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AA 737 Limitations Flashcards

1
Q

Intentional selection of thrust reversers in flight is _______

A

Prohibited

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2
Q

Do not engage the autopilot for takeoff below _______

A

500 feet AGL

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3
Q

Do not operate Weather Radar near _________, or within _________

A

Fuel Spills

50 ft of people

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4
Q

Max Headwind/Crosswind for HUD CAT II OR CAT III approach

A

Headwind 25 kts

Crosswind 15 kts

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5
Q

Intentional running of center tank fuel pump (low pressure light illuminated) is _________

A

Prohibited

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6
Q

The deadbolt position allowing access with a key is to be used ______ ______ ______ only.

A

On the ground

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7
Q

Transmitting Personal Electronic Devices (T-PED) are not approved for use forward of the flight deck door during _______________.

A

Any phase of flight

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8
Q

Random Fuel Imbalance must not exceed ________ for taxi, takeoff, flight, or landing.

A

1000 lbs

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9
Q

If one HF radio is selected for transmission, _______ the other HF radio on all audio select panels to prevent audio interference.

A

Deselect

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10
Q

Lateral fuel imbalance between main tanks 1 and 2 must be scheduled to be ________

A

Zero

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11
Q

The use of Fuel System icing inhibitor additives ______ ______
change the minimum fuel tank temperature limit

A

Does not

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12
Q

Max Crosswind on Narrow (less than 148ft) Runway

A

20 kts

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13
Q

Avoid rapid and large _________ control inputs, especially in combination with large changes in pitch, roll, or yaw as they may result in structural failure at any speed, including below Va

A

Alternating

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14
Q

27K thrust may not be selected or requested through ACARS if the TPS is ______________________
SNA operations are not part of this limitation.

A

Based on any other Thrust Rating

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15
Q

Max Crosswind with Visibility less than 3/4 (RVR 4000)

A

15 kts

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16
Q

Engine Anti-ice must be on during all ground and flight operations when icing conditions exist or are anticipated, except during climb or cruise when the temperature is below _______

A

-40 C SAT

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17
Q

Max altitude for APU Bleed + Electrical Load

A

10,000 ft

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18
Q

Use of dual channel autopilot for approach is ______

A

Prohibited

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19
Q

When extending or retracting with the ALTERNATE FLAPS position switch, allow ________ after releasing the switch before moving the switch again to avoid damage to the Alternate Flap motor clutch

A

15 Seconds

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20
Q

Autopilot to minimums is required for approaches with an RNP value of ________ unless adequate visual references is established.

A

RNP 0.3

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21
Q

Do not operate Wing Anti-ice on the ground when the OAT is above
_________

A

10 C (50 F)

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22
Q

With Engine Bleed Air Switches ON, do not operate the air conditioning packs in HIGH for ______, ______, or ______

A

Takeoff, Approach, or Landing

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23
Q

APU Bleed Valve may be open during engine start, but avoid

_____________________

A

Engine power above idle

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24
Q

Main fuel tanks 1 and 2 must be full if center tank contains more than _______

A

1000 lbs

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25
Icing Conditions Exist when....
OAT on the ground or for takeoff, or TAT in flight is 10C (50F) or below and: - Visible moisture in any form is present (such as clouds, fog with visibility of one mile or less, rain, snow, sleet, and ice crystals), or... - When operating on ramps, taxiways, or runways where surface snow, ice, standing water, or slush may be ingested by the engines or freeze on the engines or nacelles.
26
What is the maximum airspeed allowable on the final approach segment of an RNAV/RNP approach?
180 kts
27
Max Tailwind for Landing
10 kts* *Ops engineering will compute special data for 15 kt TW for select airports
28
On revenue flights, the escape slide retention bar (girt bar) must be inserted in the brackets on all doors during _____, _____, & _____
Taxi, Takeoff, & Landing
29
After 3 consecutive aborted start attempts a ____________ cooling period is required
15 minute
30
Do not use EGPWS terrain display for __________
Navigation
31
Operation with assumed temperature reduced takeoff thrust is not permitted with _________
Anti-skid Inoperative
32
The following limitations apply with the EEC's in Alternate Mode - _____________________ - _____________________ - _____________________ - _____________________
- Both EEC's must be in Alternate Mode - 26K max (27K If planned) T/O thrust must be used - Do not use the FMC takeoff N1or QRH V-speeds - Use of Auto-throttle for takeoff is prohibited.
33
Maximum Takeoff Weight
174,200 lbs (NG) 181,200 lbs (MAX)
34
Maximum altitude for unpressurized flight, following an in-flight depressurization is ______. This altitude may be exceeded when terrain clearance requirements dictate.
14,000 ft
35
Severe Turbulence Speed
280kts/.76M
36
Exceptions to Maximum Flight Latitudes
Between 80W & 130W........70N Between 120E & 160E........60S
37
Maximum Allowable in-flight difference between CA and FO altimeters for RVSM operations is __________
200 ft
38
Normal operating range of the Engine Limit Display Markings is marked by __________
A white arc
39
Any time passengers are on board prior to airplane movement, at least one _____ _____ _____ must be open or armed
Floor Level Exit
40
The Maximum on-the-ground difference between the CA and FO altimeters for RVSM operations is _______ (from sea level to 5000 ft) _______ (from 5000 ft to 10,000)
50 feet 60 feet
41
Max Operating Altitude
41,000 ft
42
27K operations will be authorized for use by _______ and may only be selected if it is specified on the Load Agent generated ______
Dispatch TPS
43
Maximum allowable on-the-ground difference between CA or FO altimeters and Field Elevation for RVSM operations is ______
75 ft
44
Accomplish a pre-flight check of the Reinforced Flight Deck Door and Flight Deck Access System prior to the _____ _____ of the day.
First Flight
45
APU Bleed Valve must be closed when... - _________________________ - _________________________ - _________________________
- Ground air is connected and Isolation Valve is open - Engine #1 Bleed Valve is open - Isolation Valve and Engine #2 Bleed Valves are open
46
The EGPWS "TERR INHIBIT" switch should be selected within 15 nm of an airfield under the following conditions - _________________________ - _________________________
- Operations to/from runways not in the EGPWS database | - Specific approach procedures previously identified as potentially producing false terrain alerts
47
Use of aileron trim with the autopilot engaged is ______
Prohibited
48
In flight, do not extend the Speed Brake Lever beyond the _________ detent
FLIGHT
49
Do not deploy the Speed Brakes in flight at Radio Altitudes less than _____________
1000 feet
50
Max altitude for APU bleed air
17,000 feet
51
If DC Bus 2 is unpowered, place the ______ ______ switch in ______, and use the deadbolt in the ______ ______ _______ position to lock the door.
- POWER CUTOFF - OFF - LOCKED KEY INOPERABLE
52
Max Crosswind with Braking Action Medium (Fair)
20kts
53
Air Data Inertial Reference Unit (ADIRU) alignment must not be attempted at latitudes greater than ___________
78 degrees, 15 minutes
54
Maximum Flight Operating Latitude
82N/82S
55
Do not rely on airframe visual icing cues to turn engine anti-ice on. Delaying the use of engine anti-ice until ice buildup is visible from the cockpit may result in ______ ______ ______
Severe engine damage
56
Max Demonstrated Crosswind
33 kts (NG) 32 kts (MAX)
57
GPS updating must be disabled for approach operation when operating ________________________ , if the FMC database and charts are not referenced to _________ reference datum, unless other appropriate procedures are used.
Outside of the United States National Airspace WGS-84
58
Do not apply brakes until______
After Touchdown
59
Runway Slope Limits
+/- 2%
60
Maximum Taxi Weight
174,700 lbs (NG) 181,700 lbs (MAX)
61
Normal access to the flight deck will be accomplished as specified under Normal Procedures. Use of the access code is considered an ______ ______ request (except prior to departure, when flight deck crew may be required to enter access code to gain entry to the flight deck.)
Emergency Access
62
Maximum Takeoff and Landing Altitude
8,400 ft
63
Maximum Cabin Differential Pressure (system relief)
9.1 psi
64
What is the minimum RNP value authorized for RNAV/RNP approaches.
RNP 0.11
65
Maximum Fuel Tank Temperature
49 C
66
Maximum Speeds
Observe all placards and instrument red lines. .82/340 kts. (Mmo/Vmo)
67
Use of the Head Up Display (HUD) with an inoperative ________ is prohibited
Number 1 Radio Altimeter
68
Maximum altitude when an aircraft is DISPATCHED for unpressurized flight is _____
10,000 ft
69
Max Altitude for APU Electrical Loading
41,000 feet
70
Cautionary range of Engine Limit Display Markings is marked by ____________
An amber arc
71
Engine Ignition must be ____ when operating in icing conditions.
On
72
Max Tailwind for Takeoff
15 kts
73
Maximum Landing Weight
146,300 lbs (NG) 152,800 lbs (MAX)
74
``` Engine ignition must be used for _________ _________ _________ _________ ```
- Takeoff (AUTO or CONT) - Landing (AUTO or CONT) - Anti-ice (AUTO or CONT) - Operation in heavy rain (CONT)
75
After a complete extend/retract cycle (0-15/15-0) using the ALTERNATE FLAPS position switch, allow ______ cooling before attempting another extension
5 minutes
76
Ballast Fulel is _____________
Not Authorized
77
Engine Anti-ice must be on prior to and during ______ in all icing conditions, including temperatures below -40 C SAT
Descent
78
Maximum Altitude with Flaps Extended
20,000 feet
79
The Integrated Standby Flight Display (ISFD) must be initialized in accordance with ______ ______
Approved Procedures
80
Minimum tank fuel temperature prior to takeoff and in-flight
-43 C, or 3 C above the fuel freezing point temperature limit, whichever is higher
81
The _______ _______ does not meet the accuracy requirements of RVSM airspace
Standby Altimeter
82
On B737 aircraft with 160 passenger seat configuration, the maximum aircraft capacity is limited to _____ seated occupants for all overwater flights requiring life rafts. This includes all required flight crew, passengers, observers and non-working crew members. Infants and other children not occupying a seat are not counted towards this limitation.
168
83
Max Crosswind with Braking Action Poor
10 kts
84
Pilots are authorized to deviate from __________ to the extent necessary to comply with an EGPWS warning
An ATC Clearance
85
Crews will be notified of runways/airports not contained in the EGPWS database via ____ Pilot Alert Messages, and/or Dispatch Release __________
F4 Remarks
86
Verify that an ______ ______ of the flight deck door access system has been accomplished according to approved procedures once each ______ ______
Operational Check Flight Day
87
Do not operate HF radios during _______ _______
Refueling operations
88
Maximum Zero Fuel Weight
138,300 lbs (NG) 145,400 lbs (MAX)
89
Holding in icing conditions with flaps extended is __________
Prohibited
90
Maximum and minimum Engine Limit Display Markings are marked by __________
A red line
91
For single channel operation during approach, the autopilot shall not be remain engaged below _______
50 ft AGL
92
Minimum oil quantity for Engine Start? NG________ Max_______
NG(3AA-3PX) 12 qts | Max (3RA-3VM) 17 qts
93
Backing the aircraft using reverse thrust is________
Prohibited

Boeing 737 (2 decks)

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