Cessna 182 skylane preflight inspection,

 

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CESSNA 182T PREFLIGHT INSPECTION

 





NOTE

Visually check airplane for general condition during walk around inspection. Airplane should be parked in a normal ground attitude. To make sure that fuel drain valve allow for accurate sampling. Use of the refueling steps and assist handles will simplify access to the upper wing surfaces for visual checks and refueling operations in cold weather remove even small accumulations of frost, ice or snow from wing. Tail and control surfaces. Also make sure that control surfaces contain no internal accumulations of ice or debris prior to flight. Check that pilot heater is warm to touch within 30 seconds with battery and pitot heat switches ON. If a night flight is planned. Check operation of all lights  Verify all LED landing / taxi light bulb are operational. (if installed) and make sure a flashlight is available 




1. CABIN 



1. Pitot tube cover..... Remove (check for pitot blockage 



2. Pilot's operating handbook..Accessible to pilot 





3. Garmin G1000 Cockpit reference guide.... Accessible pilot 




4. Airplane weight and balance..checked




5. Parking Brake............... SET 



6. Control wheel lock.........REMOVE 


WARNING 

When the master switch is on. Using an external power source. Or manually Rotating the propeller. Treat the propeller as if the Magnetos switch were ON do not stand nor allow anyone else to stand within the ARC of the propeller since A loose or broken wire. Or a component malfunction could cause The engine to start. 




7. Magnetos switch................OFF 











8. Avionics switch (BUS 1 &  BUS 2) OFF 








9. Master switch (ALT & BAT)..... ON 






10. Primary flight display (PFD) CHECK (verify PFD is ON) 







11. Fuel quantity (L AND  R) ....CHECK 








12. Low fuel L and low R annuciators.... CHECK (verify annuciators are not shown on PFD) 






13. OIL Pressure annuciator ....CHECK (verify annuciator is shown) 






14. Low Vacuum annuciator CHECK (verify annuciator is shown) 







15. Avionics switch (BUS 1).... ON 






16. Forward avionics fan......... CHECK 
(verify fan is heard 







17. Avionics switch (BUS 1).... OFF 








18. Avionics switch (BUS 2) .......ON 







19. ALT Avionics fan .............CHECK
 (verify fan is heard) 







20. Avionics switch (BUS 2) .....OFF 






21. Pitot heat switch................ ON 
(carefully check that pitot tube is warm to touch within 30 seconds) 







22. Pitot heat switch............ OFF 






23. stall warning system.... CHECK 
(gently move the stall vane upward and verify that the stall warning horn is heard) 






24. Low volts annuciator......CHECK 
(verify annuciator is shown) 








25. Master switch (ALT & BAT).... OFF 






26. Elevator and Rudder trim controls... Takeoff position 







27. Fuel selector valve............. BOTH 







28. ALT Static air ......OFF (push full in) 



29. Fire Extinguisher..... CHECK 
(verify Gage pointer in green arc)




2. EMPENNAGE 



 1. Gaggage compartment door... CHECK (lock with key) 


  2. Rudder Gust lock............. REMOVE.       (if installed) 


    3. Tail Tie-down............ DISCONNECT          


4. Control surfaces............... CHECK.   freedom of movement and security. 




5. Trim tabs ..........CHECK (security) 


6. Antennas...... CHECK (security of attachment and general) 





3. RIGHT WING TRAILING EDGE 




1. Flap.... CHECK.(security and condition)







2. Aileron......... CHECK (freedom of movement and security) 




4. RIGHT WING 




1. Landing / taxi lights............. CHECK  (Condition and cleanliness of cover)  
(if installed) 






2. Wing tie-down............ DISCONNECT 






3. Fuel tank vent opening........... CHECK  (verify opening is clear) 






4. Main wheel tire....... CHECK (proper inflation and general condition) (weather checks tread depth and wear. etc)) 







5. Fuel tank sump Quick drain valve..... DRAIN 
Drain at least a cupful of fuel (using sampler cup) from each sump location a check for water. Sediment and proper fuel grade before each flight and after each refueling. If water is observed. Take further sampling until clear and then gently rock wings and lower tail to the ground to move any additional contaminants to the sampling points. Take repeated samples from all fuel drain points until all contamination has been removed. If contaminants are still present, refer warning below and do not fly airplane. 


NOTE 
collect all sampled fuel in a safe container. Dispose the sampled fuel so that it does not cause a nuisance. Hazard or damage to the environment 


WARNING 
if. After Repeated Sampling. Evidence of contamination still exists. The airplane should not be flown. Tanks should be drained and system purged by Qualified Maintenance personnel. All Evidence of contamination must be Removed before further flight. 


5. NOSE 




1. Static source opening (right side fuselage)  CHECK
 (verify opening is clear) 







2. Fuel strainer Quick Drain valve
 (located on lower right side of engine cowling..... DRAIN. drain at least a cupful of fuel. (using sampler cup) from valve to check for water sediment and proper fuel grade before each flight and after each refueling. If water is observed. Take further samples until clear and then gently rock wings and lower tail to the ground to move any additional contaminants to the sampling points. Take repeated samples from all fuel drain points. Including the fuel return line and fuel selector. Until all contamination has been removed. If contaminants are still present. Refer to warning below and do not fly airplane. 


WARNING 
If.  after Repeated sampling Evidence of contamination still exists. The airplane should not be flown. Tanks should be drained and system purged by Qualified Maintenance personnel. All Evidence of contamination must be Removed before further flight 





3. Engine cooling air inlets....... CHECK 
(clear of obstructions)








4. Propeller and spinner.... CHECK 
(for Nicks. security and no red oil leaks)



NOTE 
Minor leaking of the blade seal area is possible on new propellers as the seals water in any initial leakage will be visible as minor streaking on the blade or blades clean off oil residue and cycle propeller at least 5 times leaking should be reduced  or completely stopped. If minor leaking continues after 20 hours of operation or increases Remove propeller and have repaired 




5. Air filter.......... CHECK. (for restrictions by dust or other foreign matter) 







6. Nose wheel strut and tire...... CHECK 
(proper inflation of strut and general condition of tire (weather checks. Tread depth and wear.etc))









7. Engine oil Dipstick / filler cap :

a. Oil level.... CHECK 


b.  Dipstick / filler cap... SECURE 


NOTE 
Do not operate with less than 4 quarts fill to quarts for extended flight. 





8. Static source opening (left side of fuselage) CHECK (verify opening is clear) 





6. LEFT WING 




1. Fuel Quantity............. CHECK
 (for desired level) 







2. Fuel filler cap....... SECURE and vent clear 






3. Fuel tank sump Quick drain valves ..........DRAIN 
drain at least a cupful of fuel. (using sampler cup) from each sump location to check for water sediment,  and proper fuel grade before each flight and after each refueling. If water is observed. Take further samples until clear and then gently rock wings and lower tail to the ground to move any additional contaminants to the sampling points. Take repeated samples from all fuel drain points until all contamination has been removed. If contaminants are still present, refer to warning below and do not fly airplane. 








4. Main wheel tire.... CHECK. Proper inflation and general condition (weather checks, tread depth and wear, etc)) 






7. LEFT WING LEADING EDGE 




1. Fuel Tank vent Opening..... CHECK
(blockage) 






2. Stall warning Vane...... CHECK 
(Freedom of movement) 





3. Wing Tie-down...........DISCONNECT 








4. Landing / Taxi lights ......CHECK 
(Condition and cleanliness of cover) 







8. LEFT WING TRAILING EDGE 




1. Aileron.... CHECK (freedom of movement and security) 








2. Flap... CHECK (security and condition)

CLICK 👉 CESSNA 182T HANDBOOK 

CLICK 👉 PREFLIGHT INSPECTION

CLICK 👉 STARTING ENGINE WITH BATTERY

CLICK 👉 STARTING ENGINE WITH (EXTERNAL POWER)

CLICK 👉 TAXIING

CLICK 👉 BEFORE TAKEOFF

CLICK 👉 NORMAL TAKEOFF

CLICK 👉 SHORT FIELD TAKEOFF

CLICK 👉 ENROUTE CLIMB

CLICK 👉 MAXIMUM PERFORMANCE CLIMB

CLICK 👉 CRUISE

CLICK 👉 DESCENT

CLICK 👉 BEFORE LANDING

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CLICK 👉 BALKED LANDING

CLICK 👉 AFTER LANDING

CLICK 👉 SECURING AIRPLANE

CLICK 👉 FUEL CAPACITY

CLICK 👉 OIL CAPACITY

CLICK 👉 CENTER OF GRAVITY LIMITS

CLICK 👉 MANEUVER LIMITS

CLICK 👉 FLIGHT LOAD FACTOR LIMITS

CLICK 👉 KINDS OF OPERATIONS LIMITS

CLICK 👉 AUX AUDIO SYSTEM

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CLICK 👉 CABIN FIRE

CLICK 👉 WING FIRE

CLICK 👉 INADVERTENT ICING ENCOUNTER DURING FLIGHT

CLICK 👉 EXCESSIVE FUEL VAPOR FUEL FLOW STABILIZATION PROCEDURES

CLICK 👉 LANDING WITH A FLAT MAIN TIRE

CLICK 👉 LANDING WITH A FLAT NOSE TIRE

CLICK 👉 LOW VOLTS ANNUNCIATOR COMES ON BELOW 1000 RPM

CLICK 👉 AIR DATA SYSTEM FAILURE RED X - PFD AIRSPEED INDICATOR

CLICK 👉 RED X - PFD ALTITUDE INDICATOR

CLICK 👉 RED X - HORIZONTAL SITUATION INDICATOR (HSI)

CLICK 👉 AUTOPILOT OR ELECTRIC TRIM FAILURE

CLICK 👉 LOW VACUUM ANNUNCIATOR COMES ON

CLICK 👉 HIGH CARBON MONOXIDE (CO) LEVEL ADVISORY

CLICK 👉 LANDING WITHOUT ELEVATOR CONTROL

CLICK 👉 EMERGENCY OPERATION IN CLOUDS

CLICK 👉 EXECUTING A 180° TURN IN CLOUDS (AHRS FAILED)

CLICK 👉 EMERGENCY DESCENT THROUGH CLOUDS (AHRS

CLICK 👉 RECOVERY FROM SPIRAL DIVE IN THE CLOUDS (AHRS FAILED)

CLICK 👉 INADVERTENT FLIGHT INTO ICING CONDITIONS

CLICK 👉 STATIC SOURCE BLOCKED

CLICK 👉 SPINS

CLICK 👉 SPARK PLUG FOULING

CLICK 👉 MAGNETO MALFUNCTION

CLICK 👉 ENGINE-DRIVEN FUEL PUMP FAILURE

CLICK 👉 EXCESSIVE FUEL VAPOR

CLICK 👉 LOW OIL PRESSURE

CLICK 👉 ELECTRICAL POWER SUPPLY SYSTEM MALFUNCTIONS

CLICK 👉 EXCESSIVE RATE OF CHARGE

CLICK 👉 WINDSHIELD DAMAGE

CLICK 👉 AIRFRAME

CLICK 👉 FLIGHT CONTROLS

CLICK 👉 TRIM SYSTEMS

CLICK 👉 PILOT PANEL LAYOUT

CLICK 👉 CENTER PANEL LAYOUT

CLICK 👉 RIGHT PANEL LAYOUT

CLICK 👉 CENTER PEDESTAL LAYOUT

CLICK 👉 ATTITUDE INDICATOR

CLICK 👉 AIRSPEED INDICATOR

CLICK 👉 ALTIMETER

CLICK 👉 HORIZONTAL SITUATION INDICATOR

CLICK 👉 VERTICAL SPEED INDICATOR

CLICK 👉 GROUND CONTROL

CLICK 👉 WING FLAP SYSTEM

CLICK 👉 LANDING GEAR SYSTEM

CLICK 👉 BAGGAGE COMPARTMENT

CLICK 👉 SEATS

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CLICK 👉 CONTROL LOCKS

CLICK 👉 ENGINE INSTRUMENTS

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CLICK 👉 FUEL INJECTION SYSTEM

CLICK 👉 COOLING SYSTEM

CLICK 👉 FUEL DISTRIBUTION

CLICK 👉 AUXILIARY FUEL PUMP OPERATION

CLICK 👉 FUEL RETURN SYSTEM

CLICK 👉 FUEL VENTING

CLICK 👉 REDUCED TANK CAPACITY

CLICK 👉 FUEL SELECTOR VALVE

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CLICK 👉 BRAKE SYSTEM

CLICK 👉 MASTER SWITCH

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CLICK 👉 VACUUM SYSTEM AND INSTRUMENTS

CLICK 👉 ATTITUDE INDICATOR

CLICK 👉 VACUUM INDICATOR

CLICK 👉 CLOCK/O.A.T. INDICATOR

CLICK 👉 STALL WARNING SYSTEM

CLICK 👉 STANDARD AVIONICS

CLICK 👉 GARMIN DISPLAY UNITS (GDU)

CLICK 👉 AUDIO PANEL (GMA)

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CLICK 👉 ATTITUDE AND HEADING REFERENCE SYSTEM (AHRS) AND MAGNETOMETER (GRS)

CLICK 👉 AIR DATA COMPUTER (GDC)

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CLICK 👉 XM WEATHER AND RADIO DATA LINK (GDL)

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CLICK 👉 BENDIX/KING KTA 870 TRAFFIC ADVISORY/MULTI HAZARD AWARENESS SYSTEM

CLICK 👉 AVIONICS SUPPORT EQUIPMENT

CLICK 👉 AVIONICS COOLING FANS

CLICK 👉 ANTENNAS

CLICK 👉 STATIC DISCHARGERS

CLICK 👉 CARBON MONOXIDE DETECTION SYSTEM

CLICK 👉 IDENTIFICATION PLATE

CLICK 👉 AIRPLANE FILE

CLICK 👉 CESSNA INSPECTION PROGRAMS

CLICK 👉 CESSNA CUSTOMER CARE PROGRAM

CLICK 👉 PILOT CONDUCTED PREVENTIVE MAINTENANCE

CLICK 👉 ALTERATIONS OR REPAIRS

CLICK 👉 GROUND HANDLING TOWING

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