Limitations Flashcards
0
Q
Maximum Tailwind
A
Option 10 kts
or
Option 15 kts
1
Q
Runway Slope Limits
A
+/- 2%
2
Q
Maximum Demonstrated Crosswind
A
36 kts without winglets
33 kts with winglets
3
Q
Maximum Speed (Vmo/Mmo)
A
320 kias
0.82 m
4
Q
Turbulent Air Penetration Speed
A
280 kias / .76m
250 kias when below 15,000 ft and below MLW
(AOM Vol. 1 SP.16.21)
5
Q
Maximum Altitude
A
41,000 ft
6
Q
Maximum Takeoff and Landing Altitude
A
8,400 ft
or
12,000 ft with Hight Altitude Option
7
Q
Maximum Ramp Weight
A
156,000 lbs
or
174,700 lbs with IGW Option
8
Q
Maximum Takeoff Weight
A
155,500 lbs
174,200 lbs with IGW option
9
Q
Maximum Landing Weight
A
144,000 lbs
10
Q
Maximum Zero Fuel Weight
A
136,000 lbs
11
Q
Maximum Cabin Differential Pressure
A
9.1 psi
12
Q
Maximum Altitude for APU Bleed and Electrical use
A
10,000 ft
*Under Captain’s Emergency Authority, APU has demonstrated the capability to supply both bleed air and electrical power up to 20,000 ft.
13
Q
Maximum Altitude for APU Bleed Only Use.
A
17,000 ft
14
Q
Maximum Altitude for APU Bleed and Electrical Use on Ground
A
15,000 ft
15
Q
Maximum Altitude For APU Electrical Use Only
A
41,000 ft
16
Q
Minimum Altitude for Autopilot use After Takeoff
A
400 ft AGL
17
Q
Minimum Altitude for Autopilot “ON” During Non-Precision Approach
A
50 ft Below Minimums
18
Q
Maximum Engine Limits
A
Redline
19
Q
Minimum Engine Limits
A
Redline
20
Q
Engine Caution Limits
A
Amber
21
Q
Engine Ignition Must Be On For: \_\_\_\_\_\_\_\_\_\_\_ \_\_\_\_\_\_\_\_\_\_\_ \_\_\_\_\_\_\_ \_\_\_\_\_\_\_ \_\_\_\_\_\_\_\_\_\_\_
A
Takeoff
Landing
Heavy Rain
Anti-Ice
22
Q
Maximum Flaps Extension Altitude
A
20,000 ft
23
Q
Minimum Altitude For Speed Brake Use.
A
1,000 ft
24
Alternate Flap Duty Cycle (down and back up)
0-15-0 = 5 min.
> 15 = 25 min.
25
Fuel System Minimum Temperatures
-43˚C or 3˚C above fuel freezing
Whichever is warmer
26
Fuel System Maximum Temperatures
49˚C
27
Random Fuel Imbalance
1,000 lbs for Taxi, Takeoff, Landing
28
Icing Condition Temperature
10˚C/50˚F or below
29
Air Data Inertial Reference Unit (ADIRU) Alignment Must Not be Attempted at Latitudes Greater Than
78˚ 15 min
30
Maximum Flight Operating Latitude
82˚ North and South (without Polar Navigation Option)
Exceptions:
Between 80˚W and 130˚W = 70˚N
Between 120˚E and 160˚E = 60˚S
31
Photoluminescent Floor Lighting Must be ___________
Charged IAW Approved Procedures and Charging Table in AOM Chapter 1 section 40.
32
Flight Deck Door Operational Check Must be Checked
Once a Day
33
Escape Slide Retention Bar
Must be installed for Taxi, Takeoff, and Landing
34
Standby Altimeter for RVSM Accuracy
Does not meet Accuracy Requirements for RVSM
35
Maximum Altitude Difference Between Captain's and FO's Altimeters for RVSM Use While in Flight
200 ft
36
Maximum Difference Between the Captain's and FO's Altimeters on the Ground for RVSM Use
Airport Elevation S.L. to 5000 ft = 50 ft
5001 ft to 10,000 = 60 ft
37
Maximum Difference of Captain's and FO's Altimeters to Airport Field Elevation While on Ground
75 ft
38
With Engine Bleed on do Not Run A/C Packs in _______ for Takeoff, Approach, or Landing
High
Note: Except for NNP (like Cargo Fire, Smoke Removal) Checklist Has Prioity.
39
Engine TAI Must Be On When _______
In Icing Conditions or Icing Conditions are Expected.
Exception: During Climb and Cruise When Temp is Below -40˚C SAT
40
De-Icing with Type II and IV fluids for Airplanes without Stiffened Elevator Tabs.
Max Speed 270 kias until Maintenance Procedures are Accomplished
41
Autopilot Single Channel Approach Minimum Disengagement Altitude
50 ft AGL
RA 100 ft for airports above 8,400 ft onairplanes with Hight Altitude Option
42
Maximum allowable wind components for Autoland Operations
Headwind: _________
Crosswind: _________
Tailwind: __________
25 kts
20 kts
15 kts
43
Maximum allowable wind components for Autoland Operations (Cat IIIB)
Crosswind:______
Tailwind:_______
```
25 kts (?)
10 kts
```
44
Maximum and Minimum Glideslope Angles for Autoland
3.25˚ and 2.5˚
45
Single Engine Cat IIIB Autoland Operations
Flaps 30 and only for DH at or above 50 ft AGL
46
Maximum Pressure Altitude for use of Autoland
8,400 ft
47
Integrated Approach Navigation (IAN)
Do not use if altitude constraints between the FAF and the runway have been modified by the flight crew.
48
HUD System Maximum Latitude and Limit of use
85˚ Latitude or when heading reference is set to TRUE
| with HGS 2350 and polar Nav
49
Flight Dynamics Model 4000 Phase I HGS (HUD)
AIII Mode Approach and Landing not approved
50
Limitation for use of VHF-3 for voice communications
Do Not Use with ACARS Operational
51
ACARS Limitation
Limited to transmissions that will not creat an unsafe condition
Parts of messages delayed or not received
message delivered to wrong recipient
Correct message content
52
Use of ACARS for clearances
Predeparture Clearance, D-ATIS, Ocianic Clearance, W&B, Takeoff Data messages may be used if from a verified and pre approved ops procedures.
53
Use of VHF communications with ATC on the ground
Use Radio That is Connected to Top Antenna
54
Use of auxiliary power outlets in the flight deck
Requires regulatory approval
55
Reverse Thrust Limitation
Intentional use inflight is prohibited
56
APU Bleed Valve Must Be Closed When
a - Ground Air is Connected and Isolation Valve is Open
b - Eng. #1 Bleed Valve is Open
c - Isolation Valve and Eng. #2 Bleed Valve is Open
57
APU Bleed Valve May Be Open During Engine Start But:
Avoid Power Settings Above Idle.
58
Holding In Icing Conditions With Flaps Extended
Prohibited
59
Do Not Extend Speed Brake Lever Beyond _____ ______ When InFlight
Flight Detent
60
Maximum Speed for Use of Speed Brakes
300 kias (for airplanes without stiffened elevator tabs)
use of speed brakes at speeds in excess of 320 kias can cause sever vibration and damage the horizontal stabilizer
61
Rapid and Large Alternating Control Inputs
Avoid - May Result in Structural Failure Even Below Va
62
Time Between Actuations of The Alternate Flap Switch
15 Seconds - avoids damage to motor's clutch
63
When QFE is Selected, Use of VNAV, LNAV, and Veridical Situation Display is _______
Prohibited
64
Selection of QFE is Prohibited if _______
QFE Option Is Not Installed In The FMS
65
Regarding the PFD, If QFE is Used Instead of QNH: _____________
Selection of QFE Must be Made in the FMS
66
Use of Look Ahead Terrain Alerting:
a - Without GPS or
b - With GPS and an Older GPWS Computer
Is Prohibited
67
Limitation On Use of Look Ahead Terrain Alerting (GPWS)
A - ____________________
B - ____________________
A - Do Not Use Terrain Display For Navigation
B - Do Not Use Within 15 min. of Takeoff, Approach, or Landing at
airports contained in the GPWS Database
68
Use of Integrated Approach Navigation (IAN) With QFE is _______
Prohibited
69
Weather Radar Limitations
Do Not Operate In a Hangar, 50ft From Personnel and Fuel Spills.
*Hangar and Personnel do not apply with radar in test mode.
70
Scheduled Fuel Imbalance
0 (Zero)
71
Main Fuel Tanks Must Be Full If ___________
Center Tank has More Than 1,000 lbs In It
72
Anti-Skid INOP
Assumed Temperature Reduced Thrust Takeoff Is Not Permitted.
73
Brakes
Do Not Apply Until After Touchdown
