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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR VNAA20170518HMV03Floor Support · corrodedRIGHT FLOOR SUPPORT IS CORRODED BETWEEN BS 349 AND 379. REPAIRED THE FLOOR SUPPORT.SDR VNAA20170518HMV02Stringer · corrodedFUSELAGE STRINGER 26R IS CORRODED BETWEEN BS 319 AND 349. REPLACED THE STRINGER.SDR VNAA20170518HMV01Stringer · corrodedFUSELAGE STRINGER 25R IS CORRODED BETWEEN BS 319 AND 349. REPLACED THE STRINGER.SDR VNAA20170517HMV09Skin · corrodedFUSELAGE SKIN SPLICE AT BS 333 IS CORODED BETWEEN STRINGERS 25L AND 25R.SDR VNAA20170517HMV08Intercostal · corrodedAVIONICS BAY DOOR INNERCOSTAL BETWEEN STGR 27 AND STGR 26R BETWEEN FS 364 AND FS 349 IS CORRODED.SDR VNAA20170517HMV07Intercostal · corrodedAVI BAY DOOR INTERCOSTAL BETWEEN STRINGERS 26 AND 27L, BS 349 AND FS 364 IS CORRODED.SDR VNAA20170517HMV06Bulkhead Web · corrodedFS 280 BULKHEAD RT LOWER WEB IS CORRODED BETWEEN RBL 12 AND 42. REPLACED THE BULKHEAD WEB.SDR VNAA20170517HMV05Bulkhead Web · corrodedBS 280 BULKHEAD LT LOWER WEB IS CORRODED AT LBL 12. INSTALLED A NEW LT LOWER WEB.SDR 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-53-041SDR VNAA20170517HMV03Frame · corrodedFRAME BS 517 BETWEEN STRINGER 18 AND 19L CORRODED. REMOVOVED AND REPLACED THE FRAME SEGMENT.SDR VNAA20170517HMV02Angle · corrodedSERVICE DOOR LOWER SILL ANGLE IS CORRODED BETWEEN BS 319 AND 349. REMOVED AND REPLACED THE ANGLE.SDR VNAA20170517HMV01Angle · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED BETWEEN BS 310 AND 349.SDR 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 RELEASEDSDR 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 RESDR 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.SDR 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.SDR SIMA20150608005Stringer · corrodedSTRINGER 26L BETWEEN FS 319.70 & 330.00 IS CORRODED. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-06.SDR 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.SDR 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.SDR 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.SDR SIMA20150606003Diaphragm · crackedLEFT MLG WW DIAPHRAGM HAS A 1 1/2" CRACK. R & R LT MLG WW DIAPHRAGM IAW AMM 20-21-00.SDR SIMA20150606002Diaphragm · crackedRIGHT MLG WW DIAPHRAGM HAS A 1" CRACK. R & R RT MLG WW DIAPHRAGM IAW AMM 20-21-00.SDR 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.SDR 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.SDR 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.SDR 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 TURBUSDR SIMA20141129001Light · inoperativeTHE FLIGHT ATTENDANT ADVISED US THAT SEVERAL EMER EXIT SIGNS ARE NOT ILLUMINATING, HAVE BURNED OUT BULBS. RELAMPED IAW 33-10-02.SDR 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.SDR 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.SDR 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.SDR SIMA20140502003Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. R & R ESPU BATTERY PACK 1 IAW AMM 33-51-17, OPERATIONS CHECKED OK.SDR SIMA20140129007Cradle · brokenCAPTAIN`S EMERGENCY FLASHLIGHT CRADLE BROKEN. R & R CAPTAIN`S EMERGENCY FLASHLIGHT & CRADLE IAW AMM 25-61-02, OPERATIONS CHECKED GOOD.SDR 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.SDR 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.SDR SIMA20140107003Door · lack of lubeMAIN PAX DOOR HARD TO CLOSE. LUBE PAX, CREW DOOR IAW STD MTX PRACTICE PS GOOD.SDR 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 CHECSDR 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.SDR 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.SDR 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.SDR SIMA20131009001Sign · dislodgedGALLEY EMERGENCY SIGN FELL OFF MOUNT. ATTACHED SIGN TO MOUNT IAW AMM 33-57-05.SDR 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.SDR SIMA20130913007Cradle · brokenCAPTAIN FLASHLIGHT HOLDER BROKEN. R & R FLASHLIGHT HOLDER IAW AMM 25-61-02. OPC GOOD. NO FURTHER DEFECTS NOTED.SDR 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 25SDR 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 OPERATSDR 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 70SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.
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