERAL. CORROSION ON STGR 27 BTE FS310 TO FS319 AT E/E COMPARTMENTWAS R
- [SDR VNAA202203159992](https://openairdocs.org/sdr/VNAA202203159992.md): Frame · corroded · Mar 15, 2022 · N522AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CORROSION ON FRAME STA. 1015.00, BTW STGR.26R ANS STGR.25RH AT AFT BAGGAGE BAY.
- [SDR VNAA202203159991](https://openairdocs.org/sdr/VNAA202203159991.md): Floorbeam · corroded · Mar 15, 2022 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM 27RBL, FS 980 TO FS 1098 AT AFT BAGGAGE BAY. CORRECTIVE ACTION: CORROSION ON FLOOR BEAM 27 RBL, FS 980 T
- [SDR VNAA202203149991](https://openairdocs.org/sdr/VNAA202203149991.md): Stringer · gouged · Mar 14, 2022 · N522AE · Cndair CL6002C10 · Fuselage Structure (General)
  > GOUGES ON STRINGER AND RIVET DAMAGED, STGR. 22 RH BTW FS1126.00/1144.00 CORRECTIVE ACTION. STRINGER AND RIVET. STGR 22RH BTW FS1126.00 / 1144.00 WAS REPAIRED PER EA 22-C7-53-0258 REV, IR
- [SDR VNAA202104011112](https://openairdocs.org/sdr/VNAA202104011112.md): Skin · dented · Mar 31, 2021 · N522AE · Cndair CL6002C10 · Leading Edge Devices
  > DURING OVERNIGHT OPERATIONS AT DAYTON OH (DAY) TECHNICIANS FOUND A DENT IN THE LEADING EDGE OF THE LH #1 SLAT (P/N: CC670-12600-3 S/N 10146) INBD OF TRACK 1-3. THE DENT MEASURES 1.75" L X 3" W X.004" MAX REPORTED DEPTH AND IS NOT WITHIN ALLOWABLE DAMAGE LIMIT
- [SDR VNAA2021040100011](https://openairdocs.org/sdr/VNAA2021040100011.md): Skin · dented · Mar 31, 2021 · N522AE · Cndair CL6002C10 · Leading Edge Devices
  > DURING OVERNIGHT OPERATIONS AT DAYTON OH (DAY) TECHNICIANS FOUND A DENT IN THE LEADING EDGE OF THE LH #1 SLAT (P/N: CC670-12600-3 S/N 10146) INBD OF TRACK 1-3. THE DENT MEASURES 1.75" L X 3" W X.004" MAX REPORTED DEPTH AND IS NOT WITHIN ALLOWABLE DAMAGE LIMIT
- [SDR VNAA2020061211101](https://openairdocs.org/sdr/VNAA2020061211101.md): Lens · missing · Jun 9, 2020 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > Ï¿½FORWARD FACING CEILING EMERGENCY EXIT SIGN MISSING RED LENS CAP. INSTALLED RED LENS CAP ON FWD SIDE OF CEILING EMERGENCY EXIT SIGN IAW CRJ 700 AMM 33-51-07-400-801.
- [SDR VNAA2020061211102](https://openairdocs.org/sdr/VNAA2020061211102.md): Lens · missing · Jun 9, 2020 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > AFT FACING CEILING EMERGENCY EXIT SIGN MISSING RED LENS CAP. INSTALLED RED LENS CAP ON AFT SIDE OF CEILING EMERGENCY EXIT SIGN IAW AMM 33-51-07-400-801.
- [SDR VNAA2020032721101](https://openairdocs.org/sdr/VNAA2020032721101.md): Warning System · false activation · Mar 26, 2020 · N522AE · Cndair CL6002C10 · Cabin Pressure Control System
  > AUTO PRESS CAUTION MSG AFTER T/O. CYCLED SYSTEM CBS, FAULT CLEARED AND DID NOT RETURN, PERFORMED SYSTEM OPS CHECKS, OPS CHECKS GOOD AT THIS TIME IAW 21-31-04-710-801.
- [SDR VNAA2020021751103](https://openairdocs.org/sdr/VNAA2020021751103.md): Thermocouple · failed · Feb 15, 2020 · N522AE · Cndair CL6002C10 · Landing Gear Brake System
  > BRAKE OVERHEAT WARNING AFTER GEAR RETRACTION, FLIGHT RETURNED TO FIELD. MAINTENANCE REMOVED AND REPLACED THE #4 BRAKE THERMOCOUPLE OPS CHECK GOOD.
- [SDR VNAA2019112751103](https://openairdocs.org/sdr/VNAA2019112751103.md): Door · unknown · Nov 25, 2019 · N522AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR WILL NOT CLOSE. MAINTENANCE PERFORMED AN OPERATIONS CHECK OF THE PASSENGER DOOR AND IT OPERATIONS CHECKED GOOD.
- [SDR VNAA2019112751102](https://openairdocs.org/sdr/VNAA2019112751102.md): Gate · lack of lube · Nov 25, 2019 · N522AE · Cndair CL6002C10 · Passenger/Crew Doors
  > UNABLE TO CLOSE PASSENGER DOOR. MAINTENANCE LUBED THE PASSENGER DOOR FLAPPER DOOR AND THE PASSENGER DOOR OPERATIONS CHECKED GOOD.
- [SDR VNAA2019111511102](https://openairdocs.org/sdr/VNAA2019111511102.md): Battery Pack · failed · Nov 11, 2019 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS ROW 16 FACING FWD AND BOTH SIDES ROW 8 COME ON AND FADE OUT. REMOVED AND REPLACED ALL 3 EPSU BATTERY PACKS IAW CRJ 700 AMM 33-51-17-000/400-801-A01 OPS TEST GOOD IAW AMM 33-51-17-710-801. REPLACED BATTERY PACKS P/N 2013-1A S/N 123927, S/N 1238
- [SDR VNAA2019101841103](https://openairdocs.org/sdr/VNAA2019101841103.md): Acm · failed · Oct 14, 2019 · N522AE · Cndair CL6002C10 · Cabin Cooling System
  > SHORTLY AFTER PUSH ON FLIGHT 5148 DCA-BDL TAIL N522AE, THE CABIN CREW NOTED SMOKE IN THE CABIN. THIS OCCURRED DURING TAXI. THE CREW MADE THE DECISION TO OPEN THE MAIN CABIN DOOR, AND EVACUATE THE PASSENGERS IN THE ALLEY WAY. ONCE THE MAIN CABIN DOOR EVACUATION
- [SDR SIMA20190305001](https://openairdocs.org/sdr/SIMA20190305001.md): Gusset · corroded · Mar 5, 2019 · N522AE · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > AVIONICS BAY DOOR FWD. GUSSET AT STR. LOCATION 26L IS CORRODED FS 364.00. C/A- REMOVED AND REPLACED AVIONICS BAY DOOR FWD GUSSET AT STR 26L, FS 364.00. IAW SRM 51-42-06, 51-42-20 AND 51-40-11.
- [SDR SIMA20190304007](https://openairdocs.org/sdr/SIMA20190304007.md): Bulkhead · corroded · Mar 4, 2019 · N522AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AFT SIDE OF THE COCKPIT BULKHEAD AT FS280.00 HAS CORROSION BETWEEN LBL 18.00 AND LBL 27.00 FLOOR LEVEL. C/A-COMPLETED INSTALLATION OF LT COCKPIT BULKHEAD AT FS280.00 WITH NEW WEB AND BUTTSTRAP IAW SRM 53-10-11, SRM 51-42-06, SRM 51-42-10. REF NRWC E698434 FOR
- [SDR SIMA20190301007](https://openairdocs.org/sdr/SIMA20190301007.md): Structure · cracked · Mar 1, 2019 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > 1/4 INCH CRACK ON FWD EQUIPMENT COMPARTMENT FLOOR ON LEFT SIDE AT FRAME FS193.00. C/A-COMPLETED REPAIR TO LT FWD ELECTRICAL BAY FLOOR AT FS193.00 IAW ETN-CR-53-099.
- [SDR SIMA20190301006](https://openairdocs.org/sdr/SIMA20190301006.md): Plate · cracked · Mar 1, 2019 · N522AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > JB6 CIRCUIT BREAKER BOX MOUNT PLATE HAS 2 CRACKS. 1/2 INCH TOTAL LENGTH. C/A-REMOVED AND REPLACE'D JB6 CIRCUIT BREAKER BOX MOUNT PLATE IAW SRM 51-42-06.
- [SDR SIMA20190301004](https://openairdocs.org/sdr/SIMA20190301004.md): Floorbeam · cracked · Mar 1, 2019 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280.00 FLOORBEAM HAS CORROSION BETWEEN LBL9.00 AND LBL18.00. AND HAS A 1 INCH CRACK ON THE TOP FLANGE OUTBD OF LBL9.00. C/A-REMOVED AND REPLACED LT FLOORBEAM CROSS MEMBER SEGMENT AT FS280.00 IAW SRM 51-42-06.
- [SDR SIMA20190220004](https://openairdocs.org/sdr/SIMA20190220004.md): Beam · corroded · Feb 20, 2019 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT OUTBD LONGITUDINAL BEAM HAS CORROSION AT CROSSBEAM FS1031.00. C/A-COMPLIED WITH REPAIR OF LT OUTBD LONGITUDINAL BEAM IAW SRM 53-00-41.
- [SDR SIMA20190218009](https://openairdocs.org/sdr/SIMA20190218009.md): Connector · disconnected · Feb 18, 2019 · N522AE · Cndair CL6002C10 · Light System Wiring
  > EMERGENCY EXIT LIGHT FACING AFT ON LT WARDROBE IS INOP. C/A-COMPLETE:T/S AND FOUND ELECTRICAL CONNECTOR P341 NOT CONNECTED. CONNECTED P341 EMERGENCY EXIT LIGHT FACING AFT ON LT WARDROBE OPERATIONAL CHECKS GOOD IAW AMM 33-51-00-710-802 OPERATIONAL TEST OF THE E
- [SDR SIMA20190218008](https://openairdocs.org/sdr/SIMA20190218008.md): Beam · corroded · Feb 18, 2019 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT INBD LONGITUDINAL BEAM HAS CORROSION AT CROSSBEAM FS1031.00. C/A-C/W REPAIR OF RT I/B LONGITUDINAL BEAM IAW SRM 53-00-41.
- [SDR SIMA201812287002](https://openairdocs.org/sdr/SIMA201812287002.md): Computer · malfunctioned · Dec 27, 2018 · N522AE · Cndair CL6002C10 · Stall Warning System
  > STALL FAIL CAUTION MSG UPON LINE UP FOR TAKEOFF. LOW SPEED REJECTED TAKEOFF."TRANSFERRED TO NRWC 522-ORD-03408"-C/A-TRANSFERRED FROM NRWC 522-ORD-03408. REMOVED AND REPLACED STALL PROTECTION COMPUTER IAW CRJ AMM 27-35-01. OPS CHECK GOOD FOR COMPUTER, STALL F
- [SDR SIMA2018082016001](https://openairdocs.org/sdr/SIMA2018082016001.md): Control Unit · failed · Aug 16, 2018 · N522AE · Cndair CL6002C10 · Brake Anti-Skid Section
  > ON GEAR EXTENSION ''A/SKID OUTBD'' CAUTION MSG AND ''OB GND SPLR FAULT'' STATUS MSG POSTED. WENT AROUND, RAN QRH PROCEDURES. ON RETURN, AFTER GEAR EXTENSION FOR SECOND APR.BOTH CAUTION AND STATUS MSGS CLEARED.-C/A-REMOVED AND REPLACED ANTI-SKID CONTROL UNIT IA
- [SDR SIMA2018073130005](https://openairdocs.org/sdr/SIMA2018073130005.md): Light · loose · Jul 30, 2018 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHT ON ROW 16 IS NOT ILLUMINATING. RESECURED CEILING EMERGENCY LIGHT ABOVE ROW 16 IAW AMM 33-51-09. OPC GOOD IAW AMM 33-51-00. NO OTHER DEFECTS NOTED AT THIS TIME.
- [SDR SIMA2018073020007](https://openairdocs.org/sdr/SIMA2018073020007.md): Engine · failed · Jul 20, 2018 · N522AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)
  > ON AP INTO ORD NR 1 ENG SHUTDOWN. FLT DECLARED EMRG. L OIL PRESS WARNING ON EICAS, SUBSEQUENT L ENGINE FAILURE. REMOVED AND REPLACED LT ENGINE IAW WC 71-00- AND 71-002. OPS CHECK AND LEAK CHECK GOOD.
- [SDR SIMA20180409001](https://openairdocs.org/sdr/SIMA20180409001.md): Power Supply · inoperative · Apr 9, 2018 · N522AE · Cndair CL6002C10 · Emergency Lighting
  > EXTERIOR AFT EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EPSU AND BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD. NO OTHER DEFECTS NOTED.

Next page: https://openairdocs.org/aircraft/N522AE/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 = 'N522AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N522AE/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.