What was found
(CAN) PILOT NOTED THAT TAIL ROTOR PEDALS WERE STIFF ON PRE-FLIGHT CHECK. TAIL ROTOR PITCH CHANGE SYSTEM CHECKED AND CLEANED. AIRCRAFT RETURNED TO SERVICE.
- Difficulty date
- June 28, 1999
- Submitted
- March 26, 2000
- Operation
- Air carrier
- Make and model
- Bolkms BO105S
- Engine
- Allsn 250C20B
- System (JASC)
- 6720 · Tail Rotor Control System
- Part
- Pedal
- Condition
- Stiff
- Location
- Tailrotor
- Stage of operation
- IN
- Nature of condition
- O
- Precautionary procedure
- K
As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.