14
Piper Dakota (PA-28-236) Property of the Flying 20 Club, Inc. – v.20180610 1. Oil ………………………………............. 9-10 qts (12 max) Cap Secure CABIN 1. POH & Documents …………………….. Check Available 2. Magneto Switch ……………………….. OFF 3. Pitot/Static Drains ……………………. Push to Drain 4. Avionics/Electrical Switches …………... OFF 5. Master Switch …………………………. ON 6. Fuel Quantity …………………………... Check Quantity 7. Pitot Heat / Lights ……………………... On to Check 8. Stall Warning Horn …………………….. Verify Operation 9. Pitot Heat / Lights ……………………... Off 10. Annunciator Panel ……………………... Press to Test 11. Master Switch …………………………. OFF 12. Flaps ……………………………………. Down WALKAROUND Right Wing 1. Flap & Aileron ………………………… Check Skin & Hinges 2. Wing Surfaces ………………...………. No Contamination 3. Wing Tie Down / Chock ..……………… REMOVED 4. AoA Probe …………………………….. Holes Clear 5. Right Wing Fuel Vent ………………… Unobstructed 6. Right Wing Fuel Drain ………………... Check Sample 7. Right Wing Fuel Quantity …………..... Visually Verify 8. Main Gear Strut …………………......... 4.25”-4.75” 9. Tire & Brakes …………………............. 35-40 psi Nose 1. Cowling ……………………………….. Secure 2. Prop & Spinner ……………………….. Check 3. Alternator Belt ………………………... Check 4. Cooling Inlet ………………………….. Unobstructed 5. Air Inlet ……………………………….. Unobstructed 6. Nose Wheel Strut …………….............. 3.0”-3.5” 7. Nose Wheel Tire ……………................ 29-33 psi 8. Nose Wheel Chock ………………….… REMOVED

Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

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Page 1: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

1. Oil ………………………………............. 9-10 qts (12 max) Cap Secure

CABIN

1. POH & Documents …………………….. Check Available 2. Magneto Switch ……………………….. OFF 3. Pitot/Static Drains ……………………. Push to Drain 4. Avionics/Electrical Switches …………... OFF 5. Master Switch …………………………. ON 6. Fuel Quantity …………………………... Check Quantity

7. Pitot Heat / Lights ……………………... On to Check 8. Stall Warning Horn …………………….. Verify Operation 9. Pitot Heat / Lights ……………………... Off

10. Annunciator Panel ……………………... Press to Test 11. Master Switch …………………………. OFF 12. Flaps ……………………………………. Down

WALKAROUND

Right Wing

1. Flap & Aileron ………………………… Check Skin & Hinges 2. Wing Surfaces ………………...………. No Contamination 3. Wing Tie Down / Chock ..……………… REMOVED 4. AoA Probe …………………………….. Holes Clear 5. Right Wing Fuel Vent ………………… Unobstructed 6. Right Wing Fuel Drain ………………... Check Sample 7. Right Wing Fuel Quantity …………..... Visually Verify 8. Main Gear Strut …………………......... 4.25”-4.75” 9. Tire & Brakes …………………............. 35-40 psi

Nose

1. Cowling ……………………………….. Secure 2. Prop & Spinner ……………………….. Check 3. Alternator Belt ………………………... Check 4. Cooling Inlet ………………………….. Unobstructed 5. Air Inlet ……………………………….. Unobstructed 6. Nose Wheel Strut …………….............. 3.0”-3.5” 7. Nose Wheel Tire ……………................ 29-33 psi 8. Nose Wheel Chock ………………….… REMOVED

Page 2: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

9. Main Fuel Strainer ...…………………. Check Sample (L & R)

Left Wing

1. Wing Surfaces ………………...………. No Contamination 2. Main Gear Strut …………………......... 4.25”-4.75” 3. Tire & Brakes …………………............. 35-40 psi 4. Wing Tie Down / Chock ……………….. REMOVED 5. Left Wing Fuel Vent ………………...… Unobstructed 6. Left Wing Fuel Drain ………………….. Check Sample 7. Left Wing Fuel Quantity ……………... Visually Verify 8. Pitot/Static Mast ……………………… Holes Clear 9. Flap & Aileron ………………………… Check Skin & Hinges

Fuselage

1. Empennage …………………………… No Contamination 2. Left Static Port ……………………….. Holes Clear 3. Tail Tie Down …………………………. DISCONNECT 4. Rudder & Stabilator ………………….. Check 5. Right Static Port ……………………… Holes Clear 6. Baggage Door ………………………… Closed & Locked

PRE-ENGINE START 1. Flaps …………………………………... Up 2. Brakes ……………………………….... Parking Brake Set 3. Seats & Belts ………………………….. Adjusted & Secure 4. PASSENGER BRIEFING

➢ No Smoking ➢ Turn cell phones OFF or activate “airplane” mode ➢ Seatbelts must be worn during taxi, takeoff, & landing ➢ Door operation ➢ Sterile cockpit during taxi, takeoff, and landing ➢ Fire extinguisher location ➢ Help point out other air traffic

5. Circuit Breakers ………………………. Check In 6. Avionics/Electrical Switches …………. OFF 7. Carb Heat ……………………………… OFF 8. Fuel Selector ………………………….. LOWEST/RIGHT Tank 9. Hobbs & Tachometer ………………… Record

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Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

ENGINE START 1. Throttle ………………………………… Open (1/4” cold, ½” hot) 2. Propeller ……………………………… Full FORWARD 3. Mixture ………………………………… RICH 4. Master & Alternator Switches ………… ON 5. Primer ………………………………….. 4-6 shots 6. Beacon Light (and Nav if night) ………. On 7. Fuel Pump ……………………………… ON 8. Prop Area ……………………………… CLEAR

9. Starter ....……………………………….. Engage

10. Throttle ………………………………… 800-1200 RPM 11. Oil Pressure …………………………….. IN THE GREEN 12. Fuel Selector …………………………… FULLEST/LEFT Tank 13. Fuel Pump ……………………………… Off 14. Mixture ………………………………… LEANED

PRE-TAXI 1. Fuel Quantity …………………………. Verify 2. Radios ………………………………… Set 3. Transponder ………………………….. Code & Mode Set 4. Nav/GPS ……………………………..... Programmed & Set

5. Elevator Trim …………………………. Set to Neutral 6. Flight Controls ...………………….…... Free and Correct

ENGINE RUNUP 1. Brakes ………………………………… Parking Brake Set 2. Seats & Belts ………………………….. Check 3. Doors ………………………………….. Closed & Latched 4. FLIGHT INSTRUMENTS

a. A.H. …………………………… Level b. Altimeter ……………………... Baro Set & +/- 75 feet c. VSI ……………………………. Check Zero d. Heading ………………………. Aligned & Set e. Turn & Bank ………………….. No Flags

5. Primer ……………………………...…. IN & LOCKED

Page 4: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

6. Mixture …..…………………………… Rich 7. Throttle ……………………………….. 2000 RPM

a. Magnetos …………………….. < 175 RPM Drop, < 50 RPM Difference

b. Suction Gauge ……………….. 4.9” – 5.1” c. Ammeter ……………………... Check w/ Load d. Propeller ……………………... Exercise then Full RPM

e. Carb Heat …………………….. On w/ RPM Drop f. Throttle ………………………. Idle g. Carb Heat …………………….. Off w/ RPM Rise

8. Throttle ……………………………….. 1000 RPM

9. Emergency Procedures …………...…. Reviewed 10. Departure Briefing …………………... Completed

Check THAT Setup (Transponder, Heading, Altimeter, Talk)

TAKEOFF 1. Landing Light ……………………….... On [Lights] 2. Transponder ………………………….. ALT [Camera] 3. Fuel Pump …………………………….. ON

[Action] 4. Timer …………………………...…….. Start

NORMAL:

1. Flaps ……………………………...…... Up (0) 2. Throttle …………………………...….. Full Open 3. Engine Instruments ……………….….. All In The Green 4. Rotate ………………………………… 60-65 Kts

SHORT FIELD, OBSTACLE CLEARANCE:

1. Flaps ………………………………….. 25-degrees (2) 2. Brakes ………………………………… HOLD until full power

3. Throttle …………………..................... Full Open 4. Engine Instruments……....................... All In The Green

5. Brakes ………………………………… RELEASE 6. Rotate …………………....................... 50-60 Kts, accel to 73 7. Flaps ……………………...................... Retract After 85 Kts

• Climb Speed ………………………….. Vy (85 Kts)

Page 5: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

ENROUTE CLIMB 1. Airspeed ………………………………. 100 KIAS 2. Throttle ……………………………….. Wide Open 3. Propeller ……………………………… Full Forward

4. Fuel Pump ………………..……..…….. Off, +1000’ AGL 5. Landing Light …………………………. Off, +3000’ AGL

6. Mixture ……………………………….. LEAN, +5000’ MSL

CRUISE 1. Power …………………………………. 75% or less 2. Propeller ……………………………… Adjust 3. Mixture ……………………………….. LEAN as necessary 4. Trim …………………………………… Adjust

PRE-LANDING (~12 nm / IAF) 1. ATIS & Altimeter …………..… Current & Set [WIR] 2. Landing Light ……………..…. On

[E] 3. Seats & Belts ………………..... Check

4. Fuel Selector ……….……..…. BEST TANK 5. Approach Procedures .….….... REVIEWED

Page 6: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

LANDING (pattern / FAF) 1. Fuel Pump …………………………….. ON [G] 2. Mixture ……………………………….. Rich [M] 3. Propeller ……………………………… Full RPM [P]

PATTERN:

1. Downwind ……………………………. 95 Kts (Flaps 10) 2. Base …………………………………… 80 Kts (Flaps 25) 3. Final …………………………………… 72 Kts (Flaps 40)

SHORT FIELD (AFTER TOUCHDOWN):

4. Brakes ………………………………… MAX AS NEEDED 5. Flaps …………………………………... RETRACT 6. Control Yoke ………………………….. FULL AFT

AFTER LANDING 1. Fuel Pump …………………………….. OFF 2. Landing Light …………………………. Off 3. Carb Heat ……………………………... OFF 4. Flaps …………………………………... Retract 5. Elevator Trim …………………………. SET TO NEUTRAL

SHUTDOWN 1. Brakes ………………………………… Set 2. Throttle ……………………………….. IDLE 3. Avionics/Electrical Switches

a. Avionics ………………………. OFF b. Beacon/Nav Lights …………... On until prop stops

4. Mixture ……………………………….. Idle Cutoff

5. Beacon Light ………………………….. OFF 6. Ignition Switch ………………………... OFF 7. Master & Alternator Switches ……….. OFF

8. Flight Plan …………………………….. CLOSE

Page 7: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

COMMUNICATION

DXR ATIS 127.75 NY Approach 126.40

DXR Ground 121.60 Flight Services 122.20

DXR Tower 119.40

Air-to-air 122.75

V-SPEEDS

Vfe 102 KIAS Vx 73 KIAS Vno 137 KIAS Vy 85 KIAS Vne 173 KIAS

Va – 3000 lbs 124 KIAS Vs 65 KIAS Va – 1761 lbs 96 KIAS Vs0 56 KIAS

Max Demonstrated Crosswind – 17 KIAS

Vg – 85 KIAS

ALTITUDE LIMITS

Service Ceiling 17,500

Absolute Ceiling 19,700

• Full Throttle

• Mixture 125F ROP

• Flaps Up

• 75 KIAS

• 3000 lbs Gross Weight

Departure Briefing Items

o Takeoff Abort Point ……….. 60 Kts before 50% takeoff roll o Safety Altitude …………….. At least 1000’ AGL o Initial Departure Heading …. Review o Initial Departure Altitude ….. Review

Page 8: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

Lyco

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Page 9: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

ENGINE FAILURE

TAKEOFF RUN

1. Throttle ………………………………… IDLE 2. Brakes ………………………………….. Apply As Needed

If Insufficient Runway Remaining 3. Mixture ………………………………… IDLE CUTOFF 4. Master Switch …………………………. OFF 5. Magnetos ……..……………………….. OFF 6. Fuel Selector …………………………… OFF

IMMEDIATELY AFTER TAKEOFF

1. Airspeed ……………………………….. >85 KIAS 2. Mixture ………………………………… IDLE CUTOFF 3. Master Switch …………………………. OFF 4. Magnetos ……..………………………. OFF 5. Fuel Selector …………………………… OFF 6. Flaps ……………………………………. As Required 7. Cabin Door ……………………………... Unlatch 8. Land ……………………………………. Straight Ahead

DURING FLIGHT (Restart Procedures)

1. Airspeed ……………………………….. 85 KIAS 2. Mixture ………………………………… RICH

[F] 3. Fuel Pump ……………………………… ON 4. Fuel Selector …………………………... SWITCH TANKS 5. Carb Heat ………………………………. ON [A] 6. Ignition Switch ……………………….. Left, Right [S]

ENGINE PROBLEMS

LOSS OF FUEL PRESSURE

1. Fuel Pump ……………………………… ON 2. Fuel Selector …………………………... Check On Fullest Tank

LOW OIL PRESSURE / HIGH OIL TEMPERATURE

• LAND AS SOON AS PRACTICAL

Page 10: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

HIGH (>430F) CHT

1. Mixture ………………………………… RICH 2. Airspeed ………………………………... 100+ KIAS 3. Throttle ………………………………… Reduce Power

ENGINE ROUGHNESS

1. Carb Heat ………………………………. FULL ON If roughness continues after 1-2 minutes

2. Fuel Pump ……………………………… On [F] 3. Mixture ………………………………… Adjust

4. Fuel Selector …………………………… Switch Tanks 5. Carb Heat ………………………………. OFF [A] 6. Ignition Switch ……………………….. Left, Right [S]

FIRES

DURING START ON GROUND

1. Starter ………………………………….. CONTINUE CRANKING

2. Mixture ………………………………… IDLE CUTOFF 3. Throttle ………………………………… Full Open 4. Fuel Pump ……………………………… OFF 5. Fuel Selector ……………………...…… OFF 6. Engine ……………………………...…... Secure

a. Avionics/Electrical Systems …... Off 7. Fire ……………………………………... Extinguish

DURING FLIGHT (ENGINE)

1. Mixture ………………………………… IDLE CUTOFF 2. Fuel Pump ……………………………… OFF 3. Fuel Selector ...………………………… OFF 4. Heater & Defroster ……………………. OFF

LAND AS SOON AS POSSIBLE

Page 11: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

DURING FLIGHT (ELECTRICAL)

1. Master & Alternator Switches ...…….… OFF 2. Vents, Cabin Air, Heat …………………. CLOSED 3. Fire Extinguisher ………………………. ACTIVATE 4. Avionics/Electrical Switches …………... Off

If fire appears out & electrical equipment is necessary 5. Master Switch …………………………. On 6. Circuit Breakers ………………………... Check, Don’t Reset 7. Avionics / Electrical Switches ………….. On, one at a time

ELECTRICAL PROBLEMS

ALTERNATOR FAILURE

1. Alternator Switch ……………………… Off 2. Alternator Circuit Breakers ……………. Check 3. Alternator Switch ……………………… On

If alternator still inoperative Follow ELECTRICAL OVERLOAD Checklist Below

ELECTRICAL OVERLOAD

1. Electrical Load …………………………. Reduce If loads are not reduced

2. Alternator ……………………………… Off 3. Flight …………………………………… Terminate ASAP

MISCELLANEOUS

CO ALERT

1. Cabin Heater/Defroster ……………….. OFF 2. Storm Window ………………………… OPEN 3. Cabin Vents …………………………….. OPEN

Land as soon as practical

Page 12: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

OPEN DOOR

1. Airspeed ………………………………... Slow to 83 KIAS 2. Cabin Vents …………………………….. Open 3. Storm Window ………………………… Open

• Upper latch open o Latch

• Side latch open

o Pull on armrest & move handle to latched position

• Both latches open o Latch side latch, then top latch

PROPELLER OVERSPEED

1. Throttle ………………………………… Reduce < 2400 RPM 2. Oil Pressure …………………………..… Check 3. Propeller ……………………………….. FULL DECREASE

FORCED LANDINGS

WITHOUT POWER

1. Airspeed ……………………………...… 85 KIAS 2. Seats, Belts, Harnesses ………………... SECURE

3. Mixture ………………………………… IDLE CUTOFF 4. Master Switch …………………………. OFF 5. Magnetos ……..……………………….. OFF 6. Fuel Selector …………………………… OFF 7. Flaps ……………………………………. As Required

If time permits a. Transponder …………………... 7700 b. Radio ………………………….. MAYDAY (121.5)

Prior to touchdown 8. Doors …………………………………... UNLATCH

Page 13: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

PRECAUTIONARY WITH POWER

1. Airspeed ……………………………...… 85 KIAS 2. Seats, Belts, Harnesses ………………... SECURE

3. Landing Site ……………………………. Overfly, noting conditions

If time permits a. Transponder …………………... 7700 b. Radio ………………………….. MAYDAY (121.5)

4. Mixture ………………………………… IDLE CUTOFF 5. Master Switch …………………………. OFF 6. Magnetos ……..……………………….. OFF 7. Fuel Selector …………………………… OFF 8. Flaps ……………………………………. As Required

Prior to touchdown 9. Doors …………………………………... UNLATCH

DITCHING

1. Airspeed ……………………………...… 85 KIAS 2. Seats, Belts, Harnesses ………………... SECURE 3. Heavy Objects …………………………. Secure or Jettison

4. Mixture ………………………………… IDLE CUTOFF 5. Master Switch …………………………. OFF 6. Magnetos ……..……………………….. OFF 7. Fuel Selector …………………………… OFF 8. Flaps ……………………………………. As Required

If time permits a. Transponder …………………... 7700 b. Radio ………………………….. MAYDAY (121.5)

9. Approach a. High Winds, Heavy Seas ……… Land Into Wind b. Light Winds, Heavy Swells ……. Parallel to Swells

Prior to touchdown 10. Doors …………………………………... UNLATCH

Page 14: Piper Dakota (PA-28-236) - Flying 20 Club - Home · Piper Dakota (PA-28-236) ... Fuel Pump …………………………… ... Check THAT Setup (Transponder, Heading, Altimeter,

Piper Dakota (PA-28-236)

Property of the Flying 20 Club, Inc. – v.20180610

MAXIMUM GLIDE ALTITUDE (AGL) GLIDE DISTANCE

1000 1.2 nm Vg – 85 KIAS 2000 2.4 nm

3000 3.6 nm Propeller Wind-milling 4000 4.8 nm

5000 6.0 nm Flaps Up 6000 7.2 nm

7000 8.4 nm Zero Wind 8000 9.6 nm

9000 10.8 nm 3000 lbs 10000 12.0 nm

11000 13.2 nm 12000 14.4 nm 13000 15.6 nm 14000 16.8 nm 15000 18.0 nm 16000 19.2 nm