Minimum altitude for in-flight use of speed brakes
500 feet
Max asymmetric fuel
400 Pounds
Emergency aymmetric fuel
800 Pounds
Minimum wing fuel per tank for TO
500 Pounds
Only the Goodyear 164F03-1, -2 nose tire is approved, what is the inflated pressure, unloaded
130+-5 PSIG
Mmo above 30650 feet?
0.92 Mach
Mmo Mach trim off?
0.82 Mach
Vmo 8000 feet to 30650 feet?
350 KIAS
Vmo below 8000 feet?
270 KIAS
Max Altitude for EXT of Flaps or Gear
18000 Feet
Max Slat EXT Speed?
250 KIAS
Max Flap EXT-5 Speed?
250 KIAS
Max Flap EXT-15 Speed?
210 KIAS
Max Flap EXT-FULL Speed?
180 KIAS
Max Landing Gear Operating/Ext Speed
210 KIAS
Max turbulent Air Penetration Speed
300 KIAS / 0.9 Mach
Max Speed Brake Extension Speed
No Limit
Minimum Speed Brake Extension Speed
Vref +15 KIAS
Minimum Single Engine Enroute Climb Speed
190 KIAS
Max Tire Ground Speed
210 Knots
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
10 seconds
G force upon landing
3.5 at MLW
The acceleration limit (G force) upon landing is _________feet per minute descent.
600
The acceleration limit (G force) during flight restrict angle of bank and severity of ____________maneuvers.
pullup
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.
3, 30
DO / DO NOT engage the Air Turbine Starter above 25% N2 RPM.
DO NOT
Engine Type is an AE-3007C1 Turbofan, It has _____ fadecs. Must all be operational for dispatch?
4, yes
For TO, all the Micro Air Data Computers must be operational, how many are there?
2
Minimum start duct pressure (EICAS) prior to ground start
25 PSI
Time limit in the TO/MC detent?
5 minutes
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?
100
Time limit in the CLB detent?
Continuous
When should the CRU detent be selected after level-off from TOC?
10 minutes
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).
IDLE
DO NOT exceed ______percent N1 until engine fuel TEMP is greater than 4 degrees C (cold days).
40%
FADEC automatic overspeed shutdowns are set for _______N1 and ________N2
105%, and 105.6%
The Minimum Fan Speed for TO is ________.
73.6%
FADEC wil shut the engine down if the N2 is at or below ______%.
54
Windmilling AIR Start ITT limit is _______degrees C.
888
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 ________.
55 PSIG
Max pressure of the defueling system is ________.
-10 PSIG
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.
3100
Simultaneous use of crossfeed and center-to-wing tank transfer is prohibited when the wing quantity is at or less than ______.
2900 pounds
During application of deicing fluid, the APU should ________.
not be operating
The APU may or may not be left operating while unattended.
May Not
Max operating Altitude for the APU
31000 feet
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.
6, one
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.
-20
The battery cycle limit is _______APU starts in ONE HOUR. If this is exceeded maintenance is indicated.
6
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
41000 feet
Use of the baggage compartment is not authorized with the cabin ____________.
unpressurized.
Max weight of the baggage in the baggage compartment is
700 pounds
Max floor loading distribution is __________per square foot.
170 pounds
max weight in the ski holding compartment is
75 pounds
Operation in the HIGH mode for the cockpit and cabin PAC selector switches is not approved for __________and____________. TO/landing and
45000 feet
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.
25000 feet
Single PAC ops is not approved for altitudes above _____________.
41000 feet.
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.
Pneumatic AI
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 __________.
40000 feet
Passenger Oxygen masks are not approved for sustained operation at a CABIN altitude greater than _____________.
25000 feet.
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?
TRUE
Both Rudder limiters must be operational for flight? T/F
TRUE
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.
15000 feet
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.
65
During single engine landing, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
70
During landing with INOP nosewheel steering, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
70
During landing on a slippery runway, thrust reverse must be reduced to idle by _______KIAS during landing rollout.
70
Thrust reversers MAY/MAY NOT be used for backing the aircraft during taxi.
MAY NOT
Max temperature (SAT) allowed for use of bleed air anti-ice, except for preflight ops check, is ______degrees C.
+20
Minimum speed/configuration for sustained flight in icing is _______KIAS/ slats up except for approach and landing.
200
Anti-ice systems MUST/MUST NOT be used to deice surfaces prior to takeoff.
MUST NOT
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.
IRS
Autopilot coupled ILS approaches with flaps ____ is prohibited.
