Help
Options
Didn't know it?
click below
click below
Knew it?
click below
click below
Don't Know
Remaining cards (0)
Know
retry
shuffle
restart
0:00
Embed Code - If you would like this activity on your web page, copy the script below and paste it into your web page.
Normal Size Small Size show me how
Normal Size Small Size show me how
CE 750 Limitations
| Question | Answer |
|---|---|
| Excessive roll/pitch with main gear on the ground might result in | on tail cone or wingtip strike |
| Certified for what category | Transport per Part 25 |
| Max T/O and landing altitude | 14,000 ft |
| Max tailwind component | 10 knots |
| Max crosswind component for manual flight control (dual hydraulic failure, rudder standby system off, aileron or rudder CPU off | 10 knots |
| Max crosswind component slat asymmetry | 10 knots |
| Min Altitude for for in flight use of speed brakes | 500 ft AGL |
| Emergency asymmetric fuel | 800 pounds |
| Max asymmetric fuel | 400 pounds |
| Minimum fuel per tank for T/O | 500 pounds |
| Max Design ramp weight | 36,000 pounds 36,400 pounds 0173 on |
| Max design T/O weight | 35,700 pounds 36,100 pounds 0173 on |
| Max design landing weight | 31,800 pounds |
| Max zero fuel Weight | 24,400 pounds |
| Ballast Fuel is | Non usable fuel on specific tanks to keep the aircraft balanced |
| ITT | Takeoff OEI (5 min): 888°C Max continuous: 850°C Start limit: 800°C Model 0173 on Takeoff (5 min): 907°C Max continuous: 857°C |
| N2 (high pressure turbine) RPM% | 56.7 to 101 |
| N2 automatic FADEC shut down | <54 % >105.6% |
| N1 (low pressure ) fan max RPM | 100% |
| Engine Oil pressure PSIG | 34 to 90 *95 cold day first 2 min |
| Engine oil temperature | 21°C to 127°C |
| Can you apply external airplane deicing fluid while APU is running ? | No |
| Is APU approved for unattended ground operations | No |
| Max Airspeed/Mach for starting APU | 350KIAS/0.92MACH |
| Max altitude for starting/ operating APU | 31,000 ft |
| Max generator load APU (26-29 volts) | Ground 300 Amps Flight 200 Amps |
| APU turbine speeds | Normal 1-100% Caution Range 101-108% Max 108% |
| APU max exhaust gas temperature | Max during start 973°C Max (governed operation) 718°C Max continuous (governed operation) 665°C |
| APU oil limits and ambient temperatures | Same as airplane engines |
| APU starter duty cycles | 6 consecutive successful start at 10 min intervals 1hr off after |
| APU unsuccessful start attempts with battery | 2 cycles :30 seconds each/ 30 min off . 2 cycles 30 seconds each/ 1hr off (check batteries) |
| APU unsuccessful start attempts with Generator/GPU | 2 cycles :15 seconds each/ 20 min off . 2 cycles 15 seconds each (max 4 cycles per hour) |
| APU max bleed may be used during airplane engine starting ? | No |
| Min fuel temperature (on tanks) for start, T/O | -37°C |
| Max fuel temperature (on tanks) for start, T/O | 52°C |
| Min fuel temperature (engine) engine operating | 4°C |
| Max fuel temperature (engine) engine operating | 98.9°C |
| Unusable fuel on tanks (when EICAS reads zero) | 4.81 gallons for each wing/hopper 2.2 gallons for the center tank |
| Center wing tank to wing transfer must be initiated prior to: | 3100 pounds per side wing fuel |
| Simultaneous use of cross feed and center wing tank is prohibited when: | the wing quantity is 2900 pounds or less |
| Ground Pneumatic cart min air pressure as displayed on EICAS | 30PSI |
| Baggage compartment | Smoke detector must be operational Live animals may NOT be transported Flight time not pressurized must be logged |
| Max weight in the baggage compartment | 700 pounds |
| Max weight in ski holding compartment | 75 pounds |
| GPU output requirements | 28 volts 1000 amps |
| Main Generators Limitations | 400 Amps 41,000 ft 300 Amps >41,000ft |
| If the airplane is parked below -20°C | batteries should be removed and stored in warm environment |
| The battery temperature warning system: | must be operational for all ground and flight operations |
| If battery O'temp EICAS message occurs during ground ops | do not take off until proper maintenance is done |
| PAC selector switches operation in High mode is not allowed : | T/O , landings and above 45,000 ft |
| PAC selector switches operation in High mode is not allowed if following systems are on : | Engine anti ice, Slat anti ice, Stabilizer anti ice. (exempt in emergencies but anti ice performance will be degraded) |
| AC selector switches operation in High mode is not allowed above 25,000 if | Isolation valve is open and either the left or right engine bleed air is off |
| Single PAC operations are prohibited | Above 41,000 ft |
| The use of medical oxygen | is not approved |
| Honeywell Primus 2000 avionics and A/P Manual must be available to the crew? | Yes |
| Honeywell Primus 2000 avionics and A/P the airplane should not be taxied until : | The AHRS and IRS ground alignment is complete (approx. 3min ) |
| Honeywell Primus 2000 avionics and A/P One pilot must remain in his seat with seatbelt and shoulder harness fastened | during all A/P operations |
| PFD data must be displayed on | #1 and #5 display units for dispatch |
| A/P min use heigh | Cruise 1000 AGL Precision approach 170 AGL Nonprecision approach 400AGL |
| A/P coupled operations with single operational AHRS or IRS is: | Prohibited |
| A/P coupled ILS approaches with flaps up are: | Prohibited |
| The pressure demand crew oxygen mask must be: | checked, adjusted and properly stowed prior to flight |
| Crew oxygen mask are not approved for sustained operation above altitude greater than: | 40,000ft |
| Passenger oxygen mask are not approved for sustained operation above altitude greater than: | 25,000ft |
| Standby Airspeed and Altitude are not corrected for: | Static and Pitot error and may vary from data in PFD |
| MMO: | 0.92MACH 0.82 (Mach trim off) |
| VMO: | 8,000 to 30650ft 350KIAS below 8,000 270 KIAS |
| Max altitude for extension of flaps or landing gear: | 18,000 ft |
| Max slats extended speed: | 250 KIAS |
| Max flaps extended speed VFE: | flaps 5 250 KIAS flaps 15 210 KIAS flaps 35 180 KIAS |
| Max landing gear operation/extended speed VLO/VLE | 210 KIAS |
| Max turbulent air penetration speed | 300 KIAS |
| Max speed brake extension speed | No limit |
| Min speed brake extension speed | Vref +15KIAS |
| Min single engine enroute climb speed | 190 KIAS |
| Max tire ground speed | 210 knots |
| Nose tire inflation | 130 PSI +_5PSI |
| Max Operating Altitude | 51,000 ft |
| Engine ATS (Air Turbine Starter) limitation | 3 consecutive normal starts follow by 25mn cooling (one 30 sec monitoring cycle is equivalent to 1 normal start) |
| Operations Authorized | Day and night VFR and IFR Flight into known icing conditions Over water (with applicable equipment) CAT II (does not constitute operational approval) |
| Operations NOT Authorized | Ditching Acrobatic maneuvers including spins Intentional stalls under 18,000 ft |
| Minimum crew | Pilot and Copilot |
| Max Load Factor flaps up (slats retracted) | -1 to 2.7 G at 35,7000 pounds |
| Max Load Factor flaps up (slats extended) or 5 to full position (slats extended) | 0 to 2.0 G at 35,7000 pounds |
| Max duration Zero to negative G | 10 seconds |
| Max Load Factor Landing | 3.5 at 31,800 pounds |
| Cabin pressure limitations | 9.7 PSI max differential |
| Icing Limitations Pitot static/RAT and stabilizer bleed air must be on when | operating in icing conditions |
| Icing Limitations All other anti ice system must be turn on unless | it can be verified that ice is not forming or detected |
| Max SAT ( static air temp) for ops of bleed air and anti icing | +20 C |
| Min Speed in icing conditions | 200 KIAS (for approach use normal airspeeds and configurations) |
| Airplane must be free of ice prior to | T/O |
| Engine Synchronization is prohibited during: | T/O, landings, single engine ops, revisionary ops |
| The A and B hydraulic systems may not be intentionally unloaded in flights above | 15,000 ft |
| Thrust reversers are restricted to | ground operations on paved surfaces only |
| Use of thrust reversers are prohibited during | touch an go landings |
| Max reverse thrust is limited by preset maximum reverse of | TLA (throttle lever angle ) 28 degrees and is approx. 50% N1 |
| Reverse thrust must be reversed to idle reverse | at 60 KIAS during landing rollout |
| During single engine reverse , either with nose wheel steering INOP or on slippery runway thrust must be reduced to idle reverse | by 70 KIAS during landing rollout |
| Thrust reversers must not be deployed until | nosewheel is on the ground or aircraft pitch up might occur |
| Radio altimeter must be | on and operable for dispatch |
| How many static discharge wicks , and how many can be missing | 18 total no more than 2 total , 2 adjacent missing not allowed |
| A and B Hydraulics pressure range | green 2800 to 3200 PSI amber <2800 , >3200 PSI red engine running <2600 |
| A and B Hydraulics quantity | green >16 to 100% amber <16% |
| Left and right oil quantity | green < 8 quarts low amber >8 quarts low |
| Oxygen pressure indications | green 1600 to 1800 PSI yellow arc 0 to 400 PSI red arc: 2000 PSI |
| Stabilizer trim indications (green arc) | on ground flaps <5: -2 to -5 flaps 15: 2 to -8 in flight (white arc) : 1.2 to -12 |
| Nose wheel turning limits | rudder pedals: 12 degrees tiller: 80 degrees rudder + tiller : 92 degrees |
Created by:
eugenioalfonso17
Popular Aviation sets