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• ELEVATOR SPLIT .................................................ABNORM 8−16
ABNORM 8-1
REV 69, Jun 04/07
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
Lightning Strike
Following a lightning strike, failure of the stall protection
system may occur without an associated indication to the crew.
Failure of the stall protection system must be assumed.
(1) STALL PROT, PUSHER
(either left or right) ................................................................ OFF
Prior to landing:
(2) Approach speed ...........................................................VREF + 10
minimum, to maintain margin above stall.
(3) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.40 (40%) 1.30 (30%)
END
STALL FAIL
STALL FAIL
(1) STALL PROT, PUSHER
(either left or right) ................................................................ OFF
Accompanied by nuisance shaker operation and/or warbler
aural warning:
Yes
(2) Affected STALL PROT, L CH
or R CH cbs (1N5 or 4C5) ......................................... OPEN
No
Prior to landing:
(2) Approach speed .......................................................... VREF + 10
minimum, to maintain margin above stall.
(3) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.40 (40%) 1.30 (30%)
END
ABNORM 8-2
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
ALT COMP FAIL
ALT COMP FAIL
NOTE
The stick pusher may be inoperative. One or both channels
of the stick shaker will remain operative.
Prior to landing:
(1) Approach speed ...........................................................VREF + 10
minimum.
(2) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.40 (40%) 1.30 (30%)
END
FLT SPLRS
FLT SPLRS
On ground:
(1) Do not take off.
END
FLT SPLRS DEPLOY
FLT SPLRS DEPLOY
(1) FLIGHT SPOILER lever ..............................................RETRACT
END
Flight Spoilers Failure to Deploy
........Flight spoilers cannot be deployed.
(1) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.30 (30%) 1.25 (25%)
END
ABNORM 8-3
REV 74, Nov 07/08
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
Flight Spoilers Lever Jam
........Flight spoilers cannot be retracted.
(1) Approach speed ...........................................................VREF + 10
minimum.
(2) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.50 (50%) 1.40 (40%)
END
Flight Spoiler Asymmetric Extension
........Uncommanded roll during flight spoiler extension.
(1) FLIGHT SPOILER lever ..............................................RETRACT
Do not reselect in flight.
(2) Runway ..........................................................................SELECT
to minimize crosswind.
(3) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
WITHOUT THRUST
REVERSERS
WITH THRUST
REVERSERS
1.30 (30%) 1.25 (25%)
END
ABNORM 8-4
REV 66, Feb 01/07
QUICK REFERENCE HANDBOOK
PSP 604-15
FLIGHT CONTROLS
MALFUNCTIONS
Flight Spoiler Asymmetric Retraction
........Uncommanded roll during flight spoiler retraction.
(1) Lateral control...........................................................ESTABLISH
using ailerons and rudder, if necessary.
(2) FLIGHT SPOILER lever ...............................RETRACT/ADJUST
to eliminate roll.
(3) Runway ..........................................................................SELECT
to minimize crosswind.
(4) Approach speed ...........................................................VREF + 10
minimum.
(5) Actual landing distance ............................................. INCREASE
as applicable by factor given below:
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