# Service difficulty reports: N199SW, cancelled Dec 6, 2005 A list on [N199SW, cancelled Dec 6, 2005](https://openairdocs.org/deregistered/N199SW-2005-12-06.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA200211500](https://openairdocs.org/sdr/SWIA200211500.md): Actuator · malfunctioned · Nov 24, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap Actuator > FLAP DISAGREEMENT ON NACELLE FLAPS ON RETRACTION FROM 45 DEGREES. REPLACED LEFT NACELLE FLAP ACTUATOR IAW MM 27-50-00. LEAK CHECK GOOD. - [SDR SWIA200211487](https://openairdocs.org/sdr/SWIA200211487.md): Proximity Sensor · malfunctioned · Nov 14, 2002 · N199SW · Emb EMB120ER · Landing Gear Position and Warning > AFTER ROTATION, WHEN SELECTING THE LANDING ''UP'', THE NOSE A & B SYSTEM RED AND GREEN LIGHTS REMAINED ILLUMINATED. CYCLED THE GEAR PER THE QRH AND NO GEAR MOVEMENT NOTED. RETURNED TO LAX AND WHILE ENROUTE LIGHTS EXTINGUISHED. NORMAL LANDING GEAR EXTENSION W - [SDR SWIA200211486](https://openairdocs.org/sdr/SWIA200211486.md): Handle · out of adjust · Nov 11, 2002 · N199SW · Emb EMB120ER · Passenger/Crew Doors > CAPTAIN'S DIRECT VISION WINDOW VERY HARD TO OPEN AND THEN IMPOSSIBLE TO CLOSE. ADJUSTED CAPTAIN'S DV WINDOW HANDLE OPENING ROD AND DEBURRED CATCH. OPS CHECK GOOD. - [SDR SWIA200211362](https://openairdocs.org/sdr/SWIA200211362.md): Spar Cap · cracked · Oct 7, 2002 · N199SW · Emb EMB120ER · Wing Spar > LEFT WING FORWARD LOWER SPAR CAP HAS A CRACK BETWEEN 4533.5 AND 4945. RIVET ROW ON LOWER SKINS MARKED WHERE SKIN SEAMS MEET, OUTBD OF RIB NR17. DISCOVERED DURING LINE INSPECTION OF FUEL LEAK. REPAIRED IAW EMB 120 SRM 57-20-05 AND RII CARD RII 57-301 AND RII - [SDR SWIA200211199](https://openairdocs.org/sdr/SWIA200211199.md): Connector · dirty · Sep 1, 2002 · N199SW · Emb EMB120ER · Fuel Control/Turbine Engines > LEFT EEC MANUAL REVERSION FAILED ON TAKEOFF. ABORTED TAKEOFF. CLEANED CONTAMINATION FROM LEFT ENG EEC P1 CONNECTOR. RAN ENG, OPS CHECK GOOD. - [SDR SWIA200211152](https://openairdocs.org/sdr/SWIA200211152.md): Control Unit · malfunctioned · Aug 20, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap Control System > ON APPROACH THE NACELLE FLAPS ARE INOP. REPAIRED WIRE W628-0007-22 BETWEEN P1869 & P0828. REMOVED AND REPLACED FLAP CONTROL UNIT. OPS CHECKS GOOD. - [SDR SWIA200211141](https://openairdocs.org/sdr/SWIA200211141.md): Actuator · malfunctioned · Aug 19, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap Actuator > ON DESCENT INTO ELKO, RIGHT NACELLE WOULD NOT EXTEND PAST 15 DEGREES WITH CONTROL FAULTS. AFTER LANDING, ALL FLAPS RETRACTED. THEREAFTER, RIGHT NACELLE FLAP WOULD NOT WORK, CAUSING FLAP ASYMMETRY. REMOVED AND REPLACED NACELLE FLAP ACTUATOR. REMOVED AND REP - [SDR SWIA200211127](https://openairdocs.org/sdr/SWIA200211127.md): Structure · cracked · Aug 15, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flaps > RIGHT NACELLE FLAP FOUND CRACKED. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-03. OPS CHECK GOOD. - [SDR SWIA200211126](https://openairdocs.org/sdr/SWIA200211126.md): Actuator · failed · Aug 15, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap Actuator > NACELLE FLAPS WOULD NOT GO PAST 4 ROWS OF LIGHTS WHEN 25 DEGREES OF FLAPS SELECTED. FLAP DISAGREEMENT WARNING. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW EMB120 MM 27-50-09. LEAK CHECK GOOD. OPS CHECK GOOD AT THIS TIME. - [SDR SWIA200210914](https://openairdocs.org/sdr/SWIA200210914.md): Fcu · malfunctioned · Jun 8, 2002 · N199SW · Emb EMB120ER · Trailing Edge Flap Control System > CONTROL FAULT ON TAXI OUT, COULD NOT RESET. REMOVED AND REPLACED FLAP CONTROL UNIT AND RIGHT NACELLE FLAP ACTUATOR WITH SERVICEABLE UNITS IAW MM 27-00-00. OPS CHECK GOOD. - [SDR SWIA200210977](https://openairdocs.org/sdr/SWIA200210977.md): Actuator · failed · Jun 4, 2002 · N199SW · Emb EMB120ER · Landing Gear Door Actuator > ON GEAR RETRACTION, THE RIGHT MAIN GEAR RED LIGHTS REMAINED ILLUMINATED WITH ASSOCIATED GEAR DOOR FLUTTER SOUND. RETURNED TO PSP. GEAR EXTENDED NORMALLY. REPLACED RIGHT MLG MAIN ACTUATOR WITH SERVICEABLE UNIT PER MM 32-32-10. GEAR SWING OPS CHECKS GOOD. N - [SDR SWIA200210898](https://openairdocs.org/sdr/SWIA200210898.md): Inverter · failed · May 30, 2002 · N199SW · Emb EMB120ER · AC Inverter > INVERTER NR 1 WENT INOP EN ROUTE AND WOULD NOT RESET. RETURNED TO DEN. REMOVED AND REPLACED NR 1 INVERTER. OPS CHECK GOOD. INSTALLED SERVICEABLE INVERTER IAW MM 24-20-01. OPS CHECK GOOD. FURTHER INVESTIGATION IN PROGRESS. - [SDR SWIA200210750](https://openairdocs.org/sdr/SWIA200210750.md): Seal · defective · Mar 17, 2002 · N199SW · Emb EMB120ER · Turbine Engine Oil System > ON TAKEOFF RECEIVED A RIGHT ENGINE OIL PRESSURE WARNING. OIL PRESSURE RETURNED BACK IN THE GREEN ARC AND FLUCTUATED BETWEEN 60 & 50 PSID. OIL PRESSURE DROPPED BACK OFF AGAIN WITH ASSOCIATED WARNINGS. OIL PRESSURE STABILIZED AT 63 PSID ON DOWNWIND RETURNING - [SDR SWIA200210703](https://openairdocs.org/sdr/SWIA200210703.md): Servo · binding · Mar 6, 2002 · N199SW · Emb EMB120ER · Autopilot Main Servo > LEFT RUDDER PEDAL BINDING. REMOVED AND REPLACED RUDDER AUTOPILOT SERVO IAW 27-31-00. OPS CHECKS GOOD. - [SDR SWIA200210675](https://openairdocs.org/sdr/SWIA200210675.md): Oil System · low · Feb 25, 2002 · N199SW · Emb EMB120ER · Turbine Engine Oil System > LOW OIL PRESSURE LIGHT ILLUMINATED FOR NR 2 ENGINE ON TAKEOFF ROLL. ABORTED TAKEOFF. ADDED 3 QUARTS TO NR 2 ENGINE. UPON INSPECTION NO OIL LEAKAGE FOUND. - [SDR SWIA200210653](https://openairdocs.org/sdr/SWIA200210653.md): Boot · damaged · Feb 19, 2002 · N199SW · Emb EMB120ER · Airfoil Anti/De-ice System > LEADING EDGE OUTBOARD RIGHT, LEFT AND VERTICAL STAB FAILURES ON BOTH DEICE TIMERS AT BOTH HIGH AND LOW POWER SETTINGS. OUTSIDE TEMP -6 DEGREES CELISUS AT 12,000 - 20,000 MSL. REMOVED AND REPLACED RIGHT HORIZONTAL DEICE BOOT IAW MM 30-10-00. OPS CHECKS GOOD. - [SDR SWIA200210598](https://openairdocs.org/sdr/SWIA200210598.md): Monitor · malfunctioned · Jan 28, 2002 · N199SW · Emb EMB120ER · Ice Detection > LEADING EDGE DEICE MIDDLE LEFT WING, INBOARD LEFT WING, INBOARD LEFT STAB AND INBOARD RIGHT STAB LIGHTS CAME ON IN FLIGHT. RETURNED TO SLC. REPLACED DEICE MONITOR. CYCLED WINGS AND ENGINE DEICERS 2 CYCLES ON EACH TIMER WITHOUT FAULT. P/N ON 0552-01-001, S/ - [SDR SWIA200110463](https://openairdocs.org/sdr/SWIA200110463.md): Intercostal · cracked · Nov 21, 2001 · N199SW · Emb EMB120ER · Fuselage Miscellaneous Structure > COCKPIT, CRACK IN INTERCOSTAL LOCATED AFT OF CAPTAIN'S SLIDING WINDOW AFT FRAME AT APPROXIMATE HEIGHT OF OVERHEAD SPEAKER. FABRICATED AND INSTALLED DOUBLER FOR THE CRACKED INTERCOSTAL IAW EMB SRM 51-70-05. - [SDR SWIA200110461](https://openairdocs.org/sdr/SWIA200110461.md): Channel · worn · Nov 21, 2001 · N199SW · Emb EMB120ER · Nacelle/Pylon, Main Frame > LEFT NACELLE OUTBOARD J-CHANNEL HAS DEEP GROOVES AT AFT END OUTBOARD OF AFT GEAR DOOR AREA. REPLACED J-CHANNEL REPAIR SECTION IAW EMB TECH. SUPPORT ENGINEERING APPROVAL, REF SST-1003/97 AND EMB120 SRM 51-40-02. - [SDR SWIA200110460](https://openairdocs.org/sdr/SWIA200110460.md): Stiffener · corroded · Nov 21, 2001 · N199SW · Emb EMB120ER · Fuselage Miscellaneous Structure > 1ST CROSS MEMBER AFT OF THE PASSENGER DOOR HAS INTERGRANULAR CORROSION. REMOVED AND REPLACED THE CORRODED CROSS MEMBER IAW EMB SRM 51-00-00 & 51-40-02. - [SDR SWIA200110036](https://openairdocs.org/sdr/SWIA200110036.md): Flap · cracked · Jul 17, 2001 · N199SW · Emb EMB120ER · Trailing Edge Flaps > RIGHT NACELLE FLAP HAS A CRACK IN UPPER SURFACE. REMOVED AND REPLACED RIGHT NACELLE FLAP IAW MM 27-50-02. P/N: 120-40327-001 - [SDR SWIA972531](https://openairdocs.org/sdr/SWIA972531.md): Aileron · jammed · Apr 24, 2001 · N199SW · Emb EMB120ER · Aileron Control System > AILERONS JAMMED, WILL NOT DEFLECT FOR A LEFT TURN ON TAXI. TIGHTENED SCREW THAT BACKED OUT ON RIGHT AILERON INSPECTION PANEL. CHECKED AILERONS FOR FREEDOM OF MOVEMENT IN BOTH DIRECTIONS. OPS CHECK GOOD. - [SDR SWIA972481](https://openairdocs.org/sdr/SWIA972481.md): Wire · chafed · Mar 29, 2001 · N199SW · Emb EMB120ER · Elevator Control System > TRIM AURAL WARNING DURING TAKEOFF ROLL. ABORTED TAKEOFF. FOUND AURAL CB POPPED. INSPECTED ELEVATOR TRIM PROXIMITY SENSORS WIRING ON TOP OF TAIL. FOUND WIRES CHAFING ON STEEL BRAIDED WIRE SHROUD. INSULATED BARE WIRES AND RESET AURAL WARNING CB. OPS CHECK - [SDR SWIA972496](https://openairdocs.org/sdr/SWIA972496.md): Door · out of adj · Mar 26, 2001 · N199SW · Emb EMB120ER · Passenger/Crew Doors > EXCESSIVE LOUD HISSING THROUGH FORWARD CABIN DOOR. FLIGHT ATTENDANT REPORTS HE CAN SEE DAYLIGHT THROUGH BOTTOM RIGHT SIDE OF FORWARD DOOR. SHIM FORWARD BOTTOM CORNER OF CABIN DOOR. OPS CHECK GOOD. - [SDR SWIA972440](https://openairdocs.org/sdr/SWIA972440.md): Servo · binding · Mar 18, 2001 · N199SW · Emb EMB120ER · Autopilot Trim Servo > AFTER AUTOPILOT DISCONNECTED, CAPTAINS SIDE NOTICED BINDING OF TRIM (ELEVATOR) BETWEEN 3 AND 6 UNITS. TRIM WHEEL WOULD BIND THEN RELEASE. ALTITUDE 6000 FEET WITH NO MOISTURE. INSPECTED ENTIRE ELEVATOR TRIM SYSTEM FOR DEFECTS. NONE NOTED. ALL TESTS AND FUN - [SDR SWIA972332](https://openairdocs.org/sdr/SWIA972332.md): Servo · failed · Feb 5, 2001 · N199SW · Emb EMB120ER · Autopilot Main Servo > WHEN CONTROL YOKE MOVED SIDE TO SIDE A NOISE IS HEARD IN THE FLOOR PANEL AREA. REPLACED AILERON SERVO WITH SERVICEABLE UNIT. OPS CHECK GOOD. S/N ON: 9961, S/N OFF: 5507. - [SDR SWIA972210](https://openairdocs.org/sdr/SWIA972210.md): Ejector Valve · malfunctioned · Dec 22, 2000 · N199SW · Emb EMB120ER · Airfoil Anti/De-ice System > CLIMBING THROUGH 17,000 FEET, LEFT AND RIGHT OUTBOARD LEADING EDGE DEICE INOP LIGHTS ILLUMINATED. TIMER 2 HAD THE SAME RESULT AFTER PROCEEDING PER QRH. AFTER LEAVING 6000 FEET AND ICING CONDITIONS THE BOOTS WORKED FINE. RETURNED TO SEA. REMOVED AND REPLACED - [SDR SWIA972139](https://openairdocs.org/sdr/SWIA972139.md): Sequence Valve · failed · Nov 30, 2000 · N199SW · Emb EMB120ER · Landing Gear Door Retract Section > UPON TAKEOFF RIGHT LANDING GEAR WOULD NOT COME UP FOLLOWED BY LOUD GRINDING NOISE FROM RIGHT SIDE OF AIRCRAFT. CYCLED GEAR DOWN, DID NOT CYCLE GEAR BACK UP BECAUSE OF CONCERN FOR PREVIOUS TWO RIGHT UPS OF PROBLEMS. RED INTRANSIT LIGHTS REMAINED ON WITH GEAR - [SDR SWIA972075](https://openairdocs.org/sdr/SWIA972075.md): Window · out of adj · Nov 3, 2000 · N199SW · Emb EMB120ER · Flight Compartment Windows > UNABLE TO CLOSE F/O''S WINDOW ENOUGH TO GET THE TAB DOWN. ADJUSTED THE F/O''S DIRECT VIEW WINDOW. OPS CHECKS GOOD. - [SDR SWIA971993](https://openairdocs.org/sdr/SWIA971993.md): Bushing · damaged · Sep 24, 2000 · N199SW · Emb EMB120ER · Landing Gear Retraction/Extension System > RIGHT GEAR VIBRATION ON RETRACTION, RED GEAR INDICATION REMAINED LIT. CYCLED GEAR, SAME PROBLEM. CYCLED GEAR HANDLE UP AND DOWN QUICKLY, LIGHT EXTINGUISHED, VIBRATION CEASED. RETURNED TO FIELD. REBUSHED RIGHT MAIN LANDING GEAR DRAG BRACE OUTBOARD BUSHING. - [SDR SWIA971750](https://openairdocs.org/sdr/SWIA971750.md): Computer · failed · Apr 1, 2000 · N199SW · Emb EMB120ER · Autopilot Computer > AFTER TAKEOFF AT 1500 AGL TRIPLE CHIME AND RED TRIM FAIL AND AUTO PILOT FAIL, MAP LIGHTS ILLUMINATED, THE YAW DAMPNER FAILED. CAPTAINS AND FOS COMPUTER FLAGS WAS OBSERVED ON AHRS, ARCS FGS 1 AND FGS 2 DC CIRCUIT BREAKERS POPPED AND WOULD NOT RESET. NO FLIGH - [SDR SWIA971555](https://openairdocs.org/sdr/SWIA971555.md): Filter Light · illuminated · Sep 9, 1999 · N199SW · Emb EMB120ER · Hydraulic Indicating System > GREEN SYSTEM FILTER LIGHT ILLUMINATED AFTER DEPARTURE WHEN THE GEAR WAS BROUGHT UP. RETURNED TO SLC. REMOVED AND REPLACED GREEN HYDRAULIC FILTERS. INSPECTED FILTERS WITH NO CONTAMINATION NOTED. LEAKS CHECKED GOOD IAW MM 29-10-06. - [SDR SWIA971546](https://openairdocs.org/sdr/SWIA971546.md): Fire Detector · malfunctioned · Aug 1, 1999 · N199SW · Emb EMB120ER · Fire Detection > LEFT ENGINE FIRE DETECTOR/WHEEL WELL LIGHT CAME ON IN FLIGHT. DIVERTED FROM EKO TO SLC. REPLACED LEFT ENGINE FIRE DETECTOR. FIRE DETECTION TEST GOOD. - [SDR SWIA971545](https://openairdocs.org/sdr/SWIA971545.md): Switch · failed · Aug 1, 1999 · N199SW · Emb EMB120ER · Engine Oil Pressure > ON CLIMB-OUT OF SLC, HAD AURAL WARNING AND MAP INDICATION OIL PRESS 20. RETURNED TO SLC. OIL PRESSURE GAUGE REMAINED IN GREEN AT ALL TIMES. ADDED 2 QUARTS OIL TO THE RIGHT ENGINE AND REPLACED LOW OIL PRESSURE SWITCH. GROUND RAN AIRCRAFT FOR 15 MINUTES. OP - [SDR SWIA971414](https://openairdocs.org/sdr/SWIA971414.md): Rollers · worn · Feb 7, 1999 · N199SW · Emb EMB120ER · Trailing Edge Flaps > AFTER DEPARTURE, FLAPS INCURRED DISAGREEMENT FROM FLAPS 15 TO FLAPS UP. INBOARD PAIR DISAGREEMENT. TRIED THREE TIMES TO FIX/RECONFIGURE, UNSUCCESSFUL. RETURNED TO SLC. LANDING CONFIGURATION (FLAPS 25) WORKED PROPERLY. REPLACED 2 ROLLERS ON LEFT AND RIGHT - [SDR SWIA971345](https://openairdocs.org/sdr/SWIA971345.md): Actuator · failed · Dec 25, 1998 · N199SW · Emb EMB120ER · Landing Gear Retraction/Extension System > RETURNED TO AIRPORT. RIGHT MAIN GEAR WOULD NOT RETRACT, POSSIBLY JUST THE GEAR DOOR. REMOVED AND REPLACED UPLOCK ACTUATOR AND SEQUENCING VALVES, OPS CHECK GOOD. - [SDR SWIA971335](https://openairdocs.org/sdr/SWIA971335.md): Flap · damaged · Dec 5, 1998 · N199SW · Emb EMB120ER · Trailing Edge Flaps > FLAP DISAGREEMENT ON FLAP RETRACTION RIGHT SIDE. RETURNED TO SLC. REMOVED AND REPLACED LEFT OUTBOARD FLAP IAW EMB MM 27-50-04, OPS CHECKS GOOD. - [SDR SWIA971334](https://openairdocs.org/sdr/SWIA971334.md): Connector · contaminated · Dec 5, 1998 · N199SW · Emb EMB120ER · Trailing Flap Position Indicating System > UPON CLIMBOUT AT FLAP RETRACTION, RECEIVED FLAP DISAGREEMENT RIGHT SIDE. RETURNED TO SLC. FOUND MOISTURE IN OUTBOARD LEFT FLAP CANNON PLUG. CLEANED BOTH FLAP ACTUATOR CANNON PLUGS. NO FAULTS OR DISAGREEMENTS. - [SDR SWIA971330](https://openairdocs.org/sdr/SWIA971330.md): Warning · activated · Dec 3, 1998 · N199SW · Emb EMB120ER · Attitude and Direction Data System > BOTH SIDES GYROFLAGS INTERMITTENTLY ON AND OFF, COMMAND BARS MOVED ABNORMALLY UP AND DOWN AND SIDE TO SIDE. RETURNED TO FIELD. AIRCRAFT WAS FLOWN FOR 34 MINUTES WITH NO DISCREPANCIES REPORTED. ALL SYSTEMS CHECK GOOD. - [SDR SWIA971283](https://openairdocs.org/sdr/SWIA971283.md): Controler · failed · Oct 9, 1998 · N199SW · Emb EMB120ER · Cabin Pressure Controller > AUTO CABIN PRESSURIZATION SYSTEM FAILED. RETURNED TO EKO. REPLACED CABIN PRESS CONTROL, OPS CHECKS GOOD. - [SDR SWIA971250](https://openairdocs.org/sdr/SWIA971250.md): Actuator · failed · Aug 9, 1998 · N199SW · Emb EMB120ER · Landing Gear Actuator > RIGHT MAIN GEAR INTRANSIT LIGHT (A & B SYSTEMS) ON. TOWER REPORTED RIGHT MAIN DID NOT RETRACT. COULD HEAR HYDRAULIC CYCLING IN NOSE. RETURNED TO FAT. REMOVED AND REPLACED RIGHT MAIN LANDING GEAR ACTUATOR IAW MM 32-32-10. GEAR SWING SATISFACTORY. - [SDR SWIA971224](https://openairdocs.org/sdr/SWIA971224.md): Bracket · failed · Jul 8, 1998 · N199SW · Emb EMB120ER · Landing Gear Doors > MAIN GEAR WOULD NOT RETRACT. CYCLED HANDLE, STILL DOWN INDICATION. NOSE GEAR RETRACTED FINE. INSTALLED NEW GEAR DOOR HINGE BRACKET ON RIGHT GEAR INBOARDD FORWARD DOOR. ADJUSTED AND SWUNG GEAR 20 TIMES. OPS CHECKS GOOD. - [SDR SWIA97911](https://openairdocs.org/sdr/SWIA97911.md): Hydraulic Line · chafed · Jul 9, 1997 · N199SW · Emb EMB120ER · Hydraulic System, Main > AFTER TAKEOFF, THE RIGHT MAIN HYDRAULIC PUMP FAILED AND FLUID LEVEL DROPPED TO ZERO. DIVERTED TO SBA. FOUND HYDRAULIC LINE CHAFED THROUGH AT COWL FLAPS ACTUATOR. REPLACED LINE AND REPLENISHED HYDRAULIC FLUID. CYCLED FLAPS NUMEROUS TIMES, NO LEAKS NOTED AND - [SDR SWIA97863](https://openairdocs.org/sdr/SWIA97863.md): Proximity Sensor · failed · Feb 18, 1997 · N199SW · Emb EMB120ER · Landing Gear Position and Warning > DURING FLIGHT, THE RIGHT MAIN LANDING GEAR 'A' GREEN LIGHT ILLUMINATED. LIGHT REMAINED ON FOR THE REMAINDER OF THE FLIGHT. LANDING GEAR COULD ONLY BE EXTENDED USING THE EMERGENCY EXTENSION SWITCH. REPLACED RIGHT MAIN 'A' SYSTEM DOWNLOCK PROXIMITY SENSOR. C - [SDR SWIA97838](https://openairdocs.org/sdr/SWIA97838.md): Ejector · failed · Jan 22, 1997 · N199SW · Emb EMB120ER · Air Intake Anti/De-Ice System > RIGHT ENGINE INLET DEICE FAILED INFLIGHT AT TAKEOFF/CLIMB POWER. DIVERTED TO LAX INSTEAD OF MRY. FOUND DEICE EJECTOR FOR RIGHT DEICE INLET BOOT COMING APART. REPLACED EJECTOR ON RIGHT DEICE INLET BOOT. OPS CHECKS GOOD. - [SDR SWIA97839](https://openairdocs.org/sdr/SWIA97839.md): Indicator · inoperative · Jan 15, 1997 · N199SW · Emb EMB120ER · Weather Radar System > WEATHER RADAR INOPERATIVE. PAINTS SERIES OF RECTANGLES. RETURNED TO LAX. REPLACED RADAR INDICATOR. PERFORMED OPS, CHECKS GOOD. - [SDR SWIA97813](https://openairdocs.org/sdr/SWIA97813.md): Latch Pin · failed · Jan 2, 1997 · N199SW · Emb EMB120ER · Landing Gear Door Retract Section > LEFT GEAR OUTBOARD FOWARD DOOR WILL NOT STAY LATCHED. RETURNED TO FIELD. REPLACED ROLL PIN FOR LEFT GEAR FOWARD DOOR LATCH, OPS CHECKS GOOD. - [SDR SWIA95774](https://openairdocs.org/sdr/SWIA95774.md): Prox Sensor · malfunctioned · Nov 12, 1996 · N199SW · Emb EMB120ER · Landing Gear Position and Warning > AURAL WARNING UNIT WENT OFF INFLIGHT WITH THE FOLLOWING BRAKES, TRIM FLAPS AUTOFEATHER. REPLACED NOSE GEAR AIR/GROUND PROX SENSOR CYCLED GEAR SEVERAL TIMES, OPS CKS GOOD. - [SDR SWIA95705](https://openairdocs.org/sdr/SWIA95705.md): Connectors · loose · Jan 4, 1996 · N199SW · Emb EMB120ER · Trailing Edge Flap Control System > AFTER TAKEOFF, TRIED TO RETRACT FLAPS AND THEY ONLY WENT UP TO ABOUT 7 DEGREES, RECEIVED A FLAP DISAGREEMENT WARNING. WE THEN RETURNED FOR LANDING AT SLC. AFTER TOUCHDOWN THE FLAPS RETRACTED. BEFORE TAKEOFF WE GOT DE-ICED WITH FLAPS DOWN 45 DEGREES AS 50P. - [SDR SWIA95676](https://openairdocs.org/sdr/SWIA95676.md): Linear Actuator · worn · Nov 9, 1995 · N199SW · Emb EMB120ER · Rudder Tab Control System > RUDDER TRIM ACTUATOR CABLE WORN. REMOVED AND REPLACED RUDDER TRIM LINEAR ACTUATOR IAW EMB120 MAINTENANCE MANUAL 27-00-01 AND R2 9 REV 19 DATED 7-1-91. ## 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 = 'N199SW' AND deregistration_id = 'N199SW-2005-12-06' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N199SW-2005-12-06/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.