# Service difficulty reports: N190SW, cancelled Mar 22, 2006 A list on [N190SW, cancelled Mar 22, 2006](https://openairdocs.org/deregistered/N190SW-2006-03-22.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 106 reports - [SDR SWIA200515947](https://openairdocs.org/sdr/SWIA200515947.md): Actuator · malfunctioned · Dec 4, 2005 · N190SW · Emb EMB120ER · Rudder Control System > RT RUDDER JAMMED AFTER TAKEOFF. REPLACED LOWER RUDDER ACTUATOR AND RIGGED IAW MM 27-22-02 AND 27-20-00. OPERATIONAL CHECK GOOD. - [SDR SWIA200515399](https://openairdocs.org/sdr/SWIA200515399.md): Actuator · malfunctioned · Aug 2, 2005 · N190SW · Emb EMB120ER · Trailing Edge Flap Actuator > AFTER ADDING FLAPS TO 25 DEGREES ON FINAL APPROACH, NOTICED RIGHT ROLLING TENDANCY. REPLACED RIGHT OUTBOARD FLAP ACTUATOR. OPERATIONAL CHECK GOOD IAW MM 27-50-00. - [SDR SWIA200514800](https://openairdocs.org/sdr/SWIA200514800.md): Wire · broken · Mar 29, 2005 · N190SW · Emb EMB120ER · Light System Wiring > EXIT SIGN ABOVE F/A JUMPSEAT WILL NOT ILLUMINATE. REPAIRED BROKEN WIRE AT FIXTURE, OPERATIONAL CHECK GOOD. - [SDR SWIA200514729](https://openairdocs.org/sdr/SWIA200514729.md): Wire · broken · Mar 14, 2005 · N190SW · Emb EMB120ER · Light System Wiring > EMERGENCY EXIT LIGHT AT ROW 9 OVERHEAD INOPERATIVE. REPAIRED BROKEN WIRE AT OVERHEAD BIN AT 9A FOR EMERGENCY EXIT LIGHT AS REQUIRED. OPERATIONAL CHECK GOOD. - [SDR SWIA200514669](https://openairdocs.org/sdr/SWIA200514669.md): Light · inoperative · Mar 3, 2005 · N190SW · Emb EMB120ER · Emergency Lighting > AFT SECTION OF EMERGENCY LIGHTS WILL NOT ILLUMINATE. REPLACED AFT OVERHEAD LIGHT SOCKET AS NECESSARY, OPERATIONAL CHECK GOOD. - [SDR SWIA200414310](https://openairdocs.org/sdr/SWIA200414310.md): Selector · faulty · Dec 24, 2004 · N190SW · Emb EMB120ER · Trailing Edge Flap Control System > WHEN FLAP LEVER WAS MOVED, CONTROL FAULT MESSAGE. REMOVED AND REPLACED FLAP SELECTOR IAW EMB MM 22-50-01. OPERATIONAL CHECK GOOD. - [SDR SWIA200414305](https://openairdocs.org/sdr/SWIA200414305.md): Actuator · malfunctioned · Dec 21, 2004 · N190SW · Emb EMB120ER · Trailing Edge Flap Actuator > RECEIVED CONTROL FAULT ON APPROACH WHEN SELECTING FLAPS 25 DEGREES. REMOVED AND REPLACED RIGHT INBOARD, RIGHT NACELLE, AND RIGHT OUTBOARD FLAP ACTUATORS IAW EMB MM 27-50-00. OPERATIONAL CHECK GOOD. P/N 308200-1005, S/N 0091 AND S/N 0834, P/N 320300-1007, S/ - [SDR SWIA200413862](https://openairdocs.org/sdr/SWIA200413862.md): Lamp · burned out · Sep 28, 2004 · N190SW · Emb EMB120ER · Emergency Lighting > FRONT CABIN EXIT LIGHT NEAR MAIN CABIN DOOR IS INOPERATIVE. RELAMPED AS REQUIRED, OPERATIONAL CHECK GOOD. - [SDR SWIA200413707](https://openairdocs.org/sdr/SWIA200413707.md): Duct · loose · Aug 13, 2004 · N190SW · Emb EMB120ER · Cabin Cooling System > LEFT PACK MAKES A SQUEALING SOUND WITH LOW SELECTED. IN FLIGHT, PACK CREATES A HOT, SMOKEY SMELL UNTIL TURNED OFF. TIGHTENED CLAMPS AT LEFT PACK. COULD NOT DUPLICATE SMELL. OPERATIONAL CHECK GOOD. - [SDR SWIA200413599](https://openairdocs.org/sdr/SWIA200413599.md): Signal Cond Unit · malfunctioned · Jul 18, 2004 · N190SW · Emb EMB120ER · Engine BMEP/Torque Indicating > ON T/O ROLL, RIGHT ENGINE AUTO-FEATHERED DURING POWER LEVER ADVANCEMENT. REMOVED AND REPLACED RIGHT HAND ENGINE TORQUE SIGNAL CONDITIONER IAW MM 77-11-01. OPERATIONAL CHECK GOOD. - [SDR SWIA200413555](https://openairdocs.org/sdr/SWIA200413555.md): Wire · broken · Jul 3, 2004 · N190SW · Emb EMB120ER · Light System Wiring > EMERGENCY LIGHT ON OVERHEAD BIN ROW 9 DOESN'T ILLUMINATE. REPAIRED WIRING TO EMERGENCY LIGHT ON OVERHEAD BIN. OPERATIONAL CHECK GOOD. - [SDR SWIA200413225](https://openairdocs.org/sdr/SWIA200413225.md): Battery Pack · inoperative · Apr 24, 2004 · N190SW · Emb EMB120ER · Emergency Lighting > REAR SECTION EMERGENCY LIGHTS DOES NOT ILLUMINATE. REPLACED AFT ELBP WITH A SERVICEABLE UNIT. OPS CHECK GOOD. P/N 17366-04-001, S/N OFF 397. - [SDR SWIA200413144](https://openairdocs.org/sdr/SWIA200413144.md): Annunciator · malfunctioned · Apr 1, 2004 · N190SW · Emb EMB120ER · Trailing Flap Position Indicating System > ON THE GROUND WITH FLAP LEVER AT UP POSITION, CONTROL FAULT, FLAP AND ADVANCED SWS APPEAR INTERMITTENTLY. REPLACED FLAP ANNUNCIATOR IAW MM 20-21-00, MM 27-50-05. S/N OFF: 2151. REPAIRED AND REPOSITIONED WIRE W110-2909-2H WHICH WAS CHAFING AND SHORTING ON FL - [SDR SWIA200412959](https://openairdocs.org/sdr/SWIA200412959.md): Floor Support · cracked · Jan 21, 2004 · N190SW · Emb EMB120ER · Fuselage Miscellaneous Structure > UNDER FLOOR PANEL 243 DF BRACKET BUCKLED AND CRACKED. DISCOVERED DURING C-CHECK INSPECTION. FITTED AND INSTALLED NEW FLOOR SUPPORT BRACKET. P/N: 120-14243-001. - [SDR SWIA200412958](https://openairdocs.org/sdr/SWIA200412958.md): Frame · cracked · Jan 21, 2004 · N190SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib > CHANNEL CRACKED FORWARD OF FRAME NR 1 ON RIGHT ENGINE NACELLE AT TOP INBOARD SIDE AT UPPER NUT PLATE STRIP. DISCOVERED DURING C-CHECK INSPECTION. REPLACED INBOARD SECTION OF CHANNEL FORWARD OF FRAME NR 1 ON RIGHT NACELLE IAW SRM 54-10-02. - [SDR SWIA200412957](https://openairdocs.org/sdr/SWIA200412957.md): Frame · cracked · Jan 21, 2004 · N190SW · Emb EMB120ER · Fuselage Main, Frame > CRACK ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE. DISCOVERED DURING C-CHECK INSPECTION. PERFORMED REPAIR ON CENTER FRAME RIB BELOW E-BRAKE VALVE BOX INBOARD SIDE IAW SRM 51-70-01. - [SDR SWIA200412862](https://openairdocs.org/sdr/SWIA200412862.md): Light · inoperative · Jan 20, 2004 · N190SW · Emb EMB120ER · Emergency Lighting > ENTRY EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BULB IN ENTRYWAY. OPS CHECKS GOOD. - [SDR SWIA200312702](https://openairdocs.org/sdr/SWIA200312702.md): Selector · malfunctioned · Dec 9, 2003 · N190SW · Emb EMB120ER · Trailing Edge Flap Control System > ON DESCENT INTO SGU- LOW SPEED ALARM WENT OFF AND WOULD NOT STOP DESPITE NO ICING CONDITIONS AND ONLY STANDARD ICE ON. LANDED IN SGU WITHOUT INCIDENT AND WHEN THE ALARM STOPPED, THE SMOKE STOPPED. REMOVED AND REPLACED FLAP SELECTOR PANEL IAW MM 27-50-01. S/ - [SDR SWIA200312531](https://openairdocs.org/sdr/SWIA200312531.md): Wire Harness · faulty · Oct 22, 2003 · N190SW · Emb EMB120ER · Landing Gear System Wiring > WHEN SELECTING THE GEAR DOWN, ONLY THE RIGHT MAIN EXTENDED. RIGHT GREEN B-LIGHT AND ALL DISAGREEMENTS ILLUMINATED. THE ELECTRICAL OVER RIDE PROCEDURE IN THE QRH WAS CONDUCTED, RESULTING IN A SUCCESSFUL EXTENSION. REMOVED & REPLACED RIGHT MAIN GEAR SYSTEM-A - [SDR SWIA200312427](https://openairdocs.org/sdr/SWIA200312427.md): Apu · leaking · Sep 17, 2003 · N190SW · Emb EMB120ER · APU Core Engine > CAPT REPORTS SMOKE IN COCKPIT FROM AIR CONDITIONING SYSTEM. BOTH LT AND RT AIR CONDITIONING PACKS ARE COVERED IN OIL. APU BLEED SYSTEM IS PUTTING OIL INTO PACKS. REMOVED AND REPLACED THE APU IAW RII 49-301. OPS AND LEAK CHECKS GOOD. - [SDR SWIA200312307](https://openairdocs.org/sdr/SWIA200312307.md): Servo · malfunctioned · Aug 24, 2003 · N190SW · Emb EMB120ER · Autopilot Main Servo > WITH AUTOPILOT ENGAGED ON EITHER C/A OR F/O SIDE, AP MAKES UNCOMMANDED SLOW ROLL LEFT OR RIGHT. AUTOPILOT FAIL LIGHT ON MAP DOES NOT ILLUMINATE. REMOVED AND REPLACED THE AILERON AUTOPILOT SERVO IAW EMB120 MM 27-00-03. AUTOPILOT OPS CHECK GOOD IAW MM 22-10-0 - [SDR SWIA200312114](https://openairdocs.org/sdr/SWIA200312114.md): Wire · broken · Jun 18, 2003 · N190SW · Emb EMB120ER · Light System Wiring > WHITE EMERGENCY TRACK LIGHTING A-BEAM GALLEY INOP, SINGLE LIGHT. INSPECTED AND FOUND BROKEN WIRE. REPAIRED BROKEN WIRE ON WHITE EMERGENCY LIGHT TRACK A-BEAM GALLEY IAW EMB120 WM 20-21-00. OPS CHECK GOOD. - [SDR SWIA200311835](https://openairdocs.org/sdr/SWIA200311835.md): Fcu · malfunctioned · Mar 17, 2003 · N190SW · Emb EMB120ER · Trailing Edge Flap Control System > FLAP CONTROL FAULT FOR INBOARD FLAPS UPON RETRACTING FLAPS AFTER LANDING. REMOVED AND REPLACED FLAP ANNUNCIATOR PANEL AND FCU FOR TROUBLESHOOTING. RAN FLAPS UP AND DOWN SEVERAL TIMES. OPS CHECK GOOD AT THIS TIME. - [SDR SWIA200311833](https://openairdocs.org/sdr/SWIA200311833.md): Connector · damaged · Mar 15, 2003 · N190SW · Emb EMB120ER · Flight Control System Wiring > FLAP CONTROL FAULT INDICATED FOR INBOARD FLAPS. FLAPS WOULD NOT RETRACT ON THE GROUND. REMOVED AND REPLACED CONNECTOR FOR LEFT INBOARD FLAP ACTUATOR WITH A NEW PART. OPS CHECK OF FLAPS PERFORMED SATISFACTORY. P/N ON MS3476L12-10S. - [SDR SWIA200311759](https://openairdocs.org/sdr/SWIA200311759.md): Bushing · lack of lube · Jan 31, 2003 · N190SW · Emb EMB120ER · Cabin Cooling System > BOTH AIR CONDITIONING PACKS FAILED IN THE NORMAL POSITION. SMOKE FILLED THE CABIN AND COCKPIT. VERY LIMITED AIRFLOW IN LOW/LOW CONFIGURATION. LUBRICATED LEFT AND RIGHT ACTUATOR PIVOT BUSHINGS, CLEANED OIL FROM CONNECTORS. FREED RIGHT RAM AIR CHECK VALVE FR - [SDR SWIA200211597](https://openairdocs.org/sdr/SWIA200211597.md): Wire Harness · malfunctioned · Dec 17, 2002 · N190SW · Emb EMB120 · Landing Gear System Wiring > ON TAKEOFF COULDN'T GET THE LANDING GEAR TO GO UP. ALL THE LIGHTS WOULD BE ON BUT THE LEFT RED A. RETURNED TO FAT. REMOVED AND REPLACED LEFT MAIN GEAR A-PROXIMITY HARNESS IAW 32-61-01. OPS CHECK GOOD, LEAK CHECK OF VALVE IS GOOD. - [SDR SWIA200211409](https://openairdocs.org/sdr/SWIA200211409.md): Pump · fluctuates · Oct 30, 2002 · N190SW · Emb EMB120ER · Propeller Feathering/Reversing > AUX FEATHER PUMP BROKEN, RT ENGINE TORQUE FLUCTUATES 3 PERCENT TO 4 PERCENT AT CRUISE. REMOVED AND REPLACED AUX FEATHER PUMP. - [SDR SWIA200211371](https://openairdocs.org/sdr/SWIA200211371.md): Terminal Block · loose · Oct 26, 2002 · N190SW · Emb EMB120ER · Electrical Power System Wiring > MULTIPLE FAILURES ASSOCIATED WITH THE AHAR: HSI ROTATES 60 DEGREES-BOTH SIDES THEN CENTERS ADI-COMPUTER FAILURE LT SIDE ASSOCIATED WITH A GYRO FLAG RIGHT SIDE COMPUTER FAILURE-NO GYRO FLAG.FOUND SEVERAL NUTS ON TB0033 LOOSE AND RUBBER NIPPLE ON W138-0001-2 - [SDR SWIA200211372](https://openairdocs.org/sdr/SWIA200211372.md): Control Unit · malfunctioned · Oct 17, 2002 · N190SW · Emb EMB120ER · Propeller Controlling System > DURING CLIMB, RIGHT NP DROPPED TO 96 PERCENT. TURNED OFF EEC WITH POWER LEVER AT FLIGHT IDLE AND CL MAX T6 780, TORQUE 97 PERCENT AND NP 56 PERCENT. WE FEATHERED THE ENGINE PER QRH PRECAUTIONARY ENGINE SHUT DOWN AND DIVERTED TO CYS. REPLACED RT ENGINE PCU I - [SDR SWIA200211115](https://openairdocs.org/sdr/SWIA200211115.md): Receiver · failed · Aug 2, 2002 · N190SW · Emb EMB120ER · Automatic Direction Finder (ADF) System > WHILE HOLDING AT WYS, ADF FAILED IN FLIGHT. DIVERTED TO IDA. REPLACED ADF RECEIVER. OPS CHECKS GOOD IAW MM 34-53-00. - [SDR SWIA200211081](https://openairdocs.org/sdr/SWIA200211081.md): Brake · seized · Jul 26, 2002 · N190SW · Emb EMB120ER · Brake > ON TAXI OUT THE OUTBOARD RIGHT MAIN TIRE POPPED. FOUND NR 4 BRAKE LOCKED UP. REMOVED AND REPLACED NR 4 BRAKE IAW MM 32-41-05. LEAK CHECKS GOOD. - [SDR SWIA200211004](https://openairdocs.org/sdr/SWIA200211004.md): Servo · binding · Jun 30, 2002 · N190SW · Emb EMB120ER · Autopilot Main Servo > RUDDER PEDALS FEEL LIKE RUDDERS ARE BINDING UP. INSTALLED SERVICEABLE SVO65 AUTOPILOT SERVO. OPS CHECKS GOOD. - [SDR SWIA200210916](https://openairdocs.org/sdr/SWIA200210916.md): Computer · malfunctioned · Jun 8, 2002 · N190SW · Emb EMB120ER · Integrated Flight System > AUTOPILOT/YAW FAILURE IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. CAPTAIN'S COMPUTER AND GYRO FLAGS ARE INTERMITTENT IN FLIGHT. INSTALLED SERVICEABLE AHC85 COMPUTER. OPS CHECKS GOOD. - [SDR SWIA200210826](https://openairdocs.org/sdr/SWIA200210826.md): Actuator · failed · May 2, 2002 · N190SW · Emb EMB120ER · Trailing Edge Flap Actuator > IN CRUISE FLIGHT, FLAP LIGHT ON MAP PANEL ILLUMINATED ALONG WITH ADVANCED SWS LIGHT. FLAP INBOARD LIGHTS WERE ILLUMINATED. COMPLIED WITH QRH PROCEDURES. FLAPS WOULD NOT RESET. REMOVED AND REPLACED RIGHT INBOARD FLAP ACTUATOR. REPLACED ACTUATOR CANNON PLUG - [SDR SWIA200210804](https://openairdocs.org/sdr/SWIA200210804.md): Computer · faulty · Apr 14, 2002 · N190SW · Emb EMB120ER · Integrated Flight System > FIRST OFFICER'S EHSI TURNED 30-40 DEGREES RIGHT WHILE CLIMBING STRAIGHT OUT. FIRST OFFICER'S RMI HEADING INFORMATION MATCHES CAPTAIN'S EHSI, RMI AND MAGNETIC COMPASS. RESET FIRST OFFICER'S HEADING BY SWITCHING FIRST OFFICER'S COMPASS COMPENSATOR MOMENTARILY - [SDR SWIA200210810](https://openairdocs.org/sdr/SWIA200210810.md): Computer · malfunctioned · Apr 13, 2002 · N190SW · Emb EMB120ER · Integrated Flight System > DURING CLIMBOUT, FIRST OFFICER'S HEADING INDICATOR STARTED STICKING WITH A 30 DEGREE DIFFERENCE BETWEEN HI'S WITH NO ASSOCIATED FLAGS OR ALARMS. AFTER TURNING BACK TOWARD DEN, THE GYRO BEGAN WORKING PROPERLY. FIRST OFFICER RECEIVED COMPUTER FLAG DURING TAXI - [SDR SWIA200210726](https://openairdocs.org/sdr/SWIA200210726.md): Wire · loose · Mar 13, 2002 · N190SW · Emb EMB120ER · Light System Wiring > EMERGENCY LIGHTS IN FLOOR TRACK WILL NOT ILLUMINATE. SECURED LOOSE WIRE AT CONNECTION BELOW FLOOR AT ROW 3. EMERGENCY LIGHTS, OPS CHECK OK. - [SDR SWIA200210728](https://openairdocs.org/sdr/SWIA200210728.md): Control Cable · corroded · Feb 16, 2002 · N190SW · Emb EMB120ER · Rudder Control System > LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES SHOW SIGNS OF CORROSION. REPLACED LEFT RUDDER AFT OUTBOARD AND INBOARD CABLES IAW EMB120 MM 27-00-01. - [SDR SWIA200210727](https://openairdocs.org/sdr/SWIA200210727.md): Control Cable · corroded · Feb 16, 2002 · N190SW · Emb EMB120ER · Elevator Control System > RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES SHOWING SIGNS OF WEAR AND CORROSION. REPLACED RIGHT OUTBOARD AFT ELEVATOR CABLE AND RIGHT AND LEFT AFT ELEVATOR TRIM CABLES IAW EMB120 MM 27-00-01. - [SDR SWIA200210667](https://openairdocs.org/sdr/SWIA200210667.md): Annunciator · faulty · Feb 12, 2002 · N190SW · Emb EMB120ER · Trailing Flap Position Indicating System > FLAPS INOP - ALL CONTROL FAULT, DISAGREEMENT AND ASYMMETRY LIGHTS ON. COULD NOT CLEAR ANY OF THE FAULT LIGHTS. FLAP CONTROL PANEL FLAP PORTION INDICATOR (ALL) INDICATED FLAPS UP WHEN FLAPS WERE 15 DEGREES, 25 DEGREES OR 45 DEGREES POSITION PHYSICALLY. CONDI - [SDR SWIA200210577](https://openairdocs.org/sdr/SWIA200210577.md): Tail Cone · out of position · Jan 19, 2002 · N190SW · Emb EMB120ER · Aerodynamic Fairings > CONTROL YOKE BINDS ABOUT HALFWAY THROUGH FORWARD AND AFT TRAVEL WITH ELEVATOR TRIM IN THE GREEN ARC. BIND IS LESS WITH ELEVATOR TRIM FULL FORWARD AND GOES AWAY COMPLETELY WITH TRIM FULL AFT. REPOSITIONED TAIL CONE TO PREVENT RUBBING ON ELEVATOR. OPS CHECK G - [SDR SWIA200110344](https://openairdocs.org/sdr/SWIA200110344.md): Timer · malfunctioned · Nov 8, 2001 · N190SW · Emb EMB120ER · Air Intake Anti/De-Ice System > LEFT ENGINE AIR INLET FAILED 14 MINUTES INTO FLIGHT PASSING THROUGH FL180. TURNED OFF FOR A FEW MINUTES AND THEN ON FOR ANOTHER 14 MINUTES DURING RETURN TO SLC AND IT DID NOT FAIL AGAIN. REMOVED AND REPLACED LEFT ENGINE DEICE TIMER IAW MM 30-20-05. REMOVED - [SDR SWIA200110317](https://openairdocs.org/sdr/SWIA200110317.md): Harness · faulty · Nov 3, 2001 · N190SW · Emb EMB120ER · Landing Gear System Wiring > AFTER GEAR RETRACTION, RIGHT MAIN GEAR B-GREEN LIGHT REMAINS ILLUMINATED WITH ALL OTHER LIGHTS OUT. RECYCLED GEAR WITH SAME RESULT. B-GREEN LIGHT DID FINALLY GO OUT 10 MINUTES AFTER SECOND GEAR RETRACTION. REPLACED RIGHT MLG PROXIMITY HARNESS-B IAW 32-61-01 - [SDR SWIA200110305](https://openairdocs.org/sdr/SWIA200110305.md): Actuator · failed · Oct 29, 2001 · N190SW · Emb EMB120ER · Trailing Edge Flap Actuator > CONTROL FAULT WOULD NOT RESET PER QRH. INBOARD FLAPS SHOWED 10 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR PER MM 27-50-00. OPS CHECK, LEAK CHECKS GOOD. - [SDR SWIA200110311](https://openairdocs.org/sdr/SWIA200110311.md): Door · missing · Oct 24, 2001 · N190SW · Emb EMB120ER · Hydraulic Compartment Doors > LEFT HYDRAULIC DOOR MISSING. (DISCOVERED ON WALK AROUND INSPECTION.) FIT AND INSTALLED A NEW LEFT HYDRAULIC BAY DOOR IAW EMB SRM 51-00-00 AND 51-40-02. - [SDR SWIA200110266](https://openairdocs.org/sdr/SWIA200110266.md): Roller · worn · Oct 24, 2001 · N190SW · Emb EMB120ER · Trailing Edge Flaps > CONTROL FAULT ON INBOARD FLAPS. FOUND CONTAMINATION IN INBOARD ACTUATOR CANNON PLUGS. ALSO FOUND WORN ROLLERS ON LEFT INBOARD FLAP. CLEANED CANNON PLUGS AND REMOVED AND REPLACED ROLLER LEFT INBOARD FLAP. REINSTALLED PANELS. OPS CHECK GOOD. ROLLER P/N: P - [SDR SWIA200110236](https://openairdocs.org/sdr/SWIA200110236.md): Actuator · failed · Oct 9, 2001 · N190SW · Emb EMB120ER · Trailing Edge Flap Actuator > CONTROL FAULT ON FLAPS ON TAKEOFF. REPLACED INBOARD FLAP ACTUATOR IAW MM 27-50-00. OPS AND LEAK CHECK GOOD. - [SDR SWIA200110235](https://openairdocs.org/sdr/SWIA200110235.md): Switch · inoperative · Oct 8, 2001 · N190SW · Emb EMB120ER · Communications System > FIRST OFFICER'S PTT SWITCH INOP. RETURNED TO SLC. INSTALLED NEW SWITCH. FIRST OFFICER'S PTT OPS CHECK GOOD. - [SDR SWIA200110199](https://openairdocs.org/sdr/SWIA200110199.md): Proximity Sensor · failed · Sep 22, 2001 · N190SW · Emb EMB120ER · Elevator Control System > ABORTED TAKEOFF WHEN WE BROUGHT THE POWER UP DUE TO TAKEOFF TRIM WARNING. TRIM CONFIRMED SET AT 4 IN THE GREEN BAND.REMOVED AND REPLACED LEFT TRIM PROXIMITY SENSOR. OPS CHECK GOOD. P/N: ATG120TR - [SDR SWIA200110193](https://openairdocs.org/sdr/SWIA200110193.md): Eec · malfunctioned · Sep 20, 2001 · N190SW · Emb EMB120ER · Fuel Control/Turbine Engines > LEFT EEC WENT TO MANUAL ON TAKEOFF POWER UP. ABORTED TAKEOFF.RESET LEFT EEC. OPS CHECK GOOD. Next page: https://openairdocs.org/deregistered/N190SW-2006-03-22/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 n_number = 'N190SW' AND deregistration_id = 'N190SW-2006-03-22' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N190SW-2006-03-22/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.