# Service difficulty reports: N195SW, cancelled Sep 28, 2004 A list on [N195SW, cancelled Sep 28, 2004](https://openairdocs.org/deregistered/N195SW-2004-09-28.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR SWIA972626](https://openairdocs.org/sdr/SWIA972626.md): Wire · failed · Jun 10, 2001 · N195SW · Emb EMB120ER · Auto Flight System Wiring > AUTOPILOT ENGAGED DURING CLIMB AND WOULD NOT DISENGAGE UNTIL CIRCUIT BREAKER PULLED. FOUND WIRE W201-1153-24 BETWEEN AUTOPILOT TRANSFER BOX P1122 PIN 2 AND COPILOTS FCP-65 P0178 PIN 47 BAD AND NEEDS REPAIRED. AMBER ''DIS'' FOR YAW DOES NOT ILLUMINATE WHEN CO - [SDR SWIA972608](https://openairdocs.org/sdr/SWIA972608.md): Warning System · false activation · May 31, 2001 · N195SW · Emb EMB120ER · Central Warning > FLAP AURAL WARNING ON TAKEOFF ROLL. PERFORMED TAKEOFF WARNING TEST IAW MM 27-50-00, PAGES 516-518. OPS CHECK GOOD, NO DEFECTS NOTED. - [SDR SWIA972598](https://openairdocs.org/sdr/SWIA972598.md): Actuator · failed · May 26, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > LANDING AT SLC RECEIVED FLAP CONTROL FAULT THAT WOULD NOT RESET AFTER LANDING. RETRACTED FLAPS, INBOARD FLAPS REMAINED AT 25 DEGREES SETTING. REMOVE AND REPLACE RIGHT INBOARD FLAP ACTUATOR. OPS CHECK AND LEAK CHECK GOOD. P/N ON 320300-1005, S/N ON 0427, S/ - [SDR SWIA972580](https://openairdocs.org/sdr/SWIA972580.md): Actuator · failed · May 16, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > CONTROL FAULT NAC 1 BAR IN FLIGHT, WOULD NOT RESET. BELOW 180 KTS WE WERE ABLE TO RESET AND USE FLAPS NORMALLY. PERFORMED A WIPER TEST AND FOUND THE LEFT NACELLE FLAP ACTUATOR BAD. REMOVED AND REPLACED IAW AMM 27-50-09. OPS CHECK GOOD AND PERFORMED IAW RII - [SDR SWIA972579](https://openairdocs.org/sdr/SWIA972579.md): Flap · malfunctioned · May 14, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > ASYMMETRY ON FINAL WHEN FLAPS SELECTED 45. RIGHT INBOARD FLAPS DID NOT GO DOWN ALL THE WAY. AVERAGE INDICATION OF 40 DEGREES. FLAPS WOULD NOT RETRACT AFTER LANDING (THE INBOARD). RAN QRH TO RAISE FLAPS, INBOARD FLAPS NOW INOP. RERACKED FLAP COMPUTER AND C - [SDR SWIA972408](https://openairdocs.org/sdr/SWIA972408.md): Wire · shorted · Mar 2, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > DURING CRUISE FLIGHT FLAP AND ADVANCED SWS LIGHT ON MAP AND ASSYMETRY, CONTROL FAULT AND DISAGREEMENT ON OVERHEAD. MADE FLAPS 0 LANDING. ISOLATED AND THEN MEGGERED EACH WIRE FOR THE ENTIRE FLAP SYSTEM. FOUND WIRE W602-009-22 SHORTED TO GROUND. REPLACED WIR - [SDR SWIA972404](https://openairdocs.org/sdr/SWIA972404.md): Control Unit · failed · Feb 28, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > FLAP CONTROL FAULT AT FL260 DURING CRUISE. RESET ONCE BUT REOCCURRED AGAIN AFTER ABOUT 10 MINUTES AND WOULD NOT RESET. COULD NOT RESET ON GROUND. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT IAW 27-50-06. FLAPS OPS CHECK GOOD. CYCLED MORE - [SDR SWIA972414](https://openairdocs.org/sdr/SWIA972414.md): Warning Light · illuminated · Feb 25, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > CONTROL FAULT LIGHT ILLUMINATED IN FLIGHT. WOULD RESET MOMENTARILY BUT ALWAYS CAME BACK. SECOND LIGHT BAR ON FLAP ANNUNCIATOR OUTBOARD PAIR ILLUMINATED. DIVERTED TO TWF FROM SUN. REWIRED RIGHT FLAP SYSTEM FROM WING TO FUSELAGE - INBOARD FLAP ACTUATORS, OUT - [SDR SWIA972386](https://openairdocs.org/sdr/SWIA972386.md): Actuator · faulty · Feb 22, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > DEPARTURE FROM RNO FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 6 DEGREES FOR OUTBOARD PAIRS, WITH A CORRESPONDING FLAP FAULT. RESET WOULD NOT CLEAR THE FAULT. LEFT OUTBOARD FLAP ACTUATOR FOUND TO HAVE FLUCUATING OHMS. REPLACED LEFT OUTBOARD ACTUATOR. FOUND - [SDR SWIA972381](https://openairdocs.org/sdr/SWIA972381.md): Actuator · failed · Feb 21, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > ON GROUND RECEIVED FLAP CONTROL FAULT. REMOVED AND REPLACED LEFT OUTBOARD FLAP ACTUATOR REF MM 27-50-09 AND RII 27-307. RAN FLAPS, OPS CHECKS GOOD WITH NO LEAKS NOTED. ALL REMOVED PANELS SECURED. - [SDR SWIA972374](https://openairdocs.org/sdr/SWIA972374.md): Fcu · failed · Feb 18, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > RECEIVED FLAP CONTROL FAULT ON GROUND. FLAPS WOULD NOT RESET. REMOVED AND REPLACED FCU IAW EMB MM 27-50-06. OPS CHECK GOOD. (P/N: 3077500-1007) (S/N ON: 0093) (S/N OFF: 0033). - [SDR SWIA972349](https://openairdocs.org/sdr/SWIA972349.md): Connector · contaminated · Feb 9, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > FLAPS GET DISAGREEMENT WHEN RETRACTING FROM 15 DEGREES TO 0 DEGREES. CLEANED DEICE FLUID FROM BOTH OUTBOARD FLAP CONNECTOR PLUGS. OPS CHECK GOOD. - [SDR SWIA972339](https://openairdocs.org/sdr/SWIA972339.md): Uplock Switch · malfunctioned · Feb 8, 2001 · N195SW · Emb EMB120ER · Landing Gear Position and Warning > LEFT GEAR DOOR INTERMITTENTLY WILL NOT RETRACT. (RED DISAGREEMENT LIGHT ON COLUMN A ON). ADJUSTED LEFT GEAR ACTUATOR IAW 32-30-00 AND UPLOCK PROX SWITCH ADJUSTED IAW 32-61-01. OPS CHECK GOOD. - [SDR SWIA972322](https://openairdocs.org/sdr/SWIA972322.md): Actuator · failed · Feb 2, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > AFTER TAKEOFF, WHEN FLAPS WERE RETRACTED, CONTROL FAULT AND INBOARD FLAP LIGHT BAR (2ND DIGIT) ILLUMINATED. WHEN RESET PRESSED, LIGHT EXTINGUISHED APPROXIMATELY 10 SECONDS, THEN RE-ILLUMINATED. RETURNED TO FAT. MEGGER TESTED RIGHT INBOARD FLAP ACTUATOR WIRE - [SDR SWIA972315](https://openairdocs.org/sdr/SWIA972315.md): Wire · chafed · Feb 1, 2001 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > DURING FLAP RETRACTION ON GROUND, GOT FLAP CONTROL FAULT AND ADVANCED SWS WITH INBOARD PAIR NOT MOVING. CLEARED ONLY AFTER RESET. REPLACED CHAFED WIRE AT LEFT INBOARD FLAP ACTUATOR CANNON PLUG. REPLACED RIGHT INBOARD FLAP ACTUATOR CANNON PLUG AND REPLACED - [SDR SWIA972251](https://openairdocs.org/sdr/SWIA972251.md): Fcu · malfunctioned · Jan 3, 2001 · N195SW · Emb EMB120ER · Trailing Flap Position Indicating System > DURING DESCENT, FLAP CONTROL FAULT LIGHT ILLUMINATES WITHOUT SELECTING ANY FLAPS, INBOARD PAIR FLASHING PANEL. QRH PROCEDURE CLEARED FAULT. REMOVED AND REPLACED FCU DUE TO UNCOMMAND FLAPS FAULTS INBOARD. AFTER CYCLING FLAPS SEVERAL TIMES WITH OUT DUPLICATING - [SDR SWIA972206](https://openairdocs.org/sdr/SWIA972206.md): Pump · failed · Dec 21, 2000 · N195SW · Emb EMB120ER · Hydraulic Pump (Electric/Engine), Main > CLIMBING OUT OF SLC HYDRAULIC ''LOW LEVEL'' LIGHT GAUGE SHOWED IN YELLOW TRENDING TO EMPTY. ALSO ''LOW PRESS H'' ON HYDRAULIC PANEL. RETURNED TO SLC FOR NORMAL LANDING, GEAR AND FLAPS OPS NORMAL. REPLACED LEFT ENGINE DRIVEN HYDRAULIC PUMP IAW 29-10-03. SERV - [SDR SWIA972187](https://openairdocs.org/sdr/SWIA972187.md): Servo · failed · Dec 18, 2000 · N195SW · Emb EMB120ER · Elevator Tab Control System > ELECTRIC TRIM IS FREEZING UP AND WILL NOT WORK IN THE AIR. REMOVED AND REPLACED ELEVATOR TRIM SERVO IAW MM 27-00-00. OPERATIONAL CHECKS GOOD. - [SDR SWIA972045](https://openairdocs.org/sdr/SWIA972045.md): Solenoid Valve · failed · Oct 23, 2000 · N195SW · Emb EMB120ER · Landing Gear Retraction/Extension System > LANDING GEAR WOULD NOT COME DOWN. USED ELECTRICAL OVERIDE/EXTENSION PROCEDURE TO LOWER GEAR. TROUBLESHOT SYSTEM IAW TROUBLESHOOTING GUIDE 32-31-00. REMOVED LANDING GEAR SOLENOID VALVE AND INSTALLED SERVICEABLE UNIT IAW MM 32-32-03 AND REMOVED ELECTRIC OVERR - [SDR SWIA972042](https://openairdocs.org/sdr/SWIA972042.md): Relay · failed · Oct 22, 2000 · N195SW · Emb EMB120ER · Landing Gear Selector > LANDING GEAR WOULD NOT COME DOWN. USED GEAR EXTENSION BY ELECTRICAL OVERRIDE PROCEDURES. REMOVED AND REPLACED LANDING GEAR RELAY BOX IAW 32-31-02, OPS CHECKS GOOD. P/N ON: 120-43270-501, S/N: 120119, S/N OFF: 120151. - [SDR SWIA971706](https://openairdocs.org/sdr/SWIA971706.md): Switch · failed · Feb 23, 2000 · N195SW · Emb EMB120ER · Airfoil Anti/De-ice System > OUTBOARD RIGHT STABILIZER FAILED ON BOTH TIMERS 1 AND 2. RETURNED TO THE FIELD. REMOVED AND REPLACED OUTBOARD HORIZONTAL STABILIZER PRESSURE SWITCH. ALSO, REMOVED AND REPLACED HORIZONTAL STABILIZER OUTBOARD EJECTOR VALVE. OPS CHECKS GOOD, PN ON: 211C11718 - [SDR SWIA971432](https://openairdocs.org/sdr/SWIA971432.md): Hose · failed · Mar 9, 1999 · N195SW · Emb EMB120ER · Airfoil Anti/De-ice System > LEFT AND RIGHT OUTBOARD AND VERTICAL STAB DEICE BOOTS FAILED, BOTH TIMERS, HEAVY AND LIGHT. RETURNED TO SLC. REMOVED AND REPLACED FLEXIBLE BLEED AIR HOSE ON LEFT ENGINE IAW 30-00-00. OPS CHECK SYSTEM IAW 30-10-00. NO DEFECTS NOTED. - [SDR SWIA971344](https://openairdocs.org/sdr/SWIA971344.md): Deice Boot · failed · Dec 26, 1998 · N195SW · Emb EMB120ER · Airfoil Anti/De-ice System > OUTBOARD STAB DEICE BOOTS FAILED ON TIMERS 1 AND 2 AND CYCLE LIGHT AND HEAVY. RETURNED TO SLC. REPLACED EJECTOR VALVE WITH A SERVICEABLE UNIT IAW MM 30-10-04, OPS CHECK GOOD. - [SDR SWIA971288](https://openairdocs.org/sdr/SWIA971288.md): Pressurization · malfunctioned · Oct 12, 1998 · N195SW · Emb EMB120ER · Cabin Pressure Control System > CREW REPORTED CABIN PRESSURIZATION DIFFICULT TO OPERATE IN AUTO OR MANUAL. RETURNED TO SLC. INSPECTED DOOR AND EMERGENCY EXITS SEALS, FOUND GOOD. PRESSURIZED A/C ON GROUND IN AUTO AND MANUAL CONTROL (2000 TO 5 PSI). OPS CHECKS GOOD. - [SDR SWIA971274](https://openairdocs.org/sdr/SWIA971274.md): Prox Sensor · failed · Oct 3, 1998 · N195SW · Emb EMB120ER · Landing Gear Position and Warning > LEFT MAIN 'A' SYSTEM GREEN LIGHT STAYED ON AFTER GEAR RETRACTION. RECYCLED 3 TIMES, RED TRANSIT LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS PUT BACK DOWN, GREEN LIGHT WENT OUT IN BUMPS AT ABOUT 16,000 FT. RETURNED TO SLC, REPLACED BAD LEFT GEAR PROXIMITY SENSOR - [SDR SWIA971221](https://openairdocs.org/sdr/SWIA971221.md): Flap Indication · malfunctioned · Jul 8, 1998 · N195SW · Emb EMB120ER · Trailing Flap Position Indicating System > TAKEOFF PLUS 3 MINUTES GOT FLAP DISAGREEMENT WHEN INITIATED FLAP RETRACTION AFTER TAKEOFF. RETURNED TO SLC. RESET FLAP SYSTEM AND RAN FLAPS SEVERAL TIMES. OPS CHECKS NORMAL. - [SDR SWIA97886](https://openairdocs.org/sdr/SWIA97886.md): Control Box · failed · Apr 16, 1997 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > ON SELECTING 45 DEGREES, FLAPS DISAGREEMENT WARNING OCCURRED. PRIOR TO TOUCHDOWN DISAGREEMENT LIGHT WENT OUT. CHECKED FLAP TRACKS AND REPLACED FLAP CONTROL BOX. CYCLED FLAPS SEVERAL TIMES AND OPS CHECKS GOOD. - [SDR SWIA97854](https://openairdocs.org/sdr/SWIA97854.md): T6 Indicator · malfunctioned · Feb 2, 1997 · N195SW · Emb EMB120ER · Engine EGT/TIT Indicating System > ON TAKEOFF ROLL, RIGHT T.6 FLUCTUATES. GAUGE WENT FROM 0 DEG TO 2,000 DEGREES. ENGINE PARAMETERS STABLE. TAKE OFF ABORTED. INSTALLED T6 INDICATOR, RAN RIGHT ENGINE ON GROUND THROUGH SEVERAL PARAMETERS AND IT OPERATED NORMAL AT THIS TIME. - [SDR SWIA97840](https://openairdocs.org/sdr/SWIA97840.md): Control Relay · failed · Jan 24, 1997 · N195SW · Emb EMB120ER · Landing Gear Selector > AFTER DEPARTURE, PLACED GEAR HANDLE IN UP POSITION HAD 6 GREEN AND 6 LED INTRANSIT LIGHTS, GEAR WOULD NOT DO ANYTHING. ALL OTHER INDICATIONS NORMAL. RETURNED TO FIELD. DUPLICATING SQUAWK IN HANGAR, SLAVED IN LANDING CONTROL BOX BUT DISCREPANCY STILL EXISTS - [SDR SWIA97830](https://openairdocs.org/sdr/SWIA97830.md): Valve · failed · Jan 13, 1997 · N195SW · Emb EMB120ER · Landing Gear Door Retract Section > LANDING GEAR WOULD NOT RETRACT ON TAKEOFF. RETURNED TO FIELD. REPLACED GEAR DOOR SOLENOID VALVE WITH A SERVICEABLE UNIT. PERFORMED NUMEROUS GEAR SWINGS, OPS AND LEAKS CHECKS GOOD. - [SDR SWIA95806](https://openairdocs.org/sdr/SWIA95806.md): Control Box · malfunctioned · Dec 30, 1996 · N195SW · Emb EMB120ER · Landing Gear Position and Warning > RIGHT MAIN GEAR SHOWED UNSAFE LIGHTS AFTER 3 CYCLES OF LANDING GEAR. REPLACED LANDING GEAR CONTROL BOX, SYSTEM CHECKS NORMAL, RETRACTION TEST CHECKS NORMAL. CHECKED ACTUATOR ROD END AND A AND B HARNESS CHECKED FOR CONTAMINATION, ALL CHECKS GOOD. - [SDR SWIA95735](https://openairdocs.org/sdr/SWIA95735.md): Control Unit · malfunctioned · May 6, 1996 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > AFTER TAKEOFF, FLAPS WOULD NOT RETRACT TO THE FULL UP POSITION, TWO SEGMENTS OUTBOARD, ONE SEGMENT NACELLE, ONE SEGMENT INBOARD, FOUR FLAP DISAGREEMENT INDICATION. CLEANED FLAP TRACK AND ROLLERS. REMOVED AND REPLACED FLAP CONTROL UNIT WITH SERVICEABLE UNIT. - [SDR SWIA95731](https://openairdocs.org/sdr/SWIA95731.md): Windshield · failed · Apr 20, 1996 · N195SW · Emb EMB120ER · Flight Compartment Windows > AT 15,000 FEET, HEARD LOUD THUMP AND LEFT WINDSHIELD CRAZED. NO EVIDENCE OF BIRD STRIKE. SLOWED DOWN AND STARTED DESCEND. NO FURTHER PROBLEMS. REPLACED RIGHT WINDSHIELD PER MM 56-10-01. - [SDR SWIA95565](https://openairdocs.org/sdr/SWIA95565.md): Connector · miswired · Apr 29, 1995 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > FLAP CONTROL FAULT. INBOARD FLAPS STAY AT 15 DEGREES. TROUBLESHOT SYSTEM. FOUND INBOARD FLAP ACTUATOR CONNECTOR MISWIRED. REPLACED CANNON CONNECTOR AND WIRED CORRECTLY. OPERATIONALLY CHECKS NORMAL ON GROUND. - [SDR SWIA95564](https://openairdocs.org/sdr/SWIA95564.md): Connector · dirty · Apr 27, 1995 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > UPON SELECTING FLAPS TO 25 DEGREES, A CONTROL FAULT WAS EXPERIENCED. RESET FLAPS. TRIED NEW CONTROL BOX. STILL FAULTING. FOUND MOISTURE IN LEFT INBOARD FLAP CANNON PLUG. CLEANED BOTH LEFT AND RIGHT INBOARD FLAP ACTUATOR CANNON PLUGS. CYCLED FLAPS NUMEROUS - [SDR SWIA95543](https://openairdocs.org/sdr/SWIA95543.md): Connectors · dirty · Mar 5, 1995 · N195SW · Emb EMB120ER · Trailing Edge Flap Control System > INBD FLAP CONTROL FAULT WHEN FLAPS ARE EXTENDED BEYOND 15 DEG. CLEANED FLAP TRACKS. ALSO REMOVED, CLEANED AND REINSTALLED FLAP ACTUATOR CANNON PLUGS. OPS CHECKS GOOD AT THIS TIME. SEE FL 73078. - [SDR SWIA95528](https://openairdocs.org/sdr/SWIA95528.md): Connector · dirty · Feb 14, 1995 · N195SW · Emb EMB120ER · Trailing Edge Flap Actuator > FLAP MAP LIGHTS ILLUMINATED AND CONTROL FAULT WOULD NOT CLEAR. CLEANED CANNON PLUGS ON FLAP ACTUATORS OF BOTH LEFT AND RIGHT INBOARD AND OUTBOARD FLAPS. OPS CHECKS GOOD. ## 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 = 'N195SW' AND deregistration_id = 'N195SW-2004-09-28' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N195SW-2004-09-28/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.