# Service difficulty reports: N533AE

A list on [N533AE](https://openairdocs.org/aircraft/N533AE.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 2 · 93 reports

- [SDR VNAA2025103011101](https://openairdocs.org/sdr/VNAA2025103011101.md): Smoke Detector · false activation · Oct 29, 2025 · N533AE · Cndair CL6002C10 · Detection System
  > SMOKE AFT LAV WARNING ENROUTE, DIVERTED TO NEAREST AIRPORT. / RESET CB'S LISTED IN QRH 1-14 AND C/W OPS TEST OF AFT LAV SMOKE DETECTOR. IAW AMM 26-16-00-710-801-A01-PSA. OPS CHECK GOOD. NO EVIDENCE OF SMOKE OR FIRE IN LAV. ALSO VERFIED LAV FIRE EXTINGUISHER IN
- [SDR VNAA2024111111101](https://openairdocs.org/sdr/VNAA2024111111101.md): Display · false indication · Nov 9, 2024 · N533AE · Cndair CL6002C10 · Central Display
  > LDU / DCU SHOWING ERRONEOUS INDICATIONS IN FLIGHT SOME LIGHTS ARE INTERMITTENT AND SOME PERSIST. / INTERROGATED MDC, FOUND B1 CODE 007202. TROUBLESHOT PER FIM 31-41-07-810-801. REMOVED AND REPLACED LDU IAW CRJ 700 AMM 31-41-07-000/400-801. OPS CHECK GOOD AT TH
- [SDR VNAA2024093011101](https://openairdocs.org/sdr/VNAA2024093011101.md): Insulation · torn · Sep 27, 2024 · N533AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L BLEED DUCT CAUTION FOLLOWED BY WARNING MSG / FOUND INSULATION CUFFS TO BE BURNED THROUGH AND TORN FOR BOTH L/H HOT AIR SHUTOFF VALVE AND L/H MODULATING AND SHUTOFF VALVE. REMOVED AND REINSTALLED THE INSULATION CUFFS IAW CRJ 700 AMM 21-61-08-000/400-801 AND C
- [SDR WRXR20240820001](https://openairdocs.org/sdr/WRXR20240820001.md): Floorbeam · corroded · Aug 20, 2024 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 WL72 LBL10 AFT SIDE INTERCOSTAL UPPER OUTBOARD FLANGE CORRODED AT FWD MOST FASTENER LOCATION. FABRICATED AND INSTALLED REPAIR PARTS FOR SPLICE REPAIR AT FLOOR BEAM LBL9.0 BETWEEN FS280 TO FS295. FABRICATED FLOOR BEAM SECTION SH670-32121-13, INB LOWER SPL
- [SDR VNAA20240718001](https://openairdocs.org/sdr/VNAA20240718001.md): Floorbeam · gouged · Jul 18, 2024 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FS280 WL72 LBL40 1) ANGLE COMMON TO FS280 FLOOR BEAM AND AFT INTERCOSTAL HAS BARE METAL / TOOL MARK. 2) SAME ANGLE HAS MATERIAL GOUGED OUT AT THE LWR EDGE COMMON TO BEND RADIUS. REPAIRED BY FABRICATING AND INSTALLING REPLACEMENT CLEAT (ANGLE) P/N: SH670-31736-
- [SDR VNA2024F00008](https://openairdocs.org/sdr/VNA2024F00008.md): Frame · cracked · Jun 19, 2024 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > 6EA. MISDRILLED HOLES TO FUSELAGE STRUCTURE, FRAME SECTOR (DWG CC670-34203, 7475-T7351, 0.063" NOM THK, REF), POST FS193.00 (DWG CC670-32133, 7475-T7351 AL ALY, 0.060" NOM THK, REF) AND BOX EXTERNAL POWER PROVISIONS AFT FLANGE (DWG CC670-33401, 2024-T42 AL ALY
- [SDR VNAA20240618001](https://openairdocs.org/sdr/VNAA20240618001.md): Door Sill · corroded · Jun 18, 2024 · N533AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS280, WL72, RBL 40, OUTBOARD SILL HAS CORROSION ON UPPER AND LOWER SURFACES. CORROSION WAS REMOVED IN ACCORDANCE WITH SRM 51-21-06 USING 20:1 VISUALLY INSPECT FASTENERS ADJACENT TO DAMAGE AREAS NO SIGN OF CORROSION OR DAMAGE EDDY CURRENT INSPECTED BLEND AREAS
- [SDR VNAA20240611001](https://openairdocs.org/sdr/VNAA20240611001.md): Frame · corroded · Jun 11, 2024 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION NOTED @ FS 1069.75 BETWEEN STR 24L - 25L. REMOVED AND REPLACED (3) B0205019AD5-6 RIVETS AT FS 1069.75 STR 24L-25L IAW CRJ/700 SRM 51-42-06-001-001-A01REMOVED LIGHT SURFACE CORROSION IAW CRJ 700 SRM 51-21-06-001-001-A01, CARRIED OUT NDT, REMOVED 0.00
- [SDR VNAA2024020511101](https://openairdocs.org/sdr/VNAA2024020511101.md): Control Unit · unserviceable · Feb 4, 2024 · N533AE · Cndair CL6002C10 · Drag Control System
  > IB FLT SPLRS, IB SPOILERONS CAUTION MESSAGES IN FLIGHT. IB GND SPLR FAULT, RUD LIMIT FAULT, PITCH FEEL FAULT, STAB FAULT STATUS MESSAGES IN FLIGHT. / REMOVED & REPLACED SSCU2 IAW CRJ700 AMM 27-61-05-000/400-801-A01. PERFORMED OPS CHECK IAW CRJ700 AMM 27-61-05-
- [SDR VNAA2023110311101](https://openairdocs.org/sdr/VNAA2023110311101.md): Window · delaminated · Nov 1, 2023 · N533AE · Cndair CL6002C10 · Flight Compartment Windows
  > RH SIDE COCKPIT WINDOW ARC AND DELAMINATED IN FLIGHT. / REMOVED AND REPLACED THE RH SIDE WINDOW IAW CRJ 900 AMM 56-12-01-400-801-A01-PSA. OPS CHECK OF WINDSHIELD/WINDOW TEMPERATURE CONTROLLER & LEAK TEST OF THE R/H WINDOW GOOD AT THIS TIME.
- [SDR VNAA202301160005](https://openairdocs.org/sdr/VNAA202301160005.md): Bulkhead · not reported · Jan 16, 2023 · N533AE · Bombdr CL6002D15 · Standard Practices/Structures
  > FUSELAGE - FORWARD FUSELAGE; FS144.- 00 TO FS280.00 - INSTALLATION OF STRUCTURAL PARTS ON THE NOSE LANDING GEAR (NLG) BOX AND ON THE FS202.75 BULKHEAD COMPLY WITH SB_670BA-53-047J COMPLIED WITH SB 670BA-53-047 FUSELAGE - FORWARD FUSELAGE; FS144.00 TO F
- [SDR VNAA202301160004](https://openairdocs.org/sdr/VNAA202301160004.md): Frame · not reported · Jan 16, 2023 · N533AE · Bombdr CL6002D15 · Standard Practices/Structures
  > FUSELAGE - FORWARD FUSELAGE FS144.00TO FS280.00 - REINFORCEMENT OF THE FRAMES AT FS220.00 AND FS235.00 COMPLY WITH SB_670BA-53-045G. COMPLIED SB670BA-53-045 FUSELAGE - FORWARD FUSELAGE FS144.00 TO FS280.00 - REINFORCEMENT OF THE FRAMES AT FS220.00 AND FS235.00
- [SDR VNAA202301160003](https://openairdocs.org/sdr/VNAA202301160003.md): Bulkhead · not reported · Jan 16, 2023 · N533AE · Bombdr CL6002D15 · Standard Practices/Structures
  > PRIMARY STRUCTURE; FS144.00 TO FS280.- 00 - REINFORCEMENT OF THE LEFT AND RIGHT SIDES OF THE FS202.75 BULKHEAD ABOVE THE FLOOR AND THE NOSE LANDING GEAR (NLG) BOX COMPLY WITH THE LATEST COPY OF SB_670BA-53-044. COMPLIED WITH SB 670BA-53-044 PRIMARY STRUCTURE;
- [SDR VNAA202301160002](https://openairdocs.org/sdr/VNAA202301160002.md): Beam · not reported · Jan 16, 2023 · N533AE · Bombdr CL6002D15 · Standard Practices/Structures
  > FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS295.00 INSPECTION AND REINFORCEMENT OF LINTEL STRINGER 3 OF THE MAIN PASSENGER DOOR COMPLY WITH SB 670BA53040C. COMPLIED WITH SB 670BA-53-040 FUSELAGE CENTER FUSELAGE, PRIMARY STRUCTURE FS280.00 TO FS2
- [SDR VNAA202301160001](https://openairdocs.org/sdr/VNAA202301160001.md): Beam · not reported · Jan 16, 2023 · N533AE · Bombdr CL6002D15 · Standard Practices/Structures
  > CENTER FUSELAGE, BS 669.40 - 855.40, REPLACEMENT OF THE BEAMS AT LBL 36 AND RBL 36; AND THE FLOOR ASSEMBLY BETWEEN FS693.00 AND FS847.00 WITH THE BEAMS INSTALLED AT BL 0; LBL 9, LBL 18, LBL 27, RBL 9, COMPLY WITH SB 670BA-53-036D. PERFORMED CENTER FUSELAGE,
- [SDR VNAA2022112200003](https://openairdocs.org/sdr/VNAA2022112200003.md): Doubler · corroded · Nov 22, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > CORROSION ON ANTENNA DOUBLER BOTTOM OF FUSELAGE BETWEEN FRAMES FS 295 AND FS 310. INSTALLED NEW SERVICABLE ANTENNA DOUBLER AT STR 27 BETWEEN F.S. 295 AND 310 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01
- [SDR VNAA2022112200002](https://openairdocs.org/sdr/VNAA2022112200002.md): Frame · corroded · Nov 22, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 310 BETWEEN STRINGERS 26L AND STRINGERS 26R. REPAIRED FRAME AT FS 310 BETWEEN STRINGERS 26L AND 26R IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR VNAA2022112200001](https://openairdocs.org/sdr/VNAA2022112200001.md): Frame · corroded · Nov 22, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME FS 295 BETWEEN STRINGERS 25L AND STRINGERS 26R. REPAIRED FRAME AT FS 295 BETWEEN STRINGERS 25L AND 26R IAW CRJ 700 SRM 53-00-06-201-006-A01.
- [SDR VNAA202206139999](https://openairdocs.org/sdr/VNAA202206139999.md): Stringer · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND STRINGER 26R SEGMENT FROM F.S.333 TO F.S.364 TO BE CORRODED FROM F.S.333 TO F.S.349.
- [SDR VNAA202206139998](https://openairdocs.org/sdr/VNAA202206139998.md): Seat Track · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED AT RBL 9 BETWEEN FS 349.00 AND FS 364.0
- [SDR VNAA202206139997](https://openairdocs.org/sdr/VNAA202206139997.md): Former · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Passenger/Crew Doors
  > FOUND PAX DOOR FWD FORMER TO BE CORRODED
- [SDR VNAA202206139996](https://openairdocs.org/sdr/VNAA202206139996.md): Intercostal · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > INTERCOSTAL AT STRG 26L IS CORRED BETWEEN FS 349.00 AND FS 364.00
- [SDR VNAA202206139995](https://openairdocs.org/sdr/VNAA202206139995.md): Frame · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 319.00 FRAME IS CORRODED BETWEEN STRG 26L AND 26R.
- [SDR VNAA202206139994](https://openairdocs.org/sdr/VNAA202206139994.md): Doubler · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Antenna/Radome Anti-Ice/De-Ice System
  > ANTENNA DOUBLER BETWEEN FS 349.00 AND FS 364.00 IS CORRODED BETWEEN STRG 25L AND 26L
- [SDR VNAA202206139993](https://openairdocs.org/sdr/VNAA202206139993.md): Intercostal · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > INTERCOSTAL AT STRG 26R IS CORRED BETWEEN FS 349.00 AND FS 364.00
- [SDR VNAA202206139992](https://openairdocs.org/sdr/VNAA202206139992.md): Intercostal · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT STRG 26L IS CORRED BETWEEN FS 349.00 AND FS 364.00
- [SDR VNAA202206139991](https://openairdocs.org/sdr/VNAA202206139991.md): Frame · corroded · Jun 13, 2022 · N533AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME IS CORRODED BETWEEN STRG 26L AND 26R
- [SDR VNAA202108191113](https://openairdocs.org/sdr/VNAA202108191113.md): Unknown · odor · Aug 17, 2021 · N533AE · Cndair CL6002C10 · Air Distribution System
  > ODOR IN COCKPIT AND CABIN ON PUSH BACK WHILE MOTORING LH ENG. INSP AFT EQUIPMENT BAY AREA NO DEFECTS NOTED. INSP CABIN AND COCKPIT AREA,RAN REC AND DISPLAY FANS NO SMELL DETECTED. OPS CHECKED BOTH PACKS WITH ENG RUNNING NO DEFECTS NOTED NO SMELLS DETECTED. IAW
- [SDR VNAA202107021112](https://openairdocs.org/sdr/VNAA202107021112.md): Unknown · odor · Jun 28, 2021 · N533AE · Cndair CL6002C10 · Air Distribution System
  > SMOKE IN CABIN JUST PRIOR TO LANDING, SMELL CAUSED FA TO LOSE CONSCIOUNESS / PERFORMED GVI AND GENERAL CLEANING OF APU INLET SCREEN IAW CRJ 700 SRM 51-26-00-001-001 TO REMOVE CICADAS FROM APU INLET SCREEN, PERFORMED OPS CHECK OF AIR CONDITIONING DISTRIBUTION S
- [SDR VNAA202107021111](https://openairdocs.org/sdr/VNAA202107021111.md): Unknown · odor · Jun 28, 2021 · N533AE · Cndair CL6002C10 · Air Distribution System
  > BURNT TOAST SOUR SMELL FROM PACKS WITH APU AS BLEED SOURCE / DEFERRED APU PER MEL 49-10-01-2 CAT C. M-FUNCTION COMPLIED WITH VISUALLY VERIFIED DOOR CLOSED AND PULLED AND COLLARD CB'S N10, N11, R9 ON CBP-1. REF DDG 49-10-01. / PERFORMED GVI AND GENERAL CLEANING
- [SDR VNAA202106081112](https://openairdocs.org/sdr/VNAA202106081112.md): Windshield · cracked · Jun 5, 2021 · N533AE · Cndair CL6002C10 · Flight Compartment Windows
  > WHILE CLIMBING THROUGH FL170 CA NOTICED A CRACK IN THE WINDSHIELD FORMING. WINDSHIELD HEAT THEN FAILED. CA ASKED FOR A DESCENT TO FL100. BEFORE REACHING FL100 THE WINDSHIELD COMPLETELY SPIDER-WEBBED. CA DECLARED AN EMERGENCY AND RETURNED TO CAK. TRUCKS DID ROL
- [SDR VNAA2020022871101](https://openairdocs.org/sdr/VNAA2020022871101.md): Unknown · power loss · Feb 27, 2020 · N533AE · Cndair CL6002C10 · Electrical Power System
  > LOST ALL POWER TO AIRCRAFT AT THE GATE WITH APU ON WHEN THRUST LEVERS PULLED TO SHUT OFF. BATTERY MASTER WILL NOT TURN ON. PERFORMED OPS CHECK OF MAIN BATTERY AND APU BATTERY IAW CRJ 700 AMM. OPS CHECK GOOD AT THIS TIME. PERFORMED THREE START/STOP SEQUENCES OF
- [SDR VNAA2020010231102](https://openairdocs.org/sdr/VNAA2020010231102.md): Anchor Fitting · broken · Dec 31, 2019 · N533AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT ANCHOR FITTING BROKE. R&RD REAR COUNTER BALANCE ANCHOR SHAFT. OP CHECK/ RIG CHECK GOOD.
- [SDR VNAA2019122541101](https://openairdocs.org/sdr/VNAA2019122541101.md): Connector · disconnected · Dec 24, 2019 · N533AE · Cndair CL6002C10 · Emergency Lighting
  > MAINTENANCE FOUND THAT THE GALLEY EMERGENCY LIGHT WOULD NOT ILLUMINATE. UPON FURTHER INSEPCTION FOUND THE ELECTRICAL CONNECTOR DISCONNECTED. ONCE RECONNECTED THE EMERGENCY LIGHT OPERATED NORMALLY.
- [SDR VNAA2019112971101](https://openairdocs.org/sdr/VNAA2019112971101.md): Connector · disconnected · Nov 27, 2019 · N533AE · Cndair CL6002C10 · Emergency Lighting
  > LH AFT EXTERIOR EMERGENCY LIGHT INOP. DEFERRED LH AFT EMERGENCY EXIT LIGHT. REMOVED AND RPELACED LH AFT EXTERIOR EMERGENCY LIGHT IAW 33-51-15-000/400-801. NO FIX. CHECK AND FOUND CONNECTOR J877/P877 NOT CONNECTED. CONNECTED AND OPS CHECK IAW 33-51-00-710-802.
- [SDR SIMA2019103122007](https://openairdocs.org/sdr/SIMA2019103122007.md): Step · cracked · Oct 22, 2019 · N533AE · Cndair CL6002C10 · Passenger/Crew Doors
  > AFT SIDE PANEL ON THE PAX DOOR HAS APPROX. 1/4" CRACK IN THE UPPER CORNER FRO THE LOWER MID STEP.-C/A-REPAIRED PAX DOOR STEP IAW ERS-CR-5200-1026
- [SDR SIMA2019103122006](https://openairdocs.org/sdr/SIMA2019103122006.md): Step · cracked · Oct 22, 2019 · N533AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER MID STEP ATTACH POINT SKIN NEAR NUTPLATE FOR THE AFT BOTTOM CORNER APPEARS TO BE CRACKED.-C/A-REPAIRED PAX DOOR STEP IAW ERS-CR-5200-1026
- [SDR SIMA201910292003](https://openairdocs.org/sdr/SIMA201910292003.md): Floorbeam · cracked · Oct 22, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED. -C/A-REPAIRED RH CENTER COCKPIT FLOOR BEAM AT BL 12.00 IAW SRM 53-11-43.
- [SDR SIMA201910292005](https://openairdocs.org/sdr/SIMA201910292005.md): Floorbeam · cracked · Oct 22, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LH CENTER COCKPIT FLOOR BEAM AT BL12.00 IS CRACKED. -C/A-COMPLETED REPAIR OF LH COCKPIT FLOOR BEAM AT BL12.00 IAW SRM 53-11-43.
- [SDR SIMA201910292004](https://openairdocs.org/sdr/SIMA201910292004.md): Attach Angle · cracked · Oct 22, 2019 · N533AE · Cndair CL6002C10 · Passenger/Crew Doors
  > POSSIBLE CRACK ON THE AFT STEP HOUSING ATACH ANGLE-C/A-REPAIRED ANGLE IAW SRM 52-11-04-201-002.
- [SDR SIMA201910281004](https://openairdocs.org/sdr/SIMA201910281004.md): Bulkhead · corroded · Oct 21, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > RH COCKPIT BULKHEAD AT FS280.00 HAS CORROSION ON THE LOWER SURFACE.-C/A-REMOVED AND REPLACED RH COCKPIT BULKHEAD LOWER WEB AT FS280.00 IAW SRM 53-11-10
- [SDR SIMA2019102519002](https://openairdocs.org/sdr/SIMA2019102519002.md): Bulkhead · corroded · Oct 19, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CAPTAINS BULKHEAD IS CORRODED ON THE AFT SIDE I/B LOWER CORNER. -C/A-COMPLETED REPAIR OF THE CAPTAINS BULKHEAD LOWER WEBBING IAW SRM 53-11-10, 53-41-06 AND 51-42-10.
- [SDR SIMA2019102917002](https://openairdocs.org/sdr/SIMA2019102917002.md): Floorbeam · corroded · Oct 17, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT CROSSBEAM AT FS280.00 IS CORRODED. -C/A-COMPLETED LH CROSSBEAM REPAIR AT 280.00 IAW SRM 53-11-41.
- [SDR SIMA2019102917003](https://openairdocs.org/sdr/SIMA2019102917003.md): Floorbeam · corroded · Oct 17, 2019 · N533AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > RIGHT CROSSBEAM AT FS280.00 IS CORRODED. -C/A-COMPLETED RH CROSSBEAM REPAIR AT 280.00 IAW SRM 53-11-41.
- [SDR SIMA2019102415002](https://openairdocs.org/sdr/SIMA2019102415002.md): Drag Angle · cracked · Oct 15, 2019 · N533AE · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > RIGHT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801
- [SDR SIMA2019102415001](https://openairdocs.org/sdr/SIMA2019102415001.md): Drag Angle · cracked · Oct 15, 2019 · N533AE · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > LEFT SIDE, VERTICAL STAB TO FUSELAGE AFT DRAG ANGLE HAS A 1 1/2" CRACK ALONG LEADING EDGE.-C/A-REPAIRED IAW SRM 55-31-00-995-801
- [SDR SIMA201911182002](https://openairdocs.org/sdr/SIMA201911182002.md): Lens · cracked · Oct 12, 2019 · N533AE · Cndair CL6002C10 · Emergency Lighting
  > RIGHT OVERWING EXTERIOR EMERGENCY LIGHT JUST AFT OF EMERGENCY EXIT CUTOUT HAS A CRACKED LENS.-C/A-COMPLETE:RAR'D RH OVERWING EXTERIOR EMERGENCY LIGHT LENS IAW AMM 20-21-00.
- [SDR SIMA201911182003](https://openairdocs.org/sdr/SIMA201911182003.md): Cover · cracked · Oct 12, 2019 · N533AE · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY LIGHT STRIP COVERS LH1, LH9, RH9, RH10, AND EMERGENCY EXIT ROWS (4 EACH) ARE CRACKED.-C/A-COMPLETE:INSTALLED NEW EMERGENCY LIGHT STRIP COVERS LH1, LH9, RH9, RH10, AND EMERGENCY EXIT ROWS 4EA. IAW CRJ AMM 33-51-01.
- [SDR SIMA201911182001](https://openairdocs.org/sdr/SIMA201911182001.md): Cover · broken · Oct 12, 2019 · N533AE · Cndair CL6002C10 · Emergency Lighting
  > SEVERAL AISLE LIGHTS COVERS AND LIGHT STRIPS BROKEN-C/A-COMPLETE:REPLACED SEVERAL AISLE (4EA) LIGHT COVERS AND STRIPS IAW CRJ AMM 33-51-01.
- [SDR SIMA201908098002](https://openairdocs.org/sdr/SIMA201908098002.md): Warning Message · false activation · Aug 8, 2019 · N533AE · Cndair CL6002C10 · Stabilizer Control System
  > STAB TRIM CAUTION MACH TRIM CAUTION IN FLIGHT, RAN QRH WOULD NOT ENGAGE. INSPECTED AIRCRAFT, NO MDC MSG NOTED. PREFORMED HORIZONTAIL STABLILIZER TRIM SYSTEM OPS TEST IAW AMM 27-40-00. NO DEFECTS NOTED, SYSTEM OPS CHECK GOOD, AIRCRAFT OK FOR SERVICE

Next page: https://openairdocs.org/aircraft/N533AE/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 = 'N533AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N533AE/reports

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