Limitations

Front 1

Required Flight Crew

Back 1

Pilot, Co-pilot (Captain, First Officer)

Front 2

Types of Aircraft Operations

Back 2

This aircraft meets the airworthiness requirements of Title 14 CFR Parts 25 and 36. When the appropriate equipment and instruments, as required by the airworthiness and operating regulations are approved, installed and in operable condition, flight in the following conditions are approved:
• Day and Night
• VFR and IFR
• Flight in Icing conditions
• RVSM

Front 3

Cabin Pressurization

Back 3

Maximum differential pressure........................8.1 psi

Auto Mode normal maximum differential .................... 7.8 psi

Maximum negative differential pressure...................- 0.3 psi

Front 4

Unpressurized Flight

Back 4

Maximum Altitude for operation after an in flight depressurization is 10,000 ft. MSL unless MEA or other constraints require a higher altitude.

Maximum altitude when aircraft is dispatched for unpressurized flight is 10,000 ft.

Front 5

Maximum Operating Airspeed
VMO/MMO

Back 5

320/.78

Front 6

Maximum Operating Airspeed
8000-10000 Ft MSL-VMO

Back 6

Red Line

Front 7

Maximum Turbulence Penetration-Vb/Mb

Back 7

250/.63 whichever is lower.
200 at or below 10,000 ft.

Front 8

Maximum Maneuvering- Va

Back 8

200

Front 9

Landing Gear Extension-Vloe

Back 9

250

Front 10

Landing Gear Extension-Vle

Back 10

250

Front 11

Landing Gear Retraction-Vlor

Back 11

200

Front 12

Flap Placard Speeds-9

Back 12

250

Front 13

Flap Placard Speeds-22

Back 13

200

Front 14

Flap Placard Speeds-45

Back 14

145*

Note-

*Momentary airspeed excursions that are due to wind gusts or turbulence are allowed up to 155 kts. with no crew or maintenance action required.

*Steady state operation over 145 kts. is not allowed and must be entered into the AML.

Front 15

Rudder Limitation

Back 15

4. A full or nearly full rudder deflection in one direction followed by a full or nearly full deflection in the other direction, even at speeds below the design maneuvering speed, can dramatically increase the risk of structural failure of the vertical stabilizer or the rudder.

Front 16

Maximum Operating Altitude

Back 16

37,000 ft

Front 17

Minimum Takeoff and Landing Pressure Altitude

Back 17

-1,000 ft

Front 18

Maximum Takeoff and Landing Pressure Altitude

Back 18

8,000 ft

Front 19

Takeoff and Landing Temperature Limits- Minimum

Back 19

-40 C SAT

Front 20

Takeoff and Landing Temperature Limits: Maximum -
(-1,000 ft. Pressure Altitude)

Back 20

52 C SAT

Front 21

Takeoff and Landing Temperature Limits: Maximum -
(8,000 ft. Pressure Altitude)

Back 21

34 C SAT