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64 Cards in this Set
- Front
- Back
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Weights |
Max Ramp Weight: 53,250 lbs Max T.O Weight: 53,000 lbs Max Landing Weight: 47,000 lbs Max Zero Fuel Weight: 44,000 lbs Min Flight Weight: 30,000 lbs |
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Max Cargo Compartment |
3,500 lbs |
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Max Turbulence Airspeed |
280 KIAS 0.75 Mach |
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Max Operating Speed |
335 KIAS 0.85 Mach |
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Max Altitude for Single PACK operation |
25,000 ft |
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Max Relief Differential Pressure |
8.7 psi |
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Maximum Negative Differential Pressure |
-0.5 psi |
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Max Differential Pressure for Taxi, Takeoff and Landing |
0.1 psi |
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Minimum Cabin (C ALT) while in Manual mode |
-1,500 ft |
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AFCS: Min Altitude for autopilot engagement |
600 ft |
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AFCS: Minimum Altitude for autopilot disengagement in non precision approaches. |
400 ft |
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AFCS: Minimum Altitude for Autopilot disengagement during precision approaches (PAR/ ILS) |
80 ft |
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RVSM Required Equipment |
Autopilot Altitude Alerting Altitude Reporting Transponder ADC Baro Altimeter TCAS |
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Electric: AC Generator loads limitation |
0 to 35,000 ft: 30 kVA
Above 35,000 ft: 25 kVA |
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Electrics: APU Generator Load limitation |
0 to 37,000 ft: 30 kVA Above 37,000ft: APU operation not permitted |
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Electrics: Ground: Maximum time permitted with DC power only |
5 Minutes |
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Electrics: ADG maximum speed if deployed |
250 KIAS Up to 330 KIAS for 12 Minutes Max 331 to 335 KIAS for 4 minutes |
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Flaps operating Speeds |
Flap postition Vfo Vfe Flap 8: 200 230 Flap 20: 200 230 Flap 30: 185 185 Flap 45: 170 170 |
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Flight Spoilers: Minimum Altitude for Spoiler Use |
300 ft |
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Spoilers: Min Speed for Spoiler Use |
Vref for that Flap setting PLUS 17 |
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Fuel: Capacity |
Pressure Gravity Refueling Refueling
Left and Right: 4,760 lbs 4,488 lbs Centre Tank: 4,998 lbs 4,930 lbs Total: 14,518 lbs 13,906 lbs |
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Fuel: Minimum engine fuel temperature for T.O |
+5 C |
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Fuel: Balance Fuel Distribution |
Not more than 500 lbs in centre tank unless: - Each Main tank is above 4,400 lbs OR; - Each main Tank is above 2,000 lbs AND; - The MZFW is reduced by the weight of the centre tank in excess of 500 lbs. |
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Fuel: Maximum Fuel imbalance between main tanks |
800 lbs |
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Minimum Fuel for Go Around |
450 lbs |
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Hydraulics: Normal Hydraulic Pressure |
2,800 to 3,200 psi |
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Hydraulics: Normal Hydraulic system quantity |
45% to 85% |
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Maximum Speed for Windshield Wiper operation |
220 KIAS |
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Anti ICE: Ground When to use it |
below +10 C OAT: COWL Visible Moisture Rwy contaminated Presence of Precipatation
below +5 C OAT: WING Visible Moisture Type IV de icing fluid applied |
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Anti ICE: In flight use |
TAT below +10 degrees and not colder than -40 degrees SAT |
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Anti ICE: Wing anti ice NOT required if faster than...? |
230 KIAS |
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Tire Limitation speed |
182 Kts |
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Landing gear extension and Retraction Speed |
250 KIAS For extension and down and locked 200 KIAS For Retraction |
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Brake cooling time |
Minimum 15 minutes between landing to subsequent T.O Prior to takeoff BTMS lower than 05 provided is stable and decreasing |
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Power Plant: Engine Limitations |
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Engine operating limits |
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Start crank limitation |
Start 1 min ON 10 secs OFF 1 min ON 10 secs OFF 1 min ON 5 min OFF 1 min ON 5 min OFF |
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Dry motor crank limit |
Start 90 secs ON 5 min OFF 30 secs ON 5 min OFF |
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Engine Relight envelope |
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Oil Pressure: Min Idle Min for T.O Max Continuous Max Transient after Cold Start |
Min Idle 25 psi Min for T.O 45 psi Max Continuous 115 psi Max Transient after Cold Start 156/130 psi Oil pressure may be greater than 115 psi for a maximum of 10 minutes. Engine must remain at idle until pressure returns to normal range |
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Maximum Altitude for Flap/Spoiler operation |
15,000 ft |
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Ignition ON |
T.O or Landing in contaminated RWYs T.O with more than 15 kt x-wind T.O after de-icing Vicinity THstorms |
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Airplane Cold Soaked |
Below -30 C for more than 8 hrs. Dry motor engines for more than 60 secs and verify N1 rotation. Thrust reversers must deploy within 5 seconds. |
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APU restrictions |
Max operating altitude: 37,000 ft Starting temp: -40 C Max Starting altitude: 30,000 ft Air Conditioning: 15,000 ft Engine Start in flight with APU: 13,000 ft |
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APU Start cycles Battery Power |
30 secs ON, 2 min OFF 30 secs ON, 20 min OFF 30 secs ON, 2 min OFF 30 secs ON, 40 min OFF |
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APU starting cycles DC Ground Power |
15 secs ON, 2 min OFF 15 secs ON, 20 min OFF 15 secs ON, 2 min OFF 15 secs ON, 40 min OFF |
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APU EGT |
Normal operating: 743 C Below 60% rpm: 870 C Never Exceed: 974 C |
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APU Door open or unknown |
Airplane limited to 300 KIAS, OR APU must remain in operation |
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Max and Min operating Temperatures |
Max temp for T.O and Landing: 50 C Min temp approved for T.O: -40 C |
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Wind Limitations: X-wind Component |
Dry/Damp: 27 kts Wet: 22 kts Contaminated or Slippery: 15 kts |
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Wind Limits: CAT II/III |
X-wind: 13 kts Headwind: 19 kts Tailwind: 10 kts |
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Minimun Runway Width |
98 ft |
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Runway Contamination Maximum Allowed Takeoff |
More than 0.5 inch Standing Water Slush more than 0.5 inch Wet snow more than 1.0 inch Dry snow more than 3.0 inches |
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Runway Contamination Maximum Allowed Landing |
Standing water more than 0.75 inch Slush more than 0.88 inch Wet snow more than 1.5 inch Dry snow more than 3.75 inch |
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Restrictions on non dry runways with the following inoperative systems. |
Anti Skid: prohibited contaminated rwy Nose Wheel Steering: Prohibited on wet or contaminated rwy One Thrust Reverser: Prohibited rwy contaminated with ice APR: Prohibited on contaminated rwy. Electric Hydraulic pump 2: Prohibited on contaminated rwy. |
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Engine Stable parameters After Start |
N1: 22-25% ITT: 450 - 600 C N2: 56.5 - 68% FF: 390 Oil P: 25-115 |
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Start limitation precautions |
Do not avance thrust above IDLE until oil P is in the green N2 split not greater than 2% If N2 is 57% or less with OAT -20 do not advance above IDLE If N2 is 56.5% or less do not advance above 70% N2 until speed stabilizes. If "L FUEL LO PRESS" msg advance Thrust 5% above idle and verify msg goes out. |
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RVSM error comparisson |
200 ft from CAPT and FO. STBY is not required |
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Battery Voltage and Amperage |
Main Battery: 24 V 17 Amp APU Battery: 24 V 43 Amp |
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External DC Power |
28 Volts |
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ADG Power supplied with airspeed above |
100 kts |
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System Electrical Power requirement |
28 Volts DC 115 Volt AC |
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Dimensions CRJ 200 |
Long 87 ft 10 in Wide 69 ft 9 in |
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Dimensions CRJ 705 |
Long 118 ft 10.7 in Wide 81 ft 6 in |
