FCOM 9

Stab trim is powered by _____ hydraulics. Left and centre. Left and right. Left. Right and centre.

Speed Breaks light (amber) means speed brake is extended.... Below 800RA. With flaps in landing position. Below 800RA with flaps in landing position. Below 800RA or flaps in landing position.

Flap gate positions are. 1 and 20. 5 and 20. 1 and 25. 5 and 15.

Alternate flaps are used. Flap 1 to 20. Flap 5 to 20. Flap 1 to 30. Flap UP to 20.

There are ____ spoilers. 12. 6. 8. 10.

Roll control is provided by. Four ailerons and 12 spoilers. Four ailerons, two inboard and two outboard. Two ailerons and 12 spoilers. Four ailerons and six spoilers.

Aileron lockout locks out the _____ ailerons at ____ speed. Outboard, high. Outboard, low. Inboard, high. Inboard, low.

The airplane has _____ and _____ spoilers. 8 outboard, 4 inboard. 6 outboard, 4 inboard. 4 outboard, 8 inboard. 4 outboard, 2 inboard.

Each wing has _____ and _____ spoilers. 8 outboard, 4 inboard. 6 outboard, 4 inboard. 4 outboard, 8 inboard. 4 outboard, 2 inboard.

Outboard spoilers are powered by (out>in)... LRCC. RLCC. CCRL. CCLR.

Outboard ailerons are powered by ____ hydraulic systems. LR. LC. RC. LRC.

Inboard spoilers and ailerons are powered by. LRCC/CCRL. LCCL/RCCR. LRCC/RCCR. LCCL=CCRL.

Elevator is powered by. LR. LC. RC. LRC.

Rudder is powered by. LR. LC. RC. LRC.

There are _____ modes of stabilizer trim. 1. 2. 3. 4.

Stab trim can be. Electric, alternate, automatic. Electric, alternate, manual. Alternate, automatic, manual. Electric, automatic, manual.

Electric trim can trim nose down up to _____, beyond which _____ must be used. 1.5, alternate. 2.0, alternate. 1.5, automatic. 2.0, automatic.

Automatic trim is controlled by. Autopilot. Mach speed trim system. Autopilot or Mach speed trim system.

Electric trimming with a single autopilot engaged will cause, _____ and with multiple autopilot engaged will cause ______. Autopilot disconnect, nothing the switches are inhibited. Autopilot disconnect, autopilot disconnect. Nothing the switches are inhibited, nothing the switches are inhibited. Nothing the switches are inhibited, autopilot disconnect.

Alternate trimming causes autopilot disengagement. False. True.

Alternate trimming does not cause autopilot disengagement. False. True.

Pitch enhancement system (PES) consists of a hydraulic motor in the _____ system using trapped ____ trim system fluid to operate the stabiliser. Right, left. Right, centre. Centre, right. Left, right.

PES will activate automatically if. Left and centre systems are lost. Left and right systems are lost. Centre and right systems are lost.

STAB TRIM EICAS means. Trim operates at 1/2 rate. Trim operates at 1/4 rate. Trim operates at normal rate. Trim operates at 1/3 rate.

Automatic. Trim operates at 1/2 rate. Trim operates at 1/4 rate. Trim operates at normal rate. Trim operates at 1/3 rate.

PES. Trim operates at 1/2 rate. Trim operates at 1/4 rate. Trim operates at normal rate. Trim operates at 1/3 rate.

As airpseed increases, rudder ratio _____ rudder inputs to _____ rudder deflection. Reduce, reduce. Reduce, increase. Increase, increase. Increase, reduce.

As airpseed decreases, rudder ratio _____ rudder inputs to _____ rudder deflection. Reduce, reduce. Reduce, increase. Increase, increase. Increase, reduce.

Rudder ratio provides structural protection by depressurising the _____ actuator at _____ speeds. Left, high. Left, low. Centre and right, high. Centre and right, low.

Speedbrake load alleviation system (if installed) operates when. Flaps are UP, WGT >340, IAS >320. Flaps are out, WGT >340, IAS >320. Flaps are UP, WGT >320, IAS >320. Flaps are out, WGT >340, IAS >320.

Speedbrake load alleviation system deactivates when. WGT<339 or IAS<315. WGT<340 or IAS<320. WGT<320 or IAS<315. WGT<320 or IAS<340.

Flap load relief system will automatically retract to _____ when the flap placard speed is exceeded at flap ______. F20, F25 or F30. F20, F30. F20, F25. F25, F30.

Disagree (LE/TE) means. Does not agree with commanded position, hydraulic power is removed. Has not extended symmetrically, hydraulic power is not removed. Does not agree with commanded position, hydraulic power is not removed. Has not extended symmetrically, hydraulic power is removed.

Asymmetry (LE/TE) means. Does not agree with commanded position, hydraulic power is removed. Has not extended symmetrically, hydraulic power is not removed. Does not agree with commanded position, hydraulic power is not removed. Has not extended symmetrically, hydraulic power is removed.

When the HDG is supping electrical power. Hydraulic flow is reduced, increasing operating time. Hydraulic flow is increased, increasing operating time. Hydraulic flow is reduced, reducing operating time. Hydraulic flow is increased, reducing operating time.