Hawaiian 787 > Limitations > Flashcards

Limitations Flashcards

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1
Q

What is the maximum takeoff and landing tailwind component for the aircraft?

A

15 knots

This is a critical limitation for safe aircraft operations during takeoff and landing.

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2
Q

What is the maximum operating altitude for the aircraft?

A

43,100 ft pressure altitude

This altitude limit is essential for flight planning and operational safety.

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3
Q

What is the maximum takeoff and landing altitude for the aircraft?

A

14,000 ft pressure altitude

Exceeding this altitude can affect aircraft performance and safety.

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4
Q

What should not be operated when refueling?

A

HF radios

This is a safety precaution to prevent ignition hazards.

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5
Q

True or False: The standby altimeter meets RVSM altimeter accuracy requirements.

A

False

The standby altimeter does not meet the required accuracy for RVSM airspace.

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6
Q

What must all passengers be informed of prior to each takeoff and landing?

A

Graphical exit signs

This is part of the approved briefing to ensure passenger awareness.

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7
Q

What must be armed prior to taxi, takeoff, and landing whenever passengers are carried?

A

Main door emergency power assists and evacuation slide systems
Whenever passengers are carried

This is crucial for passenger safety during emergencies.

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8
Q

What condition must the electronically dimmable door windows be in before taxi, takeoff, and landing?

A

Clear state

Whenever passengers are carried

This ensures visibility and safety during critical phases of flight.

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9
Q

What must be charged in accordance with approved procedures for emergency situations?

A

Photoluminescent floor emergency lighting

This lighting aids in passenger evacuation in low visibility situations.

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10
Q

What must be verified once each flight day regarding the Flight Deck Access System?

A

An operational check

This enhances flight deck security and operational readiness.

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11
Q

What is the maximum demonstrated crosswind for takeoff?

A

33 knots (gust included)

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12
Q

What is the maximum demonstrated crosswind component for landing?

A

40 knots (gust included)

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13
Q

Are the demonstrated crosswinds operational limitations?

A

No, they are for certification only

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14
Q

What is the severe turbulent air penetration speed below 25,000 feet?

A

290 KIAS

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15
Q

What is the severe turbulent air penetration speed at and above 25,000 feet?

A

310 KIAS/.84 Mach (whichever is lower)

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16
Q

What should be avoided regarding weather radar operation?

A

Operation in a hangar and when personnel are within the area normally enclosed by the aircraft nose radome

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17
Q

What does the hangar recommendation not apply to?

A

Weather radar test mode

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18
Q

What is the maximum allowable difference between Captain’s or First Officer’s altitude display and field elevation prior to takeoff?

A

75 feet

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19
Q

What is the maximum Center of Gravity (% MAC) for takeoff?

A

30%

This limit applies to the aircraft’s configuration during takeoff.

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20
Q

What is the crosswind component limit for a runway condition code of ‘Good’?

A

40 knots

Crosswind limits vary based on runway conditions.

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21
Q

What is the crosswind component limit when the runway condition is ‘Poor’?

A

10 knots

This limit reflects the challenges of takeoff in poor conditions.

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22
Q

What adjustment should be made to takeoff crosswind guidelines if thrust is above 40% N1?

A

Reduce by 5 knots

This adjustment is specific to GE engines at brake release.

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23
Q

What is the maximum crosswind component for a dry runway?

A

40 knots

This applies for runways 148 feet (45m) or greater in width.

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24
Q

What is the crosswind component limitation when landing on untreated ice or snow?

A

Nil

Landing on untreated ice or snow will only be attempted when no melting is present.

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25
What is the recommended crosswind limit for sideslip only landings?
25 knots ## Footnote Sideslip only landings are not recommended with crosswind components in excess of 25 knots.
26
What crosswind component is allowed when landing on standing water/slush?
20 knots ## Footnote This is a specific limitation for wet conditions.
27
What is the crosswind limitation for snow without melting?
35 knots ## Footnote This applies for snowy conditions without melting.
28
What is the crosswind limitation for ice without melting?
17 knots ## Footnote This applies for icy conditions without melting.
29
What should be done to the crosswind limitation on wet or contaminated runways when asymmetric reverse thrust is used?
Reduce by 5 knots ## Footnote This is a safety measure to ensure better control.
30
What is the maximum taxi weight for Hawaiian Airlines 787?
563,000 Pounds
31
What is the maximum takeoff weight for Hawaiian Airlines 787?
561,500 Pounds
32
What is the maximum landing weight for Hawaiian Airlines 787?
425,000 Pounds
33
What is the maximum zero fuel weight for Hawaiian Airlines 787?
400,000 Pounds
34
What is the minimum engage altitude for the autopilot after takeoff?
200 feet AGL
35
What is the maximum airport field elevation for autoland capability?
8400 feet
36
Below what altitude must the autopilot be disengaged without LAND 2 or LAND 3 annunciated?
135 feet AGL
37
At what altitude must the autopilot be disengaged with LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees?
100 feet AGL
38
At what altitude must the autopilot be disengaged if the glidepath angle for approach is greater than 3.77 degrees?
50 feet below DH/MDA
39
What is the maximum taxi weight for Hawaiian Airlines 787?
563,000 Pounds
40
What is the maximum takeoff weight for Hawaiian Airlines 787?
561,500 Pounds
41
What is the maximum landing weight for Hawaiian Airlines 787?
425,000 Pounds
42
What is the maximum zero fuel weight for Hawaiian Airlines 787?
400,000 Pounds
43
What is the minimum engage altitude for the autopilot after takeoff?
200 feet AGL
44
What is the maximum airport field elevation for autoland capability?
8400 feet
45
Below what altitude must the autopilot be disengaged without LAND 2 or LAND 3 annunciated?
135 feet AGL
46
At what altitude must the autopilot be disengaged with LAND 2 or LAND 3 annunciated and glideslope angles greater than 3.25 degrees?
100 feet AGL
47
At what altitude must the autopilot be disengaged if the glidepath angle for approach is greater than 3.77 degrees?
50 feet below DH/MDA
48
What guidance must be used for low visibility takeoff?
ILS guidance on U.S. Type II or Type III ILS facilities
49
What is the maximum headwind component speed for HUD takeoff operations?
25 knots
50
What is the maximum tailwind component speed allowed during HUD takeoff operations?
15 knots
51
What is the maximum crosswind component speed for HUD takeoff operations?
20 knots
52
What are the maximum wind component speeds for automatic landing?
Headwind: 25 knots, Tailwind: 15 knots, Crosswind: 25 knots (15 KTS for CAT II/III)
53
What is the maximum glideslope angle for autoland operations?
3.25 degrees
54
What is the minimum glideslope angle for autoland operations?
2.5 degrees
55
With what flap settings can autoland capability be used?
Flaps 20, 25, or 30
56
What must be displayed for AFDS autoland status annunciation?
LAND 2 or LAND 3
57
What is required for low visibility operations using HUD TO/GA?
Operational approval
58
Is the use of FLCH allowed on final approach below 1,000 feet AFE?
No
59
What is prohibited regarding the Audio Control Panel (ACP)?
Use of the captain's or first officer's ACP to establish a SATCOM/cabin conference
60
What is the limitation for Takeoff and Go-Around Thrust Rating?
Limited to 5 minutes, or 10 minutes in the event of loss of thrust on one engine.
61
What is the minimum oil temperature required for engine start?
Greater than -40° C.
62
Is intentional selection of reverse thrust in flight permitted?
No, it is prohibited.
63
Is backing the airplane with the use of reverse thrust allowed?
No, it is prohibited.
64
What thrust setting should be used for crosswinds greater than 40 knots?
Limit thrust to a setting normally used for taxi (45% N1).
65
What is the thrust limitation with a tailwind component greater than 5 knots and winds greater than 35 knots?
Limit thrust to a setting normally used for taxi (45% N1).
66
What should be the engine thrust setting for winds greater than 55 knots?
Limit engine thrust to idle.
67
In what flight control mode is takeoff permitted?
Normal flight control mode.
68
What should be avoided to prevent structural failure?
Rapid and large alternating control inputs, especially with large changes in pitch, roll, or yaw.
69
What is the maximum altitude with flaps extended?
20,000 feet.
70
What must be done with the Electronic Flight Bag (EFB) portable keyboard during takeoff?
Must be stowed.
71
What is the maximum tank fuel temperature at takeoff for Jet A, Jet A-1, JP-5, JP-8 or TS-1?
49° C (120° F)
72
What is the inflight fuel temperature limit for Jet A, Jet A-1, JP-5 or JP-8?
65° C (150° F)
73
What is the inflight fuel temperature limit for TS-1 at or above 35,000 feet?
57° C (135° F)
74
What is the inflight fuel temperature limit for TS-1 below 35,000 feet?
65° C (150° F)
75
What is the minimum tank fuel temperature prior to takeoff?
-29° C (-20° F)
76
What must in-flight tank fuel temperature be maintained at?
At least -42° C and 3° C above the freezing point of the fuel
77
Does the use of Fuel System Icing Inhibitor additives change the minimum fuel tank temperature limit?
No
78
What is the requirement for main tanks when center tank fuel is loaded?
Main tanks must be scheduled to be full
79
What is the maximum fuel weight allowed in the center tank if main tanks are not full?
Up to 22,000 pounds
80
What must be observed when loading fuel in the center tank?
Maximum zero fuel weight and center of gravity limits
81
Is the terrain display allowed for navigation according to GPWS limitations?
No
82
Within what distance from takeoff, approach, or landing is the use of look-ahead terrain alerting prohibited?
15 NM
83
What is prohibited when approaching or landing at an airport not contained in the GPWS terrain database?
Use of look-ahead terrain alerting and terrain display functions
84
What are pilots authorized to do in relation to TCAS resolution advisories?
Pilots are authorized to deviate from their current ATC clearance to the extent necessary to comply with a TCAS resolution advisory.
85
What must evasive maneuvers not be based solely on according to TCAS guidelines?
Evasive maneuvers must not be based solely on information from the traffic display or traffic advisory (TA) without visually sighting the traffic.
86
Fill in the blank: Evasive maneuvers must not be based solely on _______.
information from the traffic display or traffic advisory (TA)
87
True or False: Pilots can rely entirely on traffic advisories for evasive maneuvers.
False
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