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LEAR JET 60 FSI > LR 60 Limitations FSI > Flashcards

LR 60 Limitations FSI Flashcards

1
Q

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

A

10°C / 50°F

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2
Q

Max Ramp Weight

A

23,750 lbs

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3
Q

Max Certified Takeoff Weight

A

23,500 lbs

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4
Q

Max Zero Fuel Weight

A

17,000 lbs

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5
Q

Max Takeoff weight w/ Anti-Skid off or Inop

A

18,500 lbs

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6
Q

Max Landing Weight

A

19,500 lbs

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7
Q

Max Operating Speed - Mmo

A

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

With Mach Trim Inop and autopilot disengaged - M0.77

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8
Q

Max Landing Gear ‘Operating’ Speed - Vlo

A

200kts

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9
Q

Max Landing Gear ‘Extended’ Speed - Vle

A

260kts

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10
Q

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

A

8° - 250kts
20° - 200kts
40° - 165kts

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11
Q

Minimum Control Airspeed - Vmca
Flaps 8°
Flaps 20°

A

Flaps 8° - 120kts

Flaps 20° - 110kts

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12
Q

Minimum Control Speed Ground - Vmcg

A

Rudder boost ON - 95kts

Rudder boost OFF - 116kts

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13
Q 
Operational Limits/Requirements
TAKEOFF/LANDING
-Tailwind Component
-Runway Conditions 
-Fuel Load
A 
Tailwind Component - 10kts
Runway Conditions:
- T/O is limited to 'paved' runways
- Runway water/slush accumulation: 3/4"
Wings Balanced within 200lbs
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14
Q

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

A

Max Pressure Alt. - 51,000 feet

Wings Balanced within 500lbs

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15
Q

Limit Maneuvering Load Factors

  • Flaps up
  • Flaps down
A

Flaps Up +3.0g to -1.0g

Flaps Down +2.0g to 0.0g

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16
Q

Prohibited Maneuvers

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

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

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17
Q

TURN-AROUND LIMITS

A
  • 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
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18
Q

NACELLE HEAT

air

A
  • 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.
19
Q

NACELLE HEAT

ground

A
  • 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
20
Q

AIR DATA SYSTEM

A

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

21
Q

ATTITUDE AND HEADING REFERENCE SYSTEM (AHS)

A

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

22
Q

AUTOPILOT/FLIGHT DIRECTOR

A
  • 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
23
Q

ELECTRONIC FLIGHT INSTRUMENT SYSTEM (EFIS)

A
  • 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
24
Q

FLIGHT MANAGEMENT SYSTEM (FMS)

autopilot coupled VNAV operation altutide

A

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

25
Q 
ENGINE SYS LIMITS
APR or T/O  
-Time limits
-N1%
-Max ITT °C
-N2%
-Oil Pressure 
-Oil Temp
A
  • 5 min
  • 102% N1
  • 785° C
  • 102% N2
  • 36 to 80psi
  • 10° to 135° C
26
Q 
ENGINE SYS LIMITS 
MCT or MCR
-N1% 
-Max ITT °C 
-N2%
-Oil Pressure 
-Oil Temp
A
  • No time limit
  • 102% N1
  • 785° C
  • 102% N2
  • 36 to 80 psi
  • 10° to 135°
27
Q 
ENGINE SYS LIMITS 
Ground Idle
-N2%
-Oil Pressure 
-Oil Temp
A
  • 52% N2
  • 20 to 80 psi
  • 10° to 135° C
28
Q 
ENGINE SYS LIMITS 
Flight Idle 
-N2%
-Oil pressure psi
-Oil Temp
A
  • 65% N2
  • 20 to 80 psi
  • 10° to 135°
29
Q 
ENGINE SYS LIMITS
Starting
-Max ITT° C
-Oil pressure psi
-Oil Temp
A
  • 950° C
  • 20 to 220 psi
  • (-40°C minimum)
30
Q

ENGINE SYNC

A

Must be ‘OFF’ for takeoff, landing and single engine operation

31
Q

EXTERNAL POWER

A

Must be limited to 1,500 amps

(500 amps minimum)

32
Q

GENERATOR LIMITS, for start. Amps

  • Ground ops
  • Flight ops
A 
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
33
Q

STARTER LIMITS

A

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

34
Q

THRUST REVERSERS

A

Below 50 KIAS - Limited to Idle

Above 50 KIAS - From Idle to max

35
Q

CABIN PRESSURIZATION

A
  • For T/O and landings above ‘8,000’ feet, the ‘auto’ pressurization mode must be used.
  • Max diff - 9.8 psi
36
Q

COOLING SYSTEM

Freeon

A

Must be ‘off’ or ‘Manual, full cold’

37
Q

FUEL SYSTEM

A
  • 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
38
Q

HYDRAULIC SYS LIMITS

A

3 min ‘ON’, 20 min ‘OFF’

When SAT below -25° C engines must run for at least ‘3’ min

39
Q

TIRE LIMITS

A
  • Do not exceed 182 kts

- Pressure must be checked within ‘96’ hrs (not flight hours) prior to takeoff

40
Q

TIRE PRESSURES

A

Nose Gear - 104 to 114 psi

Main Gear - 209 to 219 psi

41
Q

SPOILERS

A
  • Max altitude permitted is ‘38,000’ feet
  • Do not extend ‘spoilers’ with ‘flaps’ extended
  • Do not extend spoilers above Vmo/Mmo
42
Q

EPM - AC VOLTS normal

A

110 to 130 Volts

43
Q

EPM - DC VOLTS normal

A

22 to 29.5 Volts

44
Q

EPM - DC AMPERES

A

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

LEAR JET 60 FSI (2 decks)

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