Airplane Systems

Question 1

Engine Fail Msg (less than command performance)

Answer 1

RED- thrust less than command and speed below 65 k and 6 k prior to V1

Caution ENG FAIL (L,R)-engine decelerates to less than Idle speed.
תעלם אם המנוע יתאושש או ב fuel control cut off

Question 2

ENG THRUST

Answer 2

• actual thrust significantly less than command thrust,or
• actual thrust is not increasing to command thrust, and
  -airspeed is V1-6 k or grater

Question 3

APU Automatic Start

Answer 3

In flight if Both AC Transfer busses lose power

Question 4

Center Hyd components

Answer 4

Flight cont
Leading edge
Trailing edge flaps
Landing gear
Alternate brakes
Nose gear steering
Main gear steering

Question 5

RAT

Answer 5

*Provides hyd only to the flight control connected to center hyd sys.
* provides hyd end Elec through the flight.
Deploy automatically:
-both Engines failed and Center sys pressure is low ,or
-both AC transfer buses unpowered,or
-all 3 Hyd sys pressure are low.
**the hot battery or app battery must be powered

Question 6

TAC thrust asymmetry compensation

Answer 6

• if thrust level on one engine differs by 10% from other engine, automatically adds rudder.- Before Liftoff TAC uses less rudder to help pilot recognize engine failure, after Liftoff fully compensate

TAC Available except:
* speed below 70 k on ground
* reverse applied, or
*loss of engine data or sys malfunction
** TAC May disengage following severe damage or surge

Question 7

Wheel to rudder Cross-Tie

Answer 7

Provides capability to control the initial effect of Engine failure using control wheel inputs only.
It can deflect the rudder up to 8 degrees. And below 210k in normal mode

Question 8

Flight Control Modes

Answer 8

• primary
• secondary
  -Direct

Question 9

Flaps Control Modes

Answer 9

-Primary (Hyd)
-Secondary (electric)
-Alternate (electric)

Question 10

TOGA in the ground

Answer 10

-Below 50k activate THR REF (thrust limit page).
If not pushed below 50k- no operation of A/T until 400’
-if pushed above 80k: disarms LNAV/VNAV, & automatically show FD’s if off

Question 11

TOGA in flight TAKE OFF

Answer 11

• removes T/O & Climb derates &assumed
  -A/T in THR REF mode
  -disarm LNAV/VNAV
  -50’-400’sect TOGA Roll mode
  -above 400’ selects TOGA roll & pitch

Question 12

TOGA in flight Approach
(Flaps not up or GS capture)

Answer 12

-activate AT in THR mode with GA reference. Thrust adjust to provide 2000 rpm climb
-select TOGA roll & Pitch modes
-arms LNAV
-disarm AFDS modes
-inhibits during landing from 2 feet for 3 sec or more, if Landing is cancel TOGA available again above 5 feet.

Question 13

Engine start procedure
(Oil pressure)

Answer 13

-if no oil pressure indication by EGT rise, do ABORTED START ckexklist
#oil temp must be >-40 for start and 50 c before advancing thrust to take off power

Question 14

Holding speeds ICAO

Answer 14

<14000”- 230k
14000” to 20000” 240k
>20000”-265k

Question 15

Holding speeds FAA

Answer 15

<6000”-200k
6000”-14000”-230k
>14000”-265k