# Service difficulty reports: Embraer EMB-135ER

A list on [Embraer EMB-135ER](https://openairdocs.org/model/embraer-emb-135er.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 10 · 465 reports

- [SDR FJTA2026072716502](https://openairdocs.org/sdr/FJTA2026072716502.md): Windshield · cracked · Jul 26, 2026 · N16502 · Emb EMB135ER · Flight Compartment Windows
  > WHILE CLIMBING THROUGH FL220 THE OUTER PANE OF THE FIRST OFFICER'S WINDSHIELD SHATTERED. THIS WINDSHIELD WAS RECENTLY REPLACED ON 7/18/2026 WITH AN OVERHAULED UNIT. TAT AT REPLACEMENT WAS 23586.9 AND TAC 25141.
- [SDR FJTA202407265111](https://openairdocs.org/sdr/FJTA202407265111.md): Windshield · cracked · Jul 24, 2024 · N16511 · Emb EMB135ER · Flight Compartment Windows
  > 7/24/2024 - FLT VTE3348 - CREW REPORTED THAT CAPT WINDSHIELD BROKE UPON LEVELING AT FL290. RETURNED TO KPHX. MAITNENANCE REMOVED AND REPLACED THE WINDSHIELD IAW EMB135 AMM PROCEDURES. OPS CHECKED GOOD.
- [SDR 4DPA2024013000001](https://openairdocs.org/sdr/4DPA2024013000001.md): Proximity Switch · out of adjust · Jan 30, 2024 · N265JX · Emb EMB135ER · Landing Gear Position and Warning
  > CREW REPORTED; AFTER TO, CALLED POSITIVE RATE, GEAR UP, WE RECEIVED A LDG GEAR AIR/GND FAIL. GEAR INDICATED 3 WHITE, UP. AT 500, CALLED FOR AP AND AURAL WARNINGS FOR FLAPS AND TRIM FAIL BEGAN. ASKED FOR DELAY VECTORS TO TROUBLESHOOT. AS WE LEVELED AT 7000MSL,
- [SDR 4DPA2023042100002](https://openairdocs.org/sdr/4DPA2023042100002.md): Switch Panel · failed · Apr 21, 2023 · N268JX · Emb EMB135ER · Electrical Power System
  > ISSUE-CREW REPORTED LOSS OF ALL GENERATORS, ISIS, ALL SCREENS EXCEPT PFD1, PFD1 HAD NUMEROUS CAUTION FLAGS, CREW RAN QRH WITH NO HELP DECIDED TO STOP CLIMB AT ABOUT FL280. THE PILOT DECLARED AN EMERGENCY AND BRIEFED FA AND PASSENGERS. CONTINUED ONTO PHX AND LA
- [SDR 4DPA2023042100001](https://openairdocs.org/sdr/4DPA2023042100001.md): Computer · failed · Apr 21, 2023 · N265JX · Emb EMB135ER · Attitude and Direction Data System
  > ISSUE-CREW REPORTED SPS ADVANCE AND AHRS 2 FAIL MESSAGES. AP ALSO INOP IN FLIGHT. CORR ACTION- MX TROUBLESHOT THE ISSUE TO A BAD AHRS #2 COMPUTER. R&R'D AHRS COMPUTER ALL OPS TEST CHECKED GOOD.
- [SDR 4DPA202303260002](https://openairdocs.org/sdr/4DPA202303260002.md): Controller · failed · Mar 26, 2023 · N268JX · Emb EMB135ER · Cabin Pressure Controller
  > ISSUE-CREW REPORTED LOSS CABIN ALTITUDE INDICATION IS IN THE CLIMB, STOPPED AT 10,000 THEN LOST ALL CABIN INDICATIONS WITH ORANGE DASHES AND CABIN RATE WAS 0.CORR ACTION- MX TROUBLESHOT TO BAD DIGITAL CONTROLLER SWAPPED THE CONTROLLER ALL OPS TESTS GOOD.
- [SDR 4DPA2022111400001](https://openairdocs.org/sdr/4DPA2022111400001.md): Control Module · failed · Nov 14, 2022 · N265JX · Emb EMB135ER · Cabin Cooling System
  > ISSUE-CREW REPORTED PACK1 FAIL AND PACK 2 OVERHEAT ON CLIMB OUT AND RTF TO LAS. CORR ACTION-MX TROUBLESHOT TO BAD TEMP CONTROL MODULE AND BAD #2 PUSHBUTTON SWITCH OPS TESTED GOOD.
- [SDR 4DPA2022061600002](https://openairdocs.org/sdr/4DPA2022061600002.md): Windshield · cracked · Jun 16, 2022 · N265JX · Emb EMB135ER · Window/Windshield System
  > LEFT SIDE WINDSHIELD OUTER PANE SHATTERED DURING DESCENT AT ABOUT FL 250 +/- CREW DECLARED AND EMERGENCY AND LANDED NO FURTHER ISSUES REPORTED. CORR ACTION- R&R'D PILOT WINDSHIELD ALL LK & OPS TESTS GOOD.
- [SDR 4DPA2022052100001](https://openairdocs.org/sdr/4DPA2022052100001.md): None · none · May 21, 2022 · N268JX · Emb EMB135ER · Passenger/Crew Doors
  > CREW REPORTED HIGH PITCH NOISE FROM COCKPIT, SOUNDS LIKE AIR ESCAPING DURING CLIMB. CREW RTF TO PHX. MX DISCOVERED HARDWARE ON MED SILL IMPROPERLY INSTALLED, REMOVED AND CORRECTLY INSTALLED HARDWARE PRESSURIZATION CHECK GOOD NO LEAKS FOUND.
- [SDR ASOA201703314015](https://openairdocs.org/sdr/ASOA201703314015.md): Floor Support · corroded · Mar 31, 2017 · N16502 · Emb EMB135ER · Fuselage Miscellaneous Structure
  > DURING A MAINTENANCE INSPECTION, THE LEFT OMEGA BEAM WAS FOUND TO BE CORRODED BEYOND LIMITS. MAINTENANCE PERFORMED AN INSERTION REPAIR ON THE AFFECTED BEAM, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 7GMB2013082300001](https://openairdocs.org/sdr/7GMB2013082300001.md): Unknown · odor · Aug 22, 2013 · N325JF · Emb EMB135ER · Air Distribution System
  > 30 MINUTES BEFORE LANDING, DETECTED AN ELECTRICAL BURNING ODOR THROUGHT ENTIRE CABIN. TURNED OFF PC POWER SYS IMMEDIATELY AND ODOR SLOWLY WENT AWAY. F/A COULD NOT PINPOINT WHERE THE ODOR WAS COMING FROM. AFTER TURNING PC POWER OFF, GEN 1, 3, 2, AND 4 LOADS W
- [SDR ASOA20130814209V](https://openairdocs.org/sdr/ASOA20130814209V.md): Beam · corroded · Aug 14, 2013 · N12528 · Emb EMB135ER · Fuselage Main, Structure
  > DURING SCHEDULED MX, THE CARGO DOOR CUTOUT LOWER BEAM WAS FOUND TO BE CORRODED. MX R & R THE BEAM IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR 7GMB0201306244991](https://openairdocs.org/sdr/7GMB0201306244991.md): Flex Hose · chafed · Jun 20, 2013 · N325JF · Emb EMB135ER · Hydraulic System, Main
  > ON DESCENT AT 14,000FT, HYD 2 QTY LOW MESSAGE APPEARED, THEN FOLLOWED SHORTLY BY ENG 2 HYD PUMP FAIL MESSAGE. THE CREW DIVERTED DUE TO RUNWAY REQUIREMENT AND LANDED SAFELY. DURING VISUAL INSPECTION, PN 145-31063-409 HOSE FROM NR 2 ENGINE DRIVEN HYDRAULIC PUMP
- [SDR 7GMB2013006186181](https://openairdocs.org/sdr/7GMB2013006186181.md): Tube · broken · Jun 15, 2013 · N325JF · Emb EMB135ER · Air Intake Anti/De-Ice System
  > NR 1 ENGINE ANTI-ICE PRESSURE TRANSDUCER TUBE FOUND BROKEN AT TRANSDUCER AND ENGINE AIR INTAKE ANTI-ICE DUCT. R & R WITH NEW. OPS CHECKED GOOD.
- [SDR 7GMB201306070466](https://openairdocs.org/sdr/7GMB201306070466.md): Controller · failed · Jun 7, 2013 · N926FM · Emb EMB135ER · Windshield/Door Rain/Ice Removal
  > WINDSHIELD HEAT NR 2 FAIL MESSAGE APPEARED WHEN SELECTED ON DURING DESENT. ELECTRIC BURNING SMELL SHORTLY AFTER. FOLLOWED QRH PROCEDURES AND PERFORMED A NORMAL APPROACH AND LANDING. FOUND WINDOW HEAT CONTROLLER TO BE FAILED. PLACED WINDOW HEAT SYS ON MEL
- [SDR ASOA20130518157](https://openairdocs.org/sdr/ASOA20130518157.md): Light · inoperative · May 17, 2013 · N17524 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE CHECK THE NR 4 EMERGENCY PROXIMITY LIGHT STRIP WAS FOUND TO BE INOPERATIVE. MX R & R THE DEFECTIVE LIGHT STRIP IAW AMM 33-50-12. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR ASOA20130423154](https://openairdocs.org/sdr/ASOA20130423154.md): Drag Angle · cracked · May 10, 2013 · N11526 · Emb EMB135ER · Vertical Stabilizer, Attach Fittings
  > DURING A-CHECK, THE RT VERTICAL STABILIZER TO FUSELAGE DRAG ANGLE WAS FOUND TO BE CRACKED AT FRAME 76, STRINGER 1R. MX R & R THE ANGLE IAW SRM 51-40-02. THE ACFT WAS APPROVED FOR RETURN TO SERVICE.
- [SDR SIMA20121228005](https://openairdocs.org/sdr/SIMA20121228005.md): Battery · discharged · Dec 28, 2012 · N723AE · Emb EMB135ER · Emergency Lighting
  > EMERGENCY PANEL LIGHT IN FRONT OF ROW 3BC IS INOP. REMOVED AND REPLACED BATTERY NR 2 AND EMERGENCY BATTERY NR 2 CHARGER IAW AEWC 33-700-19. PERFORMED EMERGENCY LIGHTS OPS CHECK IAW AEWC 33-700-17. OPS CHECK GOOD. NO DEFECTS NOTED.
- [SDR I06B2012113641](https://openairdocs.org/sdr/I06B2012113641.md): Panel · defective · Nov 9, 2012 · N486TM · Emb EMB135ER · Engine Cranking
  > AFTER NR 1 ENGINE START, NR 1 ENGINE FAILED (SHUTDOWN) WHEN NR 1 FADEC SWITCH WAS CYCLED FROM RESET/ALTN. PERFORMED EMB135 FIM 72-00-00-810-805-A FOR ENGINE SHUTDOWN AFTER FADEC ALTN SELECTED, ROLLS-ROYCE FIM 72-00-00-810-811 FOR OBSERVED FAULT ENGINE SHUTDOW
- [SDR I06B2012114991](https://openairdocs.org/sdr/I06B2012114991.md): Gcu · malfunctioned · Nov 6, 2012 · N325JF · Emb EMB135ER · AC Regulator
  > GEN 3 OFF BUS ON TAXI IN AFTER SHUTDOWN OF NR 2 ENGINE. SMELL OF SMOKE IN THE COCKPIT. PERFORMED FIM 21-20-00-810-801-A FOR SMELL OF SMOKE IN THE CABIN COCKPIT. NO ABNORMAL SMELL NOTED AT THIS TIME. AC RELEASED IAW MEL 24-31-01-2 CTRL # 768504B09. PLACARD
- [SDR I06B201210233641](https://openairdocs.org/sdr/I06B201210233641.md): Unknown · malfunctioned · Oct 23, 2012 · N486TM · Emb EMB135ER · Fuel Controlling System
  > ON DESCENT AT FL 250 NR 2 ENGINE THRUST WAS FLUCTUATING. THROTTLES WERE STEADY AND SET APPROX 1/3 OF TRAVEL FROM IDLE POSITION. YAWING WAS EXPERIENCED AND ITT WAS FLUCTUATING SIGNIFICANTLY AND ENTERED YELLOW BAND. DID NOT GET A CHANCE TO OBSERVE N1 OR N2 RE
- [SDR I06B201209274992](https://openairdocs.org/sdr/I06B201209274992.md): Wire · broken · Sep 26, 2012 · N325JF · Emb EMB135ER · Light System Wiring
  > 3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 3RD EMERGENCY FLOOR PROXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NO
- [SDR I06B201209274991](https://openairdocs.org/sdr/I06B201209274991.md): Wire · broken · Sep 26, 2012 · N325JF · Emb EMB135ER · Light System Wiring
  > 2ND EMERGENCY FLOOR PROXIMITY STRIP LIGHT INOP, CONNECTOR WIRES BROKEN AT BASE. REMOVED DEFECTIVE UNIT AND INSTALLED SERVICEABLE (NEW) 2ND EMERGENCY FLOOR POXIMITY STRIP LIGHT IAW EMB135 AMM TASK 33-50-12-000/400-801-A. OPS CHECK GOOD, NO FURTHER DEFECTS NOT
- [SDR I06B201208153641](https://openairdocs.org/sdr/I06B201208153641.md): Actuator · leaking · Aug 15, 2012 · N486TM · Emb EMB135ER · Drag Control Actuator
  > DURING CLIMB THROUGH 17,000 FEET HYD1 LOW QTY MESSAGE WAS DISPLAYED ON EICAS. UPON LANDING AT PDX AND SERVICING OF THE NR 1 HYDRAULIC SYSTEM A LEAK WAS IDENTIFIED AT THE RIGHT INBOARD SPOILER ACTUATOR TOP HOSE FITTING. REPLACEMENT OF O-RING PART NUMBER NAS16
- [SDR I06B201207094671](https://openairdocs.org/sdr/I06B201207094671.md): Unknown · noisy · Jul 9, 2012 · N386CH · Emb EMB135ER · Nose/Tail Landing Gear
  > CREW HEARD AN UNUSUAL NOISE ON GEAR RETRACTION FOLLOWING TAKEOFF, AND ELECTED TO MAKE A PRECAUTIONARY LANDING TO INVESTIGATE AT THE DEPARTURE AIRPORT. PASSENGERS WERE DEPLANED, NOSE WHEEL ASSEMBLIES CHANGED WITH OVERHAULED UNITS AND A VERIFICATION FLIGHT COND
- [SDR I06B201206274672](https://openairdocs.org/sdr/I06B201206274672.md): Filter · unknown · Jun 27, 2012 · N325JF · Emb EMB135ER · Engine Fuel Distribution
  > ON TAKEOFF ROLL "E1 FUEL IMPENDING BYPASS" MESSAGE WAS DISPLAYED ON EICAS. THE CREW ABORTED THE TAKEOFF AND RETURNED TO THE GATE. MAINTENANCE PERFORMED THE PROCEDURES PER THE EMB135 AMM AND REPLACED THE FILTER ELEMENT. NO VISUAL CONTAMINATION WAS FOUND IN T
- [SDR I06B20120416001](https://openairdocs.org/sdr/I06B20120416001.md): Uplock · failed · Apr 16, 2012 · N829RN · Emb EMB135ER · Landing Gear Retraction/Extension System
  > ON GEAR UP, RECEIVED MLG LEVER DISAGREE MESSAGE AND RT MLG NOT LOCKED INDICATION. CYCLED MLG AND RECEIVED SAME INDICATIONS. EXTENDED MLG AND RETURNED TO BASE NORMALLY. TROUBLESHOOTING REVEALED A FAILED RT MLG UPLOCK ASSY. UPLOCK REPLACED AND TESTED IAW MM
- [SDR 2012FA0000066](https://openairdocs.org/sdr/2012FA0000066.md): Static Inverter · inoperative · Jan 23, 2012 · N948AL · Emb EMB135ER · AC Inverter
  > STATIC INVERTER FAILED TO OPERATE. SYS POWERS THE EGPWS AND TCAS SYS, AND IS SOLE SOURCE OF POWER FOR THESE SYS.
- [SDR 2012FA0000060](https://openairdocs.org/sdr/2012FA0000060.md): Warning Message · illuminated · Jan 18, 2012 · N486TM · Emb EMB135ER · Central Display
  > CAPTAINS DISPLAY UNIT DU FAN FAIL MESSAGE APPEARED ON EICAS.
- [SDR I06B2010 01 18 JF](https://openairdocs.org/sdr/I06B2010%2001%2018%20JF.md): Engine · contaminated · Jan 18, 2010 · N325JF · Emb EMB135ER · Engine (Turbine/Turboprop)
  > AFTER TAKEOFF AT APPROX 400 FT, PILOTS RECEIVED "LAV SMOKE" EICAS INDICATION. DECLARED EMERGENCY & RETURNED FOR LANDING AT DEPARTURE. ACFT GROUNDED UNTIL MX DETERMINES ROOT CAUSE. F/A INVESTIGATED ACFT LAV - OBSERVING NO FUMES OR SMOKE. ONCE ON THE GROUND
- [SDR 2009FA0000918](https://openairdocs.org/sdr/2009FA0000918.md): Ring · corroded · Sep 2, 2009 · Emb EMB135ER · Engine (Turbine/Turboprop)
  > (16) OF THE ATTACHMENT RINGS THAT SECURE THE ENGINE INLET TO THE ENGINE, HAVE CORROSION IN ALL ATTACH HOLES. THESE RINGS WERE LOCATED IN A REPAIR STATION. (K)
- [SDR I06B20090501FM](https://openairdocs.org/sdr/I06B20090501FM.md): Panel · inactive · Apr 30, 2009 · N926FM · Emb EMB135ER · Passenger Compartment Equipment
  > ON CLIMB OUT, THROUGH APPROX 17,000, FLT ATTENDANT REPORTED THAT WHEN THE PC-POWER SYSTEM WAS TURNED ON, 1 PASSENGER MOMENTARILY SMELLED A FAINT ODOR, WHICH CAME & WENT QUICKLY, SMELLING LIKE ELECTRICAL SMOKE. NO OTHER PASSENGER IN THE AREA NOTED THE ODOR, NO
- [SDR I06B2009 02 06 TM](https://openairdocs.org/sdr/I06B2009%2002%2006%20TM.md): Thrust Reverser · defective · Feb 6, 2009 · N486TM · Emb EMB135ER · Engine Thrust Reverser
  > CONDUCTED ABORTED TAKEOFF AT APPROX 80 " 90 KIAS DUE TO EICAS MESSAGE " ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECELERATION. COULD NOT DUPLICATE THE EICAS "ENG 1 REV DISAGREE" MESSAGE. RETURNED TO THE GATE FOR FURTHE
- [SDR I06B20090206TM](https://openairdocs.org/sdr/I06B20090206TM.md): Warning System · activated · Feb 6, 2009 · N486TM · Emb EMB135ER · Engine Thrust Reverser
  > CONDUCTED ABORTED TAKEOFF AT APPROXIMATELY 80-90 KIAS DUE TO EICAS MESSAGE "ENG 1 REV DISAGREE". COMPLIED WITH ABORT PROCEDURE. MESSAGE DISAPPEARED DURING DECELERATION. COULD NOT DUPLICATE THE EICAS "ENG 1 REV DISAGREE" MESSAGE. RETURNED TO THE GATE FOR F
- [SDR I06B20081030001](https://openairdocs.org/sdr/I06B20081030001.md): Door · damaged · Oct 30, 2008 · N926FM · Emb EMB135ER · Landing Gear Doors
  > 14K FT NOTICED A FLASH OF LIGHT THAT APPEARED TO BE BELOW THE AIRCRAFT. THE CREW REPORTED NO AIRCRAFT ANOMALIES AS A RESULT OF THE SUSPECTED NEAR LIGHTNING STRIKE. FO PERFORMED THE POST FLT INSP AND IMMEDIATELY NOTICED A PIN HOLE IN THE NOSE GEAR DOOR. CAPT
- [SDR C2XA08CL092](https://openairdocs.org/sdr/C2XA08CL092.md): Apu · faulty · Aug 5, 2008 · N27506 · Emb EMB135ER · APU Core Engine
  > CLE FLIGHT 2630 - THE CREW REPORTED A LAV SMOKE WARNING MESSAGE ON THE EICAS AFTER SELECTING COOLING PACKS DURING TAXI. THE ACFT RETURNED TO THE GATE WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE APU. OPERATIONAL CHECKS WERE GOOD. (S)
- [SDR C2XA08RI103](https://openairdocs.org/sdr/C2XA08RI103.md): Light · defective · Jul 16, 2008 · N16511 · Emb EMB135ER · Passenger Compartment Lighting
  > FLIGHT 2513 -EWR- FLIGHT CREW REPORTED ELECTRICAL BURNING ODOR IN FORWARD CABIN. EWR MX REMOVED AND REPLACED PASSENGER CABIN LIGHT AT ROW 1A AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. ACFT WAS APPROVED TO RETURN TO SERVICE. (S)
- [SDR C2XA08CL072](https://openairdocs.org/sdr/C2XA08CL072.md): Light · inoperative · Jun 17, 2008 · N14505 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE NR 2 EMERGENCY AISLE PATH LIGHT STRIP WAS FOUND INOPERATIVE. MAINTENANCE REPLACED THE NR 2 EMERGENCY LIGHT STRIP. OPERATIONAL CHECKS WERE GOOD. (S)
- [SDR C2XA08CL071](https://openairdocs.org/sdr/C2XA08CL071.md): Carbon Seal · leaking · Jun 15, 2008 · N14508 · Emb EMB135ER · Turbine Engine Oil System
  > CLE FLIGHT 2290. THE CREW REPORTED ON SHORT FINAL RECEIVED AN ENG 2 LOW OIL PRESSURE WARNING MESSAGE. THE ENG WAS SHUT DOWN BY THE CREW IMMEDIATELY AFTER LANDING. MAINTENANCE INSPECTED AND FOUND MAJOR OIL LEAK AT THE REAR OF THE ENG. THE NR 2 ENG WAS REPLA
- [SDR C2XA08RI070](https://openairdocs.org/sdr/C2XA08RI070.md): Module · inaccurate · May 12, 2008 · N16502 · Emb EMB135ER · Landing Gear Steering System
  > FLIGHT 1202 - EWR - FLIGHT CREW REPORTED STEERING PULLED TO LEFT AND SHAKING LEFT & RIGHT. CREW RETURNED AIRCRAFT TO GATE. EWR MX REMOVED AND REPLACED HYDRAULIC MODULE (STEERING MANIFOLD) AND PERFORMED OPERATIONAL CHECKS SUCCESSFULLY. AIRCRAFT WAS APPROVED
- [SDR C2XA08RI067](https://openairdocs.org/sdr/C2XA08RI067.md): Smoke Detector · false activation · May 11, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVE
- [SDR C2XA08RI061](https://openairdocs.org/sdr/C2XA08RI061.md): Smoke Detector · loose · May 2, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 2424 - BAG SMOKE WARNING IN FLIGHT, BOTH LIGHTS AND EICAS MESSAGES STAYED FOR FEW SECONDS THEN WENT OFF. MX RESECURED LOOSE CONNECTOR PLUG AT AFT SMOKE DETECTOR AND PERFORMED OPERATIONAL CHECK SUCCESSFULLY. AIRCRAFT WAS APPROVED TO RETURN TO SERVICE.
- [SDR C2XA08CL053](https://openairdocs.org/sdr/C2XA08CL053.md): Wire · chafed · May 1, 2008 · N16502 · Emb EMB135ER · APU System Wiring
  > CLE FLIGHT 2419 - THE CREW REPORTED A APU FIRE DETECT FAIL MESSAGE INTERMITTENTLY DURING FLIGHT. MAINTENANCE INSPECTED AND REPAIRED A CHAFED WIRE ON THE APU HARNESS. PERFORMED OPERATIONAL CHECKS OF THE SYSTEM.
- [SDR C2XA08CL044](https://openairdocs.org/sdr/C2XA08CL044.md): Light · inoperative · Apr 5, 2008 · N25504 · Emb EMB135ER · Emergency Lighting
  > DURING ROUTINE MAINTENANCE THE EMERGENCY LIGHT STRIP AT ROW 3 & 4 FAILED OPERATIONAL CHECK. MAINTENANCE INSPECTED AND REPLACED THE FLOOR PROXIMITY LIGHT STRIP AT ROW 3 & 4. OPERATIONAL CHECKS WERE GOOD.
- [SDR CA080314007](https://openairdocs.org/sdr/CA080314007.md): Engine · leaking · Mar 12, 2008 · Emb EMB135ER · Turbine Engine Oil System
  > OIL IMPENDING BYPASS INDICATION ILLUMINATED ALONG WITH OIL TEMPERATURE RISING TO 141 DEGREES. THE PILOT COMMANDED THE SHUT DOWN OF THE ENGINE DUE TO OIL TEMPERATURE AND QUANTITY INDICATING THREE QUARTS. AIRCRAFT RETURNED TO CMH WITHOUT INCIDENT. MAGNETIC IN
- [SDR C2XA08CL014](https://openairdocs.org/sdr/C2XA08CL014.md): Module · defective · Jan 29, 2008 · N15509 · Emb EMB135ER · Fuel Control/Turbine Engines
  > DAY FLIGHT 2382 - THE CREW REPORTED 10 MINUTES INFLIGHT IN CLIMB MODE THE NR 2 ENGINE POWERED BACK TO FLIGHT IDLE UNCOMMANDED. THE AIRCRAFT DIVERTED TO CLE AND LANDED WITHOUT INCIDENT. MAINTENANCE INSPECTED AND REPLACED THE NR 2 ENGINE FADEC 2A RESISTOR MODU
- [SDR C2XA08RI068](https://openairdocs.org/sdr/C2XA08RI068.md): Smoke Detector · intermittent · Jan 11, 2008 · N16502 · Emb EMB135ER · Smoke Detection
  > FLIGHT 3096 - EWR - FLIGHT CREW REPORTED BAGGAGE EXTINGUISH WARNING LIGHT ILLUMINATED IN FLIGHT INTERMITTENTLY. ALSO, INTERMITTENT BAGGAGE SMOKE WARNING ON EICAS, BUT DISAPPEARED AFTER 1 SECOND. CREW PROCEEDED WITH EMERGENCY DESCENT AND LANDED AIRCRAFT UNEVE
- [SDR C2XA08CL007](https://openairdocs.org/sdr/C2XA08CL007.md): Fire Detector · failed · Jan 10, 2008 · N27506 · Emb EMB135ER · Fire Detection
  > YOW FLIGHT 2762 - THE CREW REPORTED AN APU FIRE DETECT FAIL MESSAGE INFLIGHT WITH APU OFF. MAINTENANCE INSPECTED AND REPLACED THE APU FIRE DETECTOR. OPERATIONAL CHECKS WERE GOOD.
- [SDR C2XA08TY004](https://openairdocs.org/sdr/C2XA08TY004.md): Charger · inoperative · Jan 9, 2008 · N27506 · Emb EMB135ER · Emergency Lighting
  > OVERWING EMERGENCY LIGHTS INOP. REMOVED AND REPLACED NR 4 EMERGENCY LIGHT BATTERY CHARGING BASE IAW EMB135 AMM 33-50-04. OPS CHECK GOOD, AIRCRAFT RELEASED AND RETURNED TO SERVICE.
- [SDR C2XA08TY005](https://openairdocs.org/sdr/C2XA08TY005.md): Fairing · damaged · Jan 8, 2008 · N27506 · Emb EMB135ER · Aerodynamic Fairings
  > LEFT WING TO FUSELAGE FAIRING 193 GROUND DAMAGE REPAIR. PERFORMED PLY RESTORATION TO EACH SKIN, ONE AT A TIME INCLUDING CORE REPLACEMENT. EXPOXY PRIME AND FINISH PAINT REPAIR. REPAIR ACCOMPLISHED IAW EC5350-01104. EMB IC2008-145/00110; ENGINEERING PROJECT

Next page: https://openairdocs.org/model/embraer-emb-135er/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'EMB135ER'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-emb-135er/reports

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