מבנה מטוס

Question 1

PTU

Answer 1

משאבה הידראולית מונעת בלחץ A על מערכת B
לתפעול le slats and flaps iaoutoslats
עובדת עם מטוס באויר ולחץ נמוך מ 2350 במשאבת edp ימין ( אבדן מנוע לדוגמה )
מדפים בין 1 ל 15 או not up ב sep

Question 2

Landing gear transfer unit

Answer 2

Backup of low A system by B for LG retract ( left eng fail )
Valve opens for B oil
Left RPM < idle
Airborn
Gear handle up
One or Two mains not up

Question 3

SEP

Answer 3

All 900 + H J K L

LE slats extend position For 1-25 , full ext position for 30,40 ( normal is full above 5)
Special FMC Database
Two position tail skid

Question 4

Auto Slats

Answer 4

At flaps 1-5 / 1-25 ( LE SLATS extend pos)
When approaching stall before stick shaker
LE Slats move to full extend

Question 5

Landing Gear warning

Answer 5

any gear is not down and locked and

Flaps up through 10 –

• altitude below 800 feet RA, when either forward thrust lever set between idle and approximately 20 degrees or an engine is not operating and the other thrust lever is less than 34 degrees. The landing gear warning horn can be silenced (reset) with the landing gear warning HORN CUTOUT switch

• if the airplane descends below 200 feet RA, the warning horn cannot be silenced by the warning HORN CUTOUT switch.

Flaps 15 through 25 –

• either forward thrust lever set below approximately 20 degrees, or an engine not operating and the other thrust lever is less than 34 degrees. The landing gear warning horn cannot be silenced with the landing gear warning HORN CUTOUT switch.

Flaps greater than 25 –

• regardless of forward thrust lever position. The landing gear warning horn cannot be silenced with the landing gear warning HORN CUTOUT switch.

Question 6

Standby Hydralic

Answer 6

rudder
Standby yaw damper
LE flaps and slats extend only
Thrust Reversers

אוטומטית באבדן מערכת a או b באויר או מעל 60 קשר עם מדפים flight control on
או בכשלון שלforce fight monitor בהגאי כיוון