LR 60 Limitations FSI

Question 1

Icing conditions exist when the OAT on the ground and for takeoff is ___°C ___°F

Answer 1

10°C / 50°F

Question 2

Max Ramp Weight

Answer 2

23,750 lbs

Question 3

Max Certified Takeoff Weight

Answer 3

23,500 lbs

Question 4

Max Zero Fuel Weight

Answer 4

17,000 lbs

Question 5

Max Takeoff weight w/ Anti-Skid off or Inop

Answer 5

18,500 lbs

Question 6

Max Landing Weight

Answer 6

19,500 lbs

Question 7

Max Operating Speed - Mmo

Answer 7

26,750 to 37,000 feet - M0.81

With Mach Trim Inop and autopilot disengaged - M0.77

Question 8

Max Landing Gear ‘Operating’ Speed - Vlo

Answer 8

200kts

Question 9

Max Landing Gear ‘Extended’ Speed - Vle

Answer 9

260kts

Question 10

Max Flap Extended Speed - Vfe
Flaps 8°
Flaps 20°
Flaps 40°

Answer 10

8° - 250kts
20° - 200kts
40° - 165kts

Question 11

Minimum Control Airspeed - Vmca
Flaps 8°
Flaps 20°

Answer 11

Flaps 8° - 120kts

Flaps 20° - 110kts

Question 12

Minimum Control Speed Ground - Vmcg

Answer 12

Rudder boost ON - 95kts

Rudder boost OFF - 116kts

Question 13

Operational Limits/Requirements
TAKEOFF/LANDING
-Tailwind Component
-Runway Conditions 
-Fuel Load

Answer 13

Tailwind Component - 10kts
Runway Conditions:
- T/O is limited to 'paved' runways
- Runway water/slush accumulation: 3/4"
Wings Balanced within 200lbs

Question 14

Operational Limits/Requirements
EN ROUTE
-Max pressure Altitude
-Fuel Load

Answer 14

Max Pressure Alt. - 51,000 feet

Wings Balanced within 500lbs

Question 15

Limit Maneuvering Load Factors

• Flaps up
• Flaps down

Answer 15

Flaps Up +3.0g to -1.0g

Flaps Down +2.0g to 0.0g

Question 16

Prohibited Maneuvers

Answer 16

• No ‘aerobatic’ maneuvers, including ‘spins’ are approved.

- Intentional stalls are prohibited above: 18,000ft with flaps and/or landing gear extended

Question 17

TURN-AROUND LIMITS

Answer 17

• Must be parked for ‘20’ minutes before the next takeoff attempt can be made
• After waiting period, a visual inspection of ‘tires’, ‘wheels’, and brakes must be made

Question 18

NACELLE HEAT

air

Answer 18

• Must be ‘ON’ during decent into visible moisture even if SAT is below -40°C
• To reduce possible engine damage, select ON at least ‘2’ min prior to entering icing conditions.

Question 19

NACELLE HEAT

ground

Answer 19

• No longer than ‘5’ sec when the engine is not running
• Do not operate for more than ‘30’ sec when SAT is above 15°C
• Except for T/O, do not operate nac heat if engine RPM is greater than ‘65%’ N1

Question 20

AIR DATA SYSTEM

Answer 20

Both air data systems must be ‘on’ and the onside system selected

Question 21

ATTITUDE AND HEADING REFERENCE SYSTEM (AHS)

Answer 21

The onside AHS must be selected and comparator annunciators ‘extinguished’ for T/O

Question 22

AUTOPILOT/FLIGHT DIRECTOR

Answer 22

• Operation of the autopilot with red ‘Trim’ fail light illuminated is prohibited
• Don’t intentionally ‘override’ the autopilot
  Minimum alt for use is:
• Approach configuration: 200 ft
• Enroute configuration: 1,000 ft

Question 23

ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS)

Answer 23

• A minimum of ‘3’ large flight displays must be operational for T/O
• Each outboard PFD must work
• At least one inboard display must work
• The stdby attitude indicator must work

Question 24

FLIGHT MANAGEMENT SYSTEM (FMS)

autopilot coupled VNAV operation altutide

Answer 24

Minimum altitude for VNAV is ‘400’ feet or MDA, whichever is higher

Question 25

``` ENGINE SYS LIMITS APR or T/O -Time limits -N1% -Max ITT °C -N2% -Oil Pressure -Oil Temp ```

Answer 25

- 5 min - 102% N1 - 785° C - 102% N2 - 36 to 80psi - 10° to 135° C

Question 26

``` ENGINE SYS LIMITS MCT or MCR -N1% -Max ITT °C -N2% -Oil Pressure -Oil Temp ```

Answer 26

- No time limit - 102% N1 - 785° C - 102% N2 - 36 to 80 psi - 10° to 135°

Question 27

``` ENGINE SYS LIMITS Ground Idle -N2% -Oil Pressure -Oil Temp ```

Answer 27

- 52% N2 - 20 to 80 psi - 10° to 135° C

Question 28

``` ENGINE SYS LIMITS Flight Idle -N2% -Oil pressure psi -Oil Temp ```

Answer 28

- 65% N2 - 20 to 80 psi - 10° to 135°

Question 29

``` ENGINE SYS LIMITS Starting -Max ITT° C -Oil pressure psi -Oil Temp ```

Answer 29

- 950° C - 20 to 220 psi - (-40°C minimum)

Question 30

ENGINE SYNC

Answer 30

Must be 'OFF' for takeoff, landing and single engine operation

Question 31

EXTERNAL POWER

Answer 31

Must be limited to 1,500 amps | (500 amps minimum)

Question 32

GENERATOR LIMITS, for start. Amps - Ground ops - Flight ops

Answer 32

``` Ground Ops - Continuous 500 amps Flight Ops - Up to 31,000: 400 amps - From 31,000 to 46,000: 325 amps - From 46,000 to 51,000: 300 amps ```

Question 33

STARTER LIMITS

Answer 33

1st attempt - 3 min 2nd attempt - 15 min 3rd attempt - 30 min

Question 34

THRUST REVERSERS

Answer 34

Below 50 KIAS - Limited to Idle | Above 50 KIAS - From Idle to max

Question 35

CABIN PRESSURIZATION

Answer 35

- For T/O and landings above '8,000' feet, the 'auto' pressurization mode must be used. - Max diff - 9.8 psi

Question 36

COOLING SYSTEM | Freeon

Answer 36

Must be 'off' or 'Manual, full cold'

Question 37

FUEL SYSTEM

Answer 37

- JP-5, JP-8, JET-A, JET-A1 are allowed - Fuel Mixing is allowed - Fuel additives such as Anti-Ice or Biocide are not required

Question 38

HYDRAULIC SYS LIMITS

Answer 38

3 min 'ON', 20 min 'OFF' | When SAT below -25° C engines must run for at least '3' min

Question 39

TIRE LIMITS

Answer 39

- Do not exceed 182 kts | - Pressure must be checked within '96' hrs (not flight hours) prior to takeoff

Question 40

TIRE PRESSURES

Answer 40

Nose Gear - 104 to 114 psi | Main Gear - 209 to 219 psi

Question 41

SPOILERS

Answer 41

- Max altitude permitted is '38,000' feet - Do not extend 'spoilers' with 'flaps' extended - Do not extend spoilers above Vmo/Mmo

Question 42

EPM - AC VOLTS normal

Answer 42

110 to 130 Volts

Question 43

EPM - DC VOLTS normal

Answer 43

22 to 29.5 Volts

Question 44

EPM - DC AMPERES

Answer 44

Normal - 0 to 325 Amber - 326 to 400 Red - 400 or above