# Service difficulty reports: N196SW, cancelled Jan 26, 2007

A list on [N196SW, cancelled Jan 26, 2007](https://openairdocs.org/deregistered/N196SW-2007-01-26.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 2 · 70 reports

- [SDR SWIA200413939](https://openairdocs.org/sdr/SWIA200413939.md): Rib · cracked · Aug 23, 2004 · N196SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > RIB ATTACH ANGLE CRACKED ON RIGHT WING, RIB 21, TOP SURFACE OF RIB, BETWEEN STRINGERS 3 AND 4. ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR PART IAW EMB 120 SRM 51-25-00, 51-40-00, 51-30-01, 51-40-01, 51-40-02, 51-40-05 AND REF 57-20-07 FIG 6 ITEM 90.
- [SDR SWIA200413938](https://openairdocs.org/sdr/SWIA200413938.md): Rib · cracked · Aug 23, 2004 · N196SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > LEFT WING FORWARD RIB 17 CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-70-05 FIG 1 AND 51-12-02.
- [SDR SWIA200413937](https://openairdocs.org/sdr/SWIA200413937.md): Rib · cracked · Aug 23, 2004 · N196SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > LEFT WING FORWARD RIB 21 IS CRACKED AT TOP. ITEM FOUND AT C-CHECK INSPECTION. RIB REPAIRED IAW EMB 120 SRM 51-12-02 & 57-20-07 FIG 203.
- [SDR SWIA200413936](https://openairdocs.org/sdr/SWIA200413936.md): Frame · cracked · Aug 23, 2004 · N196SW · Emb EMB120ER · Fuselage Main, Frame
  > FRAME 9 LEFT AND RIGHT CRACKED AT STRINGER 9 CABIN AREA. ITEM FOUND AT C-CHECK INSPECTION. FRAME 9 LEFT AND RIGHT AT STRINGER 9 REPAIRED IAW EMB SB 120-53-0073 STEPS 3C AND 3E.
- [SDR SWIA200413935](https://openairdocs.org/sdr/SWIA200413935.md): Floorbeam · corroded · Aug 23, 2004 · N196SW · Emb EMB120ER · Fuselage Main, Floor Beam
  > SURFACE CORROSION FOUND ON FLOOR SUPPORT AT FS 4214.0 - FS 5118-0 LT FLOORBEAM. ITEM FOUND AT C-CHECK INSPECTION. FLOOR SUPPORT REPAIRED IAW EMBRAER REF 1C2004-145/4092 DATE AUG 31, 2004.
- [SDR SWIA200413605](https://openairdocs.org/sdr/SWIA200413605.md): Window · cracked · Jul 26, 2004 · N196SW · Emb EMB120 · Flight Compartment Windows
  > 2 CRACKS APPROXIMATELY 3 INCHES IN LENGTH AT LT DIRECT VISION WINDOW AT LOWER FORWARD CORNER. ITEM FOUND AT C CHECK INSPECTION.
- [SDR SWIA200413455](https://openairdocs.org/sdr/SWIA200413455.md): Bulkhead · cracked · Jun 17, 2004 · N196SW · Emb EMB120ER · Nacelle/Pylon, Bulkhead/Firewall
  > RIGHT NACELLE OUTBOARD BULKHEAD CRACKED OUT AT OUTBOARD TAILPIPE SUPPORT IN NUT PLATE AREA. FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-70-05.
- [SDR SWIA200413346](https://openairdocs.org/sdr/SWIA200413346.md): Annunciator · malfunctioned · May 20, 2004 · N196SW · Emb EMB120ER · Trailing Edge Flap Control System
  > (CONTROL FAULT) ILLUMINATED ON FLAP PANEL AND MAP. REPLACED FLAP ANNUNCIATOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200413104](https://openairdocs.org/sdr/SWIA200413104.md): Control Unit · malfunctioned · Apr 2, 2004 · N196SW · Emb EMB120ER · Trailing Edge Flap Control System
  > DURING TAKEOFF ROLL FLAP AND ADVANCED SWS ILLUMINATED ON MAP WITH ASSOCIATED CONTROL FAULT ON FLAP WARNING INDICATION PANEL. COMPLIED WITH QRH RESET. OPERATED NORMALLY REMAINDER OF FLIGHT. REPLACED FLAP CONTROL UNIT IAW MM 27-50-06. OPS CHECKS GOOD.
- [SDR SWIA200413058](https://openairdocs.org/sdr/SWIA200413058.md): Sign · inoperative · Mar 16, 2004 · N196SW · Emb EMB120ER · Light System Wiring
  > EXIT SIGN ABOVE ROW 9 WILL NOT ILLUMINATE. FOUND BROKEN WIRE AT EMERGENCY EXIT SIGN AT ROW 9. INSTALLED SPLICE AT WIRE. OPS CHECKS GOOD.
- [SDR SWIA200413000](https://openairdocs.org/sdr/SWIA200413000.md): Servo · malfunctioned · Feb 27, 2004 · N196SW · Emb EMB120ER · Autopilot Trim Servo
  > ELECTRIC TRIM INOP. REMOVED AND REPLACED ELEVATOR TRIM SERVO. OPS CHECKS GOOD IAW MM 22-10-09.
- [SDR SWIA200312715](https://openairdocs.org/sdr/SWIA200312715.md): Power Supply · inoperative · Dec 22, 2003 · N196SW · Emb EMB120ER · Emergency Lighting
  > FOUR EMERGENCY LIGHTS (CENTER SECTION) AND EXIT LIGHTS INOP. REMOVED AND REPLACED CENTER ELBP, OPS CHECK GOOD.
- [SDR SWIA200312669](https://openairdocs.org/sdr/SWIA200312669.md): Engine · flamed out · Dec 6, 2003 · N196SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > LEFT ENGINE FLAMEOUT ON TAKEOFF AT 50 FEET AGL. RETURNED TO DEN. REMOVED AND REPLACED LEFT ENGINE ASSY PER MM 71-00-00. ENGINE S/N AP0018 SHUT ITSELF DOWN DUE TO A FAILED NR 29 BEARING.
- [SDR SWIA200312517](https://openairdocs.org/sdr/SWIA200312517.md): Door · unsecure · Oct 12, 2003 · N196SW · Emb EMB120ER · Landing Gear Doors
  > AFTER TAKEOFF, NOSE GEAR WOULD NOT RETRACT. FOUND LEFT NOSE GEAR DOOR NOT PROPERLY LATCHED. RESECURED LATCH AS REQUIRED. FUNCTIONAL CHECK OF NOSE GEAR DOORS FOUND GOOD.
- [SDR SWIA200312267](https://openairdocs.org/sdr/SWIA200312267.md): Starter Gen · malfunctioned · Aug 15, 2003 · N196SW · Emb EMB120ER · Starter-Generator
  > APU GEN WENT OFF LINE ON TAXI, SMELT SMOKE THROUGHOUT CABIN. REMOVED AND REPLACED APU STARTER/GEN. OPS CHECK GOOD IAW 24-35-00.
- [SDR SWIA200312247](https://openairdocs.org/sdr/SWIA200312247.md): Proximity Sensor · faulty · Aug 11, 2003 · N196SW · Emb EMB120ER · Landing Gear Position and Warning
  > ON APPROACH, GEAR WOULD NOT EXTEND. RAN THE LDG GEAR EXTENSION BY ELECTRICAL OVERRIDE WITHOUT SUCCESS. RAN LDG GEAR EXTENSION BY FREEFALL AND ALL GREEN A & B LIGHTS ILLUMINATED. REPLACED LEFT 'A' PROXIMITY SENSOR IAW 32-61-01. LANDING GEAR OPS CHECKS GOOD.
- [SDR SWIA200312043](https://openairdocs.org/sdr/SWIA200312043.md): Annunciator · malfunctioned · May 31, 2003 · N196SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP PANEL INDICATES ASYMMETRY, CONTROL FAULT & DISAGREEMENT AT SAME TIME ALONG WITH MECHANICAL FLAP INDICATOR AT 15 DEGREES AND ADVANCED SWS & FLAP AMBER LIGHTS ON MAP. FLAPS DO NOT TEST AND DO NOT RESET AND DO NOT FUNCTION. REMOVED AND REPLACED FLAP ANNUNC
- [SDR SWIA200312036](https://openairdocs.org/sdr/SWIA200312036.md): Bracket · cracked · May 28, 2003 · N196SW · Emb EMB120ER · Trailing Edge Flaps
  > RIGHT FLAP LOWER MOVEABLE PANEL HAS INBOARD ROLLER BRACKET BROKEN. REMOVED AND REPLACED FLAP PANEL ROLLER BRACKET IAW EMB SRM 51-40-02. OPS CHECK GOOD.
- [SDR SWIA200312035](https://openairdocs.org/sdr/SWIA200312035.md): Fcu · malfunctioned · May 27, 2003 · N196SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON TAXI OUT, WHILE SELECTING FLAPS 15 DEGREES, A CONTROL FAULT ON THE FLAP WARNING INDICATOR ILLUMINATED. OUTBOARD FLAPS SHOW ONLY ONE BAR DOWN. INSTALLED SERVICEABLE FCU IAW 27-50-00. OPS CHECK GOOD.
- [SDR SWIA200311928](https://openairdocs.org/sdr/SWIA200311928.md): Power Supply · inoperative · May 1, 2003 · N196SW · Emb EMB120ER · Emergency Lighting
  > FIRST 4 EMERGENCY FLOOR LIGHTS AND FIRST 2 OVERHEAD EMERGENCY LIGHTS OUT. REPLACED FORWARD EMERGENCY LIGHT BATTERY PACK WITH SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200311887](https://openairdocs.org/sdr/SWIA200311887.md): Actuator · malfunctioned · Apr 14, 2003 · N196SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > CONTROL FAULT RECEIVED ON OUTBOARD FLAPS. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR IAW MM 27-53-01 AND 27-53-05. NO LEAKS NOTED. OPS CHECK GOOD.
- [SDR SWIA200311886](https://openairdocs.org/sdr/SWIA200311886.md): Annunciator · malfunctioned · Apr 12, 2003 · N196SW · Emb EMB120ER · Trailing Edge Flap Control System
  > BOTH OUTBOARD FLAPS FLUTTER UP TO 5 DEGREES WHEN IN THE 15 DEGREE AND 25 DEGREE POSITIONS. NO FAILURE INDICATED ON THE FLAP CONTROL PANEL. REPLACED FCU AND ANNUNCIATOR WITH VERSION II. OPS CHECK GOOD.
- [SDR SWIA200311858](https://openairdocs.org/sdr/SWIA200311858.md): Landing Gear · malfunctioned · Mar 30, 2003 · N196SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LEFT MAIN LANDING GEAR INDICATION REMAINS RED ON RETRACTION AND SEEMS TO HANG. MAINTENANCE SWUNG GEAR APPROXIMATELY 20 TIMES. NO DEFECTS NOTED. PERFORMED MAIN AND NOSE LANDING GEAR EXTENSION/RETRACTION HYDRAULIC CIRCUIT TEST AS PER 32-32-00. OPS CHECK GOOD
- [SDR SWIA200311822](https://openairdocs.org/sdr/SWIA200311822.md): Warning Light · illuminated · Feb 21, 2003 · N196SW · Emb EMB120ER · Fuel Control/Turbine Engines
  > EEC LEFT FAILURE ON TAKEOFF ROLL. ABORTED TAKEOFF. RAN VARIOUS EEC-RELATED TESTS, COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD AT THIS TIME. NO DEFECTS NOTED LEFT ENGINE.
- [SDR SWIA200211507](https://openairdocs.org/sdr/SWIA200211507.md): Indicator · malfunctioned · Nov 15, 2002 · N196SW · Emb EMB120ER · Fuel Quantity Indicator
  > ENROUTE THE FIRST OFFICER NOTICED ''SOMETHING WET'' ON THE RT WING. RT FUEL GAUGE SHOWED AN IMBALANCE AND INCREASING. RETURNED TO DEN. ON SHORT FINAL THE FUEL GAUGE BECAME ERRATIC. CHECKED FUEL GAUGE WITH FUEL TANK STICKS. NO DEFECTS NOTED. OPS CHECK G
- [SDR SWIA200211461](https://openairdocs.org/sdr/SWIA200211461.md): Pressure Switch · malfunctioned · Nov 10, 2002 · N196SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > ON CLIMB OUT, WITH LIGHT ICING CONDITIONS PRESENT, THE OUTBOARD LT STAB FAILED. APPLIED QRH AND CHANGED TIMERS. REMAINED FAILED FOR 20 MINUTES, THEN WORKED AGAIN. RETURNED TO SLC. REPLACED LEFT OUTBOARD STAB TRIM PRESSURE SWITCH. OPS CHECK GOOD IAW 30-00-
- [SDR SWIA200211387](https://openairdocs.org/sdr/SWIA200211387.md): Servo · malfunctioned · Oct 26, 2002 · N196SW · Emb EMB120ER · Autopilot Main Servo
  > LOUD SOUND OF CABLE RUBBING AS THE YOKE IS PULLED BACK. REPLACED ELEVATOR AUTOPILOT SERVO (SVO-65). OPS CHECK GOOD. SN OFF 7088.
- [SDR SWIA200211145](https://openairdocs.org/sdr/SWIA200211145.md): Cooling Fan · seized · Aug 17, 2002 · N196SW · Emb EMB120ER · Air Distribution Fan
  > ON TAXI OUT THERE WAS A SMOKE SMELL IN THE CABIN AND THE LAV SMOKE DETECTOR WENT OFF. FOUND AVIONICS COOLING FAN SEIZED. REMOVED AND REPLACED FAN IAW EMB MM 21-27-02. OPS CHECK GOOD.
- [SDR SWIA200211020](https://openairdocs.org/sdr/SWIA200211020.md): Support · cracked · Jun 15, 2002 · N196SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > TWO SKIN SUPPORTS CRACKED AT FORWARD CARGO DOOR TRACK ATTACH POINTS. REPLACED BOTH SKIN SUPPORTS AND SECURED SAME IAW SRM 51-10-02.
- [SDR SWIA200211019](https://openairdocs.org/sdr/SWIA200211019.md): Rib · cracked · Jun 15, 2002 · N196SW · Emb EMB120ER · Wing, Rib/Bulkhead
  > RIGHT AND LEFT INBOARD LEADING EDGE RIBS EACH HAVE A CRACK. DOUBLER ADDED TO MENTIONED AREA IAW SRM 120 51-10-02.
- [SDR SWIA200211018](https://openairdocs.org/sdr/SWIA200211018.md): Frame · cracked · Jun 15, 2002 · N196SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > LEFT INBOARD NACELLE, WHEEL WELL AREA, FRAME CRACKED (JUST FORWARD OF POWER/CONDITION CABLE PULLEY BRACKET ASSEMBLY). NEW FRAME INSTALLED IAW SRM120 51-10-02. ALSO NEW FASTENERS INSTALLED IAW SRM120 51-40-02.
- [SDR SWIA200211017](https://openairdocs.org/sdr/SWIA200211017.md): Frame · chafed · Jun 15, 2002 · N196SW · Emb EMB120ER · Vertical Stabilizer, Spar/Rib
  > BRACKET AND FRAME CHAFED WHERE RUDDER TRIM CABLES PASS FROM AFT RIGGING BAY INTO VERTICAL STAB. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.
- [SDR SWIA200211016](https://openairdocs.org/sdr/SWIA200211016.md): Web · chafed · Jun 15, 2002 · N196SW · Emb EMB120ER · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB RUDDER TRIM CABLES ARE CHAFING ON WEBBING WHERE CABLES CHANGE DIRECTION TO GO TO THE RUDDER TRIM ACTUATOR. THE WEBBING IS DAMAGED. REPAIRED IAW GST-1980/02 AND SB 120-27-0082.
- [SDR SWIA200211015](https://openairdocs.org/sdr/SWIA200211015.md): Rib · cracked · Jun 15, 2002 · N196SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > BOTH ENGINE OUTBOARD TAIL PIPE HOLDERS NEED TO BE CHECKED FOR POSSIBLE BROKEN RIB. THE HOLDERS HAVE MOVEMENT. REPLACED RIBS IAW 120 SRM 51-20-02.
- [SDR SWIA200210888](https://openairdocs.org/sdr/SWIA200210888.md): Actuator · malfunctioned · Jun 1, 2002 · N196SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > TRAILING EDGE FLAPS COME DOWN WITHOUT HYDRAULIC POWER. REMOVED AND REPLACED LT NACELLE FLAP ACTUATOR IAW MM 27-50-08. OPS CHECK AND LEAK CHECKS GOOD.
- [SDR SWIA200210889](https://openairdocs.org/sdr/SWIA200210889.md): Squat Switch · malfunctioned · May 30, 2002 · N196SW · Emb EMB120ER · Cabin Temperature Control System
  > LEFT AND RIGHT PACKS FAILED ON THE GROUND WITH APU BLEED PACKS ON LOW. FOLLOWED QRH PROCEDURE. TURNED PACKS OFF, THEN ON. BOTH PACKS FAILED WITHIN 15 SECONDS AND SMOKE ENTERED THE CABIN. UPDATE 6/3: BOTH PACKS FAILED ON THE GROUND. REMOVED AND REPLACED L
- [SDR SWIA200210882](https://openairdocs.org/sdr/SWIA200210882.md): O-Ring · leaking · May 26, 2002 · N196SW · Emb EMB120ER · Fuel Injector Nozzle
  > NR 1 ENGINE SMOKING HEAVILY FROM THE TOP OF THE COWL AFTER SHUT DOWN. FUEL WAS DRIPPING FROM UNDERNEATH THE ENGINE. FOUND FUEL NOZZLE (9 O'CLOCK POSITION) TRANSFER TUBES NOT SEATED. REPLACED O-RINGS ON TRANSFER TUBES AND SEATED. PERFORMED LEAK CHECK. LEAK
- [SDR SWIA200210870](https://openairdocs.org/sdr/SWIA200210870.md): Odor · detected · May 12, 2002 · N196SW · Emb EMB120ER · Air Distribution System
  > WITH THE APU POWERED ON THE GROUND, WE HEARD A LOUD CLICKING NOISE, ELECTRIC LIGHT 3 CHIMES DOOR LIGHT ON MAP. WE ALSO DETECTED A PACK BURNING SMELL. RAN APU ON GROUND WITH APU GENERATOR ONLINE FOR 20 MINUTES, COULD NOT DUPLICATE. OPS CHECK GOOD. OPERATED
- [SDR SWIA200210792](https://openairdocs.org/sdr/SWIA200210792.md): Connector · corroded · Apr 17, 2002 · N196SW · Emb EMB120ER · Stabilizer Control System
  > ABORTED TAKEOFF FOR TRIM AURAL WARNING. TRIM WAS SET AT 35. FOUND THREE VERY LOOSE AND CORRODED CONNECTIONS ON THE LEFT TRIM PROXIMITY SENSOR. REPLACED ALL WITH ENVIRONMENTAL SPLICES. OPERATED TRIM SEVERAL TIMES. OPS CHECK GOOD.
- [SDR SWIA200210740](https://openairdocs.org/sdr/SWIA200210740.md): Control Servo · stiff · Mar 19, 2002 · N196SW · Emb EMB120ER · Autopilot Main Servo
  > AILERON CABLES ARE VERY STIFF. FOUND AILERON AUTOPILOT SERVO MOVEMENT STIFF. REPLACED SERVO IAW 22-10-05. AILERON AND AUTOPILOT OPS CHECKS GOOD.
- [SDR SWIA200210694](https://openairdocs.org/sdr/SWIA200210694.md): Actuator · failed · Feb 27, 2002 · N196SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > INBOARD FLAPS FAILED AT 5 DEGREES DOWN. CONTROL FAULT WILL NOT RESET. REMOVED AND REPLACED LEFT INBOARD FLAP ACTUATOR IAW RII 27-307, OPS CHECK GOOD, NO DEFECTS NOTED.
- [SDR SWIA200210668](https://openairdocs.org/sdr/SWIA200210668.md): Annunciator · faulty · Feb 25, 2002 · N196SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > DISAGREEMENT ON FLAP RETRACTION INBOARD PAIR. INBOARD FLAPS WOULD NOT RETRACT, INDICATED 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED FLAP ANNUNCIATOR UNIT WITH SERVICEABLE UNIT IAW EMB 120 MM 27-51-01. RAN FLAPS, OPS CHECK GOOD.
- [SDR SWIA200210541](https://openairdocs.org/sdr/SWIA200210541.md): Seal · loose · Jan 6, 2002 · N196SW · Emb EMB120ER · Flight Compartment Windows
  > UNUSUAL LOUD POPPING SOUND OVERHEAD. FOUND LOOSE PROSEAL ON TOP EDGE OF CAPTAIN'S WINDSHIELD. APPLIED SPEED TAPE.
- [SDR SWIA200110262](https://openairdocs.org/sdr/SWIA200110262.md): Stringer · cracked · Oct 21, 2001 · N196SW · Emb EMB120ER · Wing, Longeron/Stringer
  > RIGHT WING LOWER SURFACE STRINGER NR 10 CRACKED NEAR OUTBOARD END OF FUEL CELL OPENING JUST INBOARD OF NACELLE. REPAIRED STRINGER IAW SRM 57-20-03.
- [SDR SWIA200110246](https://openairdocs.org/sdr/SWIA200110246.md): Computer · malfunctioned · Oct 11, 2001 · N196SW · Emb EMB120RT · Integrated Flight System
  > FLYING ILS INTO JAC WHEN APP MODE SELECTED ON FCP, THE COMMAND BARS STARTED MOVING UP AND DOWN RAPIDLY, GYRO AND COMPUTER FLAGS APPEARED AND ATTITUDE DISPLAY APPEARED ON MAP. RESET ATT MON PER QRH, WHICH CANCELLED FLAGS, BUT PRESSING APPR MODE IT ALL HAPPENED
- [SDR SWIA200110152](https://openairdocs.org/sdr/SWIA200110152.md): Actuator · failed · Sep 7, 2001 · N196SW · Emb EMB120ER · Rudder Actuator
  > RUDDER LOCKED UP ON CLIMBOUT, LOSS OF AUTHORITY OF THE RIGHT RUDDER. RETURNED TO SLC.TESTED RUDDER SYSTEM IAW EMB120 MM 27-22-00. FOUND ACTUATORS THAT FAILED DIFFERENTIAL PRESSURE FUNCTIONAL TESTS. REMOVED AND REPLACED BOTH RUDDER ACTUATORS IAW EMB120 MM
- [SDR SWIA200110109](https://openairdocs.org/sdr/SWIA200110109.md): Actuator · malfunctioned · Aug 20, 2001 · N196SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > ON DEPARTURE DURING FLAP RETRACTION, FLAP DISAGREEMENT INBOARD PAIR.FOUND LEFT INBOARD FLAP ACTUATOR WITH BAD WIPER. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. OPS GOOD.
- [SDR SWIA972413](https://openairdocs.org/sdr/SWIA972413.md): Ejector Valve · failed · Feb 25, 2001 · N196SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > VERTICAL FIN LEADING EDGE DEICE INOP. FAILED AIRBORNE. REMOVED AND REPLACED DEICE EJECTOR VALVE IAW 30-20-04. OPS CHECK GOOD. P/N 3D2376-06, S/N ON PM878, OFF PM805.
- [SDR SWIA972259](https://openairdocs.org/sdr/SWIA972259.md): Strap · corroded · Dec 7, 2000 · N196SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > C-CHECK, CABIN FLOOR, BUTT STRAP, ZONE 250 RIGHT SIDE FLOOR RAIL BUTT STRAP, CORRODED. AFTER CLEANING IS.040 DEEP (RT SIDE BY SEAT 9, 10). BUTT STRAPS BETWEEN FRAME 30 & 35 AND FRAME 35 & 38 ARE ALSO CORREDED BEYOND LIMITS. REMOVED AND REPLACED THE BUTT ST
- [SDR SWIA972153](https://openairdocs.org/sdr/SWIA972153.md): Connector · dirty · Dec 6, 2000 · N196SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > ON APPROACH WHEN SELECTING FLAPS 25 DEGREES TO FLAPS 45 DEGREES OUTBOARD PAIR WILL NOT EXTEND CAUSING A FLAP DISSAGREEMENT. (WOULD NOT CLEAR USING QRH). SLOWING THROUGH 120 KNOTS, EXTENDED. FOUND FLAP TRACKS DIRTY, CLEANED FLAP TRACKS AND CANNON PLUGS. OP

Next page: https://openairdocs.org/deregistered/N196SW-2007-01-26/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 = 'N196SW' AND deregistration_id = 'N196SW-2007-01-26'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N196SW-2007-01-26/reports

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