# Textron Aviation Multi-Engine Service Bulletin MEB-27-02: Revision 1

- Rights: © Textron Aviation Inc. Filed by the FAA in regulations.gov docket FAA-2016-8992; AD 2016-17-08 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Textron Aviation Multi-Engine Service Bulletin MEB-27-02](https://openairdocs.org/service-documents/cessna/meb27-02.md)
- Title as filed: MEB-27-02 Revision 1 Flight Controls - Elevator Trim-Tab Push-Pull Tube Hardware Replacement
- Pages: 12
- PDF: https://openairdocs.org/files/sha256/68/50/685084814101d0fb252832a0aec3092d07305717894aba6ef462226d913cb628
- Page: https://openairdocs.org/service-documents/cessna/meb27-02/file/685084814101

## Text

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### Page 1

Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
REVISION
TRANSMITT
AL
This
sheet
transmits
Revision
1
to
MEB
-
27
-
02
,
which:
A.
Makes
changes
within
the
Accomplishment
Instructions
Section
to
provide
additional
details.
B.
Adds
additional
hardware
to
the
Material
Information
Section
for
alternate
bolt
grip
length
and
washers
for
correct
cotter
pin
alignment.
NOTE:
This
revision
replaces
the
original
issue
of
MEB
-
27
-
02
in
it's
entirety
.
REVISION
COMPLIANCE
NO
EFFECT
.
Airplanes
previously
modified
by
this
service
bulletin
are
not
af
fected
by
this
revision.
LOG
OF
REVISIONS
Original
Issue
February
29
,
2016
Revision
1
June
15
,
2016
Original
Issue
-
February
29
,
2016
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
1
of
1
T
extron
A
viation
Customer
Service
,
P
.O.
Box
7706
,
Wichita
,
KS
67277
,
U.S.A.
1
-
316
-
517
-
5800
COPYRIGHT
©
2016

### Page 2

(No text on this page.)

### Page 3

Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
TITLE
FLIGHT
CONTROLS
-
ELEV
A
T
OR
TRIM
-
T
AB
PUSH
-
PULL
TUBE
HARDW
ARE
REPLACEMENT
EFFECTIVITY
The
following
Cessna
Aircraft
Models
(all
serial
numbers):
310
thru
310R
,
E310H
,
E310J
,
310J
-
1
,
T310P
thru
T310R
320
thru
320F
,
320
-
1
335
340
,
340A
401
thru
401B
402
thru
402C
41
1
,
41
1A
414
,
414A
421
thru
421C
REASON
T
o
replace
the
hardware
securing
the
elevator
trim
tab
push
-
pull
tube
to
the
elevator
trim
tab
actuator
and
the
elevator
trim
tab
horn.
DESCRIPTION
This
service
bulletin
provides
instructions
to
replace
the
hardware
connecting
the
elevator
trim
tab
push
-
pull
tube
to
the
elevator
trim
actuator
and
elevator
trim
tab.
COMPLIANCE
MANDA
T
OR
Y
.
This
service
bulletin
must
be
accomplished
at
the
next
100
-
hour
or
12
-
month
(annual
-
type)
inspection
,
whichever
occurs
first.
NOTE:
A
general
visual
inspection
for
correct
installation
and
security
of
the
elevator
trim
tab
push
-
pull
tube
connecting
hardware
and
an
inspection
for
tab
deflection
(free
play)
shall
be
completed
during
each
subsequent
100
-
hour
or
12
-
month
(annual)
type
inspection
after
the
accomplishment
of
this
service
bulletin.
The
general
visual
inspection
should
check
all
elevator
trim
actuator
and
elevator
trim
tab
horn
to
push
-
pull
tube
connection
hardware
for
condition
,
corrosion
,
cracking
,
security
,
cotter
pin
installation
for
proper
safety
,
and
the
elevator
and
elevator
trim
system
for
uninterrupted
,
proper
operation
through
the
full
travel
of
the
elevator
and
elevator
trim
tab
surfaces
(pitch
up
/
pitch
down
and
nose
up
/
nose
down
trim
respectively).
Perform
the
elevator
trim
tab
deflection
(free
play)
check
per
the
applicable
maintenance
or
service
manual.
A
service
bulletin
published
by
Cessna
Aircraft
Company
may
be
recorded
as
"completed"
in
an
aircraft
log
only
when
the
following
requirements
are
satisfied:
1)
The
mechanic
must
complete
all
of
the
instructions
in
the
service
bulletin
,
including
the
intent
therein.
2)
The
mechanic
must
correctly
use
and
install
all
applicable
parts
supplied
with
the
service
bulletin
kit.
Only
with
written
authorization
from
Cessna
Aircraft
Company
can
substitute
parts
or
rebuilt
parts
be
used
to
replace
new
parts.
Original
Issue
-
February
29
,
2016
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
1
of
8
T
extron
A
viation
Customer
Service
,
P
.O.
Box
7706
,
Wichita
,
KS
67277
,
U.S.A.
1
-
316
-
517
-
5800
This
document
contains
technical
data
and
is
subject
to
U.S.
export
regulations.
This
information
has
been
exported
from
the
United
States
in
accordance
with
export
administration
regulations.
Diversion
contrary
to
U.S.
law
is
prohibited.
ECCN:
9E991
COPYRIGHT
©
2016

### Page 4

MEB
-
27
-
02
Page
2
Revision
1
-
June
15
,
2016
Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
3)
The
mechanic
or
airplane
owner
must
use
the
technical
data
in
the
service
bulletin
only
as
approved
and
published.
4)
The
mechanic
or
airplane
owner
must
apply
the
information
in
the
service
bulletin
only
to
aircraft
serial
numbers
identified
in
the
"Ef
fectivity"
section
of
the
bulletin.
5)
The
mechanic
or
airplane
owner
must
use
maintenance
practices
that
are
identified
as
acceptable
standard
practices
in
the
aviation
industry
and
governmental
regulations.
No
individual
or
corporate
organization
other
than
Cessna
Aircraft
Company
is
authorized
to
make
or
apply
any
changes
to
a
Cessna
-
issued
service
bulletin
,
service
letter
,
or
flight
manual
supplement
without
prior
written
consent
from
Cessna
Aircraft
Company
.
APPROV
AL
Cessna
received
F
AA
approval
for
the
technical
data
in
this
publication
that
changes
the
airplane
type
design.
WEIGHT
AND
BALANCE
INFORMA
TION
Negligible
REFERENCES
F
AA
Advisory
Circular
AC43.13
-
1B
Applicable
Cessna
Model
Maintenance
or
Service
Manual
PUBLICA
TIONS
AFFECTED
Applicable
Cessna
Model
Illustrated
Parts
Catalog
ACCOMPLISHMENT
INSTRUCTIONS
1.
Prepare
the
airplane
for
maintenance.
A.
Make
sure
that
the
airplane
is
electrically
grounded.
B.
Make
sure
that
all
switches
are
in
the
OFF
/
NORM
position.
C.
Disconnect
electrical
power
from
the
airplane.
(1)
Disconnect
the
airplane
battery
.
(2)
Disconnect
external
electrical
power
.
D.
Attach
maintenance
warning
tags
to
the
control
columns
and
elevator
trim
wheel
that
have
"DO
NOT
MOVE
ELEV
A
T
OR
TRIM
T
AB
MAINTENANCE
IN
PROGRESS"
written
on
them.
2.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Get
access
to
the
connecting
hardware
for
the
elevator
trim
tab
actuator
rod
end
to
push
-
pull
tube
and
the
push
-
pull
tube
to
elevator
trim
tab
horn.
3.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Remove
the
nut
,
washer
and
bolt
from
the
elevator
trim
tab
actuator
to
push
-
pull
tube
connection.
A.
Discard
the
removed
hardware.
CAUTION:
Use
of
the
correct
cotter
pin
,
part
number
MS24665
-
132
,
is
critical
in
this
installation.
Use
of
a
different
cotter
pin
could
result
in
the
hardware
becoming
loose.
Cotter
pins
must
not
be
reused.
NOTE:
Any
fit
problems
may
be
correctable
by
cleaning
out
the
debris
in
the
internal
hole
surface
of
the
bearing
and
/
or
the
clevis
or
by
replacement
of
the
rod
or
bearing
if
corrosion
or
damage
dictates
the
parts
cannot
be
used
as
is.

### Page 5

Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
4.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
NAS464P3
-
8
Bolt
,
NAS1
149F0332P
W
asher
,
MS17826
-
3
Nut
and
MS24665
-
132
Cotter
Pin
in
the
elevator
trim
tab
actuator
rod
end
to
push
-
pull
tube
connection
as
follows:
NOTE:
The
bolt
grip
length
may
be
adjusted
to
the
next
longer
grip
length
(NAS464P3
-
9)
to
permit
proper
installation
of
the
castellated
nut
and
cotter
pin.
This
may
require
extra
washers
(NAS1
149F0316P
and
/
or
NAS1
149F0332P)
for
proper
alignment
of
the
castellated
nut
cotter
pin
slot
and
the
cotter
pin
hole
in
the
bolt.
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolt.
A.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
NAS464P3
-
8
Bolt
in
the
elevator
trim
tab
actuator
rod
end
to
push
-
pull
tube
connection
in
the
orientation
(i.e.
,
bolt
head
inboard
or
outboard)
which
yields
the
greatest
clearance
with
the
spar
web
cut
-
out
and
any
other
structures.
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolt.
B.
Install
the
NAS1
149F0332P
W
asher
and
MS17826
-
3
Nut
onto
the
NAS464P3
-
8
Bolt.
C.
T
orque
the
MS17826
-
3
Nut
12
Inch
-
Pounds
,
if
a
castellation
of
the
nut
does
not
align
with
the
cotter
pin
hole
in
the
bolt
,
continue
tightening
to
the
next
alignment
position
up
to
20
Inch
-
Pounds.
D.
Make
sure
a
minimum
of
one
full
bolt
thread
is
protruding
from
the
castellated
nut.
E.
Install
the
MS24665
-
132
Cotter
Pin.
5.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Remove
the
nut
,
washer
and
bolt
from
the
elevator
trim
actuator
push
-
pull
tube
to
elevator
trim
tab
horn.
A.
Discard
the
removed
hardware.
CAUTION:
Use
of
the
correct
cotter
pin
,
part
number
MS24665
-
132
,
is
critical
in
this
installation.
Use
of
a
different
cotter
pin
could
result
in
the
hardware
becoming
loose.
Cotter
pins
must
not
be
reused.
NOTE:
Any
fit
problems
may
be
correctable
by
cleaning
out
the
debris
in
the
internal
hole
surface
of
the
bearing
and
/
or
the
clevis
or
by
replacement
of
the
rod
or
bearing
if
corrosion
or
damage
dictates
the
parts
cannot
be
used
as
is.
6.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
NAS464P3
-
8
Bolt
,
NAS1
149F0332P
W
asher
,
MS17826
-
3
Nut
and
MS24665
-
132
Cotter
Pin
in
the
elevator
trim
tab
actuator
push
-
pull
tube
to
elevator
trim
tab
horn
connection
as
follows:
NOTE:
The
bolt
grip
length
may
be
adjusted
to
the
next
longer
grip
length
(NAS464P3
-
9)
to
permit
proper
installation
of
the
castellated
nut
and
cotter
pin.
This
may
require
extra
washers
(NAS1
149F0316P
and
/
or
NAS1
149F0332P)
for
proper
alignment
of
the
castellated
nut
cotter
pin
slot
and
the
cotter
pin
hole
in
the
bolt.
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolt.
A.
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
NAS464P3
-
8
Bolt
in
the
push
-
pull
tube
to
elevator
trim
tab
horn.
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolt.
B.
Install
the
NAS1
149F0332P
W
asher
and
MS17826
-
3
Nut
onto
the
NAS464P3
-
8
Bolt.
C.
T
orque
the
MS17826
-
3
Nut
12
Inch
-
Pounds
,
if
a
castellation
of
the
nut
does
not
align
with
the
cotter
pin
hole
in
the
bolt
,
continue
tightening
to
the
next
alignment
position
up
to
20
Inch
-
Pounds.
D.
Make
sure
a
minimum
of
one
full
bolt
thread
is
protruding
from
the
castellated
nut.
E.
Install
the
MS24665
-
132
Cotter
Pin.
7.
Check
the
elevator
and
elevator
trim
system
for
uninterrupted
,
proper
operation
through
the
full
travel
of
the
elevator
and
elevator
tim
tab
surfaces
(pitch
up
/
pitch
down
and
nose
up
/
nose
down
respectively).
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
3

### Page 6

MEB
-
27
-
02
Page
4
Revision
1
-
June
15
,
2016
Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
W
ARNING:
If
there
is
any
increased
friction
or
interference
felt
during
full
yoke
travel
from
full
pitch
up
through
full
pitch
down
,
and
full
elevator
trim
travel
from
full
nose
up
through
full
nose
down
do
not
proceed
any
further
until
the
source
of
the
interference
or
increased
friction
has
been
determined
and
resolved.
8.
Make
sure
the
elevator
trim
tab
deflection
(free
-
play)
is
within
the
limits
specified
in
the
applicable
Maintenance
or
Service
Manual
and
adjust
as
necessary
.
(Refer
to
the
applicable
Maintenance
or
Service
Manual.)
9.
Make
sure
the
elevator
trim
tab
rigging
is
within
the
limits
specified
in
the
applicable
Service
/
Maintenance
Manual
and
adjust
as
necessary
.
(Refer
to
the
applicable
Maintenance
or
Service
Manual.)
10.
Operate
the
elevator
trim
tab
through
the
full
travel
of
nose
up
and
nose
down
and
while
the
elevator
trim
tab
and
elevator
are
moving
,
do
a
general
visual
inspection
that
there
is
no
interference
between
any
of
the
areas
that
follow:
•
between
the
elevator
trim
tab
actuator
rod
end
to
elevator
trim
tab
actuator
push
-
pull
tube
bolt
head
and
the
elevator
spar
web
material
•
between
the
elevator
trim
tab
horn
to
elevator
trim
tab
actuator
push
-
pull
tube
bolt
head
or
nut
and
the
cutout
in
the
lower
elevator
skin
•
between
any
other
connection
hardware
and
the
elevator
spar
web
material
•
between
any
other
connection
hardware
and
the
cutout
in
the
spar
web
•
between
any
other
connection
hardware
and
the
cutout
in
the
elevator
skin
•
between
any
moveable
parts
and
other
potential
interference
A.
If
there
is
not
suf
ficient
clearance
or
if
there
is
interference
at
the
elevator
front
spar
web
,
record
the
orientation
of
the
elevator
trim
tab
actuator
rod
end
to
elevator
trim
tab
actuator
push
-
pull
tube
bolt
head
and
other
connection
hardware.
(1)
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Disconnect
the
elevator
trim
tab
actuator
rod
end
to
elevator
trim
tab
actuator
push
-
pull
tube
connecting
hardware.
(a)
Discard
the
cotter
pin.
(2)
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
NAS464P3
-
8
Bolt
in
the
elevator
trim
tab
actuator
rod
end
to
push
-
pull
tube
connection
in
the
orientation
opposite
to
how
it
was
removed.
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolt.
(3)
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
previously
removed
W
asher(s)
and
MS17826
-
3
Nut
onto
the
NAS464P3
-
8
Bolt.
(4)
T
orque
the
MS17826
-
3
Nut
12
Inch
-
Pounds
,
if
a
castellation
of
the
nut
does
not
align
with
the
cotter
pin
hole
in
the
bolt
,
continue
tightening
to
the
next
alignment
position
up
to
20
Inch
-
Pounds.
(5)
Make
sure
a
minimum
of
one
full
bolt
thread
is
protruding
from
the
castellated
nut.
(6)
(Refer
to
Figure
1
,
Sheet
1
and
Sheet
2.)
Install
the
MS24665
-
132
Cotter
Pin.
B.
(If
adjustments
to
the
hardware
were
made.)
Operate
the
elevator
trim
tab
through
the
full
travel
of
nose
up
and
nose
down
and
while
the
elevator
trim
tab
and
elevator
are
moving
,
do
a
general
visual
inspection
that
there
is
no
interference
between
any
of
the
areas
that
follow:
•
between
the
elevator
trim
tab
actuator
rod
end
to
elevator
trim
tab
actuator
push
-
pull
tube
bolt
head
and
the
elevator
spar
web
material
•
between
the
elevator
trim
tab
horn
to
elevator
trim
tab
actuator
push
-
pull
tube
bolt
head
or
nut
and
the
cutout
in
the
lower
elevator
skin
•
between
any
other
connection
hardware
and
the
elevator
spar
web
material
•
between
any
other
connection
hardware
and
the
cutout
in
the
spar
web
•
between
any
other
connection
hardware
and
the
cutout
in
the
elevator
skin

### Page 7

Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
•
between
any
moveable
parts
and
other
potential
interference
(1)
If
interference
still
exists
between
the
elevator
trim
tab
actuator
rod
end
to
elevator
trim
tab
actuator
push
-
pull
tube
hardware
and
the
elevator
spar
web
material
,
spar
web
cutout
or
other
material
,
contact
T
extron
A
viation
for
further
direction.
1
1.
Make
sure
there
is
uninterrupted
,
with
no
interference
,
full
travel
of
the
elevator
control
system
and
the
elevator
trim
system
in
the
pitch
up
,
pitch
down
and
nose
up
,
nose
down
travels.
12.
Make
sure
all
hardware
removed
in
Steps
3
and
5
is
discarded.
13.
Remove
the
maintenance
warning
tags
and
connect
the
airplane
battery
.
14.
Make
an
entry
in
the
airplane
logbook
that
states
compliance
and
method
of
compliance
with
this
service
bulletin.
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
5

### Page 8

MEB
-
27
-
02
Page
6
Revision
1
-
June
15
,
2016
Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
C
B
Actuator 
Assembly
,
Elevator 
T
rim 
T
ab
(Reference)
T
ube 
Assembly
,
T
rim 
T
ab Push-Pull 
T
ube
(Reference)
Horn 
Assembly
,
Elevator 
T
rim 
T
ab
(Reference)
1010T1001
B20983
DET
AIL
 
A
NOTE:
Model 310R shown, location for trim tab
push-pull tube similar on other models.
This illustration is for reference only
. 
The orientation
of the bolts as shown may not lead to acceptable
clearances with the spar web, fairing, etc. 
NOTE:
A
Figure
1.
Elevator
T
rim
-
T
ab
Push
-
Pull
T
ube
Hardware
(Sheet
1)

### Page 9

Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
NAS464P3-8 or
NAS464P3-9
Bolt
(1 Required)
NAS1
149F0332P
and/or
NAS1
149F0316P
W
asher
(1 or More as Required)
MS17826-3
Nut
MS24665-132
Cotter Pin
(1 Each Required)
DET
AIL
 C
DET
AIL
 B
NAS464P3-8 or
NAS464P3-9
Bolt
(1 Required)
NAS1
149F0332P
and/or
NAS1
149F0316P
W
asher
(1 or More as Required)
MS17826-3
Nut
MS24665-132
Cotter Pin
(1 Each Required)
B10612023
C10612023
B20984
NOTE:
This illustration is for reference only
.
The orientation of the bolts as shown may
not lead to acceptable clearances with
the spar web, fairing, etc. 
Figure
1.
Elevator
T
rim
-
T
ab
Push
-
Pull
T
ube
Hardware
(Sheet
2)
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
7

### Page 10

MEB
-
27
-
02
Page
8
Revision
1
-
June
15
,
2016
Multi
-
engine
SER
VICE
BULLETIN
MEB
-
27
-
02
MA
TERIAL
INFORMA
TION
Order
the
kit
below
to
install
this
modification.
NEW
P
/
N
QUAN-
TITY
KEY
WORD
OLD
P
/
N
INSTRUCTIONS
/
DISPOSITION
MEB
-
27
-
02
1
Kit
,
consisting
of
the
following
parts:
NAS464P3
-
8
2
Bolt
Same
Discard
Old
,
Install
New
NAS464P3
-
9
2
Bolt
Same
If
longer
grip
-
length
is
needed
NAS1
149F0316P
2
W
asher
Same
Install
as
needed
for
correct
cotter
pin
alignment
NAS1
149F0332P
6
W
asher
Same
Discard
Old
,
Install
New
as
needed
for
correct
cotter
pin
alignment
MS17826
-
3
2
Nut
Same
Discard
Old
,
Install
New
MS24665
-
132
2
Cotter
Pin
Same
Discard
Old
,
Install
New
NOTE:
It
is
permissible
to
substitute
the
NAS464P3
-
X
bolt
with
a
NAS6203
-
X
bolts.

### Page 11

Multi
-
engine
OWNER
ADVISOR
Y
MEB
-
27
-
02
TITLE
FLIGHT
CONTROLS
-
ELEV
A
T
OR
TRIM
-
T
AB
PUSH
-
PULL
TUBE
HARDW
ARE
REPLACEMENT
EFFECTIVITY
The
following
Cessna
Aircraft
Models
(all
serial
numbers):
310
thru
310R
,
E310H
,
E310J
,
310J
-
1
,
T310P
thru
T310R
320
thru
320F
,
320
-
1
335
340
,
340A
401
thru
401B
402
thru
402C
41
1
,
41
1A
414
,
414A
421
thru
421C
REASON
T
o
replace
the
hardware
securing
the
elevator
trim
tab
push
-
pull
tube
to
the
elevator
trim
tab
actuator
and
the
elevator
trim
tab
horn.
COMPLIANCE
MANDA
T
OR
Y
.
This
service
letter
must
be
accomplished
at
the
next
100
-
hour
or
12
-
month
(annual
-
type)
inspection
,
whichever
occurs
first.
NOTE:
A
general
visual
inspection
for
correct
installation
and
security
of
the
elevator
trim
tab
push
-
pull
tube
connecting
hardware
and
an
inspection
for
tab
deflection
(free
play)
shall
be
completed
during
each
subsequent
100
-
hour
or
12
-
month
(annual)
type
inspection
after
the
accomplishment
of
this
service
bulletin.
The
general
visual
inspection
should
check
all
elevator
trim
actuator
and
elevator
trim
tab
horn
to
push
-
pull
tube
connection
hardware
for
condition
,
corrosion
,
cracking
,
security
,
cotter
pin
installation
for
proper
safety
,
and
the
elevator
and
elevator
trim
system
for
uninterrupted
,
proper
operation
through
the
full
travel
of
the
elevator
and
elevator
trim
tab
surfaces
(pitch
up
/
pitch
down
and
nose
up
/
nose
down
trim
respectively).
Perform
the
elevator
trim
tab
deflection
(free
play)
check
per
the
applicable
maintenance
or
service
manual.
Original
Issue
-
February
29
,
2016
MEB
-
27
-
02
Revision
1
-
June
15
,
2016
Page
1
of
2
T
extron
A
viation
Customer
Service
,
P
.O.
Box
7706
,
Wichita
,
KS
67277
,
U.S.A.
1
-
316
-
517
-
5800
This
document
contains
technical
data
and
is
subject
to
U.S.
export
regulations.
This
information
has
been
exported
from
the
United
States
in
accordance
with
export
administration
regulations.
Diversion
contrary
to
U.S.
law
is
prohibited.
ECCN:
9E991
COPYRIGHT
©
2016

### Page 12

MEB
-
27
-
02
Page
2
Revision
1
-
June
15
,
2016
Multi
-
engine
OWNER
ADVISOR
Y
MEB
-
27
-
02
P
ART
NUMBER
A
V
AILABILITY
COST
MEB
-
27
-
02
*
*
*
Please
contact
the
Authorized
Service
Facility
for
current
costs
and
availability
of
parts
listed
in
the
service
document.
Based
on
availability
and
lead
times
,
parts
may
require
advanced
scheduling.
NOTE:
As
a
convenience
,
service
documents
are
now
available
online
to
all
our
customers
through
a
simple
,
free
-
of
-
charge
registration
process.
If
you
would
like
to
sign
up
,
please
visit
the
"Customer
Access"
link
at
www
.txtavsupport.com
to
register
.

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