Limitations Flashcards
1
Q
Acft wingspan
A
19.78m
2
Q
Acft length
A
20.00m
3
Q
Acft tail height
A
6.35m
4
Q
Max rwy slope
A
±2%
5
Q
Max tw (to/ldg)
A
10 kts
6
Q
Max xwind
A
30 kts
7
Q
Max altitude - engine bleeds open/EEC on
A
32,000’
8
Q
Max altitude – engine bleeds open/EEC off
A
25,000’
9
Q
Max altitude – engine bleeds closed/EEC on
A
25,000’
10
Q
Max altitude – engine bleeds closed/EEC off
A
20,000’
11
Q
Max altitude – RH front aisle seat (1B) occupied
A
25,000’
12
Q
VA
A
200 KIAS
13
Q
VFE 10
A
200 KIAS
14
Q
VFE 25
A
150 KIAS
15
Q
VFE 45
A
135 KIAS
16
Q
VLE
A
200 KIAS
17
Q
VLO
A
200 KIAS
18
Q
MMO
A
0.52
19
Q
VMO >8000’
A
272 KIAS
20
Q
VMO ≤8000’
A
250 KIAS
21
Q
Turbulence penetration speed
A
175 KIAS
22
Q
Max G flap retracted
A
-1.0 to +2.8
23
Q
Max G flap extended
A
0 to +2.0
24
Q
Max zero fuel weight
A
10,900 kg
25
Max ramp weight
12,070 kg
26
Max takeoff weight
11,990 kg
27
Max landing weight
11,700kg
28
Max baggage compartment weight - standard
550 kg
29
Max baggage compartment weight – dual net
700 kg
30
Minimum operational temp
-54°C
31
Maximum operational temp – Air Con operating
ISA +35°C
32
Maximum operational temp – Air conditioning inop
ISA +20°C Alt alert deenergised
ISA +15°C Alt alert energised
33
Maximum cabin differential
7.2 psi
34
Starter duty cycle
30 seconds on, 3 minutes off
30 seconds on, 3 minutes off
30 seconds on, 30 minutes off
35
Max usable fuel qty per side
2866 lbs
36
Max fuel imbalance
600 lbs
37
Add __ lbs to unusable fuel when main ejector boost pump is inoperative
80 lbs
38
APU max start EGT
732°C to 974°C for 10 seconds
39
APU Max start alt
20,000’
40
Max wiper speed
160 kts
41
Min NH for pneumatic deicing systems
80%
42
Main generator max load - on ground
380A (400A < ISA +27°C)
43
Main generator max load – in flight
400A (380A > 27,000’)
44
Aux generator max load
150A (140A > 18,000’)
45
APU generator max load
400A (290A >16,000’)
46
Max battery temp
70°C
47
Min icing speed – flap up/gear up
165 KIAS
48
Min icing speed – flap 15/gear up
140 KIAS
49
Min battery voltage – engine start (no APU)
24v
50
Min battery voltage – APU start
22v
51
Max NH for positive oil px during engine start
45%
52
Main landing gear track
6.58 m
53
Min pavement width for 180° turn
18.85 m
54
Min taxi turning radius
15.76 m (wingtip)
55
Rwy considered wet
a. Surface water not more than 3mm deep
b. Slush or loose snow equivalent to surface water not more than 3mm deep
c. Sufficient moisture to appear reflective but without significant areas of standing water
56
Rwy considered contaminated
More than 25% of the runway surface area within the required length and width being used covered by:
a. water, or slush more than 3 mm deep
b. loose snow more than 20 mm deep
c. compacted snow or ice, including wet ice
57
T6 – takeoff
816°C for 5 mins
58
T6 – max continuous
800°C
59
T6 – starting
816-850°C for 20 seconds
850-950°C for 5 seconds
60
T6 – transient
816-850°C for 20 seconds
61
Torque – takeoff
110% for 5 mins
62
Torque – max continuous
100%
63
Torque – max climb/cruise
84%
64
Torque – transient
120% for 20 seconds
65
NP – takeoff/climb/cruise
100.0-101.0
66
NP – transient
110% for 20 seconds
67
NP- reverse
80.5%
68
NH – takeoff/max continuous
102%
69
NH – ground idle
62% min
70
NH – climb/cruise
100%
71
Oil temp – all airborne ops
45-115°C
72
Oil temp – ground idle
-40 to 115°C
73
Oil temp – starting
-40°C
74
Oil temp – transient
115-125°C for 15 minutes
75
Oil press – all airborne ops
55-65psi
76
Oil press – ground idle
40 psi min
77
Oil press – starting
70 psi max
78
Oil press – transient
40-70psi
79
Icing conditions exist in flight or on the ground in visible moisture with IOAT of __ C or below
+10℃
80
Leading edge deicers must be activated only after reaching __________ speed
Final segment speed (VFS)
81
In icing conditions, use of flaps is restricted to ____________.
When flaps have been extended for approach and landing, they may not be retracted unless ________ or unless _______
In icing conditions, use of flaps is restricted to takeoff, approach and landing.
When flaps have been extended for approach and landing, they may not be retracted unless upper surface of wing is clear of ice or unless flap retraction is required for go-around.
82
OEI Max Bank Angle - V2
15°
83
OEI Max Bank Angle - V2 + 5
20°
84
OEI Max Bank Angle - V2 + 10
25°
