Wheels Up - Limits from the BE300 Limitations Sheet (GREEN ITEMS)

Question 1

Torque % Limits

Answer 1

Takeoff ……… : 100%
Max Continuous …..100%
Transient. …. 156% FOR 20 SECONDS

Question 2

ITT Temp Limits

Answer 2

Starting ………….. ;1000°c FOR 5 SECONDS
Idle ………………….. 750°C
Takeoff .. …….. ….. .820°C
Max Continuous … .820°C
Transient.:. …… ….. 850°C FOR 20 SECONDS
Cruise Climb … ……785°C

Question 3

Gas Generator RPM (%N1 )

Answer 3

Minimum Idle …… … 62%
Takeoff …. .. …………104%
;Max Continuous …. 104%
Transient. ……………. 104%.

Question 4

Propeller RPM - T/O, Max Continuous, Transient

Answer 4

Takeoff .. …… ~ .. … 1700 RPM
Max Continuous ……1700 RPM
Transient… ……………1870 RPM FOR 20 SECONDS

Question 5

Oil Pressure PSI Limits

Answer 5

Starting ……. …. ……. 0-200 PSI
Takeoff ……. ….. .. .. 90-135 PSI
.Max Continuous …. 90-135 PSI
Transient. … ………………200 PSI

Question 6

Oil Temperature Limits

Answer 6

Starting -40C (Minimum)

Takeoff 0 - 110C

Max Continuous 0-110°C

Transient. 0-110°c

Temperatures between 99°C and 110°C
are limited to a maximum of 10 minutes

Question 7

External Power Limits

Answer 7

Volts _____28.0-28.4Volts
Amp,,__ 1000Amps (Momentarily) 300 Amps (Continuously)

Question 8

Generator Limits

Answer 8

Maximum Generator Load In Flight:

Sea Level to 34,000 feet altitude 100%

Above 34,000 feet altitude 95%

Maximum Generator Load Ground Operation:

62-70% N1 = 75%

70-100% N1 = 100%

Question 9

Propeller Rotational Speed Limits

Answer 9

Transients not exceeding 20 seconds 1870 RPM
Reverse 1650 RPM
All other conditions 1700 RPM
Minimum idle speed 1050 RPM

Question 10

Starter Limits

Answer 10

30 Seconds ON, 5 Minutes OFF

30 Seconds ON, 5 Minutes OFF
30 Seconds ON, 30 Minutes OFF

Question 11

Max operating air temperature limits

Answer 11

Sea Level to 25,000 ft = ISA+ 37°C
Above 25,000 ft = ISA+ 31 °C

Question 12

Weight Limits

Baggage Compartment, Ramp & Zero Fuel Weight

Answer 12

Maximum Weight in Baggage Compartment 550 lb

Maximum Zero Fuel Weight 12,500 lb

Maximum Ramp Weight 15,100 lb

Question 13

Weight Limits as limited by T/O Requirements

Answer 13

Maximum Takeoff Weight . = 15,000 lb
or as limited by the following graphs:

• Max T/O Weight to Achieve T/O Climb Requirements
• Max T/O Weight as Limited by Tire Speed
• Takeoff Field Length

For 14 CFR Part 135 Operations:
• Takeoff Flight Path Requirements to 1500 ft AGL
• Service Ceiling-One Engine Inoperative
Maximum Landing Weight = 15,000 lb

Question 14

Cabin Differential Pressure Gauge

Answer 14

Green Arc (Normal Operating Range)

0 to 6.6 psi

Red Arc (Unapproved Operating Range)

6.6 psi to end of scale

Question 15

Pneumatic Pressure Gauge

Answer 15

Green Arc (Normal Operating Range) ..... ....12 to 20 psi
Red Line (Maximum Operating Range) ... ....... ....20 psi

Question 16

Vacuum Gauge - Narrow Green Arc

Answer 16

(Normal from 35,000-15,000 ft) ………2.8 to 4.3 in. Hg

Question 17

Vacuum Gauge - Wide Green Arc

Answer 17

(Normal from 15,000 ft to Sea Level) 4.3 to 5.9 in. Hg

35K marked on face of gauge at 3.0 in. Hg

15K marked on face of gauge at 4.3 in. Hg

Question 18

Flight Load Factor Limits

Answer 18

Flaps Up Flaps Down

3. 1 Positive Gs 2.0 Positive Gs
4. 24 Negative Gs 0.0 Gs

Question 19

Landing Gear Cycle Limits

Answer 19

Landing gear cycles (1 Up-1 Down) are limited to one every 5 minutes

for a total of six (6) cycles,

followed by a 15-minute cool-down period.

Question 20

Icing Limitations

Answer 20

Minimum Ambient Temperature

for Operation of Deicing Boots -40°C

Minimum Airspeed for Sustained Icing Flight… 140 knots

Question 21

Air Conditioning Limitations

Answer 21

The supplemental electric heater must be off for at least 2 minutes prior to and
during engine start.

Do not operate the electric heat with the pedestal floor outlet blocked or the
cockpit door closed.

Question 22

Autopilot Limitations - Height specific

Answer 22

• Autopilot minimum engage height after takeoff is 400 ft AGL.
• Autopilot minimum use height during cruise is 1000 ft AGL.
• Autopilot minimum use height during approach is 79 ft AGL.
• Autopilot minimum use height during steep approach is 160 ft AGL.

Question 23

Airspeed Limitations - Vfe

Answer 23

Approach ………. … 202 KIAS
Full Down ………. . 158 KIAS

Question 24

Airspeed Limitations - Va

Answer 24

Maneuvering Speed (Va) …….184 KIAS

Question 25

Maximum Landing Gear Operating Speed (Vlo)

Answer 25

Extension …………….. 184 KIAS
Retraction .. … ….. .. . 166 KIAS

Question 26

Maximum Landing Gear Extend Speed (Vle)

Answer 26

Maximum Landing Gear Extended Speed (VLE) 184 KIAS

Question 27

Air Minimum Control Speed (VMcAl (Propeller Feathered):

Answer 27

Flaps Up ………….. 94 KIAS
Flaps Approach … 93 KIAS

Question 28

Maximum Operating Speed (Vmo)

Answer 28

Sea Level to 21000 feet = 263 KIAS
21000 to 35000 feet = 263-194 KIAS (0.58 MACH)

Question 29

Propeller Autofeather

Answer 29

The propeller autofeather system must be operable for all flights and must be
armed for takeoff, climb, approach and landing.

Question 30

CAE

Emergency Airspeeds (15,000 lbs) 1-engine Inop

Answer 30

Vxse = 125

Vyse = 125

Enroute Climb = 125

Question 31

CAE

Max demonstrated Wind Components for Coupled Approaches

Answer 31

Crosswind = 32 kts

Tailwind = 14 kts

Question 32

CAE

Aircraft Height, Length Wingspan

Answer 32

H = 14 ‘ 4 “

L = 46 ‘ 8 “

W = 57 1 11 “

Question 33

CAE

A/P Max Coupled INCPT Angle for Back Course

Autopilot Max Coupled INCPT Angle for NAV/LOC

Answer 33

For Back Course = 70 degrees

For NAV/LOC = Less than 90 degrees