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767 Flashcards

1
Q

767 Load Alleviation

A

767 (Winglets) Speedbrake Load Alleviation system
operates in flight when these conditions occur at the
same time:
– Flaps are UP
– Gross weight is greater than 340,000
– Indicated airspeed is greater than 320 kts.
– If lever is beyond the 50% position it will
automatically move to 50% position
– If lever is down it will be restricted to 50% position
System deactivates when gross weight less than
339,000 lbs or airspeed becomes less than 315 kts.

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2
Q

SPEED BRAKES EXT MESSAGE:

A
  • Speed brakes extended during descent between 800
    ft and 15 ft RA
    (Vol 2 now says 800 ft or below) or with flaps greater
    than 20 deg (Vol 2 says flaps are in a landing position)
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3
Q

What is powered if on BATTERY POWER ONLY:

What are the visibility and DH restrictions for the raw data approach?

A
  • Hot Battery / Battery / Standby AC / Standby DC
    buses. (with hydraulic pressure the flaps work, but flap
    indicators do not).
  • Min weather: RVR 2400 (1/2 mile – 750 M) and a
    DH of 250 or higher (ILS raw data)
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4
Q

Load Alleviation 757

A

Gross weight is greater than 221,000 lbs
- Indicated airspeed is greater than 330 kts
– If lever is beyond the 50% position it will
automatically move to 50% position
– If lever is down it will be restricted to 50% position
– System deactivates when gross weight less than
220,000 lbs or airspeed becomes less than 325 kts.

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5
Q

STANDBY POWER:

- If selector is in AUTO:

A

Transfers standby busses to battery power if normal

AC power is lost.

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6
Q

STANDBY POWER:

If Manually selected to Battery.

A

Selecting BAT directly powers standby busses from

the main battery.

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7
Q

GROUND HANDLING BUS:

When is it powered?

A

Only powered on the ground either by the APU or

available External power.

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8
Q

GROUND HANDLING BUS: What does it power?

A

Powers the cargo compartment doors and lights,

cargo handling equipment and airplane refueling.

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9
Q

GROUND SERVICE BUS:

What powers it?

A

Powered from right main AC bus.
- If right main AC is not available (on the ground), the
ground service bus can connect to and be powered
from APU / External power via the ground service
switch on F/A panel at 1L.

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10
Q

What does the GROUND SERVICE BUS power?

A

Powers two battery chargers, equipment cooling fan,

left forward fuel boost pump (+L Fwd door on 767).

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11
Q

Windshear Escape Maneuver

A 
Disconnect Autopilot
Press either Go Around Switch
Aggressively Apply Maximum Thrust 
Disconnect Autothrottle
Roll Wings Level/Initial Pitch 15*
Retract Speedbrakess
Follow Flight Directors
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12
Q

TCAS RA in Landing Configuration

A 
Disengage Autopilot land Autothrottles
Advance Thrust Levers to Max Thrust
Call for Flaps 20
Adjust Pitch to Satisfy RA Command
Positive Rate-Gear Up
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13
Q

RA- Not in Lamding Configuration

A

Disengage Autopilot and Autothrottles
Adjust Pitch to Satisfy RA
Follow planned Lateral Flight Path

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14
Q

ENGINE COOL-DOWN:

A
  • 757: 1 minute.

- 767: 3 minutes

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15
Q

PRESSURIZATION AUTO INOP LIGHT:

A

Mode selector in MAN or Auto 1 and 2 Pressurization

Control failed.

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16
Q

ENG OVHT MESSAGE

A
  • Engine bleed air leak in the engine nacelle area.

- 767-300 ER also has strut duct leak detectors

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17
Q

AIR CONDITIONING PACK CONTROLLERS: What temperature are they seeking?

A

Adjust output to satisfy the zone demanding the

coolest temperature.

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18
Q

PACK INOP LIGHT:

A
  • (QRH allows attempts to recover)
  • Pack controller fails
  • Excessive pack outlet temperature
    • Select STBY N, allow to cool for 5 min, press to reset
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19
Q

PACK OFF LIGHT

A

QRH only allows recovery of PACK if due to engine
bleed air loss, then consider an alternate bleed air
source.
- No resets or Stby-N
- Excessive internal temperature (no reset or Stby-N)

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20
Q

ZONE TRIM AIR FAILURE:

A

If single zone: select OFF. Temperature for that zone

will be controlled by the zone requiring coolest temp.

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21
Q

What are the indications for a EQUIPMENT COOLING OVHT while on the ground?

A
  • Light and ground crew call horn will sound (steady
    horn) if the airplane battery is the sole source of
    electrical power on the ground for more than 30
    seconds.
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22
Q

OIL - MIN QUANTITY:

A
  • Preflight: 14 Quarts OK (
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23
Q

APU STARTER DUTY CYCLE:

A

During normal operations, while on the ground or in
flight: 3 consecutive starts or attempts within a 60-
minute period.
- Capt’s Authority for additional unlimited starts during
abnormal or emergency conditions when airborne.
- To cancel an APU shutdown during the 60 second
cool-down period with the RUN light still illuminated go back to Start

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24
Q

APU FIRE PROTECTION 757

A
  • APU will auto shutdown if on fire while on the ground
    or in the air.
  • 757 will auto shutdown and auto discharge fire agent
    if on fire while on the ground, both engines not running.
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25
Q

APU FIRE PROTECTION 767:

A
  • 767: APU will auto shutdown but no auto discharge if

on fire while on the ground.

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26
Q

APU FAULT light

A

APU has automatically shut down

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27
Q

APU NOSE GEAR BUTTONS:

A

— Red: Push first, closes the APU fuel valve, trips
APU generator off, arms the bottle and silences the
APU fire horn.
— Black: Discharges APU fire agent bottle.
– (Intermittent horn during walk around is an APU fire
warning test or actual fire warning)

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28
Q

ENGINE FIRE SWITCH (looks like a Handle):

A
  • Closes associated engine and spar fuel valves
  • Closes associated engine bleed air valves
  • Trips associated engine generator off
  • Shuts off hydraulic fluid to engine-driven hyd pump
  • Arms both engine fire extinguisher bottles
  • Silences the fire warning bell
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29
Q

– If the Master Warning Lights and Bell do not work

during TEST?

A

push both master caution warning light

assemblies to reset the system.

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30
Q

Which bus provides Fire Protection?

A

Hot Battery Bus

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31
Q

Which bus provides Fire Detection?

A

Battery Bus

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32
Q

CARGO COMPARTMENT FIRE EXTINGUISHING:

767

A
  • FWD and AFT cargo compartments have smoke
    detectors.
  • Either cargo fire arming switch:
    – Arms the fire bottles
    – Silences fire bell
    Turns off both cargo heat fans on the 767
  • If FWD arming switch is pushed it will also:
    – Turn off both recirculation fans
    – Switch both AC packs to High Flow
    Closes FWD cargo heat valve (767)
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33
Q

LAV SMOKE IS DETECTED:

A
  • A horn, chime and / or a flashing lav light at F/A

station, no indication in the cockpit.

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34
Q

FLAPS 30 is recommended when landing:

A
    • Breaking action less than good
    • Tailwind
    • Runway length less than 7,000 ft
    • On a wet / contaminated runway
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35
Q 
ALTERNATE FLAPS (electric operation, slower):
757
A

757 has LE SLAT asymmetry protection
- 757/767: LE Slats go to landing position when flaps
25 are selected, increasing stall margin.
- 757 does not have TE Flap asymmetry and load relief
Max ALT FLAP setting: 20 (in case of a Go-Around)

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36
Q 
ALTERNATE FLAPS (electric operation, slower):  
767
A

767 does not have LE SLAT asymmetry protection
- 757/767: LE Slats go to landing position when flaps
25 are selected, increasing stall margin.
767: Some have TE Flap asymmetry protection.
- Max ALT FLAP setting: 20 (in case of a Go-Around)

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37
Q

AUTO SPDBRK WARNING LIGHT:

A
  • Light will illuminate anytime a fault is detected in the
    system.
  • 757: Do not exceed 330 kts (load alleviation fault)
  • 757 / 767: Do not arm automatic speed brakes for
    landing, manual deployment may be required after
    Landing
38
Q

One GENERATOR LOSS in flight, what do you lose?

A

causes both utility
buses and all galley buses to trip off. Can be reset
when another generator (APU) is established.

39
Q

What is the normal power source for the center autopilot?

What is the power source during a auto land approach?

A

Left Main AC Bus

During Autoland Approach, center autopilot powered
by battery / standby system.

40
Q

GENERATOR DRIVE LIGHTS ILLUMINATED:

A
  • Generator drive oil temperature is high

- Generator drive oil pressure is low

41
Q

HYDRAULIC DRIVEN GENERATOR (HDG):

When does it come on?

A
  • Activates automatically with loss of Left AND Right

main AC buses.

42
Q

What does the HDG power?

A

Powers 7 busses: hot battery, battery, standby DC,
standby AC, left and right AC transfer buses, Captains
instrument transfer.
(if down to 7 buses: Everything left of gear handle is
available, except for Autopilot, Command Bars, EICAS
screens, Alt Flaps and Auto Brakes)

43
Q

What powers the HDG?

A

757 ER HDG is powered by left hydraulic system,
back up pressure supplied by PTU.
- 767 ER HDG is powered by the center hydraulic
system, back up pressure supplied by Air Demand
Pump.

44
Q

When does the PTU come on in the 757?

A
  • 757: Comes on if the Left engine hydraulic pump
    pressure is low or the left engine is shut down and the
    right engine is running.
45
Q

Where does the PTU get its fluid and pressure from on the 757?

A

Uses trapped L Hydraulic fluid and R Hydraulic

pressure to operate the PTU.

46
Q

What is the purpose of the PTU on the 757.

A

PTU helps with heavy loads on the left hyd. system.

- Provides backup pressure for the HDG on 757 ER’s

47
Q

When does the PTU come on in the 767 and what system fluid does it use?

A

767: Comes on if the L + C hydraulic system

pressure is lost, uses right hydraulic fluid via the PTU

48
Q

What does the PTU power on the 767?

A

Powers the stab trim for pitch enhancement (control
wheel thumb trim switch) at ¼ rate using trapped fluid
from left stab brake assembly

49
Q

Where are the HYDRAULIC STANDPIPES on the 757 and what is the fluid reserved for?

A

LEFT CENTER RIGHT

757: PTU RAT RES BRAKES

50
Q

Where is the Hydraulic Stand Pipes on the 767 and what do they power?

A

767: Center Hydraulic System

          RAT 
          STEERING 
          RES BRAKES
51
Q

When does the RAT deploy?

A

Loss of both engines above 80 kts. and engines

sensed below 50% N2 / N3.

52
Q

What does the RAT power?

A

Provides pressure to center hydraulics for center

primary flight controls (ailerons, elevator and rudder)

53
Q

What is the min speed for RAT effectiveness?

A

130 it’s

54
Q

What power source(s) are needed for RAT deployment?

A
  • Hot Battery power needed to manually deploy RAT

- Battery power needed for automatic deployment

55
Q

What would hydraulic accumulator pressure of less than 1000lbs at the gate indicate.

A
  • Below 1,000 PSI (at the gate) indicates a bad

accumulator.

56
Q

A RIGHT HYD SYS PRESS EICAS message may

indicate?

A

the alternate brake system has been

activated.

57
Q

What does the BRAKE SOURCE LIGHT indicate and what action should be taken?

A

= low pressure in both normal and alternate brake
systems.
- Press the Reserve Brakes switch to activate the
Reserve Brakes.

58
Q

What does the reserve brake switch on the 757 do?

A
  • 757: Isolates the right AC hydraulic motor pump to

provide hydraulic brake pressure.

59
Q

What does the Reserve Brake Switch on the 767 do?

A
  • 767: Isolates the Center # 1 electric primary hydraulic

pump to provide hydraulic brake pressure

60
Q

On the 75 and 76, if the RES BRAKE source switch is flipped and the brake source light does not go out, what are you down to?

A
  • If you select the RES BRAKE source switch and the
    brake source light does not go out: you are down to
    Accumulator Pressure. Check electric pump press light
    on overhead panel to identify the failed pump/problem.
61
Q

How many IRU’s does the ANTI SKID system need to operate?

A

One

62
Q

What does the – Anti-Skid light indicate?

A

that a fault is detected in the active brake system

63
Q

Will Auto Brakes work if brake system is using the alternate line?

A

No, auto brakes will only work from the normal line.

64
Q

When is RTO braking system active and how much will it slow the aircraft?

A

Active above 85 kts. and when both
throttles are retarded to idle
- Autobrakes will bring aircraft to a complete stop.

65
Q

When must Auto Brakes be armed?

A

-

66
Q

When are auto brakes activated?

A

After landing: autobrakes are applied when both

throttles are at idle and wheel rotation is detected.

67
Q

When will the Auto Brakes Disarm?

A
  • Tilt sensor malfunctions
  • Throttles not at idle by 2 seconds after touchdown
  • Advance either throttle after touchdown
  • Apply manual brakes
  • Retract spoiler handle
  • Turn switch to disarm or off
  • Auto brake fault
  • Anti skid fault
68
Q

When do you NOT have to do a Landing Distance Assesment?

A

-Usable length >7300’
- Field Elevation below 5300’
Provided all of the below are met:
Expected breaking action is good or better
LDG weight less than structural limit
Flaps 25 or 30
No Tailwind
No MEL/CDL affecting performance

69
Q

Which ailerons lock out on the 767 and when?

A

At high speeds outboard 767 ailerons lock out.

70
Q

What does a AILERON LOCK WARNING LIGHT indicate?

A
  • At low speeds it may mean that the outboard ailerons
    might be locked out. At high speed it might mean that
    they are not locked out
71
Q

When can the auto pilot be engaged and when must it be disengaged?

A

T/O do not engage prior to 1000’AFE
Disconnect not less than 100 above TDZE(except auto land)
757- Do not use the AP below 100’RA at airport pressure altitudes above 8400’

72
Q

On a CAT II / III approach with one autopilot engaged, when should the other AP’s be engaged?

A

After arming the APP

73
Q

When does the AUTOLAND STATUS ANNUNCIATOR WINDOWS come on?

A

Upper: LAND 2 / 3 (come on at 1500 feet)
- Lower: NO LAND 3 / NO AUTOLAND
– Lower window items are continuously monitored
throughout the flight and mean what they say.

74
Q

RUDDER RATIO LIGHT:

What does it mean and what are the limitations?

A

Avoid large or abrupt rudder inputs above 160 kts.
- If normal L Hydraulic system pressure is available,
max X Wind 15 kts because a fault in the rudder ratio
control unit may limit rudder displacement.
- Left rudder actuator receives the rudder ratio inputs.
- Auto Land prohibited.

75
Q

UNSCHEDULED STAB TRIM light:

A

Stab movement sensed without trim signal
– Direction of autopilot trim opposite to elevator control
input
– Alternate trim levers used with autopilot engaged.

76
Q

STAB TRIM light:

A

One stab trim brake failed to
release, still have full travel but at ½ rate
- Autopilot use is still ok.

77
Q

SPOILERS LIGHT:

A

Disagreement between spoiler position and
commanded position or one or more spoiler pairs are
inoperative.

78
Q

Auto Spoilers will deploy on landing:

A

Hydraulic pressure to both tilt actuators
– Both truck tilt sensors indicating on the ground
– If Armed: Both throttles at idle
– If Not Armed: Both throttles at reverse idle
(single engine: operating throttle at reverse idle)

79
Q

Max FUEL IMBALANCE:

A

757: 1,950 lbs
767: 1,500 lbs > 79.8 total main tank fuel is left.
2,500 lbs

80
Q

FUEL CONFIG LIGHT WILL COME ON FOR:

A
  • LOW FUEL: 1,800 lbs

767: 2,000 lbs +/- 500 lbs

81
Q

FUEL TANK TEMPERATURE READINGS:

A
  • 757: right tank

- 767: left tank

82
Q

Which tank does Fuel Jettison from and what is the approx. rate?

A
  • From the Center Fuel tank only
  • With SEL 27: approximately 1,300 PPM / 60 minutes
    to empty a full center fuel tank. (767: SEL Item 27, 767
    center tank UFI is installed on all 767s)
83
Q

When will the IRU ALIGN LIGHTS WILL FLASH:

A

Position not entered within 10 minutes

  • Wheel rotation during alignment
  • Wrong position entered.
    • If IRU alignment is lost in flight the navigation mode is INOP.
84
Q

Procedure for IRU QUICK ALIGNMENT:

A
  • Park Brakes, all 3 IRUs to Align, Enter Position, back
    to NAV
  • Enter Qxx at gate position [3L] on Position Page
    (xx = runway or runway/intersection as identified on the
    TPS. Ex: Q08LZ. Line select from [3R] to [4R])
  • See VOL 1, SYST, Page 65.11 for complete
    procedure.
85
Q

When do the IRU’s shed on a non-ER aircraft?

A
  • If left and right main AC buses are lost, all 3 IRU’s
    go to HBB, after 5 minutes left & center shed, right
    stays on HBB until battery is dead.
    – If left main AC bus is lost: left & center IRU’s go to
    the Hot Battery Bus (HBB) and run on DC power, no
    time limit since battery charger is still powered from
    right AC, right IRU remains on right AC.
    – If right main AC bus is lost, the right IRU operates
    on HBB until battery is depleted (approx. 30 min), left &
    center remain on left AC
86
Q

How do the IRU’s shed on anER aircraft?

A
  • If left and right main AC buses are lost, all 3 IRU’s
    go to HBB, after 5 minutes right IRU sheds, HDG
    powers left & center IRU. (If no HDG, left & center stay
    on HBB until battery is dead).
    – If left main AC bus is lost, left & center IRU’s go to
    HBB and stay there (no battery time limit since battery
    charger is still powered from right AC), right IRU
    remains on right AC.
    – If right main AC bus is lost, (right DC will also be
    lost) right IRU operates on HBB and sheds after 5
    minutes, left and center IRUs remain on left AC.
87
Q

MASTER CAUTION INHIBIT?

A
  • Starts at 80 kts, ends at 20 seconds after liftoff or
    400 ft.
  • If aborting, uninhibited when below 75 kts.
  • Amber MC indication and beeps when uninhibited.
88
Q

Master Warning Inhibit?

A
  • Starts at nose strut extension, ends 20 seconds after
    liftoff or 400 ft.
  • Red indication.
  • Red Master Warning indication and bell when
    uninhibited
89
Q

TAKEOFF CONFIGURATION WARNING:

A
  • When on the ground and either engine is advanced
    toward takeoff power and any of the following occur:
  • Parking brake is parked
  • Stabilizer trim not in the green band takeoff range
  • Spoiler handle not in the DOWN detent position
  • Flaps not in the takeoff position (leading edge slats
    or trailing edge flaps)
  • Flap / slat position does not agree with flap handle
    position (767)
90
Q

ENGINE STARTER DUTY LIMITS: for the 757?

A
  • 757 engine start duty cycle: 3 cycles of up to 2
    minutes continuous operation, run down to zero N3 at
    the end of each cycle, (15 minutes of cooling after the
    3r
    d
    cycle).

767 (1 decks)

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