Non Critical Procedures
What are the two systems that comprise the FCAS?
Engine Failure Assist System (EFAS) and a full time Series Yaw Damper (SYD)
If all means of flap synchronization fail and conditions permit, initiate ______ and land as soon as possible.
Initiate Fuel Dumping (3-215)
0-200 psi (3-229)
With EFAS inoperative, VMCG can increase by as much as ____?
25 KIAS (3-215)
How many degrees of outboard flaps have to be cranked down before the full outboard ailerons become available?
At least 23 degrees (3-234)
If the flap indicators and visual inspection reflect symmetric main flap alignment but a rolling moment is present, what type of flap malfunction is indicated?
Fillet Flap Malfunction (3-215)
If rudder pedals moved when the unscheduled rudder deflection occurred, the fault is probably within the _____?
PCU, or a mechanical failure occurred. Either way, do not restore power to powered rudder (3-232)
What is the normal wheel force required to overcome the autopilot for Block 45?
50 pounds. 25 pounds for Block 40 (3-214)
Alternating the lowering of the inboard and outboard flaps, what is the maximum degree differential we want to see?
5 degrees, starting with outboard flaps (3-234)
When landing with a differential flap configuration, use the pattern, approach, and threshold speeds for which flap setting?
Minimum flap setting indicated (3-216)
When landing with normal right hydraulic system pressure and rudder power inoperative or low rudder hydraulic pressure, will rudder pedal nose wheel steering work?
Yes, but increased rudder pedal is required due to manual rudder operation. Be prepared to use the tiller as the aircraft slows (3-221).
How many degrees is the maximum yaw damper authority limited to for rudder deflection to counteract any yaw induced by a SYD failure?
4 Degrees (3-233, Yaw Damper Malfunction)
For full 50 degrees of flap extension, how many turns are required on each set of flaps if manually lowering?
405 turns (3-235)
If leading edge flaps are not extended, how many knots should be added to approach and threshold speeds?
6 Knots (3-217)
Manual damping of dutch roll shall be accomplished with what control inputs?
Aileron inputs. Do not attempt to damp dutch roll manually with rudder. (3-228)
What is the difference between the yellow TRIM annunciation and the red TRIM annunciation when the autopilot is engaged (B45)?
Red Trim means the AP processor has detected a problem in the trim feedback loop, and is no longer commanding stabilizer trim movements. Yellow means it is reaching the torque limit. (3-214)
Hydraulic Snubbers prevent damage to flight controls on the ground up to _____ knots
65 Knots (1-480)
When Landing with less than 20* Flaps, what is the -1 caution with lower approach and threshold speeds and abnormally nose high conditions?
The Tail section might contact the runway (3-217)
When a control difficulty (roll or yaw) due to suspected aileron malfunction is encountered, what is the minimum safe altitude per the -1?
10,000 AGL. (3-214)
If a known cable failure has occurred, lateral control from spoilers and partial aileron control would be lost on one side. A minimum approach and threshold speed of ___ should be maintained?
150 IAS (3-214). If more than 5 knots of crosswind, threshold speed should be increased 1.7 knots for each knot of crosswind component