The RCA26 Series electric attitude indicator employs an electrically driven rotor to sense movement in the roll and pitch axis and transmits the information to the pilot through a pictorial presentation. They have a built-in inverter which converts aircraft DC power to the required AC voltage and frequency. All units have a pull cage knob and a power failure flag. Optional slip indicator (RCA 444-0011-01) can be added.
- 5° Tilt
- 28VDC
- Lighted
- Movable pointer
- Fixed roll dial
- Blue/brown display with black roll dial
- White pointer and airplane
This instruments meets or exceeds requirements of TSO C4c and Aeronautical Standard AS396B.
ELECTRICAL REQUIREMENTS
Starting current @ 14VDC: 2.4 A Max
Running current @ 14VDC: 1.21 A Max
ELECTRICAL REQUIREMENTS
Starting current @ 28VDC: 1.40 A Max
Running current @ 28VDC: 0.62 A
DIMENSIONS
Length: 8.14 in. max.
Width: 3.38 in. max
Height: 3.38 in. max
Weight: 2.3 lbs.
