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aircraft technical logs - Quality Aircraft Sales

•
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Transport
Transports
Canada
Canada
TP3909E
AIRCRAFT
TECHNICAL
LOGS
Section 2. RECORD OF INSTALLATIONS &
MODIFICATIONS TO AIRCRAFT
Aeronautical Standards and
Legislation Branch
Canada
•
AIRFRAME LOG
1.
Nationality and Registration
~-
Manufacturer's Designation
3.
Record of
(a)
(b)
(c)
(d)
(e)
(f)
Lt .S ,
~~~~~~~~~~~~~~~~
LL Cooo - 2., 1510
~~~~~~-=....:..:::....::.__~~~~~~~
Engine Installations
Propeller Installations
Airworthiness Directives (A/D)
Service Bulletins (S/B)
Special Inspections (S/I)
Modifications (MODS)
1
RECORD OF ENGINE 8c
ENGINE OR PROPELLER
MAKE a: MODEL
DATE
I
,,
_ ..!>/~'5/0t)
.-u~ ~
&.oo" ' O
V
/
A~ ->d..11<:/-
.J>,...._
,
SERIAL N O.
-
__.:;:
POSITION
C ATE
INSTAL LED
PROPELLER
DAT E
REMOVED
R E MARKS
......
/
'
-
-
--·
-
~--
-
-
-~
-
IN STALLATIO N
R E ASON F O R C HAN G E
SIGNAT URE
LICENCE
NUMSE ..
'I
SJ rJ <JD L/ I
RECORD OF AIRFRAME
1
AIRWORTHINESS DIRECTIVES (A/Dl, SERVICE BULLETINS (S/Bl,
SPECIAL INSPECTIONS (S/ll AND MODIFICATIONS (MOos·J
WORK
OR
INS PECTION
PERFORMED
7'8<18Hr~s
Learjet
- - -c anada1r
The following Airworthiness Directives were como rtect w1·th
' 1-JA.D. 74-08-09 Rev.2 Amendment 39-96~0, C/W Inspection of Lavatory Paper and Linen Waste Receptacles_
With No Defects Noted. Next Inspection due at 4,986.9 AJC hours.
" ~ AD. 95-17-14 Amendment 39-9344, C/W paragraph (a) steps 1 thru 4 - Fuctional Test HSTA Brake_ With No
Defects Noted. Next lnsoection due at 4,086.9 AJC hours
~~ AD
97-24-02 Amendment 39-10209, C/W paragraph (b) (1) Inspection of the Under.fl
p
Bulkh d t
· ·
.
.
oor ressure
ea a
F.S. 409.00 - With No Defects Noted.
Next Insoectton Due At 2,568 AJC Landines
The following Service Bulletms were complied Wt"th
601-0482 C/W Paragraph 2B Modifi~ation-Hvdraulic Tubes-Main Landing Gear_ Install New Re-Routed Tubes
A601 0443 Rev.2 C/W Part 2A Soec1al Check- HSTA Overspeed Condition. Next due at ,
• A/C hours
4 086 9
601-0501 Rev N/C - C/W Paragraph 2A,2B,2C, and 2D Special Check- Inspection of th U d r11
p
.
e n e oor ressure
Bulkhead at F.S. 409.00 Wtth No Defects Noted.
Next Inspection Due At 2,568 A/C Landings
Reference Work Order No .. 82051604115.
...-?~/
/?
Dated:
12 Dec 1997 Signed:
~~ For:
Ron P. Kuphal
Bombardier Aviation Services, 1 Bradley Int') Airport, Windsor Locks CT. 06096-1086
'
Certified Repair Station No. SH5Rl97N
--
RECORD OF AIRFRAME
AIRWORTHINESS DIRECTIVES (A/D), SERVICE BULLETINS (S/8),
A / D,
S/ B,
S/ I,
MODS
DETAILS
OF
2
SPECIAL INSPECTIONS (5/1) AND MODIFICATIONS (MODS)
WORK
OR
INSPECTION
PERFORMED
'jo ·-Oo i
CRSVJ1R560K
AUG~
't 1998
I ?rVZosFo
(o.\-ec_~ : JCL ~~JL.\J";>
;.~~
.~
Cl. ..~
t/rY-Zcsto
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M-~-l~
\ {l~(o~O
-
\l\'{-7oSlo
111 fzo.ITG
3
RECORD OF AIRFRAME
SPECIAL INSPECTIONS (5/1) AND MODIFICATIONS (MODSJ
AIRWORTHIN ESS DIRECTIVES (A/D), SERVICE BULLETINS (S/B ),
A/ D,
DATE
Ob- .;i~
- 0 1~
AD
S/B ,
S/I,
MODS
DETA I L S
W OR K
OF
OR
INSPECT IO N
P ER F ORMED
SIGNATURE
qs-Cl~-01
I. Complied wi th Federal Mogual Service Bulletin No. MS 17976-2-24-001 (dated 14 May 99) - Electrical Power _ D.C.
Generation - TRU AC Filter Capacitor Inspection. Paragraphs 2A, B, C, D, and E.
DlNCAN
2. Complied with the following Bombardier Service Bulletin Nos.:
a) A60 1-038 I, Revision 2, dated 27 Jan 92 - Special Check I Modification - Pressure Refuel I Defuel System Relocation
of Sensing Lines. Verified installation of Jumper S/B was previously complied with.
b) 60 I -050 I. dated 12 Sept 97 - Special Check - Inspection of the Underfloor Pressure Bulkhead at F.S. 409 .00. Found
crack. To be re-inspected by 2852 Landings, repaired by 3352 Landings.
c) 60 1-0513, dated 3 I Mar 0 I - Modificati on - Engine Standby and APU Fuel Feed Systems Replacement of Flexible
Fuel Hoses. Paragraph 2A, B, C, D and E.
d) 601-0528, dated I 7 Oct 00 - Special Check I Modification - APU - Prevention of Fuselage Skin Heat Damage Under
and A ft of the Exhaust Shield .. Paragraphs 2A, B (Part A}, C {Part B), D (Part C), E, and F.
e) A60 I -0540, dated 8 Dec 00 - Special Check - Flaps - Visually Examine Flap Actuator Beam Bane Brackets for
Possible Cracks.
f) 601-1084, Revision I, dated 15 Dec 99- Special Check / Modification -Thrust Reversers Blocker Doors and Sound
Attenuating Material Panels. Completed Part C . . Repaired L/H and R/H Diverter in accordan ce with SRM PSP 607
Chapter 54.
'
'
g) 60 J - J I 00, dated 29 Sept 00 - Special Check I Rework - Thrust Reverser - Examine Condition of Act uator Attachment
Fittings. Paragraph 2A, B, C, D and E.
3. Complied with the following Airworthiness Directives Nos.:
a)- 95-17- I4, Part (a) - HSTA Brake Ops Test. ext inspection due in I00 hours or at 5679.4 hours. No defects noted at
this time.
~ 97-24-02, in accordance with S/B 601-050 I, dated Sept 12, I 997 - Special Check - Inspection of the Under Floor
At F.S. 409.00. .Paragraphs 2A, B{l),
·
d
Pressure Bulkhead
.
. (2), (5), D, and D· Crack was noted . Mus t be re-mspccte
by 2852 Landmgs
and
must
be
repaired
by
3352
landmgs
or
12
months
from
date
of
sim
off
I
·
h
ti
. .
.
.
,,.1- , w 11c ever comes 1rst.
c)'- 97-25- 1I, Rev1s1on I - NI A by aircraft sen al number.
'"'P s;gn ~~
J-;;2C:,- 0
Date
)
J\llidcoast Aviation, Inc., CRS R03R822L
# 14 Arch view Drive
Cahokia, IL 62206
11- Z.'=- ·c. I
.,).1-0,
o/-oCZ -o
?-II -oz.
AVIATION
I!.
Supplemental Log Entry
N953FA CL-601 SIN 5041 Date: August 22, 2001
Reference DQcket No. 2001-CE-22-AD; Amendment 39-1 2352;
AD 2001-15-17"'-i
fJ.'_ _._
- -- -.:
This AD does not apply due to CTL-92 p/n 622-6523-205 sin 3652 that is unaffected by
the above AD, transponder control head installed in this A/C.
All maintenance performed on this aircraft was performed in accordance with current
FAA regulations and manufacturer's requirements, and found to be airworthy.
The maintenance described above complies with FAR 43. A detailed record is on file
under Work Or~ BKB2A
Inspected By(~ · ~
For Duncan Avionics-TeterbOT;,NJRS XJRR155L
LICENCE
NUMBER
RECORD OF AIRFRAME
A IRWORTHINESS DIRECTIVES (A/D), SERVICE BULLETINS (S/B ),
D ATE
A / D,
S/ B ,
S/ I,
MODS
I
DET AILS
OF
SERIAL NUMBER:
5041
3. Complied with tti follow ing Bombardier Canadair C hallenger Service Bulletins (S.B.) and Airwonhiness Directives (A.O.):
a) S .B. 60 1-0290, evision 2, dated 15 May 93 - Auxiliary Power Un it (APU) - Modification - Exhaust Shield - Crack Prevention.
Previously comph with.
b) S.B. 60 1-0318. Revi · n 2, dated 25 May 93 - Modification - NACA Scoop Vent Line - Deletion of Check Valve. Found prel'iously
complied with.
c) S. B. 601-0372. Revision 2, ated 30 May 99 - Cabin Fuselage Floor Structure Improved. No funher action required .
d) S.B. A60 1-0443 - HSTA Ove eed Condition. Ops Check good. Next due 100 Hours.
e) S.B. 601-0478. dated 3 1 Jan 96 - o · ,,cation - Introduction of a Lead Acid Battery I Charger for IRS No. I , No. 2 and No. 3.
Only No. I and No. 2 IRS complie
No. 3 IRS not installed.
f)
S.B. 601 -050 1, dated 12 Sept 97 - lnspc i of the Undern oor Pressure Bu lkhead at FS. 409.00. Sec Item 4s) for Inspection Interval.
g) S.B. 601-0526. Revision I, dated 3 I Oct
Special Check I Modi fication - Weight-on-\Vl1ecl Proximi ty Switches_ Prevent
Uncommanded Deployment of the Air Drive
'{!Wrator on the Ground. Found no funher action required.
h) S .B. A601 -0532, Revision I, dated 8 July 02 - S ~~_Check I Modification - Flaps - Inspect Vane Brackets for Cracks, Replace
· Surfaces. Pan B only (Check for cracked gaps). Next du e 600 L a ndings.
Brackets and Remove Gaps Between Brackets an
· o n~ng Units - Replacement of Existing Relays K.2000HG and K.200 1HG
i)
S.B. 601-0533, dated 28 Feb 02 - Modification - Air
with 5-Second Delay Relays. Part A and B
J)
S .B. 601-0534 , dated 28 Sept 01 - Modification - Batt
·'k_nversion of the Main Battery PIN: 600-59 15 1- 11 to a -1 3.
Not applicable.
. 11
k) S . B. 601-0537, dated 31 Aug OJ - Modification - Main Fra m~
fa Liquid Dencctor Around Aft Equipment Compartment
Door.
~
I)
S .B. 60 I -0 545, dated 29 July 0 I - Special Check I Rework - ~'11"""~1!:
Uplock Pin for Jammed Condition.
m) S.B. A60 J-0550, dated I 5 Apr 02 - Special C heck I Rework - Stall Pr
Check and Rework of Out-of-Tolerance AOA Transducer Assemblies. Pa
. ~rt C items I . 8, Io_ I 5.
I) UH AOA Baseline Resistance - 62 1 Ohms
2) R/H AOA Basel ine Resistance - 6 19 Ohms
~
'
$'.3
n)
o)
p)
q)
r)
s)
t)
u)
Next due 300 Hours.
.
.
.
.
~'\Q,,
S .B. 60 1- 1098, dated 30 Oct 98 - Mod1ficat1on - Oil Storage - Replacement of 0 11 Ta nk_,~ £lains. Right No. 2 Engine only.
A.D. 74-08-09, Revision 2 - Inspect ion of Lavatory Receptacle. Nex t due 1000 Hours.
~
~
A.D. 95- 17- 14 - Functional Test HSTA Brake. Part A. Ops Check good. Next due 100 H o u r~
A. D. 95-22-0 1 - Mod ALC Lighting
6'
<'.::--'
A.D. 2001- 12-06 - Check No. I and No. 2 Engine Chip Detectors. Part A. Next due JOO fl o urs.
_,:¥ 'l'A. D. 2002-06-05 - Check Transponders. Not applicable.
/ "'\.
A.D . 2002-06-06 - Check Transponders. Not applicable.
A.D . 2002-13-07- Check IRU . Not applicable.
(
>
'.'?
Jnsp.S1gn _~~~
Date
~="'.L.
A.~:._z=-------­
M idcoast Aviat ion, Inc., CRS R03R822L
111 4 Arclwicw Drive
Cahokia, IL 62206
MIDCOAST
MODIFICATION LOGBOOK ENTRY
C HALLENGER CL601-3A
REGISTRATION NUMBER:
\IRCRAFT HOURS:
MODIFICATION LOGBOOK E NTRY
N953FA
4
CORRECTED COPY
N953FA
5879
SERIAL NUMBER:
LANDINGS:
5041
2867
Complied wi th the follo wing Bombardier Canadair Challenger Service Bulletins (S.B.) and Airworthiness Directives (A. O.):
a) S.B. 60 1-0290, Revision 2, dated 15 May 93 - Auxiliary Power Uni t (APU) - Modifica ti on - Exhaust Shi eld - Crack Preven tion.
Prev iously complied with.
b) S.B. 601 -0318, Revision 2, dated 25 May 93 - Modification - NACA Scoop Vent Line - Deletion of Check Valve. Found previously
complied with.
c) S.B. 601-0372, Revi sion 2, dated 30 May 99 - Cabin Fuselage Floor Structure Improved. No further action required.
d) S.B. A60 1-0443 - HSTA Overspeed Condi tion. Ops Check good. Next due 100 Hours.
e) S. B. 601 -0478, dated 3 1 Jan 96 - Modifi cation - Introduction of a Lead Acid Battery I Charger for IRS No . I, No. 2 and No. 3.
Only No. I and No. 2 IRS complied with , No. 3 IRS not installed.
t)
S.B. 601-050 I, dated 12 Sept 97 - Inspecti on of the Underfloor Pressure Bul khead at FS. 409.00. See Item 4v) o f Aircraft Logbook
entry, dated August 22, 2002, for Inspection Interval.
g) S.B. 601-0526, Revis ion 1, dated 3 1 Oct 00 - Special Check I Modifi cation - Weight-on-Wheel Proximity Switches - Prevent
Uncommanded Dep loyment of the Air Driven Generator on the Ground. Found no further action required.
h) S. B. A60 1-0532, Revi sion 1, dated 8 Ju ly 02 - Special Check I Modification - Flaps - Inspect Vane Brackets for Cracks, Replace
Brackets and Remove Gaps Between Brackets and Mating Surfaces. Part B only (Check fo r cracked gaps). Next due 600 Landings.
i)
S.B. 60 1-0533, dated 28 Feb 02 - Modification - Air Conditioning Units - Replacement of Existing Relays K2000HG and 1<2001 HG
with 5-Second Delay Relays. Part A and B only.
j)
S.B. 60 1-0534, dated 28 Sept 0 I - Modi fi cation - Battery System - Conversion of the Mai n Battery PIN: 600-59 15 1-11 to a - 13.
Not app licable.
k) S.B. 601 -053 7, dated 3 1 Aug 0 I - Modi ti cation - Main Frame - Additi on of a Liquid Deflector Around A ft Equipment Compartment
Door.
I)
S.B. 60 1-0545, dated 29 July 0 1 - Special Check I Rework - Nose Landing Gear (N LG) Extension and Retraction - Exami ne NLG
Uplock Pin fo r Jammed Condi tion.
m) S.B. A601-0550 , dated 15 Apr 02 - Special Check I Rework - Stall Protection System - Angle-o f-Attack (AO A) Transduce1 :'olerance
Check and Rework o_f Out-o_f-Tolcrance AOA Transducer Assemblies. :art A and B. ;art C items ~ - 8, I 0 - 15. ~
::..--k.:..
1) L/H AO A Baseline Resistance - 6'.tl Ohms "> Q:i ~ ::::..~ \ \ -1€. \•'"\UY 1~ f'_e...:.\ \)L..t>- 01 ,c\ cor:\~+-- _ -k'-'~ ~
2) R/HAOABasclineResistance--6+9-eltms /
Jt::_Q. ~£ ,,-~"-oi!.~-le--\ 'oA:.~ \·:.-,e ;?\l-R+ort.."":J °'" ~/ 11b ~. 'oy
Next due300Hours.
:>c. *- '4.u i.-~.°"- \ t: P.> . y~f"\.y~ fli.+-? ,9474,;i{,;r:f.
n) S.B. 601-1098, dated 30 Oct 98 - Modificatio n - Oi l Storage - Rep lacement o f Oil Tank Support Beams. Right No. 2 Engi ne on ly.
o) . A.D. 74-08-09, Revision 2 - Inspecti on o f Lavatory Receptacle. Next due 1000 Hours.
p)'\J A.O. 95-17-1 4 - Functional Test HSTA Brake. Part A. Ops Check good . Next due 100 Hours.
q) A.O. 95-22-01 - Mod ALC Lighting. Termination Action - no further action required.
r)
A.O. 97-24-02, dated December 3, 1997 - To Detect and Correct Fatigue Cracking in the Underfloor Pressure Bul khead of the
Fuselage. Refe rence S.B. 60 1-50 I . Bulkhead repaired. Re-inspect in 600 Landings or unti l alternate means of compliance received
from New York ACO.
s) A .O. 200 1- 12-06 - Check No. I and No. 2 Engine Ch ip Detectors. Part A. Next due 100 Hours.
t) "-...! A. O. 2002-06-05 - Check Transponders. Not applicable.
u) · A.O. 2002-06-06 - Check Transponders. Not applicable.
v) -.J A.D. 2002-1 3-07- Check !RU. Not applicabl e.
,
0
lnsp. Sign
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-
RECORD OF AIRFRAME
5
AIRWORTHINESS DIRECTIVES (A/D), SERVICE BULLETINS (S/B),
SPECIAL INSPECTIONS (S/I) AND MODIFICATIONS (MODSJ
LICENCE
I ~-~-~~~~_J_~~~~~~~~~~~~~-~
I
-------------------------------------i----------1---~~~--t--~
~~
~~
W OR K
DATE
A/D ,
S/B,
S/ I ,
MODS
DETAI L S
OR
I N S PE CTIO N
PERFORMED
SIGNAT U RE
NUM BE R
OF
----------------------------------1--------1----
~
BOMBARO IER
BOMBARDIER
AEROSPACE
Challenger CL600-2B16 SIN 5041
TTA: 6084.3
N953FA
LOGS: 2943
Airworthines s Directives (complied with the following)
95-17-14 Bombardier Amendment 39-9344 Compliance with SB A601 -0443 PART A satisfies the intent of this AD para (a).
Next due in 100-hours at 6184.3 TTAF
Airworthiness Directives (the following determin ed to be not applicable)
" ' 94-02-02 ROCKWELL COLLINS Amendment 39-8799 - Not applicable, affected equipment not installed.
' 97-04-15 PACIFIC SCIENTIFIC COMPANY Amendment 39-9940 - Not applicable , affected equipment not installed.
97-05-03 R1 ALLIEDSIGNAL AVIONICS INC Amendment 39-11064 - Not applicable, affected equipment not installed.
98-20-17 SAFT AMERICA INC Amendment 39-10784 - Not applicable, affected equipment not installed.
· 98-24-27 First Technology Fire and Safety Ltd Amendment 39-1 0914 - Not applicable, affected equipment not installed.
"-; 98-25-02 BFGOODRICH AVIONICS INC Amendment 39-1 0924 - Not applicable, affected equipment not installed.
-..........., 99-01-14 HONEYWELL Amendment 39-10979 - Not applicable, affected equipment not installed.
""' 99-04-10 TRANSPORT CATEGORY AIRPLANES Amendment 39-11034 - Not applicable, affected equipment not installed.
99-12-0 6 ALLIEDSIGNAL INC Amendment 39-11 190 - Not applicable, affected equipment not installed.
2001-02-05 BOMBARDIER INC Amendment 39-1 2089 - Not applicable, affected equipment not installed.
"" 2002-14-19 Rockwell Collins Inc Amendment 39-1 2819 - Not applicable, affected equipment not installed.
"'1 2002-20-09 Rockwell Collins Inc Amendment 39-12906 - Not applicable, affected equipment not installed.
""- 2002-21-01 Britax Sell GmbH & Co OHG Amendment 39-12907 - Not applicable, affected equipment not installed.
""' 2002-22-13 Rockwell Collins Inc Amendment 39-12939 - Not applicable, affected equipment not installed.
"°"
Service Bulletins (complied with the following)
A601-0443 R02 dated May 15/96 HST A - Overspeed Condition. Complied with PART A HSTA Brake operational check. No
defects noted. Next due in 100-hours at 6184.3 TTAF.
601-05511 dated Aug 30/2002 Modification - Fuselage Placards and Markings - Addition of Stow Rod Warning Decal
on Upper Core Cowl Door.
A601 -0554 dated Dec 12/2002 Special Check - Plates/Skins - Possible Development of Crack(s) on Lower Wing
Plank at WS148.02 (Rear Spar) Reinspect per th is SB each 2000-hours until TLMC Task 57-10-00-108 is revised.
A601 -0556 dated Jan 24/2003 Special Check/Rework - Wing Anti-Icing - Examine Piccolo Tube and Connecting
Duct Installation on Left and Right Wings. Com lied with PARTS A and D.
'-.~R/<"
- 19
~
SIGNATURE:
Date: 23 March 2003
W. . 107691
LEARJET, INC. CRS TJ4R546M, INDIANAPOLIS SERVICE CENTER
INDIANAPOLIS INT'L AIRPORT, INDIANAPOLIS, IN
Michael D. Davis for
----~--~~~~~~~~~~~~~------~~~~~--,--~--------,-----~
6
RECORD OF A IRFRAME
S PECIAL INSPECTIONS (S/I) AND MODIFICATIONS (MODS)
A IRWORTH INESS D IRECTIVES (A/D), SERVICE BU LLETI N S (S/ B ),
A/ D,
DAT E
S/ B,
S / I,
M ODS
D E T A I L S
WOR K
OF
OR
I NSPEC T I O N
P E R F ORMED
L IC E NC E
N U M B ER
SIGNATURE
- o~
-o4
-
T he tO IJ owmg Airworthiness Directives were comp iled w ith, or determined not applica ble:
95-1 7-14 Amendment 39-9344 dated 12 Sept 1995, Complied with paragraph (a)( I )-(4). Per AMOC letter dated IO May 1999 an
alternate means of compliance to paragraphs (b), (c)(4) and (d)(2). This approval is to allow repeat of the functional
check in paragraph (a) at intervals not to exceed 600 hours time in service fo r aircraft modi fied in accordance wi th Part
C of SIB AGO1-0443 R2. Next Due at 6,996.0 aircraft hours.
_ ·"-..., 99-23-22 RI Amendment 39- 11 4 73 Dated 29 Nov 1999. NI A by Mode "S" Transponders PIN 622-9210-003 Installed.
99-23-22 R2 Amendment 39-1 1686 Dated 20 Apr 2000. NI A bv Mode "S" Transoonders PIN 622-9210-003 Installed.
99-23-24 Amendment 39- 11420 Dated 06 Dec 1999. NIA by MFG.
2000-07-27 Amendment 39- 11 683 Dated 03 May 2000. NIA by PIN HG I075AE03 Installed.
2003-04-06 Amendment 39-13054 Dated 11 Mar 2003. NI A by FMZ-2000 installed.
-~ 2003-22-1 2 Amendment 39-13360 Dated 12 Dec 2003, - Complied with paragraphs (n) - To prevent flat spots of the AOA
transd~cers due to wear, which may cause ~delay in the commands for stall warning, stick shaker and stick pusher
operation. An Alternate Method of Compliance has been granted by the FAA in a letter dated March 29, 2004.
Reference PSP 601 A -5 T LMC fo r further inspection in te rva ls.
2003-26-1 4 Amendment 39- 13413 Dated 20 Feb 2004. NIA by MFG.
-
-~
~
-
-
The tio II owing se r v1ce B u II etms were comp I1e d Wit h:
A60 1-0443 R2, Complied with paragraph 2A Part A Special Check/Modification - Horizontal Stabilizer Trim Actuator
(HSTA) - Overspeed Condition. Part C was previously complied with on 14 Jun 2002 by installation of Pitch Trim
Actuator PIN 600-9230 1-65, SIN 258E. Next Inspection Due at 6,996.0 aircraft hours
601-05 15, C~m plied w~th p_aragraphs 2A, 28, 2C, 2D, and 2E- Modification - Static Discharger- Installation of Additional
W111glet Static Discharger
60 1-0538 CIW Para.2~, B, _c, D, E and G on Left Engin~ Only._ Right Engine was Previously Complied With _ Special
Check!Mod1ficat1on - Eng111e Controls - Possible Fail ure of Engi ne Throttle Push/Pull Control-Assembly
60 1-0546 Rev. I, Complied with paragraph 2B Part A, 2D and E - Modification-N LG and MLG System-NLG and MLG
Component Serialization. Part B to be co mo lied with orior to, or at the next IO year insoection.
A60 1-0550 Rev 0 I Special Check Stall Protection System Angle-of-Attack (AOA) Transducer Assembly Tolerance Check
and R.eplacement of Out-of-Tolerance AOA Transducer ~ssemblies. Repetitive C heck to Pa rt c is no Lon er
Required. Reference PSP 601 A -5 TLMC for fu rther msoection intervals.
g
d A d
601-0552 RI , Complied with paragraphs 2A, 28 Part A( l)-(3), 2D and 2E. Special Check Mod ification _ w· Pl
Markings - Painted Overwin_g Anti-Slio Walkway. No defects noted.
mg acar s n
601-0553 Complied with paragraphs 2A, 2B, 2C, 2D, and 2F - Modification-Wing Flap System-Serialization of the Ela
Actuator Beams.
p
60 1-0554 RI , SIB is NIA by Effectivity.
601-0558, S/B is NIA by PIN 55540-5 Valves Installed.
60 1-056 1, Comp I ied
with paragraphs 2A, 2B( I )(2), 2D, and 2E - Special Check/Rework _ Wiring - pOSSI·ble Clia fimg n
.
0
Electrical Harness Located On The APU Support Structure. No defects noted.
Messier- Dowty _SIB M- DT SB6 l 00-32-10, Co~p l ied wi th paragraphs 2A and 2B,and 3A _ CL60 1 MLG Shock Strut _ Add a
Seri al Number to the Shock Strut Pms.
Messier-Dowty S/B M- DT SB7300-32- l 6, Complied wi th paragraphs 2A, 2E and 3A CL60 I NLG Sh k S
dd p
.
•
oc trut-A
art and
Serial Numbers to Components.
Reference work order No.: 11 4005, and a
has been prooioed to t~e owner/operator.
c1;
Dated :
I 0 Agr 2004
Signed :
'-"f)
~
-R. ~ ~
·- 1
-
--·- ~
..
-·
l
-·
--- ~
-
----~ "
-
1
fo r:
Leo R. Balboni
Learjet Inc., I Bradley Int'! Airport, Windsor Locks, CT. 06096- 1086
Certified Repai r Station No. SH5R I97N
------ -
--------
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