Flight Insts/warnings Flashcards

1
Q

What Flight Information is displayed by the ISFD ?

A

Attitude Airspeed Altitude ILS GLS and heading information

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

When does the EGT start limit line appear on EGT indications?

A

When Engine Fire Switch is in
Fuel Switch - cut off
N2 RPM below Idle

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

What causes the Automatic Display of Secondary Engine indications ?

A
  1. When displays first receive electrical power
  2. Fuel Control is moved to Cut Off in flight
  3. An Engine Fire Switch is pulled in Flight
  4. A Secondary engine parameter is exceeded
  5. Engine N2 RPM is below idle in flight
  6. A Start Selector is in the START position
  7. FUEL FLOW ENG L/R Advisory is shown.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
4
Q

When AIR DATA / ATT Source selector is in Auto what is the PRIMARY source ?

A

ADRS

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

When AIR DATA / ATT Source selector is in Auto what is the Source of the backup information
AIRSPEED
ALTITUDE
ATTITUDE ..?

A

1 Angle of Attack and INERTIAL DATA
2 GPS
3 ISFD

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

Display CURSOR Control is provided by which units? (3)

A

CCD. MFK . EFIS CTRL

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

What are the Primary source of attitude and inertial navigation system information to the flight displays ?

A

The IRS is the primary source for attitude and inertial navigation position information. The major components of the IRS are:

two inertial reference units (IRU)
two attitude heading reference units (AHRU)

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

The IRUs use what Data to compute position information ?

A

The IRU is the primary source for independent inertial navigation position information. The IRU processes information measured by its internal gyros and accelerometers and GPS inputs. (Refer to Inertial Reference Unit (IRU) in Chapter 11., Section 20, for additional information.)

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

What are the major components of the ADRS ?

A

The ADRS provides primary, secondary, and standby air data. The major components of the ADRS are:

six air data modules
six static ports
three pitot probes
two angle-of-attack sensors
one total air temperature probe.
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
10
Q

What are the main components of the IRS?

A

2 IRUs

2 AHRUs

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

What is the sequence of page selections for the FMC ?

A
  1. IDENT
  2. POS REF
  3. RTE
  4. DEPARTURES
  5. NAV RAD
  6. PERF INIT
  7. THRUST LIM
  8. TAKE OFF REF P1/2
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
12
Q

On what page can the Flight Crew check accuracy of the three FMC positions ?

A

Position Reference Page 3/4
On position reference page 3, the flight crew can observe the calculated positions of the left, right and center FMCs. The line title indicates which FMC is being used as MASTER, SPARE or BACKUP. This page also allows the flight crew to enable or inhibit position updating modes used by the FMC.

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

What info is displayed on POS REF 4/4 ?

A

Position Reference Page 4/4
Position reference page 4 displays the present position of individual navigation sensors in bearing/distance format from the Master FMC position. This page provides the capability to remove specific sensors from the FMC navigation solution.

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

What type of Alert messages can be shown on the EICAS

A

Warnings Cautions Advisory Communications Status Memo

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

EICAS MESSAGES - how can they be differentiated ?

A
RED - Warning / Aural 
CAUTION - Amber / Aural
ADVISORY - Amber indented
Memo / status - White
Comms - White low indented
How well did you know this?
1
Not at all
2
3
4
5
Perfectly
16
Q

CONFIG GEAR WARNING ON APPROACH ?

A

The landing configuration warning system alerts the crew the landing gear is not extended for landing. The EICAS warning message CONFIG GEAR is displayed if:

the airplane is in flight, and
any landing gear is not down and locked, and
any of the following configurations exist:
either thrust lever closed and radio altitude less than 800 feet, or
FLAP lever in landing position

17
Q

ALERT INHIBITS- Firebell and master warning lights - when are they inhibited on takeoff ?

A

From V1 to 400’ or 25 secs after V1 whichever comes earlier.

18
Q

ALERT INHIBITS - beeper and Master Caution during takeoff ?

A

80 kts to 400’ or 20 secs after lift off , whichever comes first.