Endeavor CRJ Systems Workbook
UPDATED ACTUAL Questions and
CORRECT Answers
General Info - CORRECT ANSWER - The CL600-2C10 (CRJ 700) is a 69 seat regional
jet with an approximate range of 1700 NM.
The CL600-2D24 (CRJ 900) is a 76 seat regional jet with an approximate range of 2005 NM.
700 - CF34-8C (8C1/8C5B1) turbofan engines produce 12,600 pounds of normal takeoff thrust;
13,790 lbs. of thrust (APR) are available after an engine failure.
900 - CF34-8C5 turbofan engines produce 13,600 pounds of normal takeoff thrust; 14,510 lbs. of
thrust (APR) are available after an engine failure.
The tail requires the most clearance during a turn (CRJ 700).
The nose requires the most clearance during a turn (CRJ 900).
Both the forward and aft cargo bays are pressurized. Only the aft cargo bay is ventilated by
conditioned air.
The CRJ 700 has five emergency exits.
The CRJ 900 has seven emergency exits.
What is the minimum width required to make a 180 degree turn? CR7 / CR9 - CORRECT
ANSWER - 75' / 80'
What is the hazard area in front of the engine at idle thrust is the? CR7 / CR9 - CORRECT
ANSWER - Trailing edge / trailing edge
What is the hazard area in front of the engine at full thrust is the? CR7 / CR9 - CORRECT
ANSWER - Leading edge / leading edge
Which compartments on the CRJ-900 are pressurized? - CORRECT ANSWER - The
flight deck, passenger cabin, cargo, and avionics bay are pressurized.
,RVSM REQUIRED EQUPMENT LIST - CORRECT ANSWER - Autopilot MUST BE
OPERATIONAL
Altitude Alerting System MUST BE OPERATIONAL
Altitude Reporting Transponder ONE (1) MUST BE OPERATIONAL
Air Data Computer TWO (2) MUST BE OPERATIONAL
AIRCRAFT APPROACH CATEGORY
CR7 / CR9 - CORRECT ANSWER - When conducting instrument approach procedures,
always use CR7 (CAT C) CR9 (CAT D) to determine the applicable approach minimums.
STRUCTURAL WEIGHT LIMITATIONS (CR9) - CORRECT ANSWER - CRJ 900 LR
MAXIMUM RAMP WEIGHT (MRW) 85,000 lb
MAXIMUM TAKEOFF WEIGHT (MTOW) 84,500 lb
MAXIMUM LANDING WEIGHT (MLW) 75,100 lb
MAXIMUM ZERO FUEL WEIGHT (MZFW) 70,750 lb
MINIMUM FLIGHT WEIGHT 45,000 lb
STRUCTURAL WEIGHT LIMITATIONS (CR7) - CORRECT ANSWER - CRJ 700
MAXIMUM RAMP WEIGHT (MRW) 75,250 lb
MAXIMUM TAKEOFF WEIGHT (MTOW) 75,000 lb
MAXIMUM LANDING WEIGHT (MLW) 67,000 lb
MAXIMUM ZERO FUEL WEIGHT (MZFW) 62,300 lb
MINIMUM FLIGHT WEIGHT 42,000 lb
CARGO LOADING LIMITATIONS - CORRECT ANSWER - Aft 3,650 lb
Fwd CR7 1,000 lb
Fwd CR9 1,700 lb
,RVSM AIRSPEED LIMITATIONS
The maximum cruise Mach number during flight in RVSM air-space is - CORRECT
ANSWER - CR9 - M .82
CR7 - M .83
AIRSPEED LIMITATIONS
Max Vmo / Mmo: - CORRECT ANSWER - 335 / .85
Maximum airspeed for turbulence penetration - CORRECT ANSWER - 280 or .75
whichever is lower.
MAXIMUM AIRPORT PRESSSURE ALTITUDE FOR TAKEOFF & LANDING - CORRECT
ANSWER - Takeoff: 8000 ft.
Landing: 8000 ft.
Maximum Operating Altitude - CORRECT ANSWER - 41,000 ft.
GROUND AMBIENT AIR TEMPERATURE LIMITATIONS
Maximum ambient air temperature approved for takeoff and landing - CORRECT
ANSWER - ISA + 35 C
Minimum ambient air temperature approved for takeoff: - CORRECT ANSWER - -40 C
Maximum tailwind component for takeoff and landing - CORRECT ANSWER - 10 kts
Maximum crosswind component for takeoff and landing on a DRY runway (Company) -
CORRECT ANSWER - CR7 | CR9
T/O 28 | 35
LDG 30 | 32
, Maximum allowable crosswind component for takeoff and landing on a WET runway
(Company) - CORRECT ANSWER - 27 kts
Maximum allowable crosswind component for takeoff and landing on a runway when the
braking action is "FAIR". (Company) - CORRECT ANSWER - 20 kts
Maximum allowable crosswind component for takeoff and landing on a runway when the
braking action is "POOR". (Company) - CORRECT ANSWER - 15 kts
Maximum allowable crosswind component for takeoff and landing on a dry runway for a
crewmember on high minimums status in the CRJ-900 (Company) - CORRECT
ANSWER - 25 PIC
15 SIC
CARGO AIRPORT LIMITATIONS
Flight must be within __ minutes of a ______________ if cargo is carried in either cargo
compartment. - CORRECT ANSWER - 60 minutes of a suitable airport
REVERSE TAXI OPERATIONS
Using the thrust reversers to back-up the airplane, commonly referred to as Reverse Taxi
Operations or Power-back, is - CORRECT ANSWER - strictly prohibited in all situations.
Tire Limit Speed CR7/CR9 - CORRECT ANSWER - CR7 - 182 kts / CR9 - 195 kts
DOORS - CORRECT ANSWER - All door indications on the DOORS synoptic page
represent doors leading to the pressure vessel.
The Crew Escape Hatch in the Flight Deck is the only door, leading to the pressure vessel, which
is not depicted on the DOORS synoptic page.
Except for the passenger door, all doors are either plug or semi plug type doors.
The Flight Deck door can be removed from its hinges during an emergency.
UPDATED ACTUAL Questions and
CORRECT Answers
General Info - CORRECT ANSWER - The CL600-2C10 (CRJ 700) is a 69 seat regional
jet with an approximate range of 1700 NM.
The CL600-2D24 (CRJ 900) is a 76 seat regional jet with an approximate range of 2005 NM.
700 - CF34-8C (8C1/8C5B1) turbofan engines produce 12,600 pounds of normal takeoff thrust;
13,790 lbs. of thrust (APR) are available after an engine failure.
900 - CF34-8C5 turbofan engines produce 13,600 pounds of normal takeoff thrust; 14,510 lbs. of
thrust (APR) are available after an engine failure.
The tail requires the most clearance during a turn (CRJ 700).
The nose requires the most clearance during a turn (CRJ 900).
Both the forward and aft cargo bays are pressurized. Only the aft cargo bay is ventilated by
conditioned air.
The CRJ 700 has five emergency exits.
The CRJ 900 has seven emergency exits.
What is the minimum width required to make a 180 degree turn? CR7 / CR9 - CORRECT
ANSWER - 75' / 80'
What is the hazard area in front of the engine at idle thrust is the? CR7 / CR9 - CORRECT
ANSWER - Trailing edge / trailing edge
What is the hazard area in front of the engine at full thrust is the? CR7 / CR9 - CORRECT
ANSWER - Leading edge / leading edge
Which compartments on the CRJ-900 are pressurized? - CORRECT ANSWER - The
flight deck, passenger cabin, cargo, and avionics bay are pressurized.
,RVSM REQUIRED EQUPMENT LIST - CORRECT ANSWER - Autopilot MUST BE
OPERATIONAL
Altitude Alerting System MUST BE OPERATIONAL
Altitude Reporting Transponder ONE (1) MUST BE OPERATIONAL
Air Data Computer TWO (2) MUST BE OPERATIONAL
AIRCRAFT APPROACH CATEGORY
CR7 / CR9 - CORRECT ANSWER - When conducting instrument approach procedures,
always use CR7 (CAT C) CR9 (CAT D) to determine the applicable approach minimums.
STRUCTURAL WEIGHT LIMITATIONS (CR9) - CORRECT ANSWER - CRJ 900 LR
MAXIMUM RAMP WEIGHT (MRW) 85,000 lb
MAXIMUM TAKEOFF WEIGHT (MTOW) 84,500 lb
MAXIMUM LANDING WEIGHT (MLW) 75,100 lb
MAXIMUM ZERO FUEL WEIGHT (MZFW) 70,750 lb
MINIMUM FLIGHT WEIGHT 45,000 lb
STRUCTURAL WEIGHT LIMITATIONS (CR7) - CORRECT ANSWER - CRJ 700
MAXIMUM RAMP WEIGHT (MRW) 75,250 lb
MAXIMUM TAKEOFF WEIGHT (MTOW) 75,000 lb
MAXIMUM LANDING WEIGHT (MLW) 67,000 lb
MAXIMUM ZERO FUEL WEIGHT (MZFW) 62,300 lb
MINIMUM FLIGHT WEIGHT 42,000 lb
CARGO LOADING LIMITATIONS - CORRECT ANSWER - Aft 3,650 lb
Fwd CR7 1,000 lb
Fwd CR9 1,700 lb
,RVSM AIRSPEED LIMITATIONS
The maximum cruise Mach number during flight in RVSM air-space is - CORRECT
ANSWER - CR9 - M .82
CR7 - M .83
AIRSPEED LIMITATIONS
Max Vmo / Mmo: - CORRECT ANSWER - 335 / .85
Maximum airspeed for turbulence penetration - CORRECT ANSWER - 280 or .75
whichever is lower.
MAXIMUM AIRPORT PRESSSURE ALTITUDE FOR TAKEOFF & LANDING - CORRECT
ANSWER - Takeoff: 8000 ft.
Landing: 8000 ft.
Maximum Operating Altitude - CORRECT ANSWER - 41,000 ft.
GROUND AMBIENT AIR TEMPERATURE LIMITATIONS
Maximum ambient air temperature approved for takeoff and landing - CORRECT
ANSWER - ISA + 35 C
Minimum ambient air temperature approved for takeoff: - CORRECT ANSWER - -40 C
Maximum tailwind component for takeoff and landing - CORRECT ANSWER - 10 kts
Maximum crosswind component for takeoff and landing on a DRY runway (Company) -
CORRECT ANSWER - CR7 | CR9
T/O 28 | 35
LDG 30 | 32
, Maximum allowable crosswind component for takeoff and landing on a WET runway
(Company) - CORRECT ANSWER - 27 kts
Maximum allowable crosswind component for takeoff and landing on a runway when the
braking action is "FAIR". (Company) - CORRECT ANSWER - 20 kts
Maximum allowable crosswind component for takeoff and landing on a runway when the
braking action is "POOR". (Company) - CORRECT ANSWER - 15 kts
Maximum allowable crosswind component for takeoff and landing on a dry runway for a
crewmember on high minimums status in the CRJ-900 (Company) - CORRECT
ANSWER - 25 PIC
15 SIC
CARGO AIRPORT LIMITATIONS
Flight must be within __ minutes of a ______________ if cargo is carried in either cargo
compartment. - CORRECT ANSWER - 60 minutes of a suitable airport
REVERSE TAXI OPERATIONS
Using the thrust reversers to back-up the airplane, commonly referred to as Reverse Taxi
Operations or Power-back, is - CORRECT ANSWER - strictly prohibited in all situations.
Tire Limit Speed CR7/CR9 - CORRECT ANSWER - CR7 - 182 kts / CR9 - 195 kts
DOORS - CORRECT ANSWER - All door indications on the DOORS synoptic page
represent doors leading to the pressure vessel.
The Crew Escape Hatch in the Flight Deck is the only door, leading to the pressure vessel, which
is not depicted on the DOORS synoptic page.
Except for the passenger door, all doors are either plug or semi plug type doors.
The Flight Deck door can be removed from its hinges during an emergency.
