Initial Checks Flashcards
APPROACHING THE AIRCRAFT CHECKS
- General Position ….. Clear of obstacles, No significant tailwind, No leaks
- Ground Fire Extinguisher ….. Available
- Chocks ….. In
- Control Locks ….. Removed
- Aircraft Identity….. Check correct aircraft
COCKPIT CHECKS
- Canopy …. Condition, opens easily
- Canopy Red Lock Lever ….. Telltale wire intact
- Canopy Jettison Pins ….. Telltale wires intact
- ALT STATIC ….. NORMAL, telltale wire intact
- ELT ….. ARM
- All switches ….. Down, except
START SWITCH
GEN
PROP OVERSPEED TEST /
INTAKE HEAT TEST … Central
(20 Switches down, 3 Central) - Ventilation Levers … Exercise
- ALL CBs & CAS Mute ….. In, 12 collars in place
- FLARM CB (Far left) ….. Out if night flying
- POWER Lever ….. FI
- Condition Lever ….. CUT OFF / FEATHER
- EMERGENCY LANDING GEAR EXTEND Control ….. Turned CW to stop
- Speaker ….. OFF
- SD Card ….. Insert
- USB Mission Plan ….. Upload as required
- Aircraft Manual Stowage ….. Secure
- Hydraulic Fluid Pressure ….. Within limits
- Hydraulic Fluid Level ….. Above minimum level
- Baggage Hold ….. Clear or items secure
- First Aid Kit & Torch ….. Secure
- Fire Extinguisher ….. Secure, pressure in green, telltale intact
- Hammer ….. Secure, quick pin in
- Loose Articles ….. None
- Underseat Area ….. Clear.
RIGHT WING CHECKS
- Flap ….. Condition, linkages secure
- Aileron & Tab ….. Condition, linkages secure
- Static Dischargers (2) ….. Condition
- Wing Tip & Winglet ….. Condition
- Nav / Anti-Coll Light ….. Condition
- Landing / Taxy Light ….. Condition
- Fuel Filler Cap ….. Secure
- Stall Warning Vane ….. Free to move
- Wing Fuel Gauge ….. Check contents
- Tyre ….. Check for creep & condition
- Brake Line Connections ….. Check for leaks
NOSE SECTION CHECKS
- RH Engine Exhaust ….. Clear
- RH Cowling ….. Secure
- Engine Air Intakes (3) ….. Clear
- Spinner ….. Check for cracks
- Propeller ….. Condition
- Oil Filter ….. Sight glass, red pin not visible
- LH Cowling ….. Secure
- LH Engine Exhaust ….. Clear
- Underside Engine Cowling ….. Check for fluid leaks
- Nose Gear Strut ….. Correct extension (approx 6 ins)
- Tyre ….. Condition
- Gear Down Light ….. Condition
LEFT WING CHECKS
- Tyre ….. Check for creep & condition
- Brake Line Connections ….. Check for leaks
- Wing Fuel Gauge ….. Check contents
- OAT Probes ….. Condition
- Pitot - Static Tube ….. Cover removed, check clear
- Fuel Filler Cap ….. Secure
- Landing / Taxy Light ….. Condition
- Nav / Anti-Coll Light ….. Condition
- Wing Tip & Winglet ….. Condition
- Static Dischargers (2) ….. Condition
- Aileron ….. Condition, linkages secure
- Flap ….. Condition, linkages secure
FUSELAGE / EMPENNAGE CHECKS
- Antennas (5) ….. Condition
- Fin & Control Surfaces ….. Condition
- Mass Balances (4) ….. Condition#
- Trim Tabs (3) ….. Condition
- Nav Lights (2) ….. Condition
- Static Dischargers (4)
INTERNAL CHECKS
- BUS TIE ….. ON
- BATT ….. ON
- Seats & Rudder Pedals ….. Adjusted, locked, cushion as required
- Harnesses ….. Strap in
- PARKING BRAKE ….. Set & applied
- Chocks ….. Removed
- Stall Warning System ….. Functional Check
After Right PFD / LEFT MFD self test complete:
- Nav Database ….. Check date, press any key to start 2 min sensor acquisition
9 LDG GEAR Selector ….. Check DN, 3 greens - BLEED ….. Fully in
- FUEL Tank Selector ….. LEFT
- Condition Lever ….. Exercise, set CUT OFF / FEATHER
- POWER Lever ….. Exercise, set FI
- FRICTION ….. Set
- Trim Wheel ….. Exercise, set TAKE-OFF
- Flying Controls ….. Full, free & correct movement
After 2-minute sensor acquisition period
- Audio Warnings ….. Cancel
- Right PFD Map display ….. Note OAT
- Right PFD / Left MFD ….. < TO ESSNTL
- Voltmeter ….. Min 24v
- External Power ….. As required, max 28.0V if ON
- P/S HEAT ….. ON functional check, then OFF
- Right PFD …. Set Fuel TOTAL, Expand CAS if required
- Canopy ….. As required
- NAV LIGHT ….. ON
- ATIS & Start Clearance ….. Obtain
Starting Procedure
- Condition Lever ….. CUT OFF / FEATHER
- POWER Lever ….. FI
- FUEL PUMP ….. ON, F PRESS OUT
4 STBY FUEL PUMP ….. AUTO
Give start signal to ground crew. When clear:
If TOT above 150C, BLOW engine until below 150C then wait for N1 to decay between 1% and 4%. Note time at BLOW to ensure total starter time will not exceed 30 seconds, otherwise wait 1 minute for starter/generator cooling. A normal start cycle takes approx 15 seconds for starter to disengage at 58% N1.
- TOT ….. <150C
- START Switch ….. Trigger START, release OFF
When N1 accelerates through calculated speed:
- Condition Lever ….. HIGH
- TOT ….. Rising within 3 sec
- Propeller ….. Turning by 25% N1, Unfeathering by time N1 stabilizes
When engine has stabilized at IDLE (60% N1 or above):
- OIL LO PRESS ….. Caption Out
- IGN ON ….. Caption Out
- Oil Pressure ….. Within limits (>50 PSI)
- N2 ….. Min 1220 RPM
If External Power used:
a. EXTERNAL POWER ….. OFF
b. POWER Lever ….. GI
c. External Power ….. Disconnected
d. POWER LEVER ….. FI
- GEN ….. ON, voltages approx 28V
- GEN Ammeter ….. Indicates +ve charge
- N1 & TOT ….. Monitor
- AVIONICS MASTER ….. ON
- FLARM ….. Observe self-test unless night flying