storage.googleapis.com · Web viewObtain Weather Brief Taxi route Abort plan: On Runway Below 1000 feet Above 1000 feet Account for all W eather,W&B, and performance considerations

Piper Archer II PA-28-180 (P28A)Preflight Inspection:

1. Master ONCheck Fuel quantityLights CheckMaster OffFlaps down

2. Control surfaces check3. Wingtip & Nav lights

check4. Fuel vents check

Sump tanksFuel level CheckTire & Brake condition check

6.Empennage check

|Passenger Briefing| No Smoking including E-cigs How to use Seatbelts How to operate door Egress plan Location of Survival Equipment Ditching procedures

Ayers version 1.3-A 1 | P a g e

Piper Archer II PA-28-180 (P28A)

Strut Inflation5. Oil & Engine check

Prop and Spinner check

Aircraft Information:Empty Weight 1,593 lbs.

Max Useful Load 957 lbs.

Max Takeoff weight – 2550 lbs.

Fuel Types – 100LL (Blue)Useable Fuel – 48 Gallons

Oil Capacity – 5.5qt min | 8 maxElectrical – 12 volt | 60 ampTire Pressure – 24 PSI

Vr – Rotation speed – 45-55 kphVx – Best Angle Climb – 64 kphVy – Best Rate Climb – 76 kphVa – Maneuvering speed – 89-113 kphVg – Best Glide speed – 76 kph Vfe – Flaps Extended – 102 kphVno – Max Cruise – 125 kphVne – Never Exceed – 154 kphVs – Stall Clean – 50 kphVso – Stall dirty – 44 kph

Landing speeds Local frequenciesDownwind – 85 kph KSFZ CTAF – 123.075Base – 75 kph KSFZ Wx – 120.025


Piper Archer II PA-28-180 (P28A)Final – 65 kph PVD Appr – 123.675Max crosswinds – 17 kts


Piper Archer II PA-28-180 (P28A)Engine Start: Seatbelts ON Brakes – SET Master Switch ON Beacon Light ON Prime As Required for Wx / Eng cond. Propeller area CLEAR Mixture Rich Throttle Cracked Fuel Pump ON Throttle to 1000RPM Start Fuel Pump OFF Lean engine Oil Pressure Green in 30sec Avionics ON

Before Taxi:

Brake Check Oil temp – Green before taxi Obtain Weather Brief Taxi route

Abort plan : 1. On Runway2. Below 1000 feet3. Above 1000 feet

Account for all Weather,W&B, and performance

Engine Run up: Flight Control Check Fuel pump ON Fuel Tank Switch Fuel pump OFF Power 1700RPM Magneto Check (1750RPM Max drop|50RPM Max Diff)Carb Heat – ONEngine Instruments – GreenSuction – 4 to 6

Idle Power Check Carb Heat – OFF Power – 1000RPM Annuciator panel check

Before Takeoff Check: Flaps Set Door closed & latched Magnetos on BOTH Landing Light ON Fuel Pump ON Primer in and locked Flight Instruments Set Transponder on ALT Radios Set Trim Set

Brief Abort plan



considerations for your flight.Climb Check:

Mixture Full Rich Power Full Climb at Vy

Cruise Check:

Pitch for level flight Build speed to cruise Set power per chart Trim airplane Fuel Pump – OFF Lean mixture to 100f Power as required – normal 75% (see chart above window shade)

Descent Check:

Mixture Full Rich Fuel Pump – ON Fuel Tank – Fullest Lights – ON

Determine descent type

Cruise DescentAirspeed 122 kph, power 2500RPM Steep Descent

After Landing:

Clear all Runways & Stop Flaps UP Lights as required Fuel Pump OFF Trim SET Taxi plan – confirm

Shutdown & Securing: Avionics OFF Lights OFF except Beacon Fuel Pump OFF Shut off ventilation system Mixture Idle cutoff|Propeller Stops| Master Switch OFF HOBBS and Tach recorded Close all window and floor vents Magnetos OFF & Key OUT

|Aircraft| Cowl plugs IN Covers ON Chocks & Tie downs Secure


Piper Archer II PA-28-180 (P28A)Airspeed 100 kph, power 1500RPM

Emergency Procedures:

Power loss in flight: A (Airspeed) 76kph B (Best place to land) C (Checklist to Restart / Secure)

|Restart| Mixture RICH Power FULL Carb Heat ON Magnetos BOTH Fuel Pump ON Fuel Selector SWITCH

|No Windmill| Starter Engage

|No Restart| Squawk 7700 Transmit Mayday on 121.5 Fuel Selector OFF Fuel Pump OFF Carb Heat OFF

Spin Recovery:P (Power to Idle)A (Ailerons to Neutral)R (Rudder to Break Spin)E (Elevator to Break Stall) |Normal Stall Recovery|

Fire in flight: Power to Idle Mixture Idle cut-off Fuel selector off Cabin vents closed Window Open Door unlatched 30-45* bank Accelerate to over 100mph to extinguish engine fire Select suitable landing point Land as safely as possible Exit aircraft

Loss of oil pressure or high temp Land as soon as possible Prepare for power off landing


Piper Archer II PA-28-180 (P28A) Throttle IDLE Mixture IDLE CUTOFF Door OPEN 500AGL MASTER OFF

|Commit to Landing|

Loss of Voltage Check annunciator light If zero; alt switch off Reduce electrical load Check circuit breakers Alt switch ON

- If power not restored, ALT

- Land as soon as possible

- Battery is only source of power

- Assume power failure

Excess Voltage: Alt Switch - OFF Battery switch – ON

Or ON only as required Reduce electrical load Land as soon as possible:

- Battery is only source of power

- Assume power failure

Winter operationsBelow 50 F, winter plate to be installed

Below 32 either: Preheat engine for 25

minutes with propane heater

Preheat engine for 4



hours with plug in heater

Hangar the plane overnight

Prime 5 timesEngage engine at lowest

possible RPM; slowly increase idle to 1000 RPM

No flying when colder than 15


Piper Archer II PA-28-180 (P28A)Aircraft Performance Chart

Leaning procedure: Above 5,000 ft and PD below 5,000 ft

Lean slowly until RPMs begin to drop or engine runs rough

Adjust mixture to restore full power



Adjust red dial on EGT to mark temperature Adjust mixture to 100 cooler below the red dial







Weight & BalanceLocation Weight Arm MomentEmpty Weight

1593 87.5

Pilot & F-Pax

80.5

Rear Seat 118.1

Baggage 142.8

Fuel 95.0

CG = TM/TW




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storage.googleapis.com · Web viewObtain Weather Brief Taxi route Abort plan: On Runway Below 1000 feet Above 1000 feet Account for all W eather,W&B, and performance considerations