PSA AIRLINES FLIGHT ANSWERS AND QUESTIONS
SET A+
✔✔PSA CRJ 701: Permissible AC Electrical System Loads - ✔✔PSA CRJ 701:
Permissible AC Electrical System Loads
• 0 to 41,000 ft. 40 kVA from Main Generator and APU Generator.
✔✔PSA CRJ 701: Permissible DC Electrical System Loads. - ✔✔PSA CRJ
701:Permissible DC Electrical System Loads. Maximum continuous load on each TRU
is 120 amps.
✔✔To protect the flight compartment CRT displays, the maximum permissible time for
ground operations with DC power only is __ minutes. - ✔✔To protect the flight
compartment CRT displays, the maximum permissible time for ground operations with
DC power only is 5 minutes.
✔✔Enroute use of slats/flaps is permissible. T/F - ✔✔False, Enroute use of slats/flaps is
prohibited.
✔✔*Minimum altitude for flight spoiler deployment: - ✔✔1000 ft AGL
✔✔**To ensure adequate maneuver margins, flight spoilers must not be extended
inflight at airspeeds below the recommended reference speed plus __ KIAS. - ✔✔17
KIAS.
✔✔**The taxi lights must be switched OFF whenever the airplane is stationary in
excess of __ minutes. - ✔✔10 minutes
✔✔**Minimum brake cooling time is ___ minutes, and all BTMS indicators must be
green and are ___ _________. - ✔✔15
not increasing
✔✔**Maximum 90 degree crosswind landing for Category II Approach - ✔✔**15 knots
, ✔✔**Maximum headwind for landing from a Category II Approach - ✔✔**17 knots
✔✔Red - ✔✔Maximum and minimum limitations
✔✔Amber - ✔✔Caution Range
✔✔Green - ✔✔Normal Operating Range
✔✔**ITT must be BELOW____ °C or less for all ground starts - ✔✔120
✔✔**Maximum Altitude to use slats/flaps is probhibited - ✔✔15,000
✔✔RVSM Required Equipement List
Autopilot
Altitude Alert System
Altitude Reporting Transponder 2
Air Data computer 2 - ✔✔Autopilot must be operational
Altitude Alert System must be operational
Altitude Reporting Transponder-one must be operational
Air Data computer- tow must be operational
✔✔APU Bleed Air- Engine start during ground operation - ✔✔Each engine may be
started using the APU as a bleed air source
✔✔ Minimum flight crew - ✔✔One Captain and one First Officer
✔✔Maximum 90 degree crosswind for takeoff and landing - ✔✔27
✔✔Maximum 90 degree crosswind from a Category II approach - ✔✔15
✔✔Maximum headwind for landing from a Category II approach - ✔✔16
✔✔Maximum direct tailwind for takeoff and landing - ✔✔10
✔✔Maximum runway slope approved for takeoff and landing - ✔✔+2.0% (uphill) -2.0%
(downhill)
✔✔Maximum operating altitude PSA CRJ 701 and 900 - ✔✔41,000
✔✔Maximum pressure altitude for takeoff and landing - ✔✔8,000ft
✔✔Maximum ambient temperature for takeoff and landing - ✔✔ISA +40C
SET A+
✔✔PSA CRJ 701: Permissible AC Electrical System Loads - ✔✔PSA CRJ 701:
Permissible AC Electrical System Loads
• 0 to 41,000 ft. 40 kVA from Main Generator and APU Generator.
✔✔PSA CRJ 701: Permissible DC Electrical System Loads. - ✔✔PSA CRJ
701:Permissible DC Electrical System Loads. Maximum continuous load on each TRU
is 120 amps.
✔✔To protect the flight compartment CRT displays, the maximum permissible time for
ground operations with DC power only is __ minutes. - ✔✔To protect the flight
compartment CRT displays, the maximum permissible time for ground operations with
DC power only is 5 minutes.
✔✔Enroute use of slats/flaps is permissible. T/F - ✔✔False, Enroute use of slats/flaps is
prohibited.
✔✔*Minimum altitude for flight spoiler deployment: - ✔✔1000 ft AGL
✔✔**To ensure adequate maneuver margins, flight spoilers must not be extended
inflight at airspeeds below the recommended reference speed plus __ KIAS. - ✔✔17
KIAS.
✔✔**The taxi lights must be switched OFF whenever the airplane is stationary in
excess of __ minutes. - ✔✔10 minutes
✔✔**Minimum brake cooling time is ___ minutes, and all BTMS indicators must be
green and are ___ _________. - ✔✔15
not increasing
✔✔**Maximum 90 degree crosswind landing for Category II Approach - ✔✔**15 knots
, ✔✔**Maximum headwind for landing from a Category II Approach - ✔✔**17 knots
✔✔Red - ✔✔Maximum and minimum limitations
✔✔Amber - ✔✔Caution Range
✔✔Green - ✔✔Normal Operating Range
✔✔**ITT must be BELOW____ °C or less for all ground starts - ✔✔120
✔✔**Maximum Altitude to use slats/flaps is probhibited - ✔✔15,000
✔✔RVSM Required Equipement List
Autopilot
Altitude Alert System
Altitude Reporting Transponder 2
Air Data computer 2 - ✔✔Autopilot must be operational
Altitude Alert System must be operational
Altitude Reporting Transponder-one must be operational
Air Data computer- tow must be operational
✔✔APU Bleed Air- Engine start during ground operation - ✔✔Each engine may be
started using the APU as a bleed air source
✔✔ Minimum flight crew - ✔✔One Captain and one First Officer
✔✔Maximum 90 degree crosswind for takeoff and landing - ✔✔27
✔✔Maximum 90 degree crosswind from a Category II approach - ✔✔15
✔✔Maximum headwind for landing from a Category II approach - ✔✔16
✔✔Maximum direct tailwind for takeoff and landing - ✔✔10
✔✔Maximum runway slope approved for takeoff and landing - ✔✔+2.0% (uphill) -2.0%
(downhill)
✔✔Maximum operating altitude PSA CRJ 701 and 900 - ✔✔41,000
✔✔Maximum pressure altitude for takeoff and landing - ✔✔8,000ft
✔✔Maximum ambient temperature for takeoff and landing - ✔✔ISA +40C
