LJ75 Phase IIIA Limitations Flashcards
1
Q
Max Ramp Weight (MRW)
A
21,750 LB
2
Q
Max Takeoff Weight (MTOW)
A
21,500 LB
3
Q
Max Landing Weight (MLW)
A
19,200 LB
4
Q
Max Zero Fuel Weight (MZFW)
A
16,(5)00 LB
5
Q
Minimum Flight Weight (MFW)
A
14,000 LB
6
Q
CG
A
3.5% (16,260) to 19.5% (21,750) fwd / 28% aft
7
Q
Vmo
A
330
8
Q
Mmo
A
Mach .81
9
Q
Mmo (Mach trim inoperative and AP disengaged)
- Above FL420
A
Mach 0.78 (marked)
10
Q
Mmo (Mach trim inoperative and AP disengaged)
- FL234 - FL420
A
Mach .76 to .78 (Marked)
11
Q
Standby Vmo / Mmo
- Below FL220
A
331 KIAS
12
Q
Standby Vmo / Mmo
- Above FL220
A
330 KIAS / M.81
(AP & Mach Trim Off lims not shown)
13
Q
Vlo / Vle
A
200 / 260
14
Q
VFE (Flaps 8°)
A
250
15
Q
VFE (Flaps 20°)
A
200
16
Q
VFE (Flaps 40°)
A
150
17
Q
V MCG
A
105 (APR On or Off)
18
Q
V MCA
A
107 (8°) / 107 (20°)
19
Q
V MCL
A
110 (8°) / 102 (40°)
20
Q
Max Field Elevation for Takeoff
A
14,000’
21
Q
Max Tailwind
A
10k’ and below - 10 kts
12k’ - 5 kts
14k’ - 0 kts
22
Q
Takeoff and landings on ________ Surfaces Only
A
Paved
23
Q
Standing Water Limitation
A
3/4”
24
Q
HI FLOW Must be ____ for takeoff
A
OFF
25
Max Fuel imbalance for takeoff
200 lbs
26
Rudder Boost must be ___ for takeoff
ON
27
APR must be _______ for takeoff
armed per chart
28
Engine Sync must be ________ for takeoff
OFF
29
ADC & AHRS must be ________ for takeoff
Onside
30
All displays must be ________ for takeoff
Operational
31
Max Altitude
51,000'
32
Max landing elevation
14,000'
33
Max tailwind when landing up to 14,000'
10 kts
34
The aircraft must be _________ for landing
Unpressurized
35
Max fuel imbalance for landing
200 lbs
36
Min turn-around time
15 minutes between touchdown and TO thrust
37
Does the min turn-around time apply to touch & go landings?
No
38
Load Factors (Flaps UP)
-1 - 2.9 Gs
39
Load Factors (Flaps Down)
0 - 2 Gs
40
Prohibited Maneuvers
- Aerobatics
- Intentional stalls above 18,000'
41
Flaps and Gear must not be extended above...
18,000'
42
Seat belts & shoulder harness must be worn during
Takeoff and Landing
43
FWD Partition Door must be open for...
Taxi, Takeoff, and Landing (if installed)
44
Aircraft must be warmed to ______ before start
> -23°c
45
The aircraft is considered cold soaked on the ground at ________ or less
-23°c
46
The cabin temp must be ______ or warmer prior to takeoff.
-15°c
47
ADC must be ________ for takeoff
onside
48
AHRS must be ________ for takeoff
onside, prohibited > N, S Latitudes
49
AP & FD must be _____ for takeoff
OFF
50
It is permissible to overpower the AP.
False
51
AP min use height for climb, en route, descent
1,000' AGL
52
AP min use height on approach
180' AGL
53
Max glide slope angle for CAT I approaches
3.77°
54
Max/min Delta P
+9.9 psid to -.5 psid
55
Do not land with the cabin _________.
pressurized
56
When must HI FLOW be OFF?
- Takeoff power selected
- Landing
- Anti-Ice operations
- Flight above 30,000'
57
The ______ /_______ must be onboard (Garmin)
Approved Cockpit Reference Guide
Pilot's Guide
58
All displays must be __________ for takeoff
operational
59
Prohibited Garmin Features
- Airspace alerting
- system clock local time
60
Garmin Advisory (SA) only features
- NEXRAD Wx
- E-Checklist
- E-docs
- Moving Map
- Synthetic Vision
61
Airspace displayed on map is _________.
Allowed, but NO alerting
62
Do not ______ or _______ the DEFAULT crew profile.
change or modify
63
How many GTCs can a FMS flight plan be edited at one time?
One
64
The use of non-WGS84 waypoints is ________.
prohibited
65
Planned / flown GPS/SBAS IAPs must be __________________.
in the FMS database
66
Engine sync must be OFF for...
- Takeoff
- Landing
- Single Engine Ops
67
Max external power amps
1500 A
68
Max generator amps
300 continuous, higher transients allowed
69
The Garmin G5000 system clock must be set to ____ time.
UTC
70
The use of FMS TOLD is limited to takeoff and landing below _______ feet.
10,000
71
The obstacle database includes obstacles ____ ft and higher and the coverage area includes _____ and most of ___________.
200; US; Western Europe
72
The use of weather radar ________ mode is prohibited.
Altitude compensated Tilt
73
Crew and passenger oxygen masks are not approved for use above _______ cabin altitude.
40,000'
74
Prolonged operation of passenger masks above ______ cabin altitude is not recommended.
25,000'
75
Hats and earmuff type headsets must be _______ prior to donning crew oxygen masks.
removed
76
Rudder boost must be ___ for takeoff.
ON
77
Do not ______ spoilers with flaps extended while _______, except as specified in __________.
extend; in-flight; EMERGENCY / ABNORMAL PROCEDURES
78
Autospoilers must _______ for takeoff and landing.
ARMED
79
Do not arm autospoilers for
training maneuvers where engine failure will be simulated above V1 speed or touch and go landings.
80
Engine starter attempts; wait times
1; 1 minute
2; 2 minutes
3; 30 minutes
81
Thrust Reverser operation is limited to
ground operations on paved surfaces
82
Do not use the thrust reversers to _______ the aircraft.
back up
83
The T/R circuit breakers may only be pulled in flight if...
directed by checklist procedure
84
Thrust reversers must not be used for _______ landings.
touch and go
85
Thrust reversers are limited to ______ when the engines are operating in MAN mode.
idle reverse
86
Max tire speed
165 kts ground speed
87
Engine computers must be _____ at all times unless _______.
ON; directed by checklist procedure
88
Engine type
Honeywell TFE731-40BR-1B
89
Engine thrust at sea level
3,850 lbs
90
Engine preheat is recommended below ______.
-28°c
91
Allow oil temperature to increase above _____ prior to increasing thrust above idle.
30°c
92
Takeoff and APR time limit (two engine ops)
5 minutes
93
Takeoff and APR time limit (single engine ops)
10 minutes
94
Max engine thrust with oil temp < 30°c
IDLE
95
Approved fuels
JP-5 / JP-8 / JetA & JetA-1 / DEF STAN 91-91 Jet A1 & CAN F-34 (consult AFM)
96
SPPR refueling pressure limit
55 psig max
97
SPPR defueling is limited to ______ psig
-10
98
Hydraulic fluid type
MIL-PRF-5606
99
The APU is limited to ______ operations only.
ground
100
Max pressure altitude for APU ops
10,000'
101
The APU must be ________ prior to takeoff.
shut down
102
APU operation during gravity fill refueling is ________.
PROHIBITED
103
APU operation during fluid de-icing / anti-icing is ___________.
PROHIBITED
104
Takeoff is ____________with amber APU FAIL CAS displayed.
PROHIBITED
105
If the APU automatically shuts down due to an APU failure, a _________________ must be conducted prior to the flight.
visual inspection
106
APU start attempts; wait times.
1; 1 minute
2; 2 minutes
3; 15 minutes
107
APU generator amp limits
300 Amps continuous; higher transient allowed
