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.
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
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 SIMA200522005Gusset · corrodedDURING IMBV INSPECTION, FOUND CENTER HAT BEAM GUSSET CORRODED ON TOP. REMOVED AND INSTALLED NEW HAT BEAM GUSSET IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA20051609Floor Support · corrodedABI - A PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED REPAIR PARTS. FABRICATED A DOUBLER AND FILLER. REPAIR DONE IAW EMB IC2005-145/4050 DATED AUGUST 1, 2005. (M)SDR SIMA200521401Light · inoperativeFLT 3472 - BTR - CREW REPORTS EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED 2 FLOOR LIGHT STRIPS. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200522001Floor Support · corrodedSAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 BY CROSS BEAM ATTACHMENTS POINTS. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200522002Floor Support · corrodedSAW - DURING IMBV INSPECTION, FOUND LEFT OMEGA BEAM CORRODED BETWEEN FRAMES 24 AND 25 AT CROSSBEAM ATTACH POINT. REPAIRED LEFT OMEGA BEAM WITH DOUBLER IAW SRM 53-00-10 FIGURE 202. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200522003Floor Support · corrodedSAW - DURING IMBV INSPECTION, FOUND RIGHT OMEGA BEAM CORRODED AT FRAME 27 AT CROSSBEAM ATTACH POINT. REPAIRED RIGHT OMEGA BEAM WITH DOUBLER IAW SRM 53-22-10 FIGURE 201 SHEET 1. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200521610Sill · corrodedABI - THE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 51-40-02. (M)SDR SIMA200521611Stringer · chafedABI - FOUND STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, 145/1142 REV 29 CHAPTER 53-24-02. (M)SDR SIMA200521601Stringer · chafedSTRINGER 19R WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUTOUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM 145/1142 REV 30, CHAPTER 53-24-02. (M)SDR SIMA200521603Stringer · chafedABI - STRINGER 19L WAS FOUND TO BE CHAFED AT THE AFT BELLY PANEL CUT OUT. BLENDED THE CHAFED AREA. FABRICATED A REPAIR ANGLE AND SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-24-02. (M)SDR SIMA200521608Floor 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 EMB SRM 145/1142 REV 29, CHAPTER 53-00-10 FIG 201. (M)SDR SIMA200521602Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE SERVICE DOOR SILL TO REMOVE THE CORROSION. FABRICATED A DOUBLER. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-21-02 FIG 201 AND 203. (M)SDR SIMA200521605Floor Support · corrodedTHE LEFT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 29, CHAPTER 53-00-10. (M)SDR SIMA200521612Beam · corrodedTHE GALLEY CENTER BEAM WAS FOUND TO BE CORRODED UNDER THE FLOOR RAMP. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED EXTERNAL DOUBLER. REPAIR DONE IAW EMB SRM, SRM EMB145/1142 REV 29, CHAPTER 53-21-10 FIG 202 SHEET 2. (M)SDR SIMA200521606Floor Support · corrodedTHE LEFT OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUTOUT OF THE OMEGA BEAM TO REMOVED THE CORROSION. FABRICATED AN EXTERNAL, DOUBLER, AND FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 202. (MSDR SIMA200521604Frame · corrodedABI - FRAME 81 WAS FOUND GOUGED AT THE 6 O`CLOCK POSITION.SDR SIMA200520901Brake Assy · failedDURING LANDING, ANTI SKID CYCLED ABNORMALLY. AIRCRAFT WOULD NOT STOP IN NORMAL DISTANCES. REPLACED BRAKE CONTROL UNIT. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200521607Floor Support · corrodedABI - THE CENTER OMEGA BEAM AT FRAME 27 WAS FOUND CORRODED. PERFORMED A CUT OUT OF BEAM TO REMOVE THE CORROSION. FABRICATED AN EXTERNAL DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB 145 SRM, SRM EMB145/1142 REV 29, CHAPTER 53-00-10, FIG 203. (M)SDR SIMA200520605Skin · damagedLOWER FUSELAGE SKIN WAS DAMAGED BETWEEN FRAMES 10, 11 AND STRINGERS 20R AND 21R. REMOVED THE DAMAGED SKIN BY MAKING A CUT OUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW SRM. (K)SDR SIMA200520604Stringer · chafedA PREVIOUS REPAIR ANGLE ON STRINGER 19R WAS FOUND CHAFED. REMOVED THE EXISTING REPAIR ANGLE AND CLEANED THE AREA. FABRICATED AN INSTALLED A NEW REPAIR ANGLE. REPAIR DONE IAW SRM. (K)SDR SIMA200520603Floor Support · corrodedTHE LT OMEGA BEAM AT FR 20 WAS FOUND CORRODED. PERFORMED A CUT OUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER, PLATE, AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200520002Power Supply · dischargedLEFT WING LOWER EMERGENCY LIGHT INOPERATIVE. REPLACED NR 1 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200519317Floor Support · corrodedTHE LT OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. PERFORMED CUT OUT OF THE LT OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND 2 SHIMS. REPAIR DOEN IAW SRM. (K)SDR SIMA200519201Battery · dischargedDISC SEVERAL EMERGENCY EXIT SIGNS IN THE FORWARD CABIN WILL NOT ILLUMINATE. REPLACED BATTERY CHARGER AND BATTERY PACK IAW WC 33-700-19. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. CHARGER ASSEMBLY PN OFF IS 110049 AND SN OFF IS 17435. (K)SDR SIMA200519316Floor Support · corrodedA PREVIOUS REPAIR ON THE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED AN EXTERNAL ANGLE, FILLER REPAIR PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200519301Floor Support · corrodedTHE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200519302Floor Support · corrodedTHE LT OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A FILLER, DOUBLER AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200519303Floor Support · corrodedTHE LT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE COROSION BY MAKING A CUT OUT. FABRICATED A FILLER EXTERNAL ANGLE, PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR SIMA200519309Floor Support · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR OMEGA SHAPE HAS CORROSION AT FRAME 20. INSTALLED NEW DOUBLER IAW SRM. AC WAS RETURNED TO SERVICE. (K)SDR SIMA200519308Structure · chafedDURING INSPECTION, FOUND STRINGER 19 LT CHAFED BETWEEN FRAMES 52, 53. REPLACED DAMAGED STRINGER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200519307Doubler · corrodedDURING INSPECTION, FOUND FWD CABIN FLOOR DOUBLER HAS CORROSION AROUND NUT PLATES. INSTALLED NEW FORWARD CABIN FLOOR DOUBLER IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200519306Channel · corrodedDURING INSPECTION, FOUND SERVICE DOOR CHANNEL HAS CORROSION AROUND NUT PLATES. REPLACED SERVICE DOOR CHANNEL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200519305Sill · corrodedDURING INSPECTION, FOUND FORWARD CABIN SILL LT HAS SMALL AREA OF CORROSION ON UPPER FORWARD SIDE. REMOVED AND REPLACED LT SILL IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200517805Wire · brokenDISC - EMERGENCY LIGHT AT OVERHEAD SERVICE DOOR INOPERATIVE. FOUND WIRE SPLICE BROKEN. REPAIRED WIRING. OPERATIONAL CHECKED GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200517802Control Unit · inoperativeDUAL PITCH TRIM FAILURE. PERFORMED RESET PROCEDURES IN AOM AND PROCEEDED ON WITH NO INCIDENT. REPLACED THE HSCU. OPS CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200517801Battery · dischargedCREW DISCOVERED ON PREFLIGHT THAT EMERGENCY STRIP LITES IN FLOOR FROM ROW 11 AFT WILL NOT ILLUMINATE. REPLACED NR 4 BATTERY POWER SUPPLY IAW MM. OPERATIONAL CHECK GOOD. AC RETURNED TO SERVICE. (K)SDR SIMA200517803Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND CORRODED. REMOVED EXISTING SERVICE DOOR SILL, AND INSTALLED NEW SILL IAW SRM. (K)SDR SIMA200517804Floor Support · corrodedTHE LT OMEGA BEAM AT FRAME 20 WAS FOUND CORRODED. PERFORMED A CUTOUT TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER , PLATE AND 2 SHIMS. REPAIR DONE IAW SRM. (K)SDR CHQA200500113Warning Light · activatedDURING CLIMB AT FL210, RECEIVED "AILERON SYS 1 FAIL" EICAS MESSAGE. LEVELED OFF AT FL230 AND TOLD ATC TO STAND BY. FOLLOWED QRH AND TURNED OFF AILERON SYSTEM 1 AND SLOWED TO 250 KIAS. EMERGENCY DECLARED WITH ATC AND F/A PREPARED CABIN FOR EMERGENCY LANDING.SDR SIMA200517104Floor Support · corrodedDURING INSPECTION, FOUND LT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. REPAIRED LT OMEGA BEAM BETWEEN FRAMES 22 AND 25 IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200517105Stringer · chafedDURING INSPECTION, FOUND EXTERNAL STRINGER 19 LT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200517106Stringer · chafedDURING INSPECTION FOUND EXTERNAL STRINGER 19 RT HAS CHAFE DAMAGE BETWEEN FRAMES 52 AND 53. REPAIRED DAMAGE IAW SRM REINFORCEMENT REPAIR. AIRCARAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200517103Floor Support · corrodedDURING INSPECTION, FOUND RT OMEGA BEAM CORRODED BETWEEN FRAMES 22 AND 25. COMPLETED REPAIR TO OMEGA BEAM IAW SRM DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200517102Floor Support · corrodedDURING INSPECTION FOUND LT OMEGA BEAM CORRODED AT FRAME 20. REPAIRED LT OMEGA BEAM AT FRAME 20 IAW SRM, DOUBLER REPAIR. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR SIMA200516801Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. BLENDED THE CENTER SILL TO REMOVE THE CORROSION. PERFORMED EDDY CURRENT WITH NO REJECTABLE INDICATIONS. FABRICATED 2 DOUBLERS FOR REPAIR. REPAIR DONE IAW SRM. (K)SDR SIMA200515709Skin · damagedDURING AN MBV INSPECTION AND REPAIR OF DENT ON LEFT CENTER FUSELAGE 1 TDMI 851530243. PERFORMED CUT OUT OF THE SKIN PANEL BETWEEN FRAMES 22 AND 23 AND STRINGERS 13L AND 14. FABRICATED A FILLER AND REPAIR DOUBLER. REPAIR DONE IAW EMB 145 SRM, SRM EMB-145/114SDR CHQA200500107Contactor · burnedON CLIMB OUT OF STL THROUGH ACCELERATION ALTITUDE, THE FLIGHT CREW NOTICED A SLIGHT BURNING SMELL IN THE COCKPIT AREA. THE FLIGHT ATTENDANT REPORTED IT SMELLED A LITTLE LIKE SOMETHING IS BURNING IN THE FRONT OF THE CABIN. AN EMERGENCY WAS DECLARED AND A REQUESDR SIMA200515701Pitch Control · malfunctionedALB - FLT 4230 - TAKEOFF PITCH TRIM RECEIVED BY CREW DURING TAKEOFF. MAINTENANCE COMPLIED WITH OPERATIONAL CHECK IAW EMB MM AND COULD NOT DUPLICATE DISCREPANCY. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200515107Control Module · inoperativeAMA - FLT 3545 - CREW REPORTED SMOKE AND AN ELECTRICAL ODOR FROM THE FIRST OFFICERS SIDE INSTRUMENT PANEL. SHUTOFF ALL POWER AND SMOKE AND ODOR STARTED TO DISSIPATE. MAINTENANCE REPLACED TEMPERATURE CONTROL MODULE IAW EMB MM. OPERATIONAL CHECK WAS GOOD AND SDR SIMA200515702Floor Support · corrodedABI - DURING AN IMBV INSPECTION, THE LEFT OMEGA BEAM BETWEEN FRAMES 26 AND 27 WAS FOUND CORRODED. BLENDED THE DAMAGE AREA ON THE OMEGA BEAM TO REMOVED THE CORROSION. APPLIED ALODINE AND EPOXY PRIMER TO THE REWORKED AREA. FILLED THE BLENDED AREA WITH EA934NA
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