Limitations Flashcards
(38 cards)
1
Q
Max Operating Altitude
A
25,000
2
Q
Maneuvering Limit Load Factors
A
Flaps Retracted = 2.5g to -1g
Flaps extended = 2g to 0g
Gear Down = 2g to 0 G
3
Q
Cargo Door Crosswind Operation
A
no more than 45kts
4
Q
Max Passenger Seats
A
60
5
Q
Max Ramp Weight
A
41,380 lbs
18,770 Kg
6
Q
Max Take Off Weight
A
41,005 lbs
18,600 Kg
7
Q
Max Landing Weight
A
40,344 lbs
18,300 Kg
8
Q
Max Zero Fuel Weight
A
36,817 lbs
16,700 Kg
9
Q
Vmo
A
250 kts IAS
10
Q
Mmo
A
0.55
11
Q
Va
A
160 kts IAS
12
Q
VFE
A
Flaps 15 = 180 kts
Flaps 25 = 160 kts
Flaps 35 = 150 kts
13
Q
Vle
A
180 kts
14
Q
Vlo ret
A
160 kts
15
Q
Vlo low
A
170 kts
16
Q
Vra (max rough air)
A
180 kts
17
Q
Vwo (wiper operating)
A
160 kts
18
Q
Max Tire Speed
A
165 kts (ground speed)
19
Q
Tail Wind Limit
A
15 kts
20
Q
Max Rnwy Slope
A
+- 2%
21
Q
X-Wind
A
45 kts
22
Q
Fuel Quantity
A
4960 lbs
23
Q
Max Fuel Unbalance
A
1212lbs
24
Q
Max Dif Pressure
A
6.35 PSI
25
Max Negative Dif Pressure
-0.5 PSI
26
Max Dif Pressure for Landing
0.35 PSI
27
Max Dif Pressure for OVBD Valve Full Open
1 PSI
28
Max Alt for ONE BLEED OFF
20,000 Ft
29
Fuel Density and Temp Limitations
Density: 6.3 to 7.1 pounds per US gallon
Max Temp: 54C
Min Temp: -40 Jet A
-47 JetA1
30
Fuel and Hydraulic Circuit Breaker Reset?
Not allowed
31
Reduced Thrust
Not permitted on Contaminated Runways
| Not Permitted with significant workload items (ie inop Auto skid, engine gauges etc)
32
Evacuation System
Slide Girt Bars must be installed and emergency operating handle on rear bulkhead door must be exposed prior to leaving loading until arriving at loading ramp
33
Emergency Light System must be armed for:
all flight operations
34
Windshield Heat/Cracked Windshield
Windshield anti-ice must be on and checked for flight ops except as follows:
1) no operate on cracked window
2) Do not exceed 315 KIAS below 10000 when heat inop
Cracked wind shield below 10000 -
315 outer
235 inner
35
Air FLOW switch
Must be NORM for takeoff
36
Autoland
```
Tailwind 10kts
Crosswind 15kts
Headwind 25kts
Do not use if: 1) Align not annunciated by 100ft RAD
2) "RUDDER PWR OFF alert displayed
3) Airport elevation exceeds 8000MSL
4) runway slope +/- 0.8%
5) Flight Control adnormals
6) Runway width less than 145ft
```
37
AutoPilot
no engagement below 200ftAGL
Disengage prior than Mins minus 50 feet
no use if STAB OUT OF TRIM alert longer than 3 sec. after glideslope
38
Max Airspeed for malfunc or inop Mach Trim Compen
.78 Mach
