Brainscape's Knowledge GenomeTM


Top Flashcards (Certified)
All Flashcards

Aviation > Cards > Flashcards

Cards Flashcards

(99 cards)

Start Studying
1
Q

Takeoff is not permitted if there is cold soaked fuel frost on the lower or upper wing tank surface, as follows:

A
  • ambient air temp.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
2
Q

Engine Oil System
Min Oil Pressure ___
Max Oil Temp. ___
Operational limit between 140C & 155C-

A

Min Oil Pressure 13psi
Max Oil Temp. 155C
continuous 144C
Operational limit between 140C or 155C 45min

If oil pressure is in the amber band with T/O thrust set, do not take off

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
3
Q

When EEC’s are used in ALTN mode:

  • defrayed thrust for T/O is ___
  • ___ EEC’s must be in alternate
  • ___ the FMC T/O or Vspeed value
  • use of auto throttle for T/O is ___
A
  • defrayed thrust for T/O is allowed
  • both EEC’s must be in alternate
  • do not use the FMC T/O or Vspeed value
  • use of autothrottle for T/O is prohibited
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

Don’t use which radio for ATC voice comm with ACARS operational?

A

VHF-3

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
5
Q

Air Data Internal Reference Unit ADIRU alignment must not be attempted at altitudes greater then ___

A

78 deg 15 min

78.25 deg N/S

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
6
Q

Precipitation on Runway
T/O and Landing are prohibited when:

Slush ___
Wet Snow ___
Dry Snow ___

A

Slush at or above 13mm
Wet Snow at or above 51mm
Dry Snow at or above 71mm

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
7
Q

True or False…

Porous friction course runway should be treated as grooved runways

A

True

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
8
Q

Name three situations where the Center Tank Fuel Pumps should be turned off on the ground

A
  • no personnel are available on the flight deck to monitor the low pressure lights
  • center tank quantity not greater then 1000 lbs (453 kg) unless refueling or transferring
  • when the low pressure light illuminates (both off of quantity zero)
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Maximum Flight Operating Latitude

A

82 deg North to 82 deg South

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

Maximum Tank Fuel Temperature

A

49C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
11
Q

Do not use terrain display for ___

A

Navigation

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

In flight, do not extend the speed break lever beyond ___

A

Flight Detent

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
13
Q

Engine EGY limit for T/O, max continuous and Start

A

T/O 950C 5min (OEI 10min)
Max continuous 925C
start 725C

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
14
Q

Installation of handle covers on the overwing exit must be verified when?

A

Prior to departure whenever passengers are carried

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
15
Q

Max allowable wind speeds when landing weather minima are predicted on auto land operations:
Headwind ___
Crosswind ___
Tailwind ___

A

Headwind 25
Crosswind 20 (15 for RAM)
Tailwind 10

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

Do not use ___ ___ ___ as a substitute for ground de-icing/anti-icing and inspection procedures

A

Wing anti-ice system

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
17
Q

Minimum Flight Crew requirement

A

Captain & FO

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
18
Q

Vmo/Mmo

A

340kt/0.82M

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
19
Q

Max weight basic

A

ZFW 61,688
Landing 65,317
T/O 79,015
Taxi 79,242

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
20
Q

Describe the Fuel Usage requirements

A

With no fuel in the center tank use main tank to engine (main tanks pumps on, center tank pumps off, cross feed closed)

With fuel in the center tank use center tank fuel (all pumps on, cross feed closed) until center tank fuel depleted to (1000lbs=453kg may be retained in center if balance has been considered)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
21
Q

If Braking Action divides the runway into three sections, which one is applied to T/O and Landing

A

The worst of the three weather is for T/O and Landing

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
22
Q

Intentional dry running of a center tank fuel pumps (low pressure light illuminated) is ___

A

Prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q 
True or False...
The following fuels are allowed for use in the B737-800:
- Jet A
- Jet B
- JP-4
A

False
Only Jet A
Jet B & JP-4 is prohibited

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
24
Q

Do not operate the weather radar where?

A

In hangar or
Within 50 feet of any personnel or
Fuel spill

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
25
Do not deploy speed breaks in flight bellow ___
1000ft AGL
26
Engine RPM max are: N1 (low press compressor) N2 (high press compressor) APU
N1 104% (continuous) 104.7% (20 sec) N2 105% (continues) APU 106%
27
True or False... | Use of the aileron trim with the autopilot engaged is prohibited
True
28
Engine Anti-Ice must be on ___
during all god and fly ops when icing conditions exist or are anticipated, except during climb and cruise when temp is below -40C SAT Eng A/I must be on prior to and during descent in all icing conditions regardless of temp
29
Landing Gear Placard Speed (Vlo and Vle)
Retract 235kt Extend 270kt/.82M Extended 320kt/.82M Note: verify LDG Gear Limit (IAS) on placard under LDG Gear Lever during normal operations
30
Maximum demonstrated crosswind: Non Winglets ___ With Winglets ___
Non Winglets 36kt | With Winglets 33kt
31
The Fuel cross feed Valve is open for?
- minimum fuel operation | - to correct fuel imbalance
32
Fuel Loading | If the center tank is going to have more than 1000lbs (453kg) the main wing tank ___
Must be scheduled to be full
33
When must Engine Ignition be on
Must be on for: - T/O - Landing - heavy rain and - anti-ice operation
34
Engine Limit Display Markings Maximum and minimum engine limits are a ___ Cautionary range is marked by ___ Normal operating range is marketed by ___
Max/ min Red line Cautionary Amber arc Normal White arc
35
For single channel operation during approach, the autopilot shall not remain engaged below ___
158ft AGL EASA Certified
36
Icing conditions exist when ___
The OAT on the god or TAT in fly is 10C or less and visible moisture in any form is present Also when on ground with temp 10C or less where surface snow, ice, flooded or slush may be ingested by the engines or freeze on the engines or nacelles
37
Verify the flap limit (IAS) on the ___ during normal operations
Placard under the landing gear lever
38
Maximum T/O and Landing Altitude
8400ft
39
Fuel Loading Load main tanks ___ to the desired quantity or until full
Equally 3915kg full
40
Max allowable in flight difference between Capt & FO altitude display for RVSM ops is:
200ft
41
Holding in icing conditions with flaps extended is ___
Prohibited
42
Do not engage the autopilot after T/O below ___
400ft AGL
43
With engine bleeds on do NOT operate packs in High for ___, ___ or ___ (except for cargo fire and smoke or fumes removal checklist. Switches need to be in Hight to open the overboard exhaust valve)
T/O Approach Landing
44
Flaps packers speed Vfe
``` 1, 2, 5 250kt 10 210kt 15 200kt 25 190kt 30 175kt 40 162kt ``` Alternate flaps 230kt
45
Maximum operating altitude
41 000ft
46
If operating with secondary airframe or engine parts missing, the airplane must be operated in accordance with ___
MEL
47
Fuel imbalance must not exceed ___ for taxi, T/O flight or landing
453kg
48
Max allowable fuel weights Main tanks ___ Center tank ___ Total ___
Main tank No 1 and 2 3 915kg Center tank 13 066kg Total 20 896kg
49
Maximum allowable on ground altitude display difference:
Airfield elevation below 5000ft - 50ft (cpt & FO); between 5000 and 10000ft - 60ft (cpt & FO) 75ft (elevation)
50
Photo luminescence Floors emergency lights must be ___ in accordance with approved procedures
Charged
51
What flap setting may be used for Auto Land?
30 & 40 (and both engines must be operating)
52
Max allowable cabin pressure difference risk for T/O and Landing
0.125 psi (236 feet below airport pressure altitude)
53
Max tailwind
10kt
54
True or False... | For executing a short field landing hold the break prior to touchdown
FALSE Do not apply break until after touchdown
55
Minimum in flight tank fuel temperature
-43C or 3 degrees above fuel freezing point, whichever is higher
56
The use of look ahead terrain alerting and display functions are prohibited where?
Within 15NM of T/O, approach or landing at an airport not in the GPWS database
57
Standby altimeter ___ altimeter accuracy requirements of RVSM
does not meet
58
Which of the following does the EEC monitor? N1 N2 EGT
N1 & N2 all the time EGT only during engine started
59
The flight deck door access system must be verified operational how often?
Once each every flight day
60
Maximum and minimum glide slope angles for auto land are
2.5 - 3.25 deg
61
Don’t operate wing anti-ice when the OAT is ___
Above +10C OAT
62
Max cabin differential pressure | Relief valve
9.1 psi
63
What’s the definition of Va
Va is maneuvering speed And is the speed above which maneuvers involving full rudder, aileron or elevator, or maneuvers near stall AOA should be avoided
64
Runway slope
+/-2%
65
Avoid ___ control inputs especially in combination with large changes in pitch, roll and yaw (e.g. ___) as they may result in structural failure at any speed, including below Va
Rapid and large alternating Large side slip angles
66
Max flap extension altitude
20 000ft
67
APU bleed valve must be closed when?
- ground air connected and isolation valve open - eng no. 1 bleed air valve open - eng no. 2 bleed air valve open and isolation valve open Except: APU bleed may be open during eng start but avoid thrust above idle
68
APU max altitudes: - bleed & electrics ___ - bleed only ___ - electric only ___
- bleed & electrics 10 000ft - bleed only 17 000ft - electric only 41 000ft
69
When can you use reverse thrust
Ground operations only
70
Full T/O thrust (26k) must be checked ___
Periodically
71
width/length/height of b737 with winglets
35.8/39.5/12.5
72
oxygen masks will automatically fell down at ____
14,000ft cabin altitude
73
passenger oxygen mask provide oxygen for _____ min
12 min
74
window heat needs to be on _____ min before T/O
10 min
75
autobreak will work above ____ speed
90kt
76
stearing wheel angles are for ruddeer/stearing wheel
7 degrees/78 degreees
77
capacity of main tanks and central tank (total)
3,915 kg and 13,066 kg (20,896 kg)
78
EGT at T/O ____ Max continue ____ engine start ____
950 C (for 5 min/ OEI 10min) 925 C 725 C
79
Flight Manoeuring Load Acceleration Limit Flaps UP is _____ Flaps DOWN is _____
+2.5g to -1g | +2g to 0g
80
Max cabin diff for T/O & Landing is...
0.125 psi (236 ft below airport PA)
81
Maximal altitude for one pack inoperative T/O is...
FL250
82
Engine anti-ice must be ON during...
all ground and flight operations when icing conditions exists or are anticipated, except during climb and cruise below -40C SAT. ...prior and during descent in all icing conditions including temperatures below -40C SAT
83
Do not use wing anti-ice on the ground when OAT is above...
10C
84
Max EGT | Max Continuous EGT
760C | 710C
85
Engine Max temperatures...
155C; 140C-150C (45min limit); 140C continious
86
Engine minimum oil pressure and quantity (at dispatch)
13 psi; 75% full (3 US Gal) + 1% for each hour of flight
87
Engine stabilised indications
N1 20% N2 59% EGT 320C-520C FF 272 kg/h
88
Operating on stanby power only provides _____ available time
60 minutes
89
TR Unit voltage
24-30 V
90
Battery voltage
22-30 V
91
IDG max temperature
157C
92
Autobreak are not allowed with...
antiskid inoperative
93
T/O with antiskid inoperative is only allowed from ____ RWYs
dry
94
Use of the Vertical Situation Display (VSD) with the altimeters refer to QFE is...
prohibited
95
On the ground the center tank pumps must be OFF if center tank fuel quantity is below...
453 kg
96
Fuel crossfeed valve must be closed for...
T/O & Landing
97
Minimum required for dispatch quantity of hydraulic fluid is...
88% (86-87%?)
98
For electrical hydraulic pump cooling a minimum of ____ fuel is required in respective main tanks
760 kg
99
In case of lost of standby hydraulic fluid the system B will indicated a quantity of...
72%

Aviation (3 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2025 Bold Learning Solutions. Terms and Conditions