Systems 2 - ECS, SEAT and CANOPY Flashcards
Which lever on the OBOGS controls electrical power to the OBOGS?
oxygen regulator supply lever
The ejection seat emergency oxygen system provides which of the following?
a. 10 seconds of oxygen
b. 1 minute of oxygen
c. 5 – 7 minutes of oxygen
d. 10 minutes of oxygen
d
The __________ produces up to 350 cubic feet per minute of airflow in the HI setting. (B/5/3)
a. evaporator blower
b. condenser blower
c. bleed air inflow
d. ram air flow
a
The purpose of the CFS is to
a. close, fix, and secure the canopy.
b. seal the canopy to maintain pressurization.
c. fracture the canopy during ejection.
d. keep the center and forward windscreens clear of fog.
c
Which annunciator lights when inflow air temperature exceeds 300° Fahrenheit?
DUCT TEMP Annunciator
The amber CKPT ALT means that the cockpit pressure altitude exceeds __________ feet.
a. 10,000
b. 13,000 ±100
c. 19,000
d. 25,000
c
When flying dual, an ISS mode selector setting of __________ allows either crewmember to initiate ejection of both seats. (B/1/7)
a. SOLO
b. BOTH
c. CMD FWD
d. DUAL
b
Assuming bleed air inflow is available, the pneumatic canopy pressure seal inflates when
a. the canopy is closed and locked.
b. passing approximately 8,000 feet pressure altitude.
c. weight is off of the right main landing gear.
d. the defog lever is placed in the CANOPY position.
c
During ejection, emergency oxygen is provided __________. (B/1/5)
a. for about 10 minutes or until turned off
b. for about 10 minutes and after seat-pilot separation
c. for about 10 minutes or until seat-pilot separation
d. until seat-pilot separation or until it is turned off
c
The T-6A anti-G system helps maintain __________ during high G maneuvers. (C/2/2)
a. control coordination
b. blood circulation
c. an upright attitude
d. airspeed
b
The CFS functions __________ during __________, or __________ using internal CFS handles. (B/3/1)
a. automatically; ejection; manually
b. automatically; ground egress; manually
c. manually; ejection; manually
d. automatically; ejection; automatically
a
The environmental system has two temperature sensors to alert you to overtemperature in the
a. ECS heat exchanger.
b. heating/defog ducting.
c. evaporator/blower modules.
d. engine-driven compressor.
a (Er det givne svar… men “b” må være det rigtige, da sensorerne sidder i ducting og ikke i ECS heat exchanger….)
Which of the following statements is incorrect? (B/1/2)
a. The locking/latching system secures the canopy in the closed position.
b. The Canopy Fracturing System (CFS) provides a means for egress if you cannot open the canopy in an emergency.
c. The hinge/strut system secures the canopy in the closed position.
d. The pressure seal prevents cockpit pressure leaks.
c
What happens if the ADU Mode Selector Switch is set to AUTO?
a. The SSK is lowered 10 seconds after ejection
b. The SSK is lowered 4.0 to 6.0 seconds after seat-pilot separation
c. The SSK is lowered 4.0 seconds after ejection
d. The SSK is lowered 10 seconds after seat-pilot separation
b
SSK bliver sluppet 4 sekunder efter seat/man separation, som sker efter 1,24-1,45 sekunder
Activating the CFS handle from the front cockpit activates the
a. front and rear systems simultaneously.
b. front system followed by the rear system after a .3 second delay.
c. front cockpit system only.
d. ejection system for the front cockpit only.
c
Placing the vent lever in the __________ position causes the valve at the front cockpit assembly to direct the warm air into the windshield defog duct. (B/4/2)
a. HIGH
b. CANOPY
c. FOOT
d. HOT
b
Which switch controls the position of the fresh air valve?
RAM AIR flow switch
What is the purpose of the leg restraint system? (B/1/3)
a. Prevent movement about the cockpit during flight
b. Prevent the feet from flailing during ejection
c. Ensure freedom of movement during ejection
d. Avoid constriction during ejection
b
During the ejection process, movement of the seat is first initiated by __________. (B/2/1)
a. explosive hydraulic pressure
b. mechanical catapult thrust
c. detonated gas pressure
d. detonation of the rocket motor propellant
c
The pressurization system overrides the RAM AIR FLOW switch and closes the fresh air valve when the aircraft reaches an altitude of approximately __________ MSL. (B/2/2)
a. 5000
b. 8000
c. 10000
d. 15000
b
The engine-driven air conditioner compressor pumps refrigerant in vapor form to the
a. evaporator.
b. condenser.
c. heat exchanger.
d. blower.
b
The __________ valve incorporated into the oxygen hose attachment fitting on the right console in each cockpit allows you to continue breathing ambient cockpit air if the OBOGS fails. (C/3/2)
a. ambient air
b. fail safe
c. anti-suffocation
d. emergency oxygen
c
What happens during simultaneous ejections (ISS mode selector is set to BOTH)? (C/2/1)
a. The front seat will be delayed until the rear seat is clear.
b. The rear seat will eject second.
c. Both seats eject simultaneously with the rear rocket motor firing first.
d. The rear seat will eject first.
d
After takeoff the __________ supplies cooling air to the heat exchanger.
a. ram air inlet
b. fresh air blower
c. bleed air system
d. air conditioner
a
Which switch (In which position) opens the pressurization control valve, closes the defog valve, leaves the bleed air inflow valve open, and leaves the fresh air valve closed?
a. Air cond - on or off
b. Bleed Air In Flow - OFF-NORM-HI
c. Pressurization - RAM/DUMP-DUMP-NORM
d. Ram Air Flow - OFF-NORM-HI
c. “DUMP”-position
After pressing the BIT button on the regulator to start the OBOGS I-BIT, which light do you expect to see on the annunciator panel when the oxygen concentration falls below normal?
OBOGS FAIL annunciator
Why is it a good practice to eject from the aircraft in a level flight attitude? (C/1/2)
a. Avoid a collision of the front and rear ejection seats
b. Ensure a clear path away from the airframe
c. Avoid flying debris and rocket motor blast
d. Ensure little or no sink rate
d
While in flight, cool air from the __________ passes through the heat exchanger, cooling the hot bleed air from the engine, and then exits through a vent in the lower right cowling. (B/3/1)
a. blower
b. ram air inlet
c. right P3 air port
d. inflow valve
b
Activating the __________ prevents engine compartment smoke and/or fumes from entering the cockpit through the heating system after an engine shutdown situation. (B/3/3)
a. RAM AIR FLOW
b. EVAP BLWR
c. FIREWALL SHUTOFF
d. BLEED AIR INFLOW
c
Do not open the canopy when winds exceed __________ knots. (B/2/5)
a. 10
b. 20
c. 30
d. 40
d
The OBOGS __________ annunciator lights approximately 3 minutes after initial power up if thesystem fails the BIT. (C/3/3)
a. TEST
b. TEMP
c. FAIL
d. BIT
c