PSA Limitations Flashcards
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1
Q
Ramp Weight
A
53,250 lbs.
2
Q
Maximum Takeoff Weight
A
53,000
3
Q
Maximum Landing Weight
A
47,000
4
Q
Maximum Zero Fuel Weight
A
44,000 lbs.
5
Q
Maximum Weight in Cargo Compartment
A
3,500 lbs.
6
Q
Turbulence Penetration Speed
A
280 KIA’S / .75 M
whichever is lower
7
Q
Max gear extension speed
A
220 KIA’S
8
Q
Max gear extended speed
A
220 KIAS
9
Q
Max gear retraction speed
A
200 KIAS
10
Q
V Wiper
A
220 KIAS
11
Q
Max Tire speed (200/700)
A
182 KIAS
12
Q
Cargo in cargo compartment
A
Flight must be within 45 min of suitable airport
300 nautical miles
13
Q
Flaps Vfe
A
8 - 230 KIAS
20 - 230 KIAS
30 -185 KIAS
45 -170 KIAS
14
Q
Flaps Vfo
A
8 - 200 KIAS
20 - 200 KIAS
30 - 185 KIAS
45 - 170 KIAS
15
Q
COWL ANTI-ICE Conditons
A
- Icing conditions exist when the OAT (on the ground and for takeoff) or TAT (inflight) is 10c or below, and;
- Visible moisture in any form is present in flight or below 400’ AGL for ground operations
- When operating on surfaces that are wet or contaminated
16
Q
WING ANTI-ICE Conditions
A
- Icing conditions exist when the OAT (for takeoff) is 5c or TAT (inflight) is 10c or below, and;
- Visible moisture in any form is present in flight or below 400’ AGL for ground operations
- Runway surfaces are wet or contaminated
17
Q
Tactile check
A
- OAT 5c or less
- Wing fuel temp 0c or less
- Atmospheric conditions conducive to frost formation
- Ice and frost may contine to adhere to wing surfaces even at temps above 5c
18
Q
Cowl Anti-ice system
A
Cowl anti-ice must be on for all ground and flight ops when icing conditions exist except when
• Inflight SAT is -40 or below or
• Ice is annunciated
19
Q
Wing Anti-Ice System
A
Wing anti-ice must be ON for T/O and flight ops when
• Icing conditions exist and airspeed less than 230 KIAS
• ICE is annunciated by the ice detection system
• Except when inflight SAT is -40c or less
20
Q
When must the wing anti-ice be turned on
A
2 minutes prior to T/O during all ground ops 5c OAT or below unless type III or type IV anti-icing fluid has been applied
21
Q
EICAS Limit Markings
• Red
• Amber
• Green
A
- Maximum and Minimum Limitations
- Caution
- Normal Operating Range
22
Q
Engine start limit
Shutdown limit
A
- During all starts do not exceed 75% N1 for 2 minutes after start or until all operating indications are in the normal range whichever is longer
- Operate engines for 2 minutes prior to shutdown.
23
Q
Max ITT for start
Cold start
A
900c
Engine must be run at idle until oil pressure returns to normal range
24
Q
N2 split at ground idle power
A
Not greater than 2% N2
25
Airplane cold soak
-30 for than 8 hrs, before first flight:
• engines motored for 60 sec and fan rotation verified
• thrust reverses actuated until the deploy stow cycles less than 5 sec
26
Takeoff power oil pressure minimum
45psi
27
Continuous ignition
* T/O and landing on Contaminated Runways
* T/O with x wind components greater than 15 KIAS
* Flight through moderate or heavier intensity rain
* Flight through moderate or heavier intensity turbulence
* Flight in the vicinity of thunderstorms
28
Starter cranking limits
| 200
1 min........10 secs off
1 min........10 secs off
1 min........5 minutes off
29
Starter cranking limits
| 700/900
90 sec on ........10 secs off
90 sec on........10 secs off
90 sec on........5 minutes off
30
Initiation of thrust lever from SHUT OFF to IDLE
ITT must be 120c or less for all ground starts
| 90c or less for all air starts
31
Thrust Reversers
During landing maximum reverse thrust is prohibited below 75 KIAS
and reverse idle should be achieved by 60 KIAS
32
Max fuel imbalance (200)
Takeoff 800 lbs
All other phases of flight
800 lbs.
33
Pressure refueling
| 200
14,518 lbs.
34
APU Start cycles (Battery)
30 seconds.....2 minutes off
30 seconds.....20 minutes off
30 seconds.....2 minutes off
30 seconds.....40 minutes off
35
APU Start cycle (DC Ground Power)
15 seconds.....2 minutes off
15 seconds.....20 minutes off
15 seconds.....2 minutes off
15 seconds.....40 minutes off
36
Why 2 minute delay observed between APU cranking attempts
Allow for the starter and starter contactor cooling and fuel drainage
37
Bleed air extraction from APU
NOT permitted above
(200)
15,000'
38
APU Door not closed or position unknown (200)
300 KIAS
| And APU must remain in operation
39
If both engines are to be started using the APU bleed air
The operating engines thrust must not exceed 70% N2
40
APU Door not closed or position unknown (700/900)
220 Kts
| Or APU must remain in operation
41
• Max altitude for single pack operation (200)
• 25,000 ft
42
Automatic Flight Control System
Use of speed mode (DES or IAS), flight director or autopilot coupled, during approach is not permitted
• Not permitted for approaches below 600' AGL except
• Visual and non-precision approaches the minimum height is 400'
• For precision approaches (PAR/ILS), the minimum is 100' AGL
43
* Max load on TRU
| * Max time with DC power to protect CRT displays
* 100 amps
| * 5 minutes
44
* Maximum slats/flaps altitude
| * Enroute use of slats/flaps
* 15,000
| * Prohibited
45
Flaps can not be extended unless it is reasonably assured that
* The visibility will remain above the required visibility
| * An emergency condition exists
46
* Flight spoilers min altitude
| * To ensure adequate maneuver margins, flight spoilers must not be deployed below
* 1,000' AGL
| * Ref plus 17 KIAS
47
Taxi Lights
Off when plane is stationary for more than 10 minutes
48
Brake cooling limits
Minimum is 15 minutes and all BTMS Indicators must be green and not increasing
49
Hydraulic 3b pump
Must be on instead of Auto from the before start checklist until the shutdown checklist
50
Engine Type
| Thrust Rating
GE CF34-3B1
• 8,729 lbs per engine
• 9,220 lbs per engine
51
Dry motoring limitations
90sec-5 min off
| 30sec-5 min off
51
Maximum 90 degree crosswind
| for Takeoff and landing
27kts
| 15 kts for reduced landing minimum (RVR below 2400) to runways w/out TDZ or CL lights
52
Max altitude for engine start with APU bleed air
13,000'
53
Crew Oxygen
2 Pilot - 1410
| 3 Pilot - based on temp in POH before start check
54
No Reduced Thrust (Flex) when?
```
Contaminated Runways
De-iced
Anti-ice in use
Windshear downdrafts forecast
APR not available
Special departure procedure specifies full thrust
```
55
Min fuel for go-around (200)
450lbs per side (900lbs)
56
Min fuel for T/O when with a T/O alternate
4,600 lbs
57
Max fuel imbalance (700/900)
Takeoff 300lbs
| All other phases of flight 800lbs
58
T/O with fuel load in excess of_____in the center tank is not permitted unless each wing tank is above______
500lbs
| 4,400lbs
59
Fuel crossflow
Powered crossflow and gravity crossflow must be OFF for takeoff
60
Min fuel for go-around (700/900)
600 lbs per side
| 1200 lbs total
61
Fuel temperature?
Below 5c prohibited
62
Max cruise in RVSM
.82M
63
A/C Generator loading
Main GEN 30kVA up to 350 then 25 kVA from 350-360
65
Bleed air extraction from APU
NOT permitted above
(700) (900)
25,000 ft
65
Max 90 crosswind for takeoff and landing.
27 knots
67
Max 90 degree crosswind for landing from a cat II approach
15 kts
68
Max headwind for landing CAT II
16 kts
69
Max tailwind for takeoff and landing
10 kts
70
Max operating altitude
| 200
36,000 ft
71
• Max altitude for single pack operation (700/900)
31,000 ft
72
Max operating altitude
| 700/900
41,000 ft
73
Thrust reverser deployment
During landing, maximum reverse thrust is prohibited below 75 KIAS, and reverse idle should be achieved by 60 KIAS
