Limitations Flashcards
1
Q
45 Minute IFR Reserve
A
1627 lb
(FL330, M.80, GW 33,500lb, Anti-Ice Off)
2
Q
Hot Spare Fuel Quantity
A
5400 lb
DO/ADO may authorize reduction
3
Q
Emergency Fuel
A
1367 lb
4
Q
Inclement Weather Fuel Quantity
A
9500 lb
5
Q
Minimum Runway Length
A
4,000’
For Release Only, Use LPA
6
Q
Minimum Runway Width
A
65’
7
Q
Max Runway Slope
A
+/-2%
8
Q
Ops Review Required If Runway Is…
A
Contaminated Less Than 5500
9
Q
- Max X-Wind Dry/Wet Runway for T/O and LND
A
- 25 kt
10
Q
- Max X-Wind Contaminated Runway Width
A
- > than or = 150’
15 kt
< than 150’
10kt
11
Q
- Max Tailwind T/O or LND
A
- 10 kt
12
Q
Equipment That Must Be Operational In RVSM Airspace
A
Pilot/Co-Pilot Primary Altimeters
Autopilot (1)
Altitude Alerting Device (1)
ATCRBS Transponder (1)
13
Q
Minimum Airspeed in RVSM
A
190 kt
14
Q
Max T/O Weight Is Limited By The Most Restrictive of …
A
Max Certificated T/O Weight
Max Runway-Limited T/O Weight
Tire Speed and Brake Energy Limit Weights
Max T/O Weight (Climb Limited)
Obstacle Clearance, En Route & LND Weight Limits
15
Q
Max LND Weight Is Limited By The Most Restrictive of…
A
Max Certificated LND Weight
Max LND Weight
(Runway Length plus Obstacle)
Max LND Weight
(Climb Limit Or Brake Energy Limits)
16
Q
- Max Ramp & Taxi Weight
A
*39,700 lb
17
Q
- Max T/O Weight
A
- 39,500 lb
18
Q
- Max LND Weight
A
- 33,500 lb
19
Q
Max Zero Fuel Weight
A
26,800 lb
20
Q
Interior Baggage Compartment Door Must Be:
A
Latched Closed For T/O & LND
21
Q
If Cargo Is Carried In The Baggage Compartment, Verify…
A
The Smoke Detection System Is Operational
The Lav PBE And Fire Extinguisher Are Serviced And Accessible
22
Q
- Max Operating Altitude
A
- FL450
23
Q
Max Flaps Extended Altitude
A
FL180
24
Q
Max Gear Extended Altitude
A
FL180
25
Max T/O & LND Altitude
10,000’
26
* Minimum Speed Brake Extension Altitude
(Retracted Prior To)
* 500’
27
Max Operating Speed
(VMo)
325 kt
Below 8,000’ - 290 kt
28
Max Operating Mach (MMo)
M.84
29
* Turbulent Air Penetration Speed
(VRa/MRa)
* 235/M.75
30
* Max LND Gear Operating/Extended Speed (VLo/VLe)
* 230 kt
31
Max Tire Ground Speed
195 kt
32
* Flaps 1 Speed (VFe)
* 250 kt
33
* Flaps 2 Speed (VFe)
* 230 kt
34
* Flaps Full Speed (VFe)
* 180 kt
35
* Minimum Speed In Icing
* 200 kt
36
* Unless Directed By AFM Procedures, ECS Knob Selection To Heat Exchange Only Is:
* Prohibited
37
Operations Above FL410, The Following Must Be Selected To Norm:
Both Press Source Buttons
Both Engine Bleed Buttons
ECS Knob
38
Normal Differential Pressure
10.2 psi
39
Max Differential Overpressure
10.3 psi
40
* Cabin Must Be Depressurized Prior To:
* Opening The Cabin Door
41
Do Not Start APU During:
Pressure Refueling
Engine Shutdown
42
* Limit For Successful APU Starts
* 6 Consecutive Start Attempts At 10-min Intervals With A 1-hr Rest
43
Limit for Unsuccessful APU Starts
3 Consecutive Start Attempts, Then 20 min Off
2 Consecutive Start Attempts, Then 1-hr Off
44
* Max Altitude For APU Start
* FL 310
45
Max Altitude For Ground APU Start
13,500’
46
Minimum Battery Temp For APU Start
-20*C
47
APU Ground Start Is Prohibited With Ambient Temp below:
-40*C
48
EICAS Messages That Prohibit An APU Start Attempt
Amber BATTERY VOLT
Amber BATTERY OFF
White BATTERY OFF
49
* Max Operating Altitude for APU
* FL 350
50
When Not To Use Autopilot
T/O or LND
Severe Icing
(Unusual Lateral Trim)
(Autopilot Trim Alerts)
51
* Autopilot Minimum Altitudes
* En Route or Descent 1,000’
* Approach 160’
* T/O, Climb and Missed 400’
Approach
52
Do Not Use Autothrottle Unless:
Comparison Monitor Messages And Appropriate Sensor Reversions Are Selected
53
When Can’t You Use Or Arm The Autothrottles
During Taxi Operations
(Arm ONLY When Cleared For T/O)
54
Minimum Battery Temp For APU or Battery Start Is:
-20*C
55
If BATTERY O’TEMP L or R EICAS Message Displays On Ground…
T/O is Prohibited
(Regardless If Message Clears)
56
Use Of Hydraulic Generator Is Prohibited Unless:
Required By The QRH
57
* Voltage Value Displayed In Green On EICAS Indicates:
* Sufficient Voltage For Battery Start
58
* Max GPU Voltage
* 30V
(Batteries May Discharge If Voltage Is Below 28.5V)
59
Max GPU Load
1,500A
60
Max Engine Generator Load
(In Flight Or On The Ground)
100%
61
Max APU Generator Load
(In Flight Or On The Ground)
100%
62
Galley Pocket Door Must Be Latched Open When?
Taxi, T/O & LND
63
Do NOT Operate Radar System Where?
+/- 90* Of The Nose
Within 16’ Of Personnel or Flammable Material
64
Pressure Refueling Limits
10-55psi
65
Total Fuel Quantity
14,511 lb
66
* Max Fuel Imbalance
* 500 lb
(2,000 lb Fuel Imbalance Was Demonstrated For Emergency)
67
Fuel Temp Limits
-37*C-57*C
68
PBCS Ops Are Authorized As Follows:
Required Communication Performance (RCP) 240sec
Required Surveillance Performance (RSP) 180sec
69
On The Ground, The ENGINE ICE PROTECTION Buttons Must Be Selected ON when in:
Icing Conditions, Except During DeIcing/Anti-Icing Procedures
70
Before TakeOff
When Operating In Visible Moisture And 10*C Or Below or If Expecting To Encounter Icing Conditions At Or Below 400’
What Would Need To Be On?
L & R ENGINE -ON
WING- ON
STAB - ON
71
Can You Hold With Flaps Extended In Icing Conditions?
NO
72
Except For Ground Pre-Flt Check, What’s The Max Temp For Operation Of Wing Ice Protection?
15*C
(Use SAT for Ground, RAT In Flight)
73
Max Temp For Stabilizer Ice Protection
25*C (SAT)
(Operations Above 25*C (SAT) For Up To 2 Min Are Permitted)
74
Do NOT Change FLOW, ENGINE ICE Or WING ICE Until…
>400’
75
Flight In Freezing Rain Is…
Prohibited
76
* Limit Ground Operations Of The Pitot/Static Button ON to…
2 Minutes
77
At One Minute Prior To Takeoff And In Ground Icing Conditions, Select:
Pitot/Static ON For 15 Sec, Then NORM
78
If On The Ground At Idle In Visible Moisture Of 1 Mile Or Less With Temp/Dew Pt Are Equal, Adhere To These Restrictions
Outside Throttles to 70% Max
Temp N1 For 10 Sec Time
Every
>-2*C 30 Minutes No Limit
-2*C- -9*C 15Min 1 Hr
<-9*C 10 Min 50 Min
79
Time With WING ICE PROTECTION Button ON And Thrust Higher Than Idle While Stationary On The Ground Must Not Exceed…
15 Sec
80
Except For Pre-Flt Ck, Max Temp For Operation Of WING ICE PROTECTION Is…
15*C
81
In Icing Conditions, Maintain Flaps Up Configuration Except During…
Approach and Landing
82
If Temp Is 35*C to 45*C And 45*C And Above, Respectively, Begin Using Conditioned Air And Close Doors After
60 Min and 30 Min, Respectively
(Except During Loading And Unloading Of Passengers)
83
If Any GDU Is In Reversion Mode…
Do NOT Depart
84
Do NOT Transmit On HF When Navigation Is Based On…
ADF
85
GPS Approaches Must Be Retrieved From
Current Database
86
Manually Inserted Runway Coordinates are…
Prohibited
87
Takeoff And Landing Data (TOLD)
Do Not Mix Sources Of Performance Information, The Flight Release Is…
Controlling
88
Verify All Inputs Regarding Aircraft Configuration , Runway Information and Ambient Conditions Are In The…
Takeoff Data Window
89
SurfaceWatch
Must Be Inhibited For T/O And LND At An Airport With…
No Runway Position Data
90
SurfaceWatch
Must Not Be Used As The Primary Means To Determine If The Aircraft Can…
Safely Operate Onto A Runway
91
VNAV
If The Aircraft Is Below The VNAV Path, Altitude Preselector Must Be Set To The…
Active Altitude Constraint
92
Approach
Straight-In Vref At Max LND Wt With Anti-Ice System ON is…
125 Kt
93
* Approach
Aircraft Is Certificated In Approach Category…
* Cat C
(If Operational Requirements Dictate Appr Airspeed Faster Than 140 Kt, Then Use Cat D)
94
GPS/GNSS Approach
Applicable Annunciator ( FMS, LPV, LP, L/VNAV Must Be Displayed…
At The FAF
95
GPS/GNSS Approach
RF Legs Are…
Not Authorized
96
GPS/GNSS Approach
Initiate A Missed Approach If These Annunciators Are Displayed
GPS NOT USED
RAIM Not Available From FAF to MAP
DR
GPS LOI
97
GPS/GNSS Authorized Minima
LPV
LP
WAAS to LNAV/VNAV
Baro-VNAV to LNAV/VNAV
LNAV
98
Visual Approach
Crew Must Visually Verify…
That The Course And Path Are Acceptable
99
* Engine Limitations
Min Start Pressure
* 32 psi
100
* Engine Limitations
* Max Tailwind Component For Engine Start
* 16 Kt
101
Engine Limitations
Engine Thrust Between 45-55% N1 Is Prohibited with Tailwinds Greater Than _____ And X-Winds Greater Than _____
10 Kt
25 Kt
102
*Engine Limitations
*Takeoff Thrust:
*Transient N2%:
*AEO - 5 Min
*OEI - 10 Min
*99.9%N2
103
Oil Limitations
Minimum Oil Temp For Motor Or Start
-40*C
104
Oil Limitations
Minimum Oil Temp Above Idle
10*C
105
Oil Limitations
Minimum Oil Temp Acceleration To Climb Thrust Or Higher
15*C
(If Throttle Is Advanced After Oil Temp Reaches 15*C, The Engine Can Continue To Be Operated At Climb Thrust Or Above As Long As The Oil Temp Remains > or = 5*C
106
Starter Limitations
Engine Start
How Many Start Attempts And What’s The Cooldown Time?
3 Attempts
15 Min Cooldown
107
Starter Limitations
How Much Rest Is Required After A 5 Min Dry Motor
15 Min Rest
(Dry Motoring Longer Than 20 Sec Counts As One Normal Start)
108
Thrust Reversers
Reverse Thrust Must Be Idle By?
45 Kt On LND Roll
109
Thrust Reversers
Thrust Reverse Is Prohibited When Conducting _____________
Or _____________
Touch N Go’s
Or
To Back Up The Aircraft
