General Limitations - SII

Question 1

Authorized Operations:

• _____ and _____
• _____ and _____ flight
• Flight into ______ ______

Answer 1

• Day** and **Night
• VFR and IFR flight
• Fight into icing** **conditions

Question 2

Maximum Baggage Loads

Nose Compartment - _____

Aft Cabin - _____

Tailcone Compartment - _____

Answer 2

Nose - with SBS550-30-15 - 330 LBS

without - 350 LBS

Aft Cabin - 600 LBS, 300 each side

Tailcone - with Freon A/C - 300 LBS

without - forward of net - 300 LBS

aft of net - 200 LBS

TOTAL - 500 LBS

Question 3

Certified under FAR Part _____

Answer 3

FAR Part 25

Question 4

The emergency exit door pin must be _____ _____ _____ _____.

Answer 4

The emergency exit door pin must be removed** **prior** **to** **flight.

Question 5

No _____ _____, including _____.

No intentional stalls above _____ or at engine speeds between _____ and _____ N₁.

Answer 5

No acrobatic maneuvers, including spins.

No intentional stalls above 25,000 ft**. or at engine speeds between **61.0%** and **65.0% N1.

Question 6

Minimum crew and requirements

• (crew required)
• (PIC requirements)
• (SIC requirements)
• (Category II requirements)

Answer 6

• Pilot and copilot.
• The pilot in command 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 flights above 18,000 ft. or flight into instrument meteorological conditions, and meet the requirements of FAR 61.55.
• Category II operation requires two pilots who are qualified in accordance with FAR 61.3.

Question 7

For all takeoff and landings, the following apply:

• Seats must be _____ _____ and _____.
• Seat aft of the emergency exit in the _____ _____ _____.

Answer 7

For all takeoff and landings, the following apply:

• Seats must be fully** **upright** and **outboard.
• Seat aft of the emergency exit in the most** **aft** **position.

Question 8

Center of Gravity Moment Envelope

FWD Limit:

At 9,600 LBS or less - _____ MAC

At 14,700/15,100 LBS - _____ MAC

Straight line variation between

AFT Limit:

14,700/15,100 LBS or less - _____ MAC

Answer 8

Center of Gravity Moment Envelope

FWD Limit:

At 9,600 LBS or less - 15.0% MAC

At 14,700/15,100 LBS - 19.92/20.3 MAC

Straight line variation between

AFT Limit:

14,700/15,100 LBS or less - 28.0% MAC

Question 9

Load Factors

Answer 9

Inflight, Flaps:

Up (0^o):-1.52 to +3.8 G

T.O/ T.O. & APP/ LAND (7^o - 35^o):0.0 to +2.0 G

These accelerations limit angle of bank

in turns and severity of pull up maneuvers.

During Landing, Flaps:

T.O. & APP/ LAND (20^o - 35^o):+3.5 G