# Service difficulty reports: N214SW, cancelled Feb 8, 2007

A list on [N214SW, cancelled Feb 8, 2007](https://openairdocs.org/deregistered/N214SW-2007-02-08.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 SWIA200616291](https://openairdocs.org/sdr/SWIA200616291.md): Lever · malfunctioned · Feb 17, 2006 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > RECEIVED "TOO LOW FLAPS" AURAL WARNINGS ON APPROACH. REPLACED FLAP SELECTOR LEVER ASSY IAW 27-50-01, OPERATIONAL CHECK GOOD.
- [SDR SWIA200516032](https://openairdocs.org/sdr/SWIA200516032.md): Actuator · malfunctioned · Dec 26, 2005 · N214SW · Emb EMB120ER · Rudder Control System
  > RT RUDDER JAMMED AFTER TAKEOFF. REPLACED BOTH RUDDER ACTUATORS IAW MM 27-22-02. OPERATIONAL CHECK GOOD, PN 308140-1003, SN/OFF 0165 SN/OFF 0671.
- [SDR SWIA200515460](https://openairdocs.org/sdr/SWIA200515460.md): Control Unit · malfunctioned · Aug 23, 2005 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ABOVE 160 KTS DURING FLAP RETRACTION OUTBOARD FLAPS DISAGREE (FLAP ON MAP, DISAGREEMENT ON OVERHEAD). REPLACED FLAP CONTROL UNIT IAW A/C MM 27-50-06, OPERATIONAL CHECK GOOD.
- [SDR SWIA200515433](https://openairdocs.org/sdr/SWIA200515433.md): Control Unit · malfunctioned · Aug 17, 2005 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP CONTROL FAULT ON CLIMB-OUT. REPLACED THE FLAP CONTROL UNIT. OPERATIONAL CHECK GOOD IAW MM 27-50-00.
- [SDR SWIA200515325](https://openairdocs.org/sdr/SWIA200515325.md): Annunciator · malfunctioned · Jul 30, 2005 · N214SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > ON CLIMB-OUT, GOT A FLAP DISAGREEMENT INDICATION. REPLACED FLAP ANNUNCIATOR PANEL IAW EMB 120 MM 27-50-00. OPERATIONAL CHECK GOOD, PN ON 306900-1017; PN OFF 347100-1001; SN ON 0015; SN OFF 0089.
- [SDR SWIA200514932](https://openairdocs.org/sdr/SWIA200514932.md): Sign · inoperative · Apr 26, 2005 · N214SW · Emb EMB120ER · Emergency Lighting
  > RED EMERGENCY FLOOR LIGHTS IN GALLEY INOPERATIVE. REPLACED RED EMERGENCY SIGN AT THE GALLEY FLOOR. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514696](https://openairdocs.org/sdr/SWIA200514696.md): Door · binding · Mar 11, 2005 · N214SW · Emb EMB120ER · Passenger/Crew Doors
  > MAIN CABIN DOOR VERY HARD TO OPEN AND CLOSE. ADJUSTED AND RIGGED PAX DOOR BACKSTOP SHIMS IAW EMB 120 MM 52-11-00.
- [SDR SWIA200514697](https://openairdocs.org/sdr/SWIA200514697.md): Battery Pack · discharged · Mar 8, 2005 · N214SW · Emb EMB120ER · Emergency Lighting
  > AFT SECTION EMERGENCY LIGHTS ARE INOPERATIVE. REPLACED LIGHT BATTERY PACK FOR AFT SECTION. OPERATIONAL CHECK GOOD.
- [SDR SWIA200514992](https://openairdocs.org/sdr/SWIA200514992.md): Buttstrap · corroded · Feb 15, 2005 · N214SW · Emb EMB120ER · Fuselage Miscellaneous Structure
  > THERE IS CORROSION ON BUTT STRAP JUST AFT OF PAX DOOR ENTRANCE. ITEM FOUND AT C-CHECK INSPECTION. REPLACED AFFECTED BUTT STRAP AND SECURED SAME IAW EMB 120 MM 51-10-02 PG 3 SEC 3A.
- [SDR SWIA200414035](https://openairdocs.org/sdr/SWIA200414035.md): Lamp · burned out · Oct 25, 2004 · N214SW · Emb EMB120ER · Emergency Lighting
  > PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT DOES NOT ILLUMINATE. RELAMPED PASSENGER ENTRY OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413731](https://openairdocs.org/sdr/SWIA200413731.md): Computer · malfunctioned · Aug 20, 2004 · N214SW · Emb EMB120ER · Stall Warning System
  > LT STALL WARNING LIGHT CAME ON IN FLIGHT. REMOVED AND REPLACED LT NR 1 STALL WARNING COMPUTER. OPERATIONAL CHECK GOOD.
- [SDR SWIA200413550](https://openairdocs.org/sdr/SWIA200413550.md): Actuator · malfunctioned · Jul 6, 2004 · N214SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > AFTER LANDING SELECTED FLAPS UP, RECEIVED A CONTROL FAULT ON OUTBOARD FLAPS. REMOVED AND REPLACED FLAP ACTUATOR IAW AMM 27-50-00. REPAIRED PIN 4 AT CONNECTOR P1867. REMOVED AND REPLACED FCU IAW 27-50-00 AND OPERATIONAL CHECKED GOOD IAW 27-50-00.
- [SDR SWIA200413440](https://openairdocs.org/sdr/SWIA200413440.md): Light · inoperative · Jun 13, 2004 · N214SW · Emb EMB120ER · Emergency Lighting
  > FORWARD EMERGENCY RED LIGHT STRIP ON FLOOR INOP. REPLACED FORWARD EMERGENCY LIGHT STRIP ON FLOOR WITH SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200413430](https://openairdocs.org/sdr/SWIA200413430.md): Window · cracked · Jun 10, 2004 · N214SW · Emb EMB120ER · Flight Compartment Windows
  > LEFT CAPTIANS SIDE WINDOW CRACKED ON GROUND. REMOVED AND REPLACED LEFT SIDE WINDSHIELD IAW MM 56-10-01. PN: NP151311-1, S/N OFF: 00108.
- [SDR SWIA200413305](https://openairdocs.org/sdr/SWIA200413305.md): Lamp · inoperative · May 5, 2004 · N214SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHT AT PAX DOOR CEILING IS INOP. REMOVED AND REPLACED LAMP. OPS CHECK GOOD. P/N: 209.
- [SDR SWIA200413103](https://openairdocs.org/sdr/SWIA200413103.md): Control Panel · malfunctioned · Mar 26, 2004 · N214SW · Emb EMB120ER · Stall Warning System
  > STALL WARNING LIGHT ILLUMINATES ON THE MAP. REMOVED AND REPLACED STALL PANEL. OPS CHECKS GOOD.
- [SDR SWIA200412858](https://openairdocs.org/sdr/SWIA200412858.md): Switch · failed · Feb 4, 2004 · N214SW · Emb EMB120ER · Cabin Pressure Control System
  > DURING CRUISE FLIGHT AT 27,000 FT, HAD A PRESSURE POP AND THEN A CABIN ALT WITH TRIPLE CHIME. PERFORMED PRECAUTIONARY EMERGENCY DESCENT TO 10,000 FT AT THAT POINT, WENT TO QRH. FOLLOWED PROCEDURE FOR LOSS OF CABIN PRESSURE. WENT TO MANUAL MODE ON PRESSURIZA
- [SDR SWIA200312412](https://openairdocs.org/sdr/SWIA200312412.md): Wire · disconnected · Sep 13, 2003 · N214SW · Emb EMB120ER · Light System Wiring
  > FORWARD EMERGENCY LIGHT (INOPERATIVE). RECONNECTED BOTH POWER LEADS AT FORWARD (EXIT) SIGN. OPS CHECK GOOD.
- [SDR SWIA200312411](https://openairdocs.org/sdr/SWIA200312411.md): Channel · cracked · Aug 25, 2003 · N214SW · Emb EMB120ER · Nacelle/Pylon, Attach Fittings
  > LT MLG INSIDE WELL FORWARD OUTBOARD CRACK ON NACELLE. (DISCOVERED DURING C-CHECK INSPECTION) LT MLG OUTBOARD CHANNEL REPLACED SRM120 51-10-02.
- [SDR SWIA200312206](https://openairdocs.org/sdr/SWIA200312206.md): Battery Pack · malfunctioned · Jul 16, 2003 · N214SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHTS IN ROW 9 COME ON MOMENTARILY AND THEN GO OUT. REMOVED AND REPLACED EMERGENCY BATTERY PACK NR 4 IAW MM 33-50-02. OPS CHECK GOOD.
- [SDR SWIA200312112](https://openairdocs.org/sdr/SWIA200312112.md): Channel · cracked · Jun 14, 2003 · N214SW · Emb EMB120ER · Trailing Edge Flaps
  > AFTER DEPARTURE THE FLAPS WOULD NOT RETRACT PAST APPROXIMATELY 10 DEGREES. RECEIVED FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING APPROXIMATELY 10 DEGREES. FOUND THE LEFT OUTBOARD FLAP LOWER CHANNEL CRACKED AT INBOARD END [ROLLER BRACKET ATTACH POINT]
- [SDR SWIA200312094](https://openairdocs.org/sdr/SWIA200312094.md): Panel · malfunctioned · Jun 9, 2003 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > AFTER TAKEOFF, OUTBOARD FLAPS WOULD NOT COMPLETELY RETRACT AND FLAP DISAGREEMENT INDICATED. QRH, RECYCLED AND WOULD NOT CORRECT. FLAPS CAME DOWN FINE BUT WILL NOT RETRACT IN AIR. ON GROUND THEY RETRACT COMPLETELY. REMOVED AND REPLACED FLAP ANNUNCIATOR PANE
- [SDR SWIA200312069](https://openairdocs.org/sdr/SWIA200312069.md): Flap Track · damaged · Jun 3, 2003 · N214SW · Emb EMB120ER · Trailing Edge Flaps
  > AFTER DEPARTURE FLAPS WOULD NOT RETRACT PAST 10 DEGREES. FLAP DISAGREEMENT WITH THE OUTBOARD FLAPS INDICATING 10 DEGREES. RETURNED TO FIELD. REPLACED RIGHT OUTBOARD FLAP INNER FIXED TRACK IAW EMB MM 57-53-03. INSTALLED SERVICEABLE TRACK ON RIGHT WING, OUTB
- [SDR SWIA200312058](https://openairdocs.org/sdr/SWIA200312058.md): Switch · stuck · Jun 2, 2003 · N214SW · Emb EMB120ER · Propeller Controlling System
  > PILOT REPORTS THAT RIGHT ENGINE AUTO FEATHERED ON TAKEOFF ROLL WITH LT ENGINE TQ FLUCTUATION, BUT ENGINE DID NOT FOLLOW FLUCTUATION. FOUND LEFT ENGINE AUTO FEATHER TEST SWITCH STUCK IN THE TEST POSITION. REMOVED AND REPLACED SWITCH. RAN A/C, OPS CHECKED GOO
- [SDR SWIA200312031](https://openairdocs.org/sdr/SWIA200312031.md): Actuator · malfunctioned · May 27, 2003 · N214SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > FLAPS WILL NOT RETRACT FULLY. OUTBOARD FLAPS REMAIN AT ABOUT 10 DEGREES. RETURNED TO SLC. REMOVED AND REPLACED RIGHT OUTBOARD FLAP ACTUATOR WITH SERVICEABLE PART IAW MM 27-50-09. OPS AND LEAK CHECK GOOD.
- [SDR SWIA200312009](https://openairdocs.org/sdr/SWIA200312009.md): Stringer · cracked · May 22, 2003 · N214SW · Emb EMB120ER · Wing, Longeron/Stringer
  > CRACKED STRINGER LEFT INBOARD WING LOWER SURFACE AFT OF INBOARD FUEL CELL ACCESS PANEL. FOUND DURING A CHECK INSPECTION. COMPLIED WITH WING STRINGER REPAIR AT LEFT INBOARD WING LOWER SURFACE STRINGER NR 8 AT RIB NR 5 PER SRM 57-20-03.
- [SDR SWIA200311919](https://openairdocs.org/sdr/SWIA200311919.md): Flap Track · worn · Apr 28, 2003 · N214SW · Emb EMB120ER · Trailing Edge Flaps
  > FLAP DISAGREEMENT AFTER TAKEOFF. OUTBOARD PAIR WOULD NOT RETRACT TO LESS THAN 10 DEGREES, OTHER PAIRS RETRACTED PROPERLY. APPLIED QRH PROCEDURE 3 TIMES, FAILED ALL 3 TIMES. FLAPS EXTENDED TO 25 DEGREES PROPERLY FOR LANDING, THEN RETRACTED PROPERLY TO 0 DEGR
- [SDR SWIA200311915](https://openairdocs.org/sdr/SWIA200311915.md): Warning Light · illuminated · Apr 25, 2003 · N214SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > IN FLIGHT CLIMBING THROUGH 7,000 FEET, THE FLAP DISAGREEMENT LIGHT ILLUMINATED. COULD NOT CLEAR VIA QRH. RETURNED TO SLC. INSPECTED FLAPS. NO DEFECTS FOUND. PERFORMED FLAP FUNCTIONAL CHECKS IAW MM 27-50-00. OPERATIONAL CHECKS SATISFACTORY. NO DEFECTS NO
- [SDR SWIA200311790](https://openairdocs.org/sdr/SWIA200311790.md): Connector · contaminated · Feb 16, 2003 · N214SW · Emb EMB120ER · Flight Control System Wiring
  > FLAP DISAGREEMENT ON FLAP RETRACTION ON TAKEOFF, OUTBOARD FLAPS. RETURNED TO SLC. INSPECTED OUTBOARD FLAPS CONNECTORS, FOUND GLYCOL IN LEFT OUTBOARD CONNECTOR. CLEANED LEFT OUTBOARD CONNECTOR AND RAN FLAPS 10 CYCLES. OPS CHECK GOOD. NO FAULTS AT THIS TIME
- [SDR SWIA200311675](https://openairdocs.org/sdr/SWIA200311675.md): Connector · worn · Jan 3, 2003 · N214SW · Emb EMB120ER · Flight Control System Wiring
  > FLAPS WOULD NOT RETRACT, DISAGREEMENT WITH THE OUTBOARD PAIRS, WOULD NOT CORRECT. FOUND LEFT OUTBOARD FLAP CONNECTOR TO HAVE FLUID INSIDE AND WORN BACKSHELL. REPLACED CANNON PLUG AND BACKSHELL. APPLIED SUPER CORR-B TO CANNON PLUG AND CONNECTORS. OPS CHECK
- [SDR SWIA200211502](https://openairdocs.org/sdr/SWIA200211502.md): Signal Cond Unit · malfunctioned · Nov 22, 2002 · N214SW · Emb EMB120ER · Engine BMEP/Torque Indicating
  > NR 2 PROPELLER FEATHERED WHEN TAKEOFF POWER APPLIED. TORQUE REACHED 125 PERCENT INSTANTANEOUSLY. NP 18.9 PERCENT WHEN POWER BROUGHT BACK TO IDLE. REPLACED RIGHT ENGINE TORQUE SIGNAL CONDITIONER IAW EMB MM 77-11-01. OPERATIONAL CHECKS GOOD. REPLACED NR 2 E
- [SDR SWIA200211501](https://openairdocs.org/sdr/SWIA200211501.md): Connector · contaminated · Nov 18, 2002 · N214SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > AFTER TAKEOFF, RECEIVED A FLAP DISAGREEMENT WITH 2 BARS ON OUTBOARD FLAPS, AND ALL LIGHTS ON THE 10 DEGREE LINE FLASHING. RESET AS PER QRH. RESET NOT SUCCESSFUL. RETURNED TO LAX. FOUND LT OUTBOARD FLAP ACTUATOR CONNECTOR PLUG CONTAMINATED WITH MOISTURE. C
- [SDR SWIA200211414](https://openairdocs.org/sdr/SWIA200211414.md): Connector · contaminated · Oct 31, 2002 · N214SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT THAT WOULD NOT CLEAR AFTER TAKEOFF. RETURNED TO SLC. DEICE FLUID FOUND IN OUTBOARD FLAP ACTUATOR CONNECTOR PLUGS. CLEANED CONNECTOR PLUGS. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA200211391](https://openairdocs.org/sdr/SWIA200211391.md): Annunciator · malfunctioned · Oct 23, 2002 · N214SW · Emb EMB120ER · Trailing Flap Position Indicating System
  > FLAP DISAGREEMENT ON TAKEOFF. RECYCLED 3 TIMES - UNSUCCESSFULLY. FLAP DISAGREEMENT ON OUTBOARD PAIR DURING RETRACTION. RETURNED TO DEN. CLEANED AND INSPECTED FLAP TRACKS AND RERACKED FCU. INSTALLED SERVICEABLE FLAP ANNUNCIATOR. OPERATED FLAPS SEVERAL TIM
- [SDR SWIA200211272](https://openairdocs.org/sdr/SWIA200211272.md): Computer · malfunctioned · Sep 29, 2002 · N214SW · Emb EMB120ER · Integrated Flight System
  > FO'S EHSI FAILED DURING TAXI AND IN FLIGHT. EHSI SHOWS YELLOW FAIL FLAG AND HEADING FLAG. SUCCESSFULLY RESET BOTH TIMES. REPLACED FO'S HDG74. OPERATIONAL CHECK OF EHSI GOOD.
- [SDR SWIA200211271](https://openairdocs.org/sdr/SWIA200211271.md): Gcu · malfunctioned · Sep 29, 2002 · N214SW · Emb EMB120ER · AC Regulator
  > CAPTAIN'S EHSI WENT BLANK ON TAXI OUT. REPLACED GCU NR 1 (AUX GEN NR 1) IAW MM 24-30-02. CHECKED OPERATION OF POWER TRANSFER AT NP 70 PERCENT WITHOUT OBSERVING ANY ANOMALIES ON EHSI NR 1. CHECKS GOOD. PARALLELED AUX GEN'S IAW MM 24-30-02 ALL OPS CHECK GOOD
- [SDR SWIA200211229](https://openairdocs.org/sdr/SWIA200211229.md): Computer · malfunctioned · Sep 7, 2002 · N214SW · Emb EMB120ER · Integrated Flight System
  > CAPT'S EHIS FAILED AFTER TAKEOFF. RETURNED TO FIELD. REMOVED AND REPLACED THE NR 1 HPU WITH A SERVICEABLE UNIT. OPS CHECK GOOD.
- [SDR SWIA200211067](https://openairdocs.org/sdr/SWIA200211067.md): Engine · malfunctioned · Jul 25, 2002 · N214SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > RIGHT ENGINE AUTO FEATHERED ON THE TAKEOFF ROLL. ABORTED THE TAKEOFF. PERFORMED TWO TAKEOFF POWER RUNS, ALL CHECKS NORMAL.
- [SDR SWIA200210957](https://openairdocs.org/sdr/SWIA200210957.md): Connector · loose · Jun 8, 2002 · N214SW · Emb EMB120ER · Stall Warning System
  > FIRST OFFICER'S STICK SHAKER NOT WORKING ON FIRST FLIGHT OF THE DAY CHECK. FOUND CONNECTOR LOOSE ON SHAKER UNIT. TIGHTENED CONNECTOR. OPS CHECK PER 27-60-00 GOOD.
- [SDR SWIA200210905](https://openairdocs.org/sdr/SWIA200210905.md): Flap · malfunctioned · Jun 7, 2002 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAP DISAGREEMENT IN FLIGHT. RETURNED TO SLC. PERFORMED OPS CHECKS IAW 27-50-00. COULD NOT DUPLICATE DISCREPANCY.
- [SDR SWIA200210913](https://openairdocs.org/sdr/SWIA200210913.md): Relay · failed · Jun 5, 2002 · N214SW · Emb EMB120ER · Propeller Feathering/Reversing
  > UPON ADDING POWER ON TAKEOFF, LEFT TORQUE GAUGE WOULD NOT GO ABOVE 75PERCENT, THEN AURAL AUTO FEATHER WARNING SOUNDED AND THE RIGHT ENGINE FEATHERED. UPON PULLING BACK POWER TO GROUND IDLE BOTH SIDES (ABORT), LEFT TORQUE GAUGE REMAINED AT 75 PERCENT AND RIGHT
- [SDR SWIA200210906](https://openairdocs.org/sdr/SWIA200210906.md): Indicator · erratic · Jun 1, 2002 · N214SW · Emb EMB120ER · Engine EGT/TIT Indicating System
  > LEFT ENGINE T6 GAUGE ERRATIC. RETURNED TO DEN. REPLACED LEFT T6 GAUGE. OPS CHECK GOOD.
- [SDR SWIA200210815](https://openairdocs.org/sdr/SWIA200210815.md): Fastener · loose · Apr 23, 2002 · N214SW · Emb EMB120ER · Fasteners
  > ABORTED TAKEOFF AT 60 KIAS DUE TO A MAP RED DOOR LIGHT ILLUMINATING. FOUND CAMLOCK ON FUEL SERVICE DOOR UNSECURED. SECURED CAMLOCK ON FUEL DOOR. OPS CHECK GOOD. ALL PANELS SECURED.
- [SDR SWIA200210713](https://openairdocs.org/sdr/SWIA200210713.md): Actuator · leaking · Mar 13, 2002 · N214SW · Emb EMB120ER · Passenger/Crew Doors
  > AT 1000 FT AGL AND 10 DEGREES BANK TO THE RIGHT (AFTER TAKEOFF), THE GREEN SYSTEM RESERVOIR LOW LEVEL LIGHT ILLUMINATED WITH HYD ON MAP. THE FLUID QUANTITY NEEDLE REGISTERED IN THE YELLOW ARC. THE LIGHTS EXTINGUISHED SOON AFTER WINGS LEVELED AND THE FLUID QU
- [SDR SWIA200210714](https://openairdocs.org/sdr/SWIA200210714.md): Detector · malfunctioned · Mar 12, 2002 · N214SW · Emb EMB120ER · Ice Detection
  > ICE MONITOR FAILED INFLIGHT. RETURNED TO DEN. CYCLED CIRCUIT BREAKER. OPS CHECKED GOOD.
- [SDR SWIA200210615](https://openairdocs.org/sdr/SWIA200210615.md): Wire Harness · defective · Feb 1, 2002 · N214SW · Emb EMB120ER · Landing Gear System Wiring
  > RT MAIN LANDING GEAR -A- DISAGREEMENT LIGHT ILLUMINATED DURING FLIGHT. ALL -B- LIGHTS FUNCTION NORMAL. REMOVED AND REPLACED -A- UPLOCK HARNESS WITH SERVICEABLE HARNESS. OPS CHECKS GOOD.
- [SDR SWIA200210604](https://openairdocs.org/sdr/SWIA200210604.md): Target · out of adjust · Jan 29, 2002 · N214SW · Emb EMB120ER · Landing Gear Position and Warning
  > RIGHT GEAR LIGHTS RED A & B WOULD NOT EXTINGUISH WHEN GEAR RETRACTED. CYCLED 3 TIMES. INSPECTED RT MAIN GEAR. FOUND UPLOCK HOOK ADJUSTED OUT, PLUS ICE BUILD UP ON HOOK. ADJUSTED UPLOCK PROX TARGET. C/W GEAR SWING. OPS CHECKS GOOD.
- [SDR SWIA200210590](https://openairdocs.org/sdr/SWIA200210590.md): Connector · contaminated · Jan 26, 2002 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON TAKEOFF, DURING FLAP RETRACTION, RECEIVED A FLAP DISAGREEMENT. FOLLOWED QRH AND FLAPS RETRACTED NORMALLY. COULD NOT DUPLICATE ON GROUND. INSPECTED FLAPS, TRACKS, ACTUATORS AND FOUND LEFT OUTBOARD FLAP CANNON PLUG WET. CLEANED AND RESECURED. OPS CHECKS
- [SDR SWIA200110239](https://openairdocs.org/sdr/SWIA200110239.md): Frame · cracked · Sep 21, 2001 · N214SW · Emb EMB120ER · Nacelle/Pylon, Frame/Spar/Rib
  > RIGHT AND LEFT NACELLE NR 1 FRAMES CRACKED. REPLACED BOTH NACELLE NR 1 FRAMES IAW EMB120 SRM 51-10-02 AND SB 120-54-0036.
- [SDR SWIA200110212](https://openairdocs.org/sdr/SWIA200110212.md): Fcu · malfunctioned · Sep 20, 2001 · N214SW · Emb EMB120ER · Trailing Edge Flap Control System
  > ON CLIMBOUT RECEIVED A FLAP DISAGREEMENT AND FLAPS WOULD NOT FULLY RETRACT. RETURNED TO FAT. AIRCRAFT IN FOR C CHECK INSPECTION. DETAILS FORTHCOMING. UPDATE: PULLED FCU, MEGGED WIRES TO BOTH INBOARD FLAP ACTUATORS. NO DEFECTS NOTED. CHECKED ANNUNCIATORS FO

Next page: https://openairdocs.org/deregistered/N214SW-2007-02-08/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 = 'N214SW' AND deregistration_id = 'N214SW-2007-02-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N214SW-2007-02-08/reports

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