# Service difficulty reports: N214AM, cancelled Aug 12, 2010

A list on [N214AM, cancelled Aug 12, 2010](https://openairdocs.org/deregistered/N214AM-2010-08-12.md).

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

- [SDR ASMF200709004](https://openairdocs.org/sdr/ASMF200709004.md): Switch · out of position · Sep 12, 2007 · N214AM · Doug DC987 · Cabin Pressure Control System
  > AIRCRAFT PERFORMED AN EMERGENCY DESCENT 20 MINUTES PRIOR TO LANDING, DUE TO UNCONTROLLABLE DEPRESSURATION. MAINTENANCE PERSONNEL VERIFIED THE PNEUMATIC SYSTEM FOR LEAKS AS WELL AS THE AIR CONDITIONED SYSTEM AND THE DUCTS OF ANTI-ICE SYSTEM IAW MPCM 36-10-00,
- [SDR ASMF200708003](https://openairdocs.org/sdr/ASMF200708003.md): Shutoff Valve · leaking · Aug 12, 2007 · N214AM · Doug DC987 · Hydraulic System, Main
  > AIRCRAFT RETURN TO PLATFORM DURING TAXI, CREW SELECTED SLATS EXTEND AND THE HYDRAULIC QUANTITY LIGHT TURNED ON. MAINTENANCE DETECTED HYDRAULIC LEAK IN RT SYSTEM AND QUANTITY ZERO, SO THE SYSTEM WAS SERVICED AND HYDRAULIC PRESSURE WAS APPLIED AND THE LEAK WAS
- [SDR ASMF200707005](https://openairdocs.org/sdr/ASMF200707005.md): Switch · failed · Jul 5, 2007 · N214AM · Doug DC987 · Fuel Controlling System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO CAPTAIN REPORTED THAT THE LT INLET FUEL LOW PRESSURE AND MASTER CAUTION LIGHTS TURNED ON. REPORT WAS DEFERRED IAW MEL 73-3. DURING OVERNIGHT CHECK AT MEX, MAINTENANCE PERSONNEL REPLACED THE LOW FUEL PRESSURE CAUTION SWITCH
- [SDR ASMF200707002](https://openairdocs.org/sdr/ASMF200707002.md): A/C Pack · leaking · Jul 1, 2007 · N214AM · Doug DC987 · Air Distribution System
  > AIR TURNED BACK DUE TO HIGH TEMPERATURE IN TAIL CONE, LIGHT TURNED ON AND RT ENGINE WITH LOW ACCELERATION. MAINTENANCE CORRECTED PNEUMATIC LEAKS IN THE LT AND RT AIR-CONDITIONED SYSTEMS IAW MM 36-20-02 AND MPCM 21-10-00; ADDITIONALLY, THE ACCELERATION CAMS AN
- [SDR ASMF200610014](https://openairdocs.org/sdr/ASMF200610014.md): Strake · damaged · Oct 31, 2006 · N214AM · Doug DC987 · Fuselage Main, Plate/Skin
  > DURING TRANSIT CHECK, THE RIGHT FUSELAGE NOSE STRAKE WAS DETECTED DAMAGED WITH 1 INCH LENGTH X.7500 INCH WIDTH AND.1875 INCH OF DEPTH. RT FUSELAGE NOSE STRAKE WAS REPLACED IAW MM 53-30-01, TESTED CORRECT.
- [SDR ASMF200605012](https://openairdocs.org/sdr/ASMF200605012.md): Door · ground damage · May 20, 2006 · N214AM · Doug DC987 · Passenger/Crew Doors
  > DURING TRANSIT CHECK, AIRCRAFT WAS STRUCK ON THE MAIN PASSENGERS DOOR BY MOBIL STAIRS. AIRCRAFT WAS INSPECTED IAW SRM 51-02 AND DAMAGE WAS WITHIN LIMITS. DURING OVERNIGHT CHECK AT MEX, FINAL REPAIR WAS PERFORMED IAW SRM 51-02, FIG 1, ALL CORRECT.
- [SDR ASMF200604011](https://openairdocs.org/sdr/ASMF200604011.md): Gcu · failed · Apr 22, 2006 · N214AM · Doug DC987 · AC Generation System
  > AIRCRAFT RETURNED TO PLATFORM DUE TO AC CROSS TIE LIGHT TURNED ON. AT PLATFORM, THE RIGHT GCU WAS REPLACED IAW MM 24-20-04, TESTED CORRECT IAW MM 24-20-00.
- [SDR ASMF200603015](https://openairdocs.org/sdr/ASMF200603015.md): Hydraulic Line · leaking · Mar 28, 2006 · N214AM · Doug DC987 · Hydraulic System, Main
  > AIRCRAFT RETURNED FLIGHT, AFTER TAKEOFF AND LANDING GEARS UP, THE RIGHT HYDRAULIC FLUID QUANTITY WENT DOWN TO 2 QUARTS. AFTER LANDING, THE BRAKES TEMPERATURE REACHED 350 °C AND GOT STUCK. DURING MAINTENANCE REVISION A RIGHT HYDRAULIC SYSTEM LEAK WAS DETECTED
- [SDR ASMF200505005](https://openairdocs.org/sdr/ASMF200505005.md): Computer · failed · May 3, 2005 · N214AM · Doug DC987 · Engine Pressure Ratio (EPR)
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF LEFT ENGINE EPR INDICATOR WAS OUT OF SERVICE. EPR TRANSMMITER WAS REPLACED IAW MM 77-11-02, ENGINE WAS TESTED, ALL CORRECT.
- [SDR ASMF200504018](https://openairdocs.org/sdr/ASMF200504018.md): Fcu · failed · Apr 22, 2005 · N214AM · Doug DC987 · Fuel Control/Turbine Engines
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING TAXING, THE LEFT ENGINE GENERATOR WENT OUT OF ITS BAR TURNING ON THE MASTER CAUTION LIGHT AND THE LEFT OIL PRESSURE WAS LOW (30 PSI). DURING ENGINE CHECK THE FCU DID NOT MAINTAIN THE RPMS IN IDLE AND DE
- [SDR ASMF200504016](https://openairdocs.org/sdr/ASMF200504016.md): Transmitter · dirty · Apr 19, 2005 · N214AM · Doug DC987 · Engine Oil Pressure
  > AIRCRAFT RETURNED TO PLATFORM. DURING PUSH BACK, LT ENGINE STARTED NORMALLY AND AFTER RT ENGINE STARTED, THE LT ENGINE PRESSURE DECREASE TO 35 PSI’S. DURING REVISION WAS DETECTED OVERFILL OIL. THE EXCESS OIL WAS DRAINED AND PRESS OIL TRANSMITTER CONNECTOR WAS
- [SDR ASMF200504009](https://openairdocs.org/sdr/ASMF200504009.md): Starter · failed · Apr 10, 2005 · N214AM · Doug DC987 · Engine Starter
  > DURING ENGINES STARTING, CAPTAIN REPORTED THAT THERE WAS NOT LEFT ENGINE PARAMETERS INDICATION. THE PNEUMATIC PRESSURE AND STARTER VALVE OPENING WERE VERIFIED IAW MM 80-00-00, BEING CORRECT, SO IT WAS DETERMINED THE STARTER REPLACEMENT. THE LEFT ENGINE WAS STA
- [SDR ASMF200502013](https://openairdocs.org/sdr/ASMF200502013.md): Fuel Control · failed · Feb 24, 2005 · N214AM · Doug DC987 · Fuel Control/Turbine Engines
  > CAPTAIN REPORTED LEFT ENGINE WITH OSCILLATIONS IN ALL ITS PARAMETERS. THE COMBUSTION CHAMBER WAS SERVICED AND WATER TRAMP WAS DRAINED IAW 72-40-01, ALL CORRECT. DURING OVERNIGHT SERVICE LEFT FCU WAS REPLACED IAW MM 73-12-01 AND THE LEFT ENGINE WAS TESTED IAW
- [SDR ASMF200412006](https://openairdocs.org/sdr/ASMF200412006.md): Ignition Unit · failed · Dec 17, 2004 · N214AM · Doug DC987 · Ignition Power Supply
  > AIRCRAFT RETURNED TO PLATFORM AS A CONSEQUENCE OF DURING ENGINES STARTING, IGNITION SYSTEM FAILED IN BOTH ENGINES. DURING MAINTENANCE REVISION WAS DETECTED THAT 115VAC WAS NOT AVAILABLE AND SWITCH FASTENERS LOOSEN IN TWO LINES. FASTENERS WERE TIGHTENED AND E
- [SDR ASMF200411005](https://openairdocs.org/sdr/ASMF200411005.md): Ignition Unit · failed · Nov 9, 2004 · N214AM · Doug DC987 · Ignition Power Supply
  > DURING ENGINES STARTING, LT ENGINE DID NOT START. CIRCUIT BREAKER WAS CHECKED AND EDP TEST WAS PERFORMED IAW MM 72-21-01, ALL CORRECT. LT ENGINE START WAS PERFORMED AND FAIL CONTINUE, EGT AND RPM INDICATIONS WERE NOT SHOWN. IGNITION BOX AND EXCITER PLUG CABLE
- [SDR ASMF200406023](https://openairdocs.org/sdr/ASMF200406023.md): Tab · damaged · Jun 21, 2004 · N214AM · Doug DC987 · Elevator, Tab Structure
  > DURING OVERNIGHT SERVICE LIGHTING STRIKE DAMAGE WAS DETECTED IN LT ELEVATOR TAB, WITH 1 INCH OF DIAMETER. LIGHTING STRIKE INSPECTION WAS PERFORMED IAW MM 05-53-00 AND ELEVATOR TAB WAS REPLACED IAW MM 27-30-03, TEST CORRECT.
- [SDR ASMF200404001](https://openairdocs.org/sdr/ASMF200404001.md): Computer · failed · Apr 1, 2004 · N214AM · Doug DC987 · Engine Emergency Shutdown System
  > AIRCRAFT SUSPENDED TAKE OF AT 100 KTS AND RETURNED TO PLATFORM AS A CONSEQUENCE OF THE RIGHT ENGINE DID NOT REACH THE TAKE OF THRUST, IT ONLY REACHED 1.6 OF EPR. AT MEX PLATFORM, TECHNICAL PERSONNEL PERFORMED AN ACCELERATION TEST REACHING ONLY 1.7 OF EPR'S.
- [SDR ASMF200403008](https://openairdocs.org/sdr/ASMF200403008.md): Controller · malfunctioned · Mar 15, 2004 · N214AM · Doug DC987 · Cabin Pressure Controller
  > AIRCRAFT RETURNED OF FLIGHT AS A CONSEQUENCE OF DURING CLIMB AT 33,000 FEET, AFT CARGO DOOR AND AFT STAIRWAY DOOR LIGHTS TURNED ON AND CABIN STARTED TO DEPRESSURIZE. CARGO COMPARTMENT DOORS WERE CHECKED, ALL CORRECT. AIRCRAFT WAS PRESSURIZED WITH A GROUND PN
- [SDR MEX2004041](https://openairdocs.org/sdr/MEX2004041.md): Bungee Cylinder · damaged · Feb 1, 2004 · N214AM · Doug DC987 · Main Landing Gear Strut/Axle/Truck
  > CAPTAIN REPORTED THAT THE NLG RED LIGHT TURNE ON AND OFF SEVERAL TIMES DURING CLIMB, CRUISE AND DESCENT. AT PLATFORM IT AWS PERFORMED A BITE TO THE PROXIMITY SWITCH UNIT IAW MM. TEST, OK, AFTER CAPTAIN REPORTED THAT DURING CLIMB, A LOUD NOISE WAS HEARD IN TH
- [SDR MEX2004020](https://openairdocs.org/sdr/MEX2004020.md): Duct · broken · Jan 16, 2004 · N214AM · Doug DC987 · Ice/Rain Protection System
  > AIRCRAFT RETURNED DUE TO LIGHT OF TAIL CONE HIGH TEMPERATURE CAME ON, AFTER 3 MINUTES THAT THE ANTI-ICE PROTECTION WAS USED. AIRCRAFT WAS CARRIED TO THE HANGAR TO ATTEND REPORT. AT OVERNIGHT SERVICE, THE ANTI-ICE DUCT ASSY WAS REPLACED AND SYSTEM WAS TESTED
- [SDR MEX2003558](https://openairdocs.org/sdr/MEX2003558.md): Blade · damaged · Dec 21, 2003 · N214AM · Doug DC987 · Turbine Engine Compressor Section
  > AIRCRAFT AIR TURN BACK, DURING CLIMB THE RIGHT ENGINE STALLED. AT PLATFORM, IT WAS DETECTED DAMAGES IN FOUR C1 BLADES AND IN 2 C2 BLADES. INSPECTOR AND TECHNICAL PERSONNEL WERE SENT TO EVALUATE THE DAMAGES AND START THE CORRECTIVE ACTIONS. ENGINE WAS REPLAC
- [SDR MEX2003433](https://openairdocs.org/sdr/MEX2003433.md): Control Valve · malfunctioned · Sep 17, 2003 · N214AM · Doug DC987 · Brake Anti-Skid Section
  > AIRCRAFT RETURN TO PLATFORM DUE TO DURING TAXI THE FOURTH ANTI-SKID LIGHT TURNED ON. CIRCUIT BREAKERS WERE RESET AND ANTI-SKID BOX CONNECTORS WERE CLEANED NON REPRODUCING THE FAIL. AFTER WORKS, CAPTAIN REPORTED THE ANTISIDE LIGHTS TURNED ON AGAIN. DURING CH
- [SDR MEX2003379](https://openairdocs.org/sdr/MEX2003379.md): Battery · overheated · Aug 21, 2003 · N214AM · Doug DC987 · Battery/Charger System
  > FLT 519 - MEX-VSA - AIRCRAFT ARRIVED WITH CAPTAIN REPORT OF HOT BATTERIES AND SMOKE UNDER THE FUSELAGE. DURING REVISION DETECTED BATTERIES AND BATTERIES CHARGER WITH OVERHEAT. THE BATTERIES AND BATTERY CHARGER WAS REPLACED IAW MM 24-30-01/02, ALL CORRECT. (
- [SDR MEX2002306](https://openairdocs.org/sdr/MEX2002306.md): Exciter · failed · Sep 20, 2002 · N214AM · Doug DC987 · Exciter
  > AIRCRAFT RETURNED TO PLATFORM DUE TO AN IGNITION FAILURE IN RT ENGINE. AT PLATFORM THE TECH TRIED TO START THE ENGINE BUT THERE WAS TROUBLE WITH THE EXCITER IGNITION BOX. UNIT WAS REPLACED IAW MM.
- [SDR MEX2002238](https://openairdocs.org/sdr/MEX2002238.md): Engine · failed · Jul 24, 2002 · N214AM · Doug DC987 · APU Core Engine
  > CREW REPORTED THE PRESENCE OF SMOKE IN CABIN DUE TO AN OIL LEAK IN THE LT A/C PACK. THE MAGNETIC CAP OF THE COOLING TURBINE HAD METAL CHIPS, A/C PACK WAS INOPERATIVE PER MEL. APU WAS REPLACED IAW MM, FOR LACK OF OIL AND LEAKAGE THROUG THE LOAD CONTROL VALVE
- [SDR MEX2002060](https://openairdocs.org/sdr/MEX2002060.md): Fuel Control · failed · Mar 8, 2002 · N214AM · Doug DC987 · Fuel Control/Turbine Engines
  > FLT 419 - MEX-VSA - PILOT REPORTED A MISALIGNMENT OF MORE THAN.5 INCH BETWEEN THROTTLE LEVERS. ROD END OF FCU WAS REPLACED AND RIGGING AND OPERATIONAL TEST TRIM, WERE PERFORMED IAW MM 71-00-01. (M)
- [SDR MEX2002136](https://openairdocs.org/sdr/MEX2002136.md): Computer · failed · Mar 5, 2002 · N214AM · Doug DC987 · Integrated Flight System
  > FLT 478 - MZT-HMO - THE CAPTAIN REPORT THAT DURING CLIMB MZT-HMO, THE AIRCRAFT HAD HEADING PROBLEMS. THE FO'S WAS OUT OF SERVICE AND THE FLIGHT DIRECTOR BARS WERE LOST WHEN EFIS BOTH WAS SELECTED ON 1, THE PROBLEM WAS INTERMITTENT DURING ALL THE FLIGHT. AT H
- [SDR MEX2002046](https://openairdocs.org/sdr/MEX2002046.md): Control Valve · failed · Feb 21, 2002 · N214AM · Doug DC987 · Brake Anti-Skid Section
  > HMO-LAS - WHEN LANDING GEAR GOT DOWN, ANTI-SKID IGHTS TURNED ON. AS CONSEQUENCE OF SPARE PARTS MISSING, AN AIRCRAFT CHANGE TOOK PLACE. LEFT ANTI-SKID DUAL CONTROL VALVE WAS REPLACED IAW MM 32-43-02, TESTS WERE PERFORMED OK.

## 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 = 'N214AM' AND deregistration_id = 'N214AM-2010-08-12'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N214AM-2010-08-12/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.