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|
Attributes | |
ACN | 886194 |
Time | |
Date | 201004 |
Local Time Of Day | 1201-1800 |
Place | |
Locale Reference | ZZZ.Airport |
State Reference | US |
Environment | |
Flight Conditions | VMC |
Light | Daylight |
Aircraft 1 | |
Make Model Name | Eurocopter AS 350/355/EC130 - Astar/Twinstar/Ecureuil |
Operating Under FAR Part | Part 135 |
Flight Phase | Cruise |
Route In Use | Vectors |
Flight Plan | IFR |
Component | |
Aircraft Component | Compass (HSI/ETC) |
Person 1 | |
Function | Captain Pilot Flying |
Qualification | Flight Crew Commercial |
Events | |
Anomaly | Aircraft Equipment Problem Less Severe Deviation - Procedural Clearance Deviation - Track / Heading All Types |
Narrative:
After dropping off a patient during a reposition flight to base approximately ten minutes into the flight I was given an instruction by ATC to turn to heading 180 vectors for traffic. I immediately turned to a heading of 180 as referenced by the directional gyro. Within one minute I was re-contacted by ATC and asked for current heading. I informed him; 179 degrees. He advised that I must have hellacious winds because he had me at 145 degrees; turn left heading 120. While receiving the new course instruction I discovered that the directional gyro was in error by as much as 35 degrees as verified with a cross check of the GPS and magnetic compass. I complied with new course and was within a few minutes given an instruction to resume own navigation; frequency change approved. No further communication was given by ATC. Upon the continued flight to base I confirmed that the directional gyro was unreliable in slave mode; but operative in free mode. After landing I wrote up the discrepancy in the aircraft log book and deferred the item per the MEL and contacted the mechanic. The mechanic responded and discovered corroded/contaminated terminal ends. He cleaned them and the aircraft deferral was cleared by the mechanic. A more attentive cross check with the magnetic compass and GPS would have discovered the directional gyro error earlier; preventing the apparent failure to comply with ATC instruction.
Original NASA ASRS Text
Title: An AS350 helicopter pilot reported that during ATC vectors he discovered the Directional Gyro had approximately a thirty five degree heading error. Maintenance later reported that corroded electrical connectors caused the equipment error.
Narrative: After dropping off a patient during a reposition flight to base approximately ten minutes into the flight I was given an instruction by ATC to turn to heading 180 vectors for traffic. I immediately turned to a heading of 180 as referenced by the Directional Gyro. Within one minute I was re-contacted by ATC and asked for current heading. I informed him; 179 degrees. He advised that I must have hellacious winds because he had me at 145 degrees; turn left heading 120. While receiving the new course instruction I discovered that the Directional Gyro was in error by as much as 35 degrees as verified with a cross check of the GPS and Magnetic compass. I complied with new course and was within a few minutes given an instruction to resume own navigation; frequency change approved. No further communication was given by ATC. Upon the continued flight to base I confirmed that the Directional Gyro was unreliable in slave mode; but operative in free mode. After landing I wrote up the discrepancy in the aircraft log book and deferred the item per the MEL and contacted the mechanic. The mechanic responded and discovered corroded/contaminated terminal ends. He cleaned them and the aircraft deferral was cleared by the mechanic. A more attentive cross check with the magnetic compass and GPS would have discovered the Directional Gyro error earlier; preventing the apparent failure to comply with ATC instruction.
Data retrieved from NASA's ASRS site as of April 2012 and automatically converted to unabbreviated mixed upper/lowercase text. This report is for informational purposes with no guarantee of accuracy. See NASA's ASRS site for official report.