Cessna Citation Ce-500 Type Rating Oral Exam

Front 1

Fuel Quantity

Back 1

1903 lbs Per Wing

3806 lbs Total

Front 2

Hydraulic reservoir capacity

Back 2

0.65 Gallons Useable

Front 3

Oil tank capacity

Back 3

2.39 Gallons

1.25 Useable

Front 4

Engine

Back 4

Pratt & Whitney

JT15D-1A

Front 5

Engine Thrust

Back 5

2200 lbs.

Front 6

Maximum Ramp Weight

Back 6

12,000 lbs.

Front 7

Maximum Takeoff Weight

Back 7

11,850 lbs.

Front 8

Maximum Landing Weight

Back 8

11,350 lbs.

Front 9

Mno

Back 9

0.705 Mach

Front 10

Vmo, below 14,000 feet

Back 10

262 kts.

Front 11

Va @ Max Takeoff Weight

Back 11

187 kts.

Front 12

Maximum Speed for flaps takeoff and approach

Back 12

202 kts.

Front 13

Maximum Speed for Flaps Land

Back 13

176 kts.

Front 14

Vlo

Vle

Back 14

176 kts.

Front 15

Vmca

Back 15

Below stall for all weights

Front 16

Vmcg

Back 16

55 kts.

Front 17

Maximum operating altitude

Back 17

41,000 ft.

Front 18

Maximum altitude for takeoff and landing

Back 18

14,000 ft.

Front 19

Demonstrated X-Wind component

Back 19

25 kts.

Front 20

Maximum OAT at Sea Level

Back 20

54C

Front 21

Maximum GPU start in 30 Minutes

Back 21

3 Starts

Front 22

Maximum battery (NiCad) starts per hour

Back 22

3 Starts

Front 23

Maximum oil temperature

Back 23

-40C

Front 24

Hydraulic fluid type

Back 24

Skydrol

Front 25

Oil Type

Back 25

Type II

Front 26

Fuel Type

Back 26

Jet A

Front 27

Fuel anti-icing additive

Back 27

Prist

Front 28

Main landing gear tire pressure

Back 28

100 psi

Front 29

Nose landing gear tire pressure

Back 29

120 psi

Front 30

Normal pressurization differential

Back 30

8.5 psi

Front 31

The Freon A/C receives electrical power from

Back 31

Main DC Bus

Front 32

Maximum Alt for Freon A/C use

Back 32

18,000 ft

Front 33

The bypass ratio of JT15D-1A

Back 33

3.3:1

Front 34

After starting, the fan section (N1) is driven by

Back 34

Low Pressure Turbine

Front 35

After starting, the compressor section (N2) is driven by

Back 35

High Pressure Turbine

Front 36

How many ignitors are in each engine

Back 36

2

Front 37

N1 produces what % of total trust

Back 37

75%

Front 38

Above flight idle, the N1 tape is powered by

Back 38

N2 Tach Generator

Front 39

Thrust Reversers must be reduced to idle below

Back 39

60 kts.

Front 40

Which bus powers the fire protection system

Back 40

Main DC bus

Front 41

The maximum fuel imbalance between wings is

Back 41

800 lbs.

Front 42

How many fuel pumps are in the fuel system

Back 42

5 per side

Front 43

How many fuel drains are in each wing

Back 43

5 Wing, 1 Sump

Front 44

If a low fuel light illuminates, the appropriate fuel boost pumps must be selected to

Back 44

ON

Front 45

Engine driven fuel pump output pressure is

Back 45

500-700 lbs

Front 46

Normal hydraulic pressure is

Back 46

60 psi

Front 47

Hydraulic system operating pressure

Back 47

1500 psi

Front 48

With the landing gear not down & locked, the warning horn will sound if N2 is less than

Back 48

70%

Front 49

With the landing gear not down & locked, the warning horn will sound if flaps are beyond

Back 49

15 degrees

Front 50

If the nitrogen bottle is full, how many emergency brake applications are available

Back 50

10 applications

Front 51

Who must reset the emergency gear extension handle, if it has been used

Back 51

A&P Mechanic

Front 52

If N2 is increased to > 85% with the speed brakes extended, they will

Back 52

Retract

Front 53

The control lock should not be set if the aircraft is to be

Back 53

Towed

Front 54

To use a GPU to power the aircraft, the battery switch must be

Back 54

ON

Front 55

With the battery switch in the OFF position and both generators operating. What equipment becomes inoperative?

Back 55

Emergency Battery Items

Front 56

With a generator ONLINE and the battery switch in the EMER position. Battery charging is

Back 56

Disabled

Front 57

The engine inlet probe and bullet are anti-iced by

Back 57

Bleed Air

Front 58

Anti-Ice systems should be turned on before operating in visible moisture when the OAT is below

Back 58

4C

Front 59

Approximately how many minutes are required after selecting Engine Anti-Ice ON before the FAIL lights go out?

Back 59

2 Minutes

Front 60

How many de-ice systems are available?

Back 60

One, De-Ice Boots

Front 61

In Icing conditions, if the OAT is above 0F the W/S TEMP switch should be set to

Back 61

LOW

Front 62

The windshield alcohol supply will last

Back 62

10 minutes, pilot side only

Front 63

The primary and secondary outflow valves will close during takeoff with an N2 of greater than

Back 63

85%

Front 64

The oxygen over-pressurization disc will rupture when line pressure exceeds

Back 64

2500 psi

Front 65

The passenger oxygen masks will drop if the cabin altitude exceeds

Back 65

13,500 +/- 600 ft

Front 66

How does the emergency dump valve operate to dump cabin pressure?

Back 66

Manually opens vacuum control line to outflow valve

Front 67

F/D AC FAIL

Back 67

AC inverter to Flight Director - FAILED

Front 68

CAB ALT 10000

Back 68

Cabin pressure altitude is above 10,000 ft

Front 69

L Fuel Level LO

Back 69

Left fuel tank 179 to 264 lbs. remaining

Front 70

L Oil Press LO

Back 70

Left engine oil pressure below 35 PSI

Front 71

Fuel Filt Bypass

Back 71

Pressure differential across fuel filters is 3.5 to 4.0 psi

Front 72

L Eng Ice Fail

Back 72

Any one of the leading edge heating elements inop

Temperature controller failed

Inboard wing leading edge is below 60F

Engine Nacelle inter temp is less than 170F with N2 > 60% or bleed air valve not fully open

Engine stator anti-ice valve is not fully open

Front 73

L Gen Off

Back 73

Left generator power relay is open

Front 74

L Hyd Press L

Back 74

Left hydraulic pump failed - 25 PSI difference

Front 75

Batt O'Heat

Back 75

Battery between 140 and 160 degrees C

Front 76

Left Eng Fire (Push) (Steady Red)

Back 76

Left engine fire warning. Pushing button closed fuel F/W shut off valve, hydraulic shut off valve, trips generator relay, and arms both fire bottles

Front 77

L Fuel Press LO

Back 77

Fuel pressure to the left engine is below 20 PSI

Front 78

Hyd Press ON

Back 78

Hydraulic bypass valce is closed, pressure is 1500 PSI

Front 79

Hyd Level LO

Back 79

0.2 Gallons

Front 80

Air Duct O'Heat

Back 80

Cabin Air Duct temperature exceeds 275F

Front 81

Emer Press ON

Back 81

Emergency Pressurization valve is open due to ACM failure

Front 82

L Fuel Boost ON

Back 82

Power is applied to the left fuel boost pump

Front 83

Red MWS Light (Flashing)

Back 83

Any RED annunciator, Double generator light failure, or thrust reversers unlocked

Front 84

SPD Brake Extended

Back 84

Speeds Brakes Extended

Front 85

Door Not Locked

Back 85

Any one of the main entrance, 2 nose baggage, or rear baggage door is not locked

Front 86

WS air O'Heat (Switch on High)

Back 86

Windshield Bleed air exceeds 146F

Front 87

Batt O'Heat Flashing

Back 87

Exceeds 160F

Front 88

Surf Deice

Back 88

Wing / Stabilizer de-ice boots cycling

Front 89

Squat Switch Items (Ground Mode)

Back 89

Gear Handle locking pin engaged

Generator cross start enabled

Cabin outflow valves opened below 85% N2

Emergency pressurization bleed air valve closed

Hobbs meter disabled

Thrust reversers enabled

Front 90

Electric valves that fail OPEN

Back 90

Windshield anti-ice

Engine nose cowl anti-ice L/R

Engine stator anti-ice L/R

Hydraulic bypass

Speed brake control

Cabin bleed air flow control, and shut off L/R

Fuel motive flow shutoff L/R

Front 91

Electric valves that fail LAST position

Back 91

Crossfeed

Fuel Shutoff

Hydraulic Shutoff

Front 92

Electrical valves that fail OPEN

Back 92

Emergency Air

Ground Air

Front 93

When must oxygen masks be used?

Back 93

Single Pilot Above FL 350

and above FL 410 crew

Front 94

Clear Air Turbulence associated with the Jet Stream is typically found?

Back 94

On the polar side of the Jet Stream

Front 95

At FL 400 Time of Useful Consciousness is approx?

Back 95

9-15 seconds

Front 96

Night vision can deteriorate at cabin pressures as low as?

Back 96

5000 ft

Front 97

Emergency Restart - Two Engines

Back 97

1. Ignition Both ON

2. Boost Pumps ON

3. Throttles IDLE

4. If Alt. Allows increase airspeed to 240 KIAS

Front 98

Electrical Fire or Smoke

Back 98

1. Oxygen Masks, Select 100%

2. Oxygen MIC switches - MIC OXY MASK

Front 99

Rapid Decompression (Cabin ALT 10000)

(Master Warning)

Back 99

1. Oxygen Masks, 100%

2. Emergency Decent , As Required

3. Passenger Oxygen - ensure pass getting oxygen

4. Oxygen Mic Switches - MIC OXY MASK

Front 100

Emergency Decent

Back 100

1. Throttles IDLE

2. Speed Brakes EXTEND

3. initiate moderate bank

4. 15% Nose Down

Front 101

Total Electrical Failure

Back 101

Battery power to emergency bus , 30 Mins

*if batt left in Battery pos, less than 15 Mins

Aux Power to Standby Altitude Gyro

Flaps Inoperative , Electrical Pitch Trim

Autopilot, Yaw, Damper Radar

Air Master Warning Lights

Fire warning and extinguishing

All exterior lights , Passenger safety switch

Front 102

Total Electrical Failure (Comms)

Back 102

COMM selected to EMERG position.

Headset 1 selected, Headset required

Transponder Inoperative

Front 103

Total Electrical Failure (Hydraulic)

Back 103

Speed Brakes Open to "Trail" Position

Landing gear must be extended with AUX handle and Air Bottle

Normal Brakes Operative

Emergency Air bottle available

Front 104

What is on the EMERGENCY BUS?

Back 104

Comm 1

Nav 2

Co-Pilot HSI

Cockpit Overhead Floods

Front 105

What is on the HOT BUS?

Back 105

Nose Baggage Light

Aft. Baggage Light

Passenger safety Light

Front 106

Operational Aux Equipment on EMERGENCY

Back 106

Captains Altimeter (manual mode) Airspeed/VSI

Capts RMI compass card and remove Nav 2 CDI

CoPilots altimeter, Airspeed, VSI, and altitude ind

Suction pressure guage

Oxygen contents guage

N1 Vertical Tape

Standby altitude gyro, indicated by yellow light

Front 107

Oil Tank Capacity

Back 107

2.39 Gallons

1.25 Gallons Useable

Front 108

Maximum Fan (N1) Speed

Back 108

102.1%

Front 109

Maximum Compressor (N2) Speed

Back 109

95%

Front 110

Maximum ITT

Back 110

780C - Start

689C - max continuous (single engine)

670C - for max cruise

580C - for max idle

500C - max abnormal during start, but can still fly

Front 111

Starter Limit

Back 111

3 start attempts, 30 mins with 30 secs rest

Front 112

Nicad Battery Limit

Back 112

3 starts per hour

Front 113

Maximum oil temp

Back 113

40C

Front 114

Maximum fuel temp

Back 114

29C

Front 115

Vlo extending

Back 115

176 KIAS

Front 116

Vlo retracting

Back 116

176 KIAS

Front 117

Vle

Back 117

176 KIAS

Front 118

Vfe 15 degrees

Back 118

202 KIAS

Front 119

Vfe 40 degrees

Back 119

176 KIAS

Front 120

Vmo above 14000

Back 120

277 KIAS OR 262 KIAS

Front 121

Vmo below 14000

Back 121

262 KIAS

Front 122

Mmo

Back 122

.705 Mach

Front 123

Va

Back 123

150-187 depending on weight

Front 124

Tubular air penetration

Back 124

180 KIAS

Front 125

Landing Max Water Slush

Back 125

3/4 Inch

Front 126

Landing Max Temp

Back 126

-54C

Front 127

Landing Min Temp

Back 127

-54C

Front 128

Landing

Back 128

Autopilot OFF