Systems Limitations Flashcards
Max. Relief diff. Pressure during taxi, TO, and Lndg.
Must not exceed 1.0 psi
Air data system.
Must both air data computers be operational for TO?
YES
Air data system.
For RVSM
ADC source coupled to the active autopilot must be same as coupled ATC transponder during RVSM flight
If alternate static source is selected, airplane must not be operated in RVSM airspace
Can pilot and copilot select alternate static source simultaneously?
No
Operation of auto pilot is prohibited at altitudes below
200 feet AGL
VOR approaches are not permitted with flaps set to
0
Is the auto pilot approved for continued approach following engine failure on final approach?
No
Maximum flap angle for single-engine auto pilot approach
20° with Vref +10 K TS
Use of LNAV mode is not permitted when what is selected?
Lasertrak
For takeoff and landing with cowl and/or wing anti-ice systems on. What applies to the bleed air system?
10 stage bleed air valves must be closed
Air and press. Structural limitation
Max. Relief diff pressure in flight
9.20 psi
AC Generator load limitation
Each Main Generator (0-35,000ft.)
30Kva
AC Generator load limitation
Each Main Generator (35,000 and above)
25 KVA
APU Generator load limitation
30
Maximum load on TRU 1 or TRU 2
100 amps
Maximum continuous load on essential TRU 1 and essential TRU 2 combined
75 amps
If TRU one and TRU two loads are inadvertently exceeded on the ground
The nose bay doors must be open for 10 minutes prior to taxi for take off
Flight with flaps extended is prohibited above
15,500
Flight with spoilers extended is prohibited below
300 feet AGL
Maximum permissible fuel in balance between the contents of the main fuel tanks
800 pounds
Take off with up to 500 pounds of fuel in the auxiliary tank is permitted provided there is at least how much fuel in each wing tank and no fuel in the tail tank
1500 pounds of fuel in each wing tank
Maximum usable fuel quantity is**
Left main tank, 4909 pounds
Right main tank, 4909 pounds
Fuselage tanks, ????
Total, ??? B
Fuel jettison must not be initiated when tail tank quantity is below
30 pounds
Thrust reverse above 60% N1 is not permitted at airspeeds below
60 kts.
Maximum Crosswind component approved for use of reverse thrust is
24 kts.
Taxi light must be switched off whenever the airplane is stationary in excess of
10 minutes
Maximum nose wheel tire pressure
151 PSI +5-0% on the ground
