Systems Flashcards
Alternator Amps
65
Battery Amps
35
Battery Volts
12
Seneca System Volts
14
RPMS needed to produce full alternator output
2000
Horsepower of engines
200 at 2575 RPM at Sea Level. 215 at 12,000 Feet.
Max RPMs
2575
Max Manifold Pressure
39 Inches of Mercury (40 per the POH)
Type of fuel injectors
Continuous Flow
Feather lockout pin engages at _______ RPM
800
Gear extension or retraction takes _________ seconds
6-7
Feathering takes approximately ______ seconds
6
Do not attempt emergency gear extension above
84 Knots
The nose gear can move _______ degrees left or right of center
27 (54 degree arc)
The landing gear is ________ powered and _________ operated
Electrically / Hydraulically
Total unusable fuel
5 Gallons
Fuel minimum octane
100/130
Aux fuel pump can provide enough fuel pump for up to __% power
75
Gyro operating limits
4.5 - 5.2 Inches of Mercury
What lights will remain illuminated after an engine is feathered?
Alternator, Gyro Air, and Engine Oil Pressure
How much fuel does the heater use and where does it take it from?
(POH: 0.5) 1.5 Gallons per hour from the left fuel tank
Before turning off on the ground, set the heater to fan for ____ minutes to prevent overheating
2
The stall warning horn will sound _________ knots above stall speed
5-10
The inboard lift detector is calibrated for _________ degrees of flaps
25-40
The outboard lift detector is calibrated for _________ degrees of flaps
0-10
When will the gear warning horn sound?
Gear not down with MP below 14” and gear selector up with airplane on the ground.
Max capacity of baggage compartments
100 pounds
PSI of O2 system
1850 PSI at 70 degrees F
What type of ailerons does the Seneca have and what is it’s purpose?
Frise type and they help counteract adverse yaw.
The stabilator has what kind of tabs and how do they move?
Anti-servo tabs. They move in the same direction but further.
(N47404) What is the propeller manufacturer?
Hartzell
(N47404) What is the compression ratio of the engines?
7.5 : 1