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B-767 Oral exam guide with complete solutions
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B-767 Oral exam guide with complete solutions
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B-767 Oral exam guide with complete solutions10)The passenger oxygen system is deployed automatically when a cabin altitude of
14,000 feet is reached. - ANSWER-True
11)When the emergency handle on the over wing hatch is pulled; it retracts the inboard
spoiler (hatch side), deploys the over wing slide, illuminates the exterior emergency
lights (hatch side), and opens the hatch. - ANSWER-True
13)What happens when you rotate the oxygen mask Emergency/Test selector to
EMERGENCY? - ANSWER-Supplies 100% oxygen under positive pressure at all cabin
altitudes, and protects against smoke and harmful vapors
14)What does pulling the alternate deployment handle for the overwing exit do? -
ANSWER-Deploys the slide if the normal system fails
15)Which has priority in supplying the ground handling bus? - ANSWER-External power
18)What is the wingspan of the -200? -300? With winglets? - ANSWER--200 and -300:
156 feet 1 inch (47.57 meters)
-300 (winglets): 166 feet 11 inches (50.88 meters)
19)How is the engine thrust reverser actuated on GE engines? PW engines? -
ANSWER-767-300 GE: Pneumatically actuated by fan air from respective engine.
767-200 GE/PW and 767-300 PW: Hydraulically actuated by respective HYD system
20)The Thrust Rating of the CF6-80C2B7F engine is _____? - ANSWER-62,100 lbs
58) The Pitch Enhancement System, (PES) is an automatic feature to provide a third
power for stabilizer trim in the event what system fails? - ANSWER-Left and Center
hydraulic systems
64)With the speed brake lever NOT in the armed position, the spoilers will extend
automatically when either reverse lever is raised to the interlock stop on landing. -
ANSWER-True
64)With the speed brake lever NOT in the armed position, the spoilers will extend
automatically when either reverse lever is raised to the interlock stop on landing. -
ANSWER-True
A cargo fire warning occurs when either smoke detector senses the presence of smoke.
- ANSWER-False
a FAULT is indicated on the Left IRS, the Captain should: - ANSWER-Select his
instrument source IRS to ALTN
,A green LNAV FMA annunciation in the ADI indicates: - ANSWER-LNAV is engaged
A PACK OFF light indicates the pack valve is closed due to? - ANSWER-The selector is
in the off position or a pack trip has occurred or Loss of air to the pack
A red Warning Message can be cancelled by using the EICAS Cancel/Recall Switches.
- ANSWER-False
A skin heat exchanger is sometimes used to remove heat from the equipment cooling
air and is controlled automatically. - ANSWER-True
A white LNAV annunciation in the ADI indicates: - ANSWER-LNAV is armed
ADS can be active with CPDLC in-active - ANSWER-True
After engine start, it is not necessary to check the STATUS page, as any message
having adverse effect on the safe continuation of the flight, requiring crew attention, will
appear as an alert message. - ANSWER-True
After glide-slope capture, which of the following modes should appear on the EICAS
Thrust Mode Display? - ANSWER-GA
After landing, when can the Reverse Levers be raised to the interlock stop? - ANSWER-
When the thrust levers are at the idle position
After landing, which one of the following is required to disengage the operating AFDS
mode? - ANSWER-Disengage all autopilots and turn off both flight directors
After pulling out the APU Fire Switch, the APU fire bottle discharges when the APU Fire
Switch is rotated in either direction. - ANSWER-True
After selecting start on the APU control panel, the fault light will illuminate briefly as? -
ANSWER-A circuitry test is accomplished
After takeoff, when may the autopilot be engaged? - ANSWER-After a pitch mode is
selected
After touchdown with Auto Brakes armed, when is auto braking applied? - ANSWER-
Both thrust levers at idle and Wheels have spun up
After what point in an ILS approach can Go-Around mode be engaged? - ANSWER-G/S
capture or flaps moved from up
AIR SYSTEMS - ANSWER-AIR 1)
,AIRPLANE GENERAL - ANSWER-
All fire protection systems are powered by? - ANSWER-Hot battery bus
An amber standby bus off light illuminates and the EICAS message Standby Bus Off
displays when? - ANSWER-Either standby AC or DC bus is unpowered
An off flag in the stabilizer position indicator means? - ANSWER-Stabilizer trim indicator
failure
An off flag in the stabilizer position indicator means? - ANSWER-Stabilizer trim indicator
failure
ANTI-ICE, RAIN - ANSWER-1)
APU - ANSWER-1)
APU electrical power can be utilized; - ANSWER-Up to 43,100 feet
Are operations allowed when the reported braking action is NIL? - ANSWER-No...Ops
Prohibited
At approximately what radio altitude does the autopilot start the landing flare? -
ANSWER-50 ft
At higher airspeeds which wing components are locked out? - ANSWER-Outboard
ailerons
At least two IRS's must be aligned for the yaw damper system to operate - ANSWER-
False
At least two IRS's must be aligned for the yaw damper system to operate - ANSWER-
False
At the start of a takeoff roll, the N1 switch is pushed after manually spooling up the
engines to approximately what N1? - ANSWER-70%
At what recommended N2 RPM do you need fuel and ignition to continue the start? -
ANSWER-Max motoring
ATC clearances or instruction received digitally via CPDLC require a voice readback -
ANSWER-False
Auto Brakes are available on what brake system? - ANSWER-Normal Brake system
only
, Auto brakes can be disarmed after landing by? - ANSWER-Pedal braking applied,
either thrust lever advanced after landing,
Speed brake lever moved from the full up position after deployment,
Selecting the Auto Brakes Switch "OFF"
AUTOMATIC FLIGHT - ANSWER-1)
Automatic pressurization control for a flight requires selection of AUTO 1 or 2, desired
AUTO RATE and setting of LDG ALT. - ANSWER-True
Both batteries, (main and APU), receive power directly from which source? - ANSWER-
Ground service bus
Both the APU and the Aircrafts main batteries are required to start the APU. -
ANSWER-True
Can a chemical oxygen generator be shut off after it is activated? - ANSWER-No
Can both fire bottles be discharged into either engine? - ANSWER-Yes
Can clear air turbulence be detected by weather radar? - ANSWER-Turbulence can
only be detected when there is sufficient precipitation
Can communication with Cabin Attendant be established using an oxygen mask
microphone? - ANSWER-Yes
Can the crew manually enter a different GMT on the POS INIT page? - ANSWER-Yes-
But only the hour
Can the glideslope be captured prior to Localizer intercept? - ANSWER-Glideslope
capture is inhibited until localizer capture
Can the left forward fuel pump be switched off if it is supplying fuel to the APU on the
ground with the APU running? - ANSWER-No, the pump cannot be turned off
Can you cancel a status message with the EICAS CANCEL switch? - ANSWER-No
CAT I Autoland windspeed limitations are: Headwind, Crosswind Tailwind - ANSWER-
25, 25, 10
COMMUNICATIONS - ANSWER-1)
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