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37000 Feet | Browse and search NASA's Aviation Safety Reporting System |
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| Attributes | |
| ACN | 1057470 |
| Time | |
| Date | 201212 |
| Local Time Of Day | 0601-1200 |
| Place | |
| Locale Reference | ZZZ.Airport |
| State Reference | US |
| Environment | |
| Light | Daylight |
| Aircraft 1 | |
| Make Model Name | Eurocopter AS 350/355/EC130 - Astar/Twinstar/Ecureuil |
| Operating Under FAR Part | Part 135 |
| Flight Phase | Parked |
| Component | |
| Aircraft Component | Powerplant Fuel Control |
| Person 1 | |
| Function | Technician |
| Qualification | Maintenance Powerplant Maintenance Airframe |
| Events | |
| Anomaly | Aircraft Equipment Problem Critical Deviation - Procedural Published Material / Policy |
Narrative:
[I was] performing scheduled maintenance. Airworthiness directive (ad) required on hydro mechanical units (hmu) on number 1 and number 2 engines; which required removal of hmus and several cannon plugs. [I] complied with ad and other maintenance. [I] installed hmus. Other technicians (four) checked-over work performed and checked hmus for correct installation and foreign object debris (FOD). Pilot performed a detailed preflight to check for FOD. [I] prepped aircraft for a ground run/leak check to check operation of hmus. [I] applied power and 'caution fli/no tq' indication on number 2 engine side. [All] four technicians removed cannon plugs; cleaned and reinstalled. [I] applied power with no caution. [I] performed successful ground run. [I] performed a check flight; while landing at base; same cautions appeared. Removed cannon plugs and torque (tq) pickup; cleaned reinstalled; ground run ok. Check flight ok. Training performed 1.5 check ride with no cautions. Several times aircraft is run and positioned on dolly for bad weather; no problems. I am off on my scheduled days; will cover for mechanic Y [when I return]. Go to aircraft to troubleshoot and meet engine manufacturer technical representative and mechanic Z. After several hours troubleshooting; I look at #2 engine for the 3rd time and notice that a cannon plug to the stepper motor (hard to see); (a hard line and two other sensors and cannon plugs are over top of this); is not seated all the way. [I] managed to get it secured all the way. Applied power and all systems are normal; no 'cautions.' [I] checked number 1 engine for exceedances. Aircraft released for return to service. Was told this has happened on another occasion with same results. [Recommend] better lighting; removal of cowlings; fire walls and etc.; to get a better look; bigger mirrors.
Original NASA ASRS Text
Title: After engine ground runs; flight checks and several hours of troubleshooting for a recurring Caution FLI/No Tq (torque) indication on a Eurocopter helicopter; an Aircraft Maintenance Technician (AMT) notices a cannon plug to the Stepper Motor on Number 2 Engine was not seated all the way. Same issue happened before with same results.
Narrative: [I was] performing scheduled maintenance. Airworthiness Directive (AD) required on Hydro Mechanical Units (HMU) on Number 1 and Number 2 Engines; which required removal of HMUs and several cannon plugs. [I] complied with AD and other maintenance. [I] installed HMUs. Other technicians (four) checked-over work performed and checked HMUs for correct installation and Foreign Object Debris (FOD). Pilot performed a detailed preflight to check for FOD. [I] prepped aircraft for a ground run/leak check to check operation of HMUs. [I] applied power and 'Caution FLI/No Tq' indication on Number 2 Engine side. [All] four Technicians removed cannon plugs; cleaned and reinstalled. [I] applied power with no caution. [I] performed successful ground run. [I] performed a check flight; while landing at Base; same cautions appeared. Removed cannon plugs and torque (Tq) pickup; cleaned reinstalled; ground run OK. Check flight OK. Training performed 1.5 check ride with no cautions. Several times aircraft is run and positioned on dolly for bad weather; no problems. I am off on my scheduled days; will cover for Mechanic Y [when I return]. Go to aircraft to troubleshoot and meet Engine Manufacturer Technical Representative and Mechanic Z. After several hours troubleshooting; I look at #2 Engine for the 3rd time and notice that a cannon plug to the Stepper Motor (hard to see); (a hard line and two other sensors and cannon plugs are over top of this); is not seated all the way. [I] managed to get it secured all the way. Applied power and all systems are normal; No 'Cautions.' [I] checked Number 1 Engine for exceedances. Aircraft released for return to service. Was told this has happened on another occasion with same results. [Recommend] better lighting; removal of cowlings; fire walls and etc.; to get a better look; bigger mirrors.
Data retrieved from NASA's ASRS site as of July 2013 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.