flashcard limits 750.txt
Card Set Information
flashcard limits 750.txt
Citation 750 limits
Limitations section of the citation 750
Max Ramp Weight
Max TO Weight
Max Lnd Weight
Max Zero Fuel Weight
Max Altitude for TO/LND
Max Tailwind Component TO/LND
Max Crosswind Component with Manual Reversion
Max Crosswind Component with Slats Asymmetry
Minimum altitude for in-flight use of speed brakes
Max asymmetric fuel
Emergency aymmetric fuel
Minimum wing fuel per tank for TO
Only the Goodyear 164F03-1, -2 nose tire is approved, what is the inflated pressure, unloaded
Mmo above 30650 feet?
Mmo Mach trim off?
Vmo 8000 feet to 30650 feet?
Vmo below 8000 feet?
Max Altitude for EXT of Flaps or Gear
Max Slat EXT Speed?
Max Flap EXT-5 Speed?
Max Flap EXT-15 Speed?
Max Flap EXT-FULL Speed?
Max Landing Gear Operating/Ext Speed
Max turbulent Air Penetration Speed
300 KIAS / 0.9 Mach
Max Speed Brake Extension Speed
Minimum Speed Brake Extension Speed
Vref +15 KIAS
Minimum Single Engine Enroute Climb Speed
Max Tire Ground Speed
G force in-flight flaps/slats retracted
-1 to 2.7 at MGW
G force in-flight flaps UP/ slats EXT
0 to 2 at MGW
G force in-flight flaps 5 to FULL / slats EXT
0 to 2 at MGW
G force in-flight max duration zero to negative G
G force upon landing
3.5 at MLW
The acceleration limit (G force) upon landing is _________feet per minute descent.
The acceleration limit (G force) during flight restrict angle of bank and severity of ____________maneuvers.
Nomal Cabin Pressure Limit
9.7 PSI max Differential
Cracked windshield may be permitted for a departure to maintenance provided which ply is not damaged?
the structural ply (inner)
Describe the windshield layers.
1/10th inch outer, 3/16ths inch structural, 1/4th inch inner structural, all separated by 15/100ths inch PVB layers totaling .825 inch
The Engine Air Turbine Starter is limited to _____ consecutive normal starts followed by 25 minutes of cooling. One ______second motoring cycle is equal to one start.
DO / DO NOT engage the Air Turbine Starter above 25% N2 RPM.
Engine Type is an AE-3007C1 Turbofan, It has _____ fadecs. Must all be operational for dispatch?
For TO, all the Micro Air Data Computers must be operational, how many are there?
Minimum start duct pressure (EICAS) prior to ground start
Time limit in the TO/MC detent?
ITT Temperature limit in the TO/MC detent?
907 degress C
N2 percent Turbine RPM limit in the TO/MC detent?
56.7 to 101
N1 percent FAN RPM limit in the TO/MC detent?
Time limit in the CLB detent?
When should the CRU detent be selected after level-off from TOC?
ITT limit in the CLB, CRU detents?
857 degrees C
During single-engine operation what is the ITT limit of the operating engine?
857 degrees C
ITT during start is limited to ______.
800 degrees C
DO NOT exceed ______percent N1 until engine oil PRESSURE is less than 95 PSIG (cold days).
DO NOT exceed ______percent N1 until engine fuel TEMP is greater than 4 degrees C (cold days).
FADEC automatic overspeed shutdowns are set for _______N1 and ________N2
105%, and 105.6%
The Minimum Fan Speed for TO is ________.
FADEC wil shut the engine down if the N2 is at or below ______%.
Windmilling AIR Start ITT limit is _______degrees C.
Minimum Fuel temperature for Start is ________.
-37 degrees C
Max Fuel temperature for Start is ___________.
+52 degrees C
Minimum Fuel temperature at the ENGINE probe is________.
+4 degrees C
Max Fuel temperature at the ENGINE probe is ________.
+98.9 degrees C
Max pressure of the single point refueling system is ________.
Max pressure of the defueling system is ________.
Unusable fuel is _________gallons in each wing/hopper, and ________gallons in the center tank.
4.81 and 2.2
Center tank to wing transfer must be initiated prior to __________pounds per side wing fuel.
Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when the wing quantity is at or less than ______.
During application of deicing fluid, the APU should ________.
not be operating
The APU may or may not be left operating while unattended.
Max operating Altitude for the APU
Max Generator Load (amps) in the voltage range of 26 to 29 volts on the ground and during flight from the APU is ____and______.
300 and 200
Max continuous EGT of the APU
665 degrees C
Max starter duty cycle for the APU is ______ successful starts at ten minute intervals. Then _____ hour(s) must pass with the APU off for additional starts.
The limit of unsuccessful start attempts using the ship's batteries is_________.
2 cycles 30 sec each, 30 minutes off repeat, then one hour off. Check Batteries
The limit of unsuccessful start attempts using the ship's generator or GPU is_________.
2 cycles 15 sec each, 20 minutes off repeat, max of 4 cycles/hour.
The APU compartment must be inspected following _____________.
an automatic shutdown.
What is the annuciator indication of an automatic APU shutdown?
APU FAIL illumination.
The ship's batteries should be removed and stored in a warm environment is the aircraft is to be cold-soaked below _______degrees C.
The battery cycle limit is _______APU starts in ONE HOUR. If this is exceeded maintenance is indicated.
A ground pneumatic cart must maintain a minimum air pressure of 30 PSI prior to ___________.
initiating the start.
Max Operating altitude with the baggage compartment unpressurized
Use of the baggage compartment is not authorized with the cabin ____________.
Max weight of the baggage in the baggage compartment is
Max floor loading distribution is __________per square foot.
max weight in the ski holding compartment is
Operation in the HIGH mode for the cockpit and cabin PAC selector switches is not approved for __________and____________. TO/landing and
Ops in the HIGH mode of the cockpit and cabin PAC selector switchs is on approved during normal ops when any of the following is ON:
engine AI, Slat AI, Stab IA
During emergency ops, HIGH mode of the PAC selectors switches is approved when AI is also on, however _______________.
performance is degraded.
Ops in the HIGH mode PAC selector switches is not approved above ___________ when the isolation valve is open and engine bleed air is off.
Single PAC ops is not approved for altitudes above _____________.
HP BLEED SELECT switch to HP is not approved for ____________ and _____________ operations.
TO and LND
HP BLEED SELECT switch to HP is prohibited when any of the _____________systems are ON.
The PAC BLEED SELECT switch must be positioned to __________ or ___________ above 41000 feet.
NORM or HP
Crew Oxygen masks are not approved for sustained operation at CABIN altitude greater than __________.
Passenger Oxygen masks are not approved for sustained operation at a CABIN altitude greater than _____________.
Use of engine sync is prohibited during TO and LND, SE ops, or _________________.
FADEC ADC or N1 reversionary ops.
True or False: Both upper and lower yaw damper channels must be operational for dispatch?
Both Rudder limiters must be operational for flight? T/F
What is the purpose of the green arc in the stabilizer trim indicator?
To set trim for the TO range.
Intentional unloading of the A and/or B Hydraulic systems is prohibited above___________MSL.
Thrust Reversers are restricted to ___________operations, and on ___________surfaces only.
ground and paved
Reverse thrust must be reduced to idle by _____KIAS during landing rollout.
During single engine landing, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
During landing with INOP nosewheel steering, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
During landing on a slippery runway, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
Thrust reversers MAY/MAY NOT be used for backing the aircraft during taxi.
Max temperature (SAT) allowed for use of bleed air anti-ice, except for preflight ops check, is ______degrees C.
Minimum speed/configuration for sustained flight in icing is _______KIAS/ slats up except for approach and landing.
Anti-ice systems MUST/MUST NOT be used to deice surfaces prior to takeoff.
For dispatch, PFE information must be displayed in ___________ and ____________units.
number ONE and number FIVE
Minimum autopilot altitudes for CRUISE?
1000 feet AGL
Minimum autopilot altitude for Precision Approach (CAT 1)?
170 feet AGL
Minimum autopilot altitude for Nonprecision approach?
400 feet AGL
Autopilot coupled operation with inoperative _____ is prohibited.
Autopilot coupled ILS approaches with flaps ____ is prohibited.