Preflight Procedure and Hot Start in a Cessna 310!!!

Jasper County Airport Landing and Pre-Flight Procedures

Automated Weather Observation

• The weather at Jasper County Airport is reported as calm winds, visibility of 10 miles, clear skies below 12,000 feet, temperature at 18°C, and an altimeter setting of 30.11 inches.

Approach and Landing

• The pilot announces their approach to runway 18 at Jasper County, confirming gear and flaps are set for landing. They mention being on the glide slope with three green lights indicating a safe landing configuration.

• As they finalize their approach, the pilot emphasizes maintaining a proper descent rate while ensuring all systems are functioning correctly before landing. They confirm being on final approach with three greens still visible.

Post-Landing Procedures

• After landing, the pilot communicates that they will clear all runways and proceed to self-service fuel similar to refueling a car. They prepare for pre-flight procedures after refueling.

Pre-Flight Procedure Overview

Fuel Straining Process

• The pilot begins the pre-flight procedure by checking fuel using a GATS jar which allows for filtering and returning fuel back into tanks if necessary. They check main tanks first for clarity in color (blue indicates no contamination).

• Sumps under both wings are checked next; all samples remain clear blue indicating clean fuel without water separation issues. This includes checks on cross-feed sumps between engines as well.

Oil Check Procedure

• The oil dipstick is accessed using a Phillips screwdriver; the engine's warmth necessitates caution during this process to avoid burns while checking oil levels post-operation. The dipstick is cleaned and reinserted to ensure accurate readings before securing it again.

Systems Check Before Flight

• A master switch activation leads to checks on landing gear lights (three greens), flap functionality, fuel transfer pumps, and stall horns from within the cabin before proceeding with external walk-around inspections of static ports and control surfaces for obstructions or damage.

Final Walk-Around Inspection

• During the walk-around inspection, static ports are confirmed clear of debris; control surfaces such as elevators move freely without resistance ensuring operational readiness prior to flight departure checks across both sides of the aircraft are completed thoroughly for safety assurance before takeoff preparations begin.

Pre-Flight Inspection and Engine Start Procedures

Overview of the Aircraft's Condition

• The aircraft features three static wicks on the back end, with smooth surfaces noted during inspection. The pilot static port is clearly visible on the back left side.

• A thorough check of the left engine strut reveals good tire pressure and no obstructions in the mufflers. Ailerons are functioning properly with free movement confirmed.

• The front of the left wing shows no unconformities, and all vortex generators are intact. The alternator belt tension is adequate, with no debris found in the cowling.

Detailed Checks on Wings and Nose

• Propellers are inspected for smoothness; air intake is clear, ensuring optimal performance. Vortex generators on the inner wing section are also checked.

• The pitot tube at the nose is confirmed to be clear of obstructions. Tire pressure in the nose strut is satisfactory, and there are no blockages in the nose wheel well.

Right Wing Inspection

• Similar checks performed on the right wing confirm smoothness and absence of obstructions. Static wicks and aileron functionality are verified again.

Hot Start Procedure for Engines

• For a hot start, throttle must be fully engaged while simultaneously pressing the start button and applying a little prime to ensure successful ignition without flooding.

Run-Up Procedures Explained

• After completing pre-flight checks, a run-up procedure begins at runway 36. Throttles for both engines need to be set correctly along with mixture settings before starting.

• Left engine RPM is brought up to 1700; alternator checks follow by turning off one alternator to verify failure light activation before switching it back on.

Final Checks Before Flight

• Propeller cycling occurs twice followed by checking alt air intake for any RPM loss; all readings remain within green limits indicating proper function.

• Consistent suction readings confirm operational integrity before concluding that both engines have been adequately prepared for flight.

This structured overview encapsulates critical aspects of pre-flight inspections and engine start procedures as discussed in the transcript, providing an efficient reference guide for understanding essential aviation protocols.