Max Ramp Weight CRJ 200
53,250 lbs
Max Ramp Weight CRJ 700
75,250 lbs
Max Ramp Weight CRJ 900
85,000 lbs
Max Take Off Weight CRJ 200
53,000 lbs
Max Take Off Weight CRJ 700
75,000 lbs
Max Take Off Weight CRJ 900
84,500 lbs
Max Take Off Weight for Delta / Alaska 700’s
74,999 lbs
Max Landing Weight CRJ 200
47,000 lbs
Max Landing Weight CRJ 700
67,000 lbs
Max Landing Weight CRJ 900
75,100 lbs
Max Zero Fuel Weight CRJ 200
44,000 lbs
Max Zero Fuel Weight CRJ 700
62,300
Max Zero Fuel Weight CRJ 900
70,750 lbs
Max Aft Cargo CRJ 200
3500 lbs
Max Aft Cargo CRJ 700
3740 lbs
Max Aft Cargo CRJ 900
3740 lbs
Max Aft Cargo WiFi Equipped CRJ 700 / 900’s
3650 lbs (90 lbs less)
Max Aft Cargo Alaska CRJ 700
4375 lbs
Max Fwd Cargo CRJ 700
1000 lbs
Max Fwd Cargo CRJ 900
1700 lb total 850/850 split bin
Max Flight Time to Suitable Airport CRJ 200
45 Minutes ( limitation based on cargo fire bottle time )
Max Flight Time to Suitable Airport CRJ 700 / 900
60 Minutes
Max Temp for Take Off and Land
ISA + 35C
Max Temp for Take Off and Land Phoenix
Approx 48 degs C or 118 degrees F
Max Temp for Take Off in Denver
Approx 40 degrees C or 104 degrees F
Vmo all variants
335 Kts
Mmo CRJ 200
.85 Mach
Mmo CRJ 700
.85 Mach
Mmo CRJ 700 in RVSM
.83 Mach in RVSM
Mmo CRJ 900
.84 Mach
Mmo CRJ 900 in RVSM
.82 Mach RVSM
Vtire CRJ 200
182 Kts GS
Vtire CRJ 700
182 Kts GS
Vtire CRJ 900
195 Kts GS
Vwiper max CRJ 200
220 KIAS
Vwiper max CRJ 700 / 900
250 KIAS
Hydraulic Normal psi CRJ 200
2950 - 3050 psi
Hydraulic Low psi CRJ 200 / 700 / 900
< 1800 psi (amber)
Hydraulic High psi CRJ 200
> 3200 psi (white)
Hydraulic Pressure Relief CRJ 200
> 3750 psi (white)
Hydraulic Accumulator Pressure CRJ 200
1500 psi
Hydraulic Normal Level CRJ 200
45 - 85 % (green)
Hydraulic High Temp Caution CRJ 200
93 - 96 degrees C
Hydraulic Normal psi CRJ 700 / 900
3000 psi
Hydraulic Temp Caution CRJ 700 / 900
94 - 96 degrees C
Normal Brake Pressure CRJ 200
1000 - 3200 psi (green)
Normal Brake Pressure CRJ 700 / 900
1800 - 3200 psi (green)
Anti Skid available
Wheel Speed > 35 KTS, WOW for +5 Sec
Anti Skid inop below what speed
10 KTS
Min Spoiler Speed CRJ 200
Approach Speed + 17 KTS
Min Spoiler Speed CRJ 700 / 900
Approach Speed + 10 KTS
Min Alt for Spoilers
300’ AGL
Max ITT for Engine Start CRJ 200
900 Degrees C
Max ITT for Engine Start CRJ 700 / 900
815 degrees C
Max Continuous Thrust CRJ 200
3A1 : 860 degrees C
3B1 : 874 degrees C
Max ITT APR not operating / Normal T/O CRJ 200
928 degrees C for the first 2 minutes
884 degrees C for the next 3 minutes
Max ITT APR not operating / Normal T/O CRJ 700
920 degrees C for 5 minutes
Max ITT APR not operating / Normal T/O CRJ 900
947 degrees C for 5 minutes
Max ITT APR operating CRJ 900
990 degrees C for 5 minutes ( + 43 degrees C )
Max ITT APR operating CRJ 700
960 degrees C for 5 minutes
Max ITT APR operating CRJ 200
928 degrees C for first 2 minutes
900 degrees C for next 3 minutes
Min Oil Temp for Start all 3 variants
- 40 degrees C
Max Continuous Oil Temp all 3 variants
155 degrees C
Max Oil Temp allowed for 15 minutes
163 degrees C
Min Oil Pressure for Start / Idle CRJ 200
25 psi ( red )
Min Oil Pressure for Start / Idle CRJ 700 / 900
25 to 60 psi ( green )
Min Oil Pressure for Take Off CRJ 200
45 psi ( green )
Min Oil Pressure for Take Off CRJ 700 / 900
45 - 95 psi ( green )
Max Continuous Oil Pressure CRJ 200
115 psi ( green )
Max Continuous Oil Pressure CRJ 700 / 900
45 - 95 psi ( green )
Max Oil Pressure after Cold Start CRJ 200
156 psi ( amber ) 130 psi at idle for max of 10 minutes
Max Oil Pressure after Cold Start CRJ 700 / 900
182 psi ( amber ) 116 psi max after 10 minutes ( 95 psi for CRJ 900 )
Max Oil Consumption
.05 GPH or 1 Qt for every 5 hours
What Engines are on the CRJ 200 and how much thrust do they produce
CF 34 - 3B1
Take Off Thrust 8729 lbs
What Engines are on the CRJ 700 and how much thrust do they produce
CF 34 - 8C1
Take Off Thrust 12,670 lbs
What Engines are on the CRJ 900 and how much thrust do they produce
CF 34 - 8C5
Take Off Thrust 13,535 lbs
Engine Start Limitations CRJ 200
60 Sec ON - 10 Sec Off
60 Sec ON - 10 Sec Off
60 Sec ON - 5 Min Off
60 Sec ON - 5 Min Off
Engine Start Limitations
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
Dry Motoring Limitations CRJ 200
90 Sec ON - 5 Min OFF
30 Sec ON - 5 Min OFF
Dry Motoring CRJ 700 / 900
90 Sec ON - 5 Min OFF 30 Sec ON - 5 Min OFF 30 Sec ON - 5 Min OFF 30 Sec ON - 5 Min OFF 30 Sec ON - 5 Min OFF
Left / Right Main Tank Useable Fuel CRJ 200
( Pressure Refueling )
( Gravity Refueling )
4760 lbs with single point pressure refueling
4488 lbs with over wing / gravity refueling
Left / Right Main Tank Useable Fuel CRJ 700 900
( Pressure Refueling )
( Gravity Refueling )
7492 lbs with single point pressure refueling
7290 lbs with over wing / gravity refueling
Center Tank Useable Fuel CRJ 200
( Pressure Refueling )
( Gravity Refueling )
4998 lbs with single point pressure refueling
4930 lbs with over wing / gravity refueling
Center Tank Useable Fuel CRJ 700 / 900
( Pressure Refueling )
( Gravity Refueling )
4610 lbs Pressure Refueling
N/A
What is the difference between total useable on the CRJ 700 and the CRJ 900?
They have the same useable fuel quantities.
What is the Total Useable Fuel of the CRJ 200
( Pressure Refueling )
( Gravity Refueling )
14,518 lbs with single point pressure refueling
13,906 with over wing / gravity refueling
What is the Total Useable Fuel of the CRJ 700 / 900
( Pressure Refueling )
( Gravity Refueling )
19,594 lbs with single point pressure refueling
14,580 lbs with over wing / gravity refueling CRJ 700
14,810 lbs with over wing / gravity refueling CRJ 900
Max Fuel Imbalance all 3 variants
800 lbs
Max Fuel Imbalance for Take Off CRJ 200
800 lbs
Max Fuel Imbalance for Take Off CRJ 700 / 900
300 lbs
Minimum Fuel for Go Around per Wing CRJ 200
450 lbs ( amber )
Minimum Fuel for Go Around per Wing CRJ 700 / 900
600 lbs
Min Fuel Temp for Take Off
+ 5 degrees C
Nose Wheel Steering Limits on CRJ 200
Tiller 70 degrees L/R
Rudder 5 degrees L/R
Nose Wheel Steering Limits on the CRJ 700 / 900
Tiller 80 degrees L/R
Rudder 8 degrees L/R
Minimum Altitude for use of the AFCS ( Auto Pilot )
Take Off 600 ft AGL
Non Precision Approach 400 ft AGL
Precision Approach 80 ft AGL
(no more than 3.5 degree glideslope)
General Altitude Restrictions for use of the AFCS
50 ft below the MDA or 400 ft AGL which ever is higher for for Non Precision Approaches
And 50 ft above the terrain for precision approaches
Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope equal to or less than 3.5 degrees
4000 ft Field Elevation and below
Approved
Minimum Altitude for Use is 80 ft AGL
Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater than 3.5 to 4.0 degrees
4000 ft Field Elevation and below
Approved
But the Minimum Altitude for Use is 120 ft AGL
Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater 4.0 degrees
4000 ft Field Elevation and below
Prohibited
Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater 4.0 degrees
Field Elevation Higher than 4000 ft
Prohibited
Auto Pilot Limitations on the CRJ 700
Precision Approach
Glide Slope greater than 3.5 to 4.0 degrees
Field Elevation higher than 4000 ft
Prohibited
What is the Max Precision Approach Glide Slope Limitation for the CRJ 700
Max of 3.5 degree glide slope for all airports
3.5 to 4.0 degree glide slope for airports up to 4000’ field elevation. ( Above 4000 feet field elevation is prohibited )
Above 4.0 degree glide slope is prohibited
What is the Max Precision Approach Glide Slope Limitation for the CRJ 900
Max of 3.5 degree glide slope
If Single Engine there is an additional limitation of a max airport field elevation of 4000 feet.
Max APU RPM CRJ 200
107% ( red )
Max APU Continuous EGT
743 degrees C ( red )
Max APU EGT Start
974 degrees C
Max APU EGT on the ground for the CRJ 700 / 900
789 degrees C
Max APU EGT in flight for the CRJ 700 / 900
807 degrees C ( red )
Max APU EGT for the CRJ 700 / 900
1038 degrees C
Min Temp for APU Start
- 40 degrees C
Max APU Ops Altitude for the CRJ 200
37,000 ft
Max APU Start altitude for the CRJ 200
30,000 ft
Max altitude for APU bleed use CRJ 200
15,000 ft
Max altitude for APU use in engine start CRJ 200
13,000 ft
Max Airspeed for the APU Door open when not operating CRJ 200
300 KIAS
APU Start Limitations with AC Battery CRJ 200
2 x 30 Sec ON - 20 Min Off
2 x 30 Sec ON - 40 Min Off
Max Altitude for Single Pack Ops CRJ 200
FL 250
Pack Overheat Temp CRJ 200
88 degrees C
Pack Overpressure CRJ 200
> 53 psi
CPAM drops the Pax O2 at what cabin altitude
14,000 + / - 500 ft ( CRJ 200 )
Equal to or greater than 14,000 ft on the CRJ 700 / 900
CPAM turns on the Passenger NO SMOKING FASTEN SEATBELT sign at what cabin altitude
10,000 ft
On the CRJ 700 / 900 Use of the EMER DEPRESS switch is prohibited above what altitude
15,000 ft
On the CRJ 700 / 900 Limit Climb to ____ fpm above what altitude
Limit Climb to 1500 fpm above FL300
Do not accelerate above idle under what conditions
If N2 is 57% or less with an outside temp of -20 degrees C or warmer
Do not exceed 75% N1 for…
2 minutes after start or until all engine indications are normal
Definition of Cold Soaked
-30 degrees C or colder for more than 8 hrs.
Max APU EGT on the Ground CRJ 700 / 900
789 degrees C
Max APU EGT in flight CRJ 700 / 900
807 degrees C
Max APU EGT CRJ 700 / 900
1038 degrees C ( red )
Max APU Start Altitude CRJ 700 / 900
37,000 ft
Max Altitude APU Bleed Use CRJ 700 / 900
25,000 ft
Max Altitude APU for Engine Start CRJ 700 / 900
21,000 ft
Max Airseed with APU not operating with the APU Door Open CRJ 700 / 900
220 KIAS
APU Start Limits CRJ 700 / 900
Do not perform more than 3 starts in one hour…
A two minute delay must be observed between cranking attempts to allow for cooling and APU drainage.
Max Altitude for Single Pack Ops CRJ 700
31,000 ft
Max Altitude for Single Pack Ops CRJ 900
25,000 ft
With an outside temp of _____ , what is the engine limitation that indicates a mechanical problem with the engine?
If the N2 is 57% or less with an OAT of -20 degrees C or warmer, do not accelerate the engines above idle as the mechanical problem.
When the aircraft is cold soaked at a temp of ____ , what needs to happen on the FFOD?
When the aircraft is cold soaked at a temp of -30 degrees C for more than 8 hours, dry motor the engines and verify N1 fan rotation.
When the aircraft is cold soaked at a temp of ____ , what needs to happen with the Thrust Reversers?
The Thrust Reversers must be actuated until the deploy and stow cycles are less than 5 seconds.
On the CRJ 700 / 900 the deploy cycle is 2 seconds and the stow cycle is an additional 2 seconds.
CRJ 700 900 Takeoff Operating Procedure due to Wind
Within 30 degrees, no limitation
More than 30 degrees from 5 to 30 KTS:
CRJ 700 900 Takeoff Operating Procedure due to Wind
Wind more than 30 degrees from 5 to 30 KTS
Apply Maximum of 75% N1 before brake Release, then TOGA thrust: NML TAKEOFF PROCEDURE
CRJ 700 900 Takeoff Operating Procedure due to Wind
Wind more than 30 degrees and greater than 30 KTS
Apply Maximum of idle / taxi thrust before brake release, then TOGA thrust: RLNG TAKEOFF PROCEDURE
When is Continuous Ignition to be used?
- Takeoffs and landings on contaminated runways
- Takeoffs with high crosswind components >10KT (200 only)
- Flight through Moderate or Heavier Rain
- Flight through Moderate or Heavier Turbulence
- Flight in the vicinity of thunderstorms
What is the APR limitation for Takeoff with 3A1 Engines
The APR system must be selected off when the ambient temperature is -18 degrees C and below with pressure altitudes less than 1000 ft.
What does the SOP say about checking engine oil?
It’s been deleted
CRJ 200 APU Start Limits
Max of 60 seconds below 50% rpm
When do you get the AVAL Light on the APU
When the RPM is 99% for 4 seconds
Limitation for Take Off with fuel in the center tank
Takeoff with more than 500 lbs in the center tank is not permitted unless there is more than 4,400 lbs in each main tank.
What is the exception to the center tank fuel limitation for takeoff
Each wing tank is above 2000 lbs and the allowable zero fuel weight is reduced by the weight of the fuel in the center tank in excess of 500 lbs. and the CG is verified
Take Off with Engine Fuel temp below _____ is prohibited
+5 degrees C
What is the Bulk Fuel Temperature Limit for Take Off
-30 degrees C
The Bulk Fuel Temperature must remain at or above ____ during flight
-40 degrees C
Is Reduced Thrust allowed for Flaps 8 Take Off on the CRJ 200
NO
When must a Cold Weather PreFlight Inspection be completed
- When the OAT is 5 degrees C or less
- When the wing fuel temp is 0 degrees C or less
- Icing conditions exist
- AC has been exposed to contaminants on an overnight
- On any through flight where the AC has residual ice form the inbound flight
- Cold Soaked Ice is suspected in the fuel tank area
The aircraft wing surfaces must be checked for ice when what conditions exist?
Frost is detected below the wing tank area
or when the surface temperature is near freezing with high humidity ( temp / dewpoint spread 3 degrees C )
Are Flaps 8 takeoffs authorized on contaminated runways?
Yes… for all 3 variants
Max Standing Water Depth for Take Off CRJ 200
.50 inches
Max Standing Water Depth for Take Off CRJ 700 / 900
.50 inches
Max Wet Snow Depth for Take Off CRJ 200
1.0 inches
Max Slush Depth for Take Off CRJ 200
.50 inches
Max Dry Snow for Take Off
3.0 inches… all 3 varients
When is it possible to have clear ice on the wings?
When the fuel temperature is 0 degrees C or below even if the OAT is above freezing.
When might wing frost occur on the upper wing surface with the OAT above freezing?
When the fuel content exceeds 2297.2 lbs, it is in contact with the upper wing surface.
At what temp must the Cowl Anti-Ice be selected ON while on the ground
- OAT is 10 degrees C and visible moisture is present
Visibility 1 mile or less, fog, rain, snow etc. - While on ramps or taxiways when there are contaminants present.
OAT is 5 degrees and the visibility is 10 miles with a ceiling of 300 overcast… what anti-ice is required
CRJ 200?
CRJ 700 / 900?
Engine Cowl Anti-Ice selected on for Take Off for the CRJ 200
No anti-ice is required for the CRJ 700 / 900
When is a runway considered to be wet?
When there is sufficient moisture on the runway to cause it to appear reflective with a water depth of less than 1/8” covering 100 % of the runway.
If the runway has dry spots with no standing water, is it still considered to be wet?
NO
When is a runway considered to be contaminated
When more than 25% of the runway surface within the required length and width to be used is covered by more than 1/8th inch of standing water or its equivalent in slush or wet snow or dry snow.
If the runways expected to be used are contaminated with ice, what is the limitation?
Both Thrust Reversers must be operative prior to dispatch.
Are Reduced Thrust Take Offs permitted on wet runways?
Yes
Are Reduced Thrust Take Offs permitted with flaps 8
Yes on the CRJ 700 / 900, but not allowed on the CRJ 200
What is the tail wind component limitation for take off using reduced thrust
5 KTS
If windshear is reported, can you take off?
Yes, but normal thrust must be used.
Can you use reduced thrust if the runway is contaminated?
NO
What preflight duty must be completed when the OAT is 5 degrees or less?
a Cold Weather Preflight Inspection must be completed
What Appendix is the O2 requirements for a jumpseater found?
Appendix A
Supplemental Operating Procedures are found in what Appendix?
Appendix A
What Appendix addresses tire wear criteria?
Appendix H
Contact Mx Control if the tire is worn to the bottom of any groove to 1/8th the circumference of which variant?
CRJ 200