N633AE
Service difficulty reports · 172
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 = 'N633AE' 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 = 'N633AE' 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 SIMA20130403008Battery · dischargedDURING B INSPECTION FOUND THE EMERGENCY LIGHTS AT COCKPIT CEILING, FORWARD CEILING IN CABIN AND EXIT FORWARD LEFT WING LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY AND CHARGER ASSEMBLY IAW AESDR SIMA20130219001Battery · dischargedDURING MAINTENANCE INSPECTION FOUND MULTIPLE EMERGENCY LIGHTS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT CHARGER AND BATTERY. THE OPERATIONAL CHECK WAS GOOD IAW WORK CARDS 33-700-17 AND 33-700-19. THE ASDR SIMA20130206009Battery · dischargedDURING MAINTENANCE INSPECTION FOUND THE LEFT FWD FAIRING, AISLE NR 1, AND COCKPIT EMERGENCY LIGHTS WILL NOT ILLUMINATE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT FWD EXTERNAL BULB IAW EMB 145 AMM33-50-10. PART # 1317. REMOVED ANDSDR SIMA20130131007Fuse · blownDURING B INSPECTION FOUND THE LEFT FORWARD WING EMERGENCY LIGHT IS INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE FUSE AT NR 1 BATTERY CHARGER IAW. CMM 25-60-03. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVSDR SIMA20130117005Connector · defectiveDURING B INSPECTION FOUND THE SERVICE DOOR EXTERNAL EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED & REPLACED THE WIRE CONNECTOR FOR SERVICE DOOR LIGHT IAW EMB 145 STANDARD WIRING PRACTICES MANUAL 20-21-00. THE OPERATIONAL CHECKSDR SIMA20121227001Control Unit · malfunctionedBRAKES DEGRADED MESSAGE ON EICAS, O/B BRAKE NR 1 AT BOTTOM OF GREEN, I/B BRAKE NR 2 TOP OF GREEN, BRAKES ON THE OTHER SIDE BOTH MID RANGE. MESSAGE CAME ON WHEN WE EXTENDED THE GEAR AND WENT AWAY WHEN WE RETRACTED, CAME BACK WHEN WE EXTENDED THE GEAR A 2ND TIMSDR SIMA20121215003Holder · brokenON FLIGHT 4314 THE CREW REPORTED THEY FOUND THE FORWARD FLIGHT ATTENDANT FLASHLIGHT HOLDER BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED FLASHLIGHT ASSEMBLY IAW EMB. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICESDR SIMA20121118005Battery · dischargedDURING B INSPECTION FOUND THE COCKPIT EMERGENCY FLOOD LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHTING BATTERY AND CHARGER ASSEMBLY IAW AE WC 33-700. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS SDR SIMA20121015001Flashlight · inoperativeON FLIGHT 2877 THE CREW REPORTED THE CAPTAIN’S FLASHLIGHT WOULD NOT HOLD A CHARGE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE CAPTAIN’S FLASHLIGHT IAW AMM 33-50-16. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120714001Proximity Sensor · failedON FLIGHT 3261, THE CREW REPORTED EN ROUTE AT FL370 CAPTAIN AND THE FIRST OFFICER HEARD AND FELT A LOUD `POP` FROM FORWARD AND UNDERNEATH THEIR FEET. CREW ASSUMED NOSE GEAR DOOR(S) HAD OPENED. AC SPEED AT THE TIME WAS 240 KTS AND DECREASED TO 230 KTS. 1 TO SDR SIMA20120315004Smoke Detector · no testDURING MAINTENANCE INSPECTION THE CARGO SMOKE DETECTORS WOULD NOT TEST. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE AFT CARGO SMOKE DETECTOR IAW EMB AMM 26-15-01. THE OPERATIONAL CHECK WAS GOOD. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA20120308003Light · inoperativeDURING B-INSPECTION FOUND THE RIGHT OVERWING EMERGENCY LIGHT OUT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERWING EMERGENCY LIGHT BULB. THE OPERATIONAL CHECK WAS GOOD IAW EMB AMM 33-50-10. THE AIRCRAFT WAS RETURNED TO SERVICESDR SIMA20120305004Light · inoperativeDURING B- INSPECTION FOUND THE RIGHT OVERHEAD EMERGENCY LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE RIGHT OVERHEAD EMERGENCY LIGHT BULB IAW AMM TASK 30-50-08-000-801-A AND 30-50-08-400-801-A. THE OPERATIONAL CHECK WAS GOSDR SIMA2012041001Rib · crackedDURING MAINTENANCE BASE VISIT FOUND THE LEFT RIB 5 CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-57MR-59R1. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA2012031002Structure · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE LAVATORY SERVICE HAS CORROSION. THE AIRCRAFT WAS REMOVED FROM SERVICE. COMPLIED WITH EO EM-53MR-1926. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201135402Module · inoperativeON FLIGHT 2827 THE CREW REPORTED THAT ON CLIMBING THROUGH 14000 FEET A LOUND CLUNK WAS HEARD BEHIND THE FIRST OFFICERS SEAT. RECEIVED AN ELECTRICAL EMERGENCY ABNORMAL MESSAGE AND EMERGENCY LIGHT NOT ARMED MESSAGES ON EICAS. BOTH MESSAGES DISAPPEARED AFTER A SDR SIMA201126908Control Unit · malfunctionedON FLIGHT 4004 THE CREW REPORTED THAT AFTER LANDING, INITIAL APPLICATION OF BRAKES GAVE NO BRAKING ACTION ALONG WITH A BRAKE DEGRADE CAUTION ON EICAS. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED BRAKE CONTROL UNIT IAW AMM# 32-41-02. THE OPERSDR SIMA201126213Carbon Seal · failedON FLIGHT 2882 THE CREW REPORTED THAT DURING CLIMBOUT THROUGH 4500 FEET RECEIVED AN EICAS MESSAGE OF LAV SMOKE. THE CREW DECLARED AN EMERGENCY AND ELECTED TO RETURN TO XNA. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE E2 ZERO CARBON SEALSDR SIMA201122207ALight · inoperativeFOUND RT OVERWING EXTERNAL EMERGENCY LIGHT INOP. REPLACED BULB.SDR SIMA201115106Inverter · inoperativeFOR FLIGHT 2975 DURING THE PREFLIGHT INSPECTION FOUND THE RIGHT OVERWING EXIT UPPER EXIT SIGN LIGHT INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHTS NR 5 INVERTER IAW EMB 145 AMM 33-50-11. THE OPERATIONAL CHECK WASDR SIMA201023904Tire · blownON FLIGHT 3648 DURING LANDING THE AIRCRAFT HAD A BLOWN TIRE AND DAMAGE TO THE FLAP. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE NR 3 TIRE, PART NUMBER 31641, SERIAL NUMBER 11920643P. ALSO REMOVED AND REPLACED THE RIGHT HAND INBOARD FLAP SDR SIMA201018201Light · inoperativeDURING MAINTENANCE BASE VISIT FOUND THE AFT CEILING EMERGENCY LIGHT TO BE INOPERABLE. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPLACED THE EXIT CEILING LIGHT. THE OPERATIONAL CHECK WAS GOOD IAW AMM 33-50-15. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201013204Pump · activatedON FLIGHT 3321 CREW REPORTED, RECEIVED A HYDRAULIC 2 LOW QUANTITY MESSAGE WITH A FLUID LEVEL THAT APPEARED TO BE DROPPING. THE CREW ELECTED TO DIVERT TO GDL. THE AIRCRAFT LANDED WITHOUT INCIDENT. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SDR SIMA201006202Strip · brokenDURING MAINTENANCE BASE VISIT FOUND THE LEFT NR 1 EMERGENCY LIGHT STRIP TO BE BROKEN. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 EMERGENCY LIGHT STRIP IAW EMB 145 AMM 33-50-12. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201006109Skin · dentedDURING MAINTENANCE BASE VISIT FOUND THAT THE FUSELAGE HAS A DENT BETWEEN FRAMES 19 AND 19A AND STRINGERS 11R AND 12R. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED FRAMES 19 AND 19A AND STRINGERS 11R AND 12R IAW EMB SRM 53-21-01 FIG 204. THE AIRCRAFT WAS SDR SIMA201006108Structure · crackedDURING MAINTENANCE BASE VISIT FOUND THE REAR ELECTRONIC COMPARTMENT DOOR (272DR) TO BE CRACKED UNDER UPPER HINGE POINT SUPPORT. THE AIRCRAFT WAS REMOVED FROM SERVICE. STOP DRILLED CRACKS, FABRICATED AND INSTALLED DOUBLER IAW EO EM-52MR-234. THE AIRCRAFT WASSDR SIMA201006107Connector · missingDURING MAINTENANCE BASE VISIT FOUND THE EMERGENCY LIGHT STRIP FEMALE CONNECTOR AT SEAT 1A TO BE MISSING. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE EMERGENCY LIGHT STRIP CONNECTOR AT SEAT 1A FUSELAGE SIDE IAW EMB 145 WM 20-21-00. THE AISDR SIMA201006105Skin · dentedDURING MAINTENANCE BASE VISIT FOUND THE LEFT REAR FUSELAGE I SKIN AT FRAMES 65 - 66, AND STRINGER 20L - 51L TO BE DENTED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED LEFT REAR FUSELAGE I SKIN AT FRAMES 65 - 66, AND STRINGER 20L - 51L IAW EO EM-53MR-1479SDR SIMA201006106Fitting · crackedDURING MAINTENANCE BASE VISIT FOUND THE HORIZONTAL STABILIZER ANTI-ROTATION TAB TO BE CRACKED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND INSTALLED A SERVICEABLE HORIZONTAL STABILIZER FITTING IAW EO EM-55MR-324. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201005705Support · corrodedDURING THE MAINTENANCE BASE VISIT THE RIGHT OUTBOARD SEAT TRACK SUPPORT WAS FOUND TO BE CORRODED AT FRAME 50. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE RIGHT OUTBOARD SEAT TRACK SUPPORT AT FRAME 50 IAW EO EM-53MR-1476. THE AIRCRAFT WAS RETURNED TOSDR SIMA201005704Floor Support · corrodedDURING THE MAINTENANCE BASE VISIT THE LEFT OMEGA BEAM THAT HAD PREVIOUS REPAIRS AT FRAME 20 WAS FOUND TO BE CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED IAW EMB SRM 53-00-10 FIG 201 SHEET 1. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201005701Floor Support · corrodedDURING MAINTENANCE BASE VISIT THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED FORWARD OF FRAME 25. THE AIRCRAFT WAS REMOVED FROM SERVICE. REPAIRED THE LEFT OMEGA BEAM FORWARD OF FRAME 25 IAW EMB SRM 53-00-10. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201005405Sill · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE RIGHT NR 1 CABIN FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED SILL IAW EMB SRM 51-40-02. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA201005402Sill · corrodedDURING MAINTENANCE BASE INSPECTION FOUND THE LEFT NR 1 FLOOR SILL CORRODED. THE AIRCRAFT WAS REMOVED FROM SERVICE. REMOVED AND REPLACED THE LEFT NR 1 FLOOR SILL IAW EMB SRM 51-40-02 AND 51-40-06. THE AIRCRAFT WAS RETURNED TO SERVICE.SDR SIMA200913903Carbon Seal · failedON FLIGHT 4078, CREW REPORTED AFTER TAKEOFF RECEIVED LAV SMOKE WARNING. F/A REPORTS NO VISUAL SMOKE OR ODOR. AIRCRAFT RETURNED TO FIELD WITHOUT FURTHER INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND 0 CARBON SEAL LEAKING REMOVED AND REPLACED "0" CARBON SEASDR SIMA200818201Control Lever · inoperativeON FLIGHT 3968 - CREW REPORTED AFTER TAKEOFF THEY RECEIVED LANDING GEAR AIR/GROUND FAIL AND FEAR WOULD NOT RETRACT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LT MAIN LANDING GEAR WOW PROX SW NRSDR SIMA200817802Electronic Unit · malfunctionedON FLIGHT 4113, CREW REPORTED WHEN AIRCRAFT BECAME AIRBORNE, "LG AIR/GND FAIL" MESSAGE APPEARED ON EICAS AND GEAR HANDLE WOULD NOT MOVE SO GEAR WOULD NOT RETRACT. RETURNED FOR LANDING WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED LANSDR SIMA200808108Sill · corrodedDURING MBV INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REPAIRED SERVICE DOOR SILL IAW EMB SRM 53-21-02 FIG 201 AND 51-40-02. AIRCRAFT RETURNED TO SERVICESDR SIMA200733404Sensor · brokenABORTED TAKEOFF AT 80 KTS FOR WARNING SPS 1 INOP MESSAGE. ON POST FLIGHT INSPECTION, FOUND AOA 1 VANE BROKEN. REMOVED AND REPLACED NR 1 AOA SENSOR IAW EMB145 AMM 27-36-00 BECAUSE VANE ON AOA SENSOR DAMAGED. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200713201Control Rod · excess playPERFORMING AN A CHECK FOUND UPPER RUDDER CONTROL ROD HAD PLAY BETWEEN THE ROD END AND ROD TUBE. REMOVED AND REPLACED UPPER RUDDER CONTROL FOR PLAY AND LOWER CONTROL ROD AS PRECAUTIONARY, FDR DOWNLOADED. COMPONENTS AND FDR DATA RELEASED TO OEM FOR ANALYSIS. SDR SIMA200635404Engine · vibratesPOWER WAS REDUCED BELOW 75 PERCENT ENGINE 2 HAD A NOTICEABLE VIBRIATION. REMOVED AND REPLACED NR 2 ENGINE IAW AMERICAN EAGLE WORK CARD 72-000-00. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.SDR SIMA200633105Light · looseFORWARD FACING EMERGENCY EXIT LIGHT INOP IN CABIN. RESECURED FORWARD EMERGENCY CENTER AISLE EXIT LIGHT IAW EMB AMM 33-55-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR SIMA200532202Warning Light · false activationDURING LANDING FLARE EICAS MESSAGE RUDDER SYSTEM ONE AND 2 INOPERATIVE. NO RUDDER CONTROL DURING REMAINDER OF LANDING OR DURING TAXI. PERFORMED OPERATIONAL CHECK OF THE RUDDER SYSTEM WITH NO DISCREPANCIES NOTED. AIRCRAFT RETURNED TO SERVICE. (K)SDR SIMA200525218Skin · gougedSAW - DURING PHASE 5A INSPECTION, FOUND GOUGE ON EXTERNAL SKIN ON PASSENGER DOOR AFT LOWER EDGE. REPAIRED PAX DOOR BY INSTALLING EXTERNAL DOUBLER IAW SRM 52-10-01 FIGURE 204 AND IC 2005-145/4892. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIM2005F00007Channel · corrodedDURING AN MBV INSPECTION, THE RT HAT BEAM WAS FOUND TO BE CORRODED AT FRAME 23. BLENDED THE RT HAT BEAM TO REMOVE CORROSION. PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200435820Beam · corrodedDURING AN MBV INSPECTION THE GALLEY CENTER HAT BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER HAT BEAM. INSTALLED SERVICEABLE HAD BEAM IAW SRM. (SW21200501979) (K)SDR SIMA200435815Sill · corrodedDURING INSPECTION, THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW SRM. (SW21200501979) (K)SDR SIMA200432205Skin · damagedDAMAGE ON AFT LOWER FUSELAGE AT FRAME 68 AND STRINGER 21L. PERFORMED A CUT OUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.(K)SDR SIMA200432206Skin · damagedDAMAGE ON THE AFT LOWER FUSELAGE BETWEEN FRAMES 65 AND 66 AT STRINGER 211. PERFORMED A CUTOUT OF THE DAMAGED AREA. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW SRM.SDR SIMA200425602Control Unit · inoperativeFWA - FLT 3794 - AFTER TAKEOFF, CREW RECEIVED PITCH TRIM MAIN AND PITCH TRIM BACKUP INOPERATIVE MESSAGE. PERFORMED AOM PROCEDURES AND PITCH TRIM WAS NOT REESTABLISHED. CREW ELECTED TO RETURN TO FWA. MAINTENANCE REMOVED AND REPLACED THE HORIZONTAL STABILIZER
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