# Service difficulty reports: N207SW, cancelled Jan 10, 2005

A list on [N207SW, cancelled Jan 10, 2005](https://openairdocs.org/deregistered/N207SW-2005-01-10.md).

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

- [SDR SWIA200312698](https://openairdocs.org/sdr/SWIA200312698.md): Stringer · cracked · Dec 12, 2003 · N207SW · Emb EMB120ER · Wing, Longeron/Stringer
  > STRINGER NR 8 AT RIB 5 CRACKED. DISCOVERED DURING A CHECK INSPECTION. REPAIRED STRINGER IAW EMB SRM 57-20-03 AND GST 3176/02.
- [SDR SWIA200312627](https://openairdocs.org/sdr/SWIA200312627.md): Battery Pack · inoperative · Nov 21, 2003 · N207SW · Emb EMB120ER · Emergency Lighting
  > EMERGENCY LIGHTS ROW 1-4 INOP. REPLACED BATTERY PACK. OP CHECK OK.
- [SDR SWIA200312514](https://openairdocs.org/sdr/SWIA200312514.md): Pedal · restricted · Oct 11, 2003 · N207SW · Emb EMB120ER · Rudder Control System
  > AFTER ROTATION, RT RUDDER PEDAL RESTRICTED, WITH ABOUT 1 INCH OF MOVEMENT. RAN QRH JAMMED RUDDER PROCEDURE, TURNED OFF BLUE SYSTEM AND NORMAL RUDDER TRAVEL RETURNED.AFTER RUDDER DEFLECTIONS LEFT AND RIGHT WITH BLUE AND GREEN SYSTEMS IN DIFFERENT CONFIGURATIONS
- [SDR SWIA200311784](https://openairdocs.org/sdr/SWIA200311784.md): Proximity Sensor · malfunctioned · Feb 12, 2003 · N207SW · Emb EMB120ER · Elevator Control System
  > ABORTED TAKEOFF WITH AURAL WARNING. REPOWERED AIRCRAFT AND DID A COMPLETE AURAL WARNING SYSTEM RESET. NOW IT WILL NOT PASS A STATIC TEST. REPLACED LEFT PROXIMITY SENSOR IAW 27-32-00.
- [SDR SWIA200311665](https://openairdocs.org/sdr/SWIA200311665.md): Warning System · false activation · Jan 1, 2003 · N207SW · Emb EMB120ER · High Speed Warning
  > HIGH SPEED WARNING ON TAKEOFF AT 60 KIAS. ABORTED TAKEOFF. THIS HAPPENED TWICE. PERFORMED TEST PROCEDURES FOR BOTH AIRSPEED INDICATORS AND OVERSPEED WARNINGS. ALL READINGS CORRECT AND OPS CHECK GOOD PER 34-12-01.
- [SDR SWIA200211405](https://openairdocs.org/sdr/SWIA200211405.md): Boot · torn · Oct 30, 2002 · N207SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > RIGHT AND LEFT OUTBOARD STAB AND VERT FIN BOOTS INOP AFTER 28 SECONDS ON TIMERS 1 & 2. RETURNED TO DEN. REPLACED LEFT HORIZONTAL STAB DEICE BOOT IAW MM CHAPTER 30-10-01. OPS CHECK GOOD.
- [SDR SWIA200211226](https://openairdocs.org/sdr/SWIA200211226.md): Rib · damaged · Aug 13, 2002 · N207SW · Emb EMB120ER · Rudder, Spar/Rib
  > RIB IN RUDDER 1 DAMAGED JUST BELOW GREEN RUDDER ACTUATOR ATTACH POINT. DISCOVERED DURING C-CHECK. REPLACED DAMAGED RIB IAW 120 SRM 51-10-02.
- [SDR SWIA200210940](https://openairdocs.org/sdr/SWIA200210940.md): Sensor · malfunctioned · Jun 2, 2002 · N207SW · Emb EMB120ER · Elevator Tab Control System
  > TAKEOFF TRIM AURAL WARNING FAILURE. ABORTED TAKEOFF. REPLACED BOTH LEFT AND RIGHT ELEVATOR TRIM SENSORS. RAN BOTH ENGINES TO TAKEOFF POWER SETTINGS AND ALL TRIM SETTINGS IN GREEN BAND. OPS CHECK GOOD.
- [SDR SWIA200210525](https://openairdocs.org/sdr/SWIA200210525.md): Skin · cracked · Jan 4, 2002 · N207SW · Emb EMB120ER · Fuselage Main, Plate/Skin
  > CRACK IN SKIN AROUND FWD CORNER OF RT SIDE COCKPIT SIDE WINDOW. DISCOVERED DURING ROUTINE LINE INSPECTION. INSTALLED REPAIR DOUBLER PER SB 120-053-0010.
- [SDR SWIA200110431](https://openairdocs.org/sdr/SWIA200110431.md): Actuator · failed · Dec 11, 2001 · N207SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > AFTER TAKEOFF A FLAP DISAGREEMENT OCCURRED. TWO SEGMENTS OF THE INBOARD PAIR WERE ILLUMINATED AND 1 BAR OF THE NACELLE AND OUTBOARD PAIR FLASHED. DISAGREEMENT CLEARED AFTER SELECTING 15 DEGREES UP, BUT THEN AN INVALID ANALOG IND WAS DISPLAYED. REMOVED AND R
- [SDR SWIA200110174](https://openairdocs.org/sdr/SWIA200110174.md): Selector Switch · malfunctioned · Sep 15, 2001 · N207SW · Emb EMB120ER · Trailing Edge Flap Control System
  > FLAPS WILL NOT MOVE WHEN 45 DEGREES IS SELECTED.REMOVED AND REPLACED FLAP SELECTOR LEVER IAW MM 27-50-01. OPS CHECK GOOD IAW 27-50-00.
- [SDR SWIA972484](https://openairdocs.org/sdr/SWIA972484.md): Switch · out of adj · Apr 5, 2001 · N207SW · Emb EMB120ER · Door Warning System
  > ON TAKEOFF FORWARD DOOR LIGHT BLINKED ON WITH WARNING. ADJUSTED THE MICROSWITCH FOR THE FORWARD DOOR LIGHT. OPS CHECK GOOD.
- [SDR SWIA972471](https://openairdocs.org/sdr/SWIA972471.md): Proximity Sensor · failed · Mar 29, 2001 · N207SW · Emb EMB120ER · Elevator Tab Control System
  > ELEVATOR TRIM AURAL WARNING CONTINUOUS IN OR OUT OF TRIM. REMOVED AND REPLACED LEFT ELEVATOR TRIM PROXIMITY SENSOR WITH NEW IAW EMB MM 27-32-00. P/N 922AA2Y-A6P-Z722. ADJUSTED AND OPS CHECK GOOD.
- [SDR SWIA972304](https://openairdocs.org/sdr/SWIA972304.md): Spring · lack of lube · Jan 21, 2001 · N207SW · Emb EMB120ER · Elevator Control System
  > ELEVATOR MOVEMENT PRODUCES ABNORMAL SOUNDS, SOUNDS LIKE CABLES PRANGING. LUBED ELEVATOR RETURN SPRING FWD ATTACH POINT. SYSTEM CHECK OK.
- [SDR SWIA972154](https://openairdocs.org/sdr/SWIA972154.md): Controller · failed · Dec 7, 2000 · N207SW · Emb EMB120ER · Pressure Regulator/Outflow Valve
  > DESCENDING FROM FLIGHT LEVEL 260 CABIN ALTITUDE LIGHT ILLUMINATED ON THE MAP. LOST CONTROL OF CABIN ALTITUDE IN BOTH AUTO AND MANUAL MODES. MASKS DROPPED. PRESSURIZED AIRCRAFT ON GROUND IN MANUAL MODE. COULD NOT PRESSURIZE IN AUTO MODE. REMOVED AND REP
- [SDR SWIA972120](https://openairdocs.org/sdr/SWIA972120.md): Warning System · activated · Nov 11, 2000 · N207SW · Emb EMB120ER · Data Recorders (Flight/Maintenance)
  > TAKEOFF TRIM ALARMED, ABORTED TAKEOFF. RAN BOTH ENGINES TO TEST TAKEOFF TRIM ALARM. TAKEOFF TRIM OPS CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.
- [SDR SWIA972119](https://openairdocs.org/sdr/SWIA972119.md): Sequence Valve · failed · Nov 11, 2000 · N207SW · Emb EMB120ER · Landing Gear Door Actuator
  > LEFT LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LEFT MAIN GEAR OUTBOARD SEQUENCE VALVE IAW MM 32-32-07. CYCLED GEAR SEVERAL TIMES. OPS CHECK GOOD. P/N 120-32443-001
- [SDR SWIA972090](https://openairdocs.org/sdr/SWIA972090.md): Landing Gear · contaminated · Nov 10, 2000 · N207SW · Emb EMB120ER · Landing Gear Retraction/Extension System
  > LEFT LANDING GEAR WOULD NOT RETRACT. RETURNED TO COD. INSPECTED LEFT LANDING GEAR. CLEANED OFF SNOW AND ICE. SWUNG LANDING GEAR OVER 10 TIMES IAW 32-30-00. LANDING GEAR OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA972040](https://openairdocs.org/sdr/SWIA972040.md): Computer · malfunctioned · Oct 17, 2000 · N207SW · Emb EMB120ER · Stall Warning System
  > ON CLIMBOUT CLACKER WARNING ACTIVATED FOR DURATION OF FLIGHT. RETURNED TO SLC. REPLACED STALL WARNING COMPUTER AND TESTED IAW MM 27-34-02. REPLACED STALL PANEL PER 27-34-00. OPS CHECKS GOOD. NO FAULTS FOUND. S/N ON: 489T, S/N OFF: 686. STALL PANEL S/N
- [SDR SWIA972038](https://openairdocs.org/sdr/SWIA972038.md): Regulator · failed · Oct 14, 2000 · N207SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > RIGHT DUCT LEAK LIGHT ON INFLIGHT. FOLLOWED QRH AND LIGHT DID NOT GO OUT AFTER 3 MINUTES. SHUT DOWN RIGHT ENGINE AND RETURNED TO SLC. TROUBLESHOOT RIGHT BLEED AIR SYSTEM. REMOVED THE RIGHT DEICE AIR PRESSURE REGULATOR AND INSTALLED A SERVICEABLE REGULATOR.
- [SDR SWIA971919](https://openairdocs.org/sdr/SWIA971919.md): Engine · malfunctioned · Aug 6, 2000 · N207SW · Emb EMB120ER · Engine (Turbine/Turboprop)
  > DURING TAKEOFF ROLL, RECEIVED T6 WARNING BEFORE V1. ABORTED TAKEOFF. PERFORMED STATIC RUN UP AND RECEIVED T6 WARNING ON RIGHT ENGINE AT 90 PERCENT TORQUE WITH BLEEDS CLOSED. REMOVED AND REPLACED RIGHT ENGINE MM 71-00-00 RII 72-301. P/N ON: PW118B, S/N: 1
- [SDR SWIA971892](https://openairdocs.org/sdr/SWIA971892.md): Control Box · failed · Jul 22, 2000 · N207SW · Emb EMB120ER · Landing Gear Position and Warning
  > RED A SYSTEM GEAR LIGHTS ILLUMINATED DURING FLIGHT WITH GEAR UP. RETURNED TO SLC. REPLACED GEAR CONTROL BOX WITH SERVICEABLE ASSY, OPS CHECK GOOD IAW 32-60-00.
- [SDR SWIA971717](https://openairdocs.org/sdr/SWIA971717.md): Switch · failed · Feb 29, 2000 · N207SW · Emb EMB120ER · Door Warning System
  > SERVICE DOOR LIGHT ILLUMINATED IN FLIGHT. RETURNED TO PSP. INSPECTED FUEL DOOR SWITCH, AVIONICS BAY SWITCH AND RIGGING DOOR SWITCH. ALL SWITCHES CHECK GOOD. COULD NOT DUPLICATE DISCREPANCY.
- [SDR SWIA971633](https://openairdocs.org/sdr/SWIA971633.md): Switch · damaged · Dec 20, 1999 · N207SW · Emb EMB120ER · Hydraulic Pressure Sensor
  > GREEN SYSTEM MAIN PUMP LOW PRESSURE LIGHT AND LOW LEVEL LIGHT ILLUMINATED WITHIN A FEW SECONDS OF EACH OTHER. QUANTITY INDICATOR FOR GREEN SYSTEM INDICATED EMPTY. RETURNED TO SALT LAKE, LEFT HYDRAULIC PRESSURE SWITCH FOUND BLOWN APART. REMOVED AND REPLACED
- [SDR SWIA971512](https://openairdocs.org/sdr/SWIA971512.md): Filter · dirty · Jul 9, 1999 · N207SW · Emb EMB120ER · Hydraulic System, Main
  > RIGHT HYDRAULIC FILTER LIGHT ILLUMINATED. RETURNED TO SLC. REPLACED HIGH AND LOW PRESSURE FILTERS ON RIGHT PACK. OPS AND LEAKS CHECK GOOD.
- [SDR SWIA971463](https://openairdocs.org/sdr/SWIA971463.md): Hyd Syst · reqd service · Apr 5, 1999 · N207SW · Emb EMB120ER · Hydraulic System, Main
  > SHORTLY AFTER TAKEOFF REACHING CRUISE ALTITUDE THE LEFT HYDRAULIC RESERVOIR LOW PRESSURE LIGHT CAME ON AND WAS ACCOMPANIED BY A FLUID QUANTITY INDICATION IN MID GREEN ARC. WITHIN 5 MINUTES THE RIGHT LOW PRESS CAME ON. BOTH REMAINED TO 15,000 FEET. INSPECTED
- [SDR SWIA971342](https://openairdocs.org/sdr/SWIA971342.md): Actuator · failed · Dec 21, 1998 · N207SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > NACELLE FLAP DISAGREEMENT AT 2 BARS ON DEPARTURE. RETURNED TO SLC. REPLACED RIGHT NACELLE FLAP ACTUATOR IAW MM 27-50-08 AND OPS CHECKS GOOD.
- [SDR SWIA971289](https://openairdocs.org/sdr/SWIA971289.md): Actuator · malfunctioned · Oct 15, 1998 · N207SW · Emb EMB120ER · Trailing Edge Flap Actuator
  > UNABLE TO RETRACT FLAPS, DISAGREEMENT. RETURNED TO SLC. REMOVED AND REPLACED RIGHT WING INBOARD FLAP ACTUATOR, OPS CHECKS GOOD.
- [SDR SWIA971271](https://openairdocs.org/sdr/SWIA971271.md): Tq Sensor · malfunctioned · Sep 7, 1998 · N207SW · Emb EMB120ER · Engine Air Baffle Section
  > AFTER TAKEOFF RIGHT TORQUE GAUGE OSCILLATED BETWEEN 40 PERCENT AND 100 PERCENT AND THEN FEATHERED INADVERTENTLY. RETURNED TO FIELD, REMOVED AND REPLACED TORQUE SENSOR ON RIGHT ENGINE, IAW EMB MM 76-11-02. REMOVED AND REPLACED RIGHT ENGINE HMU IAW MM 73-21-00
- [SDR SWIA971031](https://openairdocs.org/sdr/SWIA971031.md): Ahrs Computer · malfunctioned · Nov 15, 1997 · N207SW · Emb EMB120ER · Integrated Flight System
  > CAPTAINS ATTITUDE DISPLAY FAILED. RETURNED TO FIELD. REPLACED NR 1 AHRS COMPUTER. OPS CHECKS GOOD.
- [SDR SWIA97824](https://openairdocs.org/sdr/SWIA97824.md): Clamp · loose · Jan 12, 1997 · N207SW · Emb EMB120ER · Air Intake Anti/De-Ice System
  > RIGHT ENGINE AIR INLET DE-ICE INOP. RETURNED TO FIELD AFTER TAKEOFF. TIGHTENED CLAMP ON RIGHT ENGINE INLET DE-ICE BOOT SUPPLY LINE, OPS CHECKS GOOD.
- [SDR SWIA95767](https://openairdocs.org/sdr/SWIA95767.md): Hose · chafed · Sep 30, 1996 · N207SW · Emb EMB120ER · Engine Oil Distribution (Airframe Furnished)
  > AT CRUISE ALTITUDE, RIGHT OIL PRESSURE DROPPED TO 40 PSI. PERFORMED PRECAUTIONARY ENGINE SHUT DOWN ON RIGHT ENGINE. REMOVED AND REPLACED UPPER HOSE ASSY ON RIGHT OIL COOLER. OPS CHECK AND LEAK CHECKS GOOD AT THIS TIME.
- [SDR SWIA95701](https://openairdocs.org/sdr/SWIA95701.md): Seal · loose · Dec 25, 1995 · N207SW · Emb EMB120ER · Cargo/Baggage Doors
  > CLIMBING THROUGH 24,000 FEET, CABIN ALTITUDE LIGHT CAME ON. TESTED ALTITUDE WARNING SWITCH SYSTEM IAW MM 21-30-08. SYSTEM OPERATION CHECKS GOOD. FOUND CARGO DOOR SEAL PULLED OUT. REINSTALLED SEAL AS NEEDED. PRESSURIZED AIRCRAFT. CARGO DOOR LEAK CHECK GOO
- [SDR SWIA95698](https://openairdocs.org/sdr/SWIA95698.md): Blade Tip · damaged · Dec 17, 1995 · N207SW · Emb EMB120ER · Propeller Blade Section
  > VIBRATION ON CLIMB-OUT FROM SLC, FOUND RT PROPELLER DAMAGED, ALL ENGINE PARAMETERS WERE NORMAL FOR TAKEOFF AND CLIMB. FOUND DAMAGED TO NR TWO BLADE TIP. PROPELLER REMOVED FROM SERVICE.
- [SDR SWIA95620](https://openairdocs.org/sdr/SWIA95620.md): Oil Syst · reqd service · Aug 28, 1995 · N207SW · Emb EMB120ER · Turbine Engine Oil System
  > AFTER ROTATION, RT OIL PRESSURE FLUCTUATED TO AROUND 40 PSI AND OIL AURAL WARNING SOUNDED. OIL PRESSURE IMMEDIATELY RETURNED AND MAINTAINED NORMAL PSI. SERVICED RT ENGINE OIL, 3 QTS. INSPECTED ENGINE, NO LEAKS FOUND. FILTER BYPASS PINS NOT POPPED, TRANSMIT
- [SDR SWIA95597](https://openairdocs.org/sdr/SWIA95597.md): Reg Vlv Gasket · failed · Jul 13, 1995 · N207SW · Emb EMB120ER · Airfoil Anti/De-ice System
  > FIVE MINUTES AFTER TAKEOFF USING ONLY APU BLEED X FEED TO BOTH PACS, RT DUCT LEAK LIGHT, ILLUMINATED, TURNED OFF X FEED AND RT PAC, STARTED TIME AS PER CHECK LIST, AFTER 3 MINUTES BEGAN PRECAUTIONARY ENGINE SHUT DOWN CHECK LIST WITH ENGINE AT FLIGHT IDLE AS RT
- [SDR SWIA95580](https://openairdocs.org/sdr/SWIA95580.md): Hyd Pump · failed · May 13, 1995 · N207SW · Emb EMB120ER · Hydraulic Pump (Electric/Engine), Main
  > LOST ALL HYDRAULIC PRESSURE IN FLIGHT, LOW PRESSURE ELECTRICAL STANDBY FAILED TO OPERATE. REPLACED A BROKEN RETURN LINE AT ENGINE PUMP IN THE LEFT HYDRAULICS BAY. REMOVED AND REPLACED RIGHT ENGINE HYDRAULIC PUMP. OPERATIONALLY AND LEAK CHECKS GOOD. DECONTA
- [SDR SWIA95522](https://openairdocs.org/sdr/SWIA95522.md): Wheel · cracked · Feb 8, 1995 · N207SW · Emb EMB120ER · Wheel/Ski/Float
  > NR 1 MAIN WHEEL CRACKED. REMOVED AND REPLACED NR 1 MAIN WHEEL ASSY. SEE FL 73942 FOR MECH SIGN OFF.

## 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 = 'N207SW' AND deregistration_id = 'N207SW-2005-01-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N207SW-2005-01-10/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.