# Service difficulty reports: N205AM, cancelled Oct 8, 2010

A list on [N205AM, cancelled Oct 8, 2010](https://openairdocs.org/deregistered/N205AM-2010-10-08.md).

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

- [SDR ASMF 20081202](https://openairdocs.org/sdr/ASMF%2020081202.md): Control Valve · leaking · Dec 19, 2008 · N205AM · Doug DC987 · Engine Exhaust System
  > DURING TRANSIT CHECK, A HYD LEAK ON THE RT ENG WAS DETECTED. MX TIGHTENED HYDRAULIC LINE AND REPLACED AND TESTED THE RT ENG REVERSE CONTROL VALVE IAW AMM 78-31-04, ALL CORRECT.
- [SDR 2008FA0000473](https://openairdocs.org/sdr/2008FA0000473.md): Engine · vibration · Jun 19, 2008 · N205AM · Doug DC987 · Engine (Turbine/Turboprop)
  > CAPTAIN REPORTED STRONG VIBRATION IN RT ENGINE WITH EPR`S BETWEEN 1.7 AND 1.75. TECHS VERIFIED THE RT ENGINE CONDITION AND PERFORMED OPERATIONAL TEST IAW AMM 71-00-01 FOUND ALL CORRECT. VIBRATION WAS WITHIN LIMITS (0.4 UNITS INDICATED). (K)
- [SDR ASMF200805005](https://openairdocs.org/sdr/ASMF200805005.md): Csd · damaged · May 28, 2008 · N205AM · Doug DC987 · AC Generation System
  > DURING PUSH BACK, CAPTAIN REPORTED THAT AFTER STARTED THE LEFT ENGINE, THE CSD LIGHT TURNED ON AND TEMPERATURE REACHED 150 DEGREES CELSIUS, SO ABNORMAL PROCEDURE WAS ACCOMPLISHED. MAINTENANCE PERSONNEL DETECTED THE LEFT CSD OIL LEVEL IN RED RANGE, SO THE EXCE
- [SDR ASMF200802006](https://openairdocs.org/sdr/ASMF200802006.md): Socket · burned · Feb 24, 2008 · N205AM · Doug DC987 · Passenger Compartment Lighting
  > DURING TRANSIT CHECK, A BURNED ODOR WAS DETECTED IN PASSENGERS CABIN. MAINTENANCE PERSONNEL CHECKED AFFECTED AREA AND A LAMP IN RAW 3 WAS DETECTED OVERHEATED. THE LAMP WAS REPLACED IAW MM 33-21-03 BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND DURI
- [SDR ASMF200707014](https://openairdocs.org/sdr/ASMF200707014.md): Door · damaged · Jul 19, 2007 · N205AM · Doug DC987 · Galley Doors
  > DURING TRANSIT CHECK, AIRCRAFT WAS HIT IN THE FORWARD SERVICE DOOR BY A CATERING SERVICE TRUCK. MAINTENANCE PERSONNEL REPLACED THE DOOR IAW MM 52-41-00, PRESSURIZATION TEST WAS CORRECT.
- [SDR ASMF200611003](https://openairdocs.org/sdr/ASMF200611003.md): Blade · fod · Nov 6, 2006 · N205AM · Doug DC987 · Engine (Turbine/Turboprop)
  > DURING TRANSIT CHECK, A LEFT ENGINE BLADE WAS DETECTED DAMAGED WITH 1INCH LENGTH, 0.640 INCH WIDTH IN THE MIDSPAN AND 0.359 INCH DEPTH. THE FIRST STAGE BLADES SET WAS REPLACED IAW MM 72-33-21, PAGE 401 AND ENGINE VIBRATION CHECK WAS PERFORMED IAW MM 72-00-00,
- [SDR ASMF200610013](https://openairdocs.org/sdr/ASMF200610013.md): Panel · leaking · Oct 30, 2006 · N205AM · Doug DC987 · Wing, Plate/Skin
  > DURING TRANSIT CHECK, CAPTAIN REPORTED A FUEL LEAK ON THE RT WING. DURING MAINTENANCE CHECK, A LEAK WAS DETECTED IN THE RT WING UPPER PANEL. TWO NUTS WERE REPLACED IAW SRM 51-30-2 AND PANEL WAS SEALED AGAIN, TESTED CORRECT.
- [SDR ASMF200610010](https://openairdocs.org/sdr/ASMF200610010.md): Wire · broken · Oct 17, 2006 · N205AM · Doug DC987 · Flight Control System Wiring
  > AIRCRAFT RETURNED TO PLATFORM, (RUDDER TRAVEL UNRESTRICTED) LIGHT REMAINED OFF. PROXIMITY SWITCH WAS REPLACED AND TESTED, BUT FAILURE CONTINUED. AIRCRAFT WAS SENT TO THE HANGAR AND WIRING WAS CHECKED, DETECTING A SENSOR LINE BROKEN. WIRING SENSOR WAS REPAIRED
- [SDR ASMF200609003](https://openairdocs.org/sdr/ASMF200609003.md): Wire · shorted · Sep 1, 2006 · N205AM · Doug DC987 · Oxygen System Wiring
  > CAPTAIN REPORTED THAT DURING LANDING WERE DETECTED SPARKS AND SMOKE, FROM THE ACCESS DOOR SYSTEM BOX ELECTRICAL WIRING (SIMULTANEOUSLY, THE CABIN OF PRESSURE ALARM CAME ON IN THE PASSENGERS CABIN). DURING TRANSIT CHECK, COCKPIT SECURITY DOOR LATCH AND OXYGEN M
- [SDR ASMF200609002](https://openairdocs.org/sdr/ASMF200609002.md): Wire · damaged · Sep 1, 2006 · N205AM · Doug DC987 · Oxygen System Wiring
  > CAPTAIN REPORTED THAT DURING LANDING ROLL, SPARKS AND SMOKE CAME APPARENTLY FROM THE ACCESS DOOR SYSTEM BOX (SIMULTANEOUSLY THE CABIN PRESSURE LOST ALARM CAME ON IN THE PASSENGERS CABIN). DURING TRANSIT CHECK, FLIGHT COMPARTMENT DOOR SAFETY CATCH AND OXYGEN MA
- [SDR ASMF200605009](https://openairdocs.org/sdr/ASMF200605009.md): Acm · failed · May 19, 2006 · N205AM · Doug DC987 · Cabin Cooling System
  > DURING TRANSIT CHECK, LEFT AIR CONDITIONING PACK WAS DETECTED WITH HIGH TEMPERATURE, CABIN SUPPLY TEMPERATURE WAS 40 DEGREES CELSIUS. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT CHECK THE LEFT TURBINE COOLING WAS REPLACED IAW MM 21-51-01, TESTED CORR
- [SDR ASMF200512002](https://openairdocs.org/sdr/ASMF200512002.md): Shutoff Valve · leaking · Nov 26, 2005 · N205AM · Doug DC987 · Rudder Control System
  > AIRCRAFT RETURNED TO PLATFORM, DURING TAXING, THE RT PRESSURE AND QUANTITY HYDRAULIC SYSTEM WAS LOST. DURING MAINTENANCE REVISION, THE RUDDER SHUTOFF VALVE WAS LEAKED AND IT WAS REPLACED IAW MM 27-20-08, TESTED CORRECT.
- [SDR ASMF200511008](https://openairdocs.org/sdr/ASMF200511008.md): Starter · failed · Nov 16, 2005 · N205AM · Doug DC987 · Engine Starter
  > AIRCRAFT RETURNED TO PLATFORM, RT ENGINE DID NOT START. DURING MAINTENANCE REVISION, IT WAS DETECTED THE RT ENGINE WITHOUT TURN IN N2. THE RT ENGINE STARTER WAS REPLACED IAW MM 80-10-01, TESTED CORRECT.
- [SDR ASMF200506011](https://openairdocs.org/sdr/ASMF200506011.md): Cylinder · leaking · Jun 6, 2005 · N205AM · Doug DC987 · Landing Gear Steering System
  > DURING TRANSIT CHECK WAS DETECTED HYDRAULIC LEAK IN RIGHT NOSE WHEEL STEERING CYLINDER. AIRCRAFT WAS SENT TO THE HANGAR AND RIGHT NOSE WHEEL STEERING CYLINDER WAS REPLACED IAW MM 32-5202, TESTED CORRECT.
- [SDR ASMF200506007](https://openairdocs.org/sdr/ASMF200506007.md): Sensor · dirty · Jun 4, 2005 · N205AM · Doug DC987 · Rudder Control System
  > AIRCRAFT RETURNED TO PLATFORM, DURING TAXING AND FLIGHT CONTROL TESTS THE RUDDER TRAVEL UNRESTRICTED LIGHT TURNED OFF. THE D1-33 AND D1-34 TARGET SENSORS WERE CLEANED AND ADJUSTED IAW MM 27-20-00, TESTED CORRECT. DURING OVERNIGHT SERVICE, THE TARGET SENSORS OF
- [SDR ASMF200504007](https://openairdocs.org/sdr/ASMF200504007.md): Csd · failed · Apr 8, 2005 · N205AM · Doug DC987 · Alternator-Generator Drive
  > AIRCRAFT ARRIVED WITH DEFERRED REPORT OF RIGHT CSD OIL PRESSURE LOW LIGHT TURNED ON AND BEFORE TO ENGINES STARTED, THE APU OIL TEMPERATURE HIGH LIGHT TURNED ON. ABNORMAL PROCEDURE WAS PERFORMED AND LIGHT CONTINUED ON. AIRCRAFT WAS SENT TO THE HANGAR AND DURING
- [SDR ASMF200501004](https://openairdocs.org/sdr/ASMF200501004.md): Skin · damaged · Jan 7, 2005 · N205AM · Doug DC987 · Leading Edge Devices
  > DURING TRANSIT CHECK WERE DETECTED FUEL PANEL AND SLAT NR 2 DAMAGED. INSPECTION WAS PERFORMED AND DAMAGES WERE DETECTED OUT OF LIMITS, THEREFORE AIRCRAFT WAS SENT TO THE HANGAR. SLAT NR 2 AND FUEL PANEL WERE REPLACED IAW MM 27-80-01 AND 57-30-03, RESPECTIVEL
- [SDR ASMF200412013](https://openairdocs.org/sdr/ASMF200412013.md): Fuel Control · failed · Dec 28, 2004 · N205AM · Doug DC987 · Fuel Controlling System
  > CAPTAIN REPORTED LEFT ENGINE WITH N2 47 PERCENT IN IDLE POSITION. DURING MAINTENANCE REVISION WAS DETECTED LEFT ENGINE WITH N2 52 PERCENT, EPR 1.03; ENGINE STABILIZED AT N2 50 PERCENT, EPR 1.03. WHEN LEFT AIR CONDITIONING SWITCH WAS OPERATED N2 48 PERCENT, EP
- [SDR ASMF200412001](https://openairdocs.org/sdr/ASMF200412001.md): Coupler · broken · Dec 2, 2004 · N205AM · Doug DC987 · Engine Cranking
  > DURING ENGINES START, LEFT ENGINE WAS NOT STARTED, START VALVE WAS OPENED MANUALLY AND FAIL CONTINUE. AIRCRAFT RETURNED TO PLATFORM AND DURING MAINTENANCE REVISION, ENGINE START COUPLER WAS DETECTED BROKEN. ENGINE START COUPLER WAS REPLACED IAW MM 72-61-00,
- [SDR ASMF200411011](https://openairdocs.org/sdr/ASMF200411011.md): Sensor · damaged · Nov 20, 2004 · N205AM · Doug DC987 · Landing Gear Position and Warning
  > A/C RETURNED, DUE TO "UNSAFE NLG" LIGHT TURNED ON & STRONG NOISE DETECTED. A/C SENT TO HANGAR & NOSE L/G DOORS INSPECT, DOORS TEST & EXTENSION/RETRACTION TEST WERE PERFORMED IAW MM 32-20-00, 32-22-01, 32-30-00, RESPECTIVELY, ALL CORRECT. DURING CLIMB IN NEXT
- [SDR ASMF200411006](https://openairdocs.org/sdr/ASMF200411006.md): Control Valve · failed · Nov 12, 2004 · N205AM · Doug DC987 · Landing Gear Steering System
  > CAPTAIN REPORTED THAT DURING TAXING AND TAKE OFF, AIRCRAFT TURNED TO THE RT SIDE. STEERING WAS CHECKED AND WHEELS WERE TURNED.5000 INCH TO THE RT SIDE OF STEERING INDICATOR CENTER. CABLES, PULLEYS, PRESSURE TIRES AND STEERING CONTROL VALVE TRIMMING PIN, WERE
- [SDR ASMF200407009](https://openairdocs.org/sdr/ASMF200407009.md): Servo Valve · leaking · Jul 5, 2004 · N205AM · Doug DC987 · Hydraulic System, Main
  > DURING TRANSIT CHECK, HYDRAULIC LIQUID LEAK WAS DETECTED ON RT MAIN LANDING GEAR WELL, BOTH SYSTEMS WERE PRESSURIZED, BRAKES AND CONTROL SURFACES WERE ACTUATED AND LEAK WAS DETECTED ON ANTI-SKID RT DOUBLE SERVO VALVE. SERVO VALVE WAS REPLACED IAW MM 32-43-02,
- [SDR ASMF200407007](https://openairdocs.org/sdr/ASMF200407007.md): Extinguisher · activated · Jul 3, 2004 · N205AM · Doug DC987 · Fire Bottle, Fixed
  > DURING TRANSIT CHECK, CAPTAIN REPORTED (EXTINGUISHER AGENT NR 1) LIGHT TURNED ON. FIRE EXTINGUISHER WAS DETECTED ACTIVATED BY HIGH TEMPERATURE IN TAIL CONE AND COMPRESSOR CLAMP WAS LOOSEN. FIRE EXTINGUISHER AND CLAMP WERE REPLACED IAW MM 26-20-00, LEAKS TEST C
- [SDR ASMF200406033](https://openairdocs.org/sdr/ASMF200406033.md): Wire · failed · Jun 29, 2004 · N205AM · Doug DC987 · Fire Protection System Wiring
  > AIRCRAFT RETURNED TO PLATFORM, "LEFT AIR COND SUPPLY TEMP HI" LIGHT TURNED ON. BREAKER B1-251 WAS RESEATED, TEMPERATURE SENSOR AND THERMAL SWITCH WERE DISCONNECTED AND FAIL CONTINUE. ENGINES WERE SHUTDOWN AND LIGHT WAS DEFERRED IAW MEL 21-2. DURING OVERNIGHT S
- [SDR ASMF200406026](https://openairdocs.org/sdr/ASMF200406026.md): Extinguisher · activated · Jun 22, 2004 · N205AM · Doug DC987 · Extinguishing System
  > DURING TRANSIT CHECK, FIRE EXTINGUISHER NR 2 WAS ACTIVATED WITHOUT APPARENT CAUSE. AIR CONDITIONING SYSTEM WAS CHECKED BY LEAKS AND COOLING TURBINE CLAMP AND DUCT WERE DETECTED LOOSEN. CLAMP AND DUCT WERE ADJUSTED AND FIRE EXTINGUISHER WAS REPLACED IAW MM 26-2
- [SDR ASMF200404020](https://openairdocs.org/sdr/ASMF200404020.md): Tire · failed · Apr 27, 2004 · N205AM · Doug DC987 · Tire
  > DURING TRANSIT CHECK CAPTAIN REPORTED THAT AIRCRAFT TURNED TO THE LT DURING TAXING AND NOSE LANDING GEAR INDICATOR PIN EXTENDED ALL THE TIME. AIRCRAFT WAS SENT TO THE HANGAR AND DURING OVERNIGHT SERVICE, THE NOSE LANDING GEAR TIRES WERE REPLACED IAW MM 32-40-0
- [SDR MEX2004055](https://openairdocs.org/sdr/MEX2004055.md): Switch · failed · Feb 12, 2004 · N205AM · Doug DC987 · Engine Oil System Wiring
  > FLT 944 - MEX-CUN - AIRCRAFT PERFORMED AN UNSCHEDULED LANDING AT VER AS A CONSEQUENCE DURING FLIGHT, THE RIGHT OIL STRAINER CLOGGING LIGHT TURNED ON. NO METALLIC BURRS WERE DETECTED DURING MAIN FILTER. LP5 AND LP6 OIL RESTRICTORS WERE CLEANED WITH AIR BUT FA
- [SDR MEX2004003](https://openairdocs.org/sdr/MEX2004003.md): Proximity Sensor · malfunctioned · Jan 1, 2004 · N205AM · Doug DC987 · Rudder Control System
  > FLT 6428 - MEX-LAS - CAPTAIN REPORTED THAT DURING FLIGHT CONTROL TEST WITH THE RT RUDDER THE BLUE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' REMAINED ON. AT HANGAR, THE RUDDER PROXIMITY SENSORS WERE VERIFIED AND IT WAS DETECTED A TROUBLE IN ONE SENSOR TARGET. THE
- [SDR MEX2003574](https://openairdocs.org/sdr/MEX2003574.md): Wire Harness · damaged · Dec 30, 2003 · N205AM · Doug DC987 · Flight Control System Wiring
  > FLT 605 - DFW-MEX - AIRCRAFT RETURNED TO PLATFORM, DURING THE TAXI THE LIGHT OF 'RUDDER TRAVEL UNRESTRICTED' DID NOT COME ON. THE SYSTEM WAS REVISED AND THE WIRE BUNDLE OF THE PROXIMITY SENSOR D1-33 WAS FOUND WITH DAMAGES. THE WIRE BUNDLE WAS REPAIRED IAW MM
- [SDR MEX203546](https://openairdocs.org/sdr/MEX203546.md): Tire · debonded · Dec 4, 2003 · N205AM · Doug DC987 · Tire
  > AFTER LANDING WAS LISTED AN STRONG NOISE IN THE MAIN LANDING GEAR. DURING REVISION OF THE MENTIONED AREA WERE FOUND SEVERAL DAMAGES IN THE NEARBY AREA OF THE LEFT MLG CAUSED BY A TREAD SEPARATION. AC WAS CARRIED TO THE HANGAR TO REPAIR THE FOLLOWING AFFECTED
- [SDR MEX2003287](https://openairdocs.org/sdr/MEX2003287.md): Tube · clogged · Jul 13, 2003 · N205AM · Doug DC987 · Engine Oil Distribution (Airframe Furnished)
  > FLT 440 - GDL-MTY - AIRCRAFT RETURN TO PLATFORM, DURING TAXIING THE CLOGGING LIGHT OIL ENGINE NR 2 ON. THE RESTRICTORS LP5 AND LP6 WERE CLEANED, BOTH ENDS LP5 AND LP6 TUBES WERE SERVICED WITH AIR PRESSURE TO REMOVE ANY CONTAMINATION AND THE DIFFERENTIAL PRESS
- [SDR MEX2003171](https://openairdocs.org/sdr/MEX2003171.md): Csd · failed · May 11, 2003 · N205AM · Doug DC987 · Alternator-Generator Drive
  > DURING TAXING, THE CSD TEMPERATURE INDICATES 380 DEGREES ON ENGINE NR 2. THE CSD, AC GENERATOR AND CSD EXCHANGER WERE REPLACED IAW MM 24-10-01. MM 24-10-01 AND MM 24-10-03, RESPECTIVELY, TEST CORRECT.
- [SDR MEX2003020](https://openairdocs.org/sdr/MEX2003020.md): Proximity Switch · failed · Jan 2, 2003 · N205AM · Doug DC987 · Leading Edge Slat Control System
  > FLT 486 - MEX-SLC - AIRCRAFT RETURNED, WHEN SLAT RETRACTED, THE LIGHTS SLAT DISAGREE CAME ON AND 280 KTS THE OVERSPEED ALARM WAS ACTIVATED. SPEED WAS REDUCED BELOW 280 AND AFTER 3 MINUTES LIGHT WENT OFF. IAW THE INSTRUCTIONS OF SHIFT FOREMAN AIRCRAFT RETURNE
- [SDR MEX2002144](https://openairdocs.org/sdr/MEX2002144.md): Hose · leaking · Aug 5, 2002 · N205AM · Doug DC987 · Cabin Pressure Control System
  > FLT 602 - MEX-DFW - AIRCRAFT RETURN TO FLIGHT DUE TO PRESSURIZATION FAILURE FLOW LIGHT ON WITH A 7.5 OF CABIN DIFFERENTIAL PRESSURE AT 10000 FT. HOSE RUBBER LEFT COOLER TURBINE WERE CHANGED IAW MM 21-20-00, TESTS OK. (M)
- [SDR ASM2002F00006](https://openairdocs.org/sdr/ASM2002F00006.md): Indicator · inaccurate · May 20, 2002 · N205AM · Doug DC987 · Attitude and Direction Data System
  > AIRCRAFT RETURN TO FLIGHT AS A CONSEQUENCE OF 60 DEGREE DIFFERENCE ON LEFT HEADING OR AUXILIARY AHRS, DIFFERENCE COULD NOT BE CORRECTED. AHRS ELECTRICAL CONNECTOR WAS CLEANED AND AHRS NR 1 WAS INTERCHANGED WITH AHRS NR 3, TESTS PERFORMED IAW MM.
- [SDR MEX2002084](https://openairdocs.org/sdr/MEX2002084.md): Relay · failed · Mar 25, 2002 · N205AM · Doug DC987 · Outside Air Temperature Indicator/Sensor
  > FLT 608 - MEX-DFW - AIRCRAFT RETURNED TO SOUTH POSITION AS CONSEQUENCES OF OVERHEATING OF THE RAT PROBE AND A FAIL FLAG WAS APPEARED. DURING THE CHECKING SYSTEM IT WAS FOUND ALSO THAT THE TAKEOFF ALARM DID NOT WORK. IT WAS DETECTED A TROUBLE WITH THE RELAY R

## 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 = 'N205AM' AND deregistration_id = 'N205AM-2010-10-08'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N205AM-2010-10-08/reports

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