Pressurization Flashcards
“Big” P3 components:
Pressurization and Heating
“Little” P3 components:
Pneumatic systems
Describe the motion of Uncontrolled Pressurization Airflow (P3):
1) In from engines
2) Forward to mixing plenum
3) Rearward into cabin
Describe the motion of Controlled Pressurization Outflow:
Exits through Outflow Valve at rear pressure bulkhead and ducts into the unpressurized tailcone, then overboard
Describe the Ambient Air Intakes:
Located in fire shield under intake screens.
Used to moderate temperature of P3 air once airborne.
Describe the Ambient Air Sensor:
Samples ambient air temp to meter ambient airflow into system
Pressurization Control Unit- Flow Pack
Admits hot P3 air for pressurization and heating.
Admits cool ambient air to moderate high P3 temps.
Bleed Air Valves
Valve to control pressurization airflow.
Located on the flow pack.
Valve is controlled by cockpit bleed air switch.
-In open, power applied to open environmental valves on pressurization flow packs.
-In middle and down positions, power is removed from these valves, they close, and there is no pressurization or heating from that engine.
Max. differential pressure:
200: 6.1 psid
B200: 6.6 psid
Max flight time with cracked windshield:
25 hours
Max altitude and pressure differential with cracked windshield:
25,000’
4 psid
R/L BL AIR OFF
indicates switch position of bleed air valves. NOT in the open position
Safety Valve
Hooked to Dump Solenoid (NC) Capped. Pressure dump Capability. Overpressure protection Negative differential relief
Outflow Valve
Vented into cabin pressure Hooked to Preset Solenoid (NO) Pressurization outflow control Overpressure protection Negative differential relief
Pressure controller provides vacuum to outflow valve to control airflow leaving pressure vessel
Schrader Valve
Located in Safety Valve and Outflow Valve. Compares cabin pressure to tailcone. If differential pressure exceeds 6.5 PSID (B200) valve will cycle to relieve excess pressure. I.e. Overpressure protection