# Service difficulty reports: N523AE

A list on [N523AE](https://openairdocs.org/aircraft/N523AE.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 · 124 reports

- [SDR VNAA2026083123801](https://openairdocs.org/sdr/VNAA2026083123801.md): Wire Harness · faulted · Aug 27, 2026 · N523AE · Cndair CL6002C10 · Landing Gear System Wiring
  > GEAR DISAGREE WARNING MSG IN FLIGHT. REMOVED & REPLACED LT DRAG BRACE HARNESS ASSY IAW AMM 32-61-05-000/400-804-A01.
- [SDR VNAA2026082723601](https://openairdocs.org/sdr/VNAA2026082723601.md): Actuator · faulted · Aug 24, 2026 · N523AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GEAR DISAGREE/NLG UNCOMMANDED MOVEMENT/CABIN ALT INCREASED RAPIDLY. PERFORMED A HEALTH STATUS CHECK OF THE PROXIMITY SENSOR IN THE MDC IAW 32-61-00-710-801 HEALTH CHECK GOOD NO DEFECT NOTED. TROUBLESHOOT NLG IAW SDS 32-30-00-001 AND SSM 32-30-00. SUSPECTED L
- [SDR 1Q2R2026081520119](https://openairdocs.org/sdr/1Q2R2026081520119.md): Pressure Blkhd · corroded · Aug 11, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > AT BS 235 PRESSURE BULKHEAD HAS CORROSION NEAR ELECT CONNECTOR J107. PERFORMED PERMANENT REPAIR IAW RFTS-129742, REV. 0, REO 670-53-11-2338, REV--, REO 670-53-11-2339, REV -.
- [SDR 1Q2R2026081020192](https://openairdocs.org/sdr/1Q2R2026081020192.md): Skin · dented · Aug 6, 2026 · N523AE · Cndair CL6002C10 · Passenger/Crew Doors
  > DURING OK TO INSTALL OF PAX DOOR, DENT WAS FOUND ON AFT SIDE OF PAX DOOR HINGE ON FUSELAGE SIDE. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-130175 REV. 0, DATED AUGUST 06, 2026, AND REO 670-53-21-2944, REV-.
- [SDR 1Q2R2026080220138](https://openairdocs.org/sdr/1Q2R2026080220138.md): Fitting · gouged · Aug 2, 2026 · N523AE · Cndair CL6002C10 · Horizontal Stabilizer Miscellaneous Structure
  > HORIZONTAL STAB FITTING HAS GOUGE DAMAGE ON UPPER OUTBOARD LEFT-HAND FITTING AND UPPER INBOARD LEFT-HAND FITTING.
- [SDR 1Q2R2026072950069](https://openairdocs.org/sdr/1Q2R2026072950069.md): Rib · cracked · Jul 28, 2026 · N523AE · Cndair CL6002C10 · Wing, Rib/Bulkhead
  > DURING NDT INSPECTION, CRACK INDICATION NOTED ON THE L/H SIDE AT WS178.00, FLAP HINGE BOX ATTACHMENT FITTING ON THE I/B FWD HOLE ON THE INTERNAL RIB SIDE. PERFORMED PERMANENT REPAIR IN ACCORDANCE WITH RFTS-129840 REV. 0, DATED JULY 28, 2026, AND MHI RJ REO 670
- [SDR 1Q2R2026081620178](https://openairdocs.org/sdr/1Q2R2026081620178.md): Skin · chafed · Jul 22, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN AT 2 INCHES FWD OF BS 985, STR 27L HAS CHAFE DAMAGE. PERFORMED PERMANENT REPAIR IAW RFTS-129909, REV 0, AND REO 670-53-51-401, REV-.
- [SDR 1Q2R2026080950071](https://openairdocs.org/sdr/1Q2R2026080950071.md): Skin · dented · Jul 21, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DENT DAMAGE TO FUSELAGE SKIN BETWEEN BS 319.70 - 333, S20R-S21R. PERFORMED PERMANENT REPAIR IAW RFTS-129715 REV. 0, AND REO 670-53-21-2933 REV. --,
- [SDR 1Q2R2026072920097](https://openairdocs.org/sdr/1Q2R2026072920097.md): Stringer · corroded · Jul 14, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > AT BS 295, STGR 19 LT FOUND TO BE POSSIBLE CORROSION ON BRACKET. PERFORMED PERMANENT REPAIR IAW RFTS-129854 REV. 0, AND REO 670-53-21-2936, REV--.
- [SDR 1Q2R2026071920133](https://openairdocs.org/sdr/1Q2R2026071920133.md): Hinge Fitting · gouged · Jul 8, 2026 · N523AE · Cndair CL6002C10 · Rudder Structure
  > AFT SIDE OF RUDDER, CENTER SECTION, CENTER HINGE IS GOUGED.
- [SDR 1Q2R2026071920132](https://openairdocs.org/sdr/1Q2R2026071920132.md): Hinge Fitting · gouged · Jul 8, 2026 · N523AE · Cndair CL6002C10 · Rudder Structure
  > AFT SIDE OF RUDDER, CENTER SECTION, UPPER HINGE IS GOUGED.
- [SDR 1Q2R2026072090002](https://openairdocs.org/sdr/1Q2R2026072090002.md): Skin · dented · Jun 26, 2026 · N523AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DAMAGE AT FS501, STGR17 R/H FUSELAGE. DENT/GOUGE.
- [SDR 1Q2R2026071620115](https://openairdocs.org/sdr/1Q2R2026071620115.md): Fitting · damaged · Jun 16, 2026 · N523AE · Cndair CL6002C10 · Elevator Structure
  > LEFT INBD PCU FITTING ELEVATOR SIDE LUG HAS DAMAGE ON LOWER CORNER.
- [SDR 1Q2R2026072950088](https://openairdocs.org/sdr/1Q2R2026072950088.md): Fitting · gouged · Jun 15, 2026 · N523AE · Cndair CL6002C10 · Elevator, Spar/Rib
  > LEFT ELEVATOR PCU 2 FITTING GOUGE DAMAGE. PERFORMED PERMANENT REPAIR IAW REO 670-55-21-113 REV--, AND EA 57-2025-1480, REV C.
- [SDR 1Q2R2026080550084](https://openairdocs.org/sdr/1Q2R2026080550084.md): Lock Tab · broken · Jan 12, 2026 · N523AE · Cndair CL6002C10 · Aileron Control System
  > LEFT AILERON PCU TENSION REGULATOR TO PCU LINK ASSY HAS BOTH LOCK TABS BROKEN OFF. PERFORMED PERMANENT REPAIR WITH REPLACEMENT OF TENSION REGULATOR TO PCU LINK ASSY IAW RFTS-126593, REV. 0, AND EA 2711-2026-0040, REV-.
- [SDR 1Q2R2026071650087](https://openairdocs.org/sdr/1Q2R2026071650087.md): Cap · damaged · Jan 11, 2026 · N523AE · Cndair CL6002C10 · Vertical Stabilizer
  > DURING LIGHTNING STRIKE INSPECTION FOUND MULTIPLE EXITS AT FS893.00 AND FS953.00, ALSO FOUND DAMAGE EXIT ON TOP OF SKULL CAP AND THE END CAP HAS 3 EXIT POINTS.
- [SDR VNAA202505090012](https://openairdocs.org/sdr/VNAA202505090012.md): Attach Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > RH LONGERON ATTACHMENT ANGLE (OVERWING FAIRING SUPPORT) IS CORRODED BETWEEN FS 693 AND FS 797. CORRECTIVE ACTION: REPAIRED CORRODED AREAS IAW MHIRJ REO 690-53-82-230 REV -- DATED 2025-04-14.
- [SDR VNAA202505090011](https://openairdocs.org/sdr/VNAA202505090011.md): Rivet · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > R/H F.S. 280 BEAN HAS TWO CORRODED RIVETS BETWEEN RBL 9 TO RBL 18. CORRECTIVE ACTION: REMOVED 2 EACH CORRODED FASTENERS IAW CRJ900 SRM 51-42-13-001-001-A01. INSTALLED 2 NEW FASTENERS. APPLIED TO FASTENERS. IAW CRJ900 SRM 51-42-13-001-001-A01, 51-25-16-001-001-
- [SDR VNAA202505090010](https://openairdocs.org/sdr/VNAA202505090010.md): Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Structure
  > UPON REMOVAL OF J-ANGLE FOUND L/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: REPLACED LH FS280 LWR WEB PN: 670-53-11-052-1 IAW BOMBARDIER REO 670-53-11-052 REV.-A DATED NOV-18-2004 REPAIR #2.
- [SDR VNAA202505090009](https://openairdocs.org/sdr/VNAA202505090009.md): Floorbeam · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > GALLEY 1 FWD INBRD SIDE FLOOR FITTING AT THE 280 IS CORRODED AND REQUIRES REPLACEMENT. CORRECTIVE ACTION: REMOVED THREE CORRODED FLOOR FITTING AND DOUBLER PLATES AND INSTALLED THREE NEW FLOOR FITTINGS AND DOUBLER PLATES ON GALLEY 1 IAW CRJ 700 SRM TASK 51-41-0
- [SDR VNAA202505090008](https://openairdocs.org/sdr/VNAA202505090008.md): Hinge · chafed · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (FUSELAGE SIDE) HAS CHAFING DAMAGE THE ENTIRE LENGTH BETWEEN THE LUGS. THE HINGE ALSO HAS A GOUGE BESIDE THE AFT LUG, APPROXIMATELY 0.5" LONG AND.025" DEEP. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR HINGE AT FUSELAGE SIDE P/N SH670-31876
- [SDR VNAA202505090007](https://openairdocs.org/sdr/VNAA202505090007.md): Angle · damaged · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 280 CROSSBEAM AND AFT J-ANGLE ARE CORRODED ALONG THE UPPER EDGE. CORRECTIVE ACTION: CORROSION FOUND ON MULTIPLE CROSS SECTIONS. REPLACE J-ANGLE WITH NEW. LOCATED AND DRILLED NEW "J" ANGLE CC670-34095-1 IAW CRJ 700 SRM 51-42-21-001-001-A01. INSTALLED NEW J-A
- [SDR VNAA202505090006](https://openairdocs.org/sdr/VNAA202505090006.md): Floorbeam · damaged · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > WHILE REMOVED 280 FLOOR BEAM FOUND 5 EACH FASTENERS TO BE OVERSIZED ON LH FLOOR SILL GOING THROUGH BEAM CORRECTIVE ACTION: COMPLIED WITH ALL STEPS REO 670-53--21-2609 REV-- DATED 2025-04-16
- [SDR VNAA202505090005](https://openairdocs.org/sdr/VNAA202505090005.md): Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER MID ANGLE HAS MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED PAX DOOR LOWER MID ANGLE PN: SH670-31875-3 IAW CRJ700 SRM TASKS 51-42-06-001-001-A01 AND 51-40-11-001-001-A01.
- [SDR VNAA202505090004](https://openairdocs.org/sdr/VNAA202505090004.md): Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR UPPER MID ANGLE HAVE MULTIPLE SPOTS OF CORROSION. CORRECTIVE ACTION: REMOVED AND REPLACED IAW CRJ 700 SRMS 51-40-11-001-001-A01 AND 51-42-21-001-001-A01.
- [SDR VNAA202505090003](https://openairdocs.org/sdr/VNAA202505090003.md): Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6.040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ
- [SDR VNAA202505090002](https://openairdocs.org/sdr/VNAA202505090002.md): Angle · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: FABRICATED, LOCATED AND DRILLED NEW RH LOWER WEB AND BUTTSTRAP FROM MATERIAL 7075-T6.040" IAW CRJ 700 SRM 51-40-11-001-001-A01, 51-24-36-001-001-A01. MATERIAL ID REF. CRJ
- [SDR VNAA202505090001](https://openairdocs.org/sdr/VNAA202505090001.md): Web · corroded · May 9, 2025 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > UPON REMOVAL OF J-ANGLE FOUND R/H STA 280 CROSSBEAM AND WEB CORRODED CORRECTIVE ACTION: LOCATED AND DRILLED NEW R/H CROSSBEAM PN# CC670-34094-2 IAW CRJ 700 SRM 51-40-11-001-001-A01. R/H LOWER WEB, R/H BUTTSTRAP & R/H CROSSBEAM INSTALLED PER SERVICE BULLETIN 67
- [SDR VNAA2025021911101](https://openairdocs.org/sdr/VNAA2025021911101.md): Window · arced · Feb 18, 2025 · N523AE · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN SIDE WINDOW ELECTRICAL ARCHING. / REMOVED AND REPLACED THE CAPTAIN SIDE FLIGHT COMPARTMENT SIDE WINDOW IAW AMM 56-12-01-000/400-801-A01-PSA. PERFORMED OPS TEST OF WINDSHIELD/SIDE WINDOW TEMP CONTROLLER IAW AMM 30-41-06-710-801. OPS TEST GOOD. PRESSURIZ
- [SDR VNAA2025020411101](https://openairdocs.org/sdr/VNAA2025020411101.md): Lamp · inoperative · Feb 1, 2025 · N523AE · Cndair CL6002C10 · Passenger Compartment Lighting
  > BURNING SMELL COMING FROM FWD CABIN ROW 1 CEILING LIGHT AREA. THERE WAS NO MEDICAL ATTENTION REPORTED FOR THIS EVENT. / FOUND LAMP CARRIER FOR CEILING LIGHTS ABOVE ROW 1 TO BE FAULTED INTERNALLY CAUSING BURNING SMELL. REMOVED AND REPLACED BOTH LAMP CARRIERS IA
- [SDR VNAA2024092311101](https://openairdocs.org/sdr/VNAA2024092311101.md): Bpsu · faulted · Sep 19, 2024 · N523AE · Cndair CL6002C10 · Trailing Edge Flap Control System
  > FLAPS FAIL CAUTION AFTER T/O. / UPON TROUBLESHOOTING FOUND LH FLAP BPSU DISCONNECTED. MANUALLY RIGGED LH BPSU IAW CRJ 700 AMM 27-52-03-801-A01. PRIOR TO CONNECTING OTBD FLAP TORQUE TUBE VERIFIED LH FLAP BPSU IS WITHIN RIG LIMITS. INSTALLED OTBD FLAP TORQUE TUB
- [SDR VNAA2024090411102](https://openairdocs.org/sdr/VNAA2024090411102.md): Display · failed · Aug 31, 2024 · N523AE · Cndair CL6002C10 · Central Display
  > MFD 2 FAIL IN FLIGHT DU #5 / RESET MFD 2 IAW CRJ 700 AMM 31-61-01-400-801. NO DEFECTS NOTED.
- [SDR VNAA2024090411101](https://openairdocs.org/sdr/VNAA2024090411101.md): Display · failed · Aug 31, 2024 · N523AE · Cndair CL6002C10 · Central Display
  > MFD 1 FAIL IN FLIGHT DU #5 / RESET MFD 1 IAW CRJ 700 AMM 31-61-01-400-801. NO DEFECTS NOTED.
- [SDR VNAA202111051111](https://openairdocs.org/sdr/VNAA202111051111.md): Engine · odor · Nov 3, 2021 · N523AE · Cndair CL6002C10 · Air Distribution System
  > FLIGHT 5359 WAS ALREADY DELAYED SEVERAL HOURS DUE TO SMOKE FILLING THE CABIN DURING AIR START. IT WAS DETERMINED THAT THE SMOKE WAS COMING FROM THE AIR START. FLIGHT FINALLY LEFT JAN AT 1731Z. DURING CLIMB, CREW BEGAN TO SMELL SMOKE. NONE WAS VISIBLE. CA BELIE
- [SDR VNAA202108191112](https://openairdocs.org/sdr/VNAA202108191112.md): Seal · out of position · Aug 15, 2021 · N523AE · Cndair CL6002C10 · Passenger/Crew Doors
  > CABIN DOOR SEAL POPPED, DECLARED AN EMERGENCY AND DESCENDED TO FL120, THEN CANCELED EMERGENCY. MAIN PAX DOOR SEAL BROKEN IN FLIGHT / RE-SECURED PASSENGER DOOR SEAL IAW CRJ700 AMM 52-11-07-400-801-A02. LEAK CHECK GOOD AT THIS TIME. VISUALLY CHECK PASSENGER DOO
- [SDR VNAA2020032011102](https://openairdocs.org/sdr/VNAA2020032011102.md): Power Supply · discharged · Mar 20, 2020 · N523AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHTS GO OUT AFTER A FEW SECONDS OF BEING TURNED ON. REMOVED AND REPLACED ALL FOUR EMERGENCY POWER SUPPLY UNITS. OPS CHECK GOOD. #1 P/N 2013-1A S/N 99189, #2 P/N 2013-1A S/N 125186, #3 P/N 2013-1A S/N 122970, #4 P/N AD2013-1A S/N 97199.
- [SDR VNAA20191012105](https://openairdocs.org/sdr/VNAA20191012105.md): Warning Message · false activation · Oct 11, 2019 · N523AE · Cndair CL6002C10 · Door Warning System
  > RIGHT EMER DOOR CAUTION MSG DURING TAXI OUT. DEFERRED INDICATION. ON OCT 13 MAINTENANCE PERFORMED HEALTH CHECK OF RH EMERGENCY DOOR PROX SENSOR, OPS CHECK GOOD ON SENSOR AND ALSO DOOR INDICATION SYSTEM. CLEARED MEL
- [SDR SIMA20190122002](https://openairdocs.org/sdr/SIMA20190122002.md): Angle · corroded · Jan 22, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR FUSELAGE CUT OUT HAS CORROSION ON THE SILL ANGLE BETWEEN FS 319.70 AND FS 349.00 AT FLOOR LEVEL. REMOVED AND REPLACED SERVICE DOOR SILL ANGLE BETWEEN FS 319.70-349.00 IAW SRM 51-42-06.
- [SDR SIMA2019021019008](https://openairdocs.org/sdr/SIMA2019021019008.md): Structure · corroded · Jan 19, 2019 · N523AE · Cndair CL6002C10 · Fuselage Main, Structure
  > BACK UP SILL BETWEEN FRAMES FS310.00 AND FS333.00 AT STRINGER 21L IS CORRODED-C/A-C/W INSTALLATION OF NEW BACK UP SILL IAW SRM 51-42-06.
- [SDR SIMA20190119007](https://openairdocs.org/sdr/SIMA20190119007.md): Cleat · corroded · Jan 19, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FRAME FS319.70 HAS A CORRODED SHEAR CLEAT AT 21L. EVALUATED FRAME FS319.70 AT STRINGER 21L, FOUND ONLY LIGHT SURFACE CORROSION. REPAIRED IAW SRM 51-21-06.
- [SDR SIMA20190111008](https://openairdocs.org/sdr/SIMA20190111008.md): Floor Support · corroded · Jan 11, 2019 · N523AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT OUTBD LONGITUDINAL FLOORBEAM IS CORRODED BETWEEN FS1000.00 AND FS1031.00. C/A-COMPLETE:REPAIRED IAW ERS-CR-5300-3632.
- [SDR SIMA2018091110001](https://openairdocs.org/sdr/SIMA2018091110001.md): Sign · unsecure · Sep 10, 2018 · N523AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY EXIT SIGN OVER SERVICE DOOR FALLING DOWN. REMOVED AND REPLACED EXIT SIGN ASSY OVER SERVICE DOOR IAW AMM 33-51-05.
- [SDR SIMA201809076001](https://openairdocs.org/sdr/SIMA201809076001.md): Connector · dirty · Sep 6, 2018 · N523AE · Cndair CL6002C10 · Brake
  > BRAKE OVHT WARNING ENROUTE AT FL360. RAN CHECKLIST RESET SYSTEM WITH BTMS BUTTON NR 4 BRAKE INDICATED 14. CLEANED AND APPLIED STABILANT TO J616/P616 PIN 3 AND 4 IAW EEC SPM. OPERATIONAL CHECKS GOOD IAW AMM 32-46-00. NO FURTHER FRETTING OR DEFECTS NOTED.
- [SDR SIMA2018083029002](https://openairdocs.org/sdr/SIMA2018083029002.md): Lamp · inoperative · Aug 29, 2018 · N523AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT OUT AFT CABIN 2ND LIGHT FROM END OF AFT CABIN-C/A-DEFERRED EMERGENCY LIGHT IAW MEL 33-34. REMOVED AND REPLACED CEILING EMERGENCY-FLOOD-LIGHT LAMP IAW CRJ-700 AMM 33-51-09 OPS CHECK GOOD MEL ITEM RESTORED
- [SDR SIMA201808065002](https://openairdocs.org/sdr/SIMA201808065002.md): Thermocouple · failed · Aug 5, 2018 · N523AE · Cndair CL6002C10 · Landing Gear Brake System
  > BRAKE OVERHEAT INDICATION ON THE RIGHT OUTBOARD DURING CRUISE AT FL 300. RAN THE PROCEDURE, DECLARED EMERGENCY. LANDED IWTHOUT INCIDENT. INDICATIONS NORMAL AFTER PROCEDURE. REMOVED AND REPLACED THE THERMOCOUPLE SENSOR IAW AMM 32-46-01 OPS CHECKED GOOD.
- [SDR SIMA2018043028001](https://openairdocs.org/sdr/SIMA2018043028001.md): Warning Message · illuminated · Apr 28, 2018 · N523AE · Cndair CL6002C10 · Drag Control System
  > DURING DECENT, DEPLOYED FLIGHT SPOILERS SLOWLY GOING THRU FL260 AFTER 10 SECONDS OF DEPLOYMENT, CAUTION MESSAGE FOR OTBD SPOILERONS & OTBD FLT SPOILERS DISPLAYED. INTERROGATED MDC, FOUND CORRELATED MESSAGE, LT OTBD MFS PCU BINDING. PERFORMED SPOST 1 RESET
- [SDR SIMA20171008002](https://openairdocs.org/sdr/SIMA20171008002.md): Rotor · sheared · Oct 8, 2017 · N523AE · Cndair CL6002C10 · Turbine Section
  > WHILE ACCOMPLISHING W/C 72-009 PG 5, BORESCOPE PROCEDURES, FOUND ONE STAGE 1 HP TURBINE ROTOR BLADE SHEARED. REMOVED AND REPLACED THE LT ENGINE IAW WORK CARDS 71-001 AND 71-002. OPS CHECKED GOOD. NO LEAKS NOTED.
- [SDR SIMA20170714003](https://openairdocs.org/sdr/SIMA20170714003.md): Lamp · inoperative · Jul 14, 2017 · N523AE · Cndair CL6002C10 · Emergency Lighting
  > AFT OVERHEAD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-09.
- [SDR SIMA20170623001](https://openairdocs.org/sdr/SIMA20170623001.md): Spoiler Sys · malfunctioned · Jun 23, 2017 · N523AE · Cndair CL6002C10 · Drag Control System
  > WHEN USING THE FLIGHT SPOILER LEVER IN FLIGHT AT 27,000 FEET, A CAUTION MESSAGE FOR THE INBD FLT SPOILERS AND INBD SPOILERONS APPEARED. INTERROGATED MDC, FOUND THE RT INBD MFS PCU BINDING MDC MESSAGE. PERFORMED SPOST 1 RESET. PERFORMED OPS CHECK IAW ETN-CR
- [SDR SIMA20170614001](https://openairdocs.org/sdr/SIMA20170614001.md): Sensor · failed · Jun 14, 2017 · N523AE · Cndair CL6002C10 · Landing Gear Brake System
  > BTMS OVERHEAT WARNING DURING CLIMB OUT, RIGHT OTBD BRAKE. REMOVED AND REPLACED THE RT OTBD BRAKE TEMP SENSOR IAW AMM 32-46-01, OPS CHECKED GOOD. PERFORMED DVI OF BRAKE SYSTEM IAW AMM 05-51-09, NO DEFECTS NOTED.

Next page: https://openairdocs.org/aircraft/N523AE/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 = 'N523AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N523AE/reports

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