# Textron Aviation Service Letter 560-26-02: Revision 1

- Rights: © Textron Aviation Inc. Filed by the FAA in regulations.gov docket FAA-2025-0334; AD 2025-11-09 incorporates this document by reference. Not covered by OpenAirDocs’ CC0 dedication.
- Document: [Textron Aviation Service Letter 560-26-02](https://openairdocs.org/service-documents/cessna/sl-560-26-02.md)
- Title as filed: SL560-26-02R1
- Pages: 12
- PDF: https://openairdocs.org/files/sha256/3e/31/3e3170290c1940ebdd5fda543d40e7d4d7021649f44d48d56130281e36d52560
- Page: https://openairdocs.org/service-documents/cessna/sl-560-26-02/file/3e3170290c19

## Text

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### Page 1

Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
REVISION
TRANSMITT
AL
This
sheet
transmits
Revision
1
to
SL560
-
26
-
02
which:
A.
Updated
serialization.
B.
Updated
the
Reason
statement.
C.
Changed
the
description
to
service
letter
from
service
bulletin.
D.
Changed
step
4.
to
remove
the
positive
wires
from
the
engine
fire
bottle
squibs
from
inspect
the
fire
bottle
wiring.
E.
Changed
step
5.
to
inspect
the
fire
bottle
wiring
from
remove
the
positive
wires
from
the
engine
fire
bottle
squibs.
F
.
Added
step
5.
to
install
yellow
shrink
sleeve.
G.
Changed
step
6.
thru
16.
to
refer
to
the
Maintenance
Manual
for
the
Engine
Fire
Extinguisher
Functional
T
est
,
renumbered
steps.
H.
Changed
step
6.C.
and
6.D.
to
identify
Y
ellow
ID
sleeve
legibility
and
installed.
I.
Added
HS048YW1NF050B
to
the
parts
list.
NOTE:
This
revision
replaces
SL560
-
26
-
02
in
its
entirety
.
REVISION
COMPLIANCE
EFFECT
:
Airplanes
that
have
previously
complied
with
this
document
must
inspect
the
fire
bottle
wiring
per
Step
6.
LOG
OF
REVISIONS
Original
Issue
July
8
,
2021
Revision
1
July
31
,
2024
Original
Issue
-
July
8
,
2021
SL560
-
26
-
02
Revision
1
-
July
31
,
2024
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
©
2021

### Page 2

(No text on this page.)

### Page 3

Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
TITLE
FIRE
PROTECTION
-
FIRE
BOTTLE
WIRE
VERIFICA
TION
AND
TEST
EFFECTIVITY
MODEL
SERIAL
NUMBERS
560
(Citation
V)
-
0001
thru
-
0259
560
(Citation
Ultra)
-
0260
thru
-
0538
560
(Citation
Encore)
-
0539
thru
-
0707
560
(Citation
Encore+)
-
0751
thru
-
0815
REASON
The
engine
fire
bottle
cartridge
positive
and
negative
terminal
studs
are
the
same
size.
It
is
possible
to
connect
the
wires
to
the
wrong
stud
on
the
fire
extinguisher
cartridge
and
the
wires
may
have
been
mislabeled.
Improperly
connected
wires
will
cause
the
circuit
breaker
to
disengage
(or
pop)
when
you
attempt
to
discharge
the
bottle(s).
DESCRIPTION
This
service
letter
provides
instructions
to
inspect
and
test
the
wires
to
the
fire
bottle
cartridges.
COMPLIANCE
MANDA
T
OR
Y
.
This
service
document
must
be
accomplished
within
100
flight
hours
or
60
days
from
the
date
of
receipt
,
whichever
occurs
first.
A
service
document
published
by
T
extron
A
viation
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
document
,
including
the
intent
therein.
2)
The
mechanic
must
correctly
use
and
install
all
applicable
parts
supplied
with
the
service
document
kit.
Only
with
written
authorization
from
T
extron
A
viation
can
substitute
parts
or
rebuilt
parts
be
used
to
replace
new
parts.
3)
The
mechanic
or
airplane
owner
must
use
the
technical
data
in
the
service
document
only
as
approved
and
published.
4)
The
mechanic
or
airplane
owner
must
apply
the
information
in
the
service
document
only
to
aircraft
serial
numbers
identified
in
the
Effectivity
section
of
the
document.
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
T
extron
A
viation
is
authorized
to
make
or
apply
any
changes
to
a
T
extron
A
viation
-
issued
service
document
or
flight
manual
supplement
without
prior
written
consent
from
T
extron
A
viation.
T
extron
A
viation
is
not
responsible
for
the
quality
of
maintenance
performed
to
comply
with
this
document
,
unless
the
maintenance
is
accomplished
at
a
T
extron
A
viation
-
owned
Service
Center
.
CONSUMABLE
MA
TERIAL
No
specialized
consumable
materials
are
required
to
complete
this
service
document.
Original
Issue
-
July
8
,
2021
SL560
-
26
-
02
Revision
1
-
July
31
,
2024
Page
1
of
7
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
©
2021

### Page 4

SL560
-
26
-
02
Page
2
Revision
1
-
July
31
,
2024
Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
T
OOLING
NAME
NUMBER
MANUF
ACTURER
USE
Multimeter
Commercially
A
vailable
T
o
check
for
electrical
voltage.
Electrical
Shunt
Locally
Obtained
T
o
shunt
electrical
voltage.
REFERENCES
Citation
Standard
Practices
Manual
Cessna
Model
560
Maintenance
Manual
Cessna
Model
560
Encore
Wiring
Diagram
Cessna
Model
560
Encore
Plus
Wiring
Diagram
PUBLICA
TIONS
AFFECTED
None
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
external
electrical
power
.
(2)
Disconnect
the
airplane
battery
.
D.
Attach
maintenance
warning
tags
to
the
battery
and
external
power
receptacle
that
have
"DO
NOT
CONNECT
ELECTRICAL
POWER
-
MAINTENANCE
IN
PROGRESS"
written
on
them.
2.
Disengage
the
L
F
/
W
SHUT
OFF
and
R
F
/
W
SHUT
OFF
circuit
breakers
on
the
left
circuit
breaker
panel.
3.
Remove
access
panel
31
1AZ.
(Refer
to
the
560
Maintenance
Manual
,
Chapter
6
,
Access
Plates
and
Panels
Identification
-
Description
and
Operation.)
4.
Do
the
Engine
Fire
Extinguisher
System
Functional
T
est
as
follows:
W
ARNING:
Immediately
upon
removal
of
wiring
from
fire
bottle
cartridge
(squib)
terminals
,
use
jumper
wires
to
connect
cartridge
terminals
together
to
prevent
accidental
discharge
of
fire
bottles.
NOTE:
When
you
do
this
test
,
BOTTLE
1
is
the
forward
extinguisher
bottle
and
BOTTLE
2
is
the
aft
extinguisher
bottle.
A.
(Refer
to
Figure
1
,
Sheet
1.)
Disconnect
the
cartridge
center
post
positive
(POS
+)
wires
from
the
fire
extinguisher
bottle
cartridges
on
the
list
that
follows:
•
L1BOTL1
-
NP209
(FWD)
•
R1BOTL1
-
PP209
(FWD)
•
L1BOTL2
-
KP208
(AFT)
•
R1BOTL2
-
PP208
(AFT)
B.
Apply
external
power
to
the
airplane.
C.
Engage
the
LH
F
/
W
SHUT
OFF
circuit
breaker
.
D.
Lift
the
switch
guard
,
push
and
release
the
LH
ENG
FIRE
switch
/
light
(S37).
(1)
Make
sure
that
the
BOTTLE
1
ARMED
PUSH
switch
/
light
(S39)
on
the
fire
tray
comes
on.

### Page 5

Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
E.
Engage
the
RH
F
/
W
SHUT
OFF
circuit
breaker
.
(1)
Make
sure
that
the
BOTTLE
2
ARMED
PUSH
switch
/
light
(S38)
on
the
fire
tray
comes
on.
F
.
Use
a
multimeter
to
make
sure
there
is
no
voltage
on
the
wires
that
follow:
•
L1BOTL1
-
NP209
(FWD)
•
R1BOTL1
-
PP209
(FWD)
•
L1BOTL2
-
KP208
(AFT)
•
R1BOTL2
-
PP208
(AFT)
G.
Push
and
hold
the
BOTTLE
1
ARMED
PUSH
switch
/
light.
(1)
Make
sure
that
the
BOTTLE
1
ARMED
PUSH
switch
/
light
goes
of
f.
(2)
Make
sure
wire
L1BOTL1
-
NP209
reads
(positive)
+28
VDC
while
the
switch
/
light
is
pushed.
H.
Release
the
white
BOTTLE
1
ARMED
PUSH
switch
/
light.
I.
Push
and
hold
the
BOTTLE
2
ARMED
PUSH
switch
/
light.
(1)
Make
sure
that
the
BOTTLE
2
ARMED
PUSH
switch
/
light
goes
of
f.
(2)
Make
sure
wire
L1BOTL2
-
KP208
reads
(positive)
+28
VDC.
J.
Release
the
white
BOTTLE
2
ARMED
PUSH
switch
/
light.
K.
Lift
the
switch
guard
,
push
and
release
the
LH
ENG
FIRE
switch
/
light
(S37).
(1)
Make
sure
that
the
F
/
W
SHUT
OFF
LH
annunciator
goes
of
f.
(2)
Make
sure
that
wires
L1BOTL1
-
NP209
and
L1BOTL2
-
KP208
have
no
voltage.
CAUTION:
If
there
is
voltage
,
do
not
connect
the
wires
to
the
fire
bottle
cartridges.
Do
the
troubleshooting
procedure
of
the
system
to
find
the
problem.
(Refer
to
the
Model
560
Maintenance
Manual
,
Chapter
26
,
Extinguishing
System
-
T
roubleshooting.)
L.
Disengage
the
LH
F
/
W
SHUT
OFF
circuit
breaker
.
M.
Lift
the
switch
guard
,
push
and
release
the
RH
ENG
FIRE
switch
/
light
(S36).
(1)
Make
sure
that
the
BOTTLE
2
ARMED
PUSH
switch
/
light
on
the
fire
tray
comes
on.
N.
Engage
the
LH
F
/
W
SHUT
OFF
circuit
breaker
.
(1)
Make
sure
that
the
BOTTLE
1
ARMED
PUSH
switch
/
light
comes
on.
O.
Use
a
multimeter
to
make
sure
there
is
no
voltage
on
the
wires
that
follow:
•
L1BOTL2
-
KP208
(AFT)
•
R1BOTL2
-
PP208
(AFT)
•
L1BOTL1
-
NP209
(FWD)
•
R1BOTL1
-
PP209
(FWD)
CAUTION:
If
there
is
voltage
,
do
not
connect
the
wires
to
the
fire
bottle
cartridges.
Do
the
troubleshooting
procedure
of
the
system
to
find
the
problem.
(Refer
to
the
Model
560
Maintenance
Manual
,
Chapter
26
,
Extinguishing
System
-
T
roubleshooting.)
P
.
Push
and
hold
the
BOTTLE
1
ARMED
PUSH
switch
/
light.
(1)
Make
sure
that
the
BOTTLE
1
ARMED
PUSH
switch
/
light
goes
of
f.
(2)
Make
sure
wire
R1BOTL1
-
PP209
reads
(positive)
+28
VDC.
Q.
Release
the
white
BOTTLE
1
ARMED
PUSH
switch
/
light.
R.
Push
and
hold
the
BOTTLE
2
ARMED
PUSH
switch
/
light.
(1)
Make
sure
that
the
BOTTLE
2
ARMED
PUSH
switch
/
light
goes
of
f.
(2)
Make
sure
wire
R1BOTL2
-
PP208
reads
(positive)
+28
VDC.
SL560
-
26
-
02
Revision
1
-
July
31
,
2024
Page
3

### Page 6

SL560
-
26
-
02
Page
4
Revision
1
-
July
31
,
2024
Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
S.
Release
the
white
BOTTLE
2
ARMED
PUSH
switch
/
light.
T
.
Lift
the
switch
guard
,
push
and
release
the
RH
ENG
FIRE
switch
/
light.
U.
Use
a
multimeter
to
make
sure
there
is
no
voltage
on
the
wires
that
follow:
•
L1BOTL2
-
KP208
(AFT)
•
R1BOTL2
-
PP208
(AFT)
•
L1BOTL1
-
NP209
(FWD)
•
R1BOTL1
-
PP209
(FWD)
CAUTION:
If
there
is
voltage
,
do
not
connect
the
wires
to
the
fire
bottle
cartridges.
Do
the
troubleshooting
procedure
of
the
system
to
find
the
problem.
(Refer
to
the
Model
560
Maintenance
Manual
,
Chapter
26
,
Extinguishing
System
-
T
roubleshooting.)
V
.
Disengage
the
L
F
/
W
SHUT
OFF
and
R
F
/
W
SHUT
OFF
circuit
breakers
on
the
left
circuit
breaker
panel.
5.
Disconnect
electrical
power
from
the
airplane.
A.
Disconnect
external
electrical
power
.
B.
Disconnect
the
airplane
battery
.
C.
Attach
maintenance
warning
tags
to
the
battery
and
external
power
receptacle
that
have
"DO
NOT
CONNECT
ELECTRICAL
POWER
-
MAINTENANCE
IN
PROGRESS"
written
on
them.
6.
Inspect
the
fire
bottle
cartridge
wire
numbers
and
Y
ellow
ID
Sleeves
for
proper
identification.
(Refer
to
the
Model
560
,
560
Encore
or
560
Encore
Plus
,
Wiring
Diagram
Manual
,
Chapter
26
,
Fire
Protection.)
NOTE:
The
terminal
lugs
are
the
same
size
on
the
fire
bottle
squibs
,
it
is
possible
to
install
the
wires
incorrectly
leading
to
an
unsafe
condition
where
the
fire
bottle
will
not
discharge.
This
service
letter
is
issued
to
verify
proper
fire
bottle
wiring
and
ensure
the
wires
are
correctly
labeled.
CAUTION:
THE
CIRCUIT
BREAKERS
MUST
BE
DISENGAGED
BEFORE
THE
ELECTRICAL
WIRES
ARE
CONNECTED
OR
DISCONNECTED
FROM
THE
FIRE
BOTTLE
CAR
TRIDGES
OR
ACCIDENT
AL
DISCHARGE
COULD
RESUL
T
.
A.
(Refer
to
Figure
1
,
Sheet
1.)
Make
sure
the
HS048YW1NF050B
Y
ellow
ID
Sleeve
that
is
marked
W
ARNING:
CONNECT
ONL
Y
T
O
CENTER
POST
(POS
+)
on
the
wires
that
follow:
•
L1BOTL1
-
NP209
•
R1BOTL1
-
PP209
•
L1BOTL2
-
KP208
•
R1BOTL2
-
PP208
B.
(Refer
to
Figure
1
,
Sheet
1.)
Make
sure
the
HS048YW1NF050B
Y
ellow
ID
Sleeve
that
is
marked
W
ARNING:
CONNECT
ONL
Y
T
O
SIDE
POST
(NEG
-)
on
the
wires
that
follow:
•
L2BOTL1
-
GND
-
17
•
R2BOTL1
-
GND
-
17
•
L2BOTL2
-
GND
-
16
•
R2BOTL2
-
GND
-
16
C.
If
the
wiring
is
not
properly
identified
or
if
the
Y
ellow
ID
sleeve
is
not
legible
,
print
on
a
Y
ellow
ID
Sleeve
and
install
the
sleeve
on
the
correct
wire
as
listed
in
Step
6.A
and
6.B.
(Refer
to
the
Citation
Standard
Practices
Manual
,
Chapter
20
,
Wiring
and
Resistors
-
Maintenance
Practices.)
D.
Inspect
the
wiring
and
ring
terminal.
(Refer
to
the
Citation
Standard
Practices
Manual
,
Chapter
20
,
Electrical
Component
Cleaning
and
Inspection
-
Maintenance
Practices.)
If
the
wiring
needed
to
be
relabeled
or
if
the
ring
terminal
requires
replacement
,
install
a
new
MS25036
-
149
Ring
T
erminal.
(Refer
to
the
Citation
Standard
Practices
Manual
,
Chapter
20
,
Splices
,
T
erminals
and
heat
Shrinkable
T
ubing
-
Maintenance
Practices.)
E.
Shrink
the
yellow
ID
sleeves
over
the
body
of
the
terminal.
(Refer
to
the
Citation
Standard
Practices
Manual
,
Chapter
20
,
Wiring
and
Resistors
-
Maintenance
Practices.)
F
.
T
orque
the
lock
nuts
to
10
to
15
inch
-
pounds.

### Page 7

Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
7.
Remove
the
jumper
wires
from
fire
bottle
cartridges
(squibs)
individually
before
you
connect
the
fire
bottle
wiring.
A.
Make
sure
that
the
voltage
is
less
than
0.1
VDC
in
all
wires
before
you
connect
them
to
the
fire
bottles.
8.
(Refer
to
Figure
1
,
Sheet
1.)
Make
sure
the
wires
are
correctly
connected
to
the
fire
extinguisher
bottles
as
follows:
CAUTION:
Do
not
over
torque
the
lock
nuts.
If
you
torque
the
electrical
stud
lock
nuts
more
than
25
inch
-
pounds
,
stud
rotation
and
shear
failure
can
occur
.
A.
Connect
wire
L1BOTL1
-
NP209
to
BOTTLE
1
cartridge
center
post.
B.
Connect
wire
R1BOTL1
-
PP209
to
BOTTLE
1
cartridge
center
post.
C.
Connect
wire
L1BOTL2
-
KP208
to
BOTTLE
2
cartridge
center
post.
D.
Connect
wire
R1BOTL2
-
PP208
to
BOTTLE
2
cartridge
center
post.
E.
T
orque
the
lock
nuts
to
10
to
15
inch
-
pounds.
9.
Install
access
panel
31
1AZ.
(Refer
to
the
Model
560
Maintenance
Manual
,
Chapter
6
,
Access
Plates
and
Panels
Identification
-
Description
and
Operation.)
10.
Engage
the
L
F
/
W
SHUT
OFF
and
R
F
/
W
SHUT
OFF
circuit
breakers
on
the
left
circuit
breaker
panel.
1
1.
Remove
the
maintenance
warning
tags
and
connect
the
airplane
battery
.
12.
Make
an
entry
in
the
airplane
logbook
that
states
compliance
and
method
of
compliance
with
this
service
document.
NOTE:
T
extron
A
viation
recommends
that
compliance
with
all
service
documents
is
reported
to
a
maintenance
tracking
system
provider
.
•
Complete
a
record
of
compliance.
(Maintenance
T
ransaction
Report
,
Log
Book
Entry
,
or
other
record
of
compliance.)
•
Put
a
copy
of
the
completed
record
of
compliance
in
the
airplane
logbook.
•
Send
a
copy
of
the
completed
record
of
compliance
to
the
maintenance
tracking
system
provider
used.
SL560
-
26
-
02
Revision
1
-
July
31
,
2024
Page
5

### Page 8 (OCR)

Beechcraft  Hawker
Citation  SERVICE LETTER  TEXTRON ÀVIATION  Cessna
MANDATORY  SL560-26-02
A111269
000001
FORWARD  AFT
FIRE BOTTLE  FIRE BOTTLE
(BOTTLE 1)  (BOTTLE 2)
(REFERENCE)  (REFERENCE)
R2BOTL1-GND17  L1BOTL2-KP208
(NEGATIVE SIDE POST)  (POSITIVE CENTER POST)
R1BOTL1-PP209  L2BOTL2-GND16
(POSITIVE CENTER POST)  (NEGATIVE SIDE POST)
R1BOTL2-PP208
L2BOTL1-GND17  (POSITIVE CENTER POST)
(NEGATIVE SIDE POST)
R2BOTL2-GND16
(NEGATIVE SIDE POST)
L1BOTL1-NP209
(POSITIVE CENTER POST)
VIEW A-A
5610T1049
A6555T081
Figure 1. Fire Bottle Wiring (Sheet 1)
SL560-26-02
Page 6  Revision 1 - July 31, 2024

### Page 9

Citation
SER
VICE
LETTER
MANDA
T
OR
Y
SL560
-
26
-
02
MA
TERIAL
INFORMA
TION
Order
parts
below
to
complete
this
service
document.
NEW
P
/
N
QUAN-
TITY
KEY
WORD
OLD
P
/
N
INSTRUCTIONS
/
DISPOSITION
HS048YW1NF050B
8
Y
ellow
ID
Sleeve
If
Necessary
MS25036
-
149
8
Wire
Ring
T
erminal
If
Necessary
SL560
-
26
-
02
1
Instructions
*
Please
contact
T
extron
A
viation
Parts
Distribution
for
current
cost
and
availability
of
parts
listed
in
this
service
document.
Phone
at
1
-
800
-
835
-
4000
(Domestic)
or
1
-
316
-
517
-
5603
(International).
For
more
information
,
please
visit
the
T
APD
Support
&
Aftermarket
Account
Management
website
at
https:
/
/
ww2.txtav
.com
/
Parts
/
Promos
/
T
APD.
Based
on
availability
and
lead
times
,
parts
may
require
advanced
scheduling.
SL560
-
26
-
02
Revision
1
-
July
31
,
2024
Page
7

### Page 10

(No text on this page.)

### Page 11

Citation
OWNER
ADVISOR
Y
SL560
-
26
-
02
TITLE
FIRE
PROTECTION
-
FIRE
BOTTLE
WIRE
VERIFICA
TION
AND
TEST
T
O:
Cessna
Model
560
(Citation
Encore)
Aircraft
Owner
REASON
The
engine
fire
bottle
positive
and
negative
terminal
studs
are
the
same
size.
It
is
possible
to
connect
the
wires
to
the
wrong
stud
on
the
fire
extinguisher
cartridge.
This
will
cause
the
circuit
breaker
to
disengage
(or
pop)
when
you
attempt
to
discharge
the
bottle(s).
COMPLIANCE
MANDA
T
OR
Y
.
This
service
document
must
be
accomplished
within
100
flight
hours
or
60
days
from
the
date
of
receipt
,
whichever
occurs
first.
LABOR
HOURS
WORK
PHASE
LABOR
-
HOURS
Inspect
&
T
est
1.5
MA
TERIAL
INFORMA
TION
P
ART
NUMBER
A
V
AILABILITY
COST
HS048YW1NF050B
*
*
MS25036
-
149
*
*
*
Please
contact
T
extron
A
viation
Parts
Distribution
for
current
cost
and
availability
of
parts
listed
in
this
service
document.
Phone
at
1
-
800
-
835
-
4000
(Domestic)
or
1
-
316
-
517
-
5603
(International).
For
more
information
,
please
visit
the
T
APD
Support
&
Aftermarket
Account
Management
website
at
https:
/
/
ww2.txtav
.com
/
Parts
/
Promos
/
T
APD.
Based
on
availability
and
lead
times
,
parts
may
require
advanced
scheduling.
W
ARRANTY
This
service
document
is
mandatory
.
Eligible
airplanes
may
qualify
for
parts
and
labor
coverage
to
the
extent
noted
in
the
Labor
Hours
and
Material
A
vailability
sections
of
this
document.
Original
Issue
-
July
8
,
2021
SL560
-
26
-
02
Revision
A
-
July
31
,
2024
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
©
2021

### Page 12

SL560
-
26
-
02
Page
2
Revision
A
-
July
31
,
2024
Citation
OWNER
ADVISOR
Y
SL560
-
26
-
02
Eligibility:
Airplanes
identified
within
the
serial
number
ef
fectivity
of
this
service
document
must
have
active
Airframe
warranty
coverage
on
the
original
issue
date
of
this
document
and
the
coverage
must
be
active
on
the
day
the
work
is
accomplished.
Parts
Coverage:
T
extron
A
viation
-
owned
and
T
extron
A
viation
-
authorized
Service
Facilities
,
operators
,
or
other
maintenance
facilities
may
submit
a
claim
for
the
parts
required
to
accomplish
this
service
document
as
defined
in
the
Material
A
vailability
section
of
this
document.
Labor
Coverage:
T
extron
A
viation
-
owned
and
T
extron
A
viation
-
authorized
Service
Facilities
rated
to
perform
maintenance
on
the
specific
model
of
Cessna
Aircraft
may
submit
a
claim
for
the
labor
necessary
to
accomplish
this
service
document
as
defined
in
the
Labor
Hours
section
of
this
document.
Credit
Application:
After
this
service
document
has
been
accomplished
,
a
claim
must
be
submitted
to
T
extron
A
viation
within
30
days
of
the
service
document
completion.
Claims
for
compliance
of
this
service
document
are
to
be
filed
as
a
W4
type
claim.
Please
submit
your
claim
form
online
at
ww2.txtav
.com
/
Parts
or
email
the
completed
T
extron
A
viation
Claim
Form
to
warranty@txtav
.com
.
If
submitted
on
-
line
a
Return
Authorization
will
be
provided.
If
a
paper
claim
is
submitted
your
claim
will
be
entered
into
the
system
and
a
Return
Authorization
will
be
sent
to
you.
The
Return
Authorization
must
accompany
any
required
return
parts
(see
Material
A
vailability
)
,
to
the
point
of
purchase.
Parts
to
be
returned
to
T
extron
A
viation
Parts
Distribution
should
be
forwarded
to:
T
extron
A
viation
Parts
Distribution
W
arranty
Administration
285
South
Greenwich
Road
Bldg
B89
,
Docks
1
-
4
Wichita
,
KS
67206
USA
Expiration:
July
31
,
2026
(after
this
date
the
owner
/
operator
assumes
the
responsibility
for
compliance
costs)
T
extron
A
viation
reserves
the
right
to
void
continued
airplane
warranty
coverage
for
the
parts
af
fected
by
this
service
document
until
the
service
document
is
accomplished.
NOTE:
As
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