N635AE
Service difficulty reports · 185
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 = 'N635AE' 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 = 'N635AE' 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 SIMA200821001Thermal Switch · failedON FLIGHT 3839 CREW REPORTED AT CRUISE NUMBER 2 HYDRAULIC SYSTEM OVERHEAT FOLLOWED BY NUMBER 2 HYDRAULIC SYSTEM FAIL. AFTER AOM COOL DOWN PERIOD INITIALLY WOULD NOT TURN ON WITH EICAS SYSTEM OVER HEAT MESSAGE GONE. CREW TRIED 5 MIN LATER AND SYSTEM CAME ON. SDR SIMA200733403O-Ring · brokenCREW GOT A BLEED 1 LEAK MESSAGE IN FLIGHT WHILE PASSING THROUGH 10,000 FEET. CREW FOLLOWED AOM PROCEDURES AND MESSAGE WENT AWAY. CREW DECIDED TO RETURN TO ORD. CREW DECLARED AN EMERGENCY AND LANDED WITHOUT INCIDENT. FOUND O-RING IN CARGO AREA, BOTTOM PANELSDR SIMA200722702Shutoff Valve · failedABORTED TAKEOFF, BRAKE OVERHEAT WARNING MESSAGE. REMOVED AND REPLACED INBOARD BRAKE SHUTOFF VALVE IAW EMB AMM 32-41-00. OPERATIONAL CHECK GOOD, RETURNED AIRCRAFT TO SERVICE.SDR SIMA200717505A/C Pack · odorBURNING SMELL FROM PACKS WITH NO SMOKE. INSPECTED AND FOUND APU INTAKE SCREEN COVERED WITH CICADAS. REMOVED CICADAS. PERFORMED OPERATIONAL CHECK OF PACK SYSTEM WITH NO BURNING SMELL NOTED. RETURNED AIRCRAFT TO SERVICE.SDR SIMA200621401Unknown · unknownLBB - FLT 3638 - DURING CLIMB, HEARD LOUD AIR NOISE FROM THE NOSE GEAR AREA GOT LOUDER AS THE AIRCRAFT CLIMBED. AIRCRAFT RETURNED TO LBB. (M)SDR SIMA200620828Floor Support · corrodedDURING HMBV INSPECTION, THE FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED AREA BY MAKING A CUT OUT, PREPARED STRAP AND THREE SHIMS OF VARIOUS SIZES. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, CHAPTER 53-21-10 FIG 201. RETURNED AIRCRAFT TSDR SIMA200620827Stringer · chafedABI - DURING HMBV INSPECTION, STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL. BLENDED THE DAMAGED AREA AND PERFORMED NDT INSPECTION WITH NO REJECTABLE INDICATIONS. FABRICATED A DOUBLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM145/1142 REV 33, SDR SIMA200620826Sill · corrodedDURING HMBV INSPECTION, FOUND CARGO DOOR CUTOUT LOWER SILL CORRODED. REMOVED THE CORRODED DOOR SILL AND CLEANED THE AREA. INSTALL NEW DOOR SILL. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 33, 51-20-01, 03, 51-40-04, 06 AND CPM, CMP-145/1132 REV 13 CHAPTER 51SDR SIMA200503804Skin · lightning strikeDURING AN MBV INSPECTION, A LIGHTNING STRIKE WAS FOUND ON THE LT SIDE OF THE FUSELAGE BETWEEN FRAMES 32 AND 33 AT STRINGER 6L. REMOVED THE DAMAGE BY MAKING A CUT OUT. FABRICATED A FILLER, OUTER DOUBLER AND AN INNER DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200503401Floor Support · corrodedTHE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER, TWO SHIMS AND PLATE. REPAIR DONE IAW SRM. (K)SDR SIMA200503402Floor Support · corrodedTHE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED GALLEY CENTER BEAM. INSTALLED NEW BEAM IAW SRM. (K)SDR SIMA200434905Skin · lightning strikeLIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 16788.5 STRINGER 6L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501815) (K)SDR SIMA200434904Skin · lightning strikeLIGHTNING STRIKE DAMAGE FOUND ON SKIN AT FRAME 20 BETWEEN STRINGERS 3L AND 4L. MAINTENANCE COMPLETED A PATCH REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200501814) (K)SDR SIMA200431702Smoke · detectedDURING DECENT, CREW REPORTED A BURNING ELECTRICAL SMELL IN THE COCKPIT FOR ABOUT 30 SECONDS WITH PAINT SMOKE BEING SEEN FOLLOWED QRH PROCEDURES. THERE WERE NO ALARMS, WARNING MESSAGES OR SMOKE IN CABIN. MAINTENANCE COULD NOT DUPLICATE DISCREPANCY. AIRCRAFTSDR SIMA200420102Control Unit · inoperativeCREW NOTED AFTER ROTATION SPOILER OPEN INDICATION ACCOMPANIED WITH EICAS MESSAGE SPOILER FAIL AND TAKEOFF CONFIGURATION WARNING. REPLACED SPOILER CONTROL UNIT. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200411201Connector · looseDISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406984)SDR SIMA200327201Battery · inoperativeCMH - REARE CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 4 EMERGENCY BATTERY, OPS CHECK GOOD. (M)SDR SIMA200305002Controller · inoperativePIT - FLT 4345 - CREW REPORTED DURING CLIMB THROUGH 17,000 FT, CABIN ALTITUDE EXCEEDED 14,500 FT, OXYGEN MASK DEPLOYED IN MAIN CABIN. THE FLT CREW PERFORMED EMERGENCY DESCENT OT 10,000 FT REGAINED CONTROL OF CABIN ALTITUDE AND DIFFERENTIAL PRESS. THE FLT CRESDR SIMA200236304Skin · gougedABI - DURING AN IMBV INSPECTION, A GOUGE WAS FOUND ON REAR FUSELAGE 1 BETWEEN FRAMES 65 AND 66 AND STRINGERS 20L AND 21L. REMOVED DAMAGE BY MAKING A 2.25 INCH BY 3.12 INCH CUTOUT. FABRICATED A REPAIR FILLER. REPAIR DONE IAW EMB 145 SRM (145/1142 REV 20) 53-SDR SIMA200300808Beam · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, CENTER BEAM RAMP FOUND CORRODED. REMOVED AND INSTALLED SERVICEABLE RAMP IAW EMB 145 SRM 51-40-02, 51-20-03. (M)SDR SIMA200300805Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, RIGHT SILL CORRODED BETWEEN FRAMES 23-27, 32-36, 40, 46-47, 50 AND 53-54. REMOVED RIGHT SILL AND INSTLALED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02, 51-20,03 AND 51-40-06. (M)SDR SIMA200235107Beam · corrodedABI - DUIRNG AN IMBV INSPECTION, THE GALLEY FLOOR CENTER BEAM WAS FOUND TO BE CORRODED BELOW SRM LIMITS AT FRAME 23. BLENDED THE CORRODED AREA AND PERFORMED NDT INSPECTION APPLIED ALODINE AND EPOXY PRIMER TO THE BLENDED AREA. FILLED THE BLENDED AREA WITH EPOSDR SIMA200235106Skin · corrodedABI - DURING AN IMBV INSPECTION, THE THIRD SCREW HOLE ON THE RIGHT WINDSHIELD FRAME WAS FOUND TO BE CORRODED BELOW LIMITS. REAMED FASTENER HOLE OT .313 INCH AND PERFORMED AN NDT INSPECTION WITH NO DEFECTS FOUND. FABRICATED A REPAIR BUSHING. REPAIR DONE IAW SDR SIMA200300806Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTIONS, AFT SERVICE DOOR SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE AFT SILL IAW EMB 145 SRM 51-40-02, 51-20-03. (M)SDR SIMA200300809Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT FLOOR SILL BETWEEN FRAMES 19 TO 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)SDR SIMA200300810Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING A IMBV INSPECTION, LEFT PROFILE AT FRAME 23 CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)SDR SIMA200300807Sill · corrodedABI - THIS IS A LEVEL 2 FINDING, FOUND DURING AN IMBV INSPECTION, SERVICE DOOR FORWARD SILL CORRODED. REMOVED AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM 51-40-02. (M)SDR SIMA200124802Warning System · activatedDFW - FLT 3479 - AFTER TAKEOFF, CREW NOTED E2 OIL IMPENDING BYPASS MESSAGE ON EICAS. AFTER 10 MINUTES NOTED 200 DEGREE ITT INCREASE ACCOMPANIED BY VIBRATION. ENGINE POWER WAS REDUCED TO IDLE AND CREW RETURNED TO FIELD. (M)SDR SIMA200111205Floorbeam · corrodedABI - FOUND LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND SRM LIMITS AT FRAME 20. REPAIRED FRAME IAW EMBRAER SRM 145/1142 REV 12 CHAPTER 53-21-10 PAGE 208. (M)SDR SIMA200104601Heater · failedORD - FLT 4114 - IN CRUISE WINDSHIELD 1 HEAT FAILED. RETURN TO ORD FOR MAINTENANCE REPAIR. MAINTENANCE COMPLIED WITH ENGINEERING ORDER EM 3000-018, WINDSHIELD HEATING IMPROVEMENT. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR 20010504AP004Control Unit · failedCID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICERS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. REF SIMA200101804. (M)SDR SIMA200101804Switch · failedCID - FLT 4236 - CREW REPORTED PITCH TRIM 1 FAIL ON APPROACH. MAINTENANCE REMOVED AND REPLACED CAPTAIN AND FIRST OFFICERS PITCH TRIM YOKE SWITCHES AND THE HSCU. OPS CHECK WAS GOOD AND AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA1141Light · inoperativeORD - FLT 4401 - EMERGENCY LIGHTS OVER SERVICE DOOR INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED SAME. OPS CHECK GOOD. (M)SDR SIMA992981Switch · failedORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR 2000ZZZX167. (X)SDR 2000ZZZX167Switch · failedORD - FLT 4387 - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED TWO RIGHT MAIN LANDING GEAR PROXIMITY SWITCHES. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. REF: OPER CONTROL NR SIMA99298-1.
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