# Service difficulty reports: N194SW, cancelled Nov 24, 2003

A list on [N194SW, cancelled Nov 24, 2003](https://openairdocs.org/deregistered/N194SW-2003-11-24.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SWIA200110242](https://openairdocs.org/sdr/SWIA200110242.md): Indicator · malfunctioned · Oct 9, 2001 · N194SW · Emb EMB120ER · Engine BMEP/Torque Indicating
  > LEFT TORQUE GAUGE ROLLER BACK TO ZERO ON TAKEOFF. SYSTEM AUTO FEATHERED. ABORTED TAKEOFF. INSPECTED AND CLEANED LEFT ENGINE TORQUE PROBE CANNON PLUG. NO DEFECTS NOTED. REPLACED LEFT ENGINE TORQUE INDICATOR. RAN LEFT ENGINE. OPS CHECK GOOD.
- [SDR SWIA972656](https://openairdocs.org/sdr/SWIA972656.md): Actuator · failed · Jun 25, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > OUTBOARD FLAPS DO NOT EXTEND FOR LANDING. PERFORMED TEST WITH BREAKOUT BOX AND LEFT OUTBOARD ACTUATOR FAILED WIPER TEST. INSTALLED SERVICEABLE UNIT IAW MM 27-50-09 AND CYCLED WITH BREAKOUT BOX AND WITH AIRCRAFT SYSTEM. ALL OPS AND LEAK CHECKS GOOD. PN ON 32
- [SDR SWIA972655](https://openairdocs.org/sdr/SWIA972655.md): Actuator · failed · Jun 24, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > CONTROL FAULT OCCURS IN FLIGHT, WILL NOT RESET. OUTBOARD FLAPS FLASHING. REMOVED AND REPLACED BOTH OUTBOARD FLAP ACTUATORS IAW 27-50-04. RAN FLAPS NUMEROUS TIMES, OPS AND LEAK CHECK GOOD ON BOTH SIDES. PN ON 320300-1007 SN ON RT 1148, LT 0026A SN OFF RT
- [SDR SWIA972650](https://openairdocs.org/sdr/SWIA972650.md): Control Unit · failed · Jun 20, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON DESCENT THROUGH 13,000 FT CONTROL FAULT/SWS WARNING CAUTIONS ILLUMINATE WITH NO MOVEMENT OF FLAP HANDLE. AFTER PUSHING RESET, CAUTIONS DISAPPEAR AND THEN REAPPEAR AFTER 2-3 SECONDS. WAS ABLE TO RESET AND USE FLAPS NORMALLY ON 3RD ATTEMPT. REMOVED AND REPL
- [SDR SWIA972463](https://openairdocs.org/sdr/SWIA972463.md): Actuator · failed · Mar 28, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > INBOARD FLAPS REMAIN AT 25 DEGREES AFTER LANDING WITH FLAP HANDLE AT 0 DEGREES. REMOVED AND REPLACED RT I/B FLAP ACUTATOR. USED BEAKOUT BOX. ACTUATOR POS BAD AT 15-25 DEGREES SETTING. REF MM 27-50-07 & RII 27-307. NO LEAKS NOTED. OPS CHECK GOOD. ALL OPE
- [SDR SWIA972460](https://openairdocs.org/sdr/SWIA972460.md): Panel · malfunctioned · Mar 24, 2001 · N194SW · Emb EMB120ER · Stall Warning System
  > STALL WARNING ON TAKEOFF ROLL. ABORTED TAKEOFF. REMOVED AND REPLACED STALL WARNING TEST PANEL IAW EMB120 MM 27-34-08. OPS CHECK GOOD. P/N: 120-34428-505, S/N ON: 120290, S/N OFF: 120269.
- [SDR SWIA972405](https://openairdocs.org/sdr/SWIA972405.md): Connector · dirty · Mar 1, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > ON APPROACH INBOARD FLAP PAIRS STUCK AT 25 DEGREES. UABLE TO RAISE OR LOWER INBOARD FLAPS WITH FLAP HANDLE. CLEANED INBOARD FLAP ACTUATOR CANNON PLUGS AND RERACKED FCU. OPS CHECK NORMAL.
- [SDR SWIA972328](https://openairdocs.org/sdr/SWIA972328.md): Actuator · malfunctioned · Feb 2, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP CONTROL FAULT ON INBOARD FLAP PAIR, WHEN SELECTING FLAPS FROM 15 DEGREES TO 25 DEGREES ON LANDING. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR. OPS CHECKS AND LEAK CHECKS GOOD. P/N ON 320300-1005, S/N ON 0067, S/N OFF 0067.
- [SDR SWIA972305](https://openairdocs.org/sdr/SWIA972305.md): Connector · contaminated · Jan 21, 2001 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > OUTBOARD FLAPS WOULD NOT RAISE OR LOWER FROM FLAPS 15 DEGREES AFTER DEICE. FOUND DEICE FLUID ON OUTBOARD FLAP CANNON PLUGS (LEFT AND RIGHT). CLEANED CANNON PLUGS WITH CONTACT CLEANER. OPS CHECK GOOD.
- [SDR SWIA972211](https://openairdocs.org/sdr/SWIA972211.md): Smoke · detected · Dec 24, 2000 · N194SW · Emb EMB120ER · Air Distribution System
  > DEPARTING SLC, APPROXIMATELY 1500 AGL, CABIN FILLED WITH SMOKE, INCLUDING COCKPIT. DONNED MASKS, COMPLETED QRH PROCEDURE FOR SMOKE. SECURED BLEEDS AND PACKS AND AFTER 5 MINUTES SMOKE DISSIPATED. SMELLED LIKE GLYCOL; HOWEVER, IT FILLED THE PLANE QUICKLY - DE
- [SDR SWIA972113](https://openairdocs.org/sdr/SWIA972113.md): Connector · contaminated · Nov 15, 2000 · N194SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > WHEN RETRACTING FLAPS FROM 15 DEGREES TO UP ON DEPARTURE CONTROL FAULT PERIODICALLY AND THEN EXTINGUISHES. CLEANED DEICE FLUID FROM O/B FLAP ACTUATOR CANNON PLUGS. OPS CHECK GOOD.
- [SDR SWIA971714](https://openairdocs.org/sdr/SWIA971714.md): Fuse · failed · Feb 26, 2000 · N194SW · Emb EMB120ER · Battery/Charger System
  > FOS AHRS FAILED ABOUT 10 MINUTES INTO FLIGHT, LOST BOTH ADI AND EHSI ATTITUDE AND HEADING. RETURNED TO SLC. INSTALLED A SERVICEABLE FUSE FOR THE 24 VOLT EMERGENCY BATTERY SWITCH. RAN THE AIRCRAFT FOR 20 MINUTES AND AHRS, OPS CHECKS GOOD IAW MM 342100.
- [SDR SWIA971461](https://openairdocs.org/sdr/SWIA971461.md): Indication · malfunctioned · Apr 3, 1999 · N194SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP CONTROL FAULT UPON APPROACH TO AIRPORT, DID A GO AROUND AND FLAPS RESET. MADE NORMAL LANDING. OPS CHECKED FLAPS FOUR TIMES WITH NO PROBLEMS NOTED. COULD NOT DUPLICATE DISCREPANCY.
- [SDR SWIA971106](https://openairdocs.org/sdr/SWIA971106.md): Bleed Line · ruptured · Mar 4, 1998 · N194SW · Emb EMB120ER · Pneumatic Distribution System
  > AFTER TAKEOFF, THE DUCT LEAK LIGHT ILLUMINATED, RETURNED TO LAX. MEL 32-21-1. REPLACED RUPTURED BLEED LINE AT RIGHT PACK SHUT OFF VALVE. LEAK AND OPS CHECKS GOOD.
- [SDR SWIA971067](https://openairdocs.org/sdr/SWIA971067.md): De-Ice Monitor · failed · Jan 7, 1998 · N194SW · Emb EMB120ER · Air Intake Anti/De-Ice System
  > RIGHT ENGINE INTAKE DE-ICE INOP AFTER 10 MIN. RETURNED TO SLC. REPLACED DE-ICE MONITOR IAW MM 30-00-00. RAN ENGINES FOR 30 MINUTES, OPS CHECKS GOOD.
- [SDR SWIA971036](https://openairdocs.org/sdr/SWIA971036.md): Control Box · malfunctioned · Nov 28, 1997 · N194SW · Emb EMB120ER · Landing Gear Selector
  > HAD TO CYCLE LANDING GEAR LEVER 4 TIMES TO BRING LANDING GEAR DOWN. DURING ATTEMPTS THERE WAS NO RESPONSE. JACKED AIRCRAFT AND OPERATED GEAR IN NORMAL AND FREE FALL, OPS CKS GOOD. REPLACED LANDING GEAR CONTROL BOX, CLEANED GEAR CONTROL AND INDICATION CONNEC
- [SDR SWIA97812](https://openairdocs.org/sdr/SWIA97812.md): Hub Cap · missing · Dec 27, 1996 · N194SW · Emb EMB120ER · Wheel/Ski/Float
  > ON TAKEOFF ROLL AT 80 KNOTS, RIGHT ANTI-SKID LIGHT ILLUMINATED FOLLOWED BY BRAKES LIGHT ON MAP AND CAUTION WARNING LIGHTS. ABORTED TAKEOFF. FOUND NR 3 MAIN TIRE/WHEEL ASSEMBLY HUB CAP MISSING. INSTALLED SERVICEABLE HUB CAP, TAXIED AIRCRAFT. ANTI-SKID OPERA
- [SDR SWIA95781](https://openairdocs.org/sdr/SWIA95781.md): Latch · not latched · Nov 21, 1996 · N194SW · Emb EMB120ER · Fluid Service Doors
  > SERVICE DOOR LIGHT CAME ON DURING TAKEOFF. ABORTED TAKEOFF. LIGHT WENT OUT. FOUND LATCH ON FORWARD OUTBOARDD FUEL DOOR NOT LATCHED. INSPECTED DOOR AND LATCH RECEPTACLE. ADJUSTED AND OPS CHECKS GOOD.
- [SDR SWIA95780](https://openairdocs.org/sdr/SWIA95780.md): Fasteners · failed · Nov 19, 1996 · N194SW · Emb EMB120ER · Fluid Service Doors
  > SERVICE DOOR LIGHT CAME ON SHORTLY AFTER DEPARTURE. RETURNED TO AIRPORT. CAMLOC POPPED. REPLACED BOTH RECEPTACLES FOR PRESSURE FUELING OUTBD DOOR, CHECKS GOOD.
- [SDR SWIA95666](https://openairdocs.org/sdr/SWIA95666.md): Cables · worn · Oct 30, 1995 · N194SW · Emb EMB120ER · Rudder Tab Control System
  > RUDDER TRIM CABLES WORN. REMOVED AND REPLACED RUDDER TRIM CABLES IAW EMB MM 2-00-01, OPS CHECK OK.
- [SDR SWIA95665](https://openairdocs.org/sdr/SWIA95665.md): Cables · worn · Oct 30, 1995 · N194SW · Emb EMB120ER · Elevator Tab Control System
  > ELEVATOR TRIM CABLES WORN. REMOVED AND REPLACED ELEVATOR TRIM CABLES IAW EMB MM 27-00-01, OPS CHECK OK.
- [SDR SWIA95664](https://openairdocs.org/sdr/SWIA95664.md): Control Cable · worn · Oct 30, 1995 · N194SW · Emb EMB120ER · Rudder Control System
  > RT RUDDER I/B CABLE WORN, AFT SECTION. REMOVED AND REPLACED RT I/B RUDDER CABLE IAW EMB MM 27-00-01, OP CHECK OK.
- [SDR SWIA95663](https://openairdocs.org/sdr/SWIA95663.md): Control Cable · worn · Oct 30, 1995 · N194SW · Emb EMB120ER · Rudder Control System
  > RT RUDDER O/B CABLE WORN, AFT SECTION. REMOVED AND REPLACED RT O/B RUDDER CABLE IAW EMB MM 27-00-01, OPS CHECK OK.
- [SDR SWIA95662](https://openairdocs.org/sdr/SWIA95662.md): Clips · cracked · Oct 29, 1995 · N194SW · Emb EMB120ER · Wing Miscellaneous Structure
  > RT WING RIB 15 HAS CRACKED CLIPS. REMOVED AND REPLACED THREE SKIN WING SUPPORT CLIPS ON RT WING RIB 15 IAW SB 120-57-0031 AND RII-33.
- [SDR SWIA95661](https://openairdocs.org/sdr/SWIA95661.md): Clips · cracked · Oct 29, 1995 · N194SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LT WING RIB 15 AND 16 HAVE SEVERAL CLIPS CRACKED. REMOVED AND REPLACED 5 WING SKIN SUPPORT CLIPS ON LT WING RIB 15 AND 16 IAW SB 120-57-0031 AND RII-33.
- [SDR SWIA95592](https://openairdocs.org/sdr/SWIA95592.md): Control Unit · malfunctioned · Jun 12, 1995 · N194SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT ON RETRACTION AFTER TAKEOFF. REPLACED FLAP CONTROL BOX, CYCLED FLAP 10 TIMES, OPS CKS GOOD IN ALL MODES OF OPERATION, SEE F/L 75838.
- [SDR SWIA95572](https://openairdocs.org/sdr/SWIA95572.md): Torque Sensor · malfunctioned · May 4, 1995 · N194SW · Emb EMB120ER · Engine BMEP/Torque Indicating
  > RIGHT ENGINE TORQUE GAUGE INOPERATIVE. FLUCTUATES. REPLACED THE RIGHT TORQUE SIGNAL CONDITIONER. CLEANED AND SECURED CONNECTORS. OPERATIONALLY CHECKS GOOD.
- [SDR SWIA95570](https://openairdocs.org/sdr/SWIA95570.md): Clips · cracked · Apr 24, 1995 · N194SW · Emb EMB120ER · Wing Miscellaneous Structure
  > LEFT WING OUTBOARD OF NACELLE HAS FIVE CRACKED CLIPS. FOUR AT POSITION YA-4533.5, AND ONE AT YA-6750. FABRICATED SAME AS ORIGINAL AND INSTALLED CLIPS AT YA-4533.5 (FOUR EACH) AND YA-6750 (ONE EACH).
- [SDR SWIA95536](https://openairdocs.org/sdr/SWIA95536.md): Prox Sensor · failed · Feb 28, 1995 · N194SW · Emb EMB120ER · Elevator Tab Control System
  > TAKEOFF AURAL TRIM AURAL WARNING WITH TRIM IN THE GREEN ARC. FOUND LEFT ELEVATOR TRIM TAB PROX SENSOR INTERNALLY SHORTING AND CAUSING AURAL WARNING UNIT CB TO TRIP. REPLACED LEFT ELEVATOR TRIM TAB PROX SENSOR IAW MM 27-32-05. OPS CKS GOOD. SEE FL 75461.

## 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 = 'N194SW' AND deregistration_id = 'N194SW-2003-11-24'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N194SW-2003-11-24/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.