Limitations Flashcards
TAKEOFF AND LANDING WIND LIMITS
Maximum Takeoff Tailwind Component (AFM) 15 kts
Maximum Landing Tailwind Component (AFM) 15 kts
Maximum Operating Altitude (ft)
FL410
Maximum Takeoff and Landing Altitude (ft)
8400’
Minimum Takeoff and Landing Temperature
minus 54°C
Maximum Operating Limit Speed (AFM)
Observe VMO/MMO and Gear/Flap Placards
Severe Turbulence Penetration Target Speed
280 KIAS/.76M
What limitations is there for engine bleed air switches position for take off and landing?
Do not operate air conditioning packs in HIGH for takeoff, approach or landing.
AUTOPILOT USAGE limitations
Do not engage the autopilot below 1000 ft AGL on takeoff. (AFM/ASA)
For single channel operation during approach, the autopilot shall not remain engaged below 50 ft AGL. (AFM).
For manually flown HGS AIII approach, the autopilot shall not remain engaged below 500 ft AGL. Use of aileron trim with autopilot engaged is prohibited. (AFM)
ENGINES WARMUP and COOL DOWN limitation
3 minutes
ENGINE EGT (AFM) Maximum Time Limit for Takeoff Thrust
- 5 minutes
* 10 minutes allowed in the event of the loss of thrust on one engine during takeoff.
ENGINE EGT (AFM) Maximum Start EGT
725°
Starter Duty Cycle (normal start)
First attempt 2 minutes on
REVERSE THRUST is prohibited when(AFM)?
Intentional selection of reverse thrust in flight is prohibited.
APU LOAD Limitation (AFM)with both
Bleed and Electric Load
10,000ft
APU LOAD Limitation(AFM)
Bleed Only
17,000ft
APU LOAD Limitation(AFM)
Electric Only
FL410
APU LOAD Limitation(AFM)
Maximum Operating Altitude
FL410
APU LOAD (AFM) How long are you required to wait before applying bleed air load after APU start and how long are you required let APU ideal after bleed air is removed before shutdown the APU?
1 minute after start and for 1 minute prior to shutdown.
NOTE: (NG) When the APU switch is moved to OFF, this time delay is met automatically.
APU LOAD Limitation(AFM)
APU bleed valve may be open during engine start, but pilot must avoid what in this configuration?
avoid advancing engine power above idle.
APU LOAD Limitation(AFM)
Except for engine start, the APU bleed valve must be closed when?
another source is pressurizing the left bleed air duct.
FLAPS Limitation
What is the maximum flap extension altitude?
20,000 ft. (AFM)
NG) Holding in icing conditions with flaps extended is prohibited. (AFM
SPEED BRAKES limitations for deployment
with flaps extended
in flight below 1000 ft AGL
lever beyond the FLIGHT DETENT in flight. (AFM)
LOAD ALLEVIATION SYSTEM (700W/900ER)
Manually overriding the Load Alleviation System limitation
not authorized
FUEL
Minimum fuel temperature
-37°C unless actual fuel freeze point is known
FUEL
Allowable lateral imbalance between Main Tanks 1 and 2
must be scheduled to be zero. Random fuel imbalance must not exceed 1000 lbs for taxi, takeoff, flight or landing
FUEL
Main Wing Tanks must be scheduled to be full if…
if the Center Tank contains more than 1000 lbs
FUEL. CENTER TANK FUEL PUMPS
For ground operation, Center Tank FUEL PUMP switches must not be positioned to…
ON unless the Center Tank fuel quantity exceeds 1000 lbs, except when defueling or transferring fuel
FUEL. CENTER TANK FUEL PUMPS
Center Tank Fuel Pumps must not be ON unless…
personnel are available in the Flight Deck to monitor LOW PRESSURE lights
FUEL. CENTER TANK FUEL PUMPS
(NG) For ground and flight operations, the corresponding center tank fuel pump switch must be positioned OFF when?
the low pressure light illuminates. If the Center Tank is empty, position both Center Tank FUEL PUMP switches OFF
HYDRAULICS
Ground operation of electric hydraulic pump requires minimum of how much fuel in main tanks?
1675 lbs in respective fuel tank
