N511AE

Service difficulty reports · 137

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 = 'N511AE' 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 VNAA20170518HMV03Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN BS 349 AND 379. REPAIRED THE FLOOR SUPPORT.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20170518HMV02Stringer · corrodedFUSELAGE STRINGER 26R IS CORRODED BETWEEN BS 319 AND 349. REPLACED THE STRINGER.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20170518HMV01Stringer · corrodedFUSELAGE STRINGER 25R IS CORRODED BETWEEN BS 319 AND 349. REPLACED THE STRINGER.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR VNAA20170517HMV09Skin · corrodedFUSELAGE SKIN SPLICE AT BS 333 IS CORODED BETWEEN STRINGERS 25L AND 25R.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR VNAA20170517HMV08Intercostal · corrodedAVIONICS BAY DOOR INNERCOSTAL BETWEEN STGR 27 AND STGR 26R BETWEEN FS 364 AND FS 349 IS CORRODED.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20170517HMV07Intercostal · corrodedAVI BAY DOOR INTERCOSTAL BETWEEN STRINGERS 26 AND 27L, BS 349 AND FS 364 IS CORRODED.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20170517HMV06Bulkhead Web · corrodedFS 280 BULKHEAD RT LOWER WEB IS CORRODED BETWEEN RBL 12 AND 42. REPLACED THE BULKHEAD WEB.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA20170517HMV05Bulkhead Web · corrodedBS 280 BULKHEAD LT LOWER WEB IS CORRODED AT LBL 12. INSTALLED A NEW LT LOWER WEB.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR VNAA20170517HMV04Floorbeam · damagedFS 280 FLOORBEAM IS CORRODED IN MULTIPLE AREAS AND IS CRACKED AT LBL 12 & RBL 12. THE FLOORBEAM WAS REMOVED & REPLACED IAW SERVICE BULLETIN 670BA-53-041May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR VNAA20170517HMV03Frame · corrodedFRAME BS 517 BETWEEN STRINGER 18 AND 19L CORRODED. REMOVOVED AND REPLACED THE FRAME SEGMENT.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20170517HMV02Angle · corrodedSERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN BS 319 AND 349. REMOVED AND REPLACED THE ANGLE.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA20170517HMV01Angle · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED BETWEEN BS 310 AND 349.May 16, 2017 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR VNAA2016010300003Fuel Cap · detachedCREW REPORTED RT FUEL CAP DOOR OPENED IN FLIGHT AND FUEL CAP CAME OFF AFTER BANGING UP UNDERNEATH WING WHILE ATTACHED TO CHAIN. FUEL CAP SEPARATED FROM ACFT IN FLIGHT. MAINTENANCE INSPECTED, REPLACED FUEL/DEFUEL CAP AND PERFORMED CHECKS IAW AMM. ACFT RELEASEDJan 3, 2016 · N511AE · Cndair CL6002C10 · Aircraft Fuel Distribution SystemSDR SIMA20150618001Stringer · dentedTRANSFERRED FROM AML PAGE 3644799 NR 3, ORIGINAL LOG PAGE 3491096 NR 1. PERFORM PERMANENT REPAIR AT OR BEFORE 6000 FH ON LT PACK WATER TUBE BRACKET STRINGER 6L IAW ERS-CR-53MR-663. COMPLETED REPAIR OF STRINGER 6L BETWEEN FS 1144.00 & 1162.00 BY INSTALLING REJun 18, 2015 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150608007Floorbeam · corrodedFLOORBEAM FS 280.00 IS CORRODED BETWEEN LBL 18.00 & RBL 9.00. R & R THE FLOORBEAM FS 280.00 BETWEEN LBL 18.00 & RBL 9.00 SRM 51-42-13 IAW SRM 51-42-06 & IAW SRM 51-42-20.Jun 8, 2015 · N511AE · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SIMA20150608006Stringer · corrodedSTRINGER 25R BETWEEN FS 319.70 & 330.00 IS CORRODED. REPAIRED CORROSION ON STRINGER 25R BETWEEN FS 319.70-330.00 AS REQUIRED IAW ERS-CR-5300-1408.Jun 8, 2015 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150608005Stringer · corrodedSTRINGER 26L BETWEEN FS 319.70 & 330.00 IS CORRODED. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-06.Jun 8, 2015 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20150606006Bracket · crackedT BRACKET AT FWD SIDE OF FLOORBEAM 280 & RBL 9.00 IS CRACKED APPROX .75 INCHES. REPLACED RT T BRACKET IAW SRM 53-11-41.Jun 6, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150606004Bracket · crackedT BRACKET AT FWD SIDE OF FLOORBEAM 280 & LBL 9.00 IS CRACKED APPROX 75 INCHES. REPLACED LT T BRACKET IAW SRM 53-11-41.Jun 6, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150606005Tray · crackedFORWARD EQUIP BAY TRAY FOR JB6 HAS 1/4" CRACK BY THE FWD RT CORNER. REMOVED CRACKED TRAY & INSTALLED NEW TRAY IAW SRM 51-42-06.Jun 6, 2015 · N511AE · Cndair CL6002C10 · Electronic Shelf SectionSDR SIMA20150606003Diaphragm · crackedLEFT MLG WW DIAPHRAGM HAS A 1 1/2" CRACK. R & R LT MLG WW DIAPHRAGM IAW AMM 20-21-00.Jun 6, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150606002Diaphragm · crackedRIGHT MLG WW DIAPHRAGM HAS A 1" CRACK. R & R RT MLG WW DIAPHRAGM IAW AMM 20-21-00.Jun 6, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150605006Structure · crackedFORWARD EQUIP BAY FLOOR HAS A CRACK 1/8" LONG BY THE AFT CUT OUT FOR 211 AL. REPAIRED FWD EQUIP BAY FLOOR CRACK IAW ETN CR-53-099.Jun 5, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150605004Drag Angle · crackedPASSENGER DOOR STEP AFT SKIN ATTACH ANGLE IS CRACKED BY THE PULLEY BRACKET. INSTALLED NEW DRAG ANGLE, ATTACH ANGLE, IAW SRM 52-11-04 & ETN-CR-52--037R1.Jun 5, 2015 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20150605005Structure · crackedFORWARD EQUIP BAY FLOOR HAS A 1/4" CRACK BY THE AFT CORNER CUT OUT FOR 212 AR. REPAIRED FWD EQUIP BAY FLOOR CRACK IAW ETN CR-53-099.Jun 5, 2015 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20150102001Adc · failedMULTIFUNCTION DISPLAY FIRST OFFICER`S SIDE FAILED IN FLIGHT. PERFORMED OPERATIONAL TEST OF THE FIRST OFFICER`S MFD IAW AMM 31-61-01. OPERATIONS CHECKED GOOD. 15 SECOND LOSS OF BOTH ADC'S & BOTH AHRS DURING CLIMB OUT WHILE ENCOUNTERING INTERMITTENT MOD TURBUJan 2, 2015 · N511AE · Cndair CL6002C10 · Air Data ComputerSDR SIMA20141129001Light · inoperativeTHE FLIGHT ATTENDANT ADVISED US THAT SEVERAL EMER EXIT SIGNS ARE NOT ILLUMINATING, HAVE BURNED OUT BULBS. RELAMPED IAW 33-10-02.Nov 29, 2014 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140919004Structure · crackedWHILE PERFORMING SERVICE BULLETIN 670BA-63-040 REV C FOUND PAX DOOR LINTEL AT STRINGER 3L CRACKED. REPAIRED DAMAGE IAW SERVICE BULLETIN 670BA-63-040 REV C. EO CL600-2C10-53-L02638, REPORT NCR-CR-53-036 & EO 670-53-21-493.Sep 19, 2014 · N511AE · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SIMA20140620004Fmu · failedFUEL BURN MUCH HIGHER THAN PLANNED LT NR 1 ENG BURNED 300 LBS HIGHER THAN NR 2 ENG. R & R NR 1 FMU IAW AMM 73-21-00. LEAK CHECKED IAW AMM 73-10-00, NO LEAK FOUND.Jun 20, 2014 · N511AE · Cndair CL6002C10 · Fuel Control/Turbine EnginesSDR SIMA20140610007Battery · dischargedCREW REPORTS EMER LIGHT BY EMER DOOR OVER THE WING INOPERATIVE. R & R BATTERY HOLDER & BATTERY NR 3 IAW OPERATIONS CHECK GOOD. BATTERY CHARGER ASSEMBLY PN 11-0049 SN 13662.Jun 10, 2014 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140502003Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. R & R ESPU BATTERY PACK 1 IAW AMM 33-51-17, OPERATIONS CHECKED OK.May 2, 2014 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20140129007Cradle · brokenCAPTAIN`S EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R CAPTAIN`S EMERGENCY FLASHLIGHT & CRADLE IAW AMM 25-61-02, OPERATIONS CHECKED GOOD.Jan 29, 2014 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140129006Cradle · brokenFORWARD FLIGHT ATTENDANT EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R FWD FLIGHT ATTENDANT`S EMERGENCY FLASHLIGHT & CRADDLE IAW AMM 25-81-02, OPERATIONS CHECKED GOOD.Jan 29, 2014 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140110008Flashlight · defectiveFLIGHT ATTENDANT`S FLASHLIGHT WILL NOT STAY SECURE IN THE BRACKET BEHIND 18AB. R & R FLASHLIGHT & CRADLE ASSEMBLY IAW AMM 25-61-02. NO FURTHER DEFECTS NOTED.Jan 10, 2014 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20140107003Door · lack of lubeMAIN PAX DOOR HARD TO CLOSE. LUBE PAX, CREW DOOR IAW STD MTX PRACTICE PS GOOD.Jan 7, 2014 · N511AE · Cndair CL6002C10 · Passenger/Crew DoorsSDR SIMA20131215008Light · defectiveON FLIGHT 3311 FLIGHT ATTENDANT REPORTED SMOKE & BURNING ODOR, COMING FROM 2A, READING LAMP IS MISSING LENS COVER. SHUT OFF LAMP, SMOKE & ODOR WENT AWAY. THE ACFT WAS REMOVED FROM SERVICE. RELAMPED BOTH PAX READING LIGHTS AT SEAT 2A IAW SMP. OPERATIONS CHECDec 15, 2013 · N511AE · Cndair CL6002C10 · Passenger Compartment LightingSDR SIMA20131120002Holder · inoperativeFLIGHT ATTENDANT`S FLASHLIGHT HOLDER INOPERATIVE. DEFERRED AFT FLASHLIGHT HOLDER, IAW MEL25-15. R & R AFT FLASHLIGHT & HOLDER IAW CRJ 700 AMM 25-61-02, OPERATIONS CHECKED GOOD.Nov 20, 2013 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20131017001Transducer · inoperativeOTBD FLT SPOILERS CAUTION MESSAGE, DURING TROUBLESHOOTING, FOUND SYS 1 TRANSDUCER INOPERATIVE. R & R PRESSURE TRANSDUCER NR 1 IAW AMM 29-31-01. OPS CHECKED GOOD.Oct 17, 2013 · N511AE · Cndair CL6002C10 · Drag Control SystemSDR SIMA20131017009Hydraulic System · contaminatedOTBD FLT SPOILERS CAUTION MESSAGE. BLED HYD SYS 1 IAW AMM 29-10-00. REMOVED AIR FROM SYSTEM. SERVICED NR 1 HYD SYS IAW AMM 12-12-29. PERFORMED POST 2 TEST IAW AMM 27-61-05. OPS NORMAL.Oct 17, 2013 · N511AE · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20131009001Sign · dislodgedGALLEY EMERGENCY SIGN FELL OFF MOUNT. ATTACHED SIGN TO MOUNT IAW AMM 33-57-05.Oct 9, 2013 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130928004Hose · leakingTHE CREW REPORTED DURING DESCENT A HYD 2 LOW PRESSURE CAUTION MESSAGE. COMPLIED WITH AOM VOL 1 PROCEDURES AND DECLARED AN EMERGENCY. LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R RT HYD DAMPENER HOSE IAW AMM 29-11-59. LEAK AND OPS CHECKED GOOD.Sep 28, 2013 · N511AE · Cndair CL6002C10 · Hydraulic System, MainSDR SIMA20130913007Cradle · brokenCAPTAIN FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 25-61-02. OPC GOOD. NO FURTHER DEFECTS NOTED.Sep 13, 2013 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20130424001Flashlight · missingDURING MAINTENANCE INSPECTION FOUND THE FIRST OFFICER’S EMERGENCY FLASHLIGHT MISSING FROM ITS HOLDER. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE FIRST OFFICER’S EMERGENCY FLASHLIGHT SYSTEM IAW AMM 25-61-02. THE OPERATIONAL CHECK WAS GOOD IAW AMM 25Apr 24, 2013 · N511AE · Cndair CL6002C10 · Emergency EquipmentSDR SIMA20130303007Battery · dischargedDURING B INSPECTION FOUND THE FORWARD AVIONICS BAY EMERGENCY BATTERY POWER SUPPLY UNIT FAILED THE OPERATIONAL CHECK. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY BATTERY AND BATTERY CHARGER SUPPLY UNIT IAW WC 33-002. THE OPERATMar 3, 2013 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130227003Light · inoperativeDURING MAINTENANCE INSEPCTION FOUND THE EMERGENCY EXIT LIGHT AT MAIN CABIN DOOR LOWER LEFT SIDE WOULD NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LOWER LEFT PASSENGER DOOR EMERGENCY EXIT LIGHT BULBS AND BATTERY, IAW CRJ 70Feb 27, 2013 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130208003Unknown · unknownDURING B INSPECTION FOUND THE RIGHT EMERGENCY EXIT UPPER ILLUMINATED "EXIT" SIGN INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. AN OPERATIONAL CHECK WAS PERFORMED IAW AMM 33-50-00 AND NO DISCREPANCIES WERE NOTED. THE AIRCRAFT WAS RETURNED TO SERVICE.Feb 8, 2013 · N511AE · Cndair CL6002C10 · Emergency LightingSDR SIMA20130113005Stringer · corrodedDURING 3C CHECK FOUND STRINGER 25 LEFT BETWEEN FS 333-00-FS 349.00 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO CR-53MR-315 FOR REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2013 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SIMA20130113009Frame · corrodedDURING 3C CHECK FOUND FRAME AT FS 333.00 CORRODED BETWEEN STRINGERS 26 LEFT AND 26 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO-CR-53MR-313 FOR REPAIR. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2013 · N511AE · Cndair CL6002C10 · Fuselage Main, FrameSDR SIMA20130113010Bulkhead · corrodedDURING 3C CHECK INSPECTION FOUND LEFT AFT FACE OF BULKHEAD ASSY AT FS 280.00 CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED BULKHEAD IAW EO CR-53MR-174. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2013 · N511AE · Cndair CL6002C10 · Fuselage Main, BulkheadSDR SIMA20130113008Stringer · corrodedDURING 3C CHECK FOUND STRINGER 26 RIGHT CORRODED BETWEEN FS 333.00 AND FS 349.00. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED STRINGER IAW CRJ700 STRUCTURAL REPAIR MANUAL 51-42-06. THE AIRCRAFT WAS RETURNED TO SERVICE.Jan 13, 2013 · N511AE · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
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