Brainscape's Knowledge GenomeTM

Browse over 1 million classes created by top students, professors, publishers, and experts.


See full index

DELTA > SLOD > Flashcards

SLOD Flashcards

1
Q

Minimum recommended taxiway width for 180 degree turn

A

81 Feet

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

Minimum flight crew oxygen for dispatch

A

1,000 PSI

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

Minimum quantities for engine oil

A

Maintenance Stations: 9 QTS
Non-Maintenance Stations: 7 QTS
(Displayed on Secondary Engine SD synoptic)

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

Minimum hydraulic quantities

A

7 QTS per system
(Displayed on the Hydraulic SD)

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

Function of the EMER LT Switch (Off, Arm, On)

A

OFF: Extinguishes emergency lights (battery packs are being charged)
ARM: Normal Position (battery packs are armed)
ON: Activates emergency battery packs

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

Function of LDG LT Switches (RET, EXT OFF, EXT ON)

A

RET: Retracts landing lights flush with wing
EXT OFF: Extends lights with lamps off
EXT ON: Extends lights with lamps on

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

Function of NOSE LT Switch (OFF, TAXI, LDG)

A

OFF: Extinguishes nose gear landing/taxi lights
TAXI: Illuminates light for taxi (DIM)
LDG: Illuminates lights for takeoff/landing (BRIGHT)

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

Function of WING NACL Switch (OFF, RUN, R ONLY)

A

OFF: Turns off leading edge and engine nacelle floodlights
ON: Illuminates wing leading edge and engine nacelle floodlights
R ONLY: Illuminates right leading edge and engine nacelle floodlights (used by ground)

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
9
Q

Maximum Aircraft Takeoff Weight (MTOW)

A

121,000 LBS

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

Maximum Aircraft Landing Weight (MLW)

A

110,000 LBS

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

Maximum Aircraft Taxi Weight (MTW)

A

122,000 LBS

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

Maximum Aircraft Zero Fuel Weight (MZFW)

A

100,500 LBS

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

Maximum Lateral Fuel Imbalance

A

1,500 LBS

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

Considerations for Center Tank Fuel Pumps

A

Prior to engine start where the center tank fuel is present, center tank pumps must individually be checked to verify pump operation

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

Speedbrake limitation with flaps extended

A

Speedbrakes may not be used with flaps extended beyond 20

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

Function of the PASS OXY MASK Switch

A

Eject: Opens all overhead oxygen compartment doors (Holding longer than 5 seconds can damage the oxygen compartment latches)

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

How many emergency exits are there

A

9 Total
7 Emergency Exit Doors
2 Sliding Cockpit Windows

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

Function of the Avionics Cooling Switch (FAN, OVRD)

A

The Switch is operative in flight only
FAN: Primary fan cools radios. If fails, backup fan comes on automatically
OVRD: Radio rack fans are off, the venturi valve is commanded open and airflow cools radio

On the ground, both fans stay on and venturi valve is closed

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

Function of the RAM Air Switch (OFF, ON)

A

OFF: RAM Air valve is closed
ON: RAM Air valve is open allowing ram air to enter the conditioning ducts

Provides ventilation for the cabin and cockpit when air conditioning is not available - Do not have in ON position on the ground

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

Function of the PACK SHUTDOWN Switch (AUTO, OVRD)

A

AUTO: Allows automatic pack shutdown in engine failure
OVRD: Overrides auto pack shutdown for an engine failure

Both packs automatically shut down if either engine fails during takeoff or selected off. Auto pack shutdown feature is disarmed above 3000 feet. Pack will also auto shutdown if a high supply duct temperature is sensed

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

Function of the FLOW Switch (NORM, HIGH)

A

NORM: Flow control valve is energized to provide a low airflow rate
HIGH: Flow control valve is de-energized to provide a higher airflow rate

Flow switch must be in NORM for takeoff

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

Function of the ISOL Switch (CLSD, OPEN, AUTO)

A

CLSD: Isolation valve commanded closed isolating the left and right pneumatic system
OPEN: Isolation valve is commanded open allowing crossfeed of left and right pneumatic system
AUTO: Controlled by the pneumatic system controller. Allows automatic crossfeed of left and right pneumatic systems during one bleed source operation with airfoil ice protection ON

How well did you know this?
1
Not at all
2
3
4
5
Perfectly
23
Q

Where is CABIN ALTITUDE displayed

A

AIR SD synoptic

24
Q

Where is CABIN RATE displayed

A

SECONDARY ENGINE SD synoptic

25
Q

Function of the Instrument Panel Flow Indication (ON, OFF)

A

ON: On ground, with air conditioning off, indicates instrument panel cooling fan airflow
OFF: On ground, with air conditioning off, indicates the absence of airflow and cooling fan failure

26
Q

Function of the Gasper Booster Fan Switch (ON, OFF)

A

ON: Provides supplemental airplane ventilation when the left pack is operating
OFF: Booster fan is not operating, switch is extinguished

27
Q

Function of the CABIN PRESS control panel (SELECT, MANUAL)

A

SELECT: Illuminated indicates failure of both automatic cabin pressure controllers
MANUAL: Illuminated and the pressurization system operates in manual mode

28
Q

Procedure for taking off with Air Conditioning Packs Off

A

PACKS: Line select ON to OFF, PACKS ALL OFF alert message on EAD

29
Q

Operating with Air Conditioning Packs in AUTO

A

With PACKS in AUTO, the PACKS will automatically shut off at throttle advance and will automatically come back on at 3,000 feet AGL

30
Q

What temperature does the forward cargo compartment maintain

A

60-75 degrees F

31
Q

Where must live animals be transported

A

Only in the forward cargo compartment

32
Q

How is the AFT cargo compartment heated

A

Cabin exhaust air

33
Q

What is the purpose of the Pneumatic Overheat Detection System (PODS)

A

Detects overheat conditions in the tail compartment and along the wing and tail ice protection manifolds

34
Q

What occurs if the PODS detects a failure

A

PODS automatically closes the respective anti-ice valve and alerts the flight crew

35
Q

When is the PODS tested

A

Automatically tested when the engine fire test is performed

36
Q

Which conditions require use of Engine Anti-Ice

A

OAT is 6ºC or below (10ºC in flight) and any of the following conditions exist:
- Visible moisture is present (clouds, rain, snow, fog with 1 mile visibility)
- 3ºC or less temperature/dew point spread
- Ice, snow, slush present on ramp, taxi, or runway

37
Q

Engine run up requirements during icing conditions

A
  • 40% N1 for 10 seconds at intervals no greater than 60 minutes
  • Standing takeoff is required when icing conditions exist. Hold brakes on assigned runway until engines are at or above 50% N1
38
Q

Function of the AIR DATA Heat pushbutton

A

OFF Inscription: All data system heaters are off
DARK: All system heaters are on
(RAT probe is not heated during ground operations)

39
Q

Function of the WING ICE DET switch

A

RESET: Resets system and removes WING ICE DETECTED from EAD (will not remove if ice is still detected)
TEST: Tests the wing ice detection system
(Functions only on ground to detect presence of upper wing ice. Do not take off if WING ICE DET is present)

40
Q

Which cockpit windows are electrically heated

A

Three pilot windshields are electrically anti-iced and electrically anti-fogged

41
Q

Which cockpit windows are electrically anti-fogged

A

Clearview windows are electrically anti-fogged

42
Q

Which control surfaces are anti-iced with engine bleed air

A

Wing slats
Horizontal stab leading edge
(from either or both engines)

43
Q

Which engine components are anti-iced

A

Respective engine nose cowl

44
Q

How long does the CVR record for

A

Records and preserves the last 2 hours of flight deck sounds and communications

45
Q

When does the CVR operate

A

Operates whenever power is available and no crew action is required

46
Q

How can the CVR be erased

A

Aircraft ground sensing system is in ground mode and parking brake is set

47
Q

When the anti-ice duct temperatures have exceeded their limits, what indications will display

A

Amber temperatures will be displayed on the air synoptic

48
Q

What indication displays when all the air data system heaters are selected OFF

A

Amber OFF light will illuminate on the AIR DATA HEAT pushbutton

49
Q

How do you know when you get an ACARS message in flight

A

‘C’ Light on the VHF-3 selector on the Audio Control Panel will illuminate. A chime will sound for certain messages (inhibited during critical phases of flight).

50
Q

Function of the battery switch (OFF, ON)

A

OFF: Battery connected to the battery direct bus only
ON: Connects battery to the DC transfer bus and the battery direct bus

51
Q

Function of the EMER PWR Selector (OFF, ON, ARM)

A

OFF: Emergency power is off
ARM: Supplies emergency power automatically when power loss to the EMER AC or DC is detected
ON: Emergency power is on. Battery supplies power for AC EMER Bus (through static inverter) and DC EMER bus

52
Q

Which busses are powered on the EMER PWR and how long can the battery provide power

A

Battery Direct Bus
DC Transfer bus
Emergency AC bus (through emergency inverter)
Emergency DC bus
Supplies power for 60 minutes

53
Q

Function of the L/R BUS TIE switches (OPEN, AUTO)

A

OPEN: Respective generator cannot power the bus tie
AUTO: Generator bus to tie bus connection is controlled automatically to meet aircraft power requirements

54
Q

Function of the DC BUS TIE switch (OPEN, AUTO)

A

OPEN: Opens all three DC bus tie relays
AUTO: DC bus tie relays are automatically controlled to ensure all DC buses are powered

55
Q

Function of the L/R GEN Switches (RESET, OFF, ON)

A

RESET: Resets the generator
OFF: Disconnects generator from respective bus
ON: Allows an operating generator to supply power to its respective bus

56
Q

Function of the GDN SERVICE ELEC PWR switch (OFF, ON)

A

OFF: Neutral position for ground service power
ON: Connects external power to AC ground service bus and powers DC ground service bus

57
Q
A

DELTA (3 decks)

Brainscape helps you reach your goals faster, through stronger study habits.
© 2024 Bold Learning Solutions. Terms and Conditions