| Terms |
Definitions |
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Maximum Landing Weight(all models)
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47,000
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Maximum continuous oil temp is______.
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155*C
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Maximum landing weight?
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47,000 and 67,000
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Maximum Takeoff Weight?
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53,000 and 75,000
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Maximum permissible fuel imbalance between main left tank and main right tank is____.
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800 lbs
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Use of_____submode(flight director or autopilot coupled)during approach is not permitted.
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DES (descent)
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<-701> 31,000 ft.
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Use of ________________, _______________ or ___________,during approach is not permitted.
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Maximum windshield wiper speed (VWIPE):
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220 KIAS
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Fuel remaining when fuel quantity indicator reads zero is_____.
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not usable
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Maximum speed for aircraft with landing gear extended and locked
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250 KIAS
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Maximum permissible oil temp is______.
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163*C(15 minutes maximum)
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FMS range and fuel information is_____.
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advisory only
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15,000 ft.
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<-200>⢠Flights shall not be conducted at cruise altitudes where the SAT iscolder than _____. If a SAT of _____ or colder is encountered, adescent to warmer air must be initiated within ________.
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<701> 19,594 LBS
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Powered crossflow and gravity crossflow must be ______ for takeoff.
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10 knots
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Maximum crosswind for takeoff and landing:
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Flight spoilers must not be extended in flight below_____.
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300 AGL
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The FMS is approved for use during_____and_____phases of flight.
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en routeterminal
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Windshield wipers must not be operated above_____.
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220 KIAS
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RNAV, GPS, and GPS overlay approaches must not be continued past the FAF if a_____message is diplayed.
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NO APPR
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ADG maximum speed:(wet ADG - tails 7002-7304)
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250 KIAS
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APR OFF performance must be used if___________caution message is displayed.
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APR INOP
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Ground OperationsCowl anti-ice system must be ON when the OAT is 10°C (50°F) or below:⢠And visible moisture in any form (such as clouds, fog, mist, rain, snow,sleet, or ice crystals), is present below 400 feet AGL, or⢠When operating on r
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Take-off is prohibited with:
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<700> 41,000 feet
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Definition of icing conditions with respect to the cowl anti-ice?
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Minimum fuel quantity for go-around is_____ lbs per wing, assuming a maximum climb attitude of_____.
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450 lbs10* nose up
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Maximum airspeed for turbulence penetration is the lesser of_______.
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280 KIAS or 0.75 MACH
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Continuous ignition must be used under what circumstances?
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Takeoff/landing on contaminated runwayTakeoff with high crosswind componentFlight through moderate or greater turbulenceFlight through moderate or heaver rainFlight in vicinity of T-storms (where lightning strikes may be encountered)
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Intentional speed reduction below_____, as defined by_____, is prohibited unless a lower speed is specifically authorized for flight testing or training operations.
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onset of stall warning
stick shaker operation
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During landing, application of reverse thrust is not permitted at airspeeds below_____. Below this speed, reverse thrust must be limited to_____.
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60 KIASIDLE(not above 30% N1)
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Oilpressure returns to normal range.
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When must the continuous engine ignition must be used?
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<-701> 25,000 ft.
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Each engine may be started using the APU as a bleed airsource only if:
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Engine must remain at idle until oil pressure_________.
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returns to normal limits
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Engine operation at or near shaker and pusher settings is predicated on_________.
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an operable auto-ignition system
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Maximum flap extended speeds:Flaps 08:_____Flaps 20:_____Flaps 30:_____Flaps 45:_____
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Flaps 08: 215 KIASFlaps 20: 215 KIASFlaps 30: 185 KIASFlaps 45: 170 KIAS
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PPAS UNAVAILABLE: Above 10,000 ft during climb, the aircraft will not be climbed at a speed less than_____unless a slower speed is required to comply with airspace or departure requirements.
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250 KIAS / 0.70 MACH
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Enroute use of slats/flaps is prohibited.
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Maximum slats and/or flaps extended altitude:
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⢠Takeoff and landing on contaminated runways⢠Takeoff with high crosswind components (15 knots or greater)⢠Flight through moderate or heavier intensity rain⢠Flight through moderate or heavier intensity turbulence⢠Flight in the
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Starter Cranking Limits on the 200?
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Flap Position VFE
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Flaps 1 - 230 KIAS <-701>Flaps 8 230 KIASFlaps 20 230 KIASFlaps 30 185 KIASFlaps 45 170 KIAS
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<-200>⢠Flights shall not be conducted at cruise altitudes where the SAT iscolder than -60°C. If a SAT of -60°C or colder is encountered, adescent to warmer air must be initiated within 10 minutes.
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Minimum altitude for flight spoiler deployment?
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For visual and non-precision approaches, the minimum height forautopilot use is 400 ft. AGL⢠For precision approaches (PAR/ILS), the minimum height for autopilotuse is 100 ft. AGL
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To protect the flight compartment CRT displays, the maximumpermissible time for ground operations with DC power only is__ minutes.
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With an operable GPS, the FMS is approved for RNAV, GPS and GPS overlay approaches. The FMS shall not be used as a primary guidance for_____regardless of equipment on board the aircraft.
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any other type of approach
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PPAS UNAVAILABLE:Above 10,000 ft, cruise, holding, descent - in no case will the aircraft be operated at a speed less than_____,appropriate for weight, altitude, and operational mode.
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Holding - Safe speed depicted in CRJ Flight Standards Manual
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Ground Operations:The wing anti-ice system must be confirmed ON for final taxi prior totake-off when the OAT is 5°C (41°F) or below and:⢠Visible moisture in any form (such as clouds, fog, mist, rain, snow,sleet or ice crystals), is present bel
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When must the wing anti-ice system be on when in the air?
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Engine dry-motoring limits:1st: max time ON____followed by____OFF2nd+: max time ON____followed by____OFF
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1st: 90 seconds ON, 5 minutes OFF2nd+: 30 seconds ON, 5 minutes OFF
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On the ground, Cowl Anti-ice must be ON when OAT is below______and______,or______.
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10*C(50*F)
visible moisture in any form is present(fog with visibility of 1SM or less, rain, snow, sleet and ice crystals).
when operating on runways, ramps, or taxiways where surface snow, ice, standing water, or slush is present.
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Reduced Engine "Flex" Thrust takeoff must not be used under the following conditions:
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if normal takeoff fan speed is less than 85% N1
if reduced "flex" thrust value is less than 85% N1
with an engine(s) which cannot achieve full rated thrust. (checked every 100 flight hours)
if Wing and/or Cowl Anti-icing Bleeds are in use
on runways contaminated w/ standing water, slush, snow, or ice
when warnings of windshear or downdrafts have been forecast
when using performance data derived from the Maximum Gross Load data (Temporary Runway Analysis on Dispatch Release)
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At altitudes at and below FL 250, flight spoilers mus not be extended in flight at airspeeds below_____or_____or_____as appropriate.
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Safe, Holding - Safe speedminimum maneuvering speed plus 20 KIASVref speed plus 20 KIAS
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<-200> onlythe operating engineâs thrust must not exceed70% N2, if both engines are to be started using the APU bleedair.
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With the APU door not closed or the door position is unknown:
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Above FL 250, do not extend flight spoilers in level flight. During descents above FL 250 flight spoilers must not be extended at airpeeds below_____.
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applicable Safe or Holding - Safe speed plus 25KIAS.
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Engine to engine N2 split at ground idle power should not be greaterthan 2% N2. If N2 is 57% or less with an OAT of -20°C or less, do notaccelerate above idle.
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After cold start, engine must remain at idle until:
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Use of SPEED MODE (DES or IAS), flight director or autopilot coupled,during approach is not permitted.
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Operation with the autopilot engaged is prohibited at altitudes below ____ft. AGL, except when performing the following:
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<-701> The VFE and VFO speeds are?
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<-701> The VFE and VFO speeds are equal.
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When Type II, Type III, or type IV anti-icing fluids have been applied, select anti-ice ON_____________.
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just prior to thrust increase for takeoff.
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During all starts, do not exceed 75% N1 for 2 minutes after start, or untilall operating indications are in the normal range, whichever is longer.Operate engines at idle for 2 minutes prior to shutdown.
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Engine to engine N2 split at ground idle power should not be greaterthan ___ N2. If N2 is ___ or less with an OAT of ___ or less, do notaccelerate above idle.
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Engine starter limits:1st: max time ON____followed by____OFF2nd: max time ON____followed by____OFF3rd+: max time ON____followed by____OFF
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1st: 1 minute ON, 10 seconds OFF2nd: 1 minute ON, 10 seconds OFF3rd+: 1 minute ON, 5 minutes OFF
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Max Continuous Engine Limits
(3B1)
N2____, N1____, ITT____
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N2 - 99.2%
N1 - 98.6%
ITT - 874*C
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Takeoff with a fuel load in excess of _____ lbs. in the center tank is notpermitted unless each wing tank is above _______lbs.
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Takeoff with a fuel load in excess of 500 lbs. in the center tank is notpermitted unless each wing tank is above 4,400 lbs.
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Normal Takeoff Engine limits
(all engine models)
N2____, N1____, ITT____
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N2 - 98.3%
N1 - 96.2%
ITT - 884*C for 5 minutes(900 for 2 out of 5 transient minutes)
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1 Max Time ON 15 seconds Followed By 2 minutes OFF
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2 Max Time ON 15 seconds Followed By 20 minutes OFF
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