Limitations And Memory Items Flashcards
1
Q
Max oil pressure AT OR ABOVE 88% N2
A
- 110 psi
- Operation in oil pressure amber range between 110 and 115 PSI is permitted in all operational modes and time limited to 5 minutes,
- or between 116 and 155 psi in all operational modes time limited to 2 mins.
- Total time above 110 psi may not exceed 5 mins.
2
Q
Max Landing Weight
A
42,549 lbs
3
Q
Max APU Operational Altitude
A
37,000’
4
Q
Rapid Cabin Depressurization
A
Crew Oxygen Masks… Don
Crew Communication…Establish
Emergency Descent….As Required
5
Q
Max Altitude
A
37,000’
6
Q
Max N1
A
100%
7
Q
Engine Cool Down
A
The engines must run for at least 1 min. At idle or taxi thrust before shutdown.
8
Q
ATTCS Failure
A
Thrust Levers….Max
9
Q
Pitch Trim Runaway
A
Quick Disconnect Button….Press and Hold
10
Q
ATTCS
A
Must be operative for ALT T/O-01 Mode
11
Q
Max ITT Start
A
800 degrees C
12
Q
Min Fuel Temp
A
-54 degrees C
13
Q
Tailwind
A
10 kts max for takeoff and landing
14
Q
Max ITT takeoff modes
A
948 degrees C and takeoff thrust is time limited to 5 minutes.
15
Q
Max HP Spool Vibration
A
1.1 IPS
16
Q
Max Tailwind LR/LR2 (Cat II)
A
10 kts
17
Q
Aileron/ Roll Trim Runaway
A
Quick Disconnect Button…Press and Hold
Aileron Systems 1 and 2…off
18
Q
Turbulent Air Penetration at or below 10,000’
A
200 KIAS
19
Q
Engine Starting or Dry Motoring limitation on the ground
A
Up to 5 minutes on, 5 minutes off
20
Q
Landing Gear Retraction (Vlo)
A
200 KIAS
21
Q
Max. Operating Temp
A
ISA + 35 deg C
22
Q
APU Starter Cooling Period between 3 consecutive attempts
A
1 minute off
23
Q
Min Decision Height (Cat II approaches)
A
100’
- Autopilot is mandatory for CAT II approaches.
24
Q
Inadvertent Spoiler Opening in Flight
A
Speed Brake…close
25
Max Altitude for APU Start
30,000’
26
Baggage Compartment Smoke
EICAS WARNING: BAGG SMOKE...Verify
| Baggage Fire Extinguisher Button...Press
27
Max Temp for A/I Operation
10 degrees C
28
Engine Warm Up
- Prior to take off must run at low thrust to stabilize temps
- After start engines must run at idle or taxi thrust for 4 mins if cold (shut down for more than 90 mins) or
- 2 mins for warm engines.
- To increase N2 above 83% the engine oil temp must be 40 deg C min.
- In lieu of this limit it is acceptable to run the engine for at least 8 mins.
29
Windshear Prevention/ Recovery
Thrust Levers.............Max
| Go Around Button.....Press
30
Max Fuel Imbalance
800 lbs
31
Dual Engine Failure
```
Airspeed....Min 260 kts
Oxygen Mask (if required)...Don
```
32
Single Engine Go-around on autopilot (Cat 1 approach)
Prohibited
33
Max Recommended Crosswind- Compacted Snow
25 kts (including gust)
34
Engine Fire, Severe Damage or Separation
Associated Thrust Lever....IDLE
Associated Start/ Stop Selector....Stop
Associated Fire Extinguisher Handle...Pull (DO NOT ROTATE)
35
Max N2
102.4%
36
Max LP spool vibration
1.8 IPS
37
Single Engine Cat II
Prohibited
38
Landing Gear Extended (Vle)
250 KIAS
39
Flap Extension Vfe
Flaps 9...250KIAS
Flaps 22...200KIAS
Flaps 45...145KIAS
40
Max Fuel Temp
52 degrees C
41
Windshield Wiper, Max for Operation
170KIAS
42
Max Ramp Weight
48,722 lbs
43
Max Oil pressure BELOW 88% N2
- 110 psi.
- May be exceeded during starts if oil temp is below 21 degrees C.
- The engine must remain at IDLE until the pressure is less than 110 psi.
- Operation in oil pressure amber range between 110 and 115 PSI is permitted in all operational modes and time limited to 5 minutes,
- or between 116 and 155 psi in all operational modes time limited to 2 mins.
- Total time above 110 psi may not exceed 5 mins.
44
Min Airspeed after takeoff/ during climb without re-trimming
160 KIAS
45
Max Operating Altitude when one bleed pack or one bleed pack is closed
25,000’
46
When operating with APU bleed pack supplying pack 1 (Eng. bleed closed) and engine 2 supplying pack 2 (crossbleed closed), max operating Altitude is:
37,000’
47
Max Altitude Single Engine or Single Bleed in Icing Conditions
15,000’
48
Abnormal Engine Start
To abort start:
Associated Thrust Lever...Idle
Start/ Stop Selector...Stop
49
Max Altitude to Extend Flaps
20,000’
50
Reversers
Do not go around after reverser deployment
51
Engine starter limits on the ground (first to fourth cycles)
1 minute on, 1 minute off
52
Max Recommended Crosswind - Dry Runway
30 kts (including gust)
53
Min Engagement Height after takeoff or Go-around
500’
54
Max continuous engine starter operation time IN FLIGHT
5 minutes on
| No cool down time required should an in-flight start be re-attempted.
55
APU Fire
APU Fuel Shutoff Valve...Close
56
Landing Gear Extension (Vlo)
250 KIAS
57
Direct Vision Window, Max Airspeed to Remove
140KIAS
58
Rudder/ Yaw Trim Runaway
Quick Disconnect Button...Press and Hold
| Rudder Systems 1 and 2...off
59
Engine starter limits on the ground - following cycles (after first to fourth)
1 minute on, 5 minutes off
60
Min Altitude Coupled to ILS (Cat II approach)
50’
- Autopilot is mandatory for CAT II approaches.
61
Holding Configuration in Icing Conditions
Landing Gear -up
Flaps -up
Min Airspeed - 200 KIAS
62
Turbulent Air Penetration above 10,000’
250 KIAS/ 0.63M (whichever is lower)
63
Max Crosswind (Cat II)
10 kts
64
Jammed Aileron
Aileron Disconnect...Pull
65
Jammed Elevator
Elevator Disconnect...Pull
66
Min Altitude autopilot coupled to ILS (Cat 1 approach)
200’
67
Battery Over-temperature
Associated Battery.........Off
68
Max Recommended Crosswind- Ice (No melting)
10 kts (including gust)
69
Min Oil Temp
21 degrees C
-Min Oil Temp for starting is -40 degrees C for lubrication oil specified by MIL-L-23699D
70
Max Usable Fuel quantity each tank
Main Tanks 5,717 lbs (844.9 US Gal)
71
Maneuvering Speed (Va)
200 KIAS
72
Steering System Inop or Uncommanded Swerving on the ground
Steering Handwheel...Do not use
| Steering Disengagement Button...Press
73
Max Zero Fuel Weight
39,462 lbs
74
Max Recommended Crosswind - Wet Runway
30 kts (including gust)
75
Max Takeoff Weight
48,501 lbs
76
Max Continuous ITT
901 degrees C
77
Max Duration of ISIS when operating on batteries:
40 mins
- Max duration of battery power can be extended to 45 mins if the pitot 3 heating button is turned off when not operating in icing conditions
- Airplane must not be moved during power up initialization. Do not cage attitude in turning flight.
78
APU starter cooling period between 2 series of 3 consecutive attempts
30 minutes off
79
Emergency Descent
1) Cabin Crew....Notify
2) Fasten Belts...On
3) Thrust Levers...Idle
4) Speed Brakes...Open
5) Airspeed...250KIAS
6) Landing Gear... Down
7) Altitude...MEA or 10k feet, whichever is higher.
80
Max Headwind (Cat II)
25 kts
81
Smoke Fire or Fumes/ Smoke Evacuation
Crew Oxygen Masks.............Don, 100%
Smoke Goggles....................Don
Crew Communications.........Establish
82
Max TAT in Cruise above 25,000’
-45 degrees C
83
Min RVR (Cat II)
1,200’
84
Min Oil Pressure BELOW 88% N2
34 psi
85
Max oil temp
126 degrees C
86
Max Aft Cargo Weight
2,646 lbs
87
Max Operating Vmo/ Mmo
0-8000...250KIAS
10k-260...320KIAS
260-370...0.78 Mach
88
Min. Temp. For Manual A/I Operation
-40 degrees C
89
Max Recommended Crosswind- Standing water or slush
20 kts (Including gust)
90
Min oil pressure AT OR ABOVE 88% N2
50 psi.
- while this is an abnormal condition, Operation between 50 and 34 psi is permitted during takeoff and go around phases.
91
Takeoff and Landing Structural Envelope - Pressure Altitude
-1000' to 8000'
92
Takeoff and Landing Structural Envelope - Temperature
-40 deg C to ISA+35 deg C
93
Min Operating Temp
- 54 deg C to 25,000'
| - 65 deg C to 37,000'
94
Load Factor Limit
Flaps Up: -1.00 G to 2.5 G
| Flaps Down: 0 G to 2.0 G
95
Fuel Specification
Jet A, Jet A-1, JP8, JP5
96
Fuel Tank Temp
-40 deg C to 52 deg C
97
Unusable Fuel Quantity Each Tank
39 lbs (5.8 US Gal)
Note: Unusable fuel increases to 365 lbs in each wing tank if the associated elec fuel pump is inop.
Note: When pressure refueling, the usable fuel in each tank may be reduced by 13.2 US gals.
98
Max APU rotor Speed.
108%.
| APU model T-62T-40C14 will be automatically shut down at 104% rotor speed.
99
Max EGT for APU start
884C
100
Max Continuous EGT for APU
680C
| APU EGT may be exceeded up to 717 C for 5 mins Max.
101
Min Batt Voltage to start APU
22 volts
102
Min Temp to start APU from a GPU
-54C
103
Max Differential Pressure
7.8 PSI
104
Max Differential Over Pressure
8.1 PSI
105
Max Differential Negative Pressure
-0.3
106
Max load on Main Generator
400 amps
107
Max load on APU Generator
400 amps to 30,000'
| 300 amps above 30,000'
108
Max Batt Temp
70 deg C
109
Electro-mechanical Gust Lock
each time the gust lock lever is set to the unlocked position elevator movement must be checked. Must be performed at least 10 seconds after positioning the gust lock lever from the unlocked position by moving the control column from the full stop (fwd) to the full down stop (back) and back to the full up stop (fwd) position.
110
To proceed with comparison between Altimeter Indications, the following conditions must be met
1) Airplane Leveled (+- 50' of tolerance)
2) Airplane Stabilized (+- 5 kts of tolerance)
3) Comparison started 15 secs after leveling and stabilizing the airplane.
Alt differences greater than the values in RVSM tables must be reported to MX and flight into RVSM airspace is prohibited.
Use of autopilot during the alt check is recommended.
