N516AE

Service difficulty reports · 115

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 = 'N516AE' 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 VNAA2026040950046Skin · chafedTEMP TO PERM DISPOSITION FOR BLENDED CHAFE DAMAGE TO THE LH IBD TRAILING EDGE LOWER SKIN PANEL EDGE MEMEBER.Mar 30, 2026 · N516AE · Cndair CL6002D24 · AileronsSDR VNAA2026040920491Skin · dentedDENT OF FUSELAGE. LOCATION FS 485Mar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2026040920489Skin · dentedDENT OF FUSELAGE. LOCATION FS 409-421 STGR 19RHMar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2026040920488Skin · dentedDENT OF FUSELAGE. LOCATION FS 394-409 STGR 17RH (BELOW WINDOW 2 RH)Mar 30, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR VNAA2026040920487Skin · dentedSKIN OUTER PAX DOOR HAS A DENT. LOCATION FS333, STRG 6-5LH.Mar 30, 2026 · N516AE · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA2026040920486Skin · dentedDENT ON SERVICE DOOR SKIN, OUTER FS333, BETWEEN STRG14-13.Mar 30, 2026 · N516AE · Cndair CL6002D24 · Service DoorsSDR VNAA2026040920126Slat Track · chafedRH WING SLAT 1 TRACK 1 WEAR ON UPPER SURFACE. LOCATION 14" FROM SLAT ATTACHMENT POINT.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA2026040920125Slat Track · chafedRH WING SLAT 2 TRACK 1 WEAR ON UPPER SURFACE. LOCATION 12.5" FROM SLAT ATTACHMENT POINT.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA2026040920123Slat Track · chafedLH WING SLAT 1 TRACK 1 HAS DAMAGE.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA2026040920127Slat Track · gougedRH SLAT 3 TRACK OBD HAS 3 SMALL GOUGES ON THE FLANGES OF THE TRACK UPPER SURFACE.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA2026040950052Skin · damagedDAMAGE ON SKIN LH OBD FLAP FS179.96 UPR BAY.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA2026040920559Cradle · wornR/H INBOARD FLAP, VANE ACTUATOR CRADLE ASSY, L/H INSIDE TRACK SHOWS WEAR.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Trailing Edge FlapsSDR VNAA2026040920149Crossbeam · corrodedCORROSION FOUND ON CROSSBEAM FS333 RH SIDE 5 IN FROM EDGE OF THE MEMBER P/N:SH670-32127-5.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA2026040920122Slat Track · gougedLH WING, SLAT 3 OBD TRACK HAS 4 MARKS IN TRACK UPPER SURFACES OF FLANGES.Mar 27, 2026 · N516AE · Cndair CL6002D24 · Leading Edge DevicesSDR VNAA2026040920077Floorbeam · corrodedDURING MAINTENANCE INTERGRANULAR CORROSION WAS FOUND ON BEAM LOCATED AT FLOOR SUPPORT STRUCTURE FS280. ALL CROSS THE UPPER SURFACE OF BEAM, WL72.5 . ADJACENT FINDING OF CORROSION ON ANGLE CAPS LBL11.128 FS280 AND RBL11.128Mar 27, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR VNAA2026040920230Door · corrodedMULTIPLE SPOTS OF BUBBLING/FLAKING PAINT IN INTERNAL PAX DOOR.Feb 27, 2026 · N516AE · Cndair CL6002D24 · Passenger/Crew DoorsSDR VNAA2026040920076Crossbeam · corrodedFS 280 CROSSBEAM HAS SIGNIFICANT CORROSION ACROSS THE UPPER SURFACES.Feb 12, 2026 · N516AE · Cndair CL6002D24 · Fuselage Main, StructureSDR VNAA2025052711101Fairing · missingRH INBOARD 2ND FLAP FAIRING MISSING, LOST IN FLIGHT / REMOVED WHAT WAS LEFT OF PANEL 686BB ON RH WING INBD FLAP IAW CRJ 700 AMM 57-51-84-000-802-A01.May 24, 2025 · N516AE · Cndair CL6002C10 · Trailing Edge FlapsSDR VNAA2024041711101Pcu · faultedOB FLT SPLRS AND OB SPOILERONS CAUTION MSG IN FLIGHT / T/S PER CRJ 700 FIM 27-64-01-810-807-A01-PSA, FAULT DID NOT RETURN. OPS TEST GOOD IAW CRJ 700 AMM 27-64-00-710-801-A01. REMOVED AND REPLACED LH OB MFS PCU IAW CRJ700 AMM27-62-01-000/400-801-A01-PSA. OPS ANApr 13, 2024 · N516AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA2023121811101Compensator · unserviceableAUTO XFLOW INHIB STATUS CLIMBING THRUGH 16000 FT. LOST LEFT FUEL TANK AND TOTAL FUEL INDICATION. / REMOVED AND REPLACED LH WING FUEL QUANITY PROBE 6 IAW CRJ AMM 28-41-09-000/400-801Dec 15, 2023 · N516AE · Cndair CL6002C10 · Fuel Indicating SystemSDR VNAA202204141111Track · brokenRH UPPER IB TRANSCOWL NYLON TRACK IS BROKEN. PERFORMED EA21-C7-78-710 AS TEMPORARY CORRECTIVE ACTION WITH EDDY CURRENT INSPECTION OF RH UPPER HINGE BEAM TRACK INSERT FASTENER HOLES IN ACCORDANCE WITH NDTM 51-20-006. NO CRACKS FOUND. PERFORMED REO 670-78-30-92Apr 13, 2022 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA202109281111Spoiler Sys · malfunctionedON FINAL APPROACH INTO CLT, THE AIRCRAFT OB SPOILERONS AND OB FLIGHT SPOILERS FAILED. THE FLIGHT CREW DECLARED EMERGENCY, AND LANDED THE AIRCRAFT SAFELY. EMERGENCY VEHICLES ROLLED, HOWEVER THEY WERE NOT NEEDED AS THE CREW CANCELLED THE EMERGENCY ONCE THEY WERESep 25, 2021 · N516AE · Cndair CL6002C10 · Drag Control SystemSDR VNAA202108191114Valve · stuckAFTER TAKE OFF FROM CLT THE CREW REPORTED A FUEL LEAK TO DISPATCH. THE CREW RETURNED THE FLIGHT TO CLT AND DECLARED A FUEL EMERGENCY. THEY LANDED SAFELY AND TAXIED TO THE GATE. THEY DID NOT LAND OVERWEIGHT. THE AIRCRAFT IS CURRENTLY IN MAINTENANCE. / CREW REPOAug 18, 2021 · N516AE · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR VNAA202107211112Windshield · smokeSINGLE PUFF OF SMOKE FROM CENTER FRONT WINDSHIELD. PERFORMED GVI/DAMAGE CHECK OF WINDSHIELDS IAW CRJ 700 AMM 56-11-01-210-801-PSA AND OPS CHECKED WINDSHIELD HEAT IAW CRJ 700 AMM 30-41-06-710-801, NO SIGNS OF DAMAGE OR FAULTS FOUND.Jul 18, 2021 · N516AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA202107211111Windshield · unserviceableAFTER TAKEOFF THE CREW STARTED TO SEE SMOKE ALONG THE FLIGHT DECK WINDOWS. THEY DECLARED EMERGENCY AND TURNED AROUND TO RETURN TO CLT. CAPTAIN DID NOT SPECIFY WHETHER OR NOT THEY WERE OVERWEIGHT ON LANDING. PASSENGERS DID NOT BRACE. FLIGHT RETURNED TO E19 AND Jul 18, 2021 · N516AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA202104019993Stringer · corrodedREMOVED CORROSION AT F.S. 319 STR 27 MATERIAL LOST .001 FOUND WITHIN LIMITS IAW CRJ-700 SRM 53-21-06. TREAT AND PRIME IAW SRM 51-21-11 (LEVEL 2 CPCP)Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202104019994Drag Angle · corrodedREPAIRED L/H DRAG ANGLE/AFT END @VERTICAL STABILIZER IAW BEMBARDRER REO 670-55-31-018Apr 1, 2021 · N516AE · Cndair CL6002C10 · Vertical StabilizerSDR VNAA202104019991Stringer · corrodedREPAIRED FRAME AT F.S. 517 BETWEEN STR 24L - 24R IAW EA21-C7-53-111. (LEVEL 2 CPCP) LEVEL 2 CORROSION.Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA202104019992Stringer · corrodedBLEND OUT CORROSION IAW CRJ-700 SRM 51-21-06 AND EA 21-C7-53-139. RESTORED FINISH IAW CRJ-700 SRM 51-21-11, 51-25-01 & EA 21-C7-53-139. LEVEL 2 CORROSION.Apr 1, 2021 · N516AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA2021011810111Unknown · odorIN FLIGHT TOXIC ODOR WAS NOTICED MAKING IT DIFFICULT TO BREATH ODOR CONTINUED THROUGHOUT ENTIRE FLIGHT FLIGHT DECK ONLY. PRESSURIZED LT AND RT PACK WITH APU AND RT ENGINE, IAW CRJ 700 AMM 21-50-00-862-801-A02 AND 21-50-00-862-805-A01, NO ABNORMAL SMELL NOTED.Jan 14, 2021 · N516AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA202012181112Control Valve · abnormalRTO-TAKING OFF RWY 6 IN ERI AT 40KTS THE CREW RECEIVED A RT THRUST REVERSER UNSAFE AMBER MESSAGE AND ABORTED TAKEOFF. CREW RETURNED TO GATE.Dec 16, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA202012071111Relay · abnormalTHE FLIGHT WAS TAKING OFF RWY 31 IN PIA AT 30KTS THE CREW RECEIVED A RT REVERSE UNSAFE CAUTION MESSAGE AND ABORTED TAKEOFF AND RETURNED TO GATE. DEF RT THRUST REVERSER SYSTEM, PER MEL 78-30-01 CAT C. M/FUNCTION C/W. DEACTIVATED THE RT THRUST REVERSER, IAW CDec 3, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA202011191111Warning Message · illuminatedREJECTED TAKEOFF FOR A RT THRUST REV UNSAFE CAUTION MESSAGE AT THE VERY BEGINNING OF THE TAKEOFF ROLL, LESS THAN 10 KNOTS. AIRCRAFT EXITED THE RUNWAY WITHOUT ISSUE AND RETURNED TO GATE WHERE MAINTENANCE HAS BEEN CALLED TO INSPECT AND TO POTENTIALLY DEFER THE Nov 18, 2020 · N516AE · Cndair CL6002C10 · Engine Thrust ReverserSDR VNAA20201013111Loop · unsecureRESECURED BLEED LOOP AROUND RT WING ANTI-ICE VALVE. OPERATIONS AND LEAK CHECK GOOD, IAW CRJ 700 AMM 30-12-00-710-802-A02 AND AMM 36-21-00-710-801-A01.Oct 10, 2020 · N516AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR VNAA2020100211102Seal · leakingFOUL SMELL FROM VENT IN COCKPIT. PERFORMED GVI OF RT AC PACK. FOUND AIR LEAK ON HEAT EXCHANGER PERI-SEAL/CONNECTOR. REPLACED PERI-SEAL. OPERATIONS AND LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.Sep 30, 2020 · N516AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2020091211101A/C Pack · odorOILY SMELL COMING FROM THE PACKS. INVESTIGATED OIL SMELL COMING FROM PACKS. COULD NOT REPLICATE PROBLEM. FOUND NO DEFECTS AT THIS TIME. OPS CHK OF A/C SYS SOURCING FROM APU & BOTH ENG ABOVE IDLE. NO ODORS DETECTED AT THIS TIME.Sep 11, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2020091111102Acm · failedFOUL ODOR COMING FROM PACKS. TROUBLESHOT PER FIM. INSPECTED APU AND LOAD CONTROL VALVE, FOUND NO EVIDENCE OF OIL CONTAMINATION. RAN PACKS IN ALL BLEED CONFIGURATIONS WITH AND WITHOUT ENGINES AND DETERMINED SMELL TO BE PREVALENT WITH LT PACK. SUSPECT LT ACMSep 9, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2020060211101Acm · failedCABIN FILLED WITH SMOKE FOLLOWED BY RT PACK AUTO FAIL WHILE AT GATE. MAINTENANCE REMOVED AND REPLACED THE AIR CYCLE MACHINE.May 29, 2020 · N516AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2019052511101Windshield · crackedDURING CRUISE AT FL330, CA WINDSHIELD CRACKED. EMERGENCY DECLARED FOR PRIORITY DESCENT AND FLIGHT DIVERTED INTO CLT. CA STATED THE INNER LAYER OF THE WINDSHIELD PEELED OFF AND LANDED ON HIS LAP. FLIGHT LANDED ON RWY 18L IN CLT AND CANCELLED THE EMERGENCY AFTEMay 25, 2019 · N516AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA2018100299904Floor Support · corrodedPAX DOOR SURROUND STRUCTURE CENTER FLOORBOARD SUPPORT ANGLE AND SILL ANGLE HAS CORROSION AT SCREW HOLES. REMOVED AND REPLACED SILL ANGLE SH670-31875-3 IAW SRM 51-42-06-001-001-A01, AND 51-42-21-001-001-A01.Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2018100299903Seat Track · corrodedRBL 9 FLOOR SEAT TRACK SEGMENTS FS 349 TO FS 485 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018100299902Seat Track · crackedLBL 9 FLOOR SEAT TRACK SEGMENTS FS 517 TO FS 581 AND FS 581 TO 683 ARE CORRODED. REMOVED SEAT TRACKS, FABRICATED NEW SEAT TRACKS AND INSTALLED IAW AMM 53-00-49 AND REO 670-53-00-343 REV M.Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018100299901Fitting · crackedFS 280 CROSSBEAM TO RBL 9 FLOORBEAM T FITTING IS CRACKED ON IB SIDE. FABBED & REINSTALLED 2 EA NEW ATTACH ANGLES AT FS 280 RBL 9.0 IAW SRM 51-42-21-001-001-A01 AND REO 670-53-11-165 REV B.Oct 2, 2018 · N516AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA2017110411101Warning System · activatedCREW REPORTED AP LWD CAUTION MSG. CREW DIVERTED TO BMH. MAINTENANCE INSPECTED FLIGHT CONTROL CABLES NO DEFECTS NOTED. DEFERRED AUTO PILOT.Nov 4, 2017 · N516AE · Cndair CL6002C10 · Autopilot SystemSDR SIMA20170914005Skin · damagedDURING HEAVY MAINTENANCE, DAMAGE WAS FOUND TO THE EXTERIOR FUSELAGE SKIN BETEWEEN BS 969 AND 985, STRINGER 27L. REPAIRED THE SKIN IAW ERS-CR-53MR-2905.Sep 14, 2017 · N516AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20170906008Crossbeam · crackedFRAME BS 280 LT SIDE CROSSBEAM CRACKED ON FWD SIDE BELOW CENTER COCKPIT FLOORBOARD. A NEW CROSSBEAM WAS INSTALLED IAW SRM 51--42-06, SRM 51-42-10, AND SRM 51-42-13.Sep 6, 2017 · N516AE · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20170107001Line · damagedDURING TAXI IN, LOST OF NOSE WHEEL STEERING HYDRAULIC SYSTEM NR 3 LOW PRESSURE AND ZERO QUANITY IN THE SYSTEM NR 3 RESEVOIR. REMOVED AND REPLACED THE REAR FLEXIBLE HYD HOSE FOR NLG RETRACT ACTUATOR IAW AMM 32-32-09. OPS AND LEAK CHECKED GOOD.Jan 7, 2017 · N516AE · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20161107002Connector · looseLAST TWO EMERGENCY DOME LIGHTS IN THE CABIN WILL NOT ILLUMINATE. FOUND LOOSE CONNECTOR ON EPSU 4. RE-SEATED CONNECTOR IAW ELECTRICAL STANDARD MTX PRACTICES. OPS CK GOOD. A/C OK FOR SERVICENov 7, 2016 · N516AE · Cndair CL6002C10 · Light System WiringSDR SIMA20160504001Pcu · malfunctionedON DESCENT, OTBD SPOILERONS, & OTBD FLIGHT SPOILERS", CAUTION MSGS. INTERROGATED MDC, FOUND, ROB MFS PCU FAILED PCU JAM. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN CR-27-093. OPERATIONS CHECKED GOOD. OPENED TDMI 516T2745 TA. R & R ROB MFMay 4, 2016 · N516AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20160406003Battery Pack · dischargedEMERGENCY LIGHTS AFT OF FIRST CLASS INOPERATIVE. R & R EPSU BATTERY PACK & CHARGER NR 3 IAW WC 33-002. OPERATIONAL TESTED GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 & SN 12337.Apr 6, 2016 · N516AE · Cndair CL6002C10 · Emergency Lighting
Back to N516AE