Limitations

Question 1

Minimum Crew:

Answer 1

• Pilot and Copilot
• The Pilot Must Have A CE-500 Type Rating And Meet The Requirements Of FAR 61.58
• The Copilot Shall Possess A Multi-engine Rating, An Instrument Rating For Flight Above Or Into IMC And Meet The Requirements Of FAR 61.55

Question 2

Baggage Limits:

Answer 2

Aft Cabin Storage Compartment: 600 LBS
Tailcone Baggage Compartment:500 LBS
Nose Baggage Compartment: 350 LBS

Question 3

Passenger Seat Position:

Answer 3

For Takeoff and Landings, the following apply:

• Seat Must Be Fully Upright And Outboard
• Passenger Seat Belts And Shoulder Harnesses Must Be Fastened
• The Seat Just Aft Of The Emergency Exist Must Be In Most Aft Position

Question 4

Maximum Taxi and Ramp Weight:

Answer 4

16,500 Pounds

Question 5

Maximum Takeoff Weight:

Answer 5

16,300 Pounds

Question 6

Maximum Landing Weight:

Answer 6

15,200 Pounds

Question 7

What is the Maximum Zero Fuel Weight:

Answer 7

12,200 Pounds

Question 8

Maximum Flaps Extended (VFE ) for:

Answer 8

Full Flaps (35°) : 173 KIAS
Partial Flaps (7° or 15°): 200 KIAS

Question 9

Maximum Landing Gear Extended Speed (VLE):

Answer 9

292 KIAS

Question 10

Maximum Landing Gear
Operating Speed (VLO):

Answer 10

Extending = 250 KIAS
Retracting = 200 KIAS

Question 11

VMCA (Minimum Control - Air):

Answer 11

85 KIAS

Question 12

VMCG (Minimum Control - Ground):

Answer 12

86 KIAS

Question 13

Maximum VMO Below 8,000 Feet:

Answer 13

261 KIAS

Question 14

Maximum VMO Between 8,000 and 28,907 Feet:

Answer 14

292 KIAS

Question 15

Maximum MMO (Above 28,907 Feet):

Answer 15

0.755M Indicated

Question 16

Maximum Speedbrake Extension (VSB):

Answer 16

NO LIMIT

Question 17

Maximum Autopilot Operation (Speed):

Answer 17

292 KIAS or 0.755M

Question 18

Maximum Airport Pressure Altitude for Takeoff and Landing:

Answer 18

14,000 Feet

Question 19

Maximum Air Temperature Approved for Takeoff and Landing:

Answer 19

ISA + 39°C

Question 20

Maximum Crosswind - Demonstrated:

Answer 20

20 KTS

Question 21

Maximum Tailwind Component:

Answer 21

10 KTS

Question 22

Maximum Tire Ground Speed

Answer 22

165 KTS

Question 23

Maximum Water/Slush on the Runway:

Answer 23

0.5 Inch

Question 24

Vertical Navigation (VNAV) System Must be OFF Below:

Answer 24

500 Feet AGL

Question 25

Minimum Airspeed for Sustained Flight in Icing Conditions (Except for Approach and Landing):

Answer 25

160 KIAS

Question 26

Maximum Calibrated Operating Altitude:

Answer 26

45,000 Feet

Question 27

Generator Load in Flight

Answer 27

300 Amps

Question 28

Maximum Load Factor in Flight for Flaps UP

Answer 28

-1.44 to +3.6G at 16,300 LBS

Question 29

Maximum Load Factor in Flight for Flaps 7° to 35°

Answer 29

-0.0 to +2.0G at 16,300 LBS

Question 30

Maximum Load Factor for Landing, Flaps 15° to 35°

Answer 30

+3.5G at 15,200 LBS

Question 31

Minimum Altitude for Autopilot Use:

Answer 31

- 1,000 ft AGL – Enroute - 300 ft AGL - Non-Precision Approach - 180 ft AGL - Approaches The autopilot and yaw-damper must be off for takeoff and landing.

Question 32

Which Standby Instruments Must be | Functioning for Takeoff?

Answer 32

- ATT - ALT/ASI - HSI A Satisfactory Preflight Test Must be Accomplished on the Standby Gyro System

Question 33

Generator Load ground

Answer 33

125 Amps at 46% N2 | 225 Amps at 52% N2

Question 34

Battery Limitations for Engine Starts

Answer 34

- Three Engines Starts per Hour - Three Generator-Assisted, Cross-Starts Equal One Battery Start - GPU Start Does NOT Count as a Battery Cycle

Question 35

STARTER Limitations for Engine Starts

Answer 35

With Battery as Starter Power Source: - Three Engine Starts per 30 Minutes with a 30- Second Rest Period Between Cycles With GPU or Generator-Assisted, Cross-Start: - TWO Engine Starts per 30 Minutes with 30- Second Rest Period Between Cycles

Question 36

What are the Voltage considerations when | using GPU for engine starts?

Answer 36

Use of GPU with a voltage in excess of 28V DC or current in excess of 1,000 amps may damage the starter.

Question 37

Maximum Pressure Differential

Answer 37

8.9 psid, +0.1 or -0.1 psid

Question 38

The Stall Warning System:

Answer 38

Must be Verified Operational for Takeoff per the Preflight Test in the AFM

Question 39

What Are the Maximum Asymmetric Fuel Weights for Normal and Emergency Conditions?

Answer 39

- Normal: 200 lbs | - Emergency: 600 lbs

Question 40

Pitot/Static Heat Permissible Operating Time

Answer 40

Limit Ground Operations of Pitot/Static Heat to 2 MINUTES to Preclude Damage to the Pitot/Static Tubes and the Angleof-Attack Probe

Question 41

When Must All Anti-Ice Systems Be Turned On?

Answer 41

Operating in Visible Moisture and When TAT/RAT is Below +10Flight Idle 52(min) 580

Question 42

Continuous Use of the Supplemental Oxygen System is Prohibited Above the Following CABIN Altitudes:

Answer 42

- Carrying Passengers - 25,000 ft | - Crew Only - 40,000 ft EROS

Question 43

Reverse Thrust Must be Reduced to Idle Reverse by Which Speed

Answer 43

60 KIAS

Question 44

Maximum Reverse Thrust is Limited to:

Answer 44

Fan Speed - 86% for Ambient Temperatures Above -18°C - 79% for Ambient Temperatures Below -18°C

Question 45

Additional Thrust Reverser Limitations

Answer 45

- Must be Verified Operational Per Preflight Test - Prohibited During Touch and Go Landings - Prohibited on Sod or Gravel Runways - Max. Deployment Time is 15 Minutes in Any One-Hour Period

Question 46

Powerplant Operating Limits | JT15D-5D Engines

Answer 46

N1 N2 ITT Time Takeoff 100.0 97.0 720°C 5 Min Start -- -- 550°C 700°C

Question 47

APPROACH AND LANDING IN ICING CONDITIONS

Answer 47

When any residual ice is present or can be expected during approach and landing, engine anti-ice must be on to maintain adequate stall warning margin.

Question 48

Minimum oil temperature for starting

Answer 48

-40°C

Question 49

Thrust Reverser Depoyment

Answer 49

The nosewheel must be in firm contact with the ground prior to deploying thrust reversers