Embraer EMB-135LR
Service difficulty reports · 2,545
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 = 'EMB135LR' 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 = 'EMB135LR' 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 SIMA200529304Floor Support · corrodedA PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND CORRODED. FABRICATED REPAIR DOUBLER, FILLER AND SHIMS. REPAIR DOEN IAW SRM. (SW21200600542) (K)SDR SIMA200527713Bearing · corrodedFOUND NOSE LANDING GEAR BRACE STRUT FITTINGS HAVE MINOR CORROSION. REMOVED CORROSION ON MAIN BRACE HALF BEARINGS IAW SRM 53-11-08. FOUND TO BE ACCEPTABLE AS PER FACSIMILE REF IC2005-145/5445D. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200527712Floor Support · corrodedFOUND REPAIR DOUBLER ON LEFT OMEGA BEAM AT FRAME 20 IS CORRODED. REPLACED REPAIR DOUBLER IAW EMB SRM 53-00-10 FIGURE 201. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR CHQA200500170Battery Pack · inoperativeRIGHT FUSELAGE FORWARD EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE NR 2 FORWARD EMERGENCY LIGHT BATTERY PACK AS PER THE EMB 135 MM 33-50-04. OPS CHECK IS GOOD.SDR SIMA200528001Sill · corrodedFOUND SERVICE DOOR AFT SILL CORRODED AT FRAME 22. REPAIRED AFT SILL WITH DOUBLER REPAIR IAW SRM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200600332) (K)SDR SIMA200527711Doubler · corrodedFOUND TRIANGULAR DOUBLER PLATE THAT ATTACHES FLOOR SUPPORT AT FRAME 22 CORRODED. FABRICATED AND INSTALLED NEW DOUBLER IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200527710Doubler · corrodedFOUND RIGHT SIDE DOUBLER PLATE CORRODED AT FRAME 22. INSTALLED NEW DOUBLER PLATE IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200527709Floor Support · corrodedSAW - FOUND FLOOR SUPPORT PROFILE AT FRAME 22 RIGHT IS CORRODED. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200526901Battery · unknownEMERGENCY EXIT LIGHT FLOOR STRIP AT OVERWING EXIT DOES NOT ILLUMINATE ON TEST. REPLACED NR 3 BATTERY POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200526402Floor Support · corrodedTHE LEFT 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 TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4777 PARA 8 DATED SEPT 15, 2005. (M)SDR SIMA200526405Floor Support · corrodedTHE CENTER OMEGA BEAM BETWEEN FRAMES 24 AND 25 WAS FOUND CORRODED. PERFORMED A CUT OUT OF THE OMEGA BEAM TO REMOVE THE CORROSION. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4777 PARA 7 DATED 15, 2005. (M)SDR SIMA200525703Power Supply · dischargedBOS - FLT 4592 - EMERGENCY LIGHT STRIP AT ROW 7 AND 8 INOPERATIVE. REPLACED NR 3 EMERGENCY LIGHT POWER SUPPLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200526206Channel · corrodedTHE RIGHT HAT BEAM IN THE GALLEY WAS FOUND TO BE CORRODED. REMOVED THE CORRODED HAT BEAM. INSTALLED NEW SERVICEABLE HAT BEAM IAW EMB SRM, SRM 145/1142 REV 30 CHAPTERS 51-20-03, 51-40-02 AND EMB CPM, CPM-145/1132 REV 12, CHAPTERS 51-21-04. (M)SDR SIMA200526204Floor Support · corrodedTHE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 24 AND 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED AN EXTERNAL ANGLE, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M)SDR SIMA200526203Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED BETWEEN FRAMES 23 AND 25. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB IC2005-145/4951 DATED SEPT 8, 2005. (M)SDR C2XA05IA104Light · inoperativeLRD - FLIGHT 2359, DURING PREFLIGHT INSPECTION, THE CREW REPORTED THAT BOTH SIDE PANEL EXIT LIGHTS AT THE OVERWING EXITS WERE INOPERATIVE. THE CREW RESET THE EMERGENCY LIGHT SYSTEM, OPERATIONALLY CHECK WITH NO DEFECTS, AND THE AIRCRAFT WAS APPROVED FOR RETURNSDR SIMA20052602Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED SERVICE DOOR CENTER SILL AND INSTALLED SERVICEABLE SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-20-01, 41, 51-40-06 AND 51-40-09. (M)SDR SIMA200526205Floor Support · corrodedA PREVIOUS REPAIR ON THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-00-10 FIG 201 SHEET AND 51-40-02. (M)SDR SIMA200525502Smoke Detector · will not testAFT BAGGAGE SMOKE DETECTOR WILL NOT TEST. REPLACED SMOKE DETECTOR NR 1 IAW EMB 135 AMM 26-15-01. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200525225Battery · dischargedCLT - FLT 4892 - DURING PREFLIGHT, EMERGENCY LIGHT FROM ROW 7 FORWARD FAILED TO ILLUMINATE. REMOVED AND REPLACED NR 2 EMERGENCY LIGHT BATTERY IAW EMB AMM 33-50-04. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR SIMA200525224Light · burnedSMOKE COMING FROM FLOURESCENT LAMP FIXTURE OVER ROW 6A. REPLACED LIGHT FIXTURE AT SEAT 6A IAW EMB WM SP CH 20-21. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR CHQA200500164Bulb · burned outRIGHT HAND OVERWING EMERGENCY LIGHT IS INOPERATIVE. REMOVED AND REPLACED THE RIGHT HAND OVERWING EMERGENCY LIGHT IAW EMB 134 MM 33-50-07. OPS CHECK GOOD.SDR CHQA200500163Bulb · burned outLEFT HAND OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED OVERWING EMERGENCY LIGHT BULB IAW EMB 145 MM 33-50-07. OPS CHECK GOOD.SDR SIMA200524502Smoke · detectedBOS - FLT 4596 - DURING TAXI CREW REPORTED SMOKE IN COCKPIT BUT NOT IN CABIN. AIRCRAFT WAS RETURNED TO THE GATE. MAINTENANCE COULD NOT DUPLCIATE DISCREPANCY. A GOUND ENGINE RUN WITH BOTH ENGINES AND BOTH PACKS OPERATING WAS SATISFACTORY WITH NO SMOKE NOTED.SDR SIMA200524106Stringer · chafedA PREVIOUS REPAIR OF STRINGER 19R WAS FOUND TO BE CHAFED. REMOVED THE EXISTING REPAIR AND CLEANED THE AREA. FABRICATED A REPAIR ANGLE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 53-24-02 AND EMB IC2005-145/4506 DATED AUGUST 19, 200SDR SIMA200524101Skin · bird strikeJFK - FLT 4613 - AIRCRAFT EXPERIENCED BIRDSTRIKE ON LEFT CORNER OF WINDSHIELD. COMPLETED BIRDSTRIKE INSPECTION AND FERRIED AIRCRAFT TO SAW FOR FUSELAGE STRUCTURAL REPAIR BETWEEN FRAME 1 AND FRAME 5, FORWARD OF CAPTAINS WINDSHIELD. MAINTENANCE INSTALLED NEW FSDR C2XA05IA099Battery Pack · dischargedIAH - DURING MAINTENANCE INSPECTION, THE AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NUMBER FOUR EMERGENCY LIGHT BATTERY PACK, OPERATIONALLY CHECKED WITH NO DEFECTS NOTED, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SSDR SIMA200523509Strap · damagedWHILE SITTING ON RAMP AT EWR, A/C WAS HIT IN FORWARD RIGHT FUSELAGE SECTION BY VEHICLE. COMPLETED REPAIR TO SKIN BETWEEN FRAMES 10-13 AND STRINGER 13R TO 18R BY REPLACING DAMAGED PORTION OF SKIN (P/N 14527606007) AND INSTALLING AN EXTERNAL DOUBLER IAW EO EB-5SDR SIMA2005232403Floor Support · corrodedSAW - FOUND DURING CPCP INSPECTION, DIGITAL CORRODED AT FRAME 14 COCKPIT ENTRY. REMOVED CORROSION AND FOUND DIGITAL TO BE CRACKED. REPLACED DIGITAL IAW SRM 51-21-10. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200523405Rod · damagedFOUND DURING MBV, FORWARD END OF LOWER NR 2 RUDDER ROD HAS PLAY WHERE FORWARD FITTING SCREWS INTO ROD. REPLACED LOWER NR 2 RUDDER ROD IAW EMB AMM 27-21-08. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200523505Floor Support · corrodedTHE CENTER OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 20. REMOVED THE CORROSION BY MAKING TWO CUT OUTS. FABRICATED A REPAIR CHANNEL TO COVER BOTH CUTOUTS. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4307 DATED AUGUST 12, 2005. (M)SDR SIMA200523506Floor Support · corrodedTHE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUTOUT. FABRICATED A FILLER AND DOUBLER. REPAIR DONE IAW EMB REPAIR STATEMENT IC2005-145/4287 DATED AUGUST 11,2005. (M)SDR C2XA05TY049Stringer · damagedTYS, DURING A SCHEDULED INSPECTION, STRINGER 2L, JUST FORWARD OF FRAME 75 WAS FOUND DAMAGED. MAINTENANCE CUT OUT THE DAMAGED SECTION, FABRICATED A NEW SECTION, -J- AND -L- ANGLES, PRIMED, PAINTED AND INSTALLED IAW EMB-135/145 SRM 53-00-03 AND CPM 51-21-04/05/SDR C2XA05IA098Sign · inoperativeIAH - DURING MAINTENANCE INSPECTION, THE EMERGENCY LIGHT ON THE AFT GALLEY PARTITION WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE AFFECTED LIGHT ASSY, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.SDR SIMA200523507Floor Support · corrodedA PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORRODED PREVIOUS REPAIR. FABRICATED A DOUBLER, (EPNEM53EP54701) AND FILLER (EPNNEM53EP54703). FABRICATED A PLATE AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/114SDR SIMA200523508Floor Support · corrodedA PREVIOUS REPAIR ON THE LEFT OMEGA BEAM AT FRAME 20 WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A PLATE, FILLER, AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)SDR SIMA200523404Skin · crackedFOUND DURING MBV, RUDDER NR 2 SKIN CRACKED ON RIGHT LOWER TRAILING EDGE. REPAIRED DAMAGED SKIN ON RUDDER NR 2 IAW IC2005-145/4198A. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200523503Floor Support · corrodedTHE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED AT FRAME 25. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHIMS. REPAIR DONE IAW EMB SRM, SRM 145/1142 REV 30, CHAPTER 53-00-10. (M)SDR SIMA200523502Floor Support · corrodedA PREVIOUS REPAIR ON THE CENTER OMEGA BEAM AT FRAME 25 WAS FOUND TO BE CORRODED. ADDITIONAL CORROSION WAS FOUND ON THE CENTER OMEGA BEAM AT THE GRAPHITE CROSSBEAM. REMOVED THE PREVIOUS REPAIR AND ENLARGED THE CUT OUT. FABRICATED A DOUBLER, FILLER AND TWO SHSDR SIMA200523501Floor Support · corrodedTHE GALLEY FORWARD DIGITAL WAS FOUND TO BE CORRODED. REMOVED THE CORROSION BY MAKING A CUT OUT. FABRICATED A DOUBLER. REPAIR DONE IAW EMB REPAIR IC2005-145/4212 DATED AUGUST 10, 2005. (M)SDR SIMA200523504Sill · corrodedTHE SERVICE DOOR CENTER SILL WAS FOUND TO BE CORRODED. REMOVED THE CORRODED CENTER SILL. INSTALLED A NEW SILL IAW EMB SRM, SRM 145/1142 REV 30, CHAPTERS 51-40-02, 51-20-03, 51-40-06. (M)SDR SIMA200523401Support · corrodedSAW - FOUND DURING CPCP INSPECTION, INBOARD RAMP AT FRAME 20 CORRODED. REPLACED INBOARD RAMP AT FRAME 20 IAW EMB SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR SIMA200523402Floor Support · corrodedFOUND DURING CPCP INSPECTION, GALLEY FLOOR SUPPORT CORRODED AT FRAME 22. INSTALLED NEW GALLEY FLOOR SUPPORT AT FRAME 22 IAW SRM 51-40-02. AIRCRAFT WAS RETURNED TO SERVICE. (M)SDR C2XA05SH096Firewall · crackedSHV - DURING C-CHECK APU FIRE WALL CRACK AROUND NUT PLATE FASTENERS AT 3 O`CLOCK POSITION. MAINTENANCE REPAIRED APU FIREWALL AT 3 O`CLOCK POSITION IAW EC 5330-01483. THE AIRCRAFT WAS APPROVED TO CONTINUED FOR SERVICE.SDR C2XA05SH091Handle · detachedMAIN CABIN DOOR WILL NOT OPEN FROM INSIDE CABIN. MAINTENANCE INSTALLED MAIN CABIN DOOR INTERNAL HANDLE IAW EMB 135 AMM 52-18-05, OPS CHECK GOOD. AIRCRAFT WAS RETURNED FOR SERVICE.SDR C2XA05SH90Floor Support · corrodedSHV DURING C-CHECK LT OMEGA BEAM AT FR 24 ARE CORROED. MAINTENANCE REPAIRED LT OMEGA BEAM IAW EMB 145 SRM 53-22-10.THE AIRCRAFT WAS APPROVE TO RETURN FOR SERVICE.SDR CHQA200500131Velocity Sensor · unserviceableWHILE DESCENDING OUT OF 12,000 FT, FLAP FAIL EICAS MESSAGE ASSOCIATED WITH SPS ADV MESSAGE APPEARED ON EICAS. RAN QRH & ADJUSTED LANDING SPEEDS. NOTIFIED APPROACH CONTROL & DECLARED AN EMERGENCY. RAN CHECKLISTS, DESCENT & APPROACH. LANDING NORMAL, LONGER TSDR C2XA05BT046Inverter · faultyEWR---CO2352, CREW REPORTED, BULKHEAD EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED INVERTER BY GALLEY DOOR. OPS CHECK GOOD IAW EMB145 MM 33-50-11.SDR CHQA200500128Control Module · unserviceableFLIGHT 6385 TLH-MIA - PILOT REPORTS AFTER PULLING OFF RUNWAY, AN E2 FIRE INDICATION APPEARED ON EICAS. THE FIRST ENGINE FIRE BOTTLE WAS BLOWN AND THE INDICATION REMAINED. THE SECOND ENGINE FIRE BOTTLE WAS BLOWN AND THE INDICATION REMAINED. THE FIRE DEPT FOUSDR SIMA200520101Light · inoperativeFORWARD BULKHEAD EMERGENCY LIGHT FAILS TO ILLUMINATE. REPLACED LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)
Back to Embraer EMB-135LR