# Service difficulty reports: N503AE A list on [N503AE](https://openairdocs.org/aircraft/N503AE.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 · 141 reports - [SDR VNAA2024060511101](https://openairdocs.org/sdr/VNAA2024060511101.md): Fan · odor · Jun 2, 2024 · N503AE · Cndair CL6002C10 · Indicating/Recording System > MODERATE TO STRONG ELECTRICAL BURNING SMELL COMING FROM INSIDE THE FLIGHT DECK AND FWD CABIN WITH AND WITHOUT THE PACKS AND RECIRC FANS OPERATING / REMOVED AND INSTALLED DISPLAY SUPPLY FAN IAW CRJ-700 AMM 21-24-12-000/400-801-A01 AND OPS CHECK DONE AND FOUND G - [SDR VNAA2023110911101](https://openairdocs.org/sdr/VNAA2023110911101.md): Unknown · unknown · Nov 5, 2023 · N503AE · Cndair CL6002C10 · Flight Control System > 8,500LBS FUEL, TRIM 4.6*, FLAPS 8, V1: 123, VR: 124, V2: 133, VT: 173. UPON TAKEOFF, PLANE TENDED TO PITCH UP AT A HIGHER ATTITUDE THAN ANTICIPATED. ROLLED TRIM TO MAINTAIN PROPER CLIMB ATTITUDE WITHIN COMMAND BARS. TRIM SETTINGS 1.6/1.7 LEVELED AT 4,000 FT TO - [SDR VNAA2023110111101](https://openairdocs.org/sdr/VNAA2023110111101.md): Acm · unserviceable · Oct 30, 2023 · N503AE · Cndair CL6002C10 · Cabin Cooling System > SMOKE IN CABIN AFTER RIGHT ENGINE START / REMOVED AND REPLACED THE RH ACM IAW CRJ 700 AMM 21-51-08-000/400-801 PERFORMED OPERATIONAL TEST OPS CHECK GOOD - [SDR VNAA202309131111](https://openairdocs.org/sdr/VNAA202309131111.md): Unknown · unknown · Sep 12, 2023 · N503AE · Cndair CL6002C10 · Air Distribution System > ELECTRICAL SMELL IN FLIGHT DECK UPON LANDING / PERFORMED T/S OF SMOKE AND ABNORMAL SMELL IN COCKPIT, PERFORMED OPS TEST OF THE AIR COND. DISTRIBUTION SYS, OPS CHECK GOOD NO ABNORMAL SMELL COMING FROM THE PACKS, PERFORMED OPS CHECK OF WINDSHIELD/SIDE WINDOW TEM - [SDR VNAA202207169991](https://openairdocs.org/sdr/VNAA202207169991.md): Strap · corroded · Jul 16, 2022 · N503AE · Cndair CL6002C10 · Main Landing Gear > LH MLG TRUNNION AFT STEEL STRAP FOUND TO BE CORRODED ON AFT EDGE BETWEEN LBL 22.5 AND LBL 45. - [SDR VNAA202206271111](https://openairdocs.org/sdr/VNAA202206271111.md): Hub Cap · missing · Jun 24, 2022 · N503AE · Cndair CL6002C10 · Brake Anti-Skid Section > A/SKID OUTBD AMBER CAUTION MESSAGE / TROUBLESHOT IAW CRJ700 FIM 32-44-00-810-803. FOUND IN ADVANCED DIAGNOSTICS THAT LOB WHEEL SPEED TRANSDUCER WAS NOT ROTATING. INSPECTED LOB WHEEL SPD TRANS. TO FIND WHEEL HUB CAP MISSING. REPLACED HUB CAP IAW CRJ700 AMM 32- - [SDR VNAA202203141113](https://openairdocs.org/sdr/VNAA202203141113.md): Lever · unserviceable · Mar 11, 2022 · N503AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System > GEAR DISAGREE WARNING MESSAGE ON CLIMB OUT. ALL GEAR WERE DOWN WITH GEAR SELECTED UP. TROUBLESHOT GEAR DISAGREE IAW CRJ700 FIM 32-31-00-810-803-A01. PERFORMED OPS TEST OF LANDING GEAR EXTENSION/RETRACTION SYSTEM IAW CRJ700 AMM 32-30-00-710-801-A01. CYCLED GE - [SDR VNAA202111151113](https://openairdocs.org/sdr/VNAA202111151113.md): Dcu · faulted · Nov 13, 2021 · N503AE · Cndair CL6002C10 · Central Computers > SHORTLY AFTER DEPARTING OUT OF VPS, CREW REPORTED TO GET "EVERY CAUTION MESSAGE YOU COULD THINK OF", AND DECIDED TO DIVERT TO MGM. DUE TO THE PLANE FLYING NORMALLY AND ENGINE INSTRUMENTS INDICATING NORMAL, THEY DID NOT DECLARE EMERGENCY, AND DID NOT LAND OVERW - [SDR VNAA202111151111](https://openairdocs.org/sdr/VNAA202111151111.md): Warning Message · multiple fail · Nov 12, 2021 · N503AE · Cndair CL6002C10 · Central Warning > CREW RECEIVED A LAUNDRY LIST OF CAUTION MESSAGES INBOUND TO VPS (IB/OB SPOILERONS, OIL PRESSUE, LH IB BRAKE PRESSURE, LH /AI DUCT, HYD TEMP CAUTION). EMERGENCY WAS DECLARED AND TRUCKS ROLLED ON LANDING. A/C WAS ABLE TO TAXI TO THE GATE UNDER THEIR OWN POWER AN - [SDR VNAA2021022099916](https://openairdocs.org/sdr/VNAA2021022099916.md): Bracket · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Attach Fittings > CRACK ON BRACKET IN NOSE HYDRAULIC BAY LT SIDE. REMOVED AND REPLACED BRACKET. - [SDR VNAA2021022099915](https://openairdocs.org/sdr/VNAA2021022099915.md): Hinge · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Door Hinge > GALLEY SERVICE DOOR UPPER AFT HINGE CRACKED. INSTALLED BRACKET. - [SDR VNAA2021022099914](https://openairdocs.org/sdr/VNAA2021022099914.md): Bracket · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Attach Fittings > SLAT TRACK 1-3 CANISTER BRACKET CRACKED. REPAIRED PER REO 670-57-42-577. - [SDR VNAA2021022099913](https://openairdocs.org/sdr/VNAA2021022099913.md): Structure · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Nacelle/Pylon, Main Frame > RIGHT ENG CORE COWL HAS 3" CRACK AT THE 8 O'CLOCK POSITION, REPAIRED. - [SDR VNAA2021022099912](https://openairdocs.org/sdr/VNAA2021022099912.md): Rib · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/Bulkhead > RIGHT I/B FIXED LE RIB CRACKED. REMOVED AND REPLACED. - [SDR VNAA2021022099911](https://openairdocs.org/sdr/VNAA2021022099911.md): Rib · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/Bulkhead > RIGHT I/B FIXED LE PARTIAL RIB CRACKED. REMOVED AND REPLACED. - [SDR VNAA2021022099910](https://openairdocs.org/sdr/VNAA2021022099910.md): Intercostal · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > NOSE GEAR BAY HYDRAULIC INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL. - [SDR VNAA202102209999](https://openairdocs.org/sdr/VNAA202102209999.md): Rib · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/Bulkhead > LEFT NR 2 I/B LE RIB CRACKED @ WS 27.75. REMOVED AND REPLACED RIB. - [SDR VNAA202102209998](https://openairdocs.org/sdr/VNAA202102209998.md): Drag Angle · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Structure > RIGHT DRAG ANGLE CRACKED. REPAIRED PER REO-670-55-31-018. - [SDR VNAA202102209997](https://openairdocs.org/sdr/VNAA202102209997.md): Drag Angle · cracked · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Structure > LEFT DRAG ANGLE CRACKED. REPAIRED PER REO-670-55-31-018. - [SDR VNAA202102209996](https://openairdocs.org/sdr/VNAA202102209996.md): Stringer · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > CORROSION ON STRINGER SPLICE 21R @ FS 477. REMOVED AND REPLACED FACTORY STRINGER SPLICE. - [SDR VNAA202102209995](https://openairdocs.org/sdr/VNAA202102209995.md): Stringer · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > STRINGER 21R CORROSION @ FS 437 AND 453 (EA21-C7-53-032 REV IR). - [SDR VNAA202102209994](https://openairdocs.org/sdr/VNAA202102209994.md): Crossbeam · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Structure > FRAME CORROSION ON CROSSBEAM @ FS 349.00 WL 72.5/RB L8.0 ( EA21-C7-53-022 REV IR). - [SDR VNAA202102209993](https://openairdocs.org/sdr/VNAA202102209993.md): Seat Track · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > LEFT SEAT TRACK @ FS 701.45-FS 836.55-FS 988.00 CORROSION AND GOUGED. REMOVED AND REPLACED SEAT TRACK. - [SDR VNAA202102209992](https://openairdocs.org/sdr/VNAA202102209992.md): Seat Track · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > RIGHT SEAT TRACK (ITEM 24-27-32) CORRODED AND GOUGED @ FS 693.00-FS 992.00. REMOVED AND REPLACED SEAT TRACK. - [SDR VNAA202102209991](https://openairdocs.org/sdr/VNAA202102209991.md): Angle · corroded · Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > DURING A HEAVY MAINTENANCE CHECK A VISUAL INSPECTION DETECTED SOME CORROSION ALONG THE 1/4" TURN ANGLE AT FS 280.00, LBL/RBL 12.00. REMOVED AND REPLACED THE 1/4 TURN ANGLE AND CORNER GUSSETS. - [SDR VNAA202102081111](https://openairdocs.org/sdr/VNAA202102081111.md): Striker · dented · Feb 4, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > DURING SCHEDULED MAINTENANCE, THE MAINTENANCE TEAM IDENTIFIED THAT THE SH670-31912-5 LOWER SEAL STRIKER PLATE WAS REPAIRED VIA REO 670-53-22-085 AND A TEMPORARY FASTENER (CR3212-4 OR CR3222-4 OR CR3522-4) INSTALLED. MAINTENANCE REQUESTS A PERMANENT REPAIR (MS2 - [SDR VNAA2020021671101](https://openairdocs.org/sdr/VNAA2020021671101.md): Warning Message · illuminated · Feb 7, 2020 · N503AE · Cndair CL6002C10 · Stall Warning System > STALL FAIL AMBER CAUTUON ON TAKEOFF. MAINTENANCE INSPECTED AND CLEANED PITOT WATER TRAPS AND PUGED THE PITOT SYSTEM WITH NO FURTHER DEFECTS NOTED. - [SDR VNAA2019120311101](https://openairdocs.org/sdr/VNAA2019120311101.md): Selector Valve · failed · Dec 3, 2019 · N503AE · Cndair CL6002C10 · Landing Gear Retraction/Extension System > DURING CLIMB AT AROUND 14,000FT AGL, THE CREW RECEIVED A PROXY SYSTEM FAULT MESSAGE. THEY DECLARED AN EMERGENCY AND FOLLOWED THE QRH, WHICH TOLD THEM TO LAND ON LONG RUNWAYS AND AVOID HIGH WINDS. THEY CONFERRED WITH THEIR DISPATCHER AND DETERMINED THEY NEEDED - [SDR VNAA2019040711102](https://openairdocs.org/sdr/VNAA2019040711102.md): Spoiler Sys · malfunctioned · Apr 7, 2019 · N503AE · Cndair CL6002C10 · Drag Control System > CREW RECEIVED A IB SPOILER CAUTION MESSAGE. ATC DECLARED A EMERGENCY FOR THE CREW AND AS SOON AS THE FLIGHT WAS SAFELY ON THE GROUND AND OFF THE RUNWAY IN CLT THE EMERGENCY VEHICLES WERE CALLED OFF. THE FLIGHT WAS ABLE TO TAXI TO A GATE UNDER THEIR OWN POWER. - [SDR VNAA2018111211101](https://openairdocs.org/sdr/VNAA2018111211101.md): Control Valve · malfunctioned · Nov 5, 2018 · N503AE · Cndair CL6002C10 · Engine Start Valves/Controls > AFTER DEPARTURE, THE CREW REPORTED NO STARTER CUT OUT AND DIVERTED AND LANDED WITH NO FURTHUR INCIDENTS. CURRENTLY IN MAINTENANCE.GSP MAINTENANCE REPLACED THE STARTER CONTROL VALVE. - [SDR VNAA2017081411101](https://openairdocs.org/sdr/VNAA2017081411101.md): Controller · faulty · Aug 14, 2017 · N503AE · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal > WHILE IN CRUISE, THE CREW SEEN SOME SPARKS AND A SMALL PUFF OF SMOKE FROM THE LEFT HAND WINDSHIELD, AROUND THE TERMINAL BLOCK. NO EMERGENCY WAS DECLARED. THE AIRCRAFT LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE REPLACED THE LEFT WINDSHIELD HEAT CONTROLLER - [SDR VNAA2017071000004](https://openairdocs.org/sdr/VNAA2017071000004.md): Light · inoperative · Feb 16, 2017 · N503AE · Cndair CL6002C10 · Emergency Lighting > CABIN FLOOR LEVEL EMERGENCY FLOODLIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY FLOODLIGHTS. - [SDR VNAA2017010800003](https://openairdocs.org/sdr/VNAA2017010800003.md): Unknown · unknown · Jan 7, 2017 · N503AE · Cndair CL6002C10 · Cabin Pressure Control System > AIRCRAFT WILL NOT PRESSURIZE, - [SDR VNAA2016092100048](https://openairdocs.org/sdr/VNAA2016092100048.md): Frame · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, Frame > LOWER FRAME SECTOR AT FS 549 STRINGER 16L CORRODED. MAINTENANCE REPAIRED THE FRAME SECTOR AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100042](https://openairdocs.org/sdr/VNAA2016092100042.md): Floor Support · cracked · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > UPPER FLANGE FLOOR PANEL SUPPORT AT FLOORBEAM IS CRACKED AT FS 582 LBL 9. MAINTENANCE PERFORMED A MAJOR REPAIR TO THE FLOOR PANEL SUPPORT AT FS 582 AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100041](https://openairdocs.org/sdr/VNAA2016092100041.md): Frame · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, Frame > BS 310 FRAME CORRODED BETWEEN STRINGERS 26 AND 27R. MAINTENANCE REMOVED AND REPLACED FRAME AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100040](https://openairdocs.org/sdr/VNAA2016092100040.md): Seat Track · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings > CABIN SEAT TRACK RBL 9 BS 581-677 HAS AREAS OF CORROSION. REMOVED AND REPLACED THE SEAT TRACK AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100039](https://openairdocs.org/sdr/VNAA2016092100039.md): Intercostal · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > INTERCOSTAL AND CLEAT CORRODED BELOW SERVICE DOOR THRESHOLD BS 319 - 349, STRINGER 20R. MAINTENANCE BLENDED INTERCOSTAL, REMOVED AND REPLACED CLEAT AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100038](https://openairdocs.org/sdr/VNAA2016092100038.md): Frame · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, Frame > FS 549 IS CORRODED BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPLACED THE CORRODED FRAME SEGMENT IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016092100037](https://openairdocs.org/sdr/VNAA2016092100037.md): Frame · corroded · Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, Frame > FS 597 CORRODED AT FS 597, STRINGER 17L - 18L. MAINTENANCE BLENDED CORROSION AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE. - [SDR VNAA2016082200029](https://openairdocs.org/sdr/VNAA2016082200029.md): Audio Panel · inoperative · Aug 22, 2016 · N503AE · Cndair CL6002C10 · Audio Integrating System > CAPTAIN`S AUDIO CONTROL PANEL FAILED IN FLIGHT, OBSERVERS AUDIO CONTROL PANEL WAS ALREADY DEFERRED. CREW DIVERTED AND LANDED WITHOUT INCIDENT. MAINTENANCE R & R CAPTAINS AUDIO CONTROL PANEL AND R & R OBSERVERS AUDIO CONTROL PANEL IAW AMM, OPS CHECKED GOOD. - [SDR VNAA2016011800018](https://openairdocs.org/sdr/VNAA2016011800018.md): Proximity Sensor · out of adjust · Jan 18, 2016 · N503AE · Cndair CL6002C10 · Landing Gear Position and Warning > CREW REPORTED GEAR DISAGREE WARNING MESSAGE AFTER TAKEOFF AND CLIMBING THROUGHT 4000 FEET. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND ADJUSTED PX22 SENSOR AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SERVICE. - [SDR VNAA2016011500014](https://openairdocs.org/sdr/VNAA2016011500014.md): Controller · failed · Jan 15, 2016 · N503AE · Cndair CL6002C10 · Airfoil Anti/De-ice System > CREW REPORTED RT BLEED DUCT WARNING MESSAGE FOLLOWED BY RT BLEED DUCT AMBER MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT, R & R ANTI-ICE AND LEAK DETECTION CONTROLLER AND PERFORMED CHECKS IAW AMM. ACFT RELEASED FOR SE - [SDR VNAA2016011500013](https://openairdocs.org/sdr/VNAA2016011500013.md): Seal · leaking · Jan 15, 2016 · N503AE · Cndair CL6002C10 · Pneumatic Distribution System > CREW REPORTED RT BLEED DUCT WARNING MESSAGE FOLLOWED BY RT BLEED DUCT AMBER MESSAGE. CREW RETURNED TO FIELD AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT AND INSPECTED AND FOUND RT PYLON BLEED AIR SUPPLY STUB DUCT OUTER SLEEVE DAMAGED AND SEAL LEAKING - [SDR SIMA20150824007](https://openairdocs.org/sdr/SIMA20150824007.md): Skin · damaged · Aug 24, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, Plate/Skin > FOR THE LOWER BEACON, THE AFT RT NUTPLATE HAS BEEN REMOVED & THE EFFECTED HOLE IS ELONGATED TO 1/4 " AT ITS LONGEST DIMENSION. INSTALLED NEW UPPER BEACON NUTPLATE IAW SRM 51-42-06. REPAIRED LOWER BEACON, NUTPLATE & ELONGATED HOLE, IAW ERS-CR-53MR-1575. - [SDR SIMA20150818006](https://openairdocs.org/sdr/SIMA20150818006.md): Crossbeam · corroded · Aug 18, 2015 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous Structure > CROSSBEAM AT FS 280.00 IS CORRODED. R & R LT FS 280 CROSSBEAM SEGMENT IAW SRM 51-42-06 & 51-42-13. - [SDR SIMA20150818005](https://openairdocs.org/sdr/SIMA20150818005.md): Stiffener · cracked · Aug 18, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, Bulkhead > 2ND FROM INBD VERTICAL STIFFENER AT FS 280, FWD SIDE OF BULKHEAD WEB IS CRACKED AT THE BOTTOM. R & R 2ND FROM INBD VERTICAL STIFFENER AT FS 280 FWD SIDE OF BULKHEAD WEB IAW SRM 51-42-06. - [SDR SIMA20150817005](https://openairdocs.org/sdr/SIMA20150817005.md): Drag Angle · cracked · Aug 17, 2015 · N503AE · Cndair CL6002C10 · Passenger/Crew Doors > SPLICED IN SECTION OF THE AFT DRAG ANGLE ON THE MAIN PAX DOOR IS CRACKED 1.5 INCHES. INSTALLED NEW DRAG ANGLE IAW SRM 52-11-04. - [SDR SIMA20150602001](https://openairdocs.org/sdr/SIMA20150602001.md): Stringer · unknown · Jun 2, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer > PERFORMED MAJOR REPAIR TO LINTEL STRINGER 3 OF MAIN PAX DOOR BY SB 670BA-53-0404 REV C. - [SDR SIMA20150421001](https://openairdocs.org/sdr/SIMA20150421001.md): Bulb · inoperative · Apr 21, 2015 · N503AE · Cndair CL6002C10 · Emergency Lighting > EMERGENCY EXIT LIGHT OVERHEAD BETWEEN FIRST CLASS & COACH DOESN'T TEST. REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD. Next page: https://openairdocs.org/aircraft/N503AE/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 = 'N503AE' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N503AE/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.