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77 Cards in this Set
- Front
- Back
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RVSM REQUIRED EQUIPMENT LIST |
1. Autopilot - must be operational 2. Altitude Alerting System- must be operational 3. Altitude Reporting Transponder- one must be operational 4. Air Data Computers - both(2) must be operational
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CRJ700 Max Taxi and Ramp Weight |
75,250 |
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CRJ700 Max TO Weight |
75,000 |
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CRJ700 Max Landing Weight |
67,000 |
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CRJ900 Max Taxi and Ramp Weight |
85,000 |
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CRJ900 Max TO Weight |
84,500 |
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CRJ900 Max Landing Weight |
75,100 |
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Maximum TW Component |
10 knots |
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ITT Ground Start CRJ700/900 |
815C |
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Oil Press Ground Start CRJ700/900 |
182 PSI / 95 PSI (after 10 min) |
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Normal TO/ Max Power CRJ700/900 (Two engines) |
5 min |
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APR Power (one engine) |
10 min |
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ITT must be below ____C before attempting to ground start? Air start? |
120 Ground 90 Air |
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Continuous Engine Ignition must be on... |
- TOs/Landings on contaminated runways - flight through moderate or heavier intensity rain - flight through moderate or heavier intensity turbulence - flight in the vicinity of thunderstorms |
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Max fuel imbalance between L and R wing tanks? |
- TO 300lbs - All other phases of flight 800lbs |
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TO with a fuel load in excess of 500lbs in the center tank not permitted unless... |
1. Each main wing tank is above 4,400lbs Or 2. Each main wing is above 2000lbs and -allowable ZFW reduced by weight of fuel in center tank in excess of 500lbs - CG configuration is verified in the envelope through AeroData |
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APU Starter Limitation |
- Not more than 3 starts/start attempts in 1 hour. - 2 min delay between cranking attempts (cooling of starter, contacted, APU fuel drainage) |
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Max cruise Mach Vmo In RVSM |
CRJ700 .83 CRJ900 .82 |
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Flaps 1 Vfe |
230 KIAS |
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Flaps 8 Vfe |
230 KIAS |
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Flaps 20 Vfe |
CRJ700 230 KIAS CRJ900 220 KIAS
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Flaps 30 Vfe |
185 KIAS |
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Flaps 45 Vfe |
170 KIAS |
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VLO Max Gear Extension |
220 KIAS |
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VLE Max Gear Down and Locked |
220 KIAS |
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VLO Max Gear Retraction |
200 KIAS |
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Tire Limit Speed |
CRJ700 182 knots CRJ900 195 knots |
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Max airspeed for turbulence |
280 KIAS or Mach .75 whichever is less |
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DC Electrical System Loads |
Ground Ops: Max time for ground ops with DC power is 5 min Flight Ops: Max continuous load on each TRU 120 amp. |
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Slats/ Flaps |
- Enroute use of Slats/Flaps prohibited - Flight with Slats/Flaps extended at altitudes above 15,000’ prohibited |
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Slats/Flaps |
-En-Route use prohibited -Flight with slats/Flaps Extended above 15,000’ prohibited |
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Taxi Lights |
Switched off when airplane is stationary greater than 10 minutes |
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Reduced (FLEX) T/O Thrust not Authorized when: |
1. Wing and/or cowl anti-ice bleeds in use 2. RWY is contaminated W/ standing water, slush, snow, or ice* 3. Warnings or forecasts of WS or downdrafts exist (including LLWAS advisories) 4. Anti skid system is inoperative |
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Windshield wiper |
Not above 250 KIAS |
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Single Pack Operation |
31000’ 25000’ - CRJ900 more than 82 occupants including FAs
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Maneuvering LIMIT Load Factors |
Flaps Retract -1.0 to 2.5 G Flaps Extended 0.0 to 2.0 G |
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Cowl Anti-Ice ON Ground Ops OAT 10C or below: |
1. Visible moisture in any form present (fog visibility 1 mile or less, rain, snow, sleet, ice crystals) 2. Operating on RWYs, ramps, taxiways with SURFACE SNOW, STANDING WATER, or SLUSH *turn on continuous ignition* |
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Cowl-Anti Ice ON Flight Ops TAT 10C or below, and Visible Moisture present any form, except SAT -40C or below |
1. In icing conditions or 2. ICE is annunciated by ice detection system *turn on continuous ignition* |
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Wing Anti-Ice GROUND Ops On for T/O OAT 5C or below |
1. Visible moisture present (fog visibility 1 mile or less, rain, snow, sleet, ice) 2. RWY contaminated W/ snow, slush, or standing water When Type II, III, or IV fluids applied: only selected ON, if required, just prior to thrust increase for TO |
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Wing Anti-Ice FLIGHT Ops |
TAT of 10C or below, and visible moisture encountered (clouds, rain, snow, sleet, or ice) except SAT is -40C or below. Wing anti-ice ON when: 1. ICE is annunciated by ice detection system or 2. Icing conditions and the airspeed is less than 230 KIAS |
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Wing Anti-Ice Supercooled Lg Droplet Icing |
Continued Ops in SLD icing exists prohibited *Look at flight deck side windows 1. Wing and Cowl anti-icing ON in SLD icing conditions 2. Leave icing, when side window icing occurs |
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Starter Cranking Limits Engine Start (Ground) |
1&2 / 90 seconds on / 10 seconds cool down
3-5 / 90 seconds on / 5 minutes cool down |
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Starter Cranking Limits Engine Start or Motoring (Flight) |
1 / 120 seconds / 10 seconds cool down
2-5 / 60 seconds / 5 minutes cool down |
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Starter Cranking Limits Motoring (Ground) |
1 / 90 seconds / 5 minutes cool down
2-5 / 30 seconds / 5 minutes cool down |
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Engines High-Power Schedule Switchlight |
Use prohibited |
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APU Start and Operating Limits |
APU Gen Loading limit 41,000’ APU Altitude Starting Limit 37,000’ Bleed Air Extraction 25,000’ |
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Autopilot Takeoff |
600’ AGL |
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Autopilot Non-Precision Approach |
400’ AGL |
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Autopilot Precision Approach (Both Engines) |
80’ AGL |
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Autopilot Precision Approach (One Engine) CRJ900 |
110’ AGL |
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Cold Wx Ops |
T.O. Is prohibited with frost, ice, snow, or slush adhering to any critical areas (wings, upper fuselage, horizontal stabilizer, vertical stabilizer, control surfaces, and engine inlets). |
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CRJ700 Cargo Weights |
Fwd Max 1000lbs Main Cargo Bay 3,650lbs |
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CRJ900 Cargo Weights |
Fwd Max 1,700lbs Main Cargo Max 3,650lbs |
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Cargo |
Flight within 60 minutes of suitable airport, if Cargo is carried in any labeled cargo compartment. |
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Engines |
CRJ700 2 GE CF34-8C5B1 CRJ700 2 GE CF34-8C1 Engines CRJ900 2 GE CF34-8C5 Engines |
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Airplane Cold Soak |
B4 1st flight, airplane is cold-soaked at an ambient temp -30C or below for more than 8 hrs. -motor engines for 60 secs, fan rotation verified b4 start initiated - TRs must be actuated until deploy and stow cycles 2 secs or less |
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Max Zero Fuel Weight |
62,300 70,750 |
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Minimum Flight Weight |
42,000 45,000 |
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Gravity Refueling |
CRJ700 - 7,290lbs per wing Total 14,580lbs CRJ900 - 7,405lbs per wing Total 14,810lbs |
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Pressure Refueling |
7,492lbs per wing 4,610lbs center tank Total 19,594lbs |
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EICAS Messages coding (Can’t box Xmas colors) |
Warning- Red Caution- Yellow Advisory- Green Status- White |
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Min Fuel BARHA |
Burn, Alternate, Reserve, Holding, Add Fuel |
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Thrust |
12,670 13,600 |
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APR Thrust |
13,790 14,510 |
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Minimum O2 pressure for crew |
Crew of 2 - 810psi Crew of 3 - 1110psi |
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Max X-Wind TO Dry |
CRJ700 28kts CRJ900 35kts |
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Max X-Wind Landing Dry |
CRJ700 30kts CRJ900 32kts |
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Max X-Wind TO/Landing WET |
27kts |
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Max X-Wind TO/Landing (RCC3) |
20kts |
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Max X-Wind High Mins Dry |
Captain 25kts FO 15kts |
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Starter Cranking Limit |
Starter must not be used if indicated N2 rpm exceeds 45% |
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Thrust Reversers |
1) Approved ground use only. 2) Full stop landings only 3) T.O. with reverser icons or EICAS warning/caution msgs prohibited 4) Max reverse prohibited below 75KIAS & idle by 60KIAS 5) Preflight with AC stationary, reverse thrust limited to idle. |
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APU |
Min start temp -40C Max load on APU generator 40 kVA |
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Min GA fuel |
600lbs per wing 10 degrees nose up |
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Engine Warm-up |
Engine must remain at IDLE until oil press reaches normal operating range. Don’t exceed 75% N1 for 2 min after start, or until all operating indications are in normal range, whichever is longer. |
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Stall Protection System |
Both switches must remain on all phases of flight |
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Fuel Temperature |
T/O with engine fuel temp indications below 5c is prohibited |
