N504AE

Service difficulty reports · 169

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 = 'N504AE' 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 VNAA2021051699914Support Strap · corrodedFOUND THE RH FSL 36 FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED FROM FS 847-879. INSTALLED NUTPLATES AND NEW STRAP AT FUS FAIRING SUPPORT FS 847.0 TO 879, RBL 36.0 IAW CRJ700 SRM 51-42-06-001-001-A01May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2021051699913Support Strap · corrodedFOUND THE LH BL 36 FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED FROM FS 847-879. INSTALLED NEW SREVICEABLE SUPPORT STRAP IAW CRJ 700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01 AND 51-42-06-001-001-A01.May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2021051699912Support Strap · corrodedFOUND THE LH LOWER FS 879. FUSELAGE FAIRING SUPPORT STRAP TO BE CORRODED AND THE RH LOWER STRAP ALSO. INSTALLED NEW SERVICEABLE LH AND RH LOWER FS 879 FAIRING SUPPORT STRAP IAW CRJ 700 SRM 51-42-10-001-001-A01 AND 51-42-06-001-001-A01May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2021051699911Support Strap · corrodedFOUND THE FS 879.909 FUSELAGE FAIRING SUPPORT STRAP AT RBL 17 TO BE CORRODED. INSTALLED FUSELAGE FAIRING SUPPORT STRAP FROM FS 879-909 RBL 17 IAW CRJ 700 SRM 51-42-06-001-001-A01,SRM51-45-00-001-001-A01, SRM 51-42-06-001-001-A01.May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA2021051699910Strap · corrodedFOUND THE FS 879.909 FUSELAGE FAIRING SUPPORT STRAP AT LBL 17 TO BE CORRODED. INSTALLED NEW SREVICEABLE SUPPORT STRAP IAW CRJ 700 SRM'S 51-42-10-001-001-A01 AND 51-42-06-001-001-A01May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA 202105169999Strap · corrodedFOUND THE FS 909 FUSELAGE FAIRING SUPPORT MID STRAP TO BE CORRODED. INSTALLED NEW SERVICEABLE FS 909 MID STRAP IAW CRJ700 SRM'S 51-42-06-001-001-A01 AND 51-42-10-001-001-A01.May 16, 2021 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR VNAA 202105169998Skin · corrodedINTERNAL SKIN CORRODED BETWEEN STGR 26L AND 26R FROM FS 677.00 TO 693.00. REPAIRED PER REO 670-53-31-630 AND REO 670-53-31-648May 16, 2021 · N504AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA 202105169997Support Angle · corrodedFOUND THE AFT FUSELAGE FAIRING SUPPORT ANGLE AT FS 939 TO BE CORRODED AT THE CENTERLINE. INSTALLED NEW SERVICEABLE SUPPORT ANGLE IAW CRJ 700 SRM 51-42-06-001-001-A01.May 16, 2021 · N504AE · Cndair CL6002C10 · Fuselage Main, StructureSDR VNAA 202105169996Attach Angle · corrodedFWD WING TO FUSELAGE FAIRING ATTACH ANGLES AT FS661 ARE CORRODED AT ALL NUTPLATE LOCATIONS AND CHAFED TOP EDGES. REPLACED LH ATTACH ANGLE AT FS 661 FWD BELLY FAIRING IAW CRJ 700 SRM 51-42-06-001-001-A01.May 16, 2021 · N504AE · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR VNAA 202105169995Angle · corrodedFWD WING TO FUSELAGE FAIRING ATTACH "T" IS CORRODED AND CRACKED. ATTACH "T" ANGLE IS BETWEEN FS629 AND FS661. LOCATED AND INSTALLED NEW ATTACH "T" ANGLE FS 661-629 IAW CRJ 700 SRM 51-42-06-001-001-A01,SRM 51-40-11-001-001-A01,SRM 51-42-15-001-001-A01 BLUEPRINTMay 16, 2021 · N504AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA 202105169994Skin · corrodedPAX DOOR INNER SKIN IS CORRODED AROUND PANELS 832FL, 832DL, 832BL AND 832AB. LOCATED AND DRILLED NEW SERVICEABLE SKIN AND INSTALLED NUTPLATES IAW CRJ 700 SRM 51-40-11-001-001-A01,51-42-06-001-001-A01 AND 51-45-00-001-001-A01 REV 38 DATED JUL25/2020.May 16, 2021 · N504AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA 202105169993Intercostal · corrodedPAX DOOR INTERCOSTAL CORRODED UNDER PANEL 832DR. LOCATED, DRILLED AND INSTALLED NEW INTERCOSTAL P/N 601R31802-317 IAW CRJ700 SRM 51-40-11-001-001-A01 REV 38 DATED JUL 25, 2020May 16, 2021 · N504AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA 202105169992Former · corrodedPAX DOOR FWD FORMER IS CORRODED UNDER PANEL 832FL. LOCATE DRILL AND INSTALLED NEW FWD FORMER FROM PAX DOOR. FS311.75 P/N 601R318031-5 IAW CRJ700 SRM 51-40-11-001-001-A01 REV 38 DATAED JUL 25/2020.May 16, 2021 · N504AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA 202105169991Web · corrodedPAX DOOR FWD WEB IS CORRODED AT THE TOP, MARKED WITH TAPE, AROUND PANEL 832JL. LOCATED, DRILLED AND REPLACED PAX DOOR FWD WEB IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-40-11-001-001-A01, REV.38,May 16, 2021 · N504AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR VNAA202011121111Warning Message · illuminatedDURING CLIMBOUT, THE CREW RESCIEVED AND AUTO PRESSURIZATION FAIL MESSAGE, AND DIAGNOSED THAT THEY HAD LOST THEIR PRESSURIZATION CONTROLLER. THE FLIGHT RETURNED TO DEPARTURE. NO EMERGENCY WAS DECALRED, NOR WERE PASSENGERS TOLD TO BRACENov 11, 2020 · N504AE · Cndair CL6002C10 · Cabin Pressure Control SystemSDR VNAA202009051103Pin · pulledEMERGENCY EXIT LIGHT OVER GALLEY SERVICE DOOR INOP.TROUBLESHOT AND FOUND PIN IN SPLICE PULLED OUT. REPLACED SPLICE. OPS CHECK GOOD.Sep 5, 2020 · N504AE · Cndair CL6002C10 · Light System WiringSDR VNAA202009041101Battery · dischargedFWD EMER LIGHT ONLY REMAIN ON FOR APPROX 10 SEC AFTER A 30 MIN RECHARGE. R&R ALL 4 POWER SUPPLY BATTERIES. OPS CHECK GOOD. #1 P/N 2013-1A S/N 122903 TSN 11249 CSN 10266 TSI 661. #2 P/N 2013-1A S/N 82021 TSN 40067 CSN 33576 TSI 420. #3 P/N 2013-1A S/N 104882 TSSep 4, 2020 · N504AE · Cndair CL6002C10 · Emergency LightingSDR VNAA2019110111102Unknown · smokeIN FLIGHT CAPTAIN AND FO SAW AND SMELLED SMOKE FOR ABOUT 5 TO 10 SEC. NOTICED CBP1 D2 WAS POPPED RESET W/ MTX ON GROUND AND BREAKER POPPED AGAIN. C/W GVI OF CBP1 -D1 AND ASSOCIATED WIRING IAW CRJ 700 ESPM 20-25-00, NO DEFECTS NOTED. C/W OPS CHECK OF SSPC K10Nov 1, 2019 · N504AE · Cndair CL6002C10 · Air Distribution SystemSDR VNAA2019100751102Acm · failedBEFORE PUSHBACK THE CREW NOTICED A LARGE AMOUNT OF SMOKE IN THE CABIN WHILE THE AIRPLANE WAS PARKED. THEY DEPLANED THE PASSENGERS AND CALLED MAINTENANCE CONTROL. REMOVED AND REPLACED RH ACM IAW AMM 21-51-08-000/400-801-A01 OPS CHECKS GOOD.Oct 5, 2019 · N504AE · Cndair CL6002C10 · Cabin Cooling SystemSDR VNAA2019070311101Manifold · failedSTEERING INOP IN FLIGHT (NO INFORMATION AVAILABLE - NOT REPORTED) MX REPLACED NOSEWHEEL STEERING MANIFOLD. OPS AND LEAK CHECK GOOD.Jul 3, 2019 · N504AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2019062311101Warning Message · false activationAT ROTATION RECEIVED NOSE WHEEL STEERING INOP. RAN QRH AND IT DID NOT RESET. CAPTAIN CHOSE TO RETURN TO DEPARTURE DUE TO WX. EMERGENCY WAS DECLARED. PERFORMED OPS TEST OF NOSE WHEEL STEERING IAW AMM, OPS TESTED GOOD.Jun 23, 2019 · N504AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR VNAA2019010511101Warning System · false activationCREW REPORTED A NWS 'C' MSG IN FLT, THEY DECLARED AN EMERGENCY AND LANDED WITHOUT ISSUE. THE SYSTEM WAS RESET, OPS CHECKS GOOD.Jan 5, 2019 · N504AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA20180415001Bulb · inoperativeLAST OVERHEAD DOME EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM 33-51-09. OP CHECKED GOOD. NO FURTHER FAULTS NOTEDApr 15, 2018 · N504AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20180312006Manifold · failedSTEERING INOPERATIVE CAUTION MESSAGE. REMOVED AND REPLACED THE STEERING MANIFOLD IAW AMM 32-51-50. OPS & LEAK CHECKED GOOD.Mar 12, 2018 · N504AE · Cndair CL6002C10 · Landing Gear Steering SystemSDR SIMA20180307001Controller · failedAFTER TAKEOFF WITH APU SUPPLING AIR TO THE LEFT PACK AND RIGHT PACK INOPERATIVE. THE BLEED SYSTEM DID NOT SWITCH OVER TO ENGINE BLEEDS. LEFT PACK NEVER CAME ON. NO STATUS , ADVISORY OR CAUTION MESSAGES CAME ON. TRIED TO CONFIGURE SYSTEM MANUAL BUT COULD NOTMar 7, 2018 · N504AE · Cndair CL6002C10 · Cabin Temperature Control SystemSDR SIMA20171127001Drain · crackedNR 1 ADC FAILED ON LIFT OFF. CAPTAIN`S ALT FLAG, FOLLOWED BY IAS, THEN EFIS COMPUTER MONITOR CAUTION, FOLLOWED BY MACH TRIM CAUTION, AND RUDDER LIMIT FAULT STATUS. THEN L AND R FADEC FAULT 2 STATUS.-C/A-MDC MSG ADC 1 / NO OUTPUT #005846. PERFORMED P1 AND S1/SNov 27, 2017 · N504AE · Cndair CL6002C10 · Flight Environment DataSDR SIMA20171126003Adc · failedMULTIPLE INSURMENTATION LOSS EFIS COMP MON ALT ALT. IAS, MACH TRIM (CAUTION MSG) LOSS OF FLIGHT DIRECTOR, FADEC FAULTS IMEMED IATLY AFTER T. OFF-C/A-REMOVED AND REPLACED #1 ADC IAW AMM 34-13-01-000-801 OPS CHECK SYSTEM IAW 34-13-01-740-801 ALL SYSTEM GOODNov 26, 2017 · N504AE · Cndair CL6002C10 · Air Data ComputerSDR SIMA20171103003Line · leaking30 SECONDS AFTER GEAR HANDLE UP. LOST HYD 3 WITH A LOW PRESSURE GEAR DISAGREE. NOSE DOWN. BOTH MLG UP. RAN CHECKLIST FOR HYD 3. MANUALLY EXTENED GEAR, HYD 3 WAS 25%. HYD 3 35% BEFORE FLT, SERVICED BACK UP 48% HYD 3 NORMAL AT TAXI OUT. FOUND NOSE GEARNov 3, 2017 · N504AE · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20171027002Pin · disconnectedEMERGENCY OVERHEAD LIGHT 3RD FROM FRONT INOP. FOUND A PIN DISCONNECTED FROM CONNECTOR. INSTALLED THE PIN IAW ESPM 20-16-00. OPS CHECKED GOOD IAW AMM 33-51-00-710-802.Oct 27, 2017 · N504AE · Cndair CL6002C10 · Light System WiringSDR SIMA20170416002Light · inoperativeBULB OUT IN EMER EXIT SIGN AT LEFT OVERWING EXIT, FLOOR LEVEL. INSPECTED EMERGENCY LIGHTS. THEY ALL WORK. OPS CHECK GOOD. NO DAMAGE NOTED AT THIS TIME.Apr 16, 2017 · N504AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170409001Unknown · odorON APPROACH, FA SMELLED ELECTRICAL SMOKE FROM FORWARD CLOSET. CHECKED ALL COMPONENTS AND WIRING FOR A BURNING ODOR ON FWD CLOSET. VERIEFIED ALL LRU'S ARE OK FOR SERVICE, RELATED TO WIFI COMPONENTS ON FWD CLOSET. CHECKED AVIONICS COMPARTMENT FOR UNUSUAL ODApr 9, 2017 · N504AE · Cndair CL6002C10 · Air Distribution SystemSDR SIMA20161029003Skin · corrodedSKIN CORRODED BETWEEN BS 295 & 310 AND STRINGERS 26-27L. REPAIRED PER ERS-CR-53MR-2372.Oct 29, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20161029002Beam · damagedOVERHEAD BEAM WHERE AFT BAGGAGE BAY DOOR CARGO NET ATTACHES HAS BEEN CUT BY FORWARD RECOIL CABLE. PERFORMED REPAIR ON OVER HEAD BEAM ABOVE AFT BAGGAGE BAY DOOR IAW ERS-CR-53MR-2376.Oct 29, 2016 · N504AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20161029005Skin · gougedFUSELAGE SKIN IS GOUGED BETWEEN BS 969 AND FS985.00 AT STRINGER 27. REPAIRED FUSELAGE SKIN IAW ERS-CR-53MR-2377.Oct 29, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20161013007Frame · corrodedFRAME AT BS 295 IS CORRODED BETWEEN STRINGERS 26L AND 26R. REPAIRED IAW ERS-CR-53MR-2370 AND REO 670-53-21-1281.Oct 13, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20161013006Stringer · corrodedSTR 26LT IS CORRODED BETWEEN FS 333.00 AND FS 349.00. REPAIRED IAW ERS-CR-53MR-2375.Oct 13, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20161013004Stringer · corrodedSTR 26RT BETWEEN FS 295.00 AND FS 310.00 IS CORRODED IN SEVERAL SPOTS. COMPLETED INSTALLATION OF STRINGER 26R IAW SRM 51-42-06, AND SRM 51-42-20.Oct 13, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20161013003Stringer · corrodedSTRINGER 26R IS CORRODED BETWEEN BS 333.00 AND 349. INSTALLED A NEW STRINGER IAW SRM 51-42-06.Oct 13, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20161013002Stringer Splice · corrodedSTRINGER SPLICE 26R AT BS 333 IS CORRODED. INSTALLED A NEW STRINGER SPLICE IAW SRM 51-42-06.Oct 13, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20161011001Bulkhead · corrodedLEFT BULKHEAD ABOVE CROSSMEMBER AT BS 280 IS CORRODED. INSTALLED A REPAIR IAW SRM CH. 51-42-21.Oct 11, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20161011002Floorbeam · corrodedRIGHT SIDE OF CROSSMEMBER AT BS 280 IS CORRODED. INSTALLED RT OUTBD INERCOSTAL IAW SRM CH. 51-42-21.Oct 11, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20161011003Bulkhead · corrodedRIGHT BULKHEAD ABOVE CROSSMEMBER AT BS 280 IS CORRODED. REPAIRED IAW PART B , EO-CR-53MR-174.Oct 11, 2016 · N504AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20160606004Panel · unsecureEMERGENCY LIGHTS PANEL OVER SERVICE DOOR IS FALLING DOWN. DEFERRED GALLEY CEILING PANEL PENDING. RESECURED PANEL IAW STANDARD MAINTENANCE PRACTICES.Jun 6, 2016 · N504AE · Cndair CL6002C10 · Passenger Compartment EquipmentSDR SIMA20160226010Fitting · crackedWHILE PERFORMING SERVICE BULLETIN 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.Feb 26, 2016 · N504AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20151002003Warning System · false activationAT APPROX 10800, DURING CLIMB OUT PAX OUTER HDL CAUTION MSG POSTED PRESSURIZATION CLIMBING NORMAL, 20 SEC LATER PAX DOOR WARNING MSG POSTED ALONG WITH PROX SYS 1 STATUS MSG PRESSURIZATION STILL SEEMS NORMAL. RETURNED IAW EMER PROCEDURES. PERFORMED GVI OF PX1Oct 2, 2015 · N504AE · Cndair CL6002C10 · Door Warning SystemSDR SIMA20150424002Unknown · malfunctionedWING OVERHEAT WARNING COMPLIED WITH CL, WARNING WENT AWAY. RETURNED DUE TO ICING. REF ITEM 1 THIS LOG PAGE FOR ACTION TAKEN. IAW FIM TASK 30-12-00-810-802 PERFORMED OPERATIONS CHECK OF WING ANTI-ICE CONTROL & INDICATING SYS IAW MM 30-12-00, NO FAULT MSGS NOApr 24, 2015 · N504AE · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR SIMA20150304004Pseu · faultyABORTED TAKEOFF AT 70 KTS FOR GLD UNSAFE CAUTION. TRANSFERRED TO NRWC 504-XNA-01979. R & R PSEU IAW AMM 32-61-01. OPERATIONS CHECKED GOOD IAW AMM 32-61-00.Mar 4, 2015 · N504AE · Cndair CL6002C10 · Landing Gear Position and WarningSDR SIMA20141022001Cradle · brokenCAPTAIN`S FLASHLIGHT HOLDER FOUND BROKEN. REMOVED AND REPLACED THE FLASHLIGHT HOLDER IAW AMM 25-61-02.Oct 22, 2014 · N504AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20141017003Acm · malfunctionedRIGHT PACK AUTO FAIL PACK TEMP 99C & CAN'T BE REDUCED. MANUAL MODE UNRESPONSIVE. BURNING SMELL IN CABIN. R & R RT ACM IAW AMM 21-51-08. LEAK & OPERATIONS CHECKED GOOD.Oct 17, 2014 · N504AE · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20141013005Unknown · abnormalRIGHT PACK AUTO FAIL PACK TEMP 99C & CAN’T BE REDUCED. MANUAL MODE UNRESPONSIVE BURNING SMELL IN CABIN. ITEM DEFERRED IAW MEL 21-13.Oct 13, 2014 · N504AE · Cndair CL6002C10 · Cabin Cooling System
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