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104 Cards in this Set

  • Front
  • Back
Max. Ramp Weight (MRW)
53,250 lbs
Max. Takeoff Weight (MTOW)
53,000 lbs
Max. Landing Weight (MLW)
47,000 lbs
Max. Zero Fuel Weight (MZFW)
44,000 lbs
Max. Airport Pres. Alt. for Takeoff/Landing
10,000 ft
Max Operating Alt.
41,000 ft
Max Ambient Air Temp for Takeoff/Landing
ISA +35°C
Min Ambient Temp for Takeoff/Landing
-40°C
When to use Cowl Anti-Ice (Ground)
OAT <=10 degrees Celsius with precipitation/accumulation on plane or runway
When to use Cowl Anti-Ice (Air)
TAT <= 10°C and vis. moisture, except < -40°C
OR In icing conditions
OR with ICE annunciation
When to use Wing Anti-Ice (Ground)
OAT <=5 degrees Celsius with precipitation/accumulation on plane or runway
If type 2 or 4 fluid has been applied to wing, delay anti-ice use until just prior to takeoff thrust application
When to use Wing Anti-Ice (Air)
TAT <= 10°C and vis. moisture
OR ICE annunciation
OR Icing conditions and airspeed < 230 KIAS
What to do when Super-Cooled Large Droplet Icing is detected
SLD indicated by ice accretion on flight compartment side windows.
Wing and Cowl anti-ice ON.
Leave icing conditions immediately
Can the aircraft take off in icing conditions?
Yes. However, takeoff prohibited with frost, ice, snow, or slush adhering to critical/control surfaces.
Maximum allowable Runway Slope
+/- 2%
Max. Tailwind for Takeoff/Landing
10 kts
Min. Flight Crew
1 pilot, 1 copilot
Color Logic
RED - Warning - Limits or failure reached
AMBER - Caution Range - near limits
GREEN - Normal Op Range
WHITE - Status message
Airplane Cold Soak Procedures
Before first flight of day, and aircraft is cold soaked for more than 8 hours,
1) Engines motored for 60 seconds and fan rotation verified before start initiated.
2) Thrust reversers must be actuated until deploy/stow cycles are < 5 seconds.
When must Continuous Engine Ignition be on? (2 Takeoff, 2 Weather)
Must be used:
Takeoff on contaminated rwy.
Takeoff with crosswind comp. > 10 kts.
Mod. or heavier rain or turbulence.
In vicinity of thunderstorms.
Max. Fuel Imbalance (L/R)
800 lbs
Fuel - Max. Center tank weight for takeoff
500 lbs with less than 4,400 lbs in each wing
Fuel - Go Around Fuel Requirement
450 lbs per tank with airplane level, assuming max 10° nose up.
APU Start Delays (On Batteries) (Ground/Air)
1st - starter energized for 30 sec.
2nd - 30 sec. - 20 min. off
3rd - 30 sec.
4th - 30 sec. - 40 min. off

2 minute delay between attempts for cooling/drainage.
Maximum altitude to pull APU Bleed Air
15,000 ft
What are the restrictions for using APU Bleed Air for Engine Start on ground?
None. But operating engine N2 cannot exceed 70%.
When can APU Bleed Air be used for Engine Start in Air
Not permitted for Single-engine ops.
Permitted for Double-engine failure below 13,000 ft.
Maximum APU usage altitudes (Operating, APU Start, PACKs, Engine Start)
37,000 - Operating
30,000 - APU Start
15,000 - PACKs
13,000 - Engine Start
What are the engine stabilization delays (Takeoff/Landing)?
Prior to Takeoff: 2 minutes
Prior to Shutdown: 2 minutes at IDLE. Taxi time below 70% N2 is counted.
Max. Takeoff Wind Speed - Total
60 kts
Max. Takeoff Headwind Component
55 kts
Crosswind Limitations (Max. Demo, Wet Rwy, Contaminated Rwy, Low-Time Capt.)
Max Demo - 27 kts
Wet Runways - 17 kts
Contaminated - 15 kts
Low-time Capt - 27 kts
Contaminated means braking less than Good (MU value < 40)
Low-time Capt is < 100 hrs PIC in similar craft
What condition does 10th Stage Bleed Air have to be in for Takeoff/Landing
Closed if cowl and/or wing anti-ice is on.
Max. Operation Time on DC Power (Ground)
5 min. for CRT display protection (lack of cooling)
Can a circuit breaker be reset in Flight?
Permitted only in compliance with OM/QRH or if PIC deems necessary for safe ops.
Permitted Flight Spoiler Usage (airspeed, altitude, and configuration)
Not permitted:
Below recommended flap reference speed plus 17 KIAS
Below 800 ft AGL
Flaps > 30°
When must both stall protection switches be on?
All phases of flight.
Takeoff not permitted when what messages are displayed? (Light/Gauge/EICAS)
THRUST REVERSER UNLK light
REV icon on N1 gauge
L or R REV UNLOCKED caution message
Can thrust reverse be used for pre-flight when airplane is stationary?
Yes, IDLE only
Can thrust reverse be used for taxi?
No, used for taxi only in emergency.
Min. BTMS Brake Cooling Period Between Landing/RTO and Next Takeoff
15 minutes
V(LE)
Landing gear extension speed (250KIAS)
V(LR)
Landing gear retraction speed (200KIAS)
V(LO)
Operations with gear extended (250KIAS)
V(FE8)
8 degree flap extension speed (215KIAS)
V(FE20)
20 degree flap extension speed (215KIAS)
V (FE30)
30 degree flap extension speed (185KIAS)
V (FE45)
45 degree flap extension speed (170KIAS)
V(ADG)
max speed for Air Drive Generator operation
335KTS - no more than 4 minutes
330KTS - no more than 12 minutes
250KTS - max for indefinite use
V(WWIPE)
Max speed for windshield wiper use (220KIAS)
Maximum tire rotation speed
182 KTS
Turbulent air penetration speed
280KIAS =or= .75 Mach
For which operations, altitudes, and ILS procedures may autopilot be engaged?
Operations - Takeoff and Landing
Altitudes - 600ft above takeoff altitude
ILS Procedures - 80ft AGL during precision approach, 400ft AGL during non-precision approach, or 50ft below MDA, whichever is applicable and greatest
Maximum runway slope
2%
Maximum TO/L Tailwind?
10KTS
How far may flights be conducted from the nearest suitable airport, in minutes?
45 minutes
Give examples of Performance Operation Weight Limitations
"why did you hit that tree?"
climb performance
available runway length
tire speed limits
brake temperatures
braking limits
obstacle clearance
enroute landing weight
max TO/L weights
runway altitude
tailwind
Maximum cargo load weight
3,500lbs properly loaded
Minimum crew supplemental oxygen, in PSI?
1410PSI. Must be checked before each flight for low pressure. EICAS amber caution "OXY LO PRESS" activates when below 1410PSI. Approval for dispatch at lower oxygen pressures must be received directly from maintenance.
Maximum fuel (per tank and total, pressure and gravity)
Left Main (4,760P; 4,488G)
Right Main (4,760P; 4,488G)
Center (4,998P; 4,930G)
TOTAL (14,518P; 13,906G)
Maximum center tank weight with wings empty
500lbs max center tank weight, unless wing tanks are 4,400lbs or greater (each).
Maximum wing tank fuel quantity imbalance
800lbs
What are the fuel and attitude maximums for go-around?
450lbs per wing (900lbs total)
10 degree nose-up attitude
Minimum fuel temps
(takeoff - fuel feed and bulkhead)
(in flight - bulkhead only)
Takeoff (fuel feed) - 5 degrees Celsius minimum
Takeoff (bulkhead) - minus 29 degrees Celsius
In Flight (bulkhead) - minus 40 degrees Celsius
G-Force load limits
(with and without flaps)
0 degrees flaps - minus 1 to +2.5 G's
Flaps greater than 0 degrees - 0 to 2.0 G's
TCAS
(define)
(when does it supersede ATC)
(when does the pilot ignore RA's)
TCAS - Traffic Collision Avoidance System
TCAS supersedes ATC when TCAS recommends a change in course, called a Resolution Advisory (RA).
Exceptions to RA's include: when engines failed; obvious TCAS errors; etc.
How does the pilot round the MDA when selecting it?
up to the nearest 10-foot increment
Lights
When are the red strobe lights used?
When CANT you use Taxi lights?
Red strobes - used for ground recognition only, not anti-collision
Taxi lights - must be off if stationary for more than ten minutes
Minimum Crew
1 PIlot, 1 copilot
When must seats be locked?
during TO/L
Maximum air-stair door capacity
4 persons or 1,000lbs on stairs at any given time
How long must brakes be cooled after a landing or rejected takeoff?
15 minutes, plus BTMS-06 (Brake Temperature Monitoring System condition #6) maximum brake temperature equivalent. All temperatures above BTMS-05 must comply with Vol. 1 Quick Reference Handbook Perf.04.
Define: MEL
Minimum Equipment List (minimum airworthiness equipment)
Define: QRH
Quick Reference Handbook (simplified operations standards)
Define: CDL
Configuration Deviation List (acceptable loss of non-airworthy items)
Define: STABTRIM
Stabilator or Stabilizer trim (trim for porpoising motion trim.
What is the maximum speed with STABTRIM inoperative?
250KIAS or 0.7 Mach if inoperative
EICAS
Engine Indicating and Crew Alert System (provides information to crew regarding status of numerous flight-related systems)
Who/What requires compliance with the Aircraft Flight Manual (AFM)?
FAR's (Federal Aviation Regulations)
What fuel does the CRJ use?
Jet-A (other types or any additives require maintenance approval)
How long must cold-soaked engines be motored?
60 seconds with verified fan rotation
When is a CRJ-200 considered cold-soaked?
When in an ambient temperature of minus 30 degrees Celsius or less for 8 hours or more.
Where can you readily find V-speed data?
V-speed data book on flight desk
If data book is unavailable, QRH, which may also be used to find appropriate thrust settings
CRJ-200 is certified for transport in what conditions? (4)
Day/Night
VFR/IFR
Icing
Ditching
Define: EFIS
Electronic Flight Information System
Define: APR
(What percentage increase in engine performance can be expected when using APR?)
APR - Automatic Performance Reserve (2%)
What is the maximum acceptable ITT?
900 degrees Celsius
How long must engines run prior to takeoff? Why?
2 minutes - heat up engines and equalize that temperature for metal warping
How long must engines be at IDLE prior to shutdown? Why?
2 minutes - dissipate heat and decrease and stabilize internal operating temperatures. NOTE: Taxi time below 70% N2 may be considered part of the shutdown delay period.
What is the delay between multiple failed starts? How long can the starter run each time?
After start #1 - 10 seconds off
After start #2 - 10 seconds off
After start #3 or more - 5 minutes off
Starter may not run more than 60 seconds for any reason.
What is the maximum ITT for starts on ground or in-flight?
ITT <= 120 for ground starts
ITT <= 90 for in-flight starts
What is the maximum indicated airspeed and altitude for starter-assisted cross-bleed air engine starts?
300KIAS and 21,000ft
What is the maximum continuous oil temp?
What is the maximum permissible oil temp?
What is the maximum continuous oil pressure?
155 and
163 degrees Celsius, respectively
115 PSI
Can thrust reversers be used in flight? What about to expedite touch-and-gos?
No. They are approved for ground use, full stop landings only.
What EICAS message appears when the thrust reversers are unlocked?
"L... or "R REV UNLOCKED" cautionary message
What is the minimum speed for the use of thrust reversers?
Thrust reversers may be used at full stop.
However, reverse throttle must be reduced to idle (<=30% N2) before decelerating through 60KIAS
What is the required delay between APU BATTERY start attempts? How long can the starter be energized? How does this compare to DC ground power starts?
After the second try, 20 minute delay. After fourth try, 40 minute delay. The starter cannot be energized for more than 30 seconds per start. On ground, all the same delays apply, and the starter cannot be energized for more than 15 seconds per start.
What are the maximum pressure differentials for cabin pressurization versus outside air pressure? What is the difference between positive and negative pressure differential?
Positive differential - 8.7 PSI
Negative differential - -0.5 PSI
A positive pressure differential is when the aircraft has greater pressure than the outside air. Negative differential is the exact opposite.
What is the maximum altitude for flap use?
15,000 ft.
What is the minimum altitude (AGL) for flight spoiler use?
800 ft AGL
Can the onboard wing anti-ice system be used in conjunction with type II or IV anti-icing fluids?
Yes, but only just prior to power application for takeoff.
When is the TAT temperature probe accurate?
When in flight or at appreciable forward speed
Define: Contaminated Runway
Any time braking conditions are less than GOOD (<40MU value)
Maximum Passenger Capacity
50