Embraer EMB-135KL

Service difficulty reports · 5,598

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'EMB135KL'
  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 SIMA200528315Fan · burnedAFTER TAKEOFF CREW GOT VISIBLE SMOKE IN CABIN AND LAV SMOKE EICAS MESSAGE. REPLACED RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (SW21200600536) (K)Oct 4, 2005 · N824AE · Emb EMB135KL · Air Distribution FanSDR SIMA200528303Floorbeam · corrodedTHE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. PERFORMED A CUT OUT OF THE FORWARD DIGITAL TO REMOVE THE CORROSION. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)Oct 3, 2005 · N823AE · Emb EMB135KL · Fuselage Main, Floor BeamSDR SIMA200528302Clip · corrodedTHE BAGGAGE DOOR FWD LATERIAL (SHEAR CLIP) LOWER SECTION AT FRAME 65 WAS FOUND CORRODED. REMOVED A SECTION OF THE SHEAR CLIP TO REMOVE THE CORROSION. PREPARED A SHEAR CLIP. FABRICATED A SHEAR CLIP SPLICE DOUBLER. REPAIR DONE IAW SRM. (SW21200600333) (K)Oct 2, 2005 · N823AE · Emb EMB135KL · Fuselage, Door HingeSDR SIMA200527706Frame · crackedFOUND FRAME 68 WAS FOUND CRACKED AT THE BAGGAGE DOOR STAY ROD HOLDER CUP BRACKET. PERFORMED CUT OUT OF FRAME 68 TO REMOVE THE DAMAGE. FABRICATED AN ANGLE SPLICE AFT AND ONE FOR FORWARD. FABRICATED A CUP SUPPORT. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-Sep 29, 2005 · N820AE · Emb EMB135KL · Fuselage Main, FrameSDR SIMA200527705Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE DAMAGED SILL AND CLEANED THE AREA. INSTALLED SERVICEABLE SILL IAW EMB REPAIR STATEMENT IC2005-145/5419 DATED SEPT 27, 2005. (M)Sep 29, 2005 · N820AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200527703Floor Support · corrodedTHE LEFT OMEGA BEAM AFT OF FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED A DOUBLER, FILLER AND SHIMS FOR REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 202. (M)Sep 29, 2005 · N820AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200527701Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE EXISTING SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 135 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-03. (M)Sep 28, 2005 · N832AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200527704Floor Support · corrodedTHE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. PREPARED DOUBLER, FILLER AND SHIMS FOR THE REPAIR. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M)Sep 28, 2005 · N820AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200527702Beam · corrodedTHE CENTER BEAM AT FRAME 24 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A FILLER, DOUBLER AND SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC 2005-145/5255 DATED SEPT 21, 2005 AND EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER Sep 28, 2005 · N820AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200526904Sill · corrodedTHE CARGO DOOR CUTOUT LOWER SILL WAS FOUND CORRODED. REMOVED EXISTING LOWER SILL AND INSTALLED SERVICEABLE SILL. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30) CHAPTERS 51-40-2, 51-20-03 AND 51-40-06. (M)Sep 23, 2005 · N820AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200526401Sill · corrodedSAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR SILL IS CORRODED BETWEEN FRAMES 20 AND 22. MAINTENANCE INSTALLED A NEW SERVICE DOOR SILL IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 12, 2005 · N857AE · Emb EMB135KL · Fuselage Structure (General)SDR SIMA200525701Fan · seizedSJC - FLT 3158 - CREW REPORTED PLASTIC BURNING SMELL IN ENTIRE AIRCRAFT HAD TO DON OXYGEN MASKS. REPLACED NR 1 RECIRCULATION FAN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Sep 10, 2005 · N813AE · Emb EMB135KL · Air Distribution FanSDR SIMA200525220Floor Support · corrodedTHE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE LEFT OMEGA BEAM TO REMOVE CORROSION. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10 FIGURE 201. (M)Sep 5, 2005 · N818AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525222Fitting · damagedABI - THE RIGHT AILERON PCA FITTING INBOARD BUSHING HOLE WAS FOUND DAMAGED. REMOVED AND THE EXISTING PCA FITTING. INSTALLED NEW PCA FITTING IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTERS 51-40-02 AND EMB REPAIR STATEMENT IC2005-145/4844 DATED SEPT 2, 200Sep 4, 2005 · N821AE · Emb EMB135KL · Wing Main, Frame StructureSDR SIMA200525219Sill · corrodedABI - THE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED THE SERVICE DOOR SILL AND INSTALLED SERVICEABLE SILL IAW EMB 145 SRM, SRM EMB145/1142 REV 30, CHAPTERS 51-40-02 AND 51-20-01. (M)Sep 2, 2005 · N821AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525221Floor Support · corrodedTHE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30 CHAPTER 53-00-10 FIGURE 203. (M)Sep 2, 2005 · N818AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525223Floor Support · corrodedON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE PREVIOUS REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/1142 REV 30, CHAPTER 53-00-10 FIG 201. (M)Sep 1, 2005 · N818AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525216Housing · corrodedDURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT MAIN STRUT BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Main Landing Gear Strut/Axle/TruckSDR SIMA200525215Housing · corrodedSAW - DURING MBV INSPECTION, FOUND NOSE LANDING GEAR LEFT STRUT DRAG BRACE BEARING HOUSING SHOWS SIGNS OF PITTING. REWORKED BEARING HOUSING TO WITHIN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Main Landing Gear Strut/Axle/TruckSDR SIMA200525217Cap · corrodedDURING MBV INSPECTION, FOUND NOSE LANDING GEAR RIGHT DRAG BRACE BEARING CAP HAS SIGNS OF PITTING. REMOVED NEGLIGIBLE PITTING FROM BEARING CAP FOUND TO BE IN LIMITS IAW SRM 53-11-08 PAGE 101. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Main Landing GearSDR SIMA200525211Floor Support · corrodedSAW - DURING CPCP INSPECTION, FOUND RIGHT HAT BEAM IS CORRODED BETWEEN FRAMES 18-19. REPLACED HAT BEAM IAW EMB IC2005-145/4638. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525212Floor Support · corrodedSAW - DURING CPCP INSPECTION, FOUND LEFT OMEGA BEAM CORRODED AT FRAME 20. INSTALLED DOUBLER IAW SRM 53-00-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525213Sill · corrodedSAW - DURING CPCP INSPECTION, FOUND SERVICE DOOR AFT SILL HAS CORROSION. INSTALLED NEW AFT SILL PLATE IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525214Floor Support · corrodedSAW - FOUND DURING CPCP INSPECTION, LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24-25. REPLACED DAMAGED AREA IAW SRM 53-00-01 FIG 202 AND IC2005-145/4572. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 29, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525207Cap · corrodedSAW - DURING MBV INSPECTION, FOUND RIGHT MLG AFT BEARING CAP CORRODED. REMOVED AND REPLACED RIGHT MLG AFT BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Main Landing GearSDR SIMA200525208Cap · corrodedSAW - DURING MBV INSPECTION, FOUND RIGHT MAIN LANDING GEAR FORWARD BEARING CAP CORRODED. REPLACED BEARING CAP IAW EMB 140 WORK CARD 57-200-84. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Main Landing GearSDR SIMA200525210Intercostal · corrodedSAW - DURING CPCP INSPECTION, FOUND RIGHT INTERCOSTAL FOR AISLE RAMP AT FRAME 20 IS CORRODED. INSTALLED NEW INTERCOSTAL IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200525209Sill · corrodedDURING CPCP INSPECTION, FOUND LEFT CREASE BEAM CORRODED AT FRAME 22. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage Main, StructureSDR SIMA200525201Seat Track · corrodedSAW - DURING CPCP INSPECTION, FOUND LEFT FORWARD SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200525202Seat Track · corrodedSAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 5TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200525203Seat Track · corrodedSAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 3RD FROM FRONT SEAT TRACK CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200525204Seat Track · corrodedSAW - DURING CPCP INSPECTION, FOUND RIGHT UPPER 4TH FROM FRONT SEAT TRACK CORRODED. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801-A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200525205Seat Track · corrodedSAW - DURING CPCP INSPECTION, FOUND LEFT UPPER 4TH SEAT TRACK FROM FRONT IS CORRODED AROUND SCREW HOLES. REPLACED SEAT TRACK IAW EMB AMM 53-01-06-400-801A. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage, Seat/Cargo Attach FittingsSDR SIMA200525206Doubler · corrodedSAW - DURING CPCP INSPECTION, FOUND DOUBLER PLATE WHERE RIGHT HAT BEAM AND FLOORBEAM AT FRAME 22 MEET IS CORRODED. REPLACED DOUBLER IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 28, 2005 · N817AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA200500151Lamp · burned outAISLE EMERGENCY LIGHT NR 3 LAMP INOPERATIVE. RELAMPED NR 3 AISLE EMERGENCY LIGHT IAW EMB 140 MM 33-50-08. OPS CHECK GOOD.Aug 27, 2005 · N381SK · Emb EMB135KL · Emergency LightingSDR CHQA200500150Lamp · burned outLEFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW EMB 140 MM 33-50-07.Aug 27, 2005 · N375SK · Emb EMB135KL · Emergency LightingSDR SIMA200524109Stringer · chafedSTRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL. BLENDED THE CHAFED AREA AND FABRICATED AND ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30 CHAPTER 53-24-02. (M)Aug 25, 2005 · N824AE · Emb EMB135KL · Fuselage Main, Longeron/StringerSDR SIMA20054108Floor Support · corrodedABI - THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)Aug 24, 2005 · N824AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200524103Sill · damagedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. BLENDED THE SILL TO REMOVED THE DAMAGE. APPLIED ALODINE, EPOXY PRIMER AND POLYURETHANE PAINT TO BLENDED AREA. FILLED THE BLENDED AREA WITH HYSOL 9394 RESIN AND CURED. FABRICATED TWO DOUBLERS. REPAIR DONE IAug 24, 2005 · N858AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200524107Floor Support · corrodedA PREVIOUS REPAIR, REF FAA FOR 337 DATED DEC 9, 2004, OF THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR PLATE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, EMB145/1142 REV 30, CHAPTERSAug 23, 2005 · N824AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200524110Floor Support · corrodedTHE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE CENTER OMEGA BEAM TO REMOVED THE DAMAGE. FABRICATED A FILLER, EXTERNAL, ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB 145/1142 REV 30, CHAPTER 53-00-10 FIG 203. (MAug 23, 2005 · N858AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR CHQA200500146Proximity Sensor · unsecureON DEPARTURE, LANDING GEAR WAS SELECTED UP. THE LT MAIN DID NOT INDICATE UP AND LOCKED. AN EICAS MESSAGE L/G LEVER DISAGREE APPEARED. GEAR WAS CYCLED IAW THE QRH. RETURNED TO FIELD. DID NOT DECLARE AND EMERGENCY, HOWEVER AN EMERGENCY WAS DECLARED ON OUR BAug 23, 2005 · N382SK · Emb EMB135KL · Landing Gear Position and WarningSDR SIMA200517107Inverter · inoperativeEMERGENCY EXIT SIGN FOR OVERWING EXIT INOPERATIVE. REPLACED INVERTER NR 6 IAW EMB MM 33-50-11. OPERATIONAL CHECK GOOD. REMOVED AND REPLACED BATTERY POWER SUPPLY NR 4 (BT 8503) IAW EMB MM 33-50-04. OPERATIONAL CHECK GOOD, P/N 20131A S/N 63075. AIRCRAFT RETAug 18, 2005 · N804AE · Emb EMB135KL · Emergency LightingSDR SIMA200522702Fire Warning · false indicationTHE BAGGAGE COMPARTMENT EXTINGUISHER LIGHT ILLUMINATED. THE CAPTAIN DISCHARGED THE BAGGAGE COMPARTMENT FIRE BOTTLES AS A PRECAUTIONARY. THE FIRE DEPT INSPECTED THE CARGO AREA AND FOUND NO EVIDENCE OF SMOKE OR FIRE. RAI HIGH RATE BOTTLE AS PER EMB 140 AMM 26Aug 15, 2005 · N813AE · Emb EMB135KL · Fire DetectionSDR CHQA200500137Regulator Valve · burnedFLIGHT 5282 - STL - ATL - ON CLIMB-OUT, RECEIVED BLEED 1 CLOSED MESSAGE AND A BURNING SMELL AROUND ROW 5A. FOUND THE PACK VALVE CIRCUIT BREAKER POPPED AND FOUND THE PACK VALVE WAS BURNT UP CAUSING THE CIRCUIT BREAKER TO POP. REMOVED AND REPLACED THE PACK VALAug 7, 2005 · N375SK · Emb EMB135KL · Cabin Cooling SystemSDR SIMA200521614Battery Pack · dischargedSGF - FLT 3788 - ENTRY, GALLEY DOOR, ROW 1 THROUGH ROW 8 AND LEFT EMERGENCY LIGHTS DO NOT ILLUMINATE. REPLACED EMERGENCY BATTERY PACKS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Aug 4, 2005 · N833AE · Emb EMB135KL · Emergency LightingSDR CHQA200500136Bulb · burned outLEFT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED BULB IAW EMB 140 MM 33-50-10. OPS CHECK GOOD.Aug 4, 2005 · N295SK · Emb EMB135KL · Emergency LightingSDR SIMA200521615Skin · dentedTHE FUSELAGE SKIN JUST AFT OF FRAME 11 AND BETWEEN STRINGERS 20L AND 21L WAS FOUND TO BE DENTED. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED A REPAIR DOUBLER AND FILLER. REPAIR DONE IAW EMB SRM, SRM 145 1142 REV 30, CHAPTERS 53-10-01. (M)Aug 3, 2005 · N856AE · Emb EMB135KL · Fuselage Main, Plate/SkinSDR SIMA200521616Sill · corrodedABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR TO REMOVE CORROSION. FABRICATED TWO DOUBLERS FOR REPAIR. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-21-02. (M)Aug 2, 2005 · N856AE · Emb EMB135KL · Fuselage Miscellaneous StructureSDR SIMA200522004Support · corrodedSAW - DURING IMBV INSPECTION, FOUND CENTER HAT BEAM RAMP CORRODED. REMOVED AND INSTALLED NEW HAT BEAM RAMP IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)Aug 1, 2005 · N816AE · Emb EMB135KL · Fuselage Miscellaneous Structure
Back to Embraer EMB-135KL