Odds and ends Flashcards
Preflight #2 stall warning test
Hold for 5 seconds
Note:
To ensure speed brake auto stow actuator is reset
Preflight Min Crew O2
1000 psi
Preflight HYD QTY
NO RF
Note: less than 102%
Pre Flight Engine oil qty
12 qts
Setting minimums for approach
CAT I set DA
CAT II RA AUTH set RA
CAT II RA Not AUTH set Published DA
CAT III. set 50” DA
Gust Protection
1/2 steady-state + all of the gust
not to exceed 15kts addition
example runway 36
wind 360 @ 20 G 30. 10+10 = 20 so set 15Kts
Rudder trim SE
trim rudder in direction of the low side control wheel
trim rudder to the side you are pressing rudder peddle
Runway centerline lights colors
White every 50 feet to last 3000 feet
red and white for 2000 feet
red for the last 1000 feet
Runway edge lights colors
white then yellow last 2000 feet
runway end lights red on departure green on arrival
RVSM and ALTIMETER CROSS CHECK
The maximum allowable on-the-ground altitude display differences for RVSM operations are:
Max Difference Between Captain & F/O
Field Elevation
Sea Level to 5,000 feet 50 feet.
5,001 to 10,000 feet 60 feet
Max Difference Between Captain or F/O & Field Elevation
75 feet
On the ground, the standby altimeter must be within ±75 feet of the Captain’s and First Officer’s altimeters.
The maximum allowable in-flight difference between Captain and First Officer altitude displays is 200 feet.
Standby altimeters do not meet altimeter accuracy requirements of RVSM airspace.
Quick Reference Minimum Runway Length
8,000 feet Assumptions: • Airport elevation 4,000 ft or less (including KSLC and KDEN) • Touchdown no later than 1,500 ft. from threshold • Up to Max Landing Weight • Autobrakes 3 or greater • Wet or Dry runway • Zero wind and runway slope • Two engines at full reverse thrust Additional stopping performance is available by: • Selecting a higher autobrakes setting • Max manual braking • Landing at a lower altitude • Landing at a lower weight