G550 Limitations Flashcards
(158 cards)
1
Q
Minimum Flight Crew
A
Pilot and Copilot
2
Q
Maximum Occupants
A
Total: 22
Passengers: 19
3
Q
When 10-19 Passengers…
A
Must carry additional trained crewmember - trained in emergency e prgressocedures.
4
Q
Passenger Briefing required for…
A
…configuration specific emergency egress procedures.
5
Q
Runway is wet when…
A
… >25% Runway Surface covered by visible dampness or water 1/8in or less.
6
Q
Runway is considered contaminated when…
A
> 25% Runway Surface covered by frost, ice, snow, slush, >1/8in standing water.
7
Q
Maximum Runway Slope for Takeoff/Landing
A
+2% Uphill
-2% Downhill
8
Q
Maximum Tailwind Component for Takeoff/Landing
A
10 Knots
9
Q
Runway Surface Approved
A
Smooth and/or Grooved Hard Surfaced Runway
10
Q
Maximum Approved Airport Pressure Altitude for Takeoff/Landing
A
SN5001-5059 w/o ASC 040: 12,000
SN5060 and on (and w/ ASC 040: 14,500
SN5323 and on w/ HLFE Pax O2 Controller: 15,000
11
Q
Vmo/Mmo
A
SL-8,000: 300KCAS
12,000-27,860: 340KCAS
27,860: 0.850M
32,160-43,500: 0.885M
51,000: .960M
12
Q
Types of Navigation Approved
A
See AFM 01-03-10
13
Q
Minimum Mach w/ SAT -70C to -80C
A
.67M - .87M
14
Q
Use Cold Weather Start and Operation guidance following…
A
…overnight cold soaking -15C or colder.
(02-08-120)
15
Q
Use Hot Weather APU Start guidance following…
A
…heat soaking +35C or warmer.
16
Q
Maximum Operating Altitude
A
51,000
17
Q
Max Altitude w/ Yaw Damper Inoperative
A
45,000
18
Q
Max Altitude w/ Single Air Conditioning Pack Operating:
A
48,000
19
Q
Max Altitude Landing Gear Extension
A
20,000
20
Q
Max Altitude Flaps Extended 39 deg
A
20,000
21
Q
Max Altitude Flaps Extended 10-20 deg
A
25,000
22
Q
Vmca
A
112
23
Q
Vmcl
A
110
24
Q
Vmcg
A
107 - Sea Level
86 - 15,000ft
(decrease approx. 1kt per 1,000ft)
25
Va
206
26
Vfe/Mfe
10 deg - 250/0.6M
20 deg - 220/0.6M
39 deg - 170/0.6M
27
Vlo/Mlo
Normal Operation - 225
Alternate Operation - 175
28
Minimum Holding Speed in Icing Conditions
160
29
Max Yaw Damper Inoperative Speed
Above 10,000 - 260/0.8M
Below 10,000 - 250
30
Minimum Yaw Damper Inoperative Speed
Above 20,000 - 210
Below 20,000 - See Chart - Varies w/ Config
31
Max Speed w/ Both Mach Trim Functions Inoperative or w/ Electric Elevator Trim Inoperative
0.8M
32
TAPS
At or Above 10,000 - 270/0.8M
Below 10,000 - 240
33
Maximum Tire Speed
195
34
Maximum Emergency Stabilizer Trim Speed w/ Autopilot Engaged and a Jammed Elevator
270/0.8M
35
Load Limits
Flaps Up: -1 to 2.5 G all weights up to MTOW
Flaps 10-20: 0 to 2.0 G all weights up to MTOW
Flaps 39: All weights up to MLW - 0 to 2.0 G
Flaps 39: All weights above MLW - 0 to 1.5 G
36
Max Takeoff Weight (FAA)
91,000
37
Max Takeoff Weight restricted by...
1. Climb Performance
2. Brake Engergy
3. Tire Speed
4. Ambient Temperature
5. Field Length
38
Max Ramp Weight (FAA)
91,400
39
Max Zero Fuel Weight (FAA)
54,500
40
Max Landing Weight (FAA)
75,300
41
Max Landing Weight restricted by...
1. Climb Requirements
42
If Zero Fuel CG is within limits...
...Fueled CG will be in limits for all fuel loads.
43
Maximum Fuel Imbalance for Takeoff
1000
44
Maximum Fuel Imbalance in Flight
2000 (start fuel balancing >1000)
45
When balancing fuel through crossflow valve, ensure...
1. Boosted fuel pressure always available to engines
2. Fuel tank temperature above 0C before turning BP OFF
46
Engine will only run on suction feed...
BELOW 20,000
47
Maximum Eye to Wheel Height
15.6 FT
48
Hydraulic Limitations
See OM, Ch 4 Handling and Servicing Procedures
49
APU Fuel Grades and Temperatures
See OM, Ch 4 Handling and Servicing Procedures
50
Approved Fuels
See Figure
51
Engine and APU Oil Grades
See OM, Ch 4 Handling and Servicing Procedures
52
Maximum Cabin Pressure Differential
Flight - 10.48
Taxi/Takeoff/Landing - 0.3
53
Internal Baggage Door shall remain closed above...
40,000
*Allowed for 5 minutes (limited to 45,000 if operating on single ECS pack)
54
Mach Trim must be ON for...
...All Flight Operations except as provided in Mach Trim Failure (03-02-40)
55
Mmo w/ Mach Trim Inoperative
0.80M
56
Single Engine Auto Pilot Go Around
Not Approved
57
Autopilot Minimum Engage Height
200 AGL
58
Autopilot Minimum Disengage Height
ILS or LPV - 60 AGL
All Other Operations - 50 below DA/MDA
59
Autopilot Maximum Demonstrated Altitude Loss for Coupled Go-Around
60 ft
60
Use of Auto-throttle prohibited for...
Single Engine Coupled Approaches
61
Do Not Use HF Radios while...
1. In Hangar
2. Refueling or Defueling
3. Ensure all personnel clear of vertical tail prior to transmitting
62
SATCOM systems approved for AC20-150B SATVOICE?
NO
63
When HMG in Operation, Speed brakes...
...may be used with slow operation (3sec to full-range)
64
DO NOT Operate HMG when...
Normal AC Power available, EXCEPT for ESS DC Bus Failure
65
Dispatch w/ Stall Barrier INOP Allowed?
1 Inoperative Allowed IAW MEL
66
Stall Barrier must be ON...
All Operations except for selected OFF for malfuntion
67
Speed Brakes are NOT approved for...
Flaps 39 deg
68
Takeoff with Auto Ground Spoilers INOP Provided...
1. Anti-Skid Operative
2. Flaps 20
3. Cowl/Wing Anti-Ice OFF
69
GND SPLR must be OFF for
Touch and Go Landings (use Manual Spoiler Ldg Distance)
70
Usable Fuel Capacity
Total: 41,300LB / 6,118 Gal
Wing: 20,650LB / 3059 Gal
(Can be above 41,300 as long as MTOW observed)
71
Boost Pumps must be ON...
...for All Phases of Flight unless fuel balancing
72
Do not use Boost Pumps to balance fuel...
...when Fuel Tank Temperature 0C or Below
73
Maximum Fuel Tank Temperature
+54C (Fuel Tank Temperature CAS)
74
Minimum Fuel Temperature Caution
-35C to -36C
75
Minimum Fuel Temperature Warning
-37C or Below
76
Fuel Temperature -30C and <5000LB Remaining...
1. Descend to SAT of -60C or warmer
2. Minimum Speed - 0.80M
77
Hydraulic Reservoir Capacity
Left - 4.8 gallons
Right - 1.6 gallons
78
L/R Hydraulic System Accumulator Precharge Pressure
1200 psi at 70F (25psi for ea. 10F)
79
A visual AND tactile check of wing leading edge and upper surface must be performed to ensure the wing is free from frost, ice, snow, or sluch when...
...OAT less than +42F or if it cannot be determined Fuel Temp >32F, and
1. Visible Moisture present, OR
2. Water present on Wing
3. Temp/DP Spread 5F or less.
4. Conditions conducive to Frost
80
For prolonged ground operation in icing conditions, Wing Anti-Ice should remain...
OFF
81
Wing Anti Ice Required in Flight when.
1. Icing Conditions Imminent, OR
2. Immediately on detection of ic on WINGS, WINGLETS or WINDSHIELD EDGES
82
Cowl Anti Icing required for Taxi and Takeoff when SAT 10C or below and...
1. Visible Moisture, OR
2. Precipitation, OR
3. Wet Runway
83
On ground in less than +1C in icing conditions...
Operated Engines at 40% LP
1. 10 sec just prior to Takeoff
2. Intervals of 60min or less.
84
Use of Cowl Anti Ice In Flight required in visible moisture or precipitation when SAT...
See Limitations: Temp Range for Cowl Anti Icing Table
85
Use of Flaps in Icing Conditions
Takeoff, Approach and Landing ONLY
86
Holding in Icing Conditions
Limited to Flaps 0 deg ONLY
87
Electronic Checklist conflict w/ AFM
Use AFM
88
DU Control Switches operative...
ONLY on Ground.
(DO NOT move DU Control Switches in Flight)
89
Display of Video unrelated to airplane operation
Prohibited (Includes and feed from Cabin Entertainment System)
90
USB Ports in Cockpit
1. Used only to transfer XM weather data to EFB
2. Should interfere w/ Safe Operation
3. Must be STOWED for Taxi, TO and LDG (Emergency Egress)
91
Takeoff with Anti Skid INOPERATIVE
1. Dry Runway
2. Ground Spoilers OPERATIVE
3. Flaps 20 deg used
4. Cowl/Wing Anti Ice NOT USED
92
For flights North of 73N and South of 60S
Heading must be in TURE
93
IRS in-air alignment AIM
Allowed (see Limitations)
94
DO NOT Operate Radar on ground within...
1. 300ft of other Fueling operations
2. 49ft of Ground Personnel w/ 24" antenna
95
FMS approved for
1. RNAV (GPS) (GNSS) or RNP APCH
2. RNAV (RNP) or RNP AR APCH
3. GPS or GNSS
4. VOR/DME RNAV
5. VOR/DME*
6. VOR*
7. TACAN*
8. NDB*
*Only if Country's AIP approves FMS guidance*
96
LPV Minima
Approved if equipped (ASC084B or later) when LPV minima selected (default)
97
LPV Unavailable CAS Message
Use LNAV minima or Go Around
98
Use of TOLD Software ID V1.0 and subsequent...
Permitted (Must be checked for Reasonableness)
99
TCAS when Single Engine
Select TA Mode
100
Crew and Passenger Oxygen Masks not approved for use...
...above 40,000
101
Passenger Oxygen Masks will not provide sufficient oxygen for...
prolonged operations above 34,000
102
Prolonged Passenger Mask operation not recommended above...
25,000
103
APU can be used to supply pressurization airflow during Bleeds OFF takeoff up to...
1500 AGL
104
APU may be used for starter assisted main engine starts?
Yes...Below 30,000
105
APU Maximum Operational Altitude
45,000
106
APU Maximum EGT
Start: 1050
Running: 732
107
APU Maximum Rotor Speed
106%
108
APU Starter, when power by Aircraft Batteries limited to...
3 Start Attempts, followed by 1 hour cool down period
109
APU Starter, when powered by External DC Power limited to...
3 Start Attempts, with 15 min cool down between attempts to protect aircraft wiring. followed by1 hour cool down.
110
Successful Consecutive APU Starts limited to...
6 at 10 minute intervals
111
See Cold Weather Start and Operation for APU start following...
...overnight cold soak of -15C or colder
112
APU Alternator Output
40kVA - SL to 45,000
113
Maximum APU Start Altitude
39,000 (May start up to 43,000)
114
APU Air for Engine Start not available above...
30,000
115
Interior Doors
Must be Fully Open for Taxi, Takeoff and Landing
1. Main Entry Door Curtain
2. Acoustic Door System
3. All Mid-Cabin Doors
116
Max Start TGT
700 C (Momentary)
117
Max Airstart (Relight) TGT
850 C (Momentary)
118
Max Takeoff TGT
900 C (5 Minutes)
119
Max Continuous TGT
860
120
Max Overtemp TGT
905 (20 Seconds)
121
Max Takeoff LP%
101.1% (5 Minutes)
122
Max Continous LP%
101.0%
123
Max Overspeed LP%
101.5% (20 Seconds)
124
Max Reverse Thrust LP%
70% (30 Seconds)
125
Max Takeoff HP%
99.6% (5 Minutes)
126
Max Continuous HP%
98.9%`
127
Maximum Overspeed HP%
99.8%
128
Max TGT Prior to Start
150 C
129
Static Operation of Thrust Reversers limited to...
30% LP
130
Max Reverse Minimum Speed
60 kt
131
Maximum Crosswind for Engine Start
30
132
Maximum Tailwind for Engine Start
20
133
For Engine Starts >10kt Tailwind
Before introducing Fuel
1. Allow Max Cranking RPM
2. Verify Positve LP
134
Preferred method of Engine Airstart is...
Automatic
135
Maximum Airstart Envelope Altitude
25,000
136
Windmilling Airstart Speed Range
250 - 340
137
Takeoff in Alternate Control LP Mode
Prohibited
138
For >20 Crosswind Takeoffs Limit Fan Speed to...
66% until 20 Kts, then Slam acceleration to Takeoff Power
(Add 600ft to TOFL)
139
Stabilized Engine LP% on Ground prohibited between...
66% - 80% LP
(Limited to 10 seconds)
140
Minimum Engine Fuel Temperature
-40 C
141
Maximum Engine Fuel Temperature
+140 C
142
Maximum Transient Engine Fuel Temperature
+165 C (15 Minutes)
143
Maximum Fuel Tank Temperature
+54 C
144
Continuous Ignition
No Limit
145
Reverse Thrust must be IDLE by...
60
146
Idle Reverse Thrust for Taxi
No Time Limit
147
TRs should be deployed and stowed at least...
Once every 100 hr
148
Reverse Thrust used to bring airplane to stop
Only in Emergency - Record in Logbook
149
Use of TRs to... ...not approved.
Power Back the Airplane
150
Dispatch w/ TRs Inoperative and Wet Runway
Reduce Available Runway by 1400 ft
151
Minimum Oil Temp for Start
-30 C
152
Minimum Oil Temp for Takeoff
+20 C
153
Maximum Oil Temp
160 C
154
Shutdown Oil Pressure
<25 psi
155
Minimum Engine Oil Pressure <72.3%
Takeoff - 35
To Complete Flight - 25
156
Minimum Engine Oil Pressure >90%
Takeoff - 45
To Complete Flight - 35
157
Engine Starter Duty Cycle Limit
3 Minutes w/ 15 Seconds between cycles, wait 15 Minutes after 3 cycles
158
