Read the following technical passage:
"An aircraft's pitot-static system utilizes air pressure differentials to operate three essential flight instruments: the airspeed indicator, the altimeter, and the vertical speed indicator. Ram air pressure entering the forward-facing pitot tube drives the airspeed indicator alone. Ambient atmospheric pressure enters through flush-mounted static ports on the fuselage and is routed to all three instruments. When pitot tube drain holes become clogged in icing conditions, electrical heating elements prevent ice accumulation. If the static port freezes shut, the altimeter freezes at its current altitude and the vertical speed indicator drops to zero, but the system does not utilize engine bleed air to clear the blockage."
Based on the passage, match each operational statement with its corresponding factual status according to the text.
- Engine bleed air is channeled to clear frozen static ports.Explicitly identified as a method NOT used by the system to remove ice blockages.
- Electrical heating elements are used to prevent ice accumulation on the pitot tube.Directly confirmed as the safeguard mechanism against ice buildup on the pitot tube.
- Ambient air pressure from static ports is routed exclusively to the vertical speed indicator.Directly contradicted by the passage, which states static pressure is routed to all three instruments.
- Ram air pressure captured by the forward-facing pitot tube drives only the airspeed indicator.Directly confirmed as supplying pressure exclusively to a single flight instrument.