CJ3

Question 1

Under which FAR is the CJ3 certified?

Answer 1

FAR Part 23 (commuter, single pilot)
12,500 > 19,000

Question 2

How tall is the tail?

Answer 2

15’ 3”

Question 3

What documents are required on board?

Answer 3

ARROW
AFM
Collins Pro Line 21 Reference Guide
Collins FMS 3000 Reference Guide
Normal Procedures Checklist
Emergency/Abnormal Proc Checklist
*Checklist must be the manufacturers checklist during single pilot ops

Question 4

What is the forward baggage compartment weight limit?

Answer 4

400lbs

Question 5

Where is the sensor for door unlocked annunciator in the baggage compartments?

Answer 5

Key lock

Question 6

How many door seals are there?

Answer 6

Two. One inflates with service air. Secondary door seal is in place if primary fails.

Question 7

How many door pins does the cabin door have?

Answer 7

12

Question 8

Which cabin door pins are tied to the annunciator?

Answer 8

Top two and bottom two, forward and aft.

Question 9

What is the weight limitation for the aft baggage compartment?

Answer 9

600lbs

Question 10

Describe the emergency exit door.

Answer 10

It’s a plug-type door. It will not operate if the cabin is pressurized.

Question 11

What system operates the speed brakes and flaps?

Answer 11

Hydraulic

Question 12

Describe the generators

Answer 12

2 - 29v engine mounted generators that supply DV power. Inverters are not pilot controlled.

Question 13

Which types of batteries are in the CJ?

Answer 13

Lead Acid and NICAD

Question 14

Fuel System

Answer 14

Wet wing. More fuel, stronger wing.
4710lbs of total fuel.
Fuel transfer system does not crossfeed.

Question 15

What engines does the CJ3 have

Answer 15

Williams FJ44-3A (Full Authority Digital Engine Control) Medium Bypass Turbofan Engines.
3.5:1 Ratio
Produce 2780lbs Thrust Each
Ice Protection and Fire Extinguishing Systems

Question 16

Hydraulics System

Answer 16

Engine driven hydraulic pumps.
Operate flaps, gear, speed brakes
Open center system
Only pressurized on demand

Question 17

Cabin Altitude

Answer 17

8.9psi differential
8,000’ cabin @ FL450
Sea Level Pressure up to 22,500’

Question 18

Oxygen

Answer 18

Provided for crew and passengers
Crew have quick donning, positive pressure masks

Question 19

What Avionics?

Answer 19

Collins Pro Line 21
2 PFDs, 1 MFD
Weather Radar
Dual Transponders
Autopilot

Question 20

What is the max allowable take of weight limitation?

Answer 20

13,870lbs

Question 21

What is the max allowable ramp weight limitation?

Answer 21

14,070lbs

Question 22

What is the max allowable landing weight limitation?

Answer 22

12,750lbs

*if taking off at max takeoff weight, it takes appro. one hour of flight time to be under max landing weight limitation

Question 23

What is the Zero Fuel Weight

Answer 23

10,510lbs

Question 24

What are the speed limitations?

Answer 24

< 8,000’ - 260 KIAS
> 8,000’ - 29,300’ - 278 KIAS
> 29,300 - .737 Mach

Question 25

How often are dock inspections required?

Answer 25

100hrs

Question 26

Where is the CG located

Answer 26

Back of seats 7&8

Question 27

How many pounds of ballasts moves the CG and how far does it move?

Answer 27

80lbs of ballast moves the CG 1”

Question 28

Va

Answer 28

Va is +/- 5kts of AOA Indicator = .6 L/D Max = .6

Question 29

What must be operational for single pilot ops

Answer 29

Autopilot. Pilot must wear headset as well

Question 30

V1

Answer 30

Decision Speed

Question 31

Cross Check Speed

Answer 31

70 KIAS

Question 32

V2

Answer 32

Vxse - best single engine angle of climb

Question 33

Where does 1st segment climb begin and end?

Answer 33

Begins at 35’ AGL. Ends when the gear is up.

Question 34

Where does 2nd segment climb begin?

Answer 34

It begins at gear up, and ends once the obstacle is clear or 1500’ AGL.

Question 35

Where does 3rd segment climb begin and end?

Answer 35

It begins once the obstacle is clear, speed is V2 + 10, and flaps come up.

Question 36

Where does the enroute segment begin?

Answer 36

Once the flaps are up.

Question 37

What is the en route speed?

Answer 37

130KIAS (en route ≈ Vyse)

Question 38

What is Vref?

Answer 38

Approach speed when 50’ AGL

Question 39

What is the required SINGLE ENGINE climb gradient?

Answer 39

STANDARD:1.2%. That is during 2nd segment climb. (Approx. 73’/NM) in VFR. 3.3% in IMC (Approx. 200’/NM). (3.3% is a TERPS requirement). NOT STANDARD: Must be published on a chart.

Question 40

What is the required climb gradient in IMC

Answer 40

200’/nm or 3.3%

Question 41

What is the approach climb gradient?

Answer 41

2.1%

Question 42

What is a wet runway?

Answer 42

A runway that is not dry

Question 43

What is a contaminated runway?

Answer 43

1/8” or 3mm of water on runway

Question 44

What is the best 2 engine climb speed?

Answer 44

222KIAS until FL250 and then .56mach

Question 45

During approach to landing, when are landing lights required?

Answer 45

300’ AGL and lower

Question 46

Pulse light power

Answer 46

Landing - Full Power Taxi - Half Power

Question 47

What is the power required for a battery start?

Answer 47

Volts x Amps = Power (Watts) 25v x 1,000a = 25,000 watts

Question 48

What is the battery start limitation?

Answer 48

3 starts per hour

Question 49

What is the battery usage on a generator start?

Answer 49

29v x 450a (generator) 29v x 350a (battery) Approx 1/3 of a battery start

Question 50

What does a Generator Control Unit (GCU) do?

Answer 50

Regulates, parallels, and protects

Question 51

How much time when battery power is switched to EMER?

Answer 51

Approx 30mins

Question 52

During start, when is fuel introduced?

Answer 52

Between 8-12% N1

Question 53

What is the Venr speed?

Answer 53

It is always 130KIAS

Question 54

What is the minimum single engine missed approach climb requirement?

Answer 54

Standard: Minimum climb of 2.1% Non Standard: Climb requirements are published on plate

Question 55

What system was disabled for figuring landing distance?

Answer 55

Speedbrakes were disabled.