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Icing conditions exist when OAT on ground & for takeoff is __°C (__°F) or below, or SAT in flight is __°C (__°F) to -__°C (__°F), and visible moisture in any form is present.
- 10°C (50°F)
- 10°C (50°F)
- -40°C (-40°F)
-
LR45 Max Ramp Weight
21,750 lbs
-
LR45 Max Certified Takeoff Weight
21,500 lbs
-
LR45 Minimum Flight Weight
14,000 lbs
-
LR45 Max Zero Fuel Weight
16,500 lbs
-
LR45 Max Certified Landing Weight
19,200 lbs
-
LR40 Max Ramp Weight
21,250 lbs
-
LR40 Max Certified Takeoff Weight
21,000 lbs
-
LR40 Minimum Flight Weight
13,500 lbs
-
LR40 Max Zero Fuel Weight
16,000 lbs
-
LR40 Max Certified Landing Weight
19,200 lbs
-
-
MMO Primary Display
- with Mach Trim Operative - .81MI
- with Mach Trim Inop & A/P engaged - .81MI
- with Mach Trim Inop & A/P disengaged
- - 23,400 to 42,000 feet - .76-.78 MI - Above 42,000 feet - .78 MI
-
VMO Standby Instruments
325 KIAS
-
MMO Standby Instruments
.75 MI
-
-
-
VFE
- Flaps 8°......250 KIAS
- Flaps 20°....200 KIAS
- Flaps 40°....150 KIAS
-
Turbulent Penetration
Lowest of .75 M or 230
-
Vmcg
- Rudder Boost On, APR On.....102 KIAS
- Rudder Boost On, APR Off....100 KIAS
-
Max Takeoff Pressure Altitude
14,000 feet
-
Max Takeoff Tailwind Component
- Aircraft not modified by SB 45-72-1...10 kts
- Aircraft modified by SB 45-72-1:
- - 12,000 feet and below...10 kts
- - Above 12,000 feet.........0 kts
-
Max En Route Pressure Altitude
51,000 feet
-
Max En Route Fuel Load Imbalance
- 45-002 thru 45-258 and 45-260 not modified by SB 45-28-8...Wings balanced w/in 500 lbs
- 45-259, 45-261 thru 45-200 and prior modified by SB 45-28-8...Wings balanced w/in 200 lbs
-
Max Landing Pressure Altitude
14,000 feet
-
Max Landing Tailwind Component
10 kts
-
Runway Conditions
- Landing is limited to paved runways
- Runway Water...3/4 inch (19mm)
-
Landing Pressurization
Cabin not pressurized
-
Max Fuel Load Imbalance for Landing
Wings balanced within 200 lbs
-
EICAS Landing Requirements
SUMRY or FLT page
-
A minimum of __ minutes must elapse between landing touchdown and selection of takeoff thrust for next takeoff. This does not prohibit touch-and-go landings.
15 minutes
-
EICAS or MFD __ or __ page must be selected for takeoff and landing.
SUMRY or FLT
-
Do not extend flaps above __ feet.
18,000 feet
-
Do not extend gear above __ feet.
18,000 feet
-
No __ maneuvers, including __ are approved. Intentional stalls are prohibited above __ feet.
- Aerobatic
- Spins
- 18,000 feet
-
Autopilot must be __ for takeoff and landing.
Off
-
Do not intentionally __ the autopilot
Overpower
-
Autopilot Minimum Use Height:
- Climb, En Route or Descent __ feet AGL
- Approach __ feet AGL
- Climb, En Route or Descent...500 feet AGL
- Approach............................200 feet AGL
-
Autopilot and Flight Director are approved for __ approaches.
Cat 1
-
Starter cooling periods between consecutive uses:
- After Start Attempt 1; 1 Minute
- After Start Attempt 2; 2 Minutes
- After Start Attempt 3; 30 Minutes
-
-
-
-
-
-
Tire Limiting Speed (Ground Speed)... __ kts
165 kts
-
Do not takeoff or land with wing fuel imbalance greater than __ lbs.
200 lbs
-
APU Generator Limits
Continuous- __ amps
300 amps
-
Fuels approved for the main aircraft engines are also approved for the __
APU
-
Delta P Pressurization Limits..... __
+9.9 psid to -0.5 psid
-
Do not __ with the cabin pressurized.
Land
-
Operating the APU during __ refueling is prohibited.
Gravity Fill
-
Operating the APU during fluid de-icing/anti-icing is __ .
Prohibited
-
Do not takeoff with an -APU FAIL- amber CAS illuminated. In the event the APU automatically shuts down due to and APU failure, a visual inspection of the unit must be conducted prior to __ .
Flight
-
HI FLOW must be __ with takeoff power selected , or for landing, anti-icing operations and flight above 30,000 feet.
Off
-
ENG Sync must be __ for takeoff, landing and single-engine operation.
Off
-
The max amperage from an external power source must be limited to __ amps.
1,500 amps
-
Generator output is limited as follows:
-- Continuous - __ amps
-- Transient - Higher transient loads for cross-starts and battery charging are __ .
-
Crew and pax O2 masks are not approved for use above __ feet cabin altitude. Prolonged operation of pax O2 masks above __ feet cabin altitude is not recommended.
-
Rudder boost must be __ for takeoff.
On
-
Do not extend spoilers with flaps __ while airborne, except as specified in EMERGENCY and/or ABNORMAL PROCEDURES.
Extended
-
Autospoilers must be __ for takeoff and landing, except do not __ autospoilers for training maneuvers where engine failure will be simulated above V1 speed or for touch-and-go landings.
-
__ __ use Thrust Reversers for backing up aircraft.
Do not
-
TR circuit breaker must __ be intentionally pulled in flight, except as specified in QRH.
Not
-
Thrust Reverser must not be used for __ __ __ landings.
touch-and-go
-
Max reverse thrust usable at speeds down to __ KIAS.
40 KIAS
-
Thrust Reversers limited to __ when in MANual mode.
Idle
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