N522AE

Service difficulty reports · 156

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 = 'N522AE' 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 SIMA2018032600001Charger · inoperativeEMERGENCY LIGHT EXIT ROW INOPERATIVE. REMOVED AND REPLACED THE ESPU BATTERY CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD.Mar 24, 2018 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20180110006Switch Panel · intermittentEMERGENCY LIGHTS INTERMITTENT IN FLIGHT. OPS NORMAL ON GROUND. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT SWITCH PANEL IAW AMM 33-24-07.Jan 10, 2018 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20170113003Skin · dentedFUSELAGE DENTED BS 169 - 193. REMOVED AND REPLACED SKIN IAW SRM AND ERS-CR-53MR-2515Jan 13, 2017 · N522AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SIMA20170108001Support · crackedWING TO FUSELAGE AFT FAIRING SUPPORT AT BS 909, LBL 17.63 HAS A ONE INCH CRACK. REPAIRED IAW ERS-CR-5300-2519.Jan 8, 2017 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20170104004Angle · corrodedPAX DOOR MID CAP ANGLE AND KICK PLATE ANGLES HAVE AREAS OF CORROSION-C/A-REMOVED CORROSION FROM PAX DOOR KICKPLATE ANGLE AND FOUND TO BE WITHIN LIMITS IAW SRM 51-21-16. REPAINTED IAW SRM 51-25-16. REPLACED MID CAP ANGLE IAW SRM 51-42-06 AND AMM 20--21-06Jan 4, 2017 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20170104005Stringer · corrodedSTRINGER 25R CORRODED BETWEEN BS 333 AND 349. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-06 AND 51-42-21.Jan 4, 2017 · N522AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20170102003Floorbeam · damagedFLOORBEAM AT BS 280 CRACKED AND CORRODED ON RT SIDE, REPAIRED IAW SRM 51-42-06 AND SRM 51-42-13.Jan 2, 2017 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20170102002Floorbeam · crackedFLOORBEAM TEE CRACKED BS 280. INSTALLED A NEW TEE IAW SRM 51-42-06 AND SRM 51-42-21.Jan 2, 2017 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20161229003Drag Angle · crackedLT LOWER SIDE OF VERTICAL STAB. TO FUSELAGE L ANGLE HAS EVIDENCE OF TWO CRACKS. COMPLETED INSTALLATION OF FWD LH DRAG ANGLE AND SEALED AROUND EDGES IAW ERS-CR-55MR-502Dec 29, 2016 · N522AE · Cndair CL6002C10 · Vertical StabilizerSDR SIMA20161229004Structure · gougedBS 1015 - 1047 STRINGERS 21 - 25R GOUGED. REPAIRED IAW ERS-CR-53DF-2230 REV 1 PART C.Dec 29, 2016 · N522AE · Cndair CL6002C10 · Fuselage Main, StructureSDR SIMA20161229005Stringer · corrodedSTRINGER 26R CORRODED BETWEEN BS 280 AND 295. THE STRINGER REPAIRED IAW ERS-CR-53MR-2548.Dec 29, 2016 · N522AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20161003003Unknown · malfunctionedON APPROACH CREW EXPERIENCED UNCOMMANDED ROLL OF AIRCRAFT. CREW DISCONNECTED THE AUTOPILOT AND RATE OF ROLLING DECREASED. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. PERFORMED AILERON RIGGING CHECK AND AILERON OPS CHECKED IAW AMM 27-11-00 ALSO COct 3, 2016 · N522AE · Cndair CL6002C10 · Flight Control SystemSDR SIMA20160209003Glowstrip · inoperativeTHE EMER PATH LIGHTING GLOW STRIPS DO NOT APPEAR TO BE WORKING. TRANSFERRED TO NRWC 522-ORD-02141. CLEANED EMER PATH FLOOR STRIPS IN FWD CABIN. REPLACED STRIPS IN AFT CABIN IAW AMM 33-51-01.Feb 9, 2016 · N522AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20150719003Windshield · crackedCLIMBING THROUGH 18,000 FEET THE CAPTAINS SIDE WINDSHIELD CRACKED. DECLARED AN EMER & DIVERTED WITHOUT INCIDENT. REMOVED AND REPLACED CAPTAINS WINDSHEILD IAW CRJ-700 AMM 56-11-01 OPS CHECK GOOD AND LEAK CHECK GOODJul 19, 2015 · N522AE · Cndair CL6002C10 · Flight Compartment WindowsSDR SIMA20150718003Clamp · unsecureAFTER LEVELING OFF, LT BLEED DUCT WARNING POSTED, FOLLOWED BY LT BLEED DUCT CAUTION. FOUND AIR LEAK AT BELLOWS FOR LT ACM. TORQUED CLAMPS IAW AMM 21-51-14. REPOSITIONED SENSE LINE FOR LT BLEED DUCT CLAMPS FOR PYLON DUCT IAW AMM 36-21-01. RAN BOTH ENGS, NO Jul 18, 2015 · N522AE · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20150622006Stringer · damagedPERFORMED A MAJOR REPAIR TO LINTEL STRINGER 3L OF THE MAIN PAX DOOR BY INCORPORATING SB 670BA-53-040 REV C DATED SEP 20 2012.Jun 22, 2015 · N522AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150120006Unknown · malfunctionedWHILE BOARDING, TURNED RED ON RT PACK & ENTERED CABIN. PERFORMED OPERATION CHECK OF THE AIR CONDITIONING DISTRIBUTION SYS IAW AMM 21-51-00. NO DEFECTS NOTED.Jan 20, 2015 · N522AE · Cndair CL6002C10 · Cabin Cooling SystemSDR SIMA20150101002Light · sparksSIDE POST MAP LIGHT SPARKS WHEN MOVED WITH BURNING SMELL. R & R MAP LIGHT IAW AMM 33-13-03. OPERATIONS CHECKED GOOD.Jan 1, 2015 · N522AE · Cndair CL6002C10 · Flight Compartment LightingSDR SIMA20140510007Plate · crackedRIGHT FWD EQUIPMENT BAY PLATE UNDER ADG RETRACTION PUMP IS CRACKED APPROX. 3/8 INCHES. COMPLIED WITH REPAIR OF RH FWD EQUIPMENT BAY PLATE UNDER ADG PUMP IAW ETN CR-53-099.May 10, 2014 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140510006Floorbeam · crackedLEFT HAND FLOORBEAM FS 280 HAS A 1 INCH CRACK AT LBL 9.00. RT FLOORBEAM FS 280 HAS 1 INCH CRACK AT RBL 9.00. THE TOP FLANGES ARE CORRODED BETWEEN LT & RT OTBD FLOOR SILL & LBL 9.00 & RB L9.00 REPLACED FLOORBEAM IAW SRM 51-42-06 & REPLACED FLOORBEAM IAW SRM 5May 10, 2014 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20140504023Floorbeam · crackedLEFT FLOORBEAM FS 280 HAS A 1 INCH CRACK AT LBL 9.00 & THE TOP FLANGE IS CORRODED BETWEEN THE LT OTBD FLOOR SILL & LBL 9.00. REPLACED FLOORBEAM IAW SRM 51-42-06.May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20140504024Floor Support · corrodedFLOORBOARD SUPPORT ATTACHED TO FWD SIDE OF FLOORBEAM FS 280.00 BETWEEN LBL 9.00 & RBL 9.00 IS CORRODED. INSTALLED FLOOR SUPPORT IAW SRM 51-42-06.May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140504020Strap · crackedSTRAP ASSEMBLY FOR AFT FUSELAGE FAIRINGS 195DL & 196DR IS CRACKED IN 2 PLACES. ONE CRACK IS ON STRAP ON FWD END OF AFT ANGLE. CRACK 2 IS ON AFT ANGLE ABOUT 6 INCHES FWD OF AFT END. FABRICATED NEW STRAP ASSEMBLY IAW DWG BA670-00001.May 4, 2014 · N522AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20140504019Support · corrodedMAIN AVIONICS UNDERFLOOR RT. SUPPORT BETWEEN FS 349.00 & FS 364.00 IS CORRODED. REPLACED MAIN AVIONICS UNDERFLOOR RT. SUPPORT BETWEEN FS 349.00 & FS364.00 IAW SRM 51-40-00May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140504018Intercostal · corrodedMAIN AVIONICS UNDERFLOOR LIGHT. SUPPORT BETWEEN FS 349.00 & FS 364.00 IS CORRODED. NEW INTERCOSTAL INSTALLED IAW SRM 51-42-21 & 51-42-06.May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140504017Structure · crackedAFT INNER PAX DOOR CORNER HAS A DENT & IS CRACKED. INSTALLED NEW AFT INNER PAX DOOR CORNER IAW SRM 51-42-06 & 51-42-10.May 4, 2014 · N522AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140504013Bracket · crackedLEFT ENG LOWER TRANS COWL HAS A CRACKED BRACKET ABOVE THE OTBD SLIDER. CRACK IS 1/2 INCH LONG. R & R LT LWR TRANS COWL IAW AMM 78-33-01-400-801. IAW NRWC E388882 FOR FUNCTIONAL TEST OF THRUST REVERSER.May 4, 2014 · N522AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20140504012Support · crackedINTERNAL STRUCTURAL SUPPORT AT PAX DOOR ACCESS PANEL 832JL IS CRACKED APPROX 1/4 INCH. R & R INTERNAL STRUCTURAL SUPPORT AT PAX DOOR ACCESS PANEL 832JL IAW SRM 51-42-06.May 4, 2014 · N522AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140504011Support · crackedINTERNAL STRUCTURAL SUPPORT AT PAX DOOR ACCESS PANEL 832JR IS CRACKED APPROX 1/4 INCH. R & R INTERNAL STRUCTURAL SUPPORT AT PAX DOOR ACCESS PANEL 832JR IAW SRM 51-42-06.May 4, 2014 · N522AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140504010Plate · crackedLEFT ENG LOWER TRANS COWL LATCH NR 4 HAS A CRACKED MOUNT PLATE 1 INCH LONG. R & R LT ENG LOWER TRANS COWL. IAW NRWC E385670 FOR CORRECTIVE ACTION & FOLLOW ON STEPS.May 4, 2014 · N522AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20140504009Fairing · crackedRIGHT MLG BAY BELLY SUPPORT FAIRING IS CRACKED. R & R RT MLG BAY BELLY SUPPORT FAIRING IAW SRM 51-42-10.May 4, 2014 · N522AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20140504008Fairing · crackedLEFT MLG BAY BELLY SUPPORT FAIRING IS CRACKED. R & R LT MLG BAY BELLY SUPPORT FAIRING IAW SRM 51-42-10.May 4, 2014 · N522AE · Cndair CL6002C10 · Aerodynamic FairingsSDR SIMA20140504007Support · crackedFORWARD SKIN STRUCTURAL SUPPORT FOR PAX DOOR MID STEP HAS 2 CRACKS. 1/2 INCH LENGTH TOTAL. COMPLETED REPAIR OF THE FWD SKIN STRUCTURAL SUPPORT FOR PAX DOOR MID STEP IAW SRM 52-11-04-201-004-A001.May 4, 2014 · N522AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20140504016Cascade · crackedLEFT ENG LOWER CASCADE CRACKED. R & R LT LWR CASCADES IAW AMM 78-34-01 & ERS-CR-7800-015. IAW NRWC E388882 FOR FUNCTIONAL TEST OF THRUST REVERSER.May 4, 2014 · N522AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20140504015Bracket · crackedL BRACKET ATTACHED TO AFT SIDE OF FLOORBEAM FS 280.00 AT RBL9 .00 IS CRACKED APPROX 1/4 INCH. INSTALLED BRACKET IAW SRM 51-42-06, ERS-CR-5300-450.May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140504021Floorboard · damagedFLOORBOARD 231ALF HAS COMPOSITE DAMAGE OUT OF LIMITS. REPLACED FLOORBOARD 231ALF IAW COMCMM-030, IAW REPANEL CHECKLIST FOR INSTALLATION.May 4, 2014 · N522AE · Cndair CL6002C10 · Fuselage Floor PanelSDR SIMA20140504022Light · brokenNUMBER 4 LT & RT EMER EXIT EMER LIGHTS BROKEN. INSTALLED NEW EMER FLOOR PATH MARKINGS AT LT & RT EMER EXITS IAW AMM TASK 33-51-01-400-801, DWG E177001 & ETN-CR-33-004.May 4, 2014 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140504014Bracket · crackedLEFT ENG UPPER TRANS COWL HAS A CRACKED BRACKET AT THE INBD SLIDER. CRACK IS 1/2 INCH LONG. R & R LT ENG UPPER TRANS COWL IAW AMM 78-33-01-400-801. IAW REF NRWC E385669 FOR FOLLOW ON STEPS.May 4, 2014 · N522AE · Cndair CL6002C10 · Engine Thrust ReverserSDR SIMA20140426001Light · inoperativeSECOND TO LAST CEILING EMERGENCY FLOODLIGHT BURNED OUT. FLIGHT CREW PLACARDED IAW MEL 33-34. R & R NR 5 CEILING EMERGENCY LIGHT BULB IAW AMM 33-51-09 MEL RESTORED.Apr 26, 2014 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140420002Flashlight · inoperativeFIRST OFFICER`S SIDE COCKPIT FLASHLIGHT IS NOT CHARGING. R & R FIRST OFFICER`S FLASHLIGHT, OPERATIONS CHECKED GOOD.Apr 20, 2014 · N522AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140407003Light · inoperativeREENTER MEL 33-34 EMERGENCY CEILING LIGHT INOPERATIVE. R & R EMERGENCY CEILING LIGHT IAW MSP, OPERATIONS CHECKED GOOD MEL RESTORED.Apr 7, 2014 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140213003Crash Ax · missingCRASH AX MISSING. REPLACED MISSING AX AS REQUIRED.Feb 13, 2014 · N522AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20131229002Seal · dirtyEMERGENCY EXIT IN FLIGHT DECK IS LEAKING ANTI-ICE FLUID. OPENED FLIGHT DECK EMERGENCY DOOR. CLEANED DOOR SEAL AREA, NO DEFECTS NOTED. SECURED DOOR IAW AMM 52-22-00.Dec 29, 2013 · N522AE · Cndair CL6002C10 · Emergency ExitsSDR SIMA20131216001Light · looseFLOOR LIGHTING STRIP ON FIRST OFFICER SIDE BY WING EXIT IS LOOSE. SECURED EMERGENCY FLOOR PATH MARKING IAW CRJ-700 AMM 33-51-01.Dec 16, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130826007Lens · unsecureEMERGENCY LIGHTS LENS ON LT WING PULLED OUT. REPAIRED IAW EO CR-3300-009, PART B.Aug 26, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130821002Battery Pack · inoperativeFOUND EMERGENCY LIGHTS IN ZONE NR 2 INOPERATIVE DURING PS-2 CHECK. R & R BATTERY AND CHARGER IAW AMM 33-51-17. OPS CHECKED GOOD.Aug 21, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130817005Light · obstructedTHE CREW REPORTED LT OVERWING EMERGENCY LIGHT WAS TAPED OVER. PERFORMED PERMANENT REPAIR OF LEFT HAND OVERWING EMERGENCY LIGHT IAW PART C OF EO CR-3300-009. OPS CHECKED GOOD. ACFT RETURNED TO SERVICEAug 17, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130731003Battery Pack · inoperativeCABIN EMERGENCY LIGHTS INOPERATIVE. R & R NR 3 EMERGENCY BATTERY IAW AMM 33-50-00. OPS CHECKED GOOD.Jul 31, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130727010Battery Pack · inoperativeOVERHEAD CABIN EMERGENCY EXIT SIGN AND REAR BULKHEAD EMERGENCY EXIT SIGNS NOT ILLUMINATING WHEN EMERGENCY LIGHTS SELECTED ON. R & R BATTERY PACK 2 EMERGENCY LIGHTING SYS.Jul 27, 2013 · N522AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130727004Battery Pack · inoperativeOVERHEAD EMERGENCY LIGHTS IN CABIN NR 2 AND NR 3 NOT ILLUMINATING. R & R BATTERY NR 2 IAW AMM 33-51-17, OPS CHECKED GOOD.Jul 27, 2013 · N522AE · Cndair CL6002C10 · Emergency Lighting
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