N513AE

Service difficulty reports · 179

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 = 'N513AE' 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 VNAA202005069999Frame · corrodedFRAME AT FS 693.00 CORRODED BETWEEN STGR 26R. REPLACED FRAME.May 6, 2020 · N513AE · Bombdr CL6002D15 · Fuselage Main, FrameSDR VNAA202005069991Skin · corrodedPAX DOOR FWD INNER SKIN IS CORRODED AROUND NUTPLATE HOLES FOR ACCESS PNL CUTOUTS 832AL, 832BL, 832D AND 832FL. INSTALLED NEW SERVICEABLE INNER SKIN ON PAX DOOR IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-22-001-001A01, AND 51-42-21-001-001-A01, AND 51-42-13-0May 6, 2020 · N513AE · Bombdr CL6002D15 · Passenger/Crew DoorsSDR VNAA2019122981101Windshield · crackedWHILE AT FL320, RIGHT WS CRACKED AND RECEIVED W/S HEAT MSG. BEGAN DESCENT AND RAN QRH. QRH CALLED FOR NEAREST SUITABLE. ONCE AT FL140, DECIDED TO DIVERT TO PHL. EMERGENCY WAS DECLARED AND TRUCKS DID ROLL. CABIN WAS NOT BRACED. UPON LANDING ON RWY 27L, AIRCDec 28, 2019 · N513AE · Cndair CL6002C10 · Flight Compartment WindowsSDR VNAA201908221101Clamp · detachedSHORTLY AFTER TAKE OFF THE CREW RECEIVED A LEFT ENGINE FIRE WARNING MESSAGE. THE CREW CUT OFF FUEL TO THE ENGINE AND THE FIRE EXTINGUISHED. THE CREW DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. THE FLIGHT LANDED SAFELY AND TAXIED TO THE GATE WHERE THE PAAug 21, 2019 · N513AE · Cndair CL6002C10 · Pneumatic Distribution SystemSDR VNAA2019061871101Unknown · unknownIMMEDIATELY AFTER LIFT-OFF, CREW HEARD LOUD NOISE THEN VIBRATION. CREW DECIDED TO RETURN TO CLT. UPON CHECKING THE SYSTEMS, THEY FOUND THAT THE ADG HAD DEPLOYED. AIRCRAFT LANDED OVERWEIGHT, BUT WITHOUT INCIDENT AND WAS ABLE TO TAXI TO THE GATE UNDER ITS OWN POJun 17, 2019 · N513AE · Cndair CL6002C10 · Standard Practices/StructuresSDR VNAA2019010111100Fadec · malfunctionedAFTER TAKEOFF THE CREW REPORTED A LT FADEC CAUTION MESSAGE AND RETURNE TO FIELD. MAINTENANCE SWAPPED FADEC'S AND MESSAGE CLEARED AND RETURNED TO SERVICE.Dec 26, 2018 · N513AE · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR SIMA20170730002Floor Panel · crackedLEFT SIDE OF THE FWD EQUIPMENT COMPARTMENT WEB FLOOR PANEL IS CRACKED 3/8 INCH. COMPLETED A REPAIR IAW ETN-CR-53-099.Jul 30, 2017 · N513AE · Cndair CL6002C10 · Fuselage Floor PanelSDR SIMA20170725008Stringer Splice · corrodedSTRINGER SPLICE 26R CORRODED BETWEEN BS 319 AND 333. REPLACED THE STRINGER SPLICE IAW SRM 51-42-06.Jul 25, 2017 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20170725006Stringer · corrodedSTRINGER 26L CORRODED BETWEEN BS 280 AND 295. REPLACED THE STRINGER IAW SRM 51-42-06.Jul 25, 2017 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20170725007Light · damagedRIGHT EMERGENCY LIGHT STRIP NR 8 IS DAMAGED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01.Jul 25, 2017 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170515003Latch · obstructedMAIN CABIN DOOR WILL NOT OPEN FROM INSIDE OR OUTSIDE. CLEANED DEBRIS FROM MAIN DOOR LATCH CAM AND UPPER DOOR FRAME ROLLERS. FUNCTIONAL CHECKED GOOD IAW MM 52-11-00.May 15, 2017 · N513AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20170415001Bpsu · failedFLAPS FAILED CAUTION MESSAGE AFTER TAKEOFF, DURING FLAP RETRACTION. REMOVED AND REPLACED A BAD RT FLAP BPSU IAW AMM 27-52-03-400-801. OPS CHECKED GOOD.Apr 15, 2017 · N513AE · Cndair CL6002C10 · Trailing Edge Flap Control SystemSDR SIMA20161112001Bulb · inoperativeNR 5 OVERHEAD EMERGENCY FLOOD LIGHT NOT WORKING. REMOVED AND REPLACED THE BULB IAW AMM 33-51-09. OPS CHECKED GOOD.Nov 12, 2016 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20160929004Adc · failedFIRST OFFICER LOST AIRSPEED, ALTITUDE, VS, I FD AND COMPASS ON SHORT FINAL. DEBRIEF WITH CAPTAIN, NO COMPARITOR WARNING DURING FINAL. LOGGED MDC EQ. ID. 005866 AND 005863 FOR MTX PURPOSES. REMOVED AND REPLACED THE NR 2 ADC. CHECKED GOOD IAW AMM 34-13-01.Sep 29, 2016 · N513AE · Cndair CL6002C10 · Air Data ComputerSDR SIMA20160919002Light · inoperativeLEFT REAR OVERWING EXTERIOR EMERGENCY LIGHT INOPERATIVE, REF AML PAGE 4080849, ITEM, NR 2, MEL 33-39. R & R LT REAR OVERWING EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15. OPS CHECK GOOD. MEL RESTORED.Sep 19, 2016 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20160702002Spring · out of adjustUNABLE TO OPEN MAIN PASSENGER DOOR FROM INSIDE OR OUTSIDE OF AIRCRAFT. DEFERRED MAIN PASSENGER DOOR IAW MEL 52-3 AUTH 070023D-A. ADJUSTED THE COUNTER BALANCE SPRINGS IAW AMM 52-11-17. OPS CHECKED OK, MEL ITEM RESTORED.Jul 2, 2016 · N513AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20160223003Pitot Tube · defectiveDURING CRUISE FLIGHT AT 28000' WITH THE ACFT COUPLED TO FIRST OFFICERS SIDE & FIRST OFFICER FLYING, ALTIMETER & ISI MATCH WITH 29.92 SET, CAPTAINS ALTIMETER SHOWING APPROX 150 FEET LOW. COUPLED FIRST OFFICERS TO CAPTAIN SIDE & AUTO PILOT ADJUSTED TO CAPTAIN AFeb 23, 2016 · N513AE · Cndair CL6002C10 · Pitot/Static SystemSDR SIMA20160206002Bushing · crackedRIGHT HINGE FITTING FOR THE AFT NLG DOOR, JUST FWD OF FRAME FS235.00 HAS A HAT BUSHING THAT IS CRACKED & MIGRATING FROM ITS BORE. INSTALLED NEW BUSHING IAW AMM 20-31-00.Feb 6, 2016 · N513AE · Cndair CL6002C10 · Fuselage, Door HingeSDR SIMA20160203005Longeron · corrodedLONGERON 25R IS CORRODED, BETWEEN FS 333.00 & 349.00. REPLACED LONGERON 25R, BETWEEN FS 319.00 & 364.00 IAW SRM 51-42-06.Feb 3, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20160203004Stringer · corrodedSTRINGER 26R HAS SPOTS OF CORROSION, BETWEEN FS 333.00 & 349.00. REPLACED STRINGER 26R, BETWEEN FS 333.00 & 364.00 IAW SRM 51-42-06.Feb 3, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20160203006Stringer · corrodedSTRINGER 26L HAS SPOTS OF CORROSION, FROM FS 333.00 TO 346.00. REPLACED STRINGER 26L, BETWEEN FS 333.00 TO 364.00 IAW SRM 51-42-06.Feb 3, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20160202008Stringer · corrodedSTRINGER 25R IS CORRODED, BETWEEN FRAMES FS 310.00 & 333.00. REPLACED STRINGER 25R FROM FS 280 TO 333 IAW SRM 51-42-06.Feb 2, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20160201005Floorbeam · crackedL BRACKET ATTACHED TO THE AFT SIDE OF FLOORBEAM FS 280.00, AT RBL 9.00 IS CRACKED APPROX 1 INCH. INSTALLED NEW L BRACKETS IAW SRM 51-42-06 & 51-42-21.Feb 1, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20160201007Floorbeam · crackedRIGHT SIDE OF FLOORBEAM FS 280.00 HAS A 1 INCH CRACK ON THE UPPER SURFACE, AT RBL 9.00. R & R IAW SRM 51-42-06.Feb 1, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20160201006Floorbeam · crackedFLOORBEAM FS 280.00 IS CRACKED, APPROX 3 INCHES ON THE LT UPPER SURFACE, BETWEEN LBL 9.00 & 18.00. R & R FS 280 FLOORBEAM LT SIDE IAW SRM 51-42-06.Feb 1, 2016 · N513AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20160127002Shelf · crackedFORWARD EQUIP BAY COMPARTMENT, INSIDE DOOR 212AR, SHEET METAL SHELF IS CRACKED UNDER THE ADG RETRACTION PUMP. COMPLIED WITH REPAIR OF FWD EQUIP COMPARTMENT INSIDE DOOR 212AR, SHEET METAL SHELF CRACK UNDER ADG RETRACTION PUMP IAW ETN-CR-53-099.Jan 27, 2016 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151225001Warning System · false activationINBOARD FLIGHT SPOILERS CAUTION MSG. INBD SPOILERON CAUTION MSG ON EICAS. LT INBD SPOILERON FAILED ON FLIGHT SYNOPTIC PAGE. INTEGRATED MDC, FOUND LT INBD MFS PCU & PCU JAMB MDC MSG. PERFORMED SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN- CR-27-093. Dec 25, 2015 · N513AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20151215004Heater · failedELECTRICAL BURNING ODOR IN COCKPIT ONCE POWER WAS APPLIED TO THE PLANE. INSPECTED COCKPIT FOUND ODOR TO BE COMING FROM LT SIDE CONSOLE. PERFORMED AC POWER GENERATION. OPERATIONS CHECKED IAW AMM 24-11-00. ODOR DISSIPATED THROUGHOUT OPS CHECKS. OPS CHECKED Dec 15, 2015 · N513AE · Cndair CL6002C10 · Ice/Rain Protection SystemSDR SIMA20151202002Warning System · activatedON CLIMB OUT, HYD 3A INOPERATIVE CAUTION, FOLLOWED BY HYD 3 LOW PRESS & INBD SPOILERONS CAUTION. COMPLIED WITH PROCEDURES & RETURNED IAW MOC INSTRUCTIONS. PERFORMED SELF-TEST OF THE SPOILER & STABILIZER CONTROL UNIT FOUND WORKING PROPERLY IAW AMM 27-61-05. Dec 2, 2015 · N513AE · Cndair CL6002C10 · Hydraulic Indicating SystemSDR SIMA20151020007Frame · damagedACFT WILL REQUIRE A MAJOR REPAIR. AIRWORTHINESS RELEASE FOR RT INTERCOSTAL REPAIR AT FS 1162.00 IAW 513-MQT-02095 & FRAME REPAIR AT LT FS 1162.00 IAW AML PG 3960106-3. COMPLIED WITH ACFT MAJOR REPAIR AIRWORTHINESS RELEASE FOR REPAIRS ON THIS LOG PAGE 3690109Oct 20, 2015 · N513AE · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20151020006Intercostal · damagedFOUND DAMAGED INTERCOSTAL, BETWEEN FRAMES 1144.00 & 1162.00 AT STRINGER 9R. DAMAGE FROM BROKEN BRACKET FOR WATER INJECTION LINE IAW NRWC 513-MQT-02094. MAJOR REPAIR. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-21 & 51-42-06.Oct 20, 2015 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20151020004Stringer · damagedFOUND DAMAGE ON STRINGER 7L, BETWEEN FRAMES 1144.00 & 1162.00. DAMAGE FROM BROKEN BRACKET FOR WATER INJECTION LINE IAW NRWC 513-MQT-02093. MAJOR REPAIR. COMPLIED WITH ERS-CR-53MR-1728.Oct 20, 2015 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20151020003Bracket · brokenRIGHT DUAL HEAT EXCHANGER WATER INJECTION LINE, UPPER & LOWER BRACKET BROKEN & CRACKED. INSTALLED NEW & LOWER BRACKETS IAW SRM 51-42-06 & 51-42-21 IAW 513-MQT-02094. BRACKET ASSEMBLY PN MM670-97111-006.Oct 20, 2015 · N513AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SIMA20151020002Bracket · brokenLEFT DUAL HEAT EXCHANGER WATER INJECTION LINE UPPER BRACKET IS BROKEN & CRACKED. R & R LT DUAL HEAT EXCHANGER WATER INJECTION LINE UPPER BRACKET IAW SRM 51-42-06.Oct 20, 2015 · N513AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SIMA20150828008Spoiler · malfunctionedINBOARD SPOILER, INBD FLIGHT SPOILER, THE LT INBD FLIGHT SPOILER DID NOT DEPLOY IN FLIGHT OR ON GND. INTERROGATED MDC, FOUND LT INBD MFS PCU & PCU JAM MDC MSG. PERFORM SPOST 1 RESET. PERFORMED OPERATIONS CHECK IAW ETN-CR-27-093. OPERATIONS CHECKED GOOD.Aug 28, 2015 · N513AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150816002Warning System · false activationINBD SPOILERONS CAUTION MSG. MSG APPEARED SIMULTANEOUSLY WITH INBD FLIGHT SPOILERS CAUTION MSG. COMPLIED WITH ETN CR -27 093, NO DEFECTS NOTED.Aug 16, 2015 · N513AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20150724002Cooling Fan · failedDISPLAY COOL CAUTION MSG, FOLLOWED BY BURNING SMELL IN COCKPIT ON APPROACH TO LANDING. MEL DISPLAY FAN AVIONICS GND ALTN POSITION INOPERATIVE. DEFERRED MEL 21-5 CAT C M PROV COMPLIED WITH. R & R DISPLAY COOLING FAN IAW AMM 21-24-12. OPERATIONS TEST IAW AMJul 24, 2015 · N513AE · Cndair CL6002C10 · Air Distribution FanSDR SIMA20150424001Structure · crackedWHILE PERFORMING SB 670BA-53-040 REV C, FOUND PAX DOOR LINTEL, STRINGER 3, CRACKED. REPAIRED IAW SB 670BA-53-040 REV C & REO 670-53-21-493.Apr 24, 2015 · N513AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20150328004Wire · damagedCEILING EMERGENCY FLOODLIGHT INOPERATIVE AT ROW 10. SPLICED WIRE IAW ESPM 20-44-00 OPS TEST GOOD IAW MM 33-51-00.Mar 28, 2015 · N513AE · Cndair CL6002C10 · Light System WiringSDR SIMA20150217005Proximity Sensor · faultyAFTER TAKEOFF, PAX DOOR HDL, CAUTION MSG. THEN FOLLOWED BY PAX DOOR WARNING MSG. R & R DOOR PROX SENSOR PX101 IAW MM 52-70-04. INSPECTED ADJUSTMENT OF SENSOR PX107 IAW MM 52-70-04-820-808. OPERATIONS CHECKED GOOD.Feb 17, 2015 · N513AE · Cndair CL6002C10 · Door Warning SystemSDR SIMA20150212003Structure · dentedDENT ON TOP EDGE OF RT RVSM AREA. REPAIRED DENT IAW ERS-CR-53MR-1079.Feb 12, 2015 · N513AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150109001Cradle · brokenCAPTAINS SIDE FLASHLIGHT CRADLE IS BROKEN. R & R CAPTAINS SIDE FLASHLIGHT CRADLE IAW AMM 25-61-06. OPERATIONS CHECKED GOOD.Jan 9, 2015 · N513AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20141217001Battery Pack · dischargedFIRST OFFICER FOUND EMER LTS LIFTED IN THE ARM POS WITH NO APU ON OR GPU PLUGGED IN. STARTED APU TO CHARGE BATTERIES, AFTER 10 MINS, LIGHTS ARE STILL FLICKERING WHEN TURNED O. R & R ALL 4 ESPU BATTERY PACKS IAW MM 33-51-17. OPERATIONS CHECKED GOOD. SEE MX Dec 17, 2014 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140812004Attach Bracket · brokenTRANSFERRED FROM AML PAGE 3651037 ITEM 1. TRANSFERRED FROM NRWC 513-XNA-01700 ITEM 3. UPPER RT PACK WATER INJECTION LINE ADEL CLAMP ATTACH BRACKET IS BROKEN WITH DAMAGE TO STRINGER. THIS IS A MAJOR REPAIR. R & R ATTACH BRACKET, COMPLIED WITH REPAIR ON STRIAug 12, 2014 · N513AE · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20140811006Stringer · wornTRANSFERRED FROM NRWC 513-XNA-01700 ITEM 1. RT PACK WATER INJECTION LINE BONDING STRAP HARDWARE WORE HOLE INTO NEARBY STRINGER. TRANSFERRED TO NRWC 513-MQT-01712, THIS IS A MAJOR REPAIR. COMPLIED WITH PERMANENT REPAIR IAW ERS-CR-5300-673R1 & SRM 51-42-06 & Aug 11, 2014 · N513AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20140626005Light · inoperativeONE CEILING LIGHT CABIN IS INOPERATIVE. DEFERRED IAW MEL 33-34, LIGHT DEFERRED IS NR 4. R & R BULB IAW AMM 33-51-09. OPERATIONS CHECKED GOOD, MEL RESTORED.Jun 26, 2014 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140610006Light · inoperativeLEFT FUSELAGE EXTERIOR EMER LIGHT JUST AFT OF EMER EXIT FAILS TO ILLUMINATE. R & R LIGHT BULB IN EMER LIGHT ON LT FUSELAGE AFT OF LT EMER EXIT IAW CMM 33-52-07. OPERATIONS CHECKED GOOD.Jun 10, 2014 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140408003Light · looseEMERGENCY OVERHEAD LIGHT BY ROW 7 INOPERATIVE. SECURED LOOSE BULB IAW MM 33-51-09, OPERATIONS CHECKED GOOD.Apr 8, 2014 · N513AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140204005Engine · vibrationON TAKEOFF TKO E1 VIB ON 1.4. VIBE CLIMBED DURING ACCENT AT 17,500 E2 VIB WENT AMBE AT 1.8. THRUST REDUCED TO CRUISE POWER TO LOWER VIB. GOT VIB REDUCED TO 1.6 THEN WITHOUT INPUT VIB RETURNED TO AMBER 1.8 BOTH REDUCED TO TAKE VIB TO GREEN RANGE AT 1.4 AT 22Feb 4, 2014 · N513AE · Cndair CL6002C10 · Engine (Turbine/Turboprop)SDR SIMA20131124002Warning System · false activationON GO AROUND AFTER SELECTING FLAP EIGHT FLAP FAILED CAUTION MESSAGE CAME ON. PERFORMED OPERATIONS CHECK OF FLAP SLAT SYS IAW FIM TASK 27-52041-810-809-A01 FAILED MESSAGE DID NOT APPEAR, OPERATIONS CHECKED GOOD.Nov 24, 2013 · N513AE · Cndair CL6002C10 · Trailing Flap Position Indicating System
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