N836AE

Service difficulty reports · 82

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 = 'N836AE' 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 SIMA20120926001Holder · brokenON FLIGHT 4425 THE CREW REPORTED THE AFT FLIGHT ATTENDANT FLASHLIGHT HOLDER WAS BROKEN. FLIGHT CREW PLACARD PER MEL 25-53. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT IAW AMM 33-50-16. MEL ITEM RESTORED. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS Sep 26, 2012 · N836AE · Emb EMB135KL · Emergency EquipmentSDR SIMA20120614003Unknown · smokeFLIGHT 4118, NR 1 ENGINE SMOKING 10 MINUTES AFTER SHUTDOWN. AIRCRAFT REMOVED FROM SERVICE. INSPECTED INTAKE AND EXHAUST OF ENGINE FOR OIL LEAK, GROUND RAN ENGINE IAW MM 72-00-00. COULD NOT DUPLICATE. THE AIRCRAFT WAS RETURNED TO SERVICE.Jun 14, 2012 · N836AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA20120509007Floor Support · corrodedDURING "C" CHECK FOUND THE LEFT OMEGA BEAM CORRODED UNDER CARBON CROSSSBEAM AT FR 38. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR TO LEFT HAND OEMGA BEAM AT FRAME 38 IAW SRM 53-00-10 STEP 3 FIG 202 SHEET 2. THE AIRCRAFT WAS RETURNED TO SERVICE.May 9, 2012 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA20120502008Frame · crackedDURING MBV INSPECTION FOUND FRAME 23 IN CRACKED AT STRINGR 15 RIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIR OF FRAME 23 IAW EM-53MR-1808. THE AIRCRAFT WAS RETURNED TO SERVICE.May 8, 2012 · N836AE · Emb EMB135KL · Fuselage Main, FrameSDR SIMA20120502012Light · unknownDURING B INSPECTION, FOUND THE COCKPIT OVERHEAD EMERGENCY LIGHT PANEL 225 INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. COULD NOT DUPLICATE. COCKPIT OVERHEAD EMERGENCY LIGHT PANEL 225 CHECKED GOOD. NO DEFECTS NOTED IAW TASK 33-50-00-700-801-A. NO PARTS REMOMay 2, 2012 · N836AE · Emb EMB135KL · Emergency LightingSDR SIMA20120502011Light · inoperativeDURING B INSPECTION, FOUND THE FLOOR EMERGENCY LIGHT STRIP AT OVERWING EMERGENCY EXIT AREA INOPERATIVE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED FLOOR EMERGECNY LIGHT IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.May 2, 2012 · N836AE · Emb EMB135KL · Emergency LightingSDR SIMA20120502010Wire · brokenDURING MAINTENANCE INSPECTION, FOUND THE SECOND EMERGENCY LIGHT STRIP FROM BACK HAS BROKEN WIRE. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED THE SECOND EMERGENCY LIGHT STRIP IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.May 2, 2012 · N836AE · Emb EMB135KL · Light System WiringSDR SIMA20120502009Light · damagedDURING MAINTENANCE INSPECTION, FOUND THE FLOOR PROXIMITY EMERGENCY LIGHT PLASTIC EXTRUSIONS ARE DAMAGED. AIRCRAFT REMOVED FROM SERVICE. PROCURED EXTRUSIONS AND ASSEMBLED WITH LIGHT STRIPS IAW AMM 33-50-12. OPS CHECKED GOOD. AIRCRAFT RETURNED TO SERVICE.May 2, 2012 · N836AE · Emb EMB135KL · Emergency LightingSDR SIMA201208101Adc · malfunctionedON FLIGHT 2702 THE AIRCRAFT WAS GOING FROM GDL TO DFW BUT DUE TO WEATHER DIVERTED TO SAT. THEN TOOK OFF FROM SAT TOWARDS DFW AND EN ROUTE GOT AIRSPEED INDICATIONS ROLLING BACK WITH SPS ADVANCED MESSAGE. THE CAPTAIN RETURNED TO SAT AND DID DECLARE EMERGENCY. Mar 19, 2012 · N836AE · Emb EMB135KL · Air Data ComputerSDR SIMA2011332003Handle · misinstalledON FLIGHT 3341 THE CREW REPORTED THE FLIGHT ATTENDANT COULD NOT OPEN THE CABIN DOOR (HANDLE BINDING). THE AIRCRAFT WAS REMOVED FROM SERVICE. FOUND MAIN DOOR HANDLE NOT INSTALLED PROPERLY. INSTALLED MAIN DOOR HANDLE IAW EMB 140 AMM 52-18-05. PERFORMED FUNCTNov 23, 2011 · N836AE · Emb EMB135KL · Passenger/Crew DoorsSDR SIMA201132907Handle · misinstalledF/A COULD NOT OPEN CABIN DOOR - HANDLE BINDING, 3RD WRITE UP IN 4 DAYS. FOUND MAIN DOOR HANDLE NOT INSTALLED PROPERLY. INSTALLED MAIN DOOR HANDLE IAW EMB 140 AMM 52-18-05. PERFORMED OPS CHECK OF DOOR IAW EMB 140 AMM 52-18-00. NO OTHER DEFECTS NOTED.Nov 23, 2011 · N836AE · Emb EMB135KL · Passenger/Crew DoorsSDR SIMA2011321004Unknown · smokeFOR FLIGHT 2926 DURING THE PREFLIGHT INSPECTION THE FIRST OFFICERS FOUND A TRAIL OF WHITE SMOKE COMING FROM THE EXHAUST WITH A RUBBERY SMELL TO IT. THE AIRCRAFT WAS REMOVED FROM SERVICE. INSPECTED LEFT ENGINE FOR POSSIBLE SMOKE IN EXHAUST, RAN LEFT ENGINE IANov 16, 2011 · N836AE · Emb EMB135KL · Engine (Turbine/Turboprop)SDR SIMA201122902Inverter · inoperativeEMERGENCY EXIT SIGN AT EMERGENCY HATCH INOP (UPPER) LEFT SIDE OVERWING. REMOVED AND INSTALLED NR 4 INVERTER IAW EMB MM 33-50-11, OPT CHECK GOOD IAW 33-50-00.Aug 16, 2011 · N836AE · Emb EMB135KL · Emergency LightingSDR SIMA201113304Unknown · odorON FLIGHT 9802 THE CREW REPORTED A SMOKE SMELL WITH NO VISUAL SMOKE INDICATION. THE AIRCRAFT WAS REMOVED FROM SERVICE. MAINTENANCE REPORTED AN AIR TURNBACK DUE TO A POSSIBLE LIGHTNING STRIKE. THE AIRCRAFT RETURNED TO ABI. PERFORMED ENGINE RUNS IAW RR MM 72May 11, 2011 · N836AE · Emb EMB135KL · Air Distribution SystemSDR SIMA201113003Engine · bird ingestionON FLIGHT 2754 AFTER TAKEOFF THE CREW REPORTED SMOKE AND SMOKE ODOR IN CABIN. THE CAPTAIN DECLARED AN EMERGENCY AND RETURNED TO LFT. THE AIRCRAFT HAD AN OVERWEIGHT LANDING AT 42000 POUNDS 500 FPM SINK RATE. THE AIRCRAFT LANDED WITHOUT INCIDENT AND WAS REMOVMay 8, 2011 · N836AE · Emb EMB135KL · Air Distribution SystemSDR SIMA201101801Windshield Wiper · stuckON FLIGHT 4264 THE CREW ELECTED TO ABORT THE LOW SPEED TAKEOFF DUE TO DEICE FLUID ON THE WINDSHIELD AND UNABLE TO USE THE WIPER TO CLEAR. THE AIRCRAFT WAS REMOVED FROM SERVICE. UNSTUCK WIPER BLADE AND PERFORMED OPERATIONAL TEST OF WINDSHIELD WIPER SYSTEM IAWJan 17, 2011 · N836AE · Emb EMB135KL · Windshield/Door Rain/Ice RemovalSDR SIMA201102001Flashlight · looseON FLIGHT 3940 THE CREW REPORTED THE FLIGHT ATTENDANT REAR CABIN FLASHLIGHT ASSEMBLY WAS LOOSE, CAUSING INTERMITTENT CHARGING OF THE FLASH LIGHT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT FLIGHT ATTENDANT FLASHLIGHT ASSEMBLY. THE OJan 16, 2011 · N836AE · Emb EMB135KL · Emergency EquipmentSDR SIMA201033305Skin · damagedDURING MAINTENANCE BASE VISIT FOUND THE AIRCRAFT WAS STRUCK BY A BAGGAGE CART FORWARD OF RIGHT WING ON FUSELAGE. THE RIGHT CENTER FUSELAGE NR 2 HAS SKIN DENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. FERRIED FROM ORD TO SAW FOR REPAIR. REPAIRED DAMAGE IN ACCNov 24, 2010 · N836AE · Emb EMB135KL · Fuselage Main, Plate/SkinSDR SIMA201028801Power Supply · inoperativeDURING MAINTENANCE BASE INSPECTION FOR FLIGHT 2712 THE NR 2 EMERGENCY FLOOR LIGHTS FAILED TO LIGHT AFTER BATTERY REPLACEMENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY POWER SUPPLY. THE AIRCRAFT WAS RETURNED TO SERVICE.Oct 14, 2010 · N836AE · Emb EMB135KL · Emergency LightingSDR SIMA201017209Skin · damagedDURING MAINTENANCE BASE VISIT FOUND THE AIRCRAFT HAD SUSTAINED DAMAGE ON CENTER THE FUSELAGE I LOWER SKIN BETWEEN FRAME 21 AND FRAME 22 AT STRINGER 20 LEFT. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLETED REPAIR OF DAMAGE IAW EO EM-53MR-1513. THE AIRCRAFT Jun 20, 2010 · N836AE · Emb EMB135KL · Fuselage Main, Plate/SkinSDR SIMA200934102Battery · inoperativeDURING MAINTENANCE BASE INSPECTION FOUND THAT THE AFT CABIN FLASHLIGHT FAILED TO ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CABIN FLASHLIGHT BATTERY. THE AIRCRAFT WAS RETURNED TO SERVICE.Dec 5, 2009 · N836AE · Emb EMB135KL · Emergency EquipmentSDR SIMA200816504Floorbeam · corrodedDURING A MBV INSP, THE GALLEY FLOOR CENTER BEAM AT FR 20 WAS FOUND CORRODED WITH LEVEL TWO CORROSION. PERFORMED CUT OUT OF THE CENTER BEAM TO REMOVE THE DAMAGE. FAB A DOUBLER, DRILLED, APPLIED PREVENTIVE AND INSTALLED. WORK DONE IAW EMB 145 SRM (SRM EMB-145Jun 9, 2008 · N836AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200733206Anti-Ice Valve · faultyON T/O ROLL GOT E2 A/ICE FAIL MESSAGE. ABORTED TAKEOFF SPEED BELOW 100KTS APU WAS OFF T/O THRUST WAS 84. 2N1 MESSAGE DISAPPEARED AFTERWARDS TO IDLE. REMOVED AND REPLACED ANTI-ICE VALVE IAW MM 30-21-01 AND REMOVED AND REPLACED DELIVERY TUBE IAW AMM 36-11-00. Nov 25, 2007 · N836AE · Emb EMB135KL · Air Intake Anti/De-Ice SystemSDR SIMA200712001Unknown · odorSTRONG OIL ODOR IN COCKPIT DURING FLIGHT. [SUP 05-08-07] REMOVED AND REPLACED LEFT HAND ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL AND LEAK CHECKS COMPLIED WITH NO LEAKS - RETURNED AIRCRAFT TO SERVICE.Apr 23, 2007 · N836AE · Emb EMB135KL · Air Distribution SystemSDR SIMA200620821Floor Support · corrodedABI - DURING IMBV INSPECTION, RIGHT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. CUT OUT OF RIGHT OMEGA BEAM TO REMOVE CORROSION. FABRICATED A FILLER, REPAIR DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 33, CHAPTERS 53-00-10 FIG 20Jul 21, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620817Floor Support · corrodedDURING IMBV INSPECTION CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. REMOVED CORROSION BY CUTTING OUT SECTION OF THE CENTER OMEGA BEAM FOUND CORRODED. FABRICATED FILLER, DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 33, CHAPTEJul 21, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620822Floor Support · corrodedABI - DURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO HAVE ONE SPOT OF CORROSION 6 INCHES AFT OF FRAME 25. DRILLED A HOLE TO REMOVE THE CORROSION AND INSTALLED A RIVET. RESTORED THE SURFACE FINISH AND APPLIED CORROSION PREVENTATIVE. REPAIR DONE IAW EMBJul 18, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620819Floor Support · corrodedABI - DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 27. REMOVED CORROSION BY MAKING A CUTOUT, PREPARED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 53-00-10 FIG 202. RETURNED AIRCRAFT TO SERVICE. Jul 18, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620816Sill · corrodedDURING IMBV INSPECTION, FOUND CARGO DOOR CUT OUT LOWER SILL CORRODED. REMOVED THE CORRODED LOWER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-40-02 AND EMB CPM, CPM 145/1132 REV 13, CHAPTER 51-21-06. AIRCRAFT RETURNED TO Jul 18, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620823Floor Support · corrodedDURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT, PREPARED A FILLER, DOUBLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTER 53-00-10 FIG 202. RETURNED AIRCRAFT TO Jul 17, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620820Floor Support · corrodedDURING IMBV INSPECTION, LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED CORROSION BY MAKING A CUTOUT. PREPARED A FILLER, DOUBLER, PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM145/1142 REV 33. RETURNED AIRCRAFT TO SERVICE. (M)Jul 17, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200620818Sill · corrodedDURING IMBV INSPECTION, SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 33, CHAPTERS 51-140-02, 03, 51-40-06 AND EMB CPM, CPM 145/1132 REV 13, CHAPTER 51-21-04. Jul 14, 2006 · N836AE · Emb EMB135KL · Fuselage Miscellaneous Structure
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