What was found
ON TEST FLIGHT AFTER INSTALLATION OF ACTUATOR, THE T/R PEDAL WAS STIFF IN LEFT FORWARD QUADRANT.
- Difficulty date
- December 23, 1996
- Submitted
- March 26, 2000
- Operation
- General aviation
- Aircraft
- N214AE
- Make and model
- Bolkms BK117B1
- Aircraft serial
- 7206
- System (JASC)
- 6720 · Tail Rotor Control System
- Part
- Actuator
- Part number
- 741C000005
- Condition
- Defective
- Location
- T/R
- Stage of operation
- NR
- Nature of condition
- F
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.