1
Q
Wingspan, Length and Height?
A
87’ 1” x 91’ 2” x 25’ 6”
(88 x 92 x 26 approx)
2
Q
Minimum Taxi Strip for 180 degree turn?
A
Tiller: 57’ (Actual 56.4’)
Rudder: 125’ (Actual 122.1’)
3
Q
Max Ramp Weight?
A
80,000 lbs
4
Q
Max Takeoff Weight?
A
79,600 lbs
(74,900 lbs with ASC005 Placard Installed)
5
Q
Max Landing Weight?
A
64,350 lbs
6
Q
Max Zero Fuel Weight?
A
52,100 lbs
7
Q
Max Baggage Compartment Weight?
A
2,250 lbs
(90 lbs per square foot)
8
Q
Max Fuel Imbalance?
- Takeoff
- In Flight
A
- 1000 lbs
- 2000 lbs
9
Q
Useable Fuel?
A
30,250 lbs
4,515 US Gallons
10
Q
VTurb:
>10,000’
<10,000’
A
- 270 KCAS / .85 M
- 240 KCAS
11
Q
Flap Speeds:
- 10
- 20
- 39
A
- 250 KCAS
- 220 KCAS
- 180 KCAS
12
Q
Gear Speeds:
- VLo
- VLe
- VEmer
A
- 225 KCAS
- 250 KCAS
- 175 KCAS (Max speed with gear extended via Emer is 225 KCAS)
13
Q
VMCA:
- Flaps 10
- Flaps 20
- Flaps 39
A
- 120 KCAS
- 112 KCAS
- 109 KCAS
14
Q
VMCG:
- Flaps 10
- Flaps 20
A
111 KCAS
15
Q
Tire Speed Limit?
A
195 KTS
16
Q
Max Speed:
- Degraded CLAW Mode
- Flight Control Failure (other than tail surfaces)
A
285 KCAS / 0.90 M
17
Q
VAppr minimum:
A
VRef + 1/2 Steady State + Full Gust (up to 20kts)
(Minimum VRef + 5)
18
Q
Thrust Reversers:
- Reverse Idle Before?
- Minimum for Dual Reversers?
A
- 60 KCAS
- 10 KTs Ground Speed
19
Q
Max Operating Altitude?
A
51,000’
20
Q
Max Single Pack Altitude?
A
48,000’
21
Q
Max Baggage Door Access Altitude?
A
45,000’
22
Q
Max Altitude WAI ON with Single Bleed?
A
32,000’
23
Q
Max Altitude with:
- Rudder Jammed
- Yaw Damper Failed
A
35,000’
24
Q
Max Altitude with Flaps 10 / 20?
A
25,000’
25
Max Altitude with Flaps 39 / Gear Down?
20,000'
26
Max Landing Field Elevation?
15,000'
27
Autopilot Minimum Engage Height (AGL)?
200'
28
Autopilot Minimum Disengage Height (AGL)?
- ILS/LPV
- Other
- 90'
- 200'
(Min Disengage Height on Partial Flap ILS/LPV is 130')
29
Autopilot Max Coupled Go Around Loss?
50'
30
APU Altitudes:
- Guaranteed Start
- Max Operating Altitude
- Assisted Airstart
- 37,000'
- 45,000'
- 30,000'
31
Starting aircraft prohibited after extended exposure to temps below:
-40 C (aircraft may be operated down to -50°C provided it does not shut down and cold soak below -40°C)
32
Cowl and WAI On:
- Ground
- Flight
- -40 C < SAT < 10 C + Visible Moisture
- -40 C < TAT < 10 C + Visible Moisture
33
Minimum Engine Fuel Temp for Takeoff?
+9 C
34
Minimum Oil Temp to Exceed Idle Thrust?
+10 C (must be above 9°C)
35
Takeoff with WAI?
- Preheat 4 - 20 Minutes Prior to Takeoff
- Verify Heated to 130F +/- 10
36
Ice Shedding - Ground
2 Seconds at 60% N1, Every 10 Minutes.
The first engine acceleration should be done as soon as practical during taxi, not more than 10 minutes.
37
Ice Shedding, Flight
Automatic (Manual not recommended)
38
Ground Operations in Freezing Fog
> -9 C: Max of 60 Minutes + CAI On
< -9 C: Max of 30 Minutes + CAI On
39
Tactile Icing Check
OAT < 10 C + Visible Moisture
OR
Wing Fuel Temp < 0 C + Moisture
40
Flaps or Gear in Icing Conditions
Restricted to Takeoff, Approach and Landing only
41
Max Tailwind - T/O and Landing
10 KTS
42
Max Tailwind - Flaps 10 or less
0 KTS
43
- Max Landing Crosswind
- Max Static T/O Crosswind
- (Max Demonstrated 33 KTS)
- Above 30 KTS reference high crosswind takeoff procedure
44
Engine Start Wind Limits?
XW: 40 KTS
TW: 25 KTS
45
Engine Run (>30% N1) Wind Limits?
XW: 25 KTS
TW: 20 KTS
46
Taxi (<30% N1) Engine Wind Limits?
XW: 40 KTS
TW: 40 KTS
47
Static Takeoff Engine Wind Limits?
XW: 30 KTS
TW: 10 KTS
48
Starter Duty - Engines?
Three 3 Minute Attempts, 15 Seconds after each, then cool for 10 Minutes.
(One start attempt of up to 5 minutes, followed by a 10 minute cooling period)
49
Starter Duty - APU?
Three attempts, 1 Minute after each, then cool for 1 Hour
50
Max Payload?
5,250 lbs
51
Recommended Tire Pressure:
- Nose
- Main
Nose - 182 psi
Main - 223 psi
52
Minimum Pneumatic Pressures (2 Pack Ops)
- Normal
- Low power ground, Descent, WAI
- 14 psi - normal high stage set point
- 24 psi - low power ground ops, descent, use of WAI
53
Minimum Pneumatic Pressures (Single Pack Ops)
- Below FL390
- Above FL400
-35 psi - Up to FL390
-22 psi - Above FL400
54
G500 Landing Field Elevation (LFE) limit in CPCS Semi Mode
Limited to < 10,000 ft MSL
55
Max Cabin Differential Pressures:
- In Flight
- Taxi, Takeoff, Landing
- Before MED Open
In Flight: 10.69 psid
Taxi, Takeoff, Landing: 0.3 psid
Before Opening Door: 0.1 psid
56
Maximum crosswind component for landing in anything other than Normal Law:
10 KTS
57
Minimum in flight temp is:
-54°C TAT
See minimum Mach to maintain -54°C chart in limitations. (E.g. Lowest SAT of -80°C needs Mach .87, -76 = .80)
58
Maneuvering Speed (Va)?
206 KCAS
59
Max speed:
Yaw Damper Failure
270 KCAS / 0.85 Mach
60
Use of Autothrottle is prohibited during:
- Single engine approaches
- Approach and landing with flaps 10 or 0
61
Single Engine autopilot coupled go-around is:
Prohibited
62
Limit Datalink free text messages to no more than how many lines of text?
4 lines
63
Minimum Fuel Tank Temperature:
-Greater than 5000 lbs total fuel
-Less than 5000 lbs total fuel
Greater than 5000lbs: - 37°C
Less than 5000lbs: - 30°C
64
If N1 EVM exceeds 0.15 IPS at idle immediately after engine start:
Do not advance throttles. Shutdown engines and re-accomplish the cold weather ops engine preflight inspection.
65
Maximum fuel via over wing fueling:
22,500 lbs
66
APU EGT Limits:
- Starting
- Running
Starting: 1050°C
Running: 732°C
67
Takeoff with APU operating prohibited with OAT above?
45°C
68
APU Generator Load Limits:
- On ground or SL to FL350
- If load is > 55%
- 100%
- Descend <= FL350
69
Flight Load Accelerations:
- Flaps Up
- Flaps 10/20
- Flaps Down
- -1G to 2.5G
- 0 to 2G
- 0 to 2G below MGLW
- 0 to 1.5G above MGLW
Gulfstream G500
flashcards
Decks in class (1)
# Cards
