B737 Questions - Air/Bleed/Pressurization Systems
m m m m
Studymonlinematmhttps://quizlet.com/_c7y2vm
B737 Questions - Air/Bleed/Pressurization Systems Questions And Answers
1. The overboard exhaust valve:
m m m
(a) is normally open in flight and exhaust air is diffused to the lining of the
m m m m m m m m m m m m m m
mforward cargo compartment. m m
(b) remains closed if both pack switches are in high.
m m m m m m m m
(c) allows for increased ventilation in the smoke removal config uration.
m m m m m m m m
(d) remains closed on the ground and in flight with low different ial pressure.-
m m m m m m m m m m m
: The overboard exhaust valve:
m m m m
(c) allows for increased ventilation in the smoke removal configuration. Re
m m m m m m m m m m
f : FCOM 02.40.03
m m m
2. What is the position of the isolation valve when the ISOLATION VALVE
m m m m m m m m m m m
mswitch is in AUTO? m m m
(a) The isolation valve automatically modulates between open and closed,
m m m m m m m m
mdepending on pneumatic load. m m m
(b) It depends on the position of the APU bleed switch.
m m m m m m m m m
(c) The isolation valve is always closed.
m m m m m
(d) Open, if either engine BLEED air or air conditioning PACK switch is posi-
m m m m m m m m m m m m
tioned OFF.: What is the position of the isolation valve when the ISOLATION VALVE
m m m m m m m m m m m m m m
switch is in AUTO? m m m
(d) Open, if either engine BLEED air or air conditioning PACK switch is positioned O
m m m m m m m m m m m m m m
F.
Ref: FCOM 02.10.02
m m
3. When making a no engine bleed takeoff and an engine failure occurs, when
m m m m m m m m m m m m
mshould the engine BLEED air switch be positioned to ON?
m m m m m m m m m
(a) After passing through 2000 feet.
m m m m
(b) There is no altitude restriction. m m m m
(c) At not less than 400 feet and prior to 2000 feet.
m m m m m m m m m m
(d) When reaching 1500 feet or after obstacle clearance height h as been
m m m m m m m m m m
mattained.: When making a no engine bleed takeoff and an engine failure occurs,
m m m m m m m m m m m m
mwhen should the engine BLEED air switch be positioned to ON?
m m m m m m m m m m
(d) When reaching 1500 feet or after obstacle clearance height has been attained.
m m m m m m m m m m m m m
Ref : FCOM SP 2.5
m m m m
4. The maximum cabin differential pressure allowed by the two pressure relief
m m m m m m m m m m
mvalves is: m
1m/m
7
, B737 Questions - Air/Bleed/Pressurization Systems
m m m m
Studymonlinematmhttps://quizlet.com/_c7y2vm
(a) 7.8 psi. m
(b) 9.1 psi. m
(c) 7.1 psi. m
(d) 8.3 psi.: The maximum cabin differential pressure allowed by the two pressure
m m m m m m m m m m m m
relief valves is:
m m
2m/m
7
m m m m
Studymonlinematmhttps://quizlet.com/_c7y2vm
B737 Questions - Air/Bleed/Pressurization Systems Questions And Answers
1. The overboard exhaust valve:
m m m
(a) is normally open in flight and exhaust air is diffused to the lining of the
m m m m m m m m m m m m m m
mforward cargo compartment. m m
(b) remains closed if both pack switches are in high.
m m m m m m m m
(c) allows for increased ventilation in the smoke removal config uration.
m m m m m m m m
(d) remains closed on the ground and in flight with low different ial pressure.-
m m m m m m m m m m m
: The overboard exhaust valve:
m m m m
(c) allows for increased ventilation in the smoke removal configuration. Re
m m m m m m m m m m
f : FCOM 02.40.03
m m m
2. What is the position of the isolation valve when the ISOLATION VALVE
m m m m m m m m m m m
mswitch is in AUTO? m m m
(a) The isolation valve automatically modulates between open and closed,
m m m m m m m m
mdepending on pneumatic load. m m m
(b) It depends on the position of the APU bleed switch.
m m m m m m m m m
(c) The isolation valve is always closed.
m m m m m
(d) Open, if either engine BLEED air or air conditioning PACK switch is posi-
m m m m m m m m m m m m
tioned OFF.: What is the position of the isolation valve when the ISOLATION VALVE
m m m m m m m m m m m m m m
switch is in AUTO? m m m
(d) Open, if either engine BLEED air or air conditioning PACK switch is positioned O
m m m m m m m m m m m m m m
F.
Ref: FCOM 02.10.02
m m
3. When making a no engine bleed takeoff and an engine failure occurs, when
m m m m m m m m m m m m
mshould the engine BLEED air switch be positioned to ON?
m m m m m m m m m
(a) After passing through 2000 feet.
m m m m
(b) There is no altitude restriction. m m m m
(c) At not less than 400 feet and prior to 2000 feet.
m m m m m m m m m m
(d) When reaching 1500 feet or after obstacle clearance height h as been
m m m m m m m m m m
mattained.: When making a no engine bleed takeoff and an engine failure occurs,
m m m m m m m m m m m m
mwhen should the engine BLEED air switch be positioned to ON?
m m m m m m m m m m
(d) When reaching 1500 feet or after obstacle clearance height has been attained.
m m m m m m m m m m m m m
Ref : FCOM SP 2.5
m m m m
4. The maximum cabin differential pressure allowed by the two pressure relief
m m m m m m m m m m
mvalves is: m
1m/m
7
, B737 Questions - Air/Bleed/Pressurization Systems
m m m m
Studymonlinematmhttps://quizlet.com/_c7y2vm
(a) 7.8 psi. m
(b) 9.1 psi. m
(c) 7.1 psi. m
(d) 8.3 psi.: The maximum cabin differential pressure allowed by the two pressure
m m m m m m m m m m m m
relief valves is:
m m
2m/m
7