N503AE

Service difficulty reports · 141

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR VNAA2024060511101Fan · odorMODERATE 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 GJun 2, 2024 · N503AE · Cndair CL6002C10 · Indicating/Recording SystemSDR VNAA2023110911101Unknown · unknown8,500LBS 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 TONov 5, 2023 · N503AE · Cndair CL6002C10 · Flight Control SystemSDR VNAA2023110111101Acm · unserviceableSMOKE 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 GOODOct 30, 2023 · N503AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA202309131111Unknown · unknownELECTRICAL 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 TEMSep 12, 2023 · N503AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202207169991Strap · corrodedLH MLG TRUNNION AFT STEEL STRAP FOUND TO BE CORRODED ON AFT EDGE BETWEEN LBL 22.5 AND LBL 45.Jul 16, 2022 · N503AE · Cndair CL6002C10 · Main Landing GearSDR VNAA202206271111Hub Cap · missingA/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-Jun 24, 2022 · N503AE · Cndair CL6002C10 · Brake Anti-Skid SectionSDR VNAA202203141113Lever · unserviceableGEAR 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 GEMar 11, 2022 · N503AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA202111151113Dcu · faultedSHORTLY 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 OVERWNov 13, 2021 · N503AE · Cndair CL6002C10 · Central ComputersSDR VNAA202111151111Warning Message · multiple failCREW 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 ANNov 12, 2021 · N503AE · Cndair CL6002C10 · Central WarningSDR VNAA2021022099916Bracket · crackedCRACK ON BRACKET IN NOSE HYDRAULIC BAY LT SIDE. REMOVED AND REPLACED BRACKET.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA2021022099915Hinge · crackedGALLEY SERVICE DOOR UPPER AFT HINGE CRACKED. INSTALLED BRACKET.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Door HingeSDR VNAA2021022099914Bracket · crackedSLAT TRACK 1-3 CANISTER BRACKET CRACKED. REPAIRED PER REO 670-57-42-577.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Attach FittingsSDR VNAA2021022099913Structure · crackedRIGHT ENG CORE COWL HAS 3" CRACK AT THE 8 O'CLOCK POSITION, REPAIRED.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Nacelle/Pylon, Main FrameSDR VNAA2021022099912Rib · crackedRIGHT I/B FIXED LE RIB CRACKED. REMOVED AND REPLACED.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/BulkheadSDR VNAA2021022099911Rib · crackedRIGHT I/B FIXED LE PARTIAL RIB CRACKED. REMOVED AND REPLACED.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/BulkheadSDR VNAA2021022099910Intercostal · crackedNOSE GEAR BAY HYDRAULIC INTERCOSTAL CRACKED. REMOVED AND REPLACED INTERCOSTAL.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202102209999Rib · crackedLEFT NR 2 I/B LE RIB CRACKED @ WS 27.75. REMOVED AND REPLACED RIB.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Wing, Rib/BulkheadSDR VNAA202102209998Drag Angle · crackedRIGHT DRAG ANGLE CRACKED. REPAIRED PER REO-670-55-31-018.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202102209997Drag Angle · crackedLEFT DRAG ANGLE CRACKED. REPAIRED PER REO-670-55-31-018.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202102209996Stringer · corrodedCORROSION ON STRINGER SPLICE 21R @ FS 477. REMOVED AND REPLACED FACTORY STRINGER SPLICE.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202102209995Stringer · corrodedSTRINGER 21R CORROSION @ FS 437 AND 453 (EA21-C7-53-032 REV IR).Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202102209994Crossbeam · corrodedFRAME CORROSION ON CROSSBEAM @ FS 349.00 WL 72.5/RB L8.0 ( EA21-C7-53-022 REV IR ).Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA202102209993Seat Track · corrodedLEFT SEAT TRACK @ FS 701.45-FS 836.55-FS 988.00 CORROSION AND GOUGED. REMOVED AND REPLACED SEAT TRACK.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202102209992Seat Track · corrodedRIGHT SEAT TRACK (ITEM 24-27-32) CORRODED AND GOUGED @ FS 693.00-FS 992.00. REMOVED AND REPLACED SEAT TRACK.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA202102209991Angle · corrodedDURING 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.Feb 20, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA202102081111Striker · dentedDURING 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 (MS2Feb 4, 2021 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2020021671101Warning Message · illuminatedSTALL FAIL AMBER CAUTUON ON TAKEOFF. MAINTENANCE INSPECTED AND CLEANED PITOT WATER TRAPS AND PUGED THE PITOT SYSTEM WITH NO FURTHER DEFECTS NOTED.Feb 7, 2020 · N503AE · Cndair CL6002C10 · Stall Warning SystemSDR VNAA2019120311101Selector Valve · failedDURING 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 Dec 3, 2019 · N503AE · Cndair CL6002C10 · Landing Gear Retraction/Extension SystemSDR VNAA2019040711102Spoiler Sys · malfunctionedCREW 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. Apr 7, 2019 · N503AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2018111211101Control Valve · malfunctionedAFTER 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.Nov 5, 2018 · N503AE · Cndair CL6002C10 · Engine Start Valves/ControlsSDR VNAA2017081411101Controller · faultyWHILE 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 CONTROLLERAug 14, 2017 · N503AE · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR VNAA2017071000004Light · inoperativeCABIN FLOOR LEVEL EMERGENCY FLOODLIGHTS INOPERABLE. REMOVED AND REPLACED EMERGENCY FLOODLIGHTS.Feb 16, 2017 · N503AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2017010800003Unknown · unknownAIRCRAFT WILL NOT PRESSURIZE,Jan 7, 2017 · N503AE · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA2016092100048Frame · corrodedLOWER 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.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016092100042Floor Support · crackedUPPER 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.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016092100041Frame · corrodedBS 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.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016092100040Seat Track · corrodedCABIN 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.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2016092100039Intercostal · corrodedINTERCOSTAL 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.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016092100038Frame · corrodedFS 549 IS CORRODED BETWEEN STRINGER 17L AND 18L. MAINTENANCE REPLACED THE CORRODED FRAME SEGMENT IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016092100037Frame · corrodedFS 597 CORRODED AT FS 597, STRINGER 17L - 18L. MAINTENANCE BLENDED CORROSION AND PERFORMED CHECKS IAW THE AMM. THE AIRCRAFT WAS RELEASED FOR SERVICE.Sep 21, 2016 · N503AE · Cndair CL6002C10 · Fuselage Main, FrameSDR VNAA2016082200029Audio Panel · inoperativeCAPTAIN`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. Aug 22, 2016 · N503AE · Cndair CL6002C10 · Audio Integrating SystemSDR VNAA2016011800018Proximity Sensor · out of adjustCREW 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.Jan 18, 2016 · N503AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR VNAA2016011500014Controller · failedCREW 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 SEJan 15, 2016 · N503AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR VNAA2016011500013Seal · leakingCREW 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 LEAKINGJan 15, 2016 · N503AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR SIMA20150824007Skin · damagedFOR 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.Aug 24, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20150818006Crossbeam · corrodedCROSSBEAM AT FS 280.00 IS CORRODED. R & R LT FS 280 CROSSBEAM SEGMENT IAW SRM 51-42-06 & 51-42-13.Aug 18, 2015 · N503AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150818005Stiffener · cracked2ND 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.Aug 18, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20150817005Drag Angle · crackedSPLICED 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.Aug 17, 2015 · N503AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20150602001Stringer · unknownPERFORMED MAJOR REPAIR TO LINTEL STRINGER 3 OF MAIN PAX DOOR BY SB 670BA-53-0404 REV C.Jun 2, 2015 · N503AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150421001Bulb · inoperativeEMERGENCY EXIT LIGHT OVERHEAD BETWEEN FIRST CLASS & COACH DOESN'T TEST. REMOVED AND REPLACED LIGHT BULB IAW AMM 33-51-09. OPS CHECK GOOD.Apr 21, 2015 · N503AE · Cndair CL6002C10 · Emergency Lighting
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