PA 44 - 180 - Seminole Flashcards
Wingspan
38’ 6.6”
Length
27’ 7.2”
Turn Radius
33’
Ramp Weight
3816 lbs
MTOW
3800 lbs
MLW
3800 lbs
Airframe Materials
Aluminium alloy with steel engine mounts plus fibreglass nosecone, cowling, wingtips, rudder, fin and stabilator.
Airframe Structure
Semi monocoque
Wing design
Semi tapered (main spar 40% chord)
Purpose of rear spar
Takes torque and drag and provide mounts for flaps and ailerons.
Engine specs
Lycoming (L) 0-360 A1H6 180 bhp @ 2700 rpm 8.5:1 comp ratio Direct drive Horizontally opposed 4 cylinder Air cooled
Propellor specs
Hartzell 74" maximum diameter / 72" minimum diameter Constant speed Full feather Counter rotating Engine 1 = Clockwise Engine 2 = Anticlockwise
How is propellor pitch controlled?
Nitrogen and Oil pressure.
Increase in oil px = High RPM and Unfeather position / fine pitch.
Increase in nitrogen px = Low RPM and feather position coarse pitch.
Purpose of large spring in the variable pitch propellor?
To prevent overspeed of propellor.
Above what rpm does the feather lock prevent feathering?
950 rpm
Type of motor that powers landing gear?
Electric hydraulic motor.
(N.B: gear should not be change up/down or vice versa if gear is in transit).
MFD landing gear annunciators (lights).
Gear down = Solid green circle
Gear up = hollow white circle
Transit = crosshatched square
Abnormal = red circle.
Landing gear direction of retraction?
Nosewheel = retracts aft Mains = inwards
How can gear position be verified?
Mirror on side of nacelle / MFD annunciator.