CL605 Limitations Flashcards
1
Q
Max take off weight
A
48200 lbs
2
Q
Max ramp/taxi weight
A
48300 lbs
3
Q
Max landing weight
A
38000 lbs
4
Q
Max zero-fuel weight
A
32000 lbs
5
Q
Max airport pressure altitude for take-off and landing
A
10,000 feet
6
Q
Max operating altitude
A
41,000 feet
7
Q
Max OAT for take-off and landing
A
ISA +35
8
Q
Min OAT for take-off
A
-40º C
9
Q
Max tailwind for take-off and landing
A
10 knots
10
Q
Max crosswind to use reverse thrust
A
24 knots
11
Q
Max Flaps-up load factors
A
-1.0 G to +2.5 G
12
Q
Max flaps-down load factors
A
0.0 G to 2.0 G
13
Q
Max glide-path angle at or below 1500 feet above touch-down zone elevation
A
4.49º
14
Q
Max altitude for flaps use
A
15,500 feet
15
Q
Max gear extend or retract speed (VLO)
A
197 knots / M0.6
16
Q
Max speed with gear down and locked
A
250 knots / M0.7
17
Q
Max gear-down altitude
A
20,000 feet
18
Q
Tyre speed limit
A
182 knots
19
Q
Turbulence penetration speed
A
280 knots / M0.75
20
Q
Max RVSM speed
A
M0.83
21
Q
Flap 20º limiting speed
A
231 knots
22
Q
Flap 30º limiting speed
A
197 knots
23
Q
Flaps 45º limiting speed
A
189 knots
24
Q
Max runway slope
A
± 2%
25
Fuel quantity - main tanks
4860 lbs each
26
Fuel quantity - Aux tank
7168
27
Fuel quantity - Tail tank
3112 lbs
28
Max fuel imbalance between wing tanks - cruise
800 lbs
29
Max fuel imbalance between wing tanks - Taxi / take-off / landing
400 lbs
30
Take-off with \<500 lbs of fuel in the Aux tank. How much must there be in the Main tanks and Tail tank?
1500 lbs in each Main tank and nothing in the Tail tank.
31
Flap setting and conditions for fuel jettison
0º, No lightning.
32
Min bulk fuel temperature for take-off
5º C
33
Min autopilot use altitude - Take-off
320 feet
34
Min autopilot altitude for visual/non-precision approach
320 feet
35
Min autopilot altitude use for a precision approach - Glide-path 3.5º or less
80 feet
36
Min autopilot altitude for a precision approach with a glide-path of 3.6º-4.49º
160 feet
37
Aircraft max relief differential pressure
9.2 psi
38
Aircraft max negative differential pressure
-0.5 psi
39
Max aircraft differential pressure - taxi / take-off / landing
0.2 psi
40
Altitude above which one ACU or cowl anti-ice must be selected on for each engine
40,000 feet
41
Max AC main generator loading: 0 - 35,000 feet
30 kva
42
Max main AC generator load: \> 35,000 feet
25 kva
43
Max APU generator load up to 20,000 feet
30 kva
44
Max load on TRUs
100 amps
45
Limitations for flight spoiler use in flight
No use below 300 feetNo use below Vref + 10
46
Taxi light limitation when aircraft stationary
Off after 10 minutes
47
APU Max EGT on start
974º C
48
Max APU EGT
731º C
49
APU max RPM
110 %
50
rpm that APU auto-shut down occurs
107 %
51
Min temp for APU start
-40º C
52
Max alt for APU start
20,000 feet
53
Max speed for APU start
290 knots
54
Max altitude for APU bleed air extraction
15,000 feet
55
Max altitude for in-flight engine start with APU (double engine failure only)
15,000 feet
56
If both engines started with APU: Max rpm for operating engine
70 % N2
57
APU start cycles using APU battery
3 attempts of 30 seconds cranking, then 20 minutes rest. 2 further attempts of 30 seconds cranking, then 35 minutes rest before further attempts
58
APU start cycles using ground power
2 attempts of 15 seconds cranking, then 20 minutes rest. 2 further attempts of 15 seconds cranking, then 35 minutes rest before further attempts
59
APU hung start definition
not more than 30 % rpm within 60 seconds
60
Cold soaked aircraft \> 8 hours: first flight of the day if temp is \< -30º C
1. Motor engines for 60 seconds and confirm N1 rotation before start. 2. Reversers must be actuated until the deploy and stow cycles are less than 5 seconds
61
Engine oil max consumption
0.2 quarts or 0.05 US gallons per hour
62
Max engine oil refill before dry motoring is necessary
2 quarts
63
Min steady state oil pressure
25 psi
64
Min oil pressure at take-off power
45 psi
65
Max continuous engine oil pressure
115 psi
66
Max transient engine oil pressure after a cold start
156 psi (130 psi at idle - max 10 mins). AFM 02-05-2
67
Min oil temp for engine start
-40º C
68
Max continuous oil temp
+155º C
69
Max permissible oil temp
+163º C (15 mins)
70
Engine start: fuel introduction limitations - ground start
ITT \< 120º C and N2 \> 20%
71
Engine starter cranking cycle limits (ground and air)
Starter not to be used if N2 is above 55% 3 consecutive start cycles, then 5 minutes cooling between additional cycles
72
Engine start: fuel introduction limitations - starting in the air using starter
ITT \< 90º CN2 \<55%N2 \>28%
73
Engine start: fuel introduction limitations - windmill start below 10,000 feet
N2 greater than 10%
74
Engine start: fuel introduction limitations - windmill start above 10,000 feet
N2 greater than 12%
75
Dry motoring limitations (ignition off, thrust levers at shut-off)
First cycle - 90 seconds max, then 5 minutes off. Subsequent cycles - 30 seconds max, than 5 minutes off.
76
Icing conditions on the ground: Cowl anti-ice limitations
OAT is below +10º C and visible moisture/ contaminated surface
77
Icing conditions on the ground: Wing anti-ice limitations
Wing anti-ice on for final taxi before take-off if OAT below +5º C regardless of conditions unless anti-ice fluids applied. Wing anti-ice on for take-off when OAT is below +5º C and visible moisture below 400 feet AGL. (Wing tactile check if OAT below +5º C or wing fuel below 0º C)
78
Icing conditions in the air: Cowl and Wing anti-ice limitations
Must be on when: 1. Ice detection system detects ice. 2. below 22,000 feet and in icing conditions (TAT below +10º C and visible moisture) 3. Above 22,000 feet and in icing conditions when ice detector has failed
79
Min fuel quantity for go-around and subsequent rotation limit
500 lbs per main tank with max 10º nose-up
80
Reduction in max fuel quantity in Aux and Main tanks for gravity refuling
7%
81
Max Speed with ADG deployed
250 KIASIf necessary: up to 330 KIAS for 12 minutes; up to 348 KIAS for 4 minutes (215 KIAS for flight testing)
82
Electrical load at which generators overload
34.5 kva
83
Cabin altitude at which CABIN PRESSURE aural warning triggered
10,000 feet (14,500 high alt airfield ops)
84
ITT limit for all ground starts
120º C
85
ITT limit for all air starts
90º C
86
Ground operation of electrical/avionics equipment: temp and time limitations
At temps above +40º C, avionics/electrical system use restricted to 30 mins unless one pack is on and the main door closed.
87
Max N1 RPM
98.5% N1
88
Maximum engine ITT
899ºC
89
Maximum engine N2 RPM
99.2% N2
90
Digital FAN VIB amber indication on N1 gauge.
N1 = 2.7 MILS or greater
91
Amber VIB indication on N2 gauge
N2 = 1.7 MILS or greater
