Term
The Citation 560 is certified under which CFR part? |
|
Definition
CFR part 25; certification of transport aircraft |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
Minimum in-flight weight? |
|
Definition
|
|
Term
|
Definition
|
|
Term
What are your takeoff weights limited to? |
|
Definition
Takeoff weight is limited to: A. max takeoff weight B. climb performance/gradient requirements C. runway lengths |
|
|
Term
What are your landing weights limited to? |
|
Definition
A. maximum landing weight B. brake energy and climb requirements C. runway landing distance |
|
|
Term
|
Definition
Pratt & Whitney PW545C turbofans |
|
|
Term
Normal engine oil pressure below 60% N2 |
|
Definition
|
|
Term
Normal engine oil pressure above 60% N2 |
|
Definition
|
|
Term
100% N2 corresponds to how many RPM's? |
|
Definition
|
|
Term
100% N1 corresponds to how many RPM's? |
|
Definition
|
|
Term
What is maximum takeoff power, in percent N1 & N2? |
|
Definition
|
|
Term
How many minutes may max takeoff power be maintained? |
|
Definition
-for temperatures below 30 C; 5 minutes -for temperatures above 30 C; 4 minutes -during OEI; 10 minutes |
|
|
Term
What is the maximum inter-turbine temperature(ITT) for takeoff? |
|
Definition
|
|
Term
What are the limitations on the starter? |
|
Definition
3 engine starts per 30 minutes, but a 90-second rest period must be given between cycles |
|
|
Term
What is are the starting limitations on the battery? |
|
Definition
3 engine starts per hour. Using a GPU does not count as a battery-assisted start, and a cross generator start counts as 1/3 of a battery start. |
|
|
Term
|
Definition
Skydrol 500A, B, B-4, C or LD-4 |
|
|
Term
|
Definition
Should be 1 quart per 10 hours, any more than this, consult the manual |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
Full flaps - 35 degrees - 175KIAS Partial flaps - 7 to 15 degrees - 200KIAS |
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
None; may be deployed at any speed |
|
|
Term
What could occur if the speed brake is deployed near Mmo? |
|
Definition
The nose-down pitch attitude created by the deploying the speed brakes may be enough to exceed Mmo. Furthermore, the increase in AoA to raise the nose may cause mach buffet due to the increased speed/flow of air over the wings. |
|
|
Term
Max speed for autopilot operation? |
|
Definition
Mmo (.75 mach) or 305 KIAS |
|
|
Term
Minimum speed for sustained FIKI operations? |
|
Definition
|
|
Term
Can the 560XL be operated off on other-than-paved surfaces? |
|
Definition
No. limited to paved runways. |
|
|
Term
Maximum operating altitude? |
|
Definition
|
|
Term
Maximum operating altitude with a VG missing? |
|
Definition
|
|
Term
How many VG's may be missing to continue a flight? |
|
Definition
|
|
Term
What is the highest altitude that flaps/gear may be operated? |
|
Definition
|
|
Term
|
Definition
52 total, 26 per wing. 3 may be missing and the flight continued. |
|
|
Term
How many boundary layer energizers? |
|
Definition
22 total, 11 per wing. All must be present for the flight to be dispatched. |
|
|
Term
What is the green circle on the PFD airspeed tapes? |
|
Definition
represents your approach speed ...or 1.3VS1 ...Vref |
|
|
Term
When will the stick shaker activate? |
|
Definition
at any point that an impending stall is suspected; stick shaker is a function of AoA |
|
|
Term
What is the normal cabin pressure range? |
|
Definition
|
|
Term
When will the pressure relief valve open? |
|
Definition
above 9.5 psi, or when the differential pressure exceeds +/- 0.1 psi |
|
|
Term
What is the red line on the cabin pressure gauge? |
|
Definition
|
|
Term
Type of avionics package? |
|
Definition
Rockwell Collins Pro Line 21 and FCS-3000 |
|
|
Term
What type of APU is installed and where? |
|
Definition
Honeywell RE100(XL) gas turbine installed in the tailcone. |
|
|
Term
When can the APU be used? |
|
Definition
APU operation is approved for both ground and in flight operations. |
|
|
Term
What purpose does the APU serve on the ground? |
|
Definition
The APU provides supplemental electrical power for engine starting, and also bleed-air for cooling and heating of the cabin during ground op's. |
|
|
Term
What could cause excessive loads on the APU during starting? |
|
Definition
leaving the 'MAX COOL' selected on the APU control. This draws an excessive amount of air away from the combustor, and may exceed the APU EGT limits due to a lack of cooling. |
|
|
Term
What is the APU fuel burn on the ground? |
|
Definition
|
|
Term
APU fuel burn with bleed air load on the ground? |
|
Definition
|
|
Term
|
Definition
|
|
Term
|
Definition
Flight Guidance Computer; two aboard the aircraft working either together (x-checking) or independently in APPR and GA modes |
|
|
Term
|
Definition
Primary servos for the pro line 21; three aboard the aircraft |
|
|
Term
What kind of radio altimeter is installed? |
|
Definition
|
|
Term
When does the radio altimeter become active? |
|
Definition
when the electrical system is turned on |
|
|
Term
What is the max altitude of the radio altimeter? |
|
Definition
|
|
Term
What is the range of the weather radar? |
|
Definition
Forward facing, 60 degrees to either side, out to 300 nm. Can sense moisture-based turbulence. |
|
|
Term
|
Definition
1006 gallons (approx. 6,790 lbs) |
|
|
Term
Describe the fuel system: |
|
Definition
Fully automatic when in normal operation; Fuel ejectors in each tank supply fuel to the engine-driven pump, which supplies the fuel control unit. |
|
|
Term
at what psi will the fuel boost pump automatically turn on? |
|
Definition
If the fuel supply to the engine-driven pump falls below 5 psi, the boost pump will turn on. |
|
|
Term
What will inform the crew that the engine-driven fuel pump is receiving less than 5 psi? |
|
Definition
FUEL BOOST PUMP L or R CAS |
|
|
Term
In the event that the boost pressure to the engine driven pump falls below the required pressure, will the FUEL PRESS LOW (L or R) CAS stay illuminated indefinately? |
|
Definition
No. The FUEL PRESS LOW CAS will illuminate momentarily (if at all) until the boost pump activates, then at least 5 psi is maintained to the engine -driven pump. |
|
|
Term
Where does the fuel go after it leaves the engine-driven pump? |
|
Definition
|
|
Term
Where does the metered fuel go after leaving the FCU? |
|
Definition
metered fuel from the FCU supplies two manifolds at the combustor (PRI and SEC) |
|
|
Term
What does the GROUND DISPATCH feature provide? |
|
Definition
provides power to avionics essential for receiving inputting clearances/routes into the FMS. |
|
|