Hodgepodge Flashcards
1
Q
When must you request landing data
A
- Landing at other than planned destination
- Available runway less than 9000’
- Reported breaking action less than dry
- Using auto brakes less than 3
- Non-normal aircraft condition affecting stopping distance
- Landing with a tailwind
- Engine inoperative
2
Q
When must you request new takeoff data
A
- Using max thrust data, actual OAT>Assumed temperature
- Using reduced thrust data, actual OAT>Assumed temperature
- Altimeter setting decreases by .03 inches
- CG difference between FWM CG value and Takeoff Ref pg CG exceeds 3%
- GW at takeoff is greater than Assumed wt uploaded to TOW
3
Q
Autothrottle Disengaged Target Speed
A
1/2 the steady state winds + Full gust value
4
Q
The engines should be run at idle thrust for at least how many minutes prior to takeoff?
A
3 min
5
Q
If the engines have been shutdown for more than __ hrs, they should be run at idle thrust for at least ___.
A
5 hrs, 5 minutes
6
Q
Stabilized Approach Criteria
A
- Plan- Gear down, Airspeed < 180 kts by 1500’ AGL or FAF
- Report- Final landing configuration, checklist complete by 1000’ AGL
- Reject- “Stable” or “Unstable, going around” by 500’ AGL
7
Q
Short field or contaminated runway (7,500’)
A
- Flaps/Autobrakes- 3 or MAX (Dry), Flaps 40 autobrakes MAX (Wet)
- Aimpoint- 200’ RA, shift slightly toward threshold. PAPI one white, three reds
- Flare- 20’ Thrust idle at TD
- Touchdown- 1000’ from Threshold, max reverse
GO AROUND IF LANDING NOT ASSURED BY 1500’
8
Q
Pilot LAHSO Procedures
A
- LAHSO procedures must be provided on the airport info pages (10-7)
- LAHSO must be noted on ATIS or advised by ATC
- The tailwind on the hold short runway must be calm
- Dry runway
- Weather no less than 1000 ft and 3 sm with VASI/PAPI
- Weather no less than 1500 ft and 5 sm with no VASI/PAPI
9
Q
Final weight manifest- Advise the Captain and contact dispatch if any of the following apply:
A
- Actual takeoff weight (GW) is greater than the flight plan TOW + 2000 lbs
- The actual takeoff weight (GW) will exceed the M1 ENRTE ATOG (if planned Method 1)
- CALL DD is displayed on the Final Weight Manifest