JoeWinn 75/76 09 Flt Controls

Stab Trim LEVERS signal Stabilizer movement _____ and _____ conflicting trim commands

Stab Trim SWITCHES signal Stabilizer movement _____ and _____ conflicting trim commands
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Stab Trim LEVERS signal Stabilizer movement _____ and _____ conflicting trim commands

Stab Trim SWITCHES signal Stabilizer movement _____ and _____ conflicting trim commands
• Mechanically
• Override
• Electrically
• Neutralize

[9.10.5/9.10.3]
The Stabilizer Trim OFF Flag indicates the _____
• Trim Indicator is inop

[9.10.5/9.10.3]
A Stab Trim Cutout Switch in the CUTOUT Position will _____ to the _____
• Shut off the L/C/R Hydraulic System power
• Related Stab Trim Control Module

[9.10.5/9.10.3]
An illuminated STAB TRIM Light indicates the _____
• Stab Trim rate is 1/2 the normal Control Wheel Stab Trim Switch rate
•• (prob due to 1 of 2 Stab Trim Brakes failing to release)

[9.10.6/9.10.4]
An illuminated UNSCHED STAB TRIM Light indicates _____ or _____
• Uncommanded Stabilizer motion detected
•• (runaway or wrong way)
• Alt Trim is used with an A/P engaged

[9.10.6/9.20.4 & 9.20.6/9.20.7]
An illuminated MACH SPD TRIM Light only found on the _____ indicates the _____
• 757
• Mach/Speed Trim System is inop

[9.10.6]
Pushing both Aileron Trim Switches will move the _____ in the desired direction
• Control Wheel, Ailerons and Spoilers

[9.10.7/9.10.5]
An illuminated Yaw Damper INOP Light indicates the _____
• Yaw Damper is inop
•• (due to a controller failure)
• The Switch is OFF, or
• The IRS isn't aligned

[9.10.9/9.10.6 & Sys Study Guide]
With the Yaw Damper INOP Light not illuminated, the Yaw Damper won't work when there is _____
• No hydraulic pressure to the system

[Ground School Instructor]
An illuminated RUDDER RATIO Light indicates the _____ or _____
• Rudder Ratio System is failed
•• (due to a computer failure)
• Isn't receiving left Hyd Sys pressure

[9.10.9/9.10.7]
An illuminated Flight Control Shutoff OFF Light indicates the _____• Related Flight Control Valve is closed [9.10.10/9.10.7]On the ground, the Speedbrake Lever moves to DOWN and _____ if _____• All Spoiler Panels retract • Either T/L advanced to the T/O Position [9.10.12/9.10.9]On the ground, the Speedbrake Lever moves to UP and _____ if _____• All spoiler panels extend • Either Rev T/L raised to Rev Idle Detent [9.10.12/9.10.9]An illuminated SPOILERS Light indicates _____• One or more Spoiler Pairs not in the signaled position [9.10.12/9.10.9]An illuminated SPEED BRAKES Light indicates the _____Speedbrakes are extended when: • The Flaps are in a landing position, or • RA is 800' or below [9.10.12/9.10.10]On 757 Ships 5801-5816, the SPEED BRAKES Light will also illuminate due to _____• Speedbrakes extended with a T/L forward of Flight Idle for more than 15 seconds [9.10.12]On aircraft without Winglets, an illuminated AUTO SPD BRK Light indicates a _____• Fault in the Automatic Speedbrake System [9.10.12/9.10.9]On aircraft with Winglets, an illuminated AUTO SPD BRK Light indicates a _____ or a _____• Fault in the Automatic Speedbrake System • Fault in the Load Alleviation System [9.10.12/9.10.9]With an illuminated AUTO SPD BRK Light, if the Speedbrake Lever is ARMED, Speedbrakes may _____• Extend in flight if additional faults occur [9.10.12/9.10.9]With an illuminated AUTO SPD BRK Light, do not _____ and do not _____• Exceed 330 kts - 757 • Exceed 320 kts - 767 • Arm automatic Speedbrakes for landing [9.10.13/9.10.9]N: The AUTO SPD BRK Light may illuminate momentarily when the _____ after automatic deployment• S/B Handle is moved to the DOWN position •• (only in the 757 Vol II) [9.10.13]An illuminated 767 AIL LOCK Light indicates the _____• Aileron Lockout Actuator disagrees with the commanded position [9.10.9]The Slats will extend to the Mid-Range position when the Flap Lever is moved _____ and will remain in that position until the Flap Lever is moved _____• Out of UP • Out of 20 toward 25 or 30 [9.10.13/9.10.11]An illuminated TRAILING EDGE Light indicates _____• Flap disagree, • Flap asymmetry, or • Flap LRS not operating when required • F/Lever not in detent for ext per of time •• 767 only [9.10.16/9.10.15 & 9.20.13]An illuminated LEADING EDGE Light indicates _____• Slat disagree, or • Slat asymmetry [9.10.16/9.10.15]A Flap Indicator Needle between UP and 1 indicates the Slats are _____• Between Retracted and Mid-Range [9.10.17/9.10.15]A Flap Indicator Needle between UP and 1 indicates the Flaps are _____• Between Retracted and 1 on the 757 • UP on the 767 [9.10.17/9.10.15]The Alternate Flaps Selector ALTN position: • Arms the selected _____ • Shuts off hydraulic power to _____• LE Slat or TE Flap Alternate Drive Unit • Both Flap & Slat Drive Sys - 757 • Selected LE Slat/TE Flap Drive Sys - 767 [9.10.17/9.10.15]If a Jam occurs in a column or wheel, the Pilots can maintain control by _____ to overcome the jam• Applying force to the other column or wheel [9.20.1/9.20.2]Roll control is provided by _____ on the 757 and by _____ on the 767• 10 Spoilers & two Ailerons • 12 Spoilers & four Ailerons [9.20.2/9.20.3]The Elevator Feel System and Stabilizer are powered by the _____ Hydraulic Systems on the 757 and by the _____ Hydraulic Systems on the 767• Center & Right • Left & Center [9.20.5/9.20.6]The Electrical Trim Switches on the Control Wheel can be overriden by _____• Alternate Trim: •• Stab Trim Levers Override, and •• Stab Trim Switches Neutralize [9.20.5/9.20.6]Automatic Stabilizer Trim uses _____ and trims at _____• Only one Trim Control Module • 1/2 of the Electric or Alternate Trim rate [9.20.5/9.20.6]If a single Autopilot is engaged, Electric Trimming _____• Causes the A/P to disengage [9.20.6/9.20.7]If multiple Autopilots are engaged, the Electric Trim Switches _____• Are inhibited [9.20.6/9.20.7]Alternate Trimming does not cause _____• Autopilot disengagement [9.20.6/9.20.7]The pilot can quickly stop Uncommanded Stabilizer Trim changes by _____• Displacing the Control Column in the opposing direction [9.20.6/9.20.7]With an illuminated STAB TRIM Light, if the malfunction is unique to the Electric Trim Control, then the _____• Full Trim rate will be available using Alternate Trim [9.20.6/9.20.7]The 767 Pitch Enhancement System consists of a _____ driving a pump which uses _____ to operate the _____• Hydraulic motor in the Right System • Trapped Left Trim System fluid • Stabilizer [9.20.7]The 767 Pitch Enhancement System will activate automatically if _____ are _____• Both Left & Center Hyd Systems • Lost in flight [9.20.7]After the 767 Pitch Enhancement System activates, only _____ Trim will be available• Electric (Yoke) [9.20.7]After the 767 Pitch Enhancement System activates, _____ Trim will be inop• Alternate and Automatic [9.20.7]After the 767 Pitch Enhancement System activates, Electric (Yoke) Trim will operate at _____• Approximately 1/4 the normal rate [9.20.7]The Inboard Ailerons droop in conjunction with _____• Trailing Edge Flap extension [9.20.8]The 767 Aileron Lockout Control System permits full travel of the _____ at _____ and locks out the _____ at _____• Outboard Ailerons • Low speeds • Outboard Ailerons • High speeds [9.20.8]At high speeds, the 767 AIL LOCK Light may indicate that _____ failed to _____• One or both of the O/B Ailerons • Lock out [9.20.8]At low speeds, the 767 AIL LOCK Light may indicate that _____ failed to _____• One or both of the O/B Ailerons • Unlock [9.20.8]An illuminated RUDDER RATIO Light indicates the _____• Rudder Ratio System has failed [9.20.7/9.20.9]With an inop Rudder Ratio System, Rudder structural protection is provided by _____ of the _____ which limits rudder displacement at high airspeeds• Automatic depressurization • Left Hydraulic System Actuator [9.20.7/9.20.9]The Yaw Damper Systems improve _____• Turn coordination and dutchroll damping [9.20.7/9.20.9]During flight, Spoilers _____ are not used on the 757• Four & nine [9.20.8]On aircraft with Winglets, the Speedbrake Load Alleviation System will operate in flight under the following conditions: • Flaps _____ • GW > 221K/340K • Indicated airspeed > _____• Up • 330 knots in the 757 • 320 knots in the 767 [9.20./9.20.10]On aircraft with Winglets, if the Speedbrake Load Alleviation System begins to operate with the Speedbrake Lever beyond the 50-Percent position _____• It'll automatically move to the 50% position [9.20./9.20.10]On aircraft with Winglets, if the Speedbrake Load Alleviation System begins to operate with the Speedbrake Lever DOWN _____• Any attempt to move it past the 50% position will be restricted [9.20./9.20.10]On aircraft with Winglets, if the Speedbrake Load Alleviation System begins to operate, the Pilot may override the Speedbrake Lever restriction by _____• Applying additional force to the Lever [9.20./9.20.10]During landing, the Speedbrake Lever will move from ARMED to UP when the _____ and the _____• Landing Gear is fully on the ground •• Not tilted • Thrust Levers are at IDLE [9.20.9/9.20.11]On the ground when either Reverse Thrust Lever is moved to the Reverse Idle Detent, the Speedbrake Lever will _____• Drive to the UP position and extend Spoilers [9.20.9/9.20.11]On the ground, the Speedbrake Lever will drive to the UP position and extend Spoilers when _____• Either Reverse Thrust Lever is moved to the Reverse Idle Detent [9.20.9/9.20.11]Starting from Flaps UP, selection of Flaps 1 will result in Flaps _____• One on the 757, and • UP on the 767 [9.20.10/9.20.12]Flap Load Relief works for Flaps _____• 30 on the 757 and some 763s • 25 & 30 on all 76ERs and some 763s [9.20.11/9.20.12]For those 767 aircraft that have Load Relief for Flaps 25 and 30, exceeding the Flap Speed will result in the Flaps _____• Retracting to 20 wx they were at 30 or 25 [9.20.11/9.20.12]Autoslats will cause the Slats to go from _____ to _____ during _____ upon receiving a signal from the _____• Mid-Range • Fully Extended • Normal Flap/Slat operation • Stall Warning System [9.20.11]On the 757, when using the Alternate Flap Extension System, the Slats will move to the Fully Extended position when _____• Flaps 20 is selected •• (since no Autoslats in this mode) [9.20.11]During Alternate Flap Operation there will be no _____• Flap Load Relief • Autoslats (757) • TE Flap Asymmetry Protection on: •• All 757s, and •• Most 767s [9.20.11/9.20.13]Alternate Mode Flap & Slat Extension is limited to Flaps _____ with the Slats _____• 20 (procedurally) • Fully Extended on the 757, and • Mid-Range on the 767 [9.20.11/9.20.13]Selecting the Alternate Flaps ALTN LE or TE Switch will render the Flap Lever useless on the _____• 757 [9.20.11]Hydraulic power to both Slats and Flaps is automatically shut off with the illumination of a _____ Light on the _____• LEADING EDGE or TRAILING EDGE • 757 [9.20.11 & 12]After Selecting the Alternate Flaps ALTN LE or TE Switch on the 767, the Flap Lever will continue to operate the _____• Non-selected LE or TE Subsystem [9.20.13]On the 767, an illuminated LEADING EDGE or TRAILING EDGE Light will result in automatic Hydraulic power shutoff on the _____• Associated LE or TE Subsystem only [9.20.13 & 14]When the HDG is supplying electrical power, hydraulic flow to the Slats and Flaps is reduced, resulting in _____• Increased Slat and Flap operation time [9.20.12 & 14]There is no Cockpit indication of a failure of the Mach Trim System on _____ aircraft• 767 [Vol I DF.20.3]There is no Autoslat System on the _____ aircraft• 767 [CBT]The Elevator Feel System is active when the Flaps are _____ on the 757 and when the Flaps are _____ on the 767• Up or down • Only up [Handout]The Elevator Feel System is inhibited when the _____ or when _____• Autopilot is engaged • Using Electric or Alternate Trim [Handout]The Elevator Feel System compensates for _____ and improves _____• Mach tuck • Stability during airspeed changes [Handout]Elevator Feel consists of a Mach/Speed Trim System on the 757 and a _____ on the 767• Mach Trim Mode only [Systems Study Guide]Flight Control Trim System Power: • Rudder _____ • Aileron _____ • Elevator/Stab _____• Electric • Electric • Center & Right Hyd - 757 • Left & Center Hyd - 767 [Ground School Instructor]The Yaw Dampers will be inop until the _____• IRSs are aligned [Ground School Instructor]