Ground Check Piper Archer III PA-28-181 step by step,

 

WELCOME ADVANCE FLYING ACADEMY 

Ground Check Piper Archer III PA-28-181 step by step,

GROUND CHECK

Parking brake ......................................set

Throttle ...................................2000 RPM

Magnetos ..............max. drop 175 RPM 

max. diff. 50 RPM


Vacuum .........................4.8 to 5.2 in. Hg.

Oil temperature .............................check

Oil pressure....................................check

Air conditioner (if installed) ........check

Ammeter .........................................check

Annunciator panel...............press-to-test

Carburetor heat........approx. 75 RPM drop

 Engine is warm for takeoff when throttle can be opened without engine faltering.

Electric fuel pump................................OFF

Fuel pressure.........................................check

Throttle ...............................................retard


GROUND CHECK

Set the parking brake.

The magnetos should be checked at 2000 RPM. Drop off on either magneto should not exceed 175 RPM and the difference between the magnetos should not exceed 50 RPM. Operation on one magneto should not exceed 10 seconds.

Check the vacuum gauge; the indicator should read 4.8" to 5.2" Hg at 2000 RPM.

Check the annunciator panel lights with the press-to-test button. Also check the air conditioner. Carburetor heat should also be checked prior to takeff to be sure the control is operating properly and to clear any ice which may have formed during taxiing. Avoid prolonged ground operation with carburetor heat ``ON’’ as the air is unfiltered. Engine RPM should decrease no more than 75 RPM when carburator heat is on. If no or excessive RPM decrease is observed, investigate and have the cause corrected prior to flight.

The electric fuel pump should be turned OFF after starting or during warm-up to make sure that the engine driven pump is operating. Prior to takeoff the electric pump should be turned ON again to prevent loss of power during takeoff should the engine driven pump fail. 

👉 PIPER ARCHER III PA 28-181 HANDBOOK

👉 PREFLIGHT INSPECTION 

👉 MISCELLANEOUS

👉 BEFORE STARTING ENGINE

👉 NORMAL START - COLD ENGINE

👉 NORMAL START - HOT ENGINE

👉 ENGINE START WHEN FLOODED

👉 STARTING WITH EXTERNAL POWER

👉 WARM-UP

👉 TAXIING

👉 GROUND CHECK

👉 BEFORE TAKEOFF

👉 TAKEOFF

👉 SHORT FIELD, OBSTACLE CLEARANCE

👉 CLIMB

👉 CRUISING

👉 DESCENT

👉 APPROACH AND LANDING

👉 STOPPING ENGINE

👉 MOORING

👉 ENGINE

👉 PROPELLERS

👉 FUEL & OIL CAPACITY

👉 MAXIMUM WEIGHTS

👉 BAGGAGE SPACE

👉 POWER PLANT LIMITATIONS

👉 POWER PLANT INSTRUMENT MARKINGS

👉 WEIGHT LIMITS

👉 TYPES OF OPERATION

👉 AIRSPEEDS FOR SAFE OPERATION

👉 ENGINE FIRE DURING START

👉 ENGINE POWER LOSS IN FLIGHT

👉 POWER OFF LANDING

👉 FIRE IN FLIGHT

👉 LOSS OF OIL PRESSURE

👉 LOSS OF FUEL PRESSURE

👉 HIGH OIL TEMPERATURE

👉 SPIN RECOVERY

👉 CARBURETOR ICING

👉 AIRFRAME

👉 LANDING GEAR

👉 FLIGHT CONTROLS

👉 ENGINE CONTROLS

👉 ELECTRICAL SYSTEM

👉 VACUUM SYSTEM

👉 PITOT-STATIC SYSTEM

👉 STALL WARNING

👉 ENGINE AIR FILTER

👉 BRAKE SERVICE

👉 TIRE INFLATION

👉 BATTERY SERVICE

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