# Service difficulty reports: N511AE

A list on [N511AE](https://openairdocs.org/aircraft/N511AE.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 · 137 reports

- [SDR VNAA202501090016](https://openairdocs.org/sdr/VNAA202501090016.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK LOCATED ON RBL 9 BETWEEN F.S 834 - F.S 974 HAS DENTS AND DEEP GOUGES. THIS SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.
- [SDR VNAA202501090015](https://openairdocs.org/sdr/VNAA202501090015.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE SEAT TRACK LOCATED ON LBL9 BETWEEN F.S 687 - F.S 581 HAS DEEP GOUGES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.
- [SDR VNAA202501090014](https://openairdocs.org/sdr/VNAA202501090014.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK BETWEEN F.S 865 - F.S 969 HAS GOUGING AND PITTING. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.
- [SDR VNAA202501090013](https://openairdocs.org/sdr/VNAA202501090013.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SIDE SEAT TRACK BETWEEN F.S 483 - F.S 570 HAS GOUGES AND SCRATCHES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.
- [SDR VNAA202501090012](https://openairdocs.org/sdr/VNAA202501090012.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LH SIDE SEAT TRACK BETWEEN F.S 674 - F.S 712 HAS MULTIPLE GOUGES AND SCRATCHES. THE SEAT TRACK IS OUT OF LIMITS AND REQUIRES REPLACEMENT.
- [SDR VNAA202501090011](https://openairdocs.org/sdr/VNAA202501090011.md): Seat Track · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT SIDE SEAT TRACK BETWEEN F.S 712 - F.S 761 HAS MULTIPLE GOUGES.
- [SDR VNAA202501090010](https://openairdocs.org/sdr/VNAA202501090010.md): Fitting · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT FLAP FITTING (AFT) AT WS 264.00 HAS GOUGED ON LUG EAR.
- [SDR VNAA202601090009](https://openairdocs.org/sdr/VNAA202601090009.md): Skin · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN UNDER FWD DRAIN MAST IS GOUGED
- [SDR VNAA202601090008](https://openairdocs.org/sdr/VNAA202601090008.md): Skin · corroded · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FUSELAGE EXTERNAL SKIN UNDER LOWER BEACON LIGHT IS GOUGED AND CORRODED IN MULTIPLE AREA SH670-33202 SKIN UNDER LWR. BEACON
- [SDR VNAA202601090007](https://openairdocs.org/sdr/VNAA202601090007.md): Torque Tube · corroded · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR PULL-IN LEVER TORQUE TUBE PN 601R31863-1 HAS CORROSION
- [SDR VNAA202601090006](https://openairdocs.org/sdr/VNAA202601090006.md): Washer · cracked · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Wing Main, Frame Structure
  > REQUEST, SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR, HR00572741 SO# 400416899 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7
- [SDR VNAA202601090005](https://openairdocs.org/sdr/VNAA202601090005.md): Washer · cracked · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Wing Main, Frame Structure
  > SUBMIT RFTS FOR AN EA TO FABRICATE PN CC670-10635-7 FOR HR00572740, SO 400416898 AND FABRICATE AS INSTRUCTED. (THIS CARD IS FOR RFTS SUBMITTAL AND FABRICATION OF QTY 1 PN CC670-10635-7) RETENTION WASHER
- [SDR VNAA202601090004](https://openairdocs.org/sdr/VNAA202601090004.md): Skin · cracked · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Wing, Plate/Skin
  > WHILE DRILLING TO EXTRACT SCREWS ON RH OVER WING INSPECTION LIGHT DRILL BIT WALKED FROM CENTER AND DAMAGED SURROUNDING HOLE. DWG SH670-33162 FUSELAGE SKIN PANEL
- [SDR VNAA202601090003](https://openairdocs.org/sdr/VNAA202601090003.md): Skin · cracked · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR SURROUND STRUCTURE SKIN AT FS310.00 AND STGR17L IS CRACKED DUE TO PAX DOOR HINGE BEING MISALIGNED ONE LUG FWD SH670-31187-9 SKIN
- [SDR VNAA202601090002](https://openairdocs.org/sdr/VNAA202601090002.md): Angle · corroded · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR ANGLE AT FS338-963 TRACE DATUM 6 HAS MINOR SURFACE CORROSION PN 600-31902-269. (INSIDE PAX DOOR)
- [SDR VNAA202601090001](https://openairdocs.org/sdr/VNAA202601090001.md): Lug · gouged · Jan 9, 2026 · N511AE · Cndair CL6002C10 · Engine Thrust Reverser
  > FOUND R/H UPPER THRUST EVERSER CENTER HINGE BRACKET IS GOUGED LOWER EDGE OF LUG. CN624-1404-212 HINGE BEAM LUG
- [SDR VNAA2024121311101](https://openairdocs.org/sdr/VNAA2024121311101.md): Skin · damaged · Dec 10, 2024 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > #3 VHF ANTENNA MOUNTING AREA UNDER ANTENNA FUSELAGE SKIN IS DAMAGED. / C/W INTELSAT EA9596-REVB FUSELAGE / FS 629-645 / SCRATCHES UNDER VHF-3 ANTENNA, DELTA ENGINEERING 8100-9 # ST04797NY-011. IAW EA9596-REVC INSTRUCTIONS.
- [SDR VNAA2024041711102](https://openairdocs.org/sdr/VNAA2024041711102.md): Door · damaged · Apr 16, 2024 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > AFTER TAKE OFF THE FA'S COULD SEE LIGHT THROUGH THE PAX DOOR / REMOVED AND REPLACED PAX DOOR SEAL IAW CRJ700 AMM 52-11-07-000/400-804(A02)PSA. LEAK CHECK GOOD.
- [SDR VNAA2024010911101](https://openairdocs.org/sdr/VNAA2024010911101.md): Unknown · unknown · Jan 6, 2024 · N511AE · Cndair CL6002C10 · Ice/Rain Protection System Wiring
  > ANTI-DUCT WARNING AND ANTI-ICE CAUTION MSG IN FLIGHT / INTERROGATED MAC FOUND EVENT LOC HISTORY AT SS14. REMOVED CONNECTOR MT168P2 IAW CRJ700 AMM 36-21-09-000-801. FOUND OLD STYLE INSERT. R&R CERAMIC INSERT IAW CRJ700 ESPM 20-26-00. RECONNECTED MT168P2 IAW CRJ
- [SDR VNAA202308292](https://openairdocs.org/sdr/VNAA202308292.md): Plate · corroded · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Doors
  > PAX DOOR CUTOUT, ATTACHMENT PLATE CORRODED AT STGR 18L, FS295.00 AND FS364.00
- [SDR VNAA20230829001](https://openairdocs.org/sdr/VNAA20230829001.md): Skin · corroded · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DISCREPANCY: FUSELAGE SKIN IS CORRODED UNDER FOOTPRINT OF PANEL 196DR AT STR 27.
- [SDR VNAA2023082903](https://openairdocs.org/sdr/VNAA2023082903.md): Unknown · damaged · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Service Doors
  > SERVICE DOOR STABILIZATION BRACKET IS CRACKED.
- [SDR VNAA2023082904](https://openairdocs.org/sdr/VNAA2023082904.md): Skin · damaged · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Wing, Plate/Skin
  > LEADING EDGE 522AL HAS ONE DAMAGED FASTENER COUNTERSINK ON THE LOWER LEADING EDGE AT WS 178.00.
- [SDR VNAA2023082905](https://openairdocs.org/sdr/VNAA2023082905.md): Angle · corroded · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Structure (General)
  > CLIP CORRODED AT FRAME AT FS295 AND STRG21R.
- [SDR VNAA2023082907](https://openairdocs.org/sdr/VNAA2023082907.md): Stringer · corroded · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STINGER 21R CORRODED BETWEEN FS319 AND FS333.
- [SDR VNAA2023082908](https://openairdocs.org/sdr/VNAA2023082908.md): Doubler · corroded · Aug 29, 2023 · N511AE · Cndair CL6002C10 · Fuselage Structure (General)
  > DOUBLER FOR AFT POTABLE WATER LINES CORRODED BETWEEN FS 1031.00 AND FS 1047.00 STR 26R.
- [SDR VNAA202207011113](https://openairdocs.org/sdr/VNAA202207011113.md): Fuel Sys · odor · Jun 30, 2022 · N511AE · Cndair CL6002C10 · Fuel Transfer Valve
  > STRONG FUEL SMELL IN AFT CABIN AND LAV / OPENED PAX DOOR, SERVICE DOOR & REMOVED OVER-WING DOORS, CABIN FLOOR PANELS 272 GRF & 271 ALF, & AFT CARGO BAY FLOOR PANELS 281 HLF & 281 BLF TO ALLOW FOR AIR VENTILATION & TO SEARCH FOR SOURCE OF ODOR. REMOVED & DEFER
- [SDR VNAA202207011112](https://openairdocs.org/sdr/VNAA202207011112.md): B-Nut · loose · Jun 29, 2022 · N511AE · Cndair CL6002C10 · Fuel Transfer Valve
  > STRONG FUEL SMELL IN PAX CABIN. PERFORMED DVI OF BELLY OF AIRCRAFT IN AFT CARGO BAY AND FOUND B-NUT ON APU FUEL-FEED DRAIN LINE T-FITTING TO BE LOOSE. INSULATION IN THE SURROUNDING AREA AT FS1000 WAS SOAKED IN FUEL. TIGHTENED B-NUT I.A.W. CRJ700 AMM 28-24-23-4
- [SDR VNAA202207011111](https://openairdocs.org/sdr/VNAA202207011111.md): Cabin Air Sys · odor · Jun 29, 2022 · N511AE · Cndair CL6002C10 · Aircraft Fuel System
  > STRONG FUEL SMELL IN PAX CABIN. MAINTENANCE VENTED A/C FOR SEVERAL HOURS AS REQUIRED. "
- [SDR VNAA202110271111](https://openairdocs.org/sdr/VNAA202110271111.md): Instrument Panel · abnormal · Oct 23, 2021 · N511AE · Cndair CL6002C10 · Instrument Panel
  > FO LOST ALL INSTRUMENTATION RAN QRH. ADC2 SWITCHED WORKED LOST AGAIN. PITCH FEEL STATUS, FADEC FAULT STATUS, YAW DAMPER 2 FAULT STATUS MESSAGES / PERFORMED OPS TEST OF ADC IAW CRJ700 AMM 34-13-01-740-801( A01) OPS TEST GOOD. PERFORMED OPS TEST OF AHRS IAW CRJ7
- [SDR VNAA202109021112](https://openairdocs.org/sdr/VNAA202109021112.md): Warning Message · false activation · Aug 31, 2021 · N511AE · Cndair CL6002C10 · Central Warning
  > COMING INTO CLT AROUND FL120, THE CREW EXPERIENCED ICING CONDITIONS AND TURNED ON THE A/I SYSTEM. SHORTLY AFTER, THEY RECEIVED A A/I DUCT WARNING MESSAGE THAT THEN WENT TO AMBER. THE QRH SAID TO TURN OFF THE ANTI-ICE SYSTEM AND LEAVE ICING CONDITIONS. THE CREW
- [SDR VNAA2021051311101](https://openairdocs.org/sdr/VNAA2021051311101.md): Proximity Switch · failed · May 9, 2021 · N511AE · Cndair CL6002C10 · Door Warning System
  > AIRCRAFT HAS A DOOR INDICATOR MEL. CREW WAS TOLD TO EXPECT DOOR CAUTION MESSAGE. NEAR CRUISE, RECEIVED A DOOR WARNING MSG. NO PRESSURIZATION ISSUES THOUGH. CREW RAN THE QRH, AND DETERMINED TO RETURN TO SYR. CREW DID DECLARE AN EMERGENCY. ONCE FLIGHT DESCENDED
- [SDR VNAA2020081611101](https://openairdocs.org/sdr/VNAA2020081611101.md): Controller · failed · Aug 16, 2020 · N511AE · Cndair CL6002C10 · Navigation System
  > CREW THE BROUGHT AIRCRAFT INTO FNT LAST NIGHT HAD NO ISSUES. UPON ARRIVING FOR OUTBOUND FLIGHT, FOUND A WRITE-UP FOR A BURNING ELECTRICAL SMELL IN AFT OF AIRCRAFT. CREW ALSO FOUND MULTIPLE BREAKERS POPPED. UPON START-UP CREW ALSO FOUND MULTIPLE LRU INOP, ACSC
- [SDR VNAA202008161111](https://openairdocs.org/sdr/VNAA202008161111.md): Computer · failed · Aug 16, 2020 · N511AE · Cndair CL6002C10 · Navigation System
  > CREW THE BROUGHT AIRCRAFT INTO FNT LAST NIGHT HAD NO ISSUES. UPON ARRIVING FOR OUTBOUND FLIGHT, FOUND A WRITE-UP FOR A BURNING ELECTRICAL SMELL IN AFT OF AIRCRAFT. CREW ALSO FOUND MULTIPLE BREAKERS POPPED. UPON START-UP CREW ALSO FOUND MULTIPLE LRU INOP, ACSC
- [SDR VNAA2020071711101](https://openairdocs.org/sdr/VNAA2020071711101.md): Power Supply · failed · Jul 17, 2020 · N511AE · Cndair CL6002C10 · Emergency Lighting
  > SEVERAL EMERGENCY LIGHTS INOP. R&R #2 EMERGENCY LIGHT BATTERY. OPS CHECK GOOD.
- [SDR VNAA202005119991](https://openairdocs.org/sdr/VNAA202005119991.md): Hinge · worn · May 11, 2020 · N511AE · Bombdr CL6002D15 · Passenger/Crew Doors
  > PAX DOOR HINGE HAS EXCESSIVE PLAY ON FWD SIDE. PERFORMED DETAILED INSPECTION OF THE PASSENGER DOOR PIANO HINGE LUGS FUSELAGE SIDE AND PASSENGER DOOR SIDE AND FOUND FUSELAGE SIDE LUGS AND PASSENGER DOOR SIDE LUGS OUT OF LIMITS. PASSENGER DOOR FUSELAGE SIDE HING
- [SDR VNAA2020012301102](https://openairdocs.org/sdr/VNAA2020012301102.md): Battery Pack · inoperative · Jan 20, 2020 · N511AE · Cndair CL6002C10 · Emergency Lighting
  > MULTIPLE PORTIONS OF EMERGENCY LIGHT SYSTEM INOP. REMOVED AND REPLACED POWER SUPPLY BATTERY IAW CRJ 700 AMM. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. (P/N: 2013-1A S/N: 122248)
- [SDR VNAA2020011499907](https://openairdocs.org/sdr/VNAA2020011499907.md): Stiffener · cracked · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR POWER ASSIST MOTOR STIFFENER FOUND TO BE CRACKED. REMOVED PAX DOOR POWER ASSIST MOTOR FOR ACCESS IAW AMM 52-11-08-000-801-A02. REINSTALLED PAX DOOR POWER ASSIST MOTOR IAW AMM 52-11-08-400-801-A02. REMOVED PAX DOOR POWER ASSIST MOTOR CABLE GUARD FOR AC
- [SDR VNAA2020011419906](https://openairdocs.org/sdr/VNAA2020011419906.md): Stiffener · cracked · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR POWER ASSIST MOTOR STIFFENER FOUND TO BE CRACKED. REMOVED UNSERVICEABLE PAX DOOR AFT WEB STIFFENER IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW SERVICEABLE PAX DOOR AFT WEB STIFFENER IAW SRM 51-40-11-001-001-A01. INSTALLED NEW SERVICEABLE
- [SDR VNAA2020011409906](https://openairdocs.org/sdr/VNAA2020011409906.md): Drag Angle · cracked · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PASSENGER DOOR AFT DRAG ANGLE WITHIN 1000 FLIGHT HOURS AFTER SECTION I, ACCOMPLISH A PERMANENT REPAIR AT DISCREPANT AREA IN ACCORDANCE WITH APPROVED PROCEDURES. REMOVED PREVIOUS AFT DRAG ANGLE REPAIR IAW SRM 51-42-13-001-001-A01. INSTALLED NEW REPAIR TO PAX
- [SDR VNAA2020011499905](https://openairdocs.org/sdr/VNAA2020011499905.md): Floorbeam · corroded · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOORBEAM AT LBL 9 HAS MULTIPLE AREAS OF CORROSION ON TOP OF THE BEAM BETWEEN FS 1007 AND FS 1064. IAW SRM 53-61-43-101-001-A01 NO DAMAGE ALLOWED TO FLOORBEAMS IN THIS LOCATION REQUIRES ENGINEERING REPAIR. BLENDED OUT DAMAGE IAW REO 670-53-61-162
- [SDR VNAA2020011499904](https://openairdocs.org/sdr/VNAA2020011499904.md): Floorbeam · corroded · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT CARGO BAY FLOOR BEAM AT LBL 27HAS MULTIPLE AREAS OF CORROSION ON TOP OF THE BEAM BETWEEN FS 992 TO FS 1033. COMPLIED WITH REO 670-53-61-1626.
- [SDR VNAA2020011499903](https://openairdocs.org/sdr/VNAA2020011499903.md): Floorbeam · corroded · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT CARGO RBL 9 AND RBL 27 FLOORBEAMS HAVE MULTIPLE AREAS OF CORROSION ON TOP OF BEAMS BETWEEN FS 1007 TO FS1064 ON RBL 9 AND FS 1060 TO FS 1075 ON RBL 27.0. IAW SRM 53-61-43-101-001-A01 NO DAMAGE ALLOWED TO FLOOR BEAMS IN THIS LOCATION REQUIRES ENGINEERING RE
- [SDR VNAA2020011499902](https://openairdocs.org/sdr/VNAA2020011499902.md): Frame · corroded · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FUSELAGE FRAME AT FS 310 IS CORRODED ON BOTH SIDES BETWEEN STGR 26L AND STGR 26R. CUT AND REMOVED DAMAGED SECTION OF FS 310.00 FRAME IAW SRM 53-00-06-201-006-A01. COMPLETED REPAIR OF DAMAGED SECTION OF FS 310.00 FRAME IAW SRM 53-00-06-201-006-A01. REPAIR INSTA
- [SDR VNAA2020011489901](https://openairdocs.org/sdr/VNAA2020011489901.md): Frame · cracked · Jan 14, 2020 · N511AE · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME BS 333, STGR 0 WAS CRACKED. REMOVED THE FRAME SECTION BETWEEN STRINGERS 0 AND 3 IAW EA 69-2019-308 REV.P1. INSTALLED FRAME SECTION IAW EA 69-2019-380 REV.P1. LOCATED AND DRILLED REPAIR FRAME SECTION IAW EA 69-2019-380 REV.P1. PERFORMED EDDY CURRE
- [SDR VNAA201908021102](https://openairdocs.org/sdr/VNAA201908021102.md): Brake Sys · malfunctioned · Aug 1, 2019 · N511AE · Cndair CL6002C10 · Landing Gear Brake System
  > WHILE CLIMBING OUT OF DCA AIRPORT THE CREW RECEIVED A ANTI SKID FAULT STATUS MESSAGE. THE CREW RAN THE QRH. CREW ALSO RAN LANDING NUMBERS THROUGH ACARS FOR THE DESTINATION AIRPORT OF BDL. CREW DETERMINED IT WAS UNSAFE TO LAND THERE DUE TO RUNWAY LENGTH. THE CR
- [SDR VNAA2019070211101](https://openairdocs.org/sdr/VNAA2019070211101.md): Drag Angle · cracked · Jul 2, 2019 · N511AE · Cndair CL6002C10 · Passenger/Crew Doors
  > PLACED ON EA69-2019-136 DURING ROUTINE MAINTENANCE IN (CAK), MAINTENANCE NOTED THAT THE 601R31772-5 AFT DRAG ANGLE HAS A CRACK IN IT THAT MEASURES APPROXIMATELY 1.60Ï¿½, AND IS LOCATED IN THE RADIUS OF THE DRAG ANGLE.
- [SDR VNAA2019042411102](https://openairdocs.org/sdr/VNAA2019042411102.md): Battery · discharged · Apr 24, 2019 · N511AE · Cndair CL6002C10 · Emergency Lighting
  > FLOOR LEVEL EMERGENCY EXIT SIGN ADJACENT TO SEAT 16F DOES NOT ILLUMINATE SWAPPED #3 AND #4 ESPU BATTERIES OPS CHECK GOOD.
- [SDR VNAA2018051011101](https://openairdocs.org/sdr/VNAA2018051011101.md): Manifold · malfunctioned · May 10, 2018 · N511AE · Cndair CL6002C10 · Landing Gear Steering System
  > IN FLIGHT WITH THE GEAR UP THE CREW RECEIVED A STEERING INOP CAS MESSAGE. THE MESSAGE RESET ON THE GROUND AND CAME BACK ON MULTIPLE TIMES. REMOVED AND REPLACED STEERING MANIFOLD. OPS AND RIG CHECK GOOD.
- [SDR VNAA2017090311101](https://openairdocs.org/sdr/VNAA2017090311101.md): Warning Light · illuminated · Sep 3, 2017 · N511AE · Cndair CL6002C10 · Door Warning System
  > RETURNED TO FIELD IMMEDIATELY AFTER TAKEOFF FOR A SERVICE DOOR INDICATOR LIGHT. FLIGHT LANDED SAFELY WITH NO COMPLICATIONS, NO EMERGENCY WAS DECLARED.

Next page: https://openairdocs.org/aircraft/N511AE/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 = 'N511AE' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N511AE/reports

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