Limitations Flashcards
1
Q
Max Ramp WT (LR)
A
53,250 lbs
2
Q
Max TO WT (LR)
A
53,000 lbs
3
Q
Max Landing WT (LR)
A
47,000 lbs
4
Q
Max zero fuel weight (ZFW)
A
44,000 lbs
5
Q
Max Temp for TO/LD
A
ISA +35 deg C
6
Q
Min Temp for TO/Dispatch
A
-40 deg C
7
Q
Max TO/LD Altitude
A
10,000’
8
Q
Max RWY Slope
A
+2 percent
9
Q
Max Tailwind
A
10 knots
10
Q
Max Operating Alt
A
FL410
11
Q
Max Load in Cargo Compartment
A
3,500 lbs
12
Q
Must be within __ min of suitable airport, with cargo hold:
A
45 min
13
Q
Min time between a RTO or LD, and subsequent TO:
A
15 min
14
Q
Max BTMS temp for TO
A
06
15
Q
Load Factor Limits (flaps UP)
A
-1.0 to +2.5 G’s
16
Q
Load Factor Limits (flaps DOWN)
A
0.0 to +2.0 G’s
17
Q
Min O2 psi for dispatch
A
1410 psi
18
Q
Vle
A
250
19
Q
Vlo
A
250
20
Q
Vlo (ret)
A
200
21
Q
Vfe (8)
A
215
22
Q
Vfe (20)
A
215
23
Q
Vfe (30)
A
185
24
Q
Vfe (45)
A
170
25
Max wiper speed
220
26
Max tire speed
182
27
Turbulence Air Penetration speed
280 or .75 Mach (whichever is lower)
28
Max ADG deployment speed
Vmo, Mmo
29
Stab/mach trim inop speed
250 or .70 Mach
30
Max number of pax on stairs
4 (or 1,000lbs)
31
Max time taxi lights on when stationary
10 min
32
Min altitude for A/P engagement
600' AGL
33
Min altitude for A/P (precision aprch)
80' AGL or no less than 50' below the DA
34
Min altitude for A/P (non-precision aprch)
400' AGL or 50' below MDA (whichever is higher)
35
Max L/R fuel tank qty
4,760 lbs
36
Max CENTER fuel tank qty
4,998 lbs
37
TO with greater than 500lbs in center of tank is prohibited unless each wing tank is greater than ___lbs
4,400 lbs
38
Approved fuel:
Jet A
39
Minimum fuel qty for Go-Around
450 lbs/side
40
Min FUEL FEED TO temp:
+5 deg C
41
Min BULK fuel temp:
-40 deg C
42
Max fuel imbalance:
800 lbs
43
Cross flows (powered and gravity) must be ___ for TO:
OFF
44
Max ITT (APR NOT Op.) ___ (first 2 min), ___ (next 3 min):
900 deg C, 884 deg C
45
Max ITT (APR Op.) ___ (first 2 min), ___ (next 3 min):
928 deg C, 900 deg C
46
MCT (max continuous thrust) max ITT
900 deg C
47
Max N1 percent
98.6 percent
48
Min N2 percent to introduce fuel during start
20 percent
49
Max ITT during start
900 deg C
50
Max N1 percent and N2 percent for normal TO
96.2 percent, 98.3 percent
51
Max N1 percent and N2 percent for APR TO
98.6 percent, 99.4 percent
52
Engines must be running for a Minimum of ___min prior to TO
2 mins
53
Engines must be idle for a Minimum of ___min prior to shutdown
2 mins
54
Engine start cycle limits:
1 min ON, 10 sec OFF
1 min ON, 10 sec OFF
1 min ON, 5 mins OFF
55
Max ITT for engine start on the ground
Less than or equal to 120 deg C
56
Max ITT for in-flight engine start
Less than or equal to 90 deg C
57
Max N2 percent to engage Starter
Starter not to be used if greater than 55 percent N2
58
Dry motoring limits
90 sec ON, 5 min OFF
| 30 sec ON, 5 min OFF
59
Thrust reverser limitations on TO (3):
1. Ground use only
2. No Go-Arounds after deployment of TRs
3. TO with any abnormal TR annunciator is prohibited
60
Reject TO (3 items)
Thrust Lever - IDLE
Wheel Brakes - Apply MAX breaking until safe stop
Thrust reversers - Apply MAXIMUM
61
What does APR stand for?
Automatic Performance Reserve...hotter/higher numbers when you have APR use
