CRJ SkyWest

53,250 lbs

53,000 lbs

47,000 lbs

3,500 lbs

75,250 lbs

• 75,000 lbs
• (74,999 lbs Delta/Alaska)

67,000 lbs

3,740 lbs

4,375 lbs

1,000 lbs

85,000 lbs

84,500 lbs

75,100 lbs

3,740 lbs

• 1,700 lbs
• (850 lbs per bin)

37,000 ft.

39,000 ft.

10 kts.

0.85 M

• 0.85 M
• (0.83 RVSM)

• 0.84 M
• (0.82 RVSM)

230 KIAS

230 KIAS

200 KIAS

200 KIAS

215 KIAS

230 KIAS

230 KIAS

215 KIAS

230 KIAS

220 KIAS

185 KIAS

185 KIAS

185 KIAS

170 KIAS

170 KIAS

170 KIAS

220 KIAS

200 KIAS

182 K GS

250 KIAS

280 KIAS

0.75 M

220 KIAS

220 KIAS

200 KIAS

182 K GS

Vmo/Mmo

280 KIAS

0.75 M

250 KIAS

220 KIAS

200 KIAS

195 K GS

Vmo/Mmo

280 KIAS

0.75 M

250 KIAS

• PSI2950-3050
• (green)

• 45%-85%
• (green)

• PSI3000 psi
• (green)

Vref+17

Vref+10

• Flight spoilers must not be
• extended in flight with flap
• settings greater than 30°

874°C (red)

900°C (red)

927°C (red)

815° (red)

960°C (red)

815°C (red)

• Engine must remain at idle thrust until oil psi returns
• to normal range

2 QT without dry motoring

• 60 sec ON---10 sec OFF
• 60 sec ON---10 sec OFF
• 60 sec ON---5 min OFF
• 60 sec ON---5 min OFF

• At initiation of thrust lever
• movement from SHUT OFF
• to IDLE, ITT must be 120°C
• or less for all ground starts

• 90 sec ON---10 sec OFF
• 90 sec ON---10 sec OFF
• 90 sec ON---5 min OFF
• 90 sec ON---5 min OFF
• 90 sec ON---5 min OFF

800 lbs

800 lbs

300 lbs

• 450 lbs per wing
• (amber)

600 lbs per wing

Prohibited during approach

Prohibited for VOR approaches

• ADC source coupled to
• the active autopilot must
• be the same as that
• coupled to the ATC
• transponder during
• flight in RVSM airspace

600 feet AGL

400 feet AGL

80 Feet AGL

• GS ≤3.5°---80 feet AGL
• ILS GS >3.5° and ≤4.0°--- 120 feet AGL

• GS ≤3.5° and Airport Elevation ≤4000 feet--- 80 feet AGL
• Single Engine:
• Airport Elevation ≤4000 feet--- 110 feet AGL
• Airport Elevation >4000 feet---Prohibited

>3.5°PROHIBITED

• 110 feet AGL or published DH,
• whichever is higher

• The autopilot may not be used
• at an altitude above the terrain
• that is less than 50 feet above
• the terrain, or the altitude specified
• above, whichever is higher

The autopilot may not be used at an altitude above the terrain that is less than 50 feet below the approved MDA for the approach procedure or 400 feet AGL, whichever is higher

743°C (red)

• Aircraft Battery
• 2x30 sec ON---20 min OFF
• 2x30 sec ON---40 min OFF
• External Power
• 2x15 sec ON---20 min OFF
• 2x15 sec ON---40 min OFF

• Do not perform more than three starts/start attempts
• in one hour. A 2 minute delay must be observed
• between cranking attempts to allow for cooling of starter and starter contactor and for APU Drainage.

8.7 psi

14,250 ± 750 ft.

14,500 ± 500 ft.

• Use of the Emergency
• Depressurization switch
• above 15,000 feet is
• prohibited.

• Limit climb to less than
• 1,500 FPM above FL300

SplitNo greater than 2%

• If engine N2 is 57% or less with an
• OAT of -20°C or warmer do not
• accelerate above idle. This
• indicates a mechanical problem

The engines must remain at idle until oil pressure reaches normal range

• Do not exceed 75% N1 for 2
• minutes after start or until all
• operating limitations are in
• normal range, whichever is
• longer

Before the first flight of the day,when the airplane is cold-soaked with temperatures of -30°C or below for more than 8 hours, the engines must be motored for 60 seconds and fan rotation verified before engine start is initiated

During preflight checks of the thrust reversers after being cold-soaked for more than 8 hours, the thrust reversers must be actuated until the deploy and stow cycles are less than 5 seconds

Thrust reversers must be actuated until the delpoy cycle is 2 seconds with an additional 2 seconds for the stow cycle

Do not exercise the thrust levers through the detent positions before engine start with the battery master on

Use of the engine high-power schedule switch is prohibited except as directed by the QRH

With engines running and bleeds configured for takeoff, the crew must verify that the target N1 values correspond with the data presented in the TLR ±1.0%. When thrust levers are set for takeoff, target and N1 values should match

• Continuous Ignition must be used during the following:
• a) Takeoff and landing on contaminated runways
• b) Crosswind components >10 kts (CRJ 200 only)
• c) Moderate or heavier intensity rain
• d) Moderate or greater intensity turbulence
• e) Flight in the vicinity of thunderstorms

Thrust reversers are approved for ground use only

• Do not attempt Takeoff events with TR indicationsTakeoff with any of the following TR lights, icons, or EICAS messages displayed is prohibited:
• a) THRUST REVERSER UNLK light
• b) REV icon displayed on N1 gauge
• c) L or R REV UNLOCKED caution message
• TR Deployment during Landing Application of maximum reverse thrust is not permitted at airspeeds below 75 KIAS. Below 60 KIAS, reverse thrust must be reduced to idle (below 30% N1)

The engine oil replenishment system must be checked within 3 minuted to 2 hours after every engine shutdown

Before starting the second engine the thrust on the operating engine must not exceed 70% N2

EICAS display cooling is not available when the battery bus is powered and normal AC power is off

The APU PWR FUEL switch/light must be selected off between each APU start. The APU PWR FUEL should be firmly pressed only once. If pressed twice, an immediate shutdown may occur

Takeoff with a fuel load in excess of 500 lbs in the center tank is not permitted unless each main tank is above 4,400 lbs

Takeoff with engine fuel temperature indications below +5°C is prohibited

Powered crossflow and gravity crossflow must be off for takeoff

-30°C

-40°C

Wheel brake cooling times in the QRH volume 1 must be observed between landing or a low-energy rejected takeoff (RTO) and subsequent takeoff, to ensure that sufficient brake energy is available to bring the aircraft to a complete stop, if the subsequent takeoff is rejected

Tuning transponder 1 and 2 from the FMS is prohibited

Pilots are authorized to deviate from ATC clearances in order to comply with a TCAS resolution advisory (RA) command

Maximum authorized altitude FL 370

Maximum authorized altitude FL 390

Reduced thrust will be used for ALL takeoffs (flaps 8 or 20) unless otherwise limited

• Reduced thrust takeoff is PROHIBITED when:
• 1) Cowl and/or wing anti-ice is selected on
• 2) The takeoff runway is contaminated with standing water, ice, or snow
• 3) Tailwind component in excess of 5 knots
• 4) Windhsear warnings or downdrafts have been forecast or reported
• 5) Anti-skid is inoperative
• 6) Takeoff behind a heavy
• 7) CRJ 200 Flaps 8 takeoff

Use of reduced thrust on wet runways is permitted

Set normal climb thrust as calculatedon the FMS climb mode or as obtained from the performance flip cards at 1500 feet above field elevation

The appropriate additions to V1 and Vr using the laminated flight deck flip cards must be made if ACARS performance is not available

The flight crew must verify (with engines running) that the target N1 displayed on EICAS, following an input of temperature, is equal to or greater than the appropriate N1 value contained in the reduced thrust section of the takeoff report

Takeoff is prohibited with frost, ice, snow, or slush adhering to any aircraft critical surface

Conditions conducive to icing exist on the ground and for takeoff when OAT is 10°C or below, when operating on ramps, taxiways or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on engines, nacelles, or engine sensor probes

Conditions conducive to icing exist in flight when the TAT is 10°C or below and visible moisture in any form is encountered (such as clouds, rain, snow, sleet, or ice crystals), except where the SAT is -40°C (-40°F) or below

The cowl anti-ice system must be ON when OAT is 10°C or below and visible moisture in any form is present (such as fog with visibility of 1 mile or less, rain, snow, sleet, and ice crystals) ON for takeoff whenever the wing anti-ice system is selected ON

The cowl anti-ice system must be ON when the OAT is 10°C or below when operating on ramps, taxiways, or runways where surface snow, ice, standing water or slush is present

Wing anti-ice must be selected ON with OAT 5°C and colder with or without visible moisture after second engine start (does not apply when type II or IV anti-ice fluid has been applied)

• ON when:
• --Visible moisture in any form such as clouds, fog, or mist below 400' agl is reported
• --Contaminated runway
• --Precipitation in any form

• OFF with OAT -5°C and below in non-icing conditions
• The WING A/ICE ON advisory message must be displayed before takeoff to ensure the wings are free of contamination

• ON whenever ICE is annunciated by the ice detection system
• ON when in icing conditions and the airspeed is less than 230 knots

• ON when in icing conditions
• ON whenever ICE is annunciated by the ice detection system

A runway is considered to be wet when there is sufficient moisture on the runway surface to cause it to appear reflective with a water depth less than 1/8" or 3mm covering 100% of the runway surface. If there are dry spots showering on a drying runway with no standing water, the runway is not considered to be wet

In addition to a runway that is not wet or contaminated, *those paved runways that have been specially prepared with grooves or porous pavement and maintained to retain effectively dry braking action even when moisture is present.

even if a wetrunway is grooved you must use wet runway performance