# Service difficulty reports: Embraer EMB-120RT A list on [Embraer EMB-120RT](https://openairdocs.org/model/embraer-emb-120rt.md). Newest first. General aviation reporting is voluntary. Page 1 of 107 · 5,310 reports - [SDR FAA2015120900010](https://openairdocs.org/sdr/FAA2015120900010.md): Blade · cracked · Dec 9, 2014 · N652CT · Emb EMB120RT · Propeller Blade Section > CRACK INDICATION OF FILLET RADIUS OF BLADE SHANK, FOUND DURING MAJOR INSPECTION. - [SDR GLBA2012092520121](https://openairdocs.org/sdr/GLBA2012092520121.md): Light · inoperative · Sep 25, 2012 · N96ZK · Emb EMB120RT · Emergency Lighting > EMERGENCY EXIT LIGHT IN CEILING ABOVE ROW 6 DOES NOT ILLUMINATE. - [SDR GLBA201004231](https://openairdocs.org/sdr/GLBA201004231.md): Acm · odor · Apr 22, 2010 · N108UX · Emb EMB120RT · Cabin Cooling System > PILOTS REPORTED THAT A DUCT OVERHEAT LIGHT ON THE LT SIDE ILLUMINTATED. DURING POST MX ENGINE RUNS, MX HAD NOTICED A BURNING SMELL COMING FROM THE LT PACK. MX ORIGINALLY PLACED THE ISSUE ON MEL 21-50-2 CAT.C, HOWEVER, ULTIMATELY MX R & R THE LT AIR CYCLE MACH - [SDR GLBA090706001](https://openairdocs.org/sdr/GLBA090706001.md): Skin · damaged · Jul 6, 2009 · N108UX · Emb EMB120RT · Elevator, Plate/Skin > PILOTS REPORTED THAT THEY OBSERVED LIGHTNING STRIKE DAMAGE ON THE LT ELEVATOR. MX REPAIRED THE EFFECTED AREA IAW EO 09-120-27-001. MX PERFORMED A BLEND OUT, FOUND BLENDED AREAS TO BE 2D FROM NEAREST RIVET. NO CRACKS WERE FOUND DURING NDI INSPECTION. STATIC - [SDR GLBA200906292](https://openairdocs.org/sdr/GLBA200906292.md): Seal · dirty · Jun 29, 2009 · N108UX · Emb EMB120RT · Cargo/Baggage Doors > PILOTS REPORTED THAT DURING CLIMB OUT THROUGHT 8,000 FT, CABIN PRESSURE CLIMBED IN A BRIEF SPIKE THEN NORMAL THROUGH 22,000 FT THE CABIN BEGAN TO DEPRESSURIZE. RATE NEVER WAS PEGGED. BEGAN A DESCENT TO 10,000 FT PRESSURE NORMALIZED. MX TROUBLESHOT THE ACFT - [SDR GLBA200906291](https://openairdocs.org/sdr/GLBA200906291.md): A/C Pack · smoke · Jun 29, 2009 · N96ZK · Emb EMB120RT · Cabin Cooling System > PILOTS REPORTED THAT THE AIR CONDITIONING PACK SYS PUT SMOKE IN THE CABIN UPON LANDING. SYS WORKED FINE IN THE AIR WITH BLEEDS IN AUTO AND PACKS ON LOW. MX PERFORMED OPS CHECKS ON THE LT AND RT AIR CONDITIONING SYS IN LOW AND HIGH FOR A GOOD AMOUNT OF TIME. - [SDR 2006FA0000065](https://openairdocs.org/sdr/2006FA0000065.md): Window Frame · cracked · Jan 11, 2006 · N200CD · Emb EMB120RT · Fuselage Main, Structure > PILOT`S SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LT WINDSHIELD AFT BEAM. NORMAL OPERATIONS. (K) - [SDR 2006FA0000047](https://openairdocs.org/sdr/2006FA0000047.md): Window Frame · cracked · Jan 11, 2006 · N196CA · Emb EMB120RT · Fuselage Main, Structure > PILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT LEFT WINDSHIELD AFT BEAM. NORMAL OPS. (K) - [SDR 2006FA0000046](https://openairdocs.org/sdr/2006FA0000046.md): Window Frame · cracked · Jan 11, 2006 · N200CD · Emb EMB120RT · Fuselage Main, Structure > COPILOTS SIDE WINDOW LOWER STRUCTURAL BEAM IS CRACKED AT RT WINDSHIELD AFT BEAM. NORMAL OPS. (K) - [SDR ASOA03283](https://openairdocs.org/sdr/ASOA03283.md): Wire · inoperative · Jul 3, 2003 · N240AS · Emb EMB120RT · Light System Wiring > DURING HANGAR MAINTENANCE IN MCN, THE EXIT SIGN AT SEAT ONE WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE WIRING TO THE EXIT SIGN AT SEAT ONE OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA03284](https://openairdocs.org/sdr/ASOA03284.md): Light · inoperative · Jul 3, 2003 · N240AS · Emb EMB120RT · Emergency Lighting > DURING HANGAR MAINTENANCE IN MCN, AN EMERGENCY FLOOR LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED AN EMERGENCY FLOOR LIGHT LAMP. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR SWIA200312073](https://openairdocs.org/sdr/SWIA200312073.md): Switch · malfunctioned · Jun 4, 2003 · N593SW · Emb EMB120RT · Trailing Edge Flap Control System > WHEN FLAPS 15 WERE SELECTED FCU INDICATES CONTROL FAULT WITH FLAP AND ASWS LIGHTS ON MAP. REMOVED AND REPLACED FLAP HANDLE WITH A SERVICEABLE UNIT. OPS CHECK GOOD. - [SDR ASOA03226](https://openairdocs.org/sdr/ASOA03226.md): Wire · loose · May 20, 2003 · N258AS · Emb EMB120RT · Light System Wiring > FLT 4939 - DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT EXTERIOR EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REPAIRED THE DEFECTIVE WIRE SPLICE ON THE RIGHT AFT EXTERIOR EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M - [SDR ASOA03223](https://openairdocs.org/sdr/ASOA03223.md): Windshield · separated · May 18, 2003 · N258AS · Emb EMB120RT · Flight Compartment Windows > FLT 4888 - DURING CLIMB-OUT FROM AEX-GTR, AT APPROXIMATELY 14,000 FEET THE CABIN PRESSURE BEGAN TO CLIMB AT 2,000 FEET PER MINUTE. THE AIRCRAFT DESCENDED TO 10,000 FEET DURING WHICH TIME THE CAPTIAN NOTICED A GAP HAD OCCURRED BETWEEN HIS WINDSHIELD AND THE AI - [SDR ASOA03192](https://openairdocs.org/sdr/ASOA03192.md): Bulb · burned out · May 1, 2003 · N264AS · Emb EMB120RT · Emergency Lighting > DURING A GROUND INSPECTION IN ATL, THE RIGHT EMERGENCY EXIT LIGHT AT ROW 8 B/C WAS FOND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT EMERGENCY EXIT LIGHT LAMP AT ROW 8 B/C. OPS CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA03193](https://openairdocs.org/sdr/ASOA03193.md): Light · inoperative · May 1, 2003 · N274AS · Emb EMB120RT · Emergency Lighting > DURING A GROUND INSPECTION IN DFW, THE RIGHT AFT OVERWING EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE RIGHT AFT OVERWING EMERGENCY LIGHT ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA03194](https://openairdocs.org/sdr/ASOA03194.md): Battery · inoperative · May 1, 2003 · N274AS · Emb EMB120RT · Emergency Lighting > FLT 4374 - DURING A GROUND INSPECTION IN ATL, THE EXTERIOR EMERGENCY LIGHTS WOULD NOT ILLUMINATE. MAINTENANCE REMOVED AND REPLACED THE AFT EMERGENCY LIGHT BATTEYR. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR SWIA200311895](https://openairdocs.org/sdr/SWIA200311895.md): Switch · malfunctioned · Apr 3, 2003 · N593SW · Emb EMB120RT · Trailing Edge Flap Control System > WITH FLAPS SELSECTED TO 15 DEGREES FLAP CONTROL FAULT. REMOVED AND REPLACED FLAP SELECTOR HANDLE WITH SERVICEABLE UNIT. RAN FLAPS FULL SCALE MULTIPLE TIMES. OPS CHECKS GOOD. - [SDR ASOA03143](https://openairdocs.org/sdr/ASOA03143.md): Battery Pack · inoperative · Apr 1, 2003 · N281AS · Emb EMB120RT · Emergency Lighting > DURING A GROUND INSPECTION IN DFW, THE EMERGENCY LIGHTS IN THE AFT SECTION OF THE CABIN WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHTING BATTERY PACK IN THE AFT SECTION OF THE CABIN. OPERATIONAL CHECKS GOOD. AIRCRAFT OK - [SDR ASOA03111](https://openairdocs.org/sdr/ASOA03111.md): Wire · loose · Mar 15, 2003 · N264AS · Emb EMB120RT · Engine Bleed Air System Wiring > FLT 4320 - DURING DESCENT INTO MCN FROM ATL, THE CREW RECEIVED A LT DUCT LEAK MESSAGE. THE CRE COMPLIED WITH QRH PROCEDURES AND SHUT DOWN THE LT ENGINE. AN EMERGENCY WAS DECLARED AND EMERGENCY EQUIPMENT REQUESTED. THE AIRCRAFT LANDED SAFELY IN MCN. MAINTEN - [SDR ASOA03101](https://openairdocs.org/sdr/ASOA03101.md): Battery · inoperative · Mar 10, 2003 · N258AS · Emb EMB120RT · Smoke Detection > FLT 4903 - DURING CRUISE FROM IAH-DFW, THE LAVATORY SMOKE DETECTOR GAVE RANDOM FALSE ALARMS. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA03055](https://openairdocs.org/sdr/ASOA03055.md): Window Post · cracked · Feb 12, 2003 · N280AS · Emb EMB120RT · Fuselage Main, Structure > DURING A HANGAR CHECK IN TXK, THE LT DIRECT VISUAL WINDOW POST SKIN AT THE LOWER TRAILING EDGE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M) - [SDR ASOA03051](https://openairdocs.org/sdr/ASOA03051.md): Battery · inoperative · Feb 9, 2003 · N257AS · Emb EMB120RT · Emergency Lighting > DURING A HANGAR CHECK IN MCN, THE FORWARD SEGMENT OF EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE NR 1 EMERGENCY LIGHT BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR SWIA200311775](https://openairdocs.org/sdr/SWIA200311775.md): Control Unit · malfunctioned · Feb 7, 2003 · N593SW · Emb EMB120RT · Trailing Edge Flap Control System > ON TAKEOFF THE ANALOG FLAP INDICATOR BOUNCED BACK AND FORTH BETWEEN 0-15 DEGREES, SETTING OFF THE TAKEOFF AURAL WARNING SYSTEM. ALSO, EACH TIME IT WENT TO 0 DEGREES, RECEIVED FLAP AND ADVANCED SWS WARNINGS ON THE MAP. OPERATED FLAPS SEVERAL TIMES, COULD NOT - [SDR SWIA200311705](https://openairdocs.org/sdr/SWIA200311705.md): Engine · malfunctioned · Jan 9, 2003 · N593SW · Emb EMB120RT · Engine (Turbine/Turboprop) > ON CLIMBOUT HEARD AND FELT A LOUD THUMP AND SLIGHT LOSS OF POWER ON THE LEFT ENGINE. ABOUT 30 SECONDS LATER RECEIVED AN 'OIL' MAP AND AURAL WARNING. OIL PRESSURE WAS '0'. PERFORMED PRECAUTIONARY SHUTDOWN AND RETURNED TO SEA. REMOVED AND REPLACED THE LEFT E - [SDR SWIA200311697](https://openairdocs.org/sdr/SWIA200311697.md): Actuator · malfunctioned · Jan 8, 2003 · N269UE · Emb EMB120RT · Trailing Edge Flap Actuator > FLAP LIGHT ON MAP PANEL ASSOCIATED WITH ADVANCED SWS AND CONTROL FAULT ON OVERHEAD. REPLACED LEFT NACELLE FLAP ACTUATOR PER MM 27-50-00. CYCLED FLAPS SEVERAL TIMES. ALL CHECKS GOOD. - [SDR ASOA02654](https://openairdocs.org/sdr/ASOA02654.md): Skin · cracked · Dec 31, 2002 · N283AS · Emb EMB120RT · Fuselage Main, Plate/Skin > DURING A HANGAR INSPECTION IN TXK, THE FIRST OFFICER'S WINDOW POST SKIN WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE CRACKED SKIN IAW ASA EO 120-53-0119A. (M) - [SDR ASOA02652](https://openairdocs.org/sdr/ASOA02652.md): Wire · broken · Dec 28, 2002 · N283AS · Emb EMB120RT · Emergency Lighting > FLT 4056 - DURING GROUND INSPECTION IN ATL, THE EXTEROR RIGHT AFT EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FUSE ABOVE ROWS 7 AND 8, AND ALSO REPAIRED THE BROKEN GROUND WIRE (P/N M22759-20-9) ON THE EXTERIOR RIGHT AFT E - [SDR ASOA02646](https://openairdocs.org/sdr/ASOA02646.md): Clip · cracked · Dec 26, 2002 · N238AS · Emb EMB120RT · Fuselage Miscellaneous Structure > DURING HANGAR INSPECTION IN TXK, THE SKIN SHEAR CLIP ON FRAMES 15 AND 15A WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REMOVED AND REPLACED THE SKIN SHEAR CLIP ON FRAMES 15 AND 15A IAW SRM 53-10-04. (M) - [SDR ASOA02634](https://openairdocs.org/sdr/ASOA02634.md): Stringer · cracked · Dec 19, 2002 · N258AS · Emb EMB120RT · Wing, Longeron/Stringer > DURING HANGAR INSPECTION IN TXK, THE RIGHT WING STRINGER NR 10 CLOSE TO RIB NR 3 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REPAIR THE RIGHT WING STRINGER NR 19 CLOSE TO RIB 3 IAW SRM 57-20-03. (M) - [SDR ASOA02616](https://openairdocs.org/sdr/ASOA02616.md): Battery · discharged · Nov 23, 2002 · N258AS · Emb EMB120RT · Smoke Detection > FLT 4286 - DURING CRUISE FROM AVL-ATL, THE LAVATORY SMOKE DETECTOR MALFUNCTIONED. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA02615](https://openairdocs.org/sdr/ASOA02615.md): Battery · discharged · Nov 23, 2002 · N258AS · Emb EMB120RT · Smoke Detection > FLT 4081 - DURING CRUISE FROM ATL-CSG, THE SMOKE DETECTOR IN THE LAVATORY BEGAN TO BEEP INTERMITTENTLY. MAINTENANCE REMOVED AND REPLACED THE LAVATORY SMOKE DETECTOR BATTERY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR SWIA200211497](https://openairdocs.org/sdr/SWIA200211497.md): Control Unit · malfunctioned · Nov 22, 2002 · N269UE · Emb EMB120RT · Trailing Edge Flap Control System > FLAPS HAD RT INBOARD FLAP ASYMMETRY WHEN SET FOR LANDING AND FAILED TO RETRACT AFTER LANDING (RT AND LT INBOARD). RE-RACKED FLAP CONTROL UNIT. PERFORMED FUNCTIONAL CHECK OF FLAP SYSTEM. CYCLED FLAPS SEVERAL TIMES. NO DISCREPANCIES NOTED. - [SDR SWIA200211496](https://openairdocs.org/sdr/SWIA200211496.md): Terminal · broken · Nov 21, 2002 · N269UE · Emb EMB120RT · Electrical Power System Wiring > DURING THE TAKEOFF RUN THE NR 1 GEN OFF BUS LIGHT ILLUMINATED. THE TAKEOFF WAS ABORTED. ATTEMPTED RESET PER QRH WITH NO SUCCESS. FOUND BROKEN WIRE ON NR 1 GENERATOR. REPLACED WIRE EYELET WITH SERVICEABLE UNIT AND CONNECTED TO NR 1 GENERATOR. RAN RT ENGINE - [SDR SWIA200211480](https://openairdocs.org/sdr/SWIA200211480.md): Control Unit · malfunctioned · Nov 14, 2002 · N269UE · Emb EMB120RT · Trailing Edge Flap Control System > CONTROL FAULT ON INBOARD FLAPS AFTER TRYING TO RAISE FLAPS. REMOVED AND REPLACED FLAP CONTROL UNIT. FLAPS FUNCTIONAL CHECK GOOD. - [SDR ASOA02588](https://openairdocs.org/sdr/ASOA02588.md): Controller · malfunctioned · Nov 10, 2002 · N240AS · Emb EMB120RT · Propeller Controlling System > DURING CLIMB OUT, THE LT PROPELLER SPEED REACHED 101.2 PERCENT IN A STEADY STATE. THE CREW SET THE PROPELLER SPEED TO 85 PERCENT FOR CRUISE AND THE PROPELLER SPEED BECAME NORMAL. FLIGHT IDLE WAS SELECTED AND THE PROPELLER WAS FEATHERED. THE AIRCRAFT DIVERTE - [SDR SWIA200211411](https://openairdocs.org/sdr/SWIA200211411.md): Actuator · malfunctioned · Oct 29, 2002 · N269UE · Emb EMB120RT · Trailing Edge Flap Actuator > AFTER FLAP RETRACTION ON LANDING, THE INBOARD PAIR OF FLAPS REMAINED AT 25 DEGREES. THERE WERE NO CONTROL FAULTS OR DISAGREEMENT WARNINGS. AFTER RESETTING THE SYSTEM, THE FLAPS RETRACTED. REPLACED LEFT INBOARD FLAP ACTUATOR WITH SERVICEABLE UNIT IAW MM 27-5 - [SDR SWIA200211314](https://openairdocs.org/sdr/SWIA200211314.md): Lockwasher · broken · Oct 10, 2002 · N593SW · Emb EMB120RT · Landing Gear Actuator > AFTER DEPARTURE, LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO RDM. FOUND TANG BROKEN ON LOCKING WASHER FOR LEFT MAIN LANDING GEAR ACTUATOR. REPLACED TANG WASHER AND RIGGED LEFT MAIN GEAR IAW MM 32-32-11. PERFORMED SEVERAL GEAR SWINGS WITH NO DEFECTS NOTED - [SDR SWIA200211315](https://openairdocs.org/sdr/SWIA200211315.md): Wire · missing · Oct 7, 2002 · N236SW · Emb EMB120RT · Light System Wiring > FORWARD EMERGENCY LIGHT EXIT SIGN DOES NOT ILLUMINATE. FOUND WIRE MISSING FROM REAR TERMINAL BLOCK. REINSTALLED WIRE FOR FORWARD EMERGENCY LIGHT WITH NEW HARDWARE. COMPLIED WITH OPS CHECK OF LIGHT AND FOUND OK. - [SDR SWIA200211221](https://openairdocs.org/sdr/SWIA200211221.md): Actuator · failed · Sep 11, 2002 · N1105G · Emb EMB120RT · Trailing Edge Flap Actuator > INBOARD FLAPS CONTROL FAULT FROM 15 DEGREES TO 0 DEGREES WHEN RETRACTING THEM. REPAIRED ENVIRONMENTAL SPLICE AT LEFT I/B FLAP ACTUATOR CANNON PLUG. INSPECTED WIRING AT CANNON PLUGS AND FCU. FOUND LEFT INBOARD FLAP ACTUATOR BAD. REPLACED LEFT FLAP ACTUATOR - [SDR ASOA020492](https://openairdocs.org/sdr/ASOA020492.md): A/C Pack · contaminated · Sep 8, 2002 · N232AS · Emb EMB120RT · Cabin Cooling System > DURING CLIMBOUT, A BURNING ODOR CAME FROM THE PACKS WAS EXPERIENCED. THE CAPTAIN TURNED OFF BOTH THE LT AND RT PACKS SEPARATELY AND DETERMINED THE RIGHT PACK WAS EMITTING THE SMELL. SUBSEQUENTLY THE RIGHT PACK WAS TURNED OFF FOR THE REMAINDER OF THE FLIGHT A - [SDR SWIA200211212](https://openairdocs.org/sdr/SWIA200211212.md): Valve · malfunctioned · Sep 7, 2002 · N137H · Emb EMB120RT · APU Bleed Air System > APU CAUSES SMOKE IN COCKPIT & CABIN. FOUND LCV NOT OPENING CAUSING SMELL TO COME FROM PACKS. REPLACED APU LCV, OPS CHECK GOOD. - [SDR SWIA200211202](https://openairdocs.org/sdr/SWIA200211202.md): Wire Harness · faulty · Sep 5, 2002 · N1105G · Emb EMB120RT · Landing Gear System Wiring > ON DEPARTURE FROM SFO, LANDING GEAR WOULD NOT RETRACT. ALL GREEN REMAINED ILLUMINATED & ALL REDS EXCEPT RIGHT A WERE ILLUMINATED W/GEAR HANDLE IN UP POSITION. CYCLED GEAR - SAME RESULTS. RETURNED TO SFO. PERFORMED GEAR SWING. OPS CHECKED GOOD BUT NOTICED - [SDR SWIA200211201](https://openairdocs.org/sdr/SWIA200211201.md): Engine · overtemp · Sep 2, 2002 · N196CA · Emb EMB120RT · Engine (Turbine/Turboprop) > ON CLIMBOUT (LEFT) T6 RAISED WITH POWER REDUCTION. T6 CONTINUED TO RISE TO THE POINT OF T6 WARNING. T6 FINALLY CAME DOWN TO ABOUT 684 DEGREES, PRODUCING NO TORQUE. DID A PRECAUTIONARY ENGINE SHUTDOWN. RETURNED TO LAX. REMOVED AND REPLACED LEFT ENGINE IAW - [SDR SWIA200211150](https://openairdocs.org/sdr/SWIA200211150.md): Control Box · malfunctioned · Aug 17, 2002 · N196CA · Emb EMB120RT · Landing Gear Retraction/Extension System > LEFT LANDING RED LIGHTS REMAIN ON (A & B) WITH GEAR HANDLE SELECTED. INSTALLED SERVICEABLE LANDING GEAR RELAY BOX ASSY, SWUNG LANDING GEAR 35 PLUS TIMES. OPS CHECKS GOOD. - [SDR ASOA02451](https://openairdocs.org/sdr/ASOA02451.md): Light · inoperative · Aug 15, 2002 · N244AS · Emb EMB120RT · Emergency Lighting > DURING A HANGAR INSPECTION IN MCN, THE CEILING EMERGENCY LIGHT AT ROW 2 WAS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BURNED OUT CEILING EMERGENCY LIGHT BULB. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) - [SDR ASOA02449](https://openairdocs.org/sdr/ASOA02449.md): Proximity Sensor · failed · Aug 12, 2002 · N232AS · Emb EMB120RT · Landing Gear Position and Warning > WHILE WAITING TO TAXI, THE CAPTAIN RECEIVED AN ELECTRONIC CAPTION WITH NO ASSOCIATED ALARM LIGHT. SHORTLY AFTER THAT THE FIRST OFFICER REPORTED SMOKE. THE CAPTAIN ATTEMPTED TO TAXI THE AIRCRAFT TO THE GATE, BUT THE STICK SHAKER WENT OFF AND NEITHER NOSE WHEE - [SDR SWIA200211112](https://openairdocs.org/sdr/SWIA200211112.md): Warning System · false activation · Aug 6, 2002 · N269UE · Emb EMB120RT · Central Warning > ON TAKEOFF GOT TRIPLE CHIME EEC WARNING. ABORTED TAKEOFF. SUSPECT LEFT EEC THE CULPRIT, LOWER NP THAN RT ON FFOD. INSPECTED CANNON PLUGS AND WIRING FOR CHAFING ON LT ENGINE EEC. RAN ENGINE FOR TRIM CHECK AND TAXIED AIRCRAFT. COULD NOT DUPLICATE. OPS CHEC - [SDR ASOA02440](https://openairdocs.org/sdr/ASOA02440.md): Seat · out of position · Aug 4, 2002 · N280AS · Emb EMB120RT · Passenger Compartment Equipment > DURING HANGAR INSPECTION IN MCN, THE EMERGENCY EXIT DOORS AT ROWS 5 AND 8 WERE INHIBITED FROM OPENING. MAINTENANCE FOUND THE EXIT AT ROW 5 WAS OPENING AGAINST THE SEAT BACK AT ROW 4A. MAINTENANCE REPOSITIONED THE SEAT FOR SUFFICIENT CLEARANCE OF THE EXIT DOO - [SDR ASOA02438](https://openairdocs.org/sdr/ASOA02438.md): Fitting · cracked · Aug 2, 2002 · N240AS · Emb EMB120RT · Trailing Edge Flaps > DURING HANGAR MAINTENANCE IN TXK, THE RIGHT WING OUTBOARD FLAP OUTBOARD END CLOSURE FITTING WAS FOUND CRACKED. MAINTENANCE REMOVED AND REPLACED THE RIGHT OUTBOARD FLAP ASSEMBLY. OPERATIONAL CHECKS GOOD. AIRCRAFT OK FOR SERVICE. (M) Next page: https://openairdocs.org/model/embraer-emb-120rt/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 = 'EMB120RT' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/embraer-emb-120rt/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.