Foul Weather / AC and PX Systems Flashcards
Two subsystems
Air scoop
Compressor inlet assembly
Prop ice control time
160 seconds, 20 seconds each of the cuffs, skirts and islands for 4 engines
76-100 amps in flight, 74-100 on the ground
Diffuser anti ice percent drop
9% and 5% increase in FF
Timer motor for emp deice
8 seconds per strip with 16 second dead band = total 176 secs
Engine and wing use what kind of heat?
Prop and emp?
Air only in normal RPM
Electric low or normal RPM
Memory aid: engines run both on the ground and in the air. Wings only work in the air (norm)
Ice detector
- when to use
- power source
- test perameters
- whenever MEAC is powered
- MEAC: probe heater, MEDC: icing light
- N/A
Pitot heat
- when to use
- power source
- test perameters
Before start to secure checklist
FEAC: pilot, MEAC(28c fwd lighting): copilot, MEDC: caution lights
N/A
AOA heat
- when to use
- power source
- test perameters
Before start to secure checklist
MEDC
N/A
Engine
- when to use
- power source
- test perameters
Prior to entering areas where structural icing is likely
MEDC (loss of power)
Normal or low rpm with a TIT increase then TIT decrease and increase
Prop
- when to use
- power source
- test perameters
Whenever stuctural icing is evident
BUS B: heater elements, aft lighting trans: GND test, EMDC: control
Reduce voltage; same speed (160 secs for complete cycle)
Wing
- when to use
- power source
- test perameters
When ice builds up to .5”
EMDC: mod valves, MEDC: caution lights
10 degrees TIT rise with corresponding wing temp rise
EMP
- when to use
- power source
- test perameters
When structural icing is encountered in flight (used with wing deice)
BUS A: parting strips, BUS B: cycling strips, MEAC: timer motor, EMDC: relay control, MEDC: caution lights
Same power; high speed motor; 44 sec vs 176 secs for normal speed
Windshield
- when to use
- power source
- test perameters
Before start to secure checklists
MEAC/MEDC: front wiper power control, BUS A/EMDC: side
MEDC: caution lights
N/A
Drive spline shear HP
257 HP
Relief valve nominal px
PRESS LOW light
100psi
Below 50psi
TEMP HIGH Light
Exceeding 121 degrees C
Control valves fully open at how many feet?
12,000
Heat exchanger REFR OVHT light on at
Exceeding 166 degrees C
Automatic temperature control mode range
18-29 C
A valve
Turbine bypass valve
Air that is partially cooled by heat exchanger to bypass the fregeratuon turbine unit to enter the flight station or cabin risers
B valve
Turbine shutoff valve
Air passes the expansion turbine driving the secondary compressor
C valve
Hot air bypass valve (hot compressed air from EDC or multiplier enters the riser)
Pressure ratio limiting
Yellow condtion psi
Red condition
72psi
50psi
Prop and Emp uses what heat?
Electrical heat
Sources of heat
APU, EDC’s, 14th stage bleed air
4 functions of the Aux Vent switch placed in the open position
EDC’s dumped
Firewall Shut off valve closes
Outflow valve opens electrically
The valve itself opens fully