Normal Operations Flashcards
Runway slope limit is…
- +/- 4%
- +/- 2%
- +/- 3%
- +/- 1%
+/- 2%
Maximum operating altitude is…
- 42,000 ft DA.
- 43,000 ft PA.
- 40,000 ft DA.
- 43,100 ft PA
43,100 ft PA
Maximum takeoff and landing altitude is…
- 14,000 ft pressure altitude.
- 8,500 ft pressure altitude.
- 8000 ft pressure altitude.
- 10,000 ft pressure altitude.
14,000 ft pressure altitude
Turbulent air penetration speed below 25,000 feet is…
- 270 KIAS.
- 285 KIAS.
- 290 KIAS.
- 300 KIAS.
290 KIAS.
Maximum demonstrated crosswind for takeoff is ___ for 787-8, and ___ for 787-9.
- 29 knots, 35 knots.
- 40 knots, 33 knots.
- 33 knots, 35 knots.
- 35 knots, 35 knots.
40 knots, 33 knots.
Maximum demonstrated crosswind for landing is ___ for 787-8, and ___ for 787-9.
- 33 knots, 35 knots.
- 37 knots, 40 knots.
- 30 knots, 29 knots.
- 25 knots, 29 knots.
37 knots, 40 knots.
Do not fly in RVSM airspace on the ________ alone.
- ISFD
- VSD
- HUD
- PFD
ISFD
Prior to takeoff, the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation is…
- 100 ft.
- 75 ft.
- 150 ft.
- 50 ft.
75 ft.
All passengers must be informed of the graphical exit signs, by ___________ prior to each takeoff and landing.
- the FO
- the captain
- an approved briefing
- the flight attendant
an approved briefing
When passengers are carried, the electronically dimmable door windows must be in the _____________ prior to taxi, takeoff and landing.
- dimmable state
- OFF mode
- clear state
- dark state
clear state
An operational check of the Flight Deck Access System is required…
- for every other flight.
- for every flight.
- once each flight day.
- once a week.
once each flight day.
Maximum taxi weight for 787-8 is…
- 500,000 lbs.
- 502,000 lbs.
- 503,500 lbs.
- 490,000 lbs.
503,500 lbs.
Maximum landing weight for 787-9 is…
- 385,500 lbs.
- 380,000 lbs.
- 425,000 lbs.
- 560,000 lbs.
425,000 lbs.
Maximum takeoff weight for 787-8 is…
- 502,500 lbs.
- 502,000 lbs.
- 508,000 lbs.
- 500,000 lbs.
502,500 lbs.
Minimum autopilot engagement altitude after takeoff is…
- 500 ft MSL.
- 200 ft AGL.
- 300 ft MSL.
- 1000 ft AGL.
200 ft AGL.
Without LAND 2 or Land 3 annunciated, the autopilot must be disengaged below…
- 50 ft. AGL.
- 200 ft. MSL.
- 135 ft. AGL.
- 100 ft. DH.
135 ft. AGL.
With LAND 2 or LAND 3 annunciated below 100 ft. AGL and glidepath angles greater than _______, the autopilot must be disengaged below 100 ft. AGL.
- 1.50°
- 3.25°
- 2.95°
- 3.00°
3.25°
If the glidepath angle for approach is greater than 3.77°, the autopilot must be disengaged no later than…
- 75 feet below DH/MDA.
- 100 feet AGL.
- 50 feet MSL.
- 50 feet below DH/MDA.
50 feet below DH/MDA.
Maximum headwind component when landing weather minima are predicated on autoland operations is…
- 20 knots.
- 25 knots.
- 10 knots.
- 15 knots.
25 knots.
Maximum tailwind component when performing autoland operations (may be limited by visibility or runway condition) is…
- 15 knots.
- 10 knots.
- 20 knots.
- 17 knots.
15 knots.
Maximum crosswind component when performing autoland operations (may be limited by visibility or runway conditions) is…
- 17 knots.
- 25 knots.
- 20 knots.
- 15 knots.
25 knots.
Turbulent air penetration at and above 25,000 feet is…
- 270 KIAS/.78 Mach (whichever is lower).
- 325 KIAS/.80 Mach (whichever is lower).
- 310 KIAS/.84 Mach (whichever is lower).
- 290 KIAS/.82 Mach (whichever is lower).
310 KIAS/.84 Mach (whichever is lower).
Autoland capability may be used with both engines operative or with one engine inoperative with flaps…
- 15, 20 and 30.
- 15, 25 and 30.
- 20, 25 and 30.
- 25 and 30 only.
20, 25 and 30.
Automatic landing requires autopilot flight director system (AFDS) autoland status annunciation…
- LAND or LAND 1 displayed.
- LAND or LAND 2 displayed.
- LAND 2 or LAND 3 displayed.
- LAND 1 or LAND 2 displayed.
LAND 2 or LAND 3 displayed.
Use of the captain’s or first officer’s audio control panel (ACP) to _____________ is prohibited.
- make a PA
- establish a SATCOM/cabin conference
- acknowledge a company communication
- establish a cabin conference
establish a SATCOM/cabin conference
Do not operate the _______ - s when refueling.
- HF
- SATCOM
- VHF
- ACARS
HF
For engine start, oil temperature must be greater than…
- -35 ° C.
- -45 ° C.
- -40 ° C.
- -30 ° C.
-40 ° C.
Intentional selection of reverse thrust is prohibited…
- on the ground after landing rollout is complete.
- in flight.
- during taxi.
- during start.
in flight.
Backing the airplane with use of reverse thrust is…
- permitted with a minimum of 2 wing walkers.
- prohibited.
- acceptable provided the ramp is free of slush.
- only acceptable if ground equipment is unavailable to ensure a timely departure.
prohibited.
While operating on the ground with crosswinds greater than ___ knots, limit thrust to a setting normally used for taxi (___ % N1).
- 35, 45
- 20, 30
- 37, 40
- 40, 45
40, 45
While operating on the ground with a tailwind component greater than 5 knots and winds greater than ___ knots, limit thrust to a setting normally used for taxi (___ % N1).
- 35, 45
- 20, 30
- 37, 40
- 40, 40
35, 45
While operating on the ground with winds greater than ______ knots, limit engine thrust to…
- 45, 25% N1.
- 35, flight idle.
- 55, idle.
- 65, 45%
55, idle.
Takeoff is permitted in the ______ flight control mode(s).
- alternate
- normal or direct
- normal
- normal or secondary
normal
Do not extend flaps above…
- 15,000 ft.
- 17,000 ft.
- 20,000 ft.
- 10,000 ft.
20,000 ft.
Do not jettison fuel at…
- speeds below 230 knots.
- the same time as crossfeeding fuel.
- flap settings listed on the FUEL JETTISON control panel placard.
- 7000’’ AFL.
flap settings listed on the FUEL JETTISON control panel placard.
Maximum tank fuel temperature at takeoff is…
- 30 ° C.
- 45 ° C.
- 35 ° C.
- 49 ° C.
49 ° C.
Tank fuel temperature prior to takeoff must not be less than…
- -25 ° C.
- -20 ° C.
- -27 ° C.
- -29 ° C.
-29 ° C.
Inflight tank fuel temperature must be maintained at least ____ above the freezing point of the fuel being used.
- 10 ° C
- 1 ° C
- 5 ° C
- 3 ° C
3 ° C
Notwithstanding an exception allowing as much as 22,000 pounds of fuel in the center tank, with less than full wing tanks, main tanks must be scheduled to be full if center tank fuel is loaded. T/F?
True
Provided center tank fuel weight plus actual zero fuel weight does not exceed the maximum zero fuel weight, and center of gravity limits are observed, the center tank may contain up to _______ pounds of fuel with less than full main tanks.
- 22,000 lbs
- 15,000 lbs
- 5,100 lbs
- 10,000 lbs
22,000 lbs
Do not use the _______________ for navigation.
- TCAS display
- weather radar map mode
- terrain display
- FMC
terrain display
The use of look-ahead terrain alerting and terrain display functions are prohibited within ___ NM of takeoff, approach or landing at an airport or runway not contained in the _____________ database.
- 10, GPWS terrain
- 10, FMC
- 15, GPWS terrain
- 25, FMC
15, GPWS terrain
Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS…
- traffic advisory.
- resolution advisory.
- proximate traffic advisory.
- other traffic advisory.
resolution advisory.
Maximum zero-fuel weight for 787-9 is…
- 355,000 pounds.
- 390,000 pounds.
- 425,000 pounds.
- 400,000 pounds.
400,000 pounds.
Maximum headwind component when takeoff weather minima are predicated on HUD takeoff operations is…
- 20 knots.
- 25 knots.
- 10 knots.
- 15 knots.
25 knots.
Maximum tailwind component when takeoff weather minima are predicated on HUD takeoff operations is…
- 10 knots.
- 20 knots.
- 17 knots.
- 15 knots.
15 knots.
Maximum crosswind component when takeoff weather minima are predicated on HUD takeoff operations is…
- 15 knots.
- 29 knots.
- 20 knot.
- 25 knots.
15 knots.
Boom mics must be used below…
- 18,000 feet.
- 10,000 feet.
- transition altitude.
- cruise altitude.
18,000 feet.
Avoid weather radar operation in a hangar or when personnel are within the area normally enclosed by the aircraft nose radome. T/F?
True
