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CE750 Limitations
| Question | Answer |
|---|---|
| Max Landing Weight? | 31,800lbs |
| Max Ramp Weight? | 36,000lbs |
| Max Xero Fuel Weight? | 24,400lbs |
| Max Takeoff Weight? | 35,7000lbs |
| Takeoff weight is limited by what? The most restrictive of: | A) Max Takeoff Weight B) Max weight permitted by CLIMB REQUIRMENTS and TAKEOFF FIELD LENGTH |
| Landing weight is limited by what? The most restrictive of: | A) Max Landing Weight (31,800lbs) B) Max weight permitted by CLIMB REQUIREMENTS or BRAKE ENERGY or LANDING DISTANCE |
| Is Ballast Fuel useable fuel? | No. |
| Max altitude for takeoff and landing? | 14,000 feet |
| Max tailwind component for takeoff and landing? | 10 kts |
| Max crosswind for manual flight controls? | 10 kts |
| Max crosswind component for slats asymemetry landing? | 10 kts |
| Minimum altitude to use speed brakes? | 500 AGL |
| Max fuel imbalance for normal operations? | 400lbs |
| Max fuel imbalance for emergency operations? | 800 lbs |
| Minimum fuel in wing tanks for takeoff? | 500 lbs |
| When is takeoff with high idle prohibited? | Any time other than touch-and -go |
| Nose wheel tire pressure on ground? | 132-135 psi +/- 5psi |
| Nose wheel tire pressure unloaded? | 130 psi +/- 5 psi |
| Maximim operating speed (Mmo)? | .92 mach |
| Maximum operating speed(Vmo)? | 350 kts |
| Max operating speed below 8000 feet (Vmo) | 270 kts |
| Max operation speed with Mach Trim off? (Vmo) | .82 mach |
| Max altitude for extension of gear? | 18,000 feet |
| Max altutide for extension of slats/flaps? | 18,000 feet |
| Max slats extended speed | 250 kts |
| Vfe 5 deg | 250 kts |
| Vfe 15 deg | 210 kts |
| Vfe 35 deg | 180 kts |
| Vlo | 210 kts |
| Vle | 210 kts |
| Maximum turbulant air penetration speed? | 300 kts/ .90 mach |
| Maximum speed brake speed? | no limit |
| Minimum speed brake extension speed? | Vref + 15 kts |
| Venr | 190 kts |
| Max tire speed on ground? | 182 kts (210 MPH) |
| Maximum altitude for cruise Operations? | 51,000 feet |
| Max ambient temperture for operations at and below 14,000 feet? | ISA + 39 deg C |
| Max G forces with flaps/slats up? | -1 to +2.7G |
| Max G forces with flaps 5 deg? | 0 to 2 G |
| Max G forces with flaps 15 deg? | 0 to 2 G |
| Max G forces with flaps 35 deg? | 0 to 2 G |
| Max G forces on landing? | 3.5 G |
| Max duration for zero to negitive Gs? | 10 seconds |
| Max cabin pressure differential? | 9.7 psi |
| If a windshield cracks in flight, can the flight proceed to the destination? | Yes |
| Once on the ground with a cracked windshild, can the aircraft proceed to maintenance center without a ferry permit? | Depends on whether a structural ply has cracked |
| How many starts can be made on the engine air trubine starter? | 3 normal starts followed with 25 mins cooling; a 30 second engine motoring counts as 1 start |
| Max N2 to engage the air turbine starter? | 25% N2 |
| What does making me re-type these limitations 3 times do to me? | Suicidal contemplation....... |
| Max generator load below 41,000 feet? | 400 amps |
| Max generator load above 41,000 feet? | 300 amps |
| Can any FADAC be inoperative before flight? | No |
| Time/temp limits for continuous engine ground static operation? | Takeoff Thrust 5 min max. |
| Must both ADC be operational for flight? | Yes |
| Minimum start duct pressure? | 25% APU 30% Air duct cart on EICAS |
| Max time for TLA to be in the TO/MC detent for takeoff/climb? | A) Continuous provided IFF not in amber area B) Recommended 5 mins |
| Max time for operations with ITT in amber area? | 5 mins |
| Recommended time to be in CMB thrust setting during climb? | Climb to level off plus 10 mins |
| Maximum oil temperature for all operations? | 127 degrees |
| Max N1 for all operations? | 100% |
| Max N2 for all operations? | 101% |
| Minumum N2? | 56.7% |
| Max ITT for start? | 800 degrees |
| Max ITT? | 888 deg |
| Max continuous ITT? | 850 deg |
| Minimum oil pressure? | 34 psi below 88% N2. |
| Max oil pressure? | 90 psi (unless cold weather and at idle) |
| Max N1 during cold weather ops concerning fuel temperature? | 40% N1 until fuel temp at +4 deg C |
| At what N2 will the FADEC automatically shut down the engine? (Under Speed) | 54% N2 or below |
| At what N1 will the FADEC automaticlly shut down the entine(over speed) | 105% N1 |
| At what N2 will the FADEC automaticlly shut down the entine(over speed) | 105.6% N2 |
| Minimum fan speed for takeoff? | 73.6 N1 |
| Minimum fuel temperature (Tank) | -37 deg C |
| Max fuel tempature? | +52 deg C |
| Max fuel temperature (tank) | +98.0 deg C |
| Maximum Single point refueling pressure? | 55 psi |
| Maximum single point Defueling pressure? | -10 psi |
| Unusable fuel per hopper tank? | 4.81 gallons |
| Unusable fuel in center tank? | 2.2 gallons |
| Center tank to wing tank fuel transfer must take place prior to when? | Before wing tanks get to 3100 lbs of fuel. |
| Simultaneous cross feed and center tank to wing tank transfer is prohibited when? | When wing tank fuel is less than 2900 lbs. |
| EJA uses what oil? | Mobil Jet II |
| Mimimum oil temp for start? | Abobe -40 deg C |
| What type of hydraulic fluid? | Skydrol |
| Can the aircraft be de-iced with the APU running? | No |
| Can the aircraft be left unattended while the APU is in operaion? | No. |
| Maximum altitude to start the APU? | 31,000 feet |
| Maximum airspeed for starting APU from 31,000 to 20,000 feet? | 300 kts |
| Maximim airspeed for starting APU from 20,000 to 8000 feet? | 350 kts |
| Maximum airspeed for starting APU from below 8000 feet? | 270 kts |
| Maximum altitude to operate the APU? | 31,000 feet |
| Maximum generator load for APU in flight? | 200 amps |
| Maximum generator load for APU on ground? | 300 amps |
| Max EGT during APU start? | 973 deg C |
| Max EGT for govered APU operations? | 718 deg C |
| Max EGT for continuous governed APU operations? | 665 deg C |
| Maximum APU successful starts? | 6 Good starts with 10 min intervals 1 hour cooling for additional starts |
| Max APU unsuccessful startsusing aircraft battery for start? | 2 bad starts (30 sec cooling) 30 mins cooling-off 2 bad starts (30 second cooling) 1 hour cooling-off |
| Must the APU be inspected after automatic shutdown? | Yes |
| When will the APU bleed air be automatically reduced? | When the EGT gets above 665 Deg C |
| Wheat temperature will render the batteries inert if cold soaked? | -20 deg C |
| Must the battery temperature indicating system be operative for lfight? | Yes |
| Can a flight depart after receiving a Battery OTEMP EICAS message? | No |
| Does a APU start using a GPU count as a battery start? | No |
| Max altitude to operate with the baggage compartment un-pressurized? | 41,000 feet |
| Can baggage be put in the bagage compartment if it will be unpressureized? | No |
| Can Baggage be carried in the baggage compartment if the smoke detection system is inoperate? | No |
| Can live amimals be carried in the baggage compartment? | No |
| Mut flight with the baggage compartment unpressurized be logged? | Yes |
| Max weight in the baggage compartment? | 700 lbs |
| Max weight in the ski tube | 75 lbs |
| Must the crew oxygen mask be stowed prior to flight? | Yes |
| Max Cabin altitude to use crew oxygen masks continously? | 40,000 feet |
| Max cabin altitude to use passenger oxygen continously? | 25,000 feet |
| Is medical oxygen approved to refill the oxtgen tanks? | No |
| What oxygen is required to fill the oxygen tanks? | Aviators Breathing Oxygen |
| When is engine syne used PROHIBITED?> | A) Single engine operaions B) Takeoff and Landing C) FADEC or ADC or N1 revesionary operations |
| Must the stall warning, mimimum speed, and ydraulic A and B slat system be checked and operational prior to flight? | Yes |
| Where must the stab trim be set for takeoff? | In the green arc |
| Above what speed must the Mach Trim be operational? | .82 mach |
| When is unloading the hydraulics A and B systems prohibied execpt for an emergency? | Above 15,000 feet |
| Are thrust reverser use on non-paved surfaces approved? | No |
| Revewse thruse must be in idle by what airspeed on landing? | 65 kts |
| Maximum reverse thrust N1 | 50% (70% some serial numbers) |
| During single engine reverse thruse use, when must the thrust be at idle at 70 kts? | On Slippery surgaces or with nose wheel steering inoperative |
| Is thrust reverser approved to touch and go operations? | Fuck NO! |
| During single engine reverse thrust use, when must the thrust be at idle? | 70 kts |
| Must the thrust reverser be operational prior to flight? | Yes |
| When should thrust reversersbe activated on landing? | After the nose wheel is on the ground. |
| Max SAT for using anti-ice on the ground (except for test)> | -20 deg C |
| Minimum airspeed for sustained flight in icing conditions? | 200 kts |
| Can PAC HP bleed air be slected when using anit-ice system? | No |
| Must the Honeywell Primus 2000 and Radio System manuals be on board the aircraft? | Yes |
| Minimum altitude for autopilot use on a percision approach? | 170 feet AGL |
| Minimum altitude for autopilot during cruise flight? | 1000 feet AGL |
| Minimum altitude for autopilot during non-precision approach? | 400 feet AGL |
| Is autopilot use during use/display of a single IRS/AHRS system approved? | No |
| Can the autopilot be used for an ILS approach with FLAPs approved? | No |
| When may the ADF pointer be unreliable? | During HF radio transmissions. |
Created by:
cmarshall3050
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