Study Packet

Question 1

Max T/O Weight

Answer 1

53,000 lbs

Question 2

Max Landing Weight

Answer 2

47,000 lbs

Question 3

Turbulence speed and mach

Answer 3

Less than 280 KIAS or .75 Mach

Question 4

Max crosswind

Answer 4

27 kts - dry

15 kts - wet

Question 5

Min takeoff temp

Answer 5

-40c

Question 6

What type of engines?

Answer 6

2 General Electric CF34-3B1 High Bypass Turbofan Engines

Question 7

How much thrust does each engine produce?

Answer 7

8729 lbs

Question 8

How many hydraulic pumps?

Answer 8

6

Question 9

How many independent hydraulic systems?

How are Systems 1 and 2 pressurized?

How is System 3 pressurized?

Answer 9

3 Independent hydraulic systems

Systems 1 and 2: each pressurized by their respective engine driven pump and electric backup pump

System 3: pressurized by 2 electric hydraulic pumps

Question 10

What is the normal pressure in the hydraulic systems?

Answer 10

3000 PSI

Question 11

What flight controls are hydraulically powered?

What provides redundancy?

Answer 11

1. Elevators
2. Ailerons
3. Spoilerons
4. Rudder

Each flight control surface is powered by more than one hydraulic system for redundancy

Question 12

How are the flaps operated?

Answer 12

Electrically

Question 13

What are the flap detents?

Answer 13

0, 8, 20, 30, 45

Question 14

Which flap detents are used for takeoff?

Answer 14

8 and 20

Question 15

Which flap detent is used for landing?

Answer 15

45 normally

Question 16

Memory Items

L or R REV UNLOCKED

Answer 16

1. Affected thrust reverser - CONFIRM and IDLE (PM)
2. Affected THRUST REVERSER, EMER STOW - SELECT (PM)
   Refer to QRH POWERPLANT page 2-11

Question 17

Memory Items

Smoke/Fire/Fumes Procedure

Answer 17

1. Oxygen Mask / Smoke Goggles - ON, 100% (CR)
2. Crew and cabin communication - ESTABLISH (CR)
   Refer to QRH SMOKE - FIRE- FUMES page 1-1