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Delta 7ER IQ > eSV > Flashcards

eSV Flashcards

1
Q

(757) Maximum operating altitude.

A

42,000 feet pressure altitude

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2
Q

(767) Maximum operating altitude.

A

43,000 feet pressure altitude

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3
Q

What is the 767-300 maximum operating altitude?

A

43,000 feet pressure altitude

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4
Q

What is the maximum takeoff and landing tailwind component?

A

10 Knots or as permitted by Delta Special Pages (Green Pages)

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5
Q

What is the turbulent air penetration speed?

A

290 KIAS or .78 Mach, whichever is less

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6
Q

The maximum takeoff and landing crosswind for normal operations is _____ knots.

A

40 knots

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7
Q

After takeoff, the autopilot must not be engaged below _____ feet AGL.

A

200 feet AGL

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8
Q

True or False: Use of aileron trim with the autopilot engaged is prohibited.

A

True.

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9
Q

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Headwind of _____ Knots.

A

25 Knots

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10
Q

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Crosswind of _____ Knots. (Boeing’s #, not the Delta Ops Spec Limit)

A

25 Knots

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11
Q

Maximum allowable wind speeds when landing weather minima are predicated on autoland operations: Tailwind of _____ Knots.

A

10 Knots

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12
Q

Autoland authorized for flaps _____ or _____ landing only.

A

Flaps 25, Flaps 30

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13
Q

The maximum altitude for flap extension is _____ feet.

A

20,000 feet

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14
Q

List the recall action step(s) for an ABORTED ENGINE START.

A

Step 1: FUEL CONTROL SWITCH (affected side)……CUTOFF

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15
Q

List the recall action step(s) for a DUAL ENGINE FAILURE.

A

Step 1 : ENG START SELECTORS (both)……FLT
Step 2 : THRUST LEVERS (both)……IDLE
Step 3 : FUEL CONTROL SWITCHES (both)……CUTOFF, then RUN

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16
Q

List the recall action step(s) for ENGINE FIRE or SEVERE DAMAGE or SEPARATION.

A

Step 1 : A/T ARM SWITCH……OFF

Step 2 : THRUST LEVER (affected side)……Confirm….IDLE

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17
Q

List the recall action step(s) for ENGINE LIMIT or SURGE or STALL.

A

Step 1 : A/T ARM SWITCH……OFF
Step 2 : THRUST LEVER (affected side)…..Confirm…..Retard until indications remain within normal limits or thrust lever is at idle.

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18
Q

List the recall action step(s) for CABIN ALTITUDE or RAPID DEPRESSURIZATION.

A

Step 1 : DON THE OXYGEN MASKS

Step 2 : ESTABLISH CREW COMMUNICATIONS

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19
Q

List the recall action step(s) for AIRSPEED UNRELIABLE.

A

Step 1 : Check the pitch attitude and thrust
Step 2 : If pitch attitude or thrust is not normal for phase of flight: 1.) Autopilot disengage switch - push 2.) Autothrottle disconnect switch - push 3.) F/D switches (both) - OFF 4.) Establish normal pitch attitude and thrust setting for phase of flight.

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20
Q

If time is critical or vision is obstructed, list the steps of an EVACUATION.

A

Step 1 : Stop
Step 2 : Configure
Step 3 : Shutdown
Step 4 : Evacuate

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21
Q

Where is the Light Override (LT OVRD) switch located?

A

The Overhead Panel

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22
Q

True or False : Any illuminated VALVE light on the B757 and B767 indicates a disagreement with the commanded position.

A

True

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23
Q

True or False : The minimum crew oxygen pressure is 1,000 psi.

A

True

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24
Q

What will pushing the passenger oxygen (PASS OXY) switch on the overhead panel do?

A
  1. ) Drop the passenger cabin oxygen masks.

2. ) Illuminate the amber passenger oxygen “ON” light

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25
Q

Explain the three switch position functions of the emergency lights (EMER LIGHTS).

A
  1. ) ARMED : All emergency lights illuminate if airplane electrical power fails or is turned off.
  2. ) ON : All emergency lights illuminate.
  3. ) OFF : Prevents emergency lights system operation if airplane electrical power fails or is turned off.
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26
Q

True or False : The emergency lights can be activated from the passenger cabin emergency lights (EMER LTG) switch, regardless of the flight deck EMER LTS switch position.

A

True

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27
Q

True or False : An illuminated emergency lights UNARMED light means the emergency lighting system has been manually activated or the emergency lights switch is OFF.

A

True

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28
Q

What will be the flight deck indications if an entry door is open?

A

You will get an ENTRY DOOR annunciator light on the overhead panel with the associated EICAS message.

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29
Q

True or False : The bulk cargo door is on the left aft fuselage of B767 aircraft.

A

True

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30
Q

Minimum pavement width to make a 180° turn in the 757-200, 757-300, and 767-300.

A

757-200 - 120 feet
757-300 - 141 feet
767-300 - 146 feet

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31
Q

Which turn radius is the largest on the B767-300? (nose, tail, or wing tip)

A

Wing tip

32
Q

On the B767, which compartment temperature control can be set to MAN to allow manual operation of the trim air valve?

A

FLT DK

33
Q

True or False : The ON position of the TRIM AIR switch commands the trim air valve open.

A

True

34
Q

Where is GASPER air discharged?

A

Through gasper outlets above each passenger seat.

35
Q

True or False : RECIRC FANs improve fuel efficiency.

A

True

36
Q

What position of the B767 Equipment Cooling Selector will arm the NO COOLING light?

A

OVRD

37
Q

True or False : Illumination of the PACK OFF light on the air conditioning panel indicates the PACK valve is closed.

A

True

38
Q

What is indicated by the illumination of the PACK INOP light on the air conditioning panel?

A
  1. ) A PACK is overheated.

2. ) A fault in the automatic control

39
Q

True or False : The illuminated gasper fan OFF light indicates the gasper fan is signaled OFF or not operating.

A

True

40
Q

What is indicated by an illuminated RECIRC FAN INOP light?

A
  1. ) The recirculation fan is failed or not operating.

2. ) The RECIRC FAN switch is OFF

41
Q

True or False : Selecting OFF on a PACK control selector closes the PACK valve.

A

True

42
Q

Which cargo heat position provides warmer temperatures, NORM or VENT?

A

VENT provides warmer cargo bin temps and is the regular position of this switch on Delta flights.

43
Q

True or False : The center isolation (C ISLN) switch on the 767 is guarded to protect the air source to the ADP.

A

True

44
Q

True or False : The illumination of the engine bleed OFF light indicates the bleed valve is closed.

A

True

45
Q

What are the flight deck indications of a dual pressurization controller failure?

A

The AUTO INOP light on the pressurization panel illuminates.

46
Q

True or False : An illuminated CABIN ALTITUDE light on the overhead panel indicates cabin altitude exceeds 10,000 feet.

A

True

47
Q

True or False : The NO COOLING light is only operational if EQUIP COOLING is in OVRD.

A

True

48
Q

The compartment temperature INOP light(s) indicate:

A
  1. ) The TRIM AIR switch is OFF
  2. ) Fault in the temperature controller
  3. ) Compartment temperature controller is OFF
49
Q

True or False : An illuminated DUCT LEAK light is an indication of high temperature bleed air leak detected in the pneumatic duct.

A

True

50
Q

True or False : An illuminated BLEED light is an indication of a bleed air malfunction.

A

True

51
Q

True or False : An illuminated HIGH STAGE / OVHT light is an indication of a bleed air malfunction.

A

True

52
Q

On the B757, what EICAS message will be displayed when the ice detector no longer senses ice accumulation?

A

Advisory message ICE DET OFF

53
Q

When is the wing anti-ice system inhibited?

A

Anytime the airplane is on the ground

54
Q

When does probe heat operate automatically?

A

Anytime an engine is running

55
Q

When would the CAPT PITOT light on the overhead panel be illuminated?

A
  1. ) The aircraft is on the ground with both engines shutdown.
  2. ) The probe is not being heated
56
Q

Engine anti-ice must be used during all ground and flight operations when icing conditions exist or are anticipated, except during climb and cruise when the temperature is below _____ °C SAT.

A

-40°C SAT

57
Q

Can the APU be the bleed air source for anti-ice?

A

No, it isn’t sufficient.

58
Q

True or False : On aircraft equipped with anti-ice selectors, when in the AUTO position, no EICAS messages are generated and no discrete lights illuminate when in icing conditions if the anti-ice systems are functioning normally.

A

True

59
Q

How long is the green box on the Flight Mode Annunciator (FMA) displayed when a pitch, roll, or autothrottle mode has changed?

A

10 seconds

60
Q

What is the meaning of a steady amber FMC light on the center forward panel?

A

The CDU is displaying an operationally significant message in the scratchpad.

61
Q

True or False : When LOC and GS are both armed, GS can always capture prior to LOC capture.

A

True

62
Q

True or False : Delta recommends selecting B/C prior to LOC when flying a localizer back course approach.

A

True

63
Q

The FL CH switch uses a “_____ minute rule” that prevents the autothrottles from performing a full EPR climb or flight idle descent for small altitude changes.

A

“2 minute rule”

64
Q

True or False : Vertical Speed (V/S) pitch mode has no overspeed or stall protection.

A

True

65
Q

True or False : Speed can be controlled in VNAV by the FMS or by using speed intervention.

A

True

66
Q

Which roll mode does the bank angle limit selector apply to?

A

HDG only.

67
Q

True or False : If the Flight Director switches are turned off, selecting go-around will cause the Flight Director command bars to appear.

A

True

68
Q

True or False : The vertical speed selector is always active, regardless of whether or not the vertical speed window is open.

A

False

69
Q

True or False : Engaging the autopilot in takeoff or go-around will result in pitch and roll modes of vertical speed and heading hold.

A

True

70
Q

True or False : After LOC or G/S are captured, a new pitch mode may be engaged by selecting a different pitch mode on the MCP.

A

False

71
Q

True or False : The Ground Service switch is located in the cabin.

A

True

72
Q

How much time is required for IRS fast realignment?

A

Approximately 30 seconds

73
Q

Which aircraft model in the 7ER category can jettison fuel?

A

767-300ER

74
Q

What is the approximate rate at which fuel can be jettisoned?

A

1,300 pounds per minute

75
Q

The Ram Air Turbine (RAT) provides adequate hydraulic power at speeds above _____ knots.

A

130 knots

Delta 7ER IQ (11 decks)

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