Airplane General, Emergency Equipment, Doors, Windows, Air Systems, Anti-Ice, Rain Flashcards

1
Q

Recall the function and location of the cockpit light override switch.

A

• Overrides normal controls and illuminates various cockpit lights at maximum brightness. Located on overhead panel.

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2
Q

Recall the location and explain the function of the 3 positions of the flight deck emergency light switch.

A
  • The switch is located on the overhead panel.
  • OFF – prevents emergency lights system operation if airplane electrical power fails or is turned off.
  • ARMED – all emergency lights illuminate if airplane electrical power fails or is turned off.
  • ON – all emergency lights illuminate.
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3
Q

Recall that the EMERGENCY LIGHTS can be activated from the flight attendant panel…

A

regardless of the flight deck switch position.

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4
Q

Identify the number and location of all normal entry / exit doors and emergency exits (include entry / exit doors, overwing emergency exits, and cockpit sliding windows).

A
  • All 757/767 aircraft have 2 cockpit sliding windows which may be used as emergency exits.
  • Most 757’s have 6 doors and 4 overwing emergency exit doors
  • Most 767’s have 4 doors and 4 overwing emergency exit doors
  • Some 757’s have 6 doors and 2 emergency exit doors aft of the wing (with no overwing emergency exits).
  • Some 767’s have 6 doors and 2 overwing exit doors
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5
Q

Locate and identify the flight deck indications for entry / service doors.

A

• Overhead panel ENTRY DOORS light and EICAS advisory message(s).
ENTRY DOORS Light
• Illuminated (amber) – an entry door is not closed, and latched and locked.
Note: An EICAS advisory message will show which specific doors are not closed, and latched, and locked. The ONLY way to tell if multiple doors are open is via the EICAS advisory message(s).

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6
Q

Locate and describe the flight deck indications for access, emergency, cargo doors and E & E.

A

• Overhead panel exterior door annunciator lights and EICAS
Advisory message(s)…
Emergency (EMER) DOORS Light
• Illuminated (amber) – a forward or aft (left or right) emergency door, or wing slide door is not closed and latched and locked.
CARGO DOORS Light
• Illuminated (amber) – the forward or aft cargo compartment door (or the bulk cargo door (B767) is not closed, and latched and locked.
ACCESS DOORS Light
• Illuminated (amber) – the forward equipment bay or the electrical
equipment compartment door is not closed and latched and locked

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7
Q

Specify the recommended minimum pavement width for a 180 turn.

A
  • 757-200 120 feet
  • 757-300 141 feet
  • 767-300 146 feet
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8
Q

Describe the relationship of the nose, wingtip and tail during a turn.

A
  • The turn radius of the wingtip is largest, except for the 757-300 where the tail radius is largest.
  • The turn radius of the tail is larger then the nose on all airplanes.
  • The turn radius of the nose is less than both the wingtip AND the tail on all airplanes.
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9
Q

Recall the location of the bulk cargo compartment door.

A

• Only the 767 has a bulk cargo compartment door, and it is located on the left aft fuselage.

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10
Q

Explain the meaning of an illuminated Emergency Lights UNARMED light.

A

Emergency Lights UNARMED Light

Illuminated (amber) – the emergency lighting system has been manually activated or the emergency lights switch is OFF.

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11
Q

Explain the meaning of ANY illuminated VALVE light on the B757/767 flight deck.

A

• Disagreement

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12
Q

Recall the minimum crew oxygen pressure.

A

• 1000 psi

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13
Q

Describe the function of the Passenger Oxygen (PASS OXY) Switch.

A

• Push – the passenger cabin oxygen masks drop
Passenger Oxygen ON light
Illuminated (amber) – the passenger oxygen system is activated and the masks have dropped.

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14
Q

Describe the function of the COMPARTMENT TEMP CONTROLS and INDICATORS.

A

Compartment Temperature Controls -
• AUTO –
provides automatic compartment temperature control.
• OFF –
closes the compartment trim air valve
the compartment temperature INOP light illuminates.
767 flight deck control only:
• MAN –
• provides manual control of compartment trim air valve
• spring loaded to the 6 o’clock position in this sector.

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15
Q

Recall the meaning of an engine bleed OFF light.

A
Engine Bleed Air OFF Lights
• Illuminated (amber) – engine bleed air valve is closed:
- automatically due to a system fault
- the switch is OFF
- the engine is not running.
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16
Q

Recall the indications of a dual auto pressurization controller failure.

A
AUTO Inoperative (INOP) Light Illuminated (amber) –
• AUTO 1 and AUTO 2 cabin altitude control functions are inoperative
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17
Q

Recall the meaning of the cargo heat OVHT light (767 Only).

A

Cargo Heat Overheat (OVHT) Lights illuminated (amber) –
• Cargo compartment temperature above standard control range
• Shutoff valve signaled closed.

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18
Q

Describe the function of the trim air system.

A

• The trim air system adds warm air to the pack output air.
• The pack controllers regulate the pack output air temperature to satisfy the temperature requirement of the compartment requiring the coolest air.
• If the trim air system is OFF or inoperative, the packs attempt to maintain all compartments at an average temperature.
TRIM AIR Switch
• ON – the trim air valve is commanded open.
• Off (ON not visible) – the trim air valve is commanded closed.
Trim Air OFF Light
• Illuminated (amber) – the TRIM AIR switch is off.

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19
Q

Describe the function of the gasper system.

A
Gasper System (As installed)
• The gasper system draws air from the forward cabin overhead air conditioning ducts and discharges it from gasper outlets in the passenger service units located above each passenger seat. Gasper air is controlled by the GASPER fan switch.
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20
Q

Recall the pressurization panel landing altitude must be reset during a destination change.

A

Recall the pressurization panel landing altitude must be reset during a destination change.

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21
Q

Discuss the purpose of the recirculation fans.

A
  • Recirculation fans maintain overall cabin air circulation while allowing a reduction of cabin air ventilation, permitting the packs to be operated at a reduced flow. This reduces bleed air demand from the engines, reducing fuel burn.
  • 757: The left recirculation fan should not be turned off because of its equipment cooling function.
22
Q

Explain how to manually control the cabin altitude.

A

• Place the Cabin Altitude MODE SELECTOR in MAN and rotate the Cabin Altitude MANUAL Control to CLIMB or DESCEND.

23
Q

Recall the location and preflight position of the BULK CARGO HEAT SELECTOR (767 Only).

A

BULK CARGO HEAT Selector
• The BULK CARGO HEAT SELECTOR is located on the accessory panel
• NORM – standard cargo heating range..
• VENT provides a warmer compartment temperature than NORM and activates a fan in the bulk cargo compartment.
Note: The preflight position for all Delta operations is VENT

24
Q

Recall the functions of the equipment cooling selector positions (767 Only): AUTO, STBY, OVRD

A

Equipment (EQUIP) COOLING Selector
• AUTO – automatically controls equipment cooling system.
• STBY – positions equipment cooling system for inboard air flow.
• OVRD – positions equipment cooling system for reverse air flow and arms the NO COOLING light.

25
Q

Explain the meaning of an illuminated PACK OFF light.

A

PACK OFF Illuminated (amber) –

The pack valve is closed. Note: The Pack is OFF.

26
Q

Explain the meaning of an illuminated Pack Inoperative (INOP) light.

A
INOP Illuminated (amber) –
• the pack is overheated.
• fault in the automatic control system.
27
Q

Explain the meaning of an illuminated gasper OFF light.

A

Gasper Fan OFF light (as installed)

• Illuminated (amber) – the GASPER fan switch is ON but the gasper fan is not operating.

28
Q

Explain the meaning of an illuminated recirc fan INOP light.

A

Recirculation Fan Inoperative (INOP) Lights
• Illuminated (amber) –
- the recirculation fan is failed or is not operating.
- the RECIRC FAN switch is off.

29
Q

Explain the meaning of an illuminated equipment cooling OVHT light (757 and 767).

A

(757) Equipment Cooling Overheat (OVHT) Light
• Illuminated (amber) – insufficient airflow due to:
- either supply fan is inoperative, or
- overboard exhaust valve is closed, with the left recirc fan failed or switched off
(767) Equipment Cooling Overheat (OVHT) light
• Illuminated (amber) – high temperature or low airflow in the equipment cooling system.

30
Q

Explain the function of the OFF, AUTO and STANDBY positions of the pack control selectors.

A

PACK Control Selectors
• OFF – closes the pack valve.
• AUTO – the pack is automatically controlled.
• STBY –
- N (normal) – regulates the pack outlet temperature to a constant, moderate temperature.
- C (cool) – sets the pack to full cold operation.
- W (warm) – sets the pack to full warm operation.
Note: The automatic controller is bypassed in the standby position.

31
Q

Explain the meaning of an illuminated CABIN ALTITUDE light on the overhead panel or an illuminated CABIN ALT light on the center forward (discrete) panel.

A

Cabin Altitude Light or Cabin Alt Light
• Illuminated (red) –
- cabin altitude exceeds 10,000 feet
- extinguishes when cabin altitude descends below 8,500 feet.

32
Q

Explain the operation of the cabin altitude auto rate control
Cabin Altitude AUTO RATE Control

A
  • Only functions if AUTO 1 or AUTO 2 selected
  • Rotate – sets limit for cabin altitude rate of climb or descent during auto control
  • The index mark is the proper preflight position
33
Q

Explain the meaning of an illuminated NO COOLING light on the 767

A

NO COOLING Light
• Illuminated (amber) –active in OVRD only
• No reverse air flow through the E/E compartment avionics.

34
Q

Recall the meaning of an illuminated compartment temperature INOP light.

A

Compartment Temperature Inoperative (INOP) Lights
• Illuminated (amber) –
- fault in the zone temperature controller
- the Compartment Temperature Control is OFF
- the trim air switch is OFF.

35
Q

Explain why the center isolation (C ISLN) switch on the 767 is guarded.

A

• To protect the air source to the ADP.

36
Q

Recall the meaning of an illuminated DUCT LEAK light.

A

DUCT LEAK Light

• Illuminated (amber) – a high temperature bleed air leak is detected

37
Q

Recall the meaning of an illuminated BLEED light.

A

BLEED Light
• “Bleed Air Malfunction” is the Delta recommended answer.
• The Volume II detailed answers are also acceptable.

38
Q

Recall the meaning of an illuminated HI STAGE / OVHT light.

A

HIGH STAGE / OVHT Light
• “Bleed Air Malfunction” is the Delta recommended answer.
• The Volume II detailed answers are also acceptable.

39
Q

Recall the conditions that require the use of Engine Anti-Ice.

A

• Required during “icing conditions”
• Icing conditions exist when OAT (on the ground) or TAT (in-flight) is 10°C or below and:
- visible moisture (clouds, fog with visibility less than one statute
mile (1600 m), rain, snow, sleet, ice crystals, and so on) is present,
or
- standing water, ice, or snow is present on the ramps, taxiways, or
runways.

40
Q

Recall the conditions that require the use of the Wing Anti-Ice.

A

All Aircraft.
• For aircraft with or without ice detectors installed, ice accumulation on the flight deck windshield frames, windshield center post, windshield wiper post, or side windows can be used as an indication of airframe icing conditions.
CAUTION: Do not operate wing anti–ice when the total air temperature (TAT) is above 10°C.

41
Q

Recall when probe heat operates.

A

• When an engine is operating.

42
Q

Describe the proper switch/selector positions for the ground and airborne use of the engine and wing anti-ice systems in both icing and non-icing conditions.

A

• IN icing conditions:
“Switch” airplanes:
- On the ground – wing OFF, engines ON.
- Airborne – wing ON or OFF as required, engines ON. Wing anti-ice, if required, is selected ON during the after takeoff flow.
“Selector” airplanes:
- On the ground – wing OFF, engines ON.
- Airborne – AUTO / AUTO / AUTO accomplished on after takeoff flow.
NOTE: Engine bleed air MUST be used for engine anti icing; APU bleed air is insufficient. When running a single engine, only run ONE pack if also using engine anti-ice on the ground.
NOT in icing conditions:
“Square switch” airplanes – All switches OFF.
- “Selector switch” airplanes:
- On the ground – wing OFF, engines AUTO.
- Airborne – AUTO / AUTO / AUTO accomplished on after takeoff flow.

43
Q

Know that advisory messages will appear as the ice detection system cycles - such as ICE DET ON and ICE DET OFF only on “switch” equipped aircraft.

A

ICE DET ON

ICE DET OFF

44
Q

Recall when wing anti-ice operation is inhibited.

A

• On the ground.

45
Q

Recall which source(s) of pneumatic air should be used for engine and wing anti-icing.

A

• Engine bleed air MUST be used for engine anti icing; APU bleed air is insufficient.

46
Q

Explain the meaning of an illuminated CAPT/FO PITOT light

A

Captain or FO Pitot (CAPT / FO PITOT) Light

• Illuminated (amber) – probe is not being heated or neither engine is running on the ground.

47
Q

Explain the meaning of an illuminated ICING light.

A

“Switch” airplanes.
ICING Light
• Illuminated (amber) – ice detection system indicates ice build up on the airplane.
“Selector” airplanes.
ICING Light
• Illuminated (amber) – engine/wing icing is detected and either engine or wing anti–ice is manually selected OFF or an anti–ice valve is closed.
Manually Selected Off with ICE detected
An Anti-Ice Valve is Closed with ICE detected

48
Q

Explain the meaning of an illuminated window heat INOP light.

A

Window Heat Inoperative (INOP) Lights

• Illuminated (amber) – the window is not being heated.

49
Q

Explain the meaning of an illuminated (ice detector) ICE DET light (On aircraft with anti-ice “selectors”).

A
Ice Detector (ICE DET) Light
• Illuminated (amber) – ice detector system is failed.
50
Q

Recall that “Selector” equipped aircraft (In AUTO) do not generate EICAS Caution messages unless there is a system fault – operation is transparent. In AUTO, a fault is indicated by an ICING light and an ICING EICAS Caution message.

A

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51
Q

Know that some aircraft DO NOT have an ice detection system installed. See aircraft differences section.

A

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