AVIT 325 FINAL TEST QUESTIONS WITH ACCURATE
ANSWER
1 method to verify inoperative engine correct answer increase/decrease throttles
and check for yawing
2 methods 2 identify inoperative engine correct answer check for dead rudder
check for lower EGT
A Critical Altitude (pertaining to turbo/super-chargers) is: correct answer the
maximum altitude at which the rated horsepower can be produced.
A Red CAS message is: correct answer Master Warning, accompanied by a
repeating triple chime aural alert
A single-engine stall is a spin condition. correct answer true
A turbo-normalized engine: correct answer maintains the rated horsepower from
sea level up to the critical altitude.
A windmilling prop (such as in an engine failure) causes approximately a
_________ FPM penalty for aircraft performance. correct answer -200
After Engine Start Check correct answer Fuel Selectors.......................... Crossfeed
Environmental Controls ........As Required
Mixtures ............................................Lean
Avionics Master ...................................On
,Engine Instruments........................ Check
ALTR AMPS ......................Check Positive
VOLTS ........................................... Check
Fuel Pumps .........................................Off
Fuel Selectors......................................On
Autopilot..................... Self-Test Complete
airspeed markings correct answer white (flaps down) = 55-111 KIAS
green (normal operating) = 57-169
yellow (caution, smooth air only) = 169-202
red (never exceed) = 202
blue line (OEI best ROC) = 88
Anti-Servo Trim Tab correct answer movement in the same direction, increases
stability
Are our Seminoles approved for RNP operations? correct answer Yes but no
Radius-to-Fix (RF) legs
Are our Seminoles approved for use for FAR Part 135 operations? correct answer
yes
Autopilot coupled go-around is allowed according to Piper. correct answer false
AUTOPILOT LIMITATIONS correct answer ALTITUDES
, T/O & climb : 400+ ft AGL
Cruise/Descent: 1000+ ft AGL
Approach: 200+ ft AGL
AIRSPEEDS
On approach: at least 90 KIAS
other than approach: at least 80-190
Max fuel imbalance = 10 gal
Before Landing Check correct answer Fuel Pumps .........................................On
Landing Gear .................. Down & Locked
Propellers ................................2500 RPM
Mixtures .............................................. Set
Before Start Check correct answer Passenger Briefing ................... Complete
Parking Brake ..................................... Set
Seats ..................................Adjust & Lock
Belts & Harnesses ..........Adjust & Secure
Cabin Door ................Close & Latch/Hold
Aircraft Lights........................As Required
Emergency Battery Switch ................Arm
Landing Gear Handle ..................... Down
Magneto Switches ...............................On
ANSWER
1 method to verify inoperative engine correct answer increase/decrease throttles
and check for yawing
2 methods 2 identify inoperative engine correct answer check for dead rudder
check for lower EGT
A Critical Altitude (pertaining to turbo/super-chargers) is: correct answer the
maximum altitude at which the rated horsepower can be produced.
A Red CAS message is: correct answer Master Warning, accompanied by a
repeating triple chime aural alert
A single-engine stall is a spin condition. correct answer true
A turbo-normalized engine: correct answer maintains the rated horsepower from
sea level up to the critical altitude.
A windmilling prop (such as in an engine failure) causes approximately a
_________ FPM penalty for aircraft performance. correct answer -200
After Engine Start Check correct answer Fuel Selectors.......................... Crossfeed
Environmental Controls ........As Required
Mixtures ............................................Lean
Avionics Master ...................................On
,Engine Instruments........................ Check
ALTR AMPS ......................Check Positive
VOLTS ........................................... Check
Fuel Pumps .........................................Off
Fuel Selectors......................................On
Autopilot..................... Self-Test Complete
airspeed markings correct answer white (flaps down) = 55-111 KIAS
green (normal operating) = 57-169
yellow (caution, smooth air only) = 169-202
red (never exceed) = 202
blue line (OEI best ROC) = 88
Anti-Servo Trim Tab correct answer movement in the same direction, increases
stability
Are our Seminoles approved for RNP operations? correct answer Yes but no
Radius-to-Fix (RF) legs
Are our Seminoles approved for use for FAR Part 135 operations? correct answer
yes
Autopilot coupled go-around is allowed according to Piper. correct answer false
AUTOPILOT LIMITATIONS correct answer ALTITUDES
, T/O & climb : 400+ ft AGL
Cruise/Descent: 1000+ ft AGL
Approach: 200+ ft AGL
AIRSPEEDS
On approach: at least 90 KIAS
other than approach: at least 80-190
Max fuel imbalance = 10 gal
Before Landing Check correct answer Fuel Pumps .........................................On
Landing Gear .................. Down & Locked
Propellers ................................2500 RPM
Mixtures .............................................. Set
Before Start Check correct answer Passenger Briefing ................... Complete
Parking Brake ..................................... Set
Seats ..................................Adjust & Lock
Belts & Harnesses ..........Adjust & Secure
Cabin Door ................Close & Latch/Hold
Aircraft Lights........................As Required
Emergency Battery Switch ................Arm
Landing Gear Handle ..................... Down
Magneto Switches ...............................On
