checklist - ERAU ETA - Embry-Riddle Aeronautical University
checklist - ERAU ETA - Embry-Riddle Aeronautical University checklist - ERAU ETA - Embry-Riddle Aeronautical University
16 PA-28R-201 SOP Fuel Vapor (Vapor Lock) Identification and Corrective Action Recognition of a Vapor Problem: Fluctuations of idle speed and fuel flow. Poor engine response to throttle movement. Engine will not run when throttle is in the Close position. High RPM drop (greater than 150 rpm) when checking magnetos. Corrective Action: 1) Advance the throttle to obtain an engine speed of 2300-2500 RPM. 2) Maintain that engine speed for 1-2 minutes, or until engine operation becomes smooth. Ensure that the oil temperature remains within the acceptable range. 3) Retard the throttle to the Close position to verify normal engine operation. 4) Advance the throttle to 1000 RPM and lean for taxi. 5) Immediately prior to brake release for the takeoff roll (coordinate with ATC, as necessary), set the mixture control to the full forward (full rich) position, advance the throttle to full forward, and hold the airplane in position with full throttle for 10 seconds to ensure satisfactory engine operation. Revised 07-01-2012 © Embry-Riddle Aeronautical University Rev 06
PA-28R-201 SOP 17 LEANING PROCEDURES The following leaning procedures, developed for use during ground, climb, cruise, descent, and landing operations, are employed to aid in preventative maintenance and flight safety operations. With respect to the engine operation, utilization and adherence to these procedures are important, especially during high power settings and rich mixture settings, to prolong the engine life and to ensure flight safety. GROUND Confirm that the Mixture Control is in the Full Forward (Full Rich) position. Lean the mixture by slowly moving the Mixture Control back to the stop. TAKEOFF (High elevation airports only) At high elevation airports (at or above 3000’ MSL), prior to takeoff, lean the mixture only enough to obtain smooth engine operation. Use care not to overheat the engine. CLIMB Below 3000’ pressure altitude, leave the Mixture Control in the Full Forward (Full Rich) position. Above 3000’ pressure altitude, lean the mixture only enough to obtain smooth engine operation. CRUISE (at all altitudes) Local Flight: Set cruise power, then slowly move the Mixture Control back until a until a slight increase of airspeed is noted or engine operation becomes rough. Next, slowly move the Mixture Control forward to obtain smooth engine operation. Cross-Country Flight: Set cruise power, then lean the mixture using the Exhaust Gas Temperature (EGT) gauge to achieve engine operation at 100°F to the “rich” side of peak (best power). 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: PA-28R-201 SOP 15 PRIMING/STARTING
- 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 and 40: PA-28R-201 SOP 31 28. ALTERNATE STA
- Page 41 and 42: PA-28R-201 SOP 33 6. TIE-DOWN/CHOCK
- 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
16 PA-28R-201 SOP<br />
Fuel Vapor (Vapor Lock)<br />
Identification and Corrective Action<br />
Recognition of a Vapor Problem:<br />
Fluctuations of idle speed and fuel flow.<br />
Poor engine response to throttle movement.<br />
Engine will not run when throttle is in the Close position.<br />
High RPM drop (greater than 150 rpm) when checking magnetos.<br />
Corrective Action:<br />
1) Advance the throttle to obtain an engine speed of 2300-2500 RPM.<br />
2) Maintain that engine speed for 1-2 minutes, or until engine operation<br />
becomes smooth. Ensure that the oil temperature remains within the<br />
acceptable range.<br />
3) Retard the throttle to the Close position to verify normal engine<br />
operation.<br />
4) Advance the throttle to 1000 RPM and lean for taxi.<br />
5) Immediately prior to brake release for the takeoff roll (coordinate with<br />
ATC, as necessary), set the mixture control to the full forward (full<br />
rich) position, advance the throttle to full forward, and hold the<br />
airplane in position with full throttle for 10 seconds to ensure<br />
satisfactory engine operation.<br />
Revised 07-01-2012 © <strong>Embry</strong>-<strong>Riddle</strong> <strong>Aeronautical</strong> <strong>University</strong> Rev 06