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FSI CL65 Limitations
Flight Safety CRJ200 Limitations
| Question | Answer |
|---|---|
| Max Taxi Weight | 53,250 |
| Max T/O Weight | 53,000 |
| Max Landing Weight | 47,000 |
| Max Zero Fuel Weight | 44,000 |
| Minimum Flight Weight | 30,000 |
| Max Cargo Weight | 3,500 |
| Max T/O & Landing Pressure Altitude | 10,000 ft. |
| Max Operating Altitude | 41,000 ft. |
| Max T/O & Landing Ambient Air Temp | ISA +35C |
| Min T/O & Landing Ambient Air Temp | -40C |
| Conditions for use of Cowl Anti-Ice while on the Ground | OAT ≤ +10C & visible moisture with visibility ≤ 1 mile OAT ≤ +10C & Contaminated runway, ramp or taxiway |
| Conditions for use of Cowl Anti-Ice while in Flight | TAT ≤ =10C & visible moisture in any form except when SAT ≤ -40C On when ICE is annunciated by the ice detection system. |
| Conditions for use of Wing Anti-Ice while on the Ground | OAT ≤ +5C & visible moisture with visibility ≤ 1 mile OAT ≤ +5 & Contaminated Runways |
| Conditions for use of Wing Anti-Ice while in Flight | When annunciated by the ice detection system TAT ≤ +10C & Visible moisture in any form, except when SAT ≤ -40C, and airspeed ≤ 230 KIAS |
| Super-Cooled Large Droplets | Continued Flight Operations prohibited. Identified by side window icing. |
| Takeoff with frost adhering to: | Upper surface of fuselage underside of wing, caused by cold soaked fuel (1/8in max) |
| Tactile Check Required of Wing: | OAT ≤ +5C or wing fuel temp is ≤ 0C and visible moisture OR water on wing OR dew point spread is 3C or less OR atmospheric conditions conductive to frost |
| Runway Slope | +/- 2% |
| Max Tailwind | 10 kts |
| Flight with Cargo | Flight must be within 45 minutes of suitable airport |
| Engine Type | General Electric CF34-3B1 |
| Max ITT for Start | 900C |
| Max ITT for T/O | 900C for 2 min, 884 next 3 min |
| Engine Warm Up | Idle power until Oil Pressure in Normal Range |
| Engine Extreme Low Temperature Precautions: | Durations ≥ 8 hrs at ≥ -30C then: Before start - motor engine for 60sec and verify fan rotation Actuate Thrust Reversers until deploy/stow cycle is 5 sec of less |
| Continuous Ignition must be used: | Takeoff and Landing on contaminated runways Flight through Rain ≥ moderate intensity Flight through Turb ≥ moderate intensity Flight in the vicinity of thunderstorms Takeoffs with high crosswind components |
| Engine Start (Ground / Flight) | Start 1/2 60sec followed by 10sec cool down Start 3-5 60sec followed by 5 min cool down |
| Motoring (Ground) | Start 1 90sec followed by 5 min cool down Start 2-5 30sec followed by 5 min cool down |
| Windmilling Engine Start Envelope: | 21,000-15,000 req 300k to Vmo/Mmo & 12-55% N2 < 15,000 req 300k to Vmo/Mmo & 9-55% N2 |
| Starter Assisted Engine Start Envelope: | 21,000 - 15,000 req 180k to Vmo & 0-55% N2 < 15,000 need Vref-Vmo & 0-55% N2 |
| APU Bleed Relight: | ONLY permitted during double engine flameout at 13,000ft or less & 240k min |
| Fuel Total: Wing Tanks: Center Tank: | Total- 14,518 lbs Wings- 4,760 lbs Center- 4,998 lbs |
| Minimum Go Around Fuel | 450 lbs per wing with Max 10deg nose up pitch |
| Takeoff Prohibited Regarding Fuel | Engine Fuel Temp < 5C Wing Fuel Imbalance > 800 lbs Center > 500lbs and Wings ≤ 4,400 lbs or Wing < 2,000lbs and ZFW reduced by the amount of center tank fuel over the 500lb. limit and CG compliance Powered Cross-flow & Gravity Cross-flow must be OFF |
| In Flight Fuel Prohibitions: | Wing imbalance > 800 lbs Jet A ≤ -30C |
| Oil Max duration without servicing_____ Over ______ must check at Eng Oil level panel within ____ to _____ after shutdown | 16hrs; 3min to 2hrs |
| APU Start Attempts: Battery | 1st 30sec / 2 min off 2nd 30sec / 20 min off 3rd 30sec / 2 min off 4th 30sec / 40 min off |
| APU Max generator load _____ | 30 kVA |
| Max ALT APU Electrics ______ Max ALT APU Starting _______ Max ALT APU Pneumatics ______ | FL370 FL300 15,000 ft |
| Vmo / Mmo | 335 KIAS / 0.85 M |
| Vt (Turbulence) | 280 KIAS / 0.75 M |
| Max Windshield Wiper Speed | 220 KIAS |
| Max RVSM airspeed | 0.83 M |
| Vfo Flaps 8 _____ Flaps 20 _____ Flaps 30 _____ Flaps 45 _____ | 200 200 185 170 |
| Vfe Flaps 8 _____ Flaps 20 _____ Flaps 30 _____ Flaps 45 _____ | 215 215 185 170 |
| Enroute use of Flaps / Slats is _______ | Prohibited |
| Flights with Flaps / Slats extend at altitudes above ______ is _______ | 15,000 ft; prohibited |
| Vlo / Vle | 250 KIAS |
| Vlr | 200 KIAS |
| Tire Speed | 182 KIAS |
| Max Crosswind Dry - ______ Max Crosswind Wet - ______ Contaminated Runway - ______ | 27k .3 (poor)= 10k .4 (average)= 15k .5 (good)= 27K |
| Flaps Up Load Limits - _____ to _____ Flaps Down Load Limits - _____ to _____ | UP: -1.0G to +2.5G's Down: -0.0G to +2.0G's |
| Max Relief Differential | + 8.7 psi |
| Min Relief Differential | - 0.5 psi |
| Max Taxi, T/O and Landing Differential | + 0.1 psi |
| Max Single Pack Operation | FL 250 |
| Max Hydraulic Temperature | 96 C |
| Hydraulic Quantity | 45-85% |
| Hydraulic Pressure | 1800-3200 psi |
| Minimum Autopilot Altitudes Takeoff _____ Non Precision/Visual _____ Precision _____ | 600 ft 400 ft 80 ft |
| Engine Electrical Loads 0 to 35,000; _____ kVA above 35,000; _____kVA | 30 kVA 25 kVA |
| APU Electrical Loads 0 to 37,000: _____kVA | 30 kVA |
| TRUs There are ____ with a maximum of ______ each. | 5; 100 amps |
| Maximum Ground Time on DC power only | 5 minutes |
| Use of Flight Spoilers < ____;_____ | 300 ft; prohibited |
| Use of Flight Spoilers at airspeed of < _______;______ | Vref + 17; prohibited |
| Stall Protection System Switches: | On for all phases of flight |
| 10th Stage Bleeds must be _____ for _____ and _____ if cowl or wing anti-ice is on | close, takeoff and landing |
| Use of ISI is ______ during backcourse approaches | Prohibited |
Created by:
pilotcarter
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