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.

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. Jul 26, 2008 · N635AE · Emb EMB145LR · Hydraulic Indicating SystemSDR 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 PANELNov 28, 2007 · N635AE · Emb EMB145LR · Engine Bleed Air SystemSDR 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.Aug 14, 2007 · N635AE · Emb EMB145LR · BrakeSDR 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.Jun 21, 2007 · N635AE · Emb EMB145LR · Cabin Cooling SystemSDR 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)Jul 31, 2006 · N635AE · Emb EMB145LR · Nose/Tail Landing GearSDR 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 TJul 4, 2006 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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, Jun 30, 2006 · N635AE · Emb EMB145LR · Fuselage Main, Longeron/StringerSDR 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 51Jun 30, 2006 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Feb 1, 2005 · N635AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR 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)Jan 30, 2005 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR SIMA200503402Floor Support · corrodedTHE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED GALLEY CENTER BEAM. INSTALLED NEW BEAM IAW SRM. (K)Jan 28, 2005 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Dec 13, 2004 · N635AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR 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)Dec 13, 2004 · N635AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR 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. AIRCRAFTNov 11, 2004 · N635AE · Emb EMB145LR · Air Distribution SystemSDR 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)Jul 18, 2004 · N635AE · Emb EMB145LR · Drag Control SystemSDR SIMA200411201Connector · looseDISC - FWD OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. RESECURED CONNECTOR. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200406984)Apr 19, 2004 · N635AE · Emb EMB145LR · Electrical ConnectorsSDR SIMA200327201Battery · inoperativeCMH - REARE CABIN EMERGENCY LIGHTS INOPERATIVE. RAI NR 4 EMERGENCY BATTERY, OPS CHECK GOOD. (M)Sep 25, 2003 · N635AE · Emb EMB145LR · Emergency LightingSDR 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 CREFeb 18, 2003 · N635AE · Emb EMB145LR · Oxygen SystemSDR 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-Dec 19, 2002 · N635AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR 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)Dec 14, 2002 · N635AE · Emb EMB145LR · Fuselage Main, StructureSDR 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)Dec 14, 2002 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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 EPODec 13, 2002 · N635AE · Emb EMB145LR · Fuselage Main, StructureSDR 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 Dec 13, 2002 · N635AE · Emb EMB145LR · Fuselage Main, Plate/SkinSDR 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)Dec 10, 2002 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Dec 10, 2002 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Dec 10, 2002 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Oct 20, 2002 · N635AE · Emb EMB145LR · Fuselage Miscellaneous StructureSDR 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)Sep 5, 2001 · N635AE · Emb EMB145LR · Engine Oil Indicating SystemSDR 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)Apr 22, 2001 · N635AE · Emb EMB145LR · Fuselage Main, Floor BeamSDR 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)Feb 15, 2001 · N635AE · Emb EMB145LR · Windshield/Door Rain/Ice RemovalSDR 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)Jan 18, 2001 · N635AE · Emb EMB145LR · Stabilizer Control SystemSDR 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)Jan 18, 2001 · N635AE · Emb EMB145LR · Elevator Tab Control SystemSDR SIMA1141Light · inoperativeORD - FLT 4401 - EMERGENCY LIGHTS OVER SERVICE DOOR INOPERATIVE. FOUND CANNON PLUG DISCONNECTED. RECONNECTED SAME. OPS CHECK GOOD. (M)Apr 23, 2000 · N635AE · Emb EMB145LR · Emergency LightingSDR 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)Oct 25, 1999 · N635AE · Emb EMB145LR · Landing Gear Retraction/Extension SystemSDR 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.Oct 25, 1999 · N635AE · Emb EMB145LR · Landing Gear Retraction/Extension System
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