SF34B+ SAAB340 Flashcards
(46 cards)
BOW
~19500
MZFW
26500
MLDW
28500
MTOW
29000
MRAMP(TAXI)
29300
Max Fuel
5690
Imbalance
200
Length
64’ 9”
Height
22’ 11”
Wing Span
70’ 4”
Minimum turning radius
57’
Seat Configuration
-12 rows of seats, 34 seats total A - Window row C - Single row D - Aile row F - Window row
Cargo Compartment
Divided into 2 sections;
C1 Max weight - 1125
C2 Max weight - 850
Total weight = 1752
Exit doors
Total 5 exit doors
- Main door
- Cockpit scape hatch
- Forward emergency exit
- 2 Over-wing emergency exit
Power plant
2 General Electric CT7-9B Turbo-prop engines
1750 SHP
Engine Modules and components
- Propeller gear case
- Cold section module
- Accessory section module
- Hot section module
- Power turbine module
APR (automatic power reserve)
Automatically increase torque to 7% on the operating engine in the event of an engine failure
Autocoarsen system (auto feather)
Automatically drives propeller blades to 55 degree angle in the event of engine failure to reduce drag
CTOT System (Constant Torque on Takeoff)
Assists pilot in setting takeoff power by electronically selecting a preset torque value speed and accuracy improves takeoff performance 60%-100%
Propeller System
Dowdy Rotol 4 composite propeller blades
Has three layer - Fiberglass woven, Amber Resin, and black paint
Fuel System
- Each wing has one inboard and one outboard tank, both are interconnected.
- Left inboard tank feeds left engine and right inboard tank feeds right engine
- Left tank can cross feed the right engine and right tank can feed the left tank, however they cannot transfer fuel between tanks
Single point fueling
Located on the right wing leading edge for pressure fueling and de-fueling, control panel is powered by right hot battery bus.
-There is an over-wing port on each wing which can be used in case the single point fueling system is inop
Primary flight control
Aileron, Elevator, Rudder (mechanical)
Secondary control
Flaps and tab trim (hydraulic)
