N430AM Limitations Flashcards
1
Q
Max Design Ramp Wt.
A
16,830
2
Q
Max Design Takeoff Wt.
A
16,630
3
Q
Takeoff weight is limited by the most restrictive of…
A
- Max Certified Takeoff Weight
- Max TO Wt. Permitted by Climb Requirements
- Takeoff Field Length (TOFL)
4
Q
Max Design Landing Wt.
A
15,200
5
Q
Landing weight is limited by the most restrictive of…
A
- Max Certified Landing Weight
- Max Landing Wt. Permitted by Climb Requirements or Brake Engergy
- Landing Distance
6
Q
Max Design Zero Fuel Wt.
A
12,600
7
Q
Max Nose Baggage Wt.
A
310
8
Q
Max Tail Baggage Compartment Wt.
A
Fwd: 300
Aft: 200
9
Q
Center of Gravity Limits
A
Refer to Figure 2-1
10
Q
Engine Type
A
Pratt and Whitney Canada Inc.
PW535A
3400lb Thrust
11
Q
Max Takeoff ITT
A
700 (5min)
12
Q
Takeoff Thrust Time Limit
A
5min (10min OEI)
13
Q
Max Continuous ITT
A
700
14
Q
Max Starting ITT
A
740 (5sec)
Refer to Figure 2-3
15
Q
Max Transient ITT
A
740 (20sec)
Refer to Figure 2-4
16
Q
Max Takeoff N2
A
100%
17
Q
Max Continuous N2
A
100%
18
Q
Min Ground Idle N2
A
49.1% MIN
19
Q
Min Flight Idle N2
A
52.9% MIN
20
Q
Max Transient N2
A
102% (20sec)
Refer to Figure 2-3
21
Q
Max Takeoff N1
A
100%
Limited by TO Charts, Section IV
22
Q
Max Continuous N1
A
100%
Limited by Climb/Cruise Charts, Section IV
23
Q
Max Transient N1
A
102% (20sec)
Refer to Figure 2-3
24
Q
Normal Takeoff Oil Pressure
A
45 TO 140
25
Normal Continuous Oil Pressure
45 TO 140
26
Transient Oil Pressure (20 Seconds)
0 MIN
27
Transient Oil Pressure (400 Seconds)
20 TO 270
28
Normal Oil Pressure - Ground Idle
25 TO 140
29
Normal Oil Pressure - Flight Idle
25 To 140
30
Takeoff Oil Temp
10 TO 132.2
31
Continuous Oil Temp
10 TO 132.2
32
Ground Idle Oil Temp
-40 TO 132.2
33
Flight Idle Oil Temp
-40 TO 132.2
34
Min Starting Oil Temp
-40
35
Max Transient Oil Temp
140.5 MAX
36
Starter Limitations
3 per 30 Min (90 Seconds Rest)
37
Battery Limitations
3 per hour
38
Generator assisted cross-start =
1/3 Battery Start
39
EPU start =
No battery cycle
40
EPU Requirements
28V
| 800-1000 amps
41
Continuous Engine Ground Operation Limit
5 Min
| Temp Range - Figure 2-8
42
Pitot/Static Ground Operation Time Limit
2 min ON - 2 min OFF
43
Max Generator Load - Ground Idle
125 amp
44
Max Generator Load - Flight Idle
225 amp
45
Max Transient Generator Load - Ground Ops
300 amp up to 4 min
46
Avionics time limit begins...
when avionics are powered on (Figure 2-5)
47
Approved Hydraulic Fluid
See Limitations
| We use Skdrol
48
Approved Engine Oil
See Limitations
| We use 2380
49
Mixing Approved Oil Brands
2qt per 400hr
| >2qt requires complete system flush
50
Max Oil Consumption
0.2qt/hr over 10hr period
51
Min Start Oil Temp
-33
52
Single Point Refueling
Fueling: 10 to 50 PSI
Defueling: -10
53
Approved Fuels
See Limitations
54
FUEL BOOST Pumps - ON when...
LOW FUEL lights or >180+/-20
55
Max Fuel Imbalance
Normal: 200
Emergency: 600
56
Fuel Temperature Limitations
See Figure 2-7
57
Vmo/Mmo
BELOW 8000: 262
8000-28907: 292
ABOVE 28907: 0.755
58
Max Maneuvering Speed
Refer to Figure 2-9
59
Vfe
0-15deg: 200
| 35deg: 173
60
Vle
250
61
Vlo
Extend: 250
Retract: 200
62
Vsb
No Limit
63
Vmca
86
64
Vmcg
Flaps 7: 96
| Flaps 15 92
65
Vmcl
88
66
Max Autopilot Operation
292/0.755
67
Min Icing Speed - Sustained Flight
| Except Takeoff, Approach, and Landing
160
68
Max Takeoff and Landing Altitude
14,000
69
Max Tailwind
10
70
Max Takeoff and Landing Temperature
Refer to Figure 2-8
71
Min Takeoff and Landing Temperature
-54C
72
Max Water/Slush on Runway
0.5 inches
73
Max Tire Ground Speed
165
74
Nose Tire Inflation
125 +/-5
75
Autopilot and yaw damper must be...
...OFF for takeoff and landing
76
ENGINE SYNC must be...
...OFF for takeoff and landing
77
VNAV must be...
off below 500AGL
78
Takeoff and Landings are limited to...
...paved runway surfaces
79
Takeoff with antiskid inoperative...
...is prohibited
80
Nosewheel must be...
...in firm contact with ground prior to deploying thrust reversers
81
Takeoff is prohibited with the following forms of contamination:
See Limitations (Clean Aircraft Concept)
82
Visual and Tactile inspection required...
<10C or Fuel Temp <0C and
a. Visible moisture
b. Water present on wing upper surface
c. < 3C temp/dew point spread
d. Conditions conducive to frost formation
83
WING/ENGINE Anti Ice - ON
<10C RAT and visible moisture
84
TAIL DEICE switches ON
+10C to -35C at >150Kts
| +10C to -40C at <150Kts
85
Pitot/Static Heat Ground Operation Limit
2 min
86
Anti-ice systems must not be used to...
...deice surfaces prior to takeoff.
87
Max Operating Altitude
45,000
88
Max Ambient Temperature
Refer to Figure 2-8
89
Min Ambient Temperature
Refer to Figure 2-8
90
Max Generator Load (Above Idle)
300 amp in Flight
91
Max Generator Load (Idle)
225 amp in Flight
92
Boundary Layer
16 per wing
| All must be present for dispatch
93
Min Flight Crew for All Operations
1 Pilot and 1 Copilot
94
Load Factor Limits - In Flight
Flaps UP: -1.44 to =3.6G at 16,630
Flaps 7-35: 0.0 to =2.0G at 16,630
Limits bank angle and pull-up/push-over maneuvers
95
Max Load Factor - Landing (Flaps 35)
+3.46 at 15,200
| Limits sink rate to 600 fpm
96
Cabin Pressure Limits
0.0 to 9.0 PSI
97
Autopilot Min Altitudes
Enroute: 1000AGL
Non-Precision: 300AGL
ILS (CAT I): 180AGL
98
Crew and Pax Oxygen Mask max approved altitude
40,000 cabin altitude
99
Passenger Oxygen Mask prolonged operations
25,000
100
Min Cabin Temp After Cold Soak
| 2hr at -10C or colder
0C for 15min prior to flight above FL250
| Oxygen Mask Deployment
101
Reverse thrust must be reduced to IDLE by...
60
102
Max Reverse Thrust
=/>-18C: 71.4%
| <18C: 68.3%
103
Max Allowable Thrust Reverser Deployment Time
3min in any 10min period
104
Engine static ground operation is limited to...
idle power if thrust reversers deployed
105
Use of Thrust Reversers is prohibited...
...for Touch and Go Landings.
106
Use of Thrust Reversers is prohibited...
...to back the airplane.
107
Thrust Reversers must be checked prior to...
1. ...first flight of the day
| 2. ...after any maintenance.
108
Elevator trim system preflight test...
...must be accomplished prior to takeoff
109
Ground Idle Switch must be in HIGH...
...when conducting touch and go landings
