Piper PA-34-200 PA-34-200T Turbo Seneca · standard normal
1. Slowly retard prop control until RPM drops to 800 RPM. 2. Immediately Restore Prop Control.
1. Advance Throttle to 2000 RPM. 2. Retard Prop Control by 200 RPM. 3. Advance Throttle Slightly and observe little or no change in RPM. 4. Restore Props to FULL RPM.
Max Drop 150 RPM. Max Diff 50 RPM.
1. LEFT ALTERNATOR OFF: 2. VERIFY: Right Takes Load 3. LEFT ALTERNATOR ON 4. RIGHT ALTERNATOR OFF: 5. VERIFY: Left Takes Load 6. RIGHT ALTERNATOR ON
1. LEFT FUEL OFF 2. When Engine Sputters Select LEFT XFEED ON 3. VERIFY ENGINE STILL RUNS 4. Reset LEFT FUEL ON 5. RIGHT FUEL OFF 6. When Engine Sputters Select RIGHT X-FEED ON 7. VERIFY ENGINE STILL RUNS 8. Reset RIGHT FUEL ON
Static / Rolling, Normal / Short Field, Flap Setting
CONSIDER: Runway Length, Runway Friction, Engine Performance, Density Altitude, Terrain and adjust courses of action to the conditions at hand. (see following page)
Verify Set as Needed
Closed Traffic/Radar Vect, Visual/ILS, Crew Duties
Current Conditions
Brief Procedure
Source: Piper/PA-34-200 Seneca/Piper_PA_34_200T_Turbo_Seneca_Normal_Procedures.txt
Rights: licensed
Checklist hash: 440083f0d235ddd82360d4ef711cdf67…
Generated from piper-pa-34-200-seneca-piper-pa-34-200t-turbo-seneca-normal-procedures.ocl.json by the Open Checklists
reference renderer. Verify against the aircraft's own approved documentation before use.