Limitations Flashcards
(69 cards)
1
Q
Oil Tank Capacity
A
2.09 Gal per Engine
2
Q
Fuel (Max Usable)
A
5816 lbs. (862 Gal)
3
Q
O² @ 70 PSI
A
1600 liters usable
4
Q
Engine Type / Thrust rating / Bypass Ratio
A
P&W JT15D-5D / 3045 lbs / 2.10 to 1
5
Q
Max Ramp Weigh
A
16,500 lbs.
6
Q
Max Takeoff Weight
A
16,300 lbs.
7
Q
Max Landing Weight
A
15,200 lbs.
8
Q
Max Zero Fuel Weight
A
12,200 lbs.
9
Q
Mmo Above 29,907 ft.
A
.755 Mach
10
Q
Vmo 8,000 - 29907 ft.
A
292 kias.
11
Q
Vmo Below 8000 ft.
A
262 kias.
12
Q
Maneuvering Speed
A
Refer to AFM
13
Q
Flaps 7° (T.O.) & 15° (T.O. & APPR)
A
200 kias
14
Q
Flaps 35° (LAND)
A
173 kias
15
Q
Vlo (Extend)
A
250 kias
16
Q
Vlo (Retract)
A
200 kias
17
Q
Vle
A
292 kias
18
Q
Speed Brake Operation
A
No Limit
19
Q
Vmca
A
95 kias
20
Q
Vmcg
A
91 kias
21
Q
Max Tire Ground Speed
A
165 kias
22
Q
A/P Off For:
A
Takeoff and Landing
23
Q
Min Enroute A/P Engaged Alt:
A
1,000 ft.
24
Q
Min VNAV A/P Engaged Alt:
A
500 ft.
25
Min CAT I ILS A/P Engaged Alt:
180 ft.
26
Max IAS/Mach for A/P Engaged:
292kias / .755 Mach
27
Max Altitude for Takeoff or Landing
14,000 ft.
28
Max Tailwind Component
10 kts.
29
Max Runway Water/Slush Accumulation
.5 Inches
30
Max Runway Water/Slush Accumulation
IAS +39° C
31
Minimum Ambient Temp
-54° C
32
Max Takeoff ITT
720° C (5 Min)
33
Max Takeoff N₂
97%
34
Max Takeoff N₁
100%
35
Takeoff Oil Pressure
60-90 PSIG *Max Transient 100 psi for 90 sec
36
Takeoff Oil Temperature
10-121
37
Max Continuous ITT
700°C
38
Max Continuous N₂
97%
39
Max Continuous N₁
100%
40
Normal Oil Temp/Press
Oil Press 60-90 PSIG
| Oil Temp 10-121
41
Flight Idle
```
Time Limit: Continuous
ITT 580°C
N₂ 52 Minimum
N₁ ----
Oil Press 40 PSIG (minimum)
Oil Teimp -40°C to 121°C
```
42
Ground Idle
```
Time Limit: Continuous
ITT 580°C
N₂ 46 (minimum) (at sea level increase slightly with altitude)
N₁ -----
Oil Press 40 PSIG (minimum)
Oil Teimp -40°C to 121°C
```
43
Starting ITT Limit
550° C
44
Min Oil Temp for Start
-40° C
45
Engine Limits, Transient:
```
ITT 740°C
N₂ 97
N₁ 101.9
Oil Press 100 PSIG for 90 Seconds
Oil Temp -18° C - 129° C
```
46
Starter Limitation w/ Battery as power source
hree engine starts per 30 minutes.
| Three cycles with 90-second rest
47
Battery Limitations for Start
3 engine starts per hour
Note: if external power is used to start no battery
cycle is counted.
48
Starter-Generation Limitation
| - Prolonged Ground Operations
Starter-Gen above 125 amps @ Ground idle (46% N₂)
or 225amps @ Flight idle (52% N₂)
PROHIBITED
49
Max Ground Pitot Heat Time
2 Minutes
50
Adding Oil
Any approved brand is acceptable provided:
1. total qty. less than 2 quarts in any 400 hr period.
2. if more than 2 drain flush and refill IAW GMM
51
Minimum Starting Oil Temp
-40° C
52
Min Fuel Temp (takeoff)
-35° C
53
Max Fuel Temp(takeoff)
+54°C
54
Max Altitude
45,000 ft.
55
Max Fuel Imbalance
```
200 lbs (normal ops)
600 lbs ( emergency return)
```
56
Fuel Limitation: Boost Pump On
When low fuel light illuminates
or
185 lbs or less indicated
Av Gas being used
57
Maneuvering Load Factor G Limit - Flaps Up
-1.52 to +3.8g@ 16,300 lbs
58
Maneuvering Load Factor G Limit - Flaps T/O & Approach to Land
0.0 to +2.0 @ 16,300 lbs
59
Maneuvering Load Factor G Limit - Landing Flaps 15° to 35°
+3.5 @ 15,200 lbs
60
Max Differential Pressure
8.9 PSI +/- .1
61
Generator Load - Ground
Ground Idle:
NORM: 125amp, 46% N₂
HIGH: 225amp, 52% N₂
62
Generator Load - Flight
300amp, normal ops
| +50% for 5min over life cycle not per occurrence
63
Thrust Reverser In Flight
Prohibited
64
Thrust Reverser - Touch & Go Landings
Prohibited
65
Idle Reverse Thrust by ____KIAS
60 KIAS
66
Max Thrust Reverser Deployment Time
15 Minutes per Hour
67
T/R's on Sod or Gravel
Prohibited
68
Max N₁ - Reverse Thrust
80.1%
69
Primus 1000 Limitations
Any "HOT" annunciation: NO GO
Any "FAN" annunciation: NO IMC
Any "FAN" annunciation: Ground Ops limited to 10min
Must pass preflight test
