INSTRUCTIONS
This record should be completed and maintained in accordance with FAA Federal Aviation Regulations
43.9, 43.11 and 91.173 and/or other prevailing government regulations.
NOTE: Record Service Bulletins and Airworthiness
Airframe Maintenance Record.
Directives in the back of this record as weD as ~e
Cop] ght
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
RECORD
AUTHORIZED SIGNATURE.
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
NEW RECIPROCATING ENGINE CERTIFICATE
This is to certify that the engine as described hereinafter bas been manufactured
run-in and tested as prescribed by TEXTRON LYCOMING specifications and
Federal Aviation Regulations. No further run-in is required. All applicable
Federal Aviation Administration Directives and Textron Lycoming ServiC(:
Bulletins have been complied with at time of Manufacture.
TIO-S40-AK1A
ItP-3/-0}
e 1993
L-11170-61A
m~
(AUTHORIZED
REPRESENTATIVE)
IlAlNTENAHCE
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
:':_5CF-?'ilOO Of inE WORK PERFORMED
r
if
Engine model TIO-S40-AK1A, SIN
b-- / 1/7~- w/A
has been installed on aircraft # 77iZO<lI£
.
This
engine serviced with Phillips XlC 20W50 Engine oil.
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
20'OL
DESCRIPTION
RECORD
OF THE WORK PERFORMED
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
7,.0
5;;0105'v
~
1,..-
3/~(o~
1'{3
()o~h)
-_
Autopilots rAlntr.J/, lne.
HttIooor23. Tuisoh" ..... '''''''''AlIIlOf1· rul'I\,OK
P.O. Box m100 • Tulsa. OK 74100
(918)OO~18·
FOX(918)8J2~1W
_. -
ens
FAA
uI
0:
CM2R747K
meoee
Work
Sokt To:
14116
Order.
=>
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MA02.Q0387
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ex:i=o<S
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Oola Mike LLC.
2186 East Goldon Oak.
Fayettevillo. AR 72703
General Comments:
62224
SAtES
OROER:
434554
Aircnatt Humber.
EOO'
93.8
,
::c.:Il!l
O,jcftlp."",,:
T_:T1=
Hobbs 11me:
11me C~
N831MC
Totaf Tlmo:
SIN
SIN: 'N820B138
93.8
1
ft2IIl.tmi
-J.II-:-tJ J
CW It~)_
EnOk,ul'OOI"JI"lnspecllool.due.
ProeTime
Proo SIN
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rM{t-~' . J ~'
1..'1c. j.8 } )_
'I 1/
Do 110'cIIOnoc oHor fin....
•
A.llon I,.on:
CW OI"lOJna100 nour inspection items per Cessna maintenance manual.
COOlples.tOn 1=12. 2=72, 3=70, 4=70. s=ra, 6=72.
No OIl or
c:Ilango at this lime.
Ol.c ... .,.ncv:
Z
fI!l!!!!m;.
Aulop801 pittillrim 1;lght and hom came on during the eeecent Had 10pull the circuit breaker
fiI'' '
to
shut off the
hom.
~gOTek!2n:
Thl. dIIlCtGPM<lYIrtlfiSfor,o WO tI AV02-0511.
CW
0
W
::;;
3
Olo.repI."'"
Problem;
Co."""
0:
58 , 02-71.05.
and Lycoming
SB ~ 555 by
A~tlle!l!!li
FOllII" nllCtlpipe P'lIIll..,. •• Iorqued allen pipe
plUg
Inspecting
lAW 58
Allen
0
u..
pipe plug 1QtqUe.
0:
W
0..
#555.
•
:.::
OIIiCtOl>I.cv:
!!I!l.!!!!!!!.;
CW WIth SA 02-5$-01, eMtvator Inspecllo" and modification on the left side only.
~aJ9D
cw
0:
0
:5:
W
I!Hn.:.
S8 02·Ba.o11AW
\,I9tructlons
by addfng
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rivets
F
LH elevalor.
u..
0
5
~MX:
f!!!ll!!ml
elm"'.
Eng"'. l1li1111.
IlSlt'!J!.!!l!!!$
~8
02 f1 04 by
..Q!;'h;'j,);"W-
drnonlng on nose
In.",1I1ngKH "
landing gear _
MK182-71002
a
.'l!l
Z
pan!.
0
and "'Ioc:aUng
engile
rue'
i=
0..
ex:
drain.
.
~~~~IC!t~~~:~~~~~:C~~Jt~gt
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oct secured at upper end to engine. Nuts used to secure cable 10engine
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7
!!.L9.!''.!tn,
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I
Ipnlit plUGcovftrod with gray
500t
I
indlc:01ingexhaust leak.
I
~11X-tlflnl
~lJr
PIOIII\III" 111111011
tllCh'llltlt tty"tum l"W'ldfound exhaust slrp jolr.t to # 2 cylinder leaking. L.eakage is seNiceable at this time.
UhI1I!,l.'HJ In '''m_l~
1'111UJClkwI,
l!!:':."Jl'I"OYI
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r
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1
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cover screw and checked torque on
(ocker
aM
rocker cover
labor charged
saews.
to
1
It
Pr"illot"l
I
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DA"
100 Hour Inspection on N831 MC
Lycoming TI0540-AK1A sin L11170-61A
Engine time since new is 163.8 hours.
WO#MA03-00507 Dated 5-5-03.
• ~1
'.,
..
Inspected this engine using the inspection form in the current service manual.
1. Changed oil and filter. Cut open old oil filter and found clean. Taken an oil sample supplied by the owner.
2. Compression figures. #1-75,2-74,3-76,4-76,
5-78, & 6-77 over 80.
3. Washed down engine.
4. Rotated spark plugs.
5. Lubricated waste gate shaft bearings.
6. Inspected magneto to engine timing.
7. Inspected cylinders and crankcase for cracks.
.
8. Insoected fuel nozzle lines and clamps iaw AD2002-26-01 paraqraph'(c) per-Lycorninq S8#3420 diagram # 19.
I CERTIFY THIS
.~
HAS B N INSPECTED
IN ACCORDANCE WITH A Ie tJ H-/L a,
INSPECTION "j
AND WAS DfTERMINED TO BE I .AN AIRWORTHY CONomON .. f
THIS DATE
~/r-I.
I ~ 31 ~ T/).llf
WIO fYllH - S-O 7
DATE '11J}£J..RS
i Til': ."
#.
SIGNATURE
d4JA
0
If? c__ f_
AUTOPILOTSCOORAl, INC.
:~
:;
TULSA, OK 74115
FAACRSCM2R747K
:
oj
I I
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
HOURS
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
10THS
11'1,ST1t-L-LI1-P NI;?W t?HI-ft.un JThe-~
~o 8 )._;)_f/} J. PH jt}-p #-.)- C'/L-I#.b
prrt Yo GJ:2 rTf
i4L_ (l.1rl'LA--C~j)
6-'-
SIGNATURE
#'1> f..IJt-il- P;v
e:-"lJ(.jj--
o /}jA.tr-r
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
HOURS
'_S7r
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
10THS
1)
~..
LVG. model TIO-540-AK'IA sin L-11170-61A
Tach and engine total time is 272.8 hours.
WO# MA04-00886 Dated 6-2-04.
Inspected this engine using the inspection form in the current maintenance manual.
1. Changed oil and filter. Taken oil sample. Cut open old filter and found clean. Serviced with Aeroshell 15W50 oil.
Cleaned oil sump suction screen.
2. Cleaned and gaped spark plugs. Rotated spark plugs top to bottom.
3. CW AD2002-26-01 para. (c) inspection of the fuel nozzle lines and clamps per Lycoming S8342E. No defeats noted.
4. Checked magneto to engine timing.
5. Compression test figures. #1-77,2-77,3-77,4-76,5-77,
& 6-76 over 80.
6. Inspected cylinders and crankcase for cracks. No cracks noted.
7 Washed down engine. Run up after inspection. Installed engine cowling.
Repaired the following items.
1. The right magneto was out of timing limits by 4 degrees. Removed the right magneto to inspect the points and cam.
Found the condenser wire connection was loose at the points. Repaired the wire crimp. Timed magneto internally arc
installed on the engine.
2. Engine idle mixture was too rich. Adjusted wheel 3 clicks to lean.
I CERTIFYTHIS
INSPECTED
IN ACCORDANCE WIT A
Ch0-tt~· INSPECTION
ANO WAS DETERMINED T() BE I AN AIRWORTHYCONOmON
01= ~f
THIS DATE frLf_rO,o,L
W!O#
SIGNATURE
[)O'II!
:TEu!
IL_OA '1~
CE~
l.. INC.
TULSA, OK 74115
FAA CRS CM2R747K
HRS j.7)'~
--
--
_
I
JI.tA
MAINTENANCE
- - ---
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
N831MC
DATE: 12-29-2004
~333.1
CHANGED OIL AND FILTER. EXAMINED OLD FILTER FOR METAL CONTAMINATION
FOUND NONE. INSTALLED NEW CH4811 0-1 OIL FILTER. SERVICED ENGINE WITH
AEROSHELL 15W50 OIL. GROUND RUN PERFORMED. NO EVIDENCE OF LEAKS.
AND
_/)J~
V';;'P219028942
MAINTENANCE
DATE
N831MC
HI
RECORD
-
DATE: 05-03-2005
~~360.7
CHANGED OIL AND FILTER. EXAMINED OLD FILTER FOR METAL CONT AMINA TION AND
FOUND NONE. INSTALLED NEW CH481 10-1 OIL FILTER. SERVICED ENGINE WITH
AERO SHELL 15W50 OIL. GROUND RUN PERFORMED. NO EVIDENCE OF LEAKS.
~~earhart
~~~
28942
JTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
--------1
----
--
cngme
-:
10U nour I'Ispecllon
-
~~-
---
IS Que.
31GNATURE,
TE TYPE
BER
Action Taken:
831Mc Engine 100 Hour Inspection.
_ycorn!:lg nO-54O-AK1A
sfn L-11170-61A
LiM and engine total time is 369.1 hours.
.
Irspecled this engine using the inspection form in the current maintenance manual.
Did not change oil or filter. This was completed at 360.7 hours.
2 Compression test figures. #1-77, 2-73, 3-77, 4-75, 5-70, & 6-77 over 80.
Cleaned and gaped spark plugs. Test spark plugs. Rotated top to bottom. Replaced
1.
3:
plugs due to
4. Inspected
5. Inspected
6. Adjusted
7. Inspected
8. Inspected
loose ceramic cone.
the exhaust system for cracks and defects. .
•
the engine crankcase and cylinders for cracxs. No defects noted.
the governor 2 turns out to increase take off rpm to 2400.
magneto to engine timing and found within limits.
'.
fuel nozzle lines and clamps per AD2002-26-01
paragraph (c) per Lycoming
defects found.
9. Inspected engine accessories for attachment.
10. Washed down engine and cleaned.
Labor included in the basic inspection.
I certify this engine has been inspected
Inspected
in accordance
the # 6 cylinder
bottom spark
.
SB# 342E diagram
# 19. No
wiring for condition.
with a 100 hr. inspection
and determined
to be in and airworthy
condition this date.
WO# MA05-01225
Date 6-10-05.
ine TSN is 359.1 hrs.
Signature Ralph P. Stahle
CM2R747K
Autopil ts entral nco
Tulsa, Ok. 74115
Part
Quantify
IJnjts
1.00[ Each
Number
C~"
RHB36S
I
Unit-Price
E'xtendeq
Is
B-fl7:J~7K
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
HOURS
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
10THS
N831MC
TACH: 397.9
HOBBS: 441.3
DATE: 812012005
CHANGED OIL AND FILTER EXAMINED OLD FILTER FOR METAL CONTAMINA nON AND FOUND
NONE . .INSTALLED NEW CH48 I 10-1 OIL FlL TER. SERVICED ENGINE WITH AERO SHELL 15W50 OIL.
GROUND RUN PERFORMED. NO EVIDENCE OF LEAKS .
.:>
~Gearhart
v-;.~~~19028942
/
.-
_I
J~
.....__
=
£
:....-
-~~
I
Autopilots Central, Inc .
Hangar
~
Sold To:
I
23, Tulsa Intemational
Airport - Tulsa, OK
P.O. Box 582108 - Tulsa, OK 74158
{918}836-6418
- Fax (918)832-0136
FAA CRS CM2R747K
Invoice
Delta Mike LLC,
2186 East Golden Oaks
Fayetteville, AR 72703
Work Order:
Acct Number:
Department
•
General Comments:
Contact is Dennis
Aircraft
& NUMBER
Opened:
MA06-01614
(479)871-6911
Maintenance
,.,
Number:
N831MC
Type:T182T
456.8
Hobbs
Time:
SIN
T:i!)e
TI0-540-AK1A
.
-"
SIN: T18208138
0.0
Time
456.8
L-11170-61A
Discrepancy:
3
Action Taken:
N831 MC, T182T, Engine 100 Hour Inspection.
Lyc. TIO-54O-AK1A sin L-11170-61A
WO# MA06-01614 Dated 7-11-06.
Tach Time:
C:icles
LG Cycles:
456.8
Pro!) T:i!)e
B3D36C442
Pro!) SIN
011585
Pro!) Time
456.8
-
•
I
-1•
Tach & Eng. TSN is 456.8 hrs.
Autopilots Central Inc. Tulsa, OK. 74115
Description
Aeroshell Oil
Oil Analysis Kit
Part Number
15WSO
AOA
CH46110-1
J7444-42
Oil Filter
Mount, Cowl
P10-61S0
Filler
j
Credit
Quantiflf
Units
9.00 Each
1.00 Each
FAA Repair Station # CM2R747K
List
Price
Disc
Unit
DATE
1.00 Each
1.00 Each
1.00 Each
r-HOI
Authorized
Signature
-------.-- .
..... _ ..-.~.--.
N831MC
Price
Extended
$
$
$
$
$
The articles andlor work hereon described islare certified
airworthy (unless otherwise specified).
Autopilots Central, Inc.
l
I
I
Inspected this engine using the inspection form in the current service manual. I
1. Taken oil sample. Changed oil and filter. Cut open filter and found clean.
2. Compression figures. #1- 77, 2-78, 3-77, 4-74, 5-76 & 6-76 over 80 Ibs.
3. Cleaned gapped and tested spark plugs. Rotated plugs top to bottom.
4. Installed new engine air filter per AD84-26-02.
5. CW AD2002-26-01, fuel nozzle line and clamp inspection per lycoming SB# 342 E dia_# 19.
6. Removed both magnetos and sent out for their 500 hour internal inspection and impulse coupling inspection.
Both mags are
Slick model 6361, LH sin 01081509 and RH sin 01081510. Both mags were sent to Quality Aircraft Accessories, Inc for the
Inspection. Installed mags with new gaskets and times to engine. Sublet Service Completed:
7/0712006 Description: Repaired
magneto. 6361 Slick Magneto SIN: 01081509 and SIN 01081510, Performed By: Quality Aircraft Accessories, Inc.
7. Replaced one lower cowling shock mount.
B. Washed down engine. Performed engine run up with proper operation.
_!-certify this engine has been in.spected in accordanca.with a..jQQbo~on
and Q§erJlllIlMJo~a
airwodhys:ondition..1his
date.
WO# M~m-11-06
Signed ~
"..
6/23/2006
7/11/2006
Closed:
Moore.
Total Time:
Eng#
1
~ORIZED SIGNATURE,
'ERTIFICATE 1YPE
74115
-
ORIZED SIGNATURE,
:RTlFICATE 1YPE
& NUMBER
1iA1!~
TACH: 521.3
HOBBS: 577.0
DATE: 7/1312007
I
I
I
I
I
CHANGED OIL AND FILTER EXAMINED OLD FILTER FOR METAL CONTAMINATION
AND FOUND NONE, lNST ALLED NEW OIL FILTER PART NO,CH48 110-1. SERVICED
ENGINE WITH 09 QUARTS OF AERO SHELL lSW-SO OIL. GROUND RUN PERFORMED.
NO EVIDENCE OF LEAKS.
~~Q
JAMES RUSSELL DAVIS
A&P 2822707
I
-
~
I
1
-
--_MAINTENANCE
DATE
~m7
TOTAL TIME
IN SERVICE
HOURS
RECORD
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER
DESCRIPTION OF THE WORK PERFORMED
10THS
Tf\-'ktTI'i CTJ~v
f'ft-fAfLe.
C'rt-N"ITP
OJJ, «t- F/J..r~ ..
1t1;"1lPJ !tt;U
IJ-""'; JV m;
CUfflrfttr'"J}j PPJ ~f - 7 e ( J..') ..."t Y 4 b - 7 8.
t W 1f~i9')" - ~ - f) J
c. fCu e;
V/l-III (/rj) Uti Til
I I J-7P(
Y-7/
It::
tiff
r~(trp
73,{)).
\:!"")
VI}-L,."
It~
TULSA, OK 74115
fAA C~ O~?R7.o17K
TACH: 577.8
N831MC
HOBBS: 637.9
DATE: 02/04/2008
DATE
.cHANGED on, AND FIL 1ER EXAMINED on, FILTER FOR METAL CONT AMINA nON & FOUND
NONE. INSTALLED NEW on, FIL1ER PIN AA48110. SERVICED ENGINE WITH AEROSHELL 15W50.
GROUND RUN PERFORMED. NO EVIDENCE OF LEAKS.
iNATURE,
TYPE
oR
JO~
~138384
r/~ ~J_Og09
PIH
IE
fZ-cfllf
r ,
f=lptfE
;:rr
rrnr«. INJT~~
IN ~
c:sf-fJA-ItJT"""'f'MIfJI71fJ/.
IVtnJI
TIT
p/?$,1 If"
f)..J;"'Y-OJ
V I?P f~f~-u..etL
FD fL N:-~eitL/lI?
1Jt{ ~
-,0
0 (L- L-
lJ=ril iIe-
------ -----~--------
~----~--------~--------------~MAINTENANCERECORD
ruRE,
'E
Summit Aviation LLC 500-7Airport Rd. Bentonville,AR 72712
9-1-08 Tach. 612.8
N831MCEngineLog Entry
•
•
•
•
Performed 100 hour/AnnualllAfIN
FAR 43 App. D and Cessna T182T Maintenance Manual.
Drained oil and inspected fitter, no abnormal contaminates noted.
Compression Test Results: #1 78/80, tr2. 77180, #3 79/80, #4 77180, #5 78/80, #6 77/80.
Removed all spark plugs, cleaned, gapped, rotated, tested, and reinstalled WlNew gaskets PIN M674.
•
•
•
•
•
•
•
Magneto timing checked good.
Removed #4 cylinder induction tube, replaced flange gasket W/New PIN 71973 and reinstalled.
Re-torqued all induction tube hose clamps, rocker boss drain hose clamps, and turbo charger exhaust clamps.
Serviced engine W/8 Quarts Aeroshell 1fNV50 oil and New AA4811 0 oil filter.
Washed engine and cowling. Performed engine run, operational and leak checked good.
Checked ADs through ATP Revision Dated 9-5-2008. See AD compliance report in aircraft records for details.
CIW AD 2008-14-07 by inspection of fuel injection lines, all required clamps are in place, no defects noted. Next due at
712.8, annual 2008 or next nozzle removal.
• I certity that this En ine was inspected IIAfIN a 100 Hour Inspection and was determined to be in airworthy condition.
~
William Dorothy
&P 4816208161A
t<4.~I\.~d E~i\l\e
f~'jV\.~
i
I.n
o>:'+'R"~Qt)e'
a~1
~."I+ec. 5"d,vr~
IDll..ts l(<' 1~-:.s-C::>.~'5~1l~C)
YI~t-J c...H4 '8)16-1
J+<:("'-n..ss+~"fc.c-LP~~<...~e-c.K) j..»"J:)f"Fe~1j lUo1;!d yJ
U-l~-{\_
d
Mr •••
:
Summit Aviation LLC 2440SWAviation St. Bentonville,AR 72712
10-14-09 Tach. 660.5
N607DMEngine Log Entry
DATE
•
•
•
•
•
Performed 100 hour/AnnualllANI
FAR 43 App. D and Cessna T182T Maintenance Manual
Drained oil and inspected fitter, no abnormal contaminates noted.
.
Compression Test Results: #1 79/80, tr2. 78180, #3 79180, #4 78/80, #5 78/80, #6 78/BO.
Removed .all.spark plugs, cleaned, gapped, rotated, tested, and reinstalled W/New gaskets PIN M674.
Magneto timing checked good.
• Removed all fuel injector nozzles, cleaned in Sonic Cleaner, inspected and reinstalled W/New o-rings PIN 951391 I k
checked gOOd.
' ea
• Serviced engine W/8 Quarts Aeroshell 1fMl50 oil and New AA4811 0 oil filter.
• Checked ADs through ATP Revision Dated 10-21-2009. See AD compliance report in aircraft records for details
• CIW AD 2008-14-07 by inspection offuel injection lines, all required clamps are in place, no defects noted. Next' due at
760.5, annual 2008 or next nozzle removal.
• I
~g
~cted
IIA/W a 100 Hour Inspection and was determined to be in airworthy condition.
William Dorothy A&P 481620816
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;IGNATURE,
iE TYPE
BER
1an1nn\ri·lIe.AR 72712
N607DM En
• ~
·X
-o.r_-
firer
• :.cr:;-ess.or. -est Resurts: #118• ~e"""oved aD spark plugs, cleaned, gappeo. rota ~. ,""" ........._ _ __
.~">"IEC
~TURE,
'PE
a:1C .....s:>eCteC
ed,
• R.eplaced both magnetos WlNew (2 each) Slick MIN 6361, SIN Rigr: J:~71
WlNfNi gasket PIN AEL 12681.
• Serviced engine W/8 Quarts Aeroshell W80 Plus oil and New AA48110-2
fNI gaskets PIN M674,
and SIN Left 10040985. Installed each
,
011 fitter..
,
.
• Checked ADs through ATP Revision Dated 11-1-2010. See AD compiance report In aircraft records for details.
• CIW AD 2008-14-07 by inspection of fuel injection lines, all required clamps are in place, no defects noted. Next due at
817.4 or next nozzle removal.
..
• I certify that this n in was inspected IIAIW a 100 Hour Inspection and was determined to be in airworthy condition.
vdf;
William Dorothy A&P 3504028 IA
DATE
Summit Aviation LLC 2440 SW Aviation St. Bentonville, AR 72712
12-8-2011. Tach. 772.3
N607DM Engine Log Entry
•
•
•
•
•
•
•
•
Performed 100 hour/AnnualllAIW
FAR 43 App. D and Cessna T182T Maintenan~ Manual.
Drained oil and inspected filter, no abnormal contaminates noted.
Compression Test Results: #179/80, #2 78/80, #3 78/80, #4 78/80, #5 78/80, #6 78/80.
Removed all spark plugs, cleaned, gapped, rotated, tested, and reinstalled W/New gaskets PIN UM674.
Magneto timing check good.
Serviced engine W/8 Quarts Aeroshell W80 Plus oil and New AA48110-2 oil filter.
Checked ADs through ATP Revision Dated 12-5-2011. See AD compliance report in aircraft records for details.
CIW AD 2008-14-07 by inspection of fuel injection lines, all required clamps are in place, no defects noted. Next due at
872.3 or next nozzle removal.
• Removed all fuel nozzles, cleaned in sonic cleaner, inspected and reinstalled W/New o-rings PIN 951391.
• Performed engine run and noted rated manifold pressure and RMP could be not obtained with oil temperature at 150 ".
Adjusted MFP up to 32" and RPM to 2350 at 150· oil temperature.
• Engine run and leak checked good.
• I certify:~
a.di.
--
was inspected IfAIW a 100 Hour Inspection and was determined to be in airworthy condition.
A&P
536946158
IA
URE,
E
--
_----
Summit Aviation LLC 2440 SW Aviation
1-6-2012
St. Bentonville, AR 72712
Tach. 773.4
N607DM Engine Log Entry
• Removed all intake tubes and interconnect hoses. Re-swaged all oil sump intake adapter tubes and leak checked good.
Reinstalled all intake tubes WlNew interconnect hoses (6 each) PIN 69603 and tube to cylinder gaskets (6 each) PIN
71973. Induction system pressure tested good.
• Checked internal gear timing, gear timing checked good. Reinstalled #2 rocker cover W/New gasket PIN 75906.
• Removed turbo waste gate for inspection. Found waste gate seized. Replaced turbo charger waste gate assembly
W/Overhauled unit PIN 470954-1, SIN IF0113. Overhaul performed by Approved Turbo Components Inc., see FAA Form
8130-3 tracking number 002264 and work order number 31649 dated Jan. 5, 2012. Installed WlNew fitting o-rings and
flange gaskets (2 each) PIN 75845. Performed engine run, adjusted max MFP to 32" and adjusted idle and idle mixture.
Operational and leak checked good.
e;;:~p~
HOBBS: 879.2
N607DM
TACH:800.7
05/29/2012
REMOVED OIL AND FILTER. EXAMINED FILTER FOR METAL CONTAMINATION & FOUND NONE.
INSTALLED NEW CH48110-1 OIL FILTER. SERVrCED ENGINE WITH AERO SHELL WIOO PLUS OIL.
PERFORMED COMPRESSION CHECK: #1 77/80 #2 76/80 #3 78/80 #4 77180 #5 77/80 #675/80. GROUND
RUN PERFORMED. ALL SYSTEMS OPERA TED NORMALLY. NO EVIDENCE OF LEAKS.
JOhnGe~fi
~3~
MAINTENANCE
DATE
TOTAL TIME
IN SERVICE
HOURS
10THS
RECORD
DESCRIPTION OF THE WORK PERFORMED
AUTHORIZED SIGNATURE,
CERTIFICATE TYPE
& NUMBER