Limitations Flashcards
1
Q
VMO
A
300
320 @ 10,000
2
Q
MMO
A
.82
3
Q
Max Turbulent air below 10,000
A
250
4
Q
Max Turbulent air Above 10,000
A
270 / .7M
5
Q
Max Tire Limit GS
A
195
6
Q
Max Wiper Speed
A
250
7
Q
VLO
A
250
8
Q
VA
A
240
9
Q
VLE
A
250
10
Q
VLO
A
250
11
Q
VFE 1
A
230
12
Q
VFE 2
A
215
13
Q
VFE 3
A
200
14
Q
VFE 4
A
180
15
Q
VFE 5
A
180
16
Q
VFE FULL
A
165
17
Q
Auto Flight Takeoff limit
A
400 ft
18
Q
Auto Flight Coupled ILS Limit
A
50 ft
19
Q
APU Starter limits 1st and 2nd
A
60 seconds on then 60 seconds off
20
Q
APU Starter limits 3rd cycle
A
60 seconds on then 5 5inutes off
21
Q
Engine Starter Duty Cycle Limits 1st and 2nd
A
Ground: 90 seconds on 10 seconds off
Flight: 120 seconds on 10 seconds off
22
Q
Engine Starter Dry Motoring 1st attempt
A
90 seconds on 5 minutes off
23
Q
Engine Starter Dry Motoring 2nd through 5th attempt
A
30 seconds on 5 minutes off
24
Q
APU Altitude Start limit
A
30,000
25
APU Altitude Electric use limit
33,000
26
APU Altitude Bleed use
15,000
27
Altitude Engine Start
21,000
28
Definition of Icing Conditions
10 degrees and below and....
a. Visible Moisture or
b. Surface Snow, Slush, Ice, or Standing Water
29
EICAS Engine Limit Max and Min markings
Red
30
EICAS Engine Limit Caution Range
Amber
31
EICAS Engine Limit Normal Range
Green
32
Engine Thrust: Use of reduced takeoff thrust procedures is not allowed....
On runways contaminated with standing water, slush, snow, or ice.
33
Max Land Weight
170 72,310
| 175 74,957
34
Max Tail Wind component
10 kts
35
Max Operating Altitude
41,000
36
Max Flap Extension Altitude
20,0000
37
Fuel Tank Min Temp
-40 C
38
Max Fuel Imbalance
800 lbs
39
Air Conditioning Max Alt for single pack Ops
31,000
40
Flap Max Altitude Extended
20,0000
41
Single Engine Taxi is not authorized when....
1) Braking action is less than good.
2) RVR is reported less than 1200
3) Power out is required (no pushback)
4) After Landing
a) If starting the APU, do not shut down an engine until the APU has stabilized at 95% or greater for a Min of 3 sec.
b) A 2 minute cool down must be observed prior to shutting down an engine.
c) Wait a Min of 1 additional minute after shutting an engine down prior to starting the APU.
42
Engine Starter Duty Cycle Limits 3rd through 5th
Ground: 90 seconds on 5 minutes off
| In Flight: 120 seconds on 5 minutes off
43
Max Takeoff and Landing Altitude
8,000 ft
44
Min Takeoff and Landing Altitude
-1,000 ft
45
Min Ambient Temp for Takeoff
-40 C (SAT)
46
Min Ambient Temp for Operation
-54 C (SAT)
47
Max Ramp Weight
170 82,364
| 175 85,870
48
Max Takeoff Weight
170 82,011
| 175 85,517
49
Fuel Quantity Capacity (Total)
20,935
50
Unusable Quantity per Tank
100lbs
51
Crossfeed Operations during takeoff and landing
Must be OFF
52
Max Differential Pressure
< 37,000 ft 7.80 psi
| >37,000 ft 8.34 psi
53
Brake Temps in Amber?
Do not take off.
54
Thrust Reversers....
- Ground use only
- Full stop landings
- Do not attempt go-around after deployment
- Powerback is prohibited
- IDLE thrust below 60 KIAS
- After selecting Reverse Thrust, do not move the thrust levers forward of the detent until the REV icon on the EICAS is amber or green.
55
APU Min start temp
-54 C
