Flight Controls and Automation

AIL DEFLECT DISAG

AIRCRAFT ON GROUND

IF IN AIR, SKIP TO AILERON DEFLECT OVRD SWITCH OPERATIVE

1. CONTACT MAINTENANCE

Contact maintenance for aircraft repairs.

NOTE

An attempt to clear the alert may be attempted on the ground by placing the FLAP/SLAT handle to UP/RET then back to the planned takeoff position. Should this clear the alert, no further crew action is required.

[END OF AIL DEFLECT DISAG CHECKLIST]

AILERON DEFLECT OVRD SWITCH OPERATIVE

IF AILERON DEFLECT OVRD SWITCH IS INOPERATIVE, SKIP TO STEP 8

1. AILERON DEFLECT OVRD SWITCH - OVRD ON

Set Aileron deflect ovrd switch to the OVRD ON position.

Push the AILERON DEFLECT OVRD switch and observe OVRD ON light illuminates.

2. AIRSPEED - MAX 255 KIAS / .51 MACH

Monitor airspeed ensuring it does not pass the max of 255 KIAS or .51 MACH.

3. FLAP / SLAT HANDLE - 10 / EXT

Set the FLAP / SLAT HANDLE to the 10 / EXT position.

4. FLAP / SLAT HANDLE - 0 / EXT

Set the FLAP / SLAT HANDLE to the 0 / EXT position.

5. AILERON DEFLECT OVRD SWITCH - OFF

Set Aileron deflect ovrd switch to the OFF position.

Push the AILERON DEFLECT OVRD switch and observe OVRD ON light extinguishes.

NOTE

The use of the AILERON DEFLECT OVRD switch is limited to one cycle.

AIL DEFLECT DISAG ALERT EXTINGUISHED

IF AIL DEFLECT DISAG ALERT IS STILL DISPLAYED, SKIP TO STEP 7

When desired,

6. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SLAT Handle to the UP / RET position.

Make log entry.

[END OF AIL DEFLECT DISAG CHECKLIST]

When desired,

7. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SLAT Handle to the UP / RET position.

NOTES

Do not exceed 280 KIA / .82 Mach
Do not use FMS fuel computations for flight planning.
Fuel consumption may be increased up to 20%.
Diversion to a suitable airport may be required.
Plan a normal FLAP/SLAT landing.
After landing, Subject Captain's Discretion (SCD), leave flaps in landing position to assist in determining which aileron remains deflected.
Do not use autoland.
Disconnect the autopilot by 200 feet AGL.
Make log entry.

[END OF AIL DEFLECT DISAG CHECKLIST]

8. AIRSPEED - MAX 255 KIAS / .51 MACH

Monitor airspeed ensuring it does not pass the max of 255 KIAS or .51 MACH.

9. FLAP / SLAT HANDLE - 10 / EXT

Set the FLAP / SLAT HANDLE to the 10 / EXT position.

10. FLAP / SLAT HANDLE - 0 / EXT

Set the FLAP / SLAT HANDLE to the 0 / EXT position.

AIL DEFLECT DISAG ALERT EXTINGUISHED

IF AIL DEFLECT DISAG ALERT IS STILL DISPLAYED, SKIP TO STEP 12

When desired,

11. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SLAT Handle to the UP / RET position.

Make log entry.

[END OF AIL DEFLECT DISAG CHECKLIST]

When desired,

12. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SLAT Handle to the UP / RET position.

NOTES

Do not exceed 280 KIA / .82 Mach
Do not use FMS fuel computations for flight planning.
Fuel consumption may be increased up to 20%.
Diversion to a suitable airport may be required.
Plan a normal FLAP/SLAT landing.
After landing, Subject Captain's Discretion (SCD), leave flaps in landing position to assist in determining which aileron remains deflected.
Do not use autoland.
Disconnect the autopilot by 200 feet AGL.
Make log entry.

[END OF AIL DEFLECT DISAG CHECKLIST]

FCC 1 / 2 FAULT

1. FIRST OFFICER'S EIS SOURCE SELECTOR - AUX (OR 1)

Move the First Officer's EIS source selector to AUX (OR 1)

FCC 1 / 2 DATA FAULT ALERT EXTINGUISHED

IF ALERT IS STILL PRESENT, SKIP TO AIRCRAFT ON GROUND

No further crew action required.

[END OF FCC 1 / 2 FAULT CHECKLIST]

AIRCRAFT ON GROUND

IF AIRCRAFT IS IN AIR, SKIP TO STEP 3

3. CONTACT MAINTENANCE

Contact maintenance for aircraft repairs.

[END OF FCC 1 / 2 FAULT CHECKLIST]

4. FIRST OFFICER'S EIS SOURCE SELECTOR - ORIGINAL POSITION

Move the First Officer's EIS source selector to it's original position.

Select appropriate procedure below.

NOTE

During the following actions, the associated LSAS and YAW DAMP OFF light(s) will illuminate, but "LSAS RIGHT OUTBD / LEFT OUTBD / RIGHT INBD / LEFT INBD OFF" and "YAW DAMP LWR A / LWR B / UPR A / UPR B OFF" alert(s) will not be displayed.

FCC 1A DATA FAULT

1. LSAS RIGHT OUTBD SWITCH - OFF

Move the LSAS RIGHT OUTBD switch to the OFF position

2. LWR YAW DAMP A SWITCH - OFF

Move the LWR YAW DAMP switch to the OFF position.

[END OF FCC 1A DATA FAULT CHECKLIST]

FCC 1B DATA FAULT

1. LSAS LEFT INBD SWITCH - OFF

Move the LSAS LEFT INBD switch to the OFF position

2. LWR YAW DAMP B SWITCH - OFF

Move the LWR YAW DAMP B switch to the OFF position.

[END OF FCC 1B DATA FAULT CHECKLIST]

FCC 2A DATA FAULT

1. LSAS LEFT OUTBD SWITCH - OFF

Move the LSAS LEFT OUTBD switch to the OFF position

2. IPR YAW DAMP A SWITCH - OFF

Move the UPR YAW DAMP A switch to the OFF position.

[END OF FCC 2A DATA FAULT CHECKLIST]

FCC 2B DATA FAULT

1. LSAS RIGHT INBD SWITCH - OFF

Move the LSAS RIGHT INBD switch to the OFF position

2. UPR YAW DAMP B SWITCH - OFF

Move the UPR YAW DAMP B switch to the OFF position.

[END OF FCC 2B DATA FAULT CHECKLIST]

FLAP DISAG

Place FLAP / SLAT handle to match flap position. Allow several seconds for system response. If alert remains displayed select the last symmetrical configuration.

PROBLEM WAS ASYMMETRIC FLAPS

IF PROBLEM WAS NOT ASYMMETRIC FLAPS, SKIP TO ALERT APPEARED DURING ATTEMPTED FLAP RETRACTION

Land at nearest suitable airport using existing flap/slat setting

If final flap setting is zero, Perform Abnormal Non-alert procedure - NO FLAP/SLAT EXTENDED LANDING.

If final flap setting is less than 35°,

1. GPWS SWITCH - FLAP OVRD

Set the GPWS switch to the FLAP OVRD position.

2. AUTOBRAKES - OFF

Set the autobrakes to the OFF position.

Wait until at 50 feet RA

3. AUTOTHROTTLES - OFF

Set the autothrottles to the OFF position.

[END OF FLAP DISAG CHECKLIST]

ALERT APPEARED DURING ATTEMPTED FLAP RETRACTION

IF ALERT DID NOT APPEAR DURING FLAP RETRACTION, SKIP TO STEP 7

Land at nearest suitable airport

If flaps now less then 50°, further extension may be attempted if desired.

NOTE

If after selecting a greater flap setting, flaps do not move as selected, place FLAP/SLAT handle to match actual flap position.

If final flap setting is less than 35°,

4. GPWS SWITCH - FLAP OVRD

Set the GPWS switch to the FLAP OVRD position.

5. AUTOBRAKES - OFF

Set the autobrakes to the OFF position.

Wait until at 50 feet RA

6. AUTOTHROTTLES - OFF

Set the autothrottles to the OFF position.

[END OF FLAP DISAG CHECKLIST]

7. AIRSPEED - REDUCE

Reduce airspeed to minimum maneuver speed displayed on PFD.

NOTE

During the next step, FLAP/SLAT handle forces will be higher than normal.

Place FLAP/SLAT handle to 50/EXT, then return handle to desired position. Allow several seconds for system response. (This action may allow flaps to reset to normal operation.)

FLAPS EXTEND AS DESIRED

IF ALERT DID NOT APPEAR DURING FLAP RETRACTION, SKIP TO RETURN FLAP / SLAT HANDLE TO MATCH ACTUAL POSITION

No further crew action is required.

Return FLAP/SLAT handle to match actual flap position.

FLAP POSITION 0 DEGREES

IF FLAP POSITION IS NOT 0 DEGREES, SKIP TO LAND WITH EXISTING FLAP / SLAT SETTING.

Refer to Abnormal Non-Alert procedure - NO FLAP/SLAT EXTENDED LANDING.

[END OF FLAP DISAG CHECKLIST]

Land with existing flap/slat setting.

If final flap setting is less than 35°,

8. GPWS SWITCH - FLAP OVRD

Set the GPWS switch to the FLAP OVRD position.

9. AUTOBRAKES - OFF

Set the autobrakes to the OFF position.

Wait until at 50 feet RA

10. AUTOTHROTTLES - OFF

Set the autothrottles to the OFF position.

[END OF FLAP DISAG CHECKLIST]

FLIGHT CONTROLS JAMMED OR RESTRICTED

NOTES

If jam occurs during manually controlled flight, attempt to engage autopilot.
If freezing water is the cause, control may be regained by descending into warmer air.

1. SEAT BELT SWITCH - ON

Set the SEAT BELT switch to the ON position.

AILERON CONTROLS JAMMED OR RESTRAINED

IF AILERON CONTROLS ARE NOT JAMMED OR RESTRAINED, SKIP TO ELEVATOR CONTROLS JAMMED OR RESTRICTED

If jam was detected during cruise, and if aircraft control is adequate, continue to normal descent point.

NOTE

Some lateral control may be available through the control wheel position sensors of Roll Control Wheel Steering.

If controls remain jammed or restricted:

2. AUTOPILOT / AUTOTHROTTLES - DISCONNECT

DISCONNECT Both the autopilot and autothrottles.

3. MAXIMUM AIRSPEED - 290 KIAS / .80 MACH

Monitor max airspeed ensuring no to pass 290 KIAS / .80 MACH.

4. CONTROL WHEELS (ROLL AXIS) - SEPARATE / DISCONNECT

SEPARATE / DISCONNECT the control wheels on the roll axis.

Use force as required to separate/disconnect the two halves of the control system (approximately 90 pounds, 41kg).

NOTES

Autothrottles will be available.
Autopilot may be available, but should be disconnected during descent and approach and landing.
Select a runway with minimum crosswind.
If roll authority is reduced, fly a wider pattern than normal to allow a stabilized approach.

[END FLIGHT CONTROLS JAMMED OR RESTRICTED CHECKLIST]

ELEVATOR CONTROLS JAMMED OR RESTRICTED

IF ELEVATOR CONTROLS ARE NOT JAMMED OR RESTRICTED, SKIP TO RUDDER JAMMED OR RESTRICTED

If jam was detected during cruise, and if aircraft control is adequate through use of the autopilot, consider continuing to normal descent point.

If controls remain jammed or restricted, and pitch is not controllable:

5. AUTOPILOT / AUTOTHROTTLES - DISCONNECT

DISCONNECT Both the autopilot and autothrottles.

6. MAXIMUM AIRSPEED - 290 KIAS / .80 MACH

Monitor max airspeed ensuring no to pass 290 KIAS / .80 MACH.

Apply force as necessary to free jam.

NOTES

Autothrottles will be available.
Autopilot may be available.
Elevator authority may be reduced.

[END FLIGHT CONTROLS JAMMED OR RESTRICTED CHECKLIST]

RUDDER JAMMED OR RESTRICTED

IF RUDDER IS NOT JAMMED OR RESTRICTED, SKIP TO END FLIGHT CONTROLS JAMMED OR RESTRICTED CHECLIST

Use rudder trim (if available) and ailerons for directional control.

If rudder input is not possible, use operative flight controls, trim, and thrust as required to maintain aircraft control.

NOTES

Select a runway with minimum crosswind.
The possibility of limited directional control with a wing engine inoperative should be considered prior to executing a missed approach.

7. AUTOBRAKE SELECTOR - OFF

Set the autobrake selector to the OFF position.

NOTES

Rudder pedal steering is inoperative.
If directional control is a concern, use differential braking at high speed.
Nose gear steering wheel may be used as speed decreases.

[END FLIGHT CONTROLS JAMMED OR RESTRICTED CHECKLIST]

LSAS ALL FAIL

1. AUTOPILOT - DISCONNECT

DISCONNECT the autopilot.

2. LSAS SWITCHES - OFF

Move all LSAS switches to the OFF position.

3. ANY ONE LSAS SWITCH - ON

Move a singular LSAS switch to the ON position.

ASSOCIATED LSAS FAIL LIGHT ILLUMINATED

IF LSAS FAIL LIGHT DOES NOT ILLUMINATE, SKIP TO THE SECTION SAYING ATTEMPT TO RESTORE

4. ASSOCIATED LSAS SWITCH - OFF

Move the associated LSAS switch to the OFF position.

Attempt to restore remaining LSAS channels by pushing any one LSAS switch on and observe its FAIL light. Any LSAS switch that illuminates FAIL should be pushed to OFF prior to pushing next switch.

ANY LSAS CHANNEL OPERATIVE

IF ALL LSAS CHANNELS ARE INOPERATIVE, SKIP TO LSAS IS INOPERATIVE AUTOPILOT IS NOT AVAILABLE.

5. Attempt to reengage autopilot.

Attempt to reengage the autopilot.

NOTE

Autopilot requires an operative inboard LSAS channel.

[END OF LSAS ALL FAIL CHECKLIST]

LSAS is inoperative. Autopilot is not available.

NOTE

Pitch rate damper, pitch protection and positive nose lowering will not be available.

Pitch sensitivity increases with altitude, avoid overcontrolling.

Also avoid pitch attitudes above 7 degrees during landing.

[END OF LSAS ALL FAIL CHECKLIST]

SEL ELEV FEEL MANF

SEL FADEC ALTN AND/OR SEL FLAP LIM OVRD AND/OR IAS CMPARATOR MONITOR ALERTS ARE ALSO DISPLAYED

IF THE ILLUMINATED ALERT DOES NOT MATCH THE MENTIONED ALERTS, SKIP TO STEP 2

1. REFER TO EMERGENCY NON-ALERT PROCEDURE - AIRSPEED: LOST, SUSPECT OR ERRATIC

Refer to Emergency Non-Alert Procedure - Airspeed: Lost, Suspect or Erratic.

[END OF SEL ELEV FEEL MANF CHECKLIST]

2. ELEV FEEL SELECTOR - MANUAL

Set the ELEV FEEL SELECTOR to the MANUAL position.

3. ELF SPEED - SET AS REQUIRED

Set the ELF SPEED as is required.

NOTES

When ELEV FEEL is in MANUAL, ELF speed is displayed on CONFIG synoptic.
Slew ELF reference speed bug to maintain approximate agreement with aircraft indicated airspeed.

[END OF SEL ELEV FEEL MANF CHECKLIST]

SEL FLAP LIM OVRD

NOTE

FLAP LIMIT MANUAL light will be illuminated.

SEL FADEC ALTN AND/OR SEL FLAP LIM OVRD AND/OR IAS CMPARATOR MONITOR ALERTS ARE ALSO DISPLAYED

IF THE ILLUMINATED ALERT DOES NOT MATCH THE MENTIONED ALERTS, SKIP TO STEP 2

1. REFER TO EMERGENCY NON-ALERT PROCEDURE - AIRSPEED: LOST, SUSPECT OR ERRATIC

Refer to Emergency Non-Alert Procedure - Airspeed: Lost, Suspect or Erratic.

[END OF SEL FLAP LIM OVRD CHECKLIST]

2. FLAP LIMIT SELECTOR - OVRD 1

Set the FLAP LIMIT SELECTOR to the OVRD 1 position.

3. WAIT 20 SECONDS

Wait 20 seconds.

FLAP LIMIT DISAG ALERT DISPLAYED

IF FLAP LIMIT DISAG ALERT IS NOT DISPLAYED, SKIP TO OBSERVE PLACARDED FLAP LIMIT SPEED

4. FLAP LIMIT SELECTOR - OVRD 2

Set the FLAP LIMIT SELECTOR to the OVRD 2 position.

FLAP LIMIT DISAG ALERT DISPLAYED

IF FLAP LIMIT DISAG ALERT IS NOT DISPLAYED, SKIP TO OBSERVE PLACARDED FLAP LIMIT SPEED

Flap extension may be limited.

[END OF SEL FLAP LIM OVRD CHECKLIST]

Observe placarded flap limit speed.

[END OF SEL FLAP LIM OVRD CHECKLIST]

SLAT DISAG

ALERT APPEARED DURING CLIMOUT WITH SLATS EXTENDED AND FLAP / SLAT HANDLE IN A SLAT EXTENDED POSITION

IF ALERT DID NOT APPEAR DURING CLIMOUT WITH SLATS EXTENDED AND FLAP / SLAT HANDLE IN A SLAT EXTENDED POSITION, SKIP TO AIRSPEED ABOVE 280 KIAS / .55 MACH

Stick shaker may actuate temporarily.

If flaps greater than 10°, retract flaps to 10°.

Accelerate and retract flaps and slats on schedule.

CAUTION

Anticipate “SLAT DISAG” alert to appear during extension. Utilize “ALERT APPEARED DURING ATTEMPTED EXTENSION” decision point in this procedure.

AIRSPEED ABOVE 280 KIAS / .55 MACH

IF AIRSPEED IS NOT ABOVE 280 KIAS / .55 MACH, SKIP TO ALERT APPEARED DURING ATTEMPTED EXTENSION

1. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SET handle into the UP / RET position.

[END OF SLAT DISAG CHECKLIST]

ALERT APPEARED DURING ATTEMPTED EXTENSION

IF ALERT DID NOT APPEAR DURING ATTEMPTED EXTENSION, SKIP TO STEP XX

SLATS INHIBITED ALERT DISPLAYED ON SD CONFIG SYNOPTIC

IF SLATS INHIBITED ALERT DID NOT DISPLAY ON SD CONFIG SYNOPTIC, SKIP TO STEP 3

2. FLAP / SLAT HANDLE - 10 / EXT OR GREATER

Set the FLAP / SET handle into the 10 / EXT or greater position.

SLATS DISAG ALERT REMOVED

IF SLATS DISAG ALERT WAS NOT REMOVED, SKIP TO STEP 3

Plan a normal flap / slat landing.

[END OF SLAT DISAG CHECKLIST]

3. FLAP / SLAT HANDLE - UP / RET

Set the FLAP / SET handle into the UP / RET position.

4. SLAT STOW SWITCH - SLAT STOW

Set the SLAT STOW switch into the SLAT STOW position.

5. FLAP / SLAT HANDLE - 0 / EXT

Set the FLAP / SLAT handle into the 0 / EXT position.

6. GPWS SWITCH - FLAP OVRD

Set the GPWS switch into the FLAP OVRD position.

APPROACH ASPECTS

Use normal descent and approach checklist.
Plan a 28/RET landing.

7. LANDING DISTANCE (28 / RET) - MULTIPLY BY 1.4

After calculating estimated landing distance multiply it by 1.4.
Calculate V_APP using 28/RET V_REF table unless flaps do not extend as desired. Tables for 15/RET and 25/RET are included for reference

15/RET REFERENCE SPEEDS

Weight (1000 Kg)	160	170	180	190	200	210	220	230
V_REF	176	181	187	192	197	202	207	212

25/RET REFERENCE SPEEDS

Weight (1000 Kg)	160	170	180	190	200	210	220	230
V_REF	171	176	181	186	191	195	200	205

28/RET REFERENCE SPEEDS

Weight (1000 Kg)	160	170	180	190	200	210	220	230
V_REF	175	180	185	190	194	199	204	209

LANDING ASPECTS

Do not use autothrottles below 50 feet RA.
Cross threshold at V_APP and reduce sink rate slightly.
Retard throttles to idle and raise nose of aircraft to at least a level attitude.
Do not hold aircraft off. Excessive flare will result in float and excessive use of runway.

CAUTION

Tail strike may occur at pitch attitudes greater than 10°.

ROLL-OUT ASPECTS

Autospoilers will not deploy until nose gear touchdown.

GO-AROUND ASPECTS

Rotate initially to 15°, then adjust pitch to maintain speed. Clean up procedure: Initially flaps 10. When passing VREF + 20, FLAP/SLAT Handle UP/RET.

QRH LANDING CHECKLIST

[END OF SLAT DISAG CHECKLIST]

8. FLAP / SLAT HANDLE - 0 / EXT

Set the FLAP / SLAT handle into the 0 / EXT position.

Plan a normal flap / slat landing.

[END OF SLAT DISAG CHECKLIST]

STAB OUT OF TRIM

Observe stabilizer position on CONFIG synoptic for proper autotrim.

NO INDICATION OF TRIM RESPONSE AFTER 5 SECONDS

If indication of trim response after 5 seconds, skip to END OF STAB OUT OF TRIM CHECKLIST.

To counteract any abrupt pitching tendencies, firmly grasp control wheel.

1. AUTO FLIGHT SWITCH - PUSH

PUSH the auto flight switch.

STABILIZER FAILS TO MOVE

IF STABILIZER MOVES, SKIP TO NO FURTHER CREW ACTION REQUIRED

To counteract any abrupt pitching tendencies, firmly grasp control wheel.

2. AUTOPILOT - DISCONNECT

Disconnect the autopilot.

Trim aircraft using control wheel trim switches or LONG TRIM handles.

STABILIZER FAILS TO MOVE

IF STABILIZER MOVES, SKIP TO NO FURTHER CREW ACTION REQUIRED

3. REFER TO ABNORMAL NON-ALERT PROCEDURE - STABILIZER INOPERATIVE

Refer to Abnormal Non-Alert procedure - STABILIZER INOPERATIVE.

[END OF STAB OUT OF TRIM CHECKLIST]

No further crew action required.

[END OF STAB OUT OF TRIM CHECKLIST]

STABILIZER INOPERATIVE

AIRCRAFT IN TRIM WITH LANDING FLAPS SET

IF AIRCRAFT IS NOT IN TRIM WITH LANDING FLAPS SET, SKIP TO STEP 1

Land with existing flap / slat setting.

[END STABILIZER INOPERATIVE CHECKLIST]

1. ELEV FEEL SELECTOR - PULL, ROTATE AS NECESSARY

PULL the ELEV FEEL SELECTOR and rotate as necessary.

Slew elevator feel reference speed on CONFIG synoptic page to desired speed. Update as required.

SLATS AVAILABLE

IF SLATS ARE NOT AVAILABLE, SKIP TO PLAN A 28 / RET APPROACH AND LANDING

Plan a 35 / EXT approach and landing.

Determine stabilizer inoperative speed additive from following table and add to V_APP, not to exceed V_REF + 25.

STABILIZER INOPERATIVE SPEED ADDITIVE 35/EXT

STABILIZER SETTING (DEG)	CENTER OF GRAVITY (% MAC)
	12	14	16	18	20	22	23-24
	SPEED ADDITIVE (KIAS)
1 AND	20	20	17	12	8	5	0
0	20	16	12	7	5	0	0
1 ANU	16	11	7	5	0	0	0
2 ANU	11	7	5	0	0	0	0
3 ANU	7	5	0	0	0	0	0
4 ANU	5	0	0	0	0	0	0
5 to 16 ANU	0	0	0	0	0	0	0

NOTES

If stabilizer and/or CG is unknown, add 20 knots to normal VAPP, not to exceed VREF + 25.
Landing distance will increase approximately 1% for each 1 knot added to VREF.

Maintain adjusted V_APP until touchdown.

NOTE

If go-around is required, use normal procedure, but do not allow speed to go below adjusted VAPP.

[END STABILIZER INOPERATIVE CHECKLIST]

Plan a 28 / RET approach and landing.

2. GPWS SWITCH - FLAP OVRD

Move the GPWS switch to the FLAP OVRD position.

APPROACH ASPECTS

Use Normal Descent and Approach Checklist.

3. LANDING DISTANCE (FOR 28 / RET) - MULTIPLY BY 1.4

Multiply aircraft landing distance by a factor of 1.4.

28/RET APPROACH SPEEDS

Weight (1000 Kg)	160	170	180	190	200	210	220	230
V_REF	170	175	180	185	189	194	199	204

LANDING ASPECTS

Do not use autothrottle below 50 feet RA.
Cross threshold at VAPP, reduce sink rate slightly.
Retard throttles to idle and raise nose to at least a level attitude.
Do not hold aircraft off. Excessive flare will result in float and excessive use of runway.

CAUTION

Tail strike may occur at pitch angles greater than 10º.

ROLL-OUT ASPECTS

Autospoilers will not deploy until nose gear touchdown.

GO-AROUND ASPECTS

Initial rotation to 15°, then adjust pitch to maintain speed.
Do not allow airspeed to go below adjusted VAPP.
Clean up procedure:
- Initially Flaps 10.
- When passing V_MIN + 20, Flap/Slat Handle UP/RET.

QRH LANDING CHECKLIST

[END STABILIZER INOPERATIVE CHECKLIST]

YAW DAMP ALL FAIL

1. YAW DAMP SWITCHES - ALL OFF

Set all YAW DAMP switches to the OFF position.

2. ANY ONE YAW DAMP SWITCH - ON

Set a singular YAW DAMP switch to the ON position.

ASSOCIATED YAW DAMP FAIL LIGHT ILLUMINATE

IF ASSOCIATED YAW DAMP FAIL LIGHT DOES NOT ILLUMINATE, SKIP TO ATTEMPT TO RESTORE

3. ASSOCIATED YAW DAMP SWITCH - OFF

Set the associated YAW DAMP switch to the OFF position.

Attempt to restore remaining yaw damp channels by pushing any one YAW DAMP switch ON and observing its FAIL light. Any YAW DAMP switch that illuminates FAIL should be pushed to OFF prior to pushing next switch.

[END OF YAW DAMP ALL FAIL CHECKLIST]

USE MAN SPOILERS

1. LANDING DISTANCE - MULTIPLY BY 1.1

Nultiply the calculated landing distance by a factor of 1.1.

2. AT NOSE GEAR TOUCHDOWN - DEPLOY SPOILERS

When the nose gear touches down deploy the spoilers.

NOTE

The pitch rate damper, pitch protection and positive nose lowering may not be available.

[END OF USE MAN SPOILERS CHECKLIST]

NO FLAP / SLAT EXTENDED LANDING

Reduce gross weight as desired.

1. GPWS SWITCH - FLAP OVRD

Move the GPWS switch to the FLAP OVRD position

2. AUTO BRAKE SELECTOR - OFF

Move the autobrake selector to the OFF position.

APPROACH ASPECTS

1. LANDING DISTANCE - MULTIPLY BY 1.2

Multiply aircraft landing distance by a factor of 1.2.
Plan a wide pattern for speed stabilization on final.
Pitch attitude in level flight approximately 10°.

0/EXT APPROACH SPEEDS

Weight (1000 Kg)	160	170	180	190	200	210	220	230
V_APP (V_REF + 15)	167	172	176	181	185	189	193	197

NOTE

Speeds are VREF + 15 to preclude tail strike.

LANDING ASPECTS

Do not use autothrottle below 50 feet RA.
Cross threshold at V_APP, reduce sink rate slightly
Retard throttles to idle and fly to a positive touchdown.
Do not attempt to achieve a smooth touchdown. Excessive flare will result in float and excessive use of runway.

CAUTION

Tail strike may occur at pitch attitudes greater than 10°.

ROLL OUT ASPECTS

On touchdown, positively lower nose gear to runway and immediately apply full reverse thrust and brakes as required.
Spoilers will not deploy until nose gear touchdown.
Full reverse may be used to a complete stop. In this case make log entry.

QRH LANDING CHECKLIST

[END NO FLAP / SLAT EXTENDED LANDING FAIL CHECKLIST]

Flight Controls and Automation

On this page