# Service difficulty reports: N209SW, cancelled Jan 7, 2005

A list on [N209SW, cancelled Jan 7, 2005](https://openairdocs.org/deregistered/N209SW-2005-01-07.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 · 59 reports

- [SDR SWIA200412946](https://openairdocs.org/sdr/SWIA200412946.md): Proximity Sensor · malfunctioned · Feb 29, 2004 · N209SW · Emb EMB120ER · Elevator Tab Control System
  > TRIM AURAL WARNING SOUNDS CONTINUOUSLY WHEN TRIM IS IN GREEN BAND. REMOVED AND REPLACED RIGHT ELEVATOR TRIM PROX SENSOR IAW EMB 120 MM 27-32-05. OPS CHECKS GOOD.
- [SDR SWIA200312717](https://openairdocs.org/sdr/SWIA200312717.md): Actuator · malfunctioned · Dec 28, 2003 · N209SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAP DISAGREEMENT AFTER TAKEOFF AND ON THE GROUND ON TAXI IN. REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS AND LEAK CHECKS GOOD. P/N: 343100-1001, S/N ON: 6024, S/N OFF: 0127.
- [SDR SWIA200312734](https://openairdocs.org/sdr/SWIA200312734.md): Control Unit · malfunctioned · Dec 27, 2003 · N209SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT WHEN RETRACTING FLAPS AFTER TAKEOFF. REMOVED AND REPLACED FLAP CONTROL UNIT IAW 27-50-06. ALSO REMOVED AND REPLACED RIGHT NACELLE FLAP ACTUATOR IAW AMM 27-50-08 AND RII CARD 27-307. REPLACED ROLLERS ON RIGHT OUTBOARD FLAP. OPS CHECKS GOOD
- [SDR SWIA200312592](https://openairdocs.org/sdr/SWIA200312592.md): Computer · malfunctioned · Nov 8, 2003 · N209SW · Emb EMB120ER · Autopilot System
  > F/O AUTOPILOT CONTINUES TO MAKE UNCOMMANDED SMALL FORE AND AFT PITCH CHANGES. REMOVED AND REPLACED NR 2 AUTOPILOT COMPUTER WITH A SERVICEABLE COMPUTER. OPS CHECK GOOD IAW 22-10-00.
- [SDR SWIA200312134](https://openairdocs.org/sdr/SWIA200312134.md): Wire · damaged · Jun 19, 2003 · N209SW · Emb EMB120ER · Light System Wiring
  > EMERGENCY LIGHT OVERHEAD BIN DOOR ROW 9 B & C INOP. REPAIRED WIRE TO EMERGENCY LIGHT AT 9BC. OPS CHECK GOOD.
- [SDR SWIA200312003](https://openairdocs.org/sdr/SWIA200312003.md): Uplock Sensor · malfunctioned · May 14, 2003 · N209SW · Emb EMB120ER · Landing Gear Position and Warning
  > UPON DEPARTURE, LANDING GEAR WOULD NOT RETRACT. SYSTEM A & B SHOWED DISAGREEMENT, WITH THE EXCEPTION OF SYSTEM A, LEFT MAIN GEAR. RAN QRH, NO RESULTS, CYCLED GEAR, NO RESULTS, PULLED & RESET LANDING GEAR CB, GEAR RETRACTED.REMOVED AND REPLACED ''A'' UPLOCK P
- [SDR SWIA200311832](https://openairdocs.org/sdr/SWIA200311832.md): Wire Harness · damaged · Mar 17, 2003 · N209SW · Emb EMB120ER · Landing Gear System Wiring
  > AFTER TAKEOFF AND GEAR RETRACTION, RECEIVED GEAR INDICATIONS, LOUD NOISE AND VIBRATION FROM THE NOSE THAT INCREASED WITH AIRSPEED. RETURNED TO LAX. PERFORMED GEAR RETRACTION. FOUND THAT GEAR DOORS WOULD NOT CLOSE DUE TO A FAULTY NOSE GEAR A-HARNESS. REMOVE
- [SDR SWIA200311801](https://openairdocs.org/sdr/SWIA200311801.md): Indicator · malfunctioned · Feb 16, 2003 · N209SW · Emb EMB120ER · Airspeed/Mach Indicator
  > HIGH SPEED AURAL WARNING ON TAKEOFF ROLL AT 70 KNOTS. ABORTED TAKEOFF. REMOVED AND REPLACED CO-PILOTS AIRSPEED INDICATOR. OPS CHECKS GOOD. LEAK CHECK GOOD.
- [SDR SWIA200211654](https://openairdocs.org/sdr/SWIA200211654.md): Support · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > COCKPIT LEFT SIDE LOWER SUPPORT FOR SIDE VIEW WINDOW, NEAR SIDE POST, IS CRACKED. FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED LEFT SIDE LOWER SUPPORT IAW SRM 51-40-02 & 51-00-00. P/N: 120-34535-005.
- [SDR SWIA200211653](https://openairdocs.org/sdr/SWIA200211653.md): Seat Track · corroded · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD AND AFT, RIGHT AND LEFT SIDES, FLOOR SEAT TRACKS ARE CORRODED. FOUND DURING C-CHECK INSPECTION. INSTALLED NEW SEAT TRACKS IAW MM 53-01-05.
- [SDR SWIA200211652](https://openairdocs.org/sdr/SWIA200211652.md): Skin · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Nacelle/Pylon, Plate/Skin
  > LEFT NACELLE OUTBOARD SIDE JUST AFT OF FRAME 3 FORWARD HOOK FOR FORWARD COWL DOOR LATCH NACELLE IS CRACKED WHERE AFT PART OF THE LATCH HOOK GOES INTO THE NACELLE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REINFORCEMENT PLATE IAW EMB120 SRM 5
- [SDR SWIA200211651](https://openairdocs.org/sdr/SWIA200211651.md): Intercostal · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > COCKPIT LEFT SIDE CRACK IN INTERCOSTAL BETWEEN FRAME 12A AND 13 (2 CRACKED RIVETS NEAR CRACK). FOUND DURING C-CHECK INSPECTION. STOP-DRILLED CRACK AND FABRICATED AND INSTALLED DOUBLER IAW EMB SRM 51-40-02 AND 51-00-00.
- [SDR SWIA200211650](https://openairdocs.org/sdr/SWIA200211650.md): Bracket · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > LEFT HYDRAULIC RESERVOIR INBOARD VERTICAL BRACKET MOUNTING HAS 3 INCH + VERTICAL CRACK INSIDE THE BRACKET. FOUND DURING C-CHECK INSPECTION. REMOVED VERTICAL MOUNTING BRACKET AND INSTALLED NEW HYDRAULIC RESERVOIR MOUNTING BRACKET IN ITS PLACE IAW EMB SRM 51-4
- [SDR SWIA200211649](https://openairdocs.org/sdr/SWIA200211649.md): Frame · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage Main, Frame
  > FRAME 13 RT AND LT SIDE INBOARD AND OUTBOARD, PREVIOUS REPAIRS CRACKED OUTBOARD SIDE. CRACK GOES BEYOND DOUBLER ON THE RIGHT SIDE. FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED DOUBLERS TO CRACKED AREAS IAW EMB SRM 51-00-00 AND 51-40-02.
- [SDR SWIA200211648](https://openairdocs.org/sdr/SWIA200211648.md): Bracket · cracked · Nov 12, 2002 · N209SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > CRACKED ALUMINUM BRACKET IN THE RIGHT SIDE OF THE HYDRAULIC BAY (AGAINST THE FIRE WALL, NEAREST TO THE INBOARD SIDE). FOUND DURING C-CHECK INSPECTION. FABRICATED AND INSTALLED REPAIR ANGLE IAW EMB SRM 51-70-06 & 51-40-02.
- [SDR SWIA200211647](https://openairdocs.org/sdr/SWIA200211647.md): Bushing · corroded · Nov 12, 2002 · N209SW · Emb EMB120ER · Elevator Control System
  > LT ELEVATOR ATTACHMENT BRACKET INBOARD BUSHINGS ARE CORRODED (HAT AND FLOAT BUSHINGS). FOUND DURING C-CHECK INSPECTION. REMOVED AND REPLACED BOTH HAT AND FLOAT BUSHINGS ON LEFT INBOARD ELEVATOR ATTACH BRACKET IAW 20-40-03.
- [SDR SWIA200211646](https://openairdocs.org/sdr/SWIA200211646.md): Bolt · corroded · Nov 12, 2002 · N209SW · Emb EMB120ER · Elevator Control System
  > THE BOLTS THAT HOLD THE ELEVATOR BELLCRANK MOUNT TO THE VERTICAL STABILIZER HAVE CORROSION ON THEM. FOUND DURING C-CHECK INSPECTION. REPLACED 8 BOLTS ON ELEVATOR BELLCRANK MOUNT WITH NEW ONES IAW 55-30-01.
- [SDR SWIA200211343](https://openairdocs.org/sdr/SWIA200211343.md): Door Frame · damaged · Oct 13, 2002 · N209SW · Emb EMB120ER · Fuselage Main, Structure
  > FRAME 13A DAMAGED AT DOOR ACTUATOR MOUNT. EXTENSIVE DAMAGE TO SHEAR CLIP 120-29047-001 AND SEVERAL OTHER TIPPED AND DAMAGED RIVETS OUTBOARD OF SHEAR CLIP. AT FRAME 13A, REMOVED AND REPLACED THE DAMAGED SHEAR CLIPS AND DAMAGED RIVETS IAW EMB SRM 51-00-00, 51-
- [SDR SWIA200211308](https://openairdocs.org/sdr/SWIA200211308.md): Actuator · failed · Oct 6, 2002 · N209SW · Emb EMB120ER · Rudder Actuator
  > RUDDER PEDALS FROZE JUST AFTER TAKEOFF, NO WARNINGS OR AURAL INDICATIONS. RIGHT SIDE COULD ONLY MOVE AN 1 INCH OR SO, LEFT PEDAL HAD SLIGHTLY MORE TRAVEL. RUDDER PEDAL TRAVEL WAS NORMAL ON THE GROUND. REMOVED AND REPLACED GREEN AND BLUE SYSTEM RUDDER ACTUAT
- [SDR SWIA200211203](https://openairdocs.org/sdr/SWIA200211203.md): Boot · failed · Sep 6, 2002 · N209SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > LEADING EDGE MIDDLE, RIGHT & LEFT WING BOOTS FAILED. RETURNED TO SLC. REMOVED AND REPLACED LEFT MIDDLE DEICE BOOT IAW 30-10-00. OPS & LEAK CHECK GOOD.
- [SDR SWIA200210890](https://openairdocs.org/sdr/SWIA200210890.md): Flap · malfunctioned · May 27, 2002 · N209SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON DEPARTURE RECEIVED A FLAP DISAGREEMENT ON THE OUTBOARD PAIR. WHILE ON THE RAMP WITHOUT ANY HYD POWER HAD A NACELLE DISAGREEMENT. LEFT NACELLE FLAP WAS HANGING DOWN A FEW DEGREES ALONG WITH ONE LIGHT BAR ILLUMINATED ON THE FLAP ANNUNCIATOR PANEL. REMOVED
- [SDR SWIA200210861](https://openairdocs.org/sdr/SWIA200210861.md): Ballast · malfunctioned · May 17, 2002 · N209SW · Emb EMB120ER · Passenger Compartment Lighting
  > SMOKE COMING FROM LAV OVERHEAD LIGHTS. CIRCUIT BREAKER 30A POPPED. REPLACED LAV LIGHT BALLAST. OPS CHECKS GOOD.
- [SDR SWIA200210506](https://openairdocs.org/sdr/SWIA200210506.md): Pressure Switch · faulty · Jan 1, 2002 · N209SW · Emb EMB120ER · Engine Oil Pressure
  > ABORTED TAKEOFF DUE TO OIL WARNING (AURAL) AND NR 1 OIL LIGHT BLINKING ON. OIL LEVELS WERE SATISFACTORY DURING PREFLIGHT. ABORT INITIATED AT APPROXIMATELY 80 KTS. REPLACED NR 1 ENGINE LOW OIL PRESSURE SWITCH. OPS CHECK AND LEAK CHECK GOOD ON GROUND RUNUP.
- [SDR SWIA200110509](https://openairdocs.org/sdr/SWIA200110509.md): Propeller · faulty · Dec 31, 2001 · N209SW · Emb EMB120ER · Propeller Assembly
  > ON ROLLING TAKEOFF, TORQUE ON LEFT ENGINE SHOT UP TO 134 PERCENT TQ. TAKEOFF AURAL WARNING AUTO FEATHER SOUNDED WITH SWITCH ON. ABORTED TAKEOFF. WHEN POWER LEVERS PULLED BACK TO GROUND IDLE, RT ENGINE READ 75 PERCENT TQ AND 53 PERCENT NH. WHEN AUTO FEATHER
- [SDR SWIA200110511](https://openairdocs.org/sdr/SWIA200110511.md): Wire · out of position · Dec 29, 2001 · N209SW · Emb EMB120ER · Light System Wiring
  > ROW SIX OVERHEAD RECESSED EMERGENCY LIGHTS ARE TOO DIM. BATTERY PACKS NEED TO BE REPLACED ON THAT CIRCUIT, NOT CHARGING. POSITIONED WIRES ON RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT TO CORRECT POSITION. OPS CHECK GOOD.
- [SDR SWIA200110510](https://openairdocs.org/sdr/SWIA200110510.md): Display · malfunctioned · Dec 28, 2001 · N209SW · Emb EMB120ER · Central Display
  > DESCENDING THROUGH 16,000 LOST CAPTAIN'S EHSI. NOTICED STRONG BURNING ODOR, SMOKE, WHICH CLEARED ALMOST IMMEDIATELY. NO CIRCUIT BREAKERS POPPED. REMOVED AND REPLACED CAPTAIN'S ELECTRONIC FLIGHT DISPLAY IAW EMB MM 34-22-03. OPS CHECK GOOD.
- [SDR SWIA200110444](https://openairdocs.org/sdr/SWIA200110444.md): Wire · burned · Dec 12, 2001 · N209SW · Emb EMB120ER · Electrical Power System Wiring
  > WIRE W110-2230-16N IS BURNED AT CANNON PLUG P0952 PIN 43 TO GROUND. INSPECTED SURROUNDING WIRING AND REPLACED BURNED WIRE IAW WM 20-00-00.`
- [SDR SWIA200110231](https://openairdocs.org/sdr/SWIA200110231.md): Door Seal · out of position · Oct 8, 2001 · N209SW · Emb EMB120ER · Cargo/Baggage Doors
  > RAPID DEPRESSURIZATION AT FL 260. MASKS DEPLOYED.REINSTALLED CARGO DOOR SEAL IAW MM 52-30-01 AND STOWED O2 MASKS IAW MM 35-20-01.
- [SDR SWIA200110113](https://openairdocs.org/sdr/SWIA200110113.md): Engine · malfunctioned · Aug 15, 2001 · N209SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > ON APPROACH, LEFT ENGINE EXPERIENCED A SEVERE POWER LOSS. TRIPLE CHIME ''ENGINE CONTROL'' AND WHITE ''MANUAL'' LIGHT ILLUMINATED. INITIATED A GO-AROUND TO AVOID TERRAIN CONTACT. ON GO-AROUND, REGAINED SOME POWER ON LEFT ENGINE. BROUGHT POWER BACK TO LEVEL
- [SDR SWIA200110055](https://openairdocs.org/sdr/SWIA200110055.md): Fan · smoke · Jul 20, 2001 · N209SW · Emb EMB120ER · Air Distribution Fan
  > IMMEDIATELY AFTER ENGINE START WHEN PACKS WERE SWITCHED ON, SMOKE BECAME VISIBLE IN CABIN.REMOVED AND REPLACED LEFT GROUND COOLING FAN WITH A SERVICEABLE UNIT IAW MM 21-51-03.
- [SDR SWIA972666](https://openairdocs.org/sdr/SWIA972666.md): Switch · out of adj · Jun 28, 2001 · N209SW · Emb EMB120ER · Fluid Service Doors
  > SERVICE DOOR LIGHT CAME ON JUST AFTER ROTATION. RETURNED TO FIELD. ADJUSTED OUTBOARD FUEL PANEL MICRO SWITCH IAW 52-73-03. OPS CHECK GOOD.
- [SDR SWIA200110021](https://openairdocs.org/sdr/SWIA200110021.md): Cable · corroded · Jun 3, 2001 · N209SW · Emb EMB120ER · Cargo/Baggage Doors
  > BOTH TOP, OUTBOARD CABLES ON CARGO DOOR CORRODED. FOUND DURING C-CHECK. REMOVED AND REPLACED BOTH OUTBOARD CABLES IAW MM 52-31-00. P/N 120-32772-003, P/N 120-32772-007.
- [SDR SWIA972597](https://openairdocs.org/sdr/SWIA972597.md): Flap Track · dirty · May 26, 2001 · N209SW · Emb EMB120ER · Trailing Edge Flaps
  > FLAP DISAGREEMENT OUTBOARD PAIR WHEN SELECTING FLAPS UP AFTER TAKEOFF, 2 BARS STILL LIGHTED ON PANEL. WOULD NOT RECYCLE PER QRH. WOULD NOT EXCEED 15 DEGREES UPON LANDING. CLEANED AND LUBRICATED TRACKS AND ROLLERS. OPS CHECK NORMAL.
- [SDR SWIA972591](https://openairdocs.org/sdr/SWIA972591.md): Stall Warning · malfunctioned · May 22, 2001 · N209SW · Emb EMB120ER · Stall Warning System
  > SYSTEM 1 STALL WARNING CAME ON DURING TAKEOFF. REPLACED LAMP IN STALL WARNING PANEL. RERACKED NR 1 STALL COMPUTER. STALL WARNING OPS CHECK GOOD.
- [SDR SWIA972543](https://openairdocs.org/sdr/SWIA972543.md): Regulator · failed · May 2, 2001 · N209SW · Emb EMB120ER · Pressure Regulator/Outflow Valve
  > A/C WOULD NOT PRESSURIZE. TRIED MANUAL CONTROLLER. STILL WOULD NOT PRESSURIZE. LEFT PACK PRESSURE REGULATOR SHUT OFF VALVE LOW PRESSURE. REPLACED PRESSURE REGULATOR AND SHUT OFF VALVE IAW 21-50-01. P/N: 3214414-3, S/N ON: 693, S/N OFF: 949. PERFORMED F
- [SDR SWIA972505](https://openairdocs.org/sdr/SWIA972505.md): Battery Pack · discharged · Apr 13, 2001 · N209SW · Emb EMB120ER · Emergency Lighting
  > FORWARD EMERGENCY LIGHTS DO NOT ILLUMINATE. REMOVE AND REPLACE THE FORWARD EMERGENCY LIGHTS BATTERY PACK. P/N D366-04-001, S/N ON 7720, OFF 891. OPS CHECK GOOD.
- [SDR SWIA972436](https://openairdocs.org/sdr/SWIA972436.md): Engine · malfunctioned · Mar 16, 2001 · N209SW · Emb EMB120ER · Fuel Control/Turbine Engines
  > LEFT ENGINE DID NOT SPOOL UP WITHIN NORMAL PARAMETERS AS DID THE RIGHT ENGINE ON TAKEOFF ROLL. AS A RESULT ABORTED TAKEOFF. RAN BOTH ENGINES TO TAKEOFF POWER SEVERAL TIMES. BOTH ENGINES ACCELERATED NORMAL. ALL CHECKS GOOD.
- [SDR SWIA972409](https://openairdocs.org/sdr/SWIA972409.md): Engine · out of adj · Mar 2, 2001 · N209SW · Emb EMB120ER · Fuel Control/Turbine Engines
  > LEFT ENGINE SPOOLED UP TO 30 PERCENT ON TAKEOFF THEN HUNG AT 30 PERCENT. ABORTED TAKEOFF. DEFERRED EEC. FOUND LEFT ENGINE OUT OF TRIM. TRIMMED ENGINE IAW MM 71-00-00. OPS CHECK GOOD.
- [SDR SWIA972382](https://openairdocs.org/sdr/SWIA972382.md): Engine · malfunctioned · Feb 20, 2001 · N209SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > ON INITIAL POWER APPLICATION LEFT TORQUE ONLY CAME UP TO APPROXIMATELY 25 PERCENT, RIGHT CAME UP NORMALLY. ABORTED TAKEOFF. RAN AIRCRAFT, ADVANCED BOTH ENGINES TO TAKEOFF POWER 6 TIMES. CHECKS NORMAL. VERIFIED EEC MANUAL REVERSION FOR OPERATION AND ADJUSTME
- [SDR SWIA972192](https://openairdocs.org/sdr/SWIA972192.md): Uplock Sensor · failed · Dec 11, 2000 · N209SW · Emb EMB120ER · Landing Gear Position and Warning
  > FELT AND HEARD A STRONG VIBRATION AFTER GEAR RETRACTION. HAD A LEFT GEAR RED LIGHT (A SYSTEM). CYCLED GEAR, VIBRATION STOPPED. HAD 3 GREEN LIGHTS WHEN GEAR CAME UP THE VIBRATION STARTED AGAIN AND CONTINUED UNTIL GEAR WAS DOWN AND LOCKED. RED GEAR LIGHT WAS
- [SDR SWIA971948](https://openairdocs.org/sdr/SWIA971948.md): Connector · inoperative · Aug 30, 2000 · N209SW · Emb EMB120ER · Air Intake Anti/De-Ice System
  > LEFT ENGINE AIR INLET INOP (WHEN SWITCH IS ON AND OFF) FL 240, TEMP -14 DEGREES. IT BEGAN OPERATING AGAIN ON DESCENT (TEMP +5 DEGREES). RETURNED TO SLC. FOUND FRONT BELLOWS LOOSE AND CANNON PLUG ON DEICE PRESSURE SWITCH FULL OF WATER. CLEANED WATER FROM SW
- [SDR SWIA971914](https://openairdocs.org/sdr/SWIA971914.md): Pcu · failed · Aug 4, 2000 · N209SW · Emb EMB120ER · Propeller Controlling System
  > TORQUE AND NP FLUCTUATE INFLIGHT. TORQUE PLUS OR MINUS 10 - 15 PERCENT, NP FLUCTUATES 5 - 7 PERCENT. NO FUEL FLOW FLUCTUATIONS NOTED. RIGHT ENGINE TAKEN TO FEATHER. NORMAL LANDING. REMOVED AND REPLACED RIGHT ENGINE PCU. OPS CHECK AND LEAK CHECKS GOOD. P
- [SDR SWIA971889](https://openairdocs.org/sdr/SWIA971889.md): Probe · failed · Jul 20, 2000 · N209SW · Emb EMB120ER · Engine RPM Indicating System
  > RIGHT EEC FAILED WHEN APPLYING TAKEOFF POWER. ABORTED TAKEOFF. REMOVED AND REPLACED NH PICKUP PROBE WITH SERVICEABLE UNIT IAW MM 77-12-00, OPS CHECKS GOOD. P/N ON: 3039242, S/N ON: CH17129, S/N OFF: CH13519.
- [SDR SWIA971712](https://openairdocs.org/sdr/SWIA971712.md): Harness · contaminated · Feb 26, 2000 · N209SW · Emb EMB120ER · Landing Gear Position and Warning
  > DEPARTING SLC, LANDING GEAR WOULD NOT RETRACT. RETURNED TO THE FIELD. DRAINED WATER FROM RIGHT MLG A UPLOCK HARNESS ON AIRFRAME. OPERATED GEAR SEVERAL TIMES, OPS CHECK GOOD MM 323000.
- [SDR SWIA971708](https://openairdocs.org/sdr/SWIA971708.md): Solenoid Valve · failed · Feb 24, 2000 · N209SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LANDING GEAR WOULD NOT RETRACT, RED TRANSIT LIGHTS CAME ON, BUT GEAR WOULD NOT MOVE. RETURNED TO SLC. REPLACED LANDING GEAR SOLENOID VALVE IAW 323203 AND LEFT MAIN LANDING GEAR OUTBOARD DOOR SEQUENCE VALVE IAW 323204. LEAK CHECK GOOD, PN ON: 12032943001SN:
- [SDR SWIA971608](https://openairdocs.org/sdr/SWIA971608.md): Retract System · contaminated · Nov 22, 1999 · N209SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR WOULD NOT RETRACT. RETURNED TO FIELD. JACKED AIRCRAFT AND CYCLED GEAR WITH GROUND POWER AND GREEN SYSTEM ONLY. FAULT FREE CYCLES. SUSPECT SNOW AND SLUSH CONDITION TO BE THE FAULT. GEAR OPERATION TESTED OK IAW MM 32.
- [SDR SWIA971489](https://openairdocs.org/sdr/SWIA971489.md): Filter · contaminated · May 6, 1999 · N209SW · Emb EMB120ER · Hydraulic Filter, Main
  > HYDRAULIC FILTER LIGHT ILLUMINATED ALONG WITH HYD LIGHT ON MAP. RETURNED TO SLC. FOUND HYDRAULIC PRESSURE FILTER BYPASS POPPED. REMOVED AND REPLACED PRESSURE RETURN FILTER. OPS CHECK AND LEAK CHECKED GOOD.
- [SDR SWIA971355](https://openairdocs.org/sdr/SWIA971355.md): Deice Boot · torn · Dec 28, 1998 · N209SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > ALL INBOARD BOOTS FAILED STAB AND WING. RETURNED TO SLC. INSTALLED PATCH ON SMALL TEAR IN LEFT INBOARD WING BOOT. SET FOR 20 MINUTES. RUN UP OPS CHECKS GOOD.
- [SDR SWIA971215](https://openairdocs.org/sdr/SWIA971215.md): Valve · malfunctioned · Jul 9, 1998 · N209SW · Emb EMB120ER · Pneumatic Distribution System
  > AFTER DEPARTURE WITH APU ASSIST TAKEOFF WHEN SWITCHING TO ENGINE BLEED, DUCT LEAK ILLUMINATED. LIGHT EXTINGUISHED AT 3 MINUTES. RETURNED TO SLC. REMOVED AND REPLACED LEFT SIDE PRESSURE VALVE WITH SERVICEABLE UNIT, IAW MM 30-10-06. OPS CHECKS GOOD.
- [SDR SWIA971150](https://openairdocs.org/sdr/SWIA971150.md): Tee Section · corroded · Mar 9, 1998 · N209SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > RIGHT T-SECTION BETWEEN CENTER AND RIGHT BUTT STRAPS AT FRAME 16 HAS CORROSION. REMOVED AND REPLACED RIGHT T-SECTION AT FRAME 16 IAW SRM 51-40-02.

Next page: https://openairdocs.org/deregistered/N209SW-2005-01-07/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 = 'N209SW' AND deregistration_id = 'N209SW-2005-01-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N209SW-2005-01-07/reports

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