Use LEFT and RIGHT arrow keys to navigate between flashcards;
Use UP and DOWN arrow keys to flip the card;
H to show hint;
A reads text to speech;
115 Cards in this Set
- Front
- Back
Max Taxi/Ramp weight? |
82,750 |
|
Max Takeoff weight? |
82,500 |
|
Max Landing Weight? |
73,500 |
|
Max Zero Fuel Weight? |
70,000 |
|
Min Flight Weight? |
45,000 |
|
Max Total Aft Cargo Compartment capacity? |
4,375 |
|
Max Total Fwd Cargo Compartment capacity? |
850 |
|
Max Total Center Cargo Compartment Capacity? |
850 |
|
Max Pressure Refueling Fuel capacity total? |
19,594 |
|
Max Pressure Refueling capacity Mains? |
7,492 |
|
Max Pressure Refueling capacity Center? |
4,610 |
|
Max Gravity Refueling capacity Total? |
14,810 |
|
Max Gravity Refueling capacity Mains? |
7,405 |
|
Max Gravity Refueling capacity Center? |
Cannot gravity refuel center tank. |
|
What is the wingspan? |
76' 3" |
|
What is the height of the Tail? |
24' 1" |
|
What is the minimum taxiway or runway surface width for a 180 degree turn? |
126' 5" |
|
What is the length? |
118' 11" |
|
What is the width of the Horizontal Stabilizer? |
28' 4" |
|
What is the distance from Main to Main? |
13' 6" |
|
What is VMO? |
335 KIAS |
|
What is Max Landing Gear Extended Speed (VLE) ? |
220 KIAS |
|
What is MMO? |
.85 Mach |
|
What is MMO during flight in RVSM airspace? |
.82 Mach |
|
Flap Extension Speed 1° ? |
230 KIAS |
|
Flap Extension Speed 8°? |
230 KIAS |
|
Flap Extension Speed 20° ? |
220 KIAS |
|
Flap Extension Speed 30° ? |
185 KIAS |
|
Flap Extension Speed 45° ? |
170 KIAS |
|
What is Max Landing Gear Operating Speed for extension (VLO) ? |
220 KIAS |
|
What is Max Landing Gear Operating Speed for retraction (VLO) ? |
200 KIAS |
|
What is Max Turbulence Penetration Speed? |
280 KIAS/.75 Mach |
|
What is Max Windshield Wiper Operation Speed ? |
250 KIAS |
|
What is Max Operating Altitude |
41,000 ft. |
|
What is Max airport pressure altitude for takeoff and landing? |
10,000 ft. |
|
CRJ 900 max demonstrated crosswind for takeoff and Landing? |
35 knots takeoff 32 knots landing 15 knots on a slippery runway |
|
CRJ 700 max demonstrated crosswind for takeoff and Landing?
|
28 knots for takeoff 30 for landing 15 knots on a slippery runway |
|
Max tailwind approved for takeoff and landing?
|
10 knots
|
|
Max tire speed?
|
195 KGS
|
|
Max altitude for extending flaps?
|
15,000 ft.
|
|
Max runway slopes for Takeoff and Landing are?
|
+2% uphill and-2% downhill
|
|
What type of flotation equipment is provided for the passengers?
|
Seat Cushions
|
|
What type of flotation equipment is provided for the flight attendants?
|
Life vests located near the FA jumpseat
|
|
How many life vests are on the flight deck?
|
(3) One under captains and FO's seat. One next to the jump seat. |
|
What is the minimum crew oxygen system pressure for dispatch?
|
Listed on a chart in the CFM, Chapter 4 (Cockpit Safety Inspection)
|
|
Where are the crew goggles located?
|
Either part of the oxygen mask or under oxygen mask.
|
|
How many sealed first aid kits and enhanced emergency medical kits must be on board?
|
One of each.
|
|
In what rows are the extra passenger oxygen masks located?
|
All rows on the right side.
|
|
Where are the 2 flight deck flashlights located?
|
One behind each seat.
|
|
What is the power source for the emergency lighting system?
|
CRJ 900 - 5 battery packs. CRJ 700 - 4 battery packs. |
|
Can the flight attendant select the emergency lights on, if the flight deck switch is off?
|
Yes
|
|
How long will the emergency lights illuminate if the battery packs are fully charged?
|
Approx. 10 minutes.
|
|
Where are the smoke detectors located?
|
1 in the fwd lavatory. 1 in the aft lavatory. 2 in the aft cargo compartment. 3 in the fwd cargo compartment. |
|
What conditions would cause a takeoff configuration warning? (PASSFAR) |
Parking brake on. Autopilot on. Spoilers extended. Stab trim out of green range. Flaps not 8 or 20. Aileron trim out of green range. Rudder trim out of the green range. |
|
The 115V External Power Receptacle is located?
|
Forward right nose area.
|
|
Where is the main battery located?
|
Nose compartment.
|
|
Where is the APU battery located?
|
Aft equipment bay
|
|
Where is the crew oxygen bottle located?
|
Forward of the passenger door.
|
|
What is indicated if the green oxygen blowout disc is blown?
|
Excessive pressure has occurred.
|
|
Will the flight deck P.A. override the flight attendant P.A.?
|
Yes
|
|
How should we contact the flight attendant in an emergency?
|
Turn the audio panel selector knob to PA, push the EMER call switchlight to generate three high/low chimes and a flashing red light on the FA's overhead panel.
|
|
What indication do we get if the flight attendant is calling the flight deck because of an emergency in the cabin?
|
We hear one high/low chime and the EMER call switchlight will be flashing.
|
|
How do we know if the company is trying to contact us?
|
An ACARS message or "SELCAL, SELCAL* voice aural and a SELCAL advisory EICAS message
|
|
How many Air Data Computers (ADC) are installed?
|
Two
|
|
How many AHRS or IRS computers are installed?
|
Two
|
|
In MAG mode, how long does it take the AHRS system to initialize?
|
30 to 70 seconds |
|
In DG mode, how long does it take the AHRS system to initialize?
|
10 to 11 minutes
|
|
From which source do the captains flight instruments receive AHRS information?
|
AHRS 1 or IRS 1
|
|
From which source do the first officers flight instruments receive AHRS information?
|
AHRS 2 or IRS 2
|
|
From which source do the captains flight instruments receive pitot/static information?
|
System #1 Pitot/static tube on left side of nose. |
|
From which source do the first officers flight instruments receive pitot/static information?
|
System #2 Pitot/static tube on right side of nose. |
|
From which source does the integrated standby instrument receive pitot/static information?
|
System 3 Standby pitot under captains side window 2 alternate static ports on left and right |
|
Where is the TAT probe located?
|
Under FO's side window.
|
|
What is the definition of Total Air Temperature?
|
The temperature of the air corrected for compressibility and friction caused by high speed.
|
|
On the ground with the probe heat ON, which probes are heated?
|
All pitot probes are heated half way. All others are fully heated except for the TAT probe which is not heated on the ground. |
|
In flight which probes are heated
|
All are fully heated regardless of probe heat switch position.
|
|
Is there a LOC and GS indication on the standby attitude indicator?
|
Yes, referencing NAV 1.
|
|
When and where will the radio altimeter information be displayed?
|
0 to 2500 AGL. Indicated in green below the altitude tape.
|
|
What does the speed trend vector indicate?
|
Predicted airspeed in 10 seconds if no changes are made.
|
|
When and where will the MACH readout appear?
|
Appears when accelerating through .45 Mach. Disappears when decelerating through 0.4 Mach. Appears just above the airspeed tape in white.
|
|
What does the green line on the airspeed tape indicate?
|
1.27 Vs based on current configuration. Not accurate at high altitudes.
|
|
Where is the slip and skid indicator located?
|
A rectangle located just under the sky pointer.
|
|
How many flight directors are installed?
|
Two
|
|
How many autopilots are installed?
|
One
|
|
What does the autopilot follow when engaged?
|
The selected side flight director which defaults to the captains FD. The XFER button must be selected on the flight control panel to transfer to the FO's FD.
|
|
What happens when TOGA is pushed on the ground?
|
TO lateral mode. TO vertical mode. FMS aligns the aircraft at the end of the runway indicated on the legs page. Autopilot disengages.
|
|
What does the TO lateral mode do?
|
On the ground it generates a wings level command. After takeoff, it generates a heading hold command with a 5 degree bank limit using the heading existing at takeoff.
|
|
What does the TO vertical mode do?
|
Generates an optimized pitch up attitude for takeoff.
|
|
What happens when TOGA is pushed in flight?
|
GA lateral mode. Ga vertical mode. Missed approach procedure depiction appears on the MFD if instrument approach procedure selected in FMS. Autopilot disengages.
|
|
What does GA lateral mode do?
|
Same as TO lateral mode and follows heading flown when TOGA was pushed.
|
|
What does GA vertical mode do?
|
Generates a 10 degree pitch up attitude.
|
|
After takeoff or go-around, the autopilot must not be engaged below what altitude?
|
600 ft. AGL
|
|
During visual and non-precision approaches, the autopilot must be disengaged by?
|
400 ft. AGL
|
|
During precision approaches, the autopilot must be disengaged by?
|
80 ft. AGL
|
|
During single-engine precision approaches, the autopilot must be disengaged by?
|
110 ft. AGL CRJ 900 80 ft. AGL CRJ 700 |
|
When will the autopilot automatically disconnect?
|
AP/SP DISC button pushed. AP ENG button on FCP pushed. AP DISC switch bar pushed down. Stick shaker activated. TOGA buttons pressed. Stab trim manually operated. Windshear warning (after 2 seconds). Excessive attitude. One or both FCC's fail. Both yaw dampers disc or fail.
|
|
Max permissible load on the APU generator?
|
40 KVA
|
|
Max altitude for APU starting?
|
37,000 ft.
|
|
Max altitude for APU operation?
|
41,000 ft.
|
|
Max altitude for APU bleed extraction?
|
25,000 ft.
|
|
Max speed with APU door open?
|
220 KIAS if APU not operating. No speed limitation if APU is operating.
|
|
What battery voltage is required before starting APU?
|
22 volts on both batteries.
|
|
What does the main battery power during an APU start?
|
APU ECU
|
|
What does the APU battery power during an APU start?
|
Cranking of the 28 VDC start motor
|
|
When will the avail light switch illuminate?
|
99% RPM plus 2 seconds.
|
|
What is the CRJ 900 power plant model number?
|
General Electric CF34-8C5
|
|
What is the CRJ 700 power plant model number?
|
General Electric CF34-8C1 or General Electric CF34-8C5B1 |
|
What is the thrust rating without APR / with APR?
|
13,560 lbs. / 14, 750 lbs.
|
|
What is the Max ambient air temperature for takeoff and landing?
|
ISA +35 C |
|
What is the Min ambient air temperature for takeoff and landing?
|
-40 C
|
|
What is the Max altitude for a windmill start?
|
21,000 ft. MSL
|
|
Max engine to engine N2 split at ground idle power?
|
2%
|
|
How much of the thrust is produced by core air?
|
Approximately 20%
|
|
How much thrust is produced by by-pass air?
|
Approximately 80%
|
|
How many stages of compression do we have?
|
The engine is equipped with a 10 stage axial flow compressor.
|