checklist - ERAU ETA - Embry-Riddle Aeronautical University
checklist - ERAU ETA - Embry-Riddle Aeronautical University checklist - ERAU ETA - Embry-Riddle Aeronautical University
32 PA-28R-201 SOP RIGHT WING CHECKLIST Start the exterior inspection at the right rear wing and proceed in a counter-clockwise direction. Emphasis and attention should be placed on all surface conditions including flight control surfaces and access panel security. Check surface areas around the aircraft for fluid leakage and foreign object damage (FOD). A flashlight is required for all preflight inspections conducted at night. 1. FLAP/AILERON ...................................................................... INSPECT 2. STATIC WICKS (3)................................................................. INSPECT 3. WING TIP/LIGHTS ................................................................. INSPECT 4. LEADING EDGE ..................................................................... INSPECT 5. FUEL QUANTITY ...................................................... VERIFY (CHECK) 6. TIE-DOWN/CHOCKS ............................................................. REMOVE 7. FUEL TANK VENT .................................................................... CHECK 8. MAIN GEAR ........................................................................... INSPECT 9. RIGHT WING FUEL SUMP DRAIN (1) ....................................... DRAIN 10. RIGHT WING CHECKLIST ................................................. COMPLETE 1. FLAP/AILERON INSPECT INSPECT the FLAP and AILERON, checking for freedom of movement and/or security of the hinges and actuators. 2. STATIC WICKS (3) INSPECT INSPECT the condition and security of the STATIC WICKS (3): one (1) on the flap and two (2) on the aileron. 3. WING TIP/LIGHTS INSPECT INSPECT the WING TIP for dents and cracks. If a crack exists, verify that is has been stop drilled to prevent further cracking. INSPECT the condition of the strobe and position LIGHTS. 4. LEADING EDGE INSPECT INSPECT the LEADING EDGE of the wing for dents and cracks. 5. FUEL QUANTITY VERIFY (CHECK) VERIFY that the FUEL QUANTITY has been checked at least once since the last refueling. If the aircraft has been refueled since originally sampling the fuel, CHECK the fuel again for proper grade and for any debris. Revised 07-01-2012 © Embry-Riddle Aeronautical University Rev 06
PA-28R-201 SOP 33 6. TIE-DOWN/CHOCKS REMOVE Slowly REMOVE the TIE-DOWN to avoid any under wing damage and place the chain adjacent to, but not in, the indentation of the concrete around the chain’s ramp securing points (water accumulation in these areas will rust the chains). Place the CHOCKS over the chain’s ramp securing point to keep them away from the landing gear and propeller. 7. FUEL TANK VENT CHECK CHECK that the FUEL TANK VENT (located on underside of wing) is unobstructed. The fuel tank vent provides a venting source to accommodate changing pressure in the fuel tank to ensure proper fuel flow. It is normal to see fuel or evidence of fuel (blue staining) at the vent due fuel expansion as its temperature increases. 8. MAIN GEAR INSPECT INSPECT the MAIN GEAR and brake assembly for damage, cracks, hydraulic fluid, and brake pad wear. Check to see that the tire looks properly inflated, is free of “flat” spots from skidding, and no cord is showing. Check the main gear retraction mechanism for any obstruction(s). Check the Up Lock and Down Lock switches. Check the strut for proper strut inflation (2.50” ± .25”). Check the main gear door for security and any damage. Finally, check the external main gear components are secure with castle nuts and safety (cotter) pins. 9. RIGHT WING FUEL SUMP DRAIN (1) DRAIN Using the fuel sample cup, DRAIN a small quantity of fuel from the RIGHT WING FUEL SUMP DRAIN (located on the inboard rear corner of the underside of the right wing). Check for water, sediment, and verify that the proper grade of fuel (100LL, Blue in color) is present. Water in the sample will be indicated by a clear amount of liquid at the bottom of the sampler cup (due to the greater density of water than fuel). Dispose of contaminated fuel in the fuel receptacles located on the east side of the ERAU ramp. Remove any residual water from inside of sampler cup and continue to take fuel samples until water is no longer present in any fuel sample. NOTE DO NOT DUMP FUEL ON THE RAMP. 10. RIGHT WING CHECKLIST COMPLETE Upon completion of the RIGHT WING CHECKLIST, verify that all items have been accomplished and that the checklist is COMPLETE. Rev 06 © Embry-Riddle Aeronautical University Revised 07-01-2012
- Page 1 and 2: PIPER ARROW PA-28R-201 Standard Ope
- Page 3 and 4: PA-28R-201 SOP i TABLE OF CONTENTS
- Page 5 and 6: PA-28R-201 SOP iii REVISION HIGHLIG
- Page 7 and 8: PA-28R-201 SOP v Page Rev # Date Pa
- Page 9 and 10: PA-28R-201 SOP 1 INTRODUCTION The p
- Page 11 and 12: PA-28R-201 SOP 3 When a callout is
- Page 13 and 14: PA-28R-201 SOP 5 Pilot Flying (PF)
- Page 15 and 16: PA-28R-201 SOP 7 NOTE If the PM doe
- Page 17 and 18: PA-28R-201 SOP 9 STANDARD CALLOUTS
- Page 19 and 20: PA-28R-201 SOP 11 ACTION Changing A
- Page 21 and 22: PA-28R-201 SOP 13 STANDARD CALLOUTS
- Page 23 and 24: PA-28R-201 SOP 15 PRIMING/STARTING
- Page 25 and 26: PA-28R-201 SOP 17 LEANING PROCEDURE
- Page 27 and 28: PA-28R-201 SOP 19 BRAKE/STEERING CH
- Page 29 and 30: PA-28R-201 SOP 21 Section 1: PRE-FL
- Page 31 and 32: PA-28R-201 SOP 23 (This page intent
- Page 33 and 34: PA-28R-201 SOP 25 PRE-FLIGHT CHECKL
- Page 35 and 36: PA-28R-201 SOP 27 NOTE The fuel qua
- Page 37 and 38: PA-28R-201 SOP 29 NOTE Each fuel ta
- Page 39: PA-28R-201 SOP 31 28. ALTERNATE STA
- Page 43 and 44: PA-28R-201 SOP 35 5. COOLING/INDUCT
- Page 45 and 46: PA-28R-201 SOP 37 LEFT WING CHECKLI
- Page 47 and 48: PA-28R-201 SOP 39 11. STATIC WICKS
- Page 49 and 50: PA-28R-201 SOP 41 around the chain
- Page 51 and 52: PA-28R-201 SOP 43 Section 2: NORMAL
- Page 53 and 54: PA-28R-201 SOP 45 BEFORE START CHEC
- Page 55 and 56: PA-28R-201 SOP 47 For night operati
- Page 57 and 58: PA-28R-201 SOP 49 (This page intent
- Page 59 and 60: PA-28R-201 SOP 51 ENGINE START CHEC
- Page 61 and 62: PA-28R-201 SOP 53 10. ELECTRIC FUEL
- Page 63 and 64: PA-28R-201 SOP 55 BEFORE TAXI CHECK
- Page 65 and 66: PA-28R-201 SOP 57 - GPS: Initialize
- Page 67 and 68: PA-28R-201 SOP 59 (This page intent
- Page 69 and 70: PA-28R-201 SOP 61 BEFORE TAKEOFF
- Page 71 and 72: PA-28R-201 SOP 63 8. MAGNETOS (175/
- Page 73 and 74: PA-28R-201 SOP 65 16. MIXTURE LEAN
- Page 75 and 76: PA-28R-201 SOP 67 BEFORE TAKEOFF CH
- Page 77 and 78: PA-28R-201 SOP 69 8. PARKING BRAKE
- Page 79 and 80: PA-28R-201 SOP 71 BEFORE TAKEOFF
- Page 81 and 82: PA-28R-201 SOP 73 (This page intent
- Page 83 and 84: PA-28R-201 SOP 75 CLIMB CHECKLIST A
- Page 85 and 86: PA-28R-201 SOP 77 (This page intent
- Page 87 and 88: PA-28R-201 SOP 79 CRUISE CHECKLIST
- Page 89 and 90: PA-28R-201 SOP 81 DESCENT CHECKLIST
PA-28R-201 SOP 33<br />
6. TIE-DOWN/CHOCKS REMOVE<br />
Slowly REMOVE the TIE-DOWN to avoid any under wing damage and<br />
place the chain adjacent to, but not in, the indentation of the concrete<br />
around the chain’s ramp securing points (water accumulation in these<br />
areas will rust the chains). Place the CHOCKS over the chain’s ramp<br />
securing point to keep them away from the landing gear and propeller.<br />
7. FUEL TANK VENT CHECK<br />
CHECK that the FUEL TANK VENT (located on underside of wing) is<br />
unobstructed. The fuel tank vent provides a venting source to<br />
accommodate changing pressure in the fuel tank to ensure proper fuel flow.<br />
It is normal to see fuel or evidence of fuel (blue staining) at the vent due<br />
fuel expansion as its temperature increases.<br />
8. MAIN GEAR INSPECT<br />
INSPECT the MAIN GEAR and brake assembly for damage, cracks,<br />
hydraulic fluid, and brake pad wear. Check to see that the tire looks<br />
properly inflated, is free of “flat” spots from skidding, and no cord is<br />
showing. Check the main gear retraction mechanism for any<br />
obstruction(s). Check the Up Lock and Down Lock switches. Check the<br />
strut for proper strut inflation (2.50” ± .25”). Check the main gear door for<br />
security and any damage. Finally, check the external main gear<br />
components are secure with castle nuts and safety (cotter) pins.<br />
9. RIGHT WING FUEL SUMP DRAIN (1) DRAIN<br />
Using the fuel sample cup, DRAIN a small quantity of fuel from the RIGHT<br />
WING FUEL SUMP DRAIN (located on the inboard rear corner of the<br />
underside of the right wing). Check for water, sediment, and verify that the<br />
proper grade of fuel (100LL, Blue in color) is present. Water in the sample<br />
will be indicated by a clear amount of liquid at the bottom of the sampler<br />
cup (due to the greater density of water than fuel). Dispose of<br />
contaminated fuel in the fuel receptacles located on the east side of the<br />
<strong>ERAU</strong> ramp. Remove any residual water from inside of sampler cup and<br />
continue to take fuel samples until water is no longer present in any fuel<br />
sample.<br />
NOTE<br />
DO NOT DUMP FUEL ON THE RAMP.<br />
10. RIGHT WING CHECKLIST COMPLETE<br />
Upon completion of the RIGHT WING CHECKLIST, verify that all items<br />
have been accomplished and that the <strong>checklist</strong> is COMPLETE.<br />
Rev 06 © <strong>Embry</strong>-<strong>Riddle</strong> <strong>Aeronautical</strong> <strong>University</strong> Revised 07-01-2012