Limitations Flashcards
APU Bleed Air Valve must be closed when:
Can APU bleed air valve be open during engine start?
- Ground air connection and isolation valve open
- Engine No. 1 Bleed Air Valve open
- isolation and No. 2 Bleed Valves open
APU bleed air valve may be open during engine start, but avoid engine power above idle.
Maximum Takeoff and Landing Tailwind Component
10 knots
Avoid rapid and large alternating 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.
Maximum Takeoff and Landing Altitude
All except N5227A - 8,400 ft.
N5227A - 13,500 ft.
On revenue flights what must be installed?
Escape Slide Retention or GIRT bar.
During taxi, takeoff, landing.
N5227A - Auto-land capability may only be used to runways at or below _____.
8,400 ft. pressure altitude
Maximum and Minimum glide-slope angles for auto-land are ____
2.5° - 3.25°
Do not use LVL CHG on final approach below
1,000 ft. AFE
Do not use VHF-3 for ATC Communication with _____ operational.
ACARS operational.
Maximum Demonstrated Takeoff and Landing Crosswind
33 knots
Use of ____ radio is uused for primary ATC communications on the ground.
Where is that antenna located?
VHF - 1
Located on the top of the fuselage
Maximum Operating Altitude
41,000
For single channel operation during approach, the autopilot shall not remain engaged below _____.
50 ft. AGL
Maximum altitude with flaps extended
20,000 ft.
Maximum Speeds
Observe Vmo pointer and gear/flap placards.
Maximum time limit for takeoff thrust
5 minutes
N5167A, N5227A, N5233A, N5237A -
Flights predicated on use of the following HF frequencies are prohibited:
29.489 Mhz and 29.490 Mhz
ACARS is limited to transmission and receipt of messages that will not create unsafe conditions if message is improperly received such as:
- the message or parts of message are delayed or not received.
- the message is delivered to the wrong recipient
- the message content may be frequently corrupted.
Do not engage autopilot for takeoff below ____.
400 ft. AGL
Extended Engine Motorings:
Limited to 15 minutes for the first two extended engine motorings.
2 minutes needed between each attempt.
For the third and subsequent extended engine motorings, start usage is limited to 5 minutes. A minimum of 10 minutes is needed between each attempt.
Normal Starter Duty Cycle
2 minutes of starter usage
10 seconds needed in-between start attempts
Multiple consecutive start attempts are permitted.
Use of aileron trim with the autopilot engaged is ______.
Prohibited.
Maximum allowable on-the-ground altitude display differences for RVSM operations are:
Sea Level to 5,000 feet - 50
5,001 - to 10,000 feet - 60
Max difference between Captain or F/O and Field Elevation - 75 feet.
Maximum Wind Component for Autoland
Headwind - 25 kts
Crosswind - 20 kts
Crosswind CAT II/III - 15 kts
Tailwind - 10 kts
In flight do not extend SPEED BRAKE lever beyond
FLIGHT DETENT
After three consecutive aborted APU start attempts, what is required?
15 minute cooling period is required.
Engine and flap requirements for auto-land
Both engines operative
Flaps 30 or 40
APU Maximum Configuration Altitudes
APU Bleed + Electrical Load -
In Flight - 10,000
Ground Only - 15,000
APU Bleed - 17,000 ft.
APU Electrical Load - 41,000 ft.
Operation with assumed temperature reduced takeoff thrust is not permitted with:
Anti-Skid Inoperative
With either one or both engine bleed air switches ON, do not operate the air conditioning packs on HIGH for __.
Takeoff, approach, landing.
Except for the region between ____ and ____ West longitude, the maximum flight operating latitude is ____North, and the region between ____ East and ____ East longitude, the maximum flight operating altitude is ____ South.
Except for the region between 80° West and 130° West longitude, the maximum flight operating latitude is 70°North, and the region between 120°East and 160° East longitude, the maximum flight operating altitude is 60° South.
Engine ignition must be on (AUTO/CON) for:
- Takeoff
- Landing
- Anti-Ice Operation
- Operation in Heavy Rain
Severe Turbulent Air Penetration
280 KIAS / .76M whichever is lower.
Applicable to climb/descent only, during cruise refer to SP.16 Severe Turbulence Supplementary Procedure.
Maximum Taxi Weight Maximum Takeoff Weight Maximum Landing Weight Maximum Zero Fuel Weight Minimum Operating Weight
Maximum Taxi Weight - 174,700 Maximum Takeoff Weight - 174,200 Maximum Landing Weight - 146,300 Maximum Zero Fuel Weight - 138,300 Minimum Operating Weight - 80,800
N5227A - Do not use the autopilot below ___ ft. RA at pressure altitudes above ____ .
100 ft. RA
8,400 ft.
Maximum Cabin Differential Pressure (relief valves) is
9.1 PSI
Intentional selection of reverse thrust is prohibited:
In Flight
Maximum Flight Operational Latitude
82° North and 82° South
Engine limit display markings
RED - Minimum and Maximum limits
Amber - Caution Limits
Runway Slope
+/- 2%
Maximum allowable in-flight difference between Captain and First Officer altitude displays for RVSM operations is…
200 feet.
Holding in icing conditions is
Prohibited
Alternate Flap Duty Cycle
When extending or retracting flaps, allow 15 seconds after releasing the ALTERNATE FLAPS switch before moving switch again to avoid damage to the ALTERNATE FLAP motor.
After a complete extend and retract cycle of 0-15 and back to 0 allow 5 minutes for cooling before trying again.
Maximum Scheduled Fuel Imbalance is?
0 lbs.
The use of what fuel is prohibited?
JP-4 and JET B
Intentionally dry running the center tank fuel pump (low pressure light) is ____-
Prohibited
If a fuel pump circuit breaker trips can you reset it?
NO
What fuel is allowed?
JET A, JET A-1, JP-5 ,JP-8,
Avoid WX operation in what or around what?
- In a hangar
- within 50 feet of fuel operations or fuel spill
- when personnel are in the vicinity of the radome
What must not be operated during refueling operations?
HF Radios
Random lateral fuel imbalance is?
Taxi, T/O, Flight, Landing
1,000 lbs.
Inflight tank fuel temp must be what in flight?
MAX +49C
MIN 3C above freezing point of fuel to be used or -43C whichever is higher.
Minimum Oil Pressure
13
Maximum Altitude for APU Start
25,000
