~SANTA MONICA ~PROPELLER - aso.com · This propeller was inspected and serviced IA W Hartzell Service Manual and the following work was performed. Filed and dressed propeller. All

~SANTA MONICA ~PROPELLER

Propeller Logbook

3135 DONALD DOUGLAS LOOPS, SANTA MONICA, CALIF. 90405-6186 PHONE #: 1-800-421 -9995

FAA ARS ZY2R362L

_;__~-------- ---- -- ·-- -- - - -

PROPELLER MAINTENANCE RECORD

LEFl ENGINE

No 1 --------'~-~------

No 2 - -------'Y--

No. 3 ----+--~------No. 4 -----~-----~------

No. 5 --~---------~~------

PITCH RANGE

Low __ ____:: ___ _

------------- Reverse -~-

-----------------------~-----~---

RIGHT EN~E 2 JF Hub Model 1/H-C.. -J 3 'if -Blade Des1gn --pc_ 7 (,'t; . 5 D JS D1ameter 7 J }/

802-~ Hub Ser. No.

Blade Ser. Nos. -=:---==--::::;:oor-::--:--:----

No. 1 _ _.!:=E~il.L--+-5-:~lf_~..6~--No. 2 & 6?'i:?L

No 4 - -------------------------No. 5 - -----------------------

~/4- PITCH RANGE rJ O

~ 20·t'c Low /~ Feather Rt/ 0) cJ Reverse ~ Governor Model

DESCRIPTION OF ALL OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES.

SERVICE BULLETINS. SERVICE LETTERS. & MINOR ADJUSTMENTS

DESCRIPTION OF All OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES.

SERVICE BULLETINS. SERVICE LETTERS. ~& MINOR ADJUSTMENTS

. ~ - VV\ 0 .-- l./

DATE TACH TIME

DESCRIPTION OF All OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES.


DESCRIPTION OF WORK

F& 13362 Edinburgh Drive

Westminster, CA 92683 562- 595-4264

SIGNATURE

Propeller: PHC-J3YF-2UF Serial# ED2525 N40PG Aircraft TT: 3814.6 SMOH: 169.6 Prop TT: 3814.6

Tach: 0 Hobbs: 2743.8 Total Time: 3814.6 This propeller was inspected and serviced IA W Hartzell Service Manual and the following work was performed. Filed and dressed propeller. All work done using manual as reference. I certify that this propeller has been inspected in accordance with 100 hour/annual inspection and was determined to be in airworthy condition.

---------,----------------------------------------END--------------------------------------------------------------

Date: July 8, 2010 Ward Foley, 3247648IA UA r ~ / v

DATE TACH TIME

DESCRIPTION OF ALL OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES.


DESCRIPTION OF WORK

~~ 13362 Edinburgh Drive

Westminster, CA 92683 562- 595-4264

SIGNATURE

Propeller: PHC-J3YF -2UF Serial # ED2525 N40PG Aircraft TT: 3913.5 SMOH: 268.5 Prop TT: 3913.5

Tach: 0 Hobbs: 2842.7 Total TT: 3913.5 This propeller was inspected and serviced lAW Hartzell Service Manual and the following work was performed. Filed and dressed propeller. All work done using manual as reference. I certify that this propeller has been inspected in accordance with 100 hour/annual inspection and was determined to be in airworthy condition.

--~::~--~:~-~-~:-~~~---------------~~:::~.--;:~~=~:TAJ]: _____ C£:_7 __ . v

--.._J'-=--___. __________ - ~ ---- ------- -

DATE TACH TIME

DESCRIPTION OF ALL OPERATIONS PERniNING TO AIRWORTHINESS DIRECTIVES.


DESCRIPTION OF WORK

~ FacEY'S 13362 Edinburgh Drive

Westminster, CA 92683 562- 595-4264

Propeller: Hartzell PHC-J3YF-2UF Serial # ED2525 Aircraft TT: 4000.5 SMOH: 355.5 Prop TT: 4000.5

SIGNATURE

N40PG Hobbs: 2929.7

This propeller was inspected and serviced in accordance with Hartzell Service Manual and following work was performed. Removed propeller this date and time for reseal only by Santa Monica Propeller (see invoice). File and dress propeller. All work done using manuals as reference. See AD list for all current A.D. 's. I certify that this propeller has been inspected in accordance with 100 hour/annual inspection and was determined to be in airworthy condition.

---:~~--~~;~-:-~:~:;~---------------:::EF:~.--~~~~=~=~---~

...

-DESCRIPTION OF All OPERATIONS

PERTAINING TO AIRWORTHINESS DIRECTIVES. SERVICE BULLETINS. SERVICE LETTERS.

& MINOR ADJUSTMENTS

------ ------- --

SERVICE BULLETINS

A D's _______ _

0 /H MANUAL # 33092A & TSP1555

~QD~-p~7 OF OKLAHOMA, INC.

FAA APPROVED REPAIR STATION

CRS # RV3R829l

2740 N. SHERIDAN - TULSA, OK 741 15

800-255-9924- PH .918-835-9924 - FAX 918-835-3681

MAINTENANCE TRAVELER

P.O.# ____ _

SHIP VIA, ____ _

{6VERHAliD flEPAIR @!fA~ SAtf"""

CUSTOMER ___ __,__f\l\__,\_._K.,...,:-t..-::;__~=-.;:..;o..;.::s±~\ ...... vo~. __,__ ___ ~ORK ORDER ~~So 1 2-oo<l£/8 DATE I ~- \\j- \<t

GOVERNOR ~hl £ ~ ... Constanl, Speed """"'t.,

PIN __ =B=-2::....:1 0::...:7-=l ....::.O _____ ___ ~~FG. ___ w_oO_D_W'-AA'-D'---___ __ .stN\:lio (\~C>

Drive Gear ~$, Idler Stud clo< Speeder Spring 0\<. Spool~ldler Gear <k Cap_LSp. Adj . Shaft ci( Housing o\( Relief Valve o¥,. Flyweight §)\(

Return Spring -n\s. Flyweight Pins Q\( Assemble / Test U'k-

Feathering _ __.V''---- Unfeathering,__ __ ../ _ _ _

Idler Bearing

Sp . Rack -

o\6.. Relief Spring El\( Control A rm $ K

Synchronized_---=../ __ _

Magnetic Pickup fil.... Coil o\( Motor Potentiomet er ___ Micro SW Uft Rod o\<. Unfeathering Rod_olf

Unfeathering Valve o\( Unfeathering Actuator oK Assemble ..1 Test Q):..

Turbo ____ _ . Primary ___ _ Overspeed, ____ _

Spring Reset ___ _;Pitch lock Solenoid _ _ __ Lever A.s.sy. Reset Post ____ Reset Switch ____ Orifice Bleed Air_-_ _ _

Lelnrilleed· Air ~--- -Feather "Switch, ___ _ · . Lever A ssy . Orifice _,Link Blee.dJ\ir Plung~r Beta Valve_ - --

(Shaft Airbleed Reset) - Pin Locating Return Spring Air Bleed Link Eccentric Reset ___ _

A ssemble Test -

PART II & NAME p 0,# QUANTITY · COS! 182 61 8 SEAL 1 182621 1

182 64 9 " 1 182738 II 1 182798 II -1 182799 II .., 1 206336 II 1 1137--82 8 S£AL NUT 1 1355-168 SEAL 1 3053-032 GASK . 1

"3053-034 " l 230625 II l

BRNG. 1 II 1 LABOR ________________________ _

1 419-534 PINS 2 3949-02 0 RETAINERS 2 PARTS ________________________ __

.2.l..Q.fr) 1 IDLER STUD l \~\ <b- ~\\.\ RACE 1 SUBTOTAL ____________________ __

TAX __________________________ _

FREIGHT ______________ __ _

MECHANIC INSPECTOR

1. Approving National Aviation 2 .

AUTHORIZED RELEASE CERTIFICATE 3. Form Tracking Number:

Authority/Country:

FANUNITED STATES FAA FORM 8130-3 AIRWORTHI~ESS APPROVAL TAG AA091412

4. Organization Name and Address: AIRCRAFT ACCESSORIES OF OKLAHOMA IN¢. 5. Work order/Contract/Invoice

2740 North Sheridan I Number: S012-00848

Tulsa, OK 74115 6. 1tem: 7 . Description: 8. Part number: 9. Eligibility: • 10. Quantity: 11 . SeriaVBatch Number: 12. Status I Work:

1 GOVERNOR 8210710 NIA I 1 2126960V OVERHAULED

I 13. Remarks: THE PART IDENTIFIED ABOVE WAS OVERHAULED IN ACCORDANfE WITH FAA APPROVED DATA THERE ARE NO APPLICABLE AIR

WORTHINESS DIRECTIVES. WORK ORDER S012-00848 SHOW1Nf THE ACTUAL WORK PERFORMED IS ON FILE AT THIS FACILITY.

I I

I . I .. I . -

-

~~-~=,~~~;,~,~ 19. ~ 14 CFR 43.9 Return to Service 0 Other regulations specified in Block 13

in a condition for safe operation. j Certifies that unless otherwise specified in Block 13: the work identified in Block 12 and described in Block 13 was accomplished in accordance with Trtle 14, Code of

pecifJed in Block 13. I Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

15. Authorized Signature

/< 16. Approval Authorization No:

1 20A~hM'~~ ~ 21. Approval Certificate Number:

RV3R 8 29 L

~

~ 18Da1e~ 22. Name (Typed or Printed): 23. Date:

DAVID DUTTON September 14, 2012

User/Installer Re jponsibilities

It is important to understand that the existence of this Document alone does not automatically constitut authority to install the part/componenVassembly. Where the user/installer performs work in accordance with the national regulations of an airworthines+hority different than the airworthiness authority of the country specified in Block 1, it is essential that the user/installer insures that his/her airworthiness authority accepts parts/ ponents/assemblies from the airworthiness authority of the country specified in

Block 1. I

Statements in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintencrce records must contain an installation certification issued in accordance with the

national regulations by the user/installer before the aircraft may be flown. , I

F rm 8130-3 ~01 FAA o • Installer must cross-check er ibili 19 ty with applicable technical data. NSN: 0052..()()..()12-9005

TACH TIME

--DESCRIPTION OF All !fPERATIDNS

PERTAINING TO AIRWORTHINESS DIRECTIVES. SERVICE BUllETINS. SERVICE lETTERS.

& MINOR ADJUSTMENTS

DESCRIPTION OF WORK

13362 Edinburgh Drive Westminster, CA 92683

562- 595-4264

SIGNATURE

Propeller: Hartzell PHC-J3YF-2UF Serial# ED-2525 N40PG Aircraft TT: 4032.8 Prop TT: 4032.8 SMOH Prop: 387.8 (02-27-09) Hobbs: 26.1

This propeller was inspected and serviced in accordance with Hartzell Service Manual. The following work was performed: Dressed and filed propeller. All work done using manual as reference. See AD list for all current A.D.'s. I certify that this propeller has been inspected in accordance with FAR43, apex. D, using Hartzell and Beech service manuals as reference. This propeller was inspected in accordance with a 100 hour inspection and current Federal Aviation Administration regulations and was determined to be in airworthy condition.

-------------------------------------------------~~-------------------------------------------~-~-------- ;I

Date: July 22, 2013 Ward Foley, 3247648IA."""l,...J=-:~'-----"""<---'~'-----=--_;:

,l;t~s I 3362 Edinburgh Drive

Westminster, CA 92683 562- 595-4264

Beech Baron 58P Serial# TJ-309 N40PG Hobbs: 128.8 Aircraft IT: 4135.5 RH Prop: Hartzell PHC-J3YF-2UF RH Serial#: ED2525 RH Prop TT: 4135.5 RH Prop SMOH: 490.5 (02/27109)

This propeller was inspected and serviced in accordance with Hartzell and Beechcraft service manuals. The following work was performed: File and dress propeller. All work done using manuals as reference. See AD. list for all current AD. ' s. I certify this propeller has been inspected in accordance with FAR43, apex D, using Hartzell and Beechcraft service manuals as reference. This propeller was inspected in accordance with a 100 hour inspection and current Federal Aviation Administration

re~~:~~~~~~~~~~~~~-~-~!~~s~;:~;~64-s~td-=-.:t-~ - - - .. ..

Aa!SANTA MONICA f(((lf; PROPELLER

..

N 4oJ?7 Left 0 Right

AMERICAN PROPELLER SERVICE A DMSION OF AMERITECH INDUSTRIES. INC.

20208 Charlanne Drive Redding, California 96002, U.S .A.

Phone Number (530) 221-44 70 I (800) 292-PROP (7767) FAA REPAIR STATION #N03R717L E-mail: [email protected]

PROPELLER LOGBOOK

0 Left Engine


Propeller Manufacturer: ---'-H....:...;...;~...:..fl.._n.;_;_;~::;..-(...::;..L=----------

f2J Right Engine D Front Engine

Hub Model No. PH C.- :J3Y F · Z.(A F Hub Serial No. ED 2 S" .l S Blade Model No. E C. i (, (, "'3 0 fl... B Blade Serial No. 1 -:::::{;::-(,~9=-=B==G...:.-Ll.---------

No.2 ~ ~99oc./ No. 3 CSot9/ 0 No. 4 _______________ _

No. 5 ________________ _

PITCH RANGE

D Rear Engine

Low _ ___.:_/...::5~·:....::3~0 ___ lA~ 20 . 8° nu. o6 Feather ___ --=o;;....,...;........;;;;....._ _____ Reverse------

Pitch-------------

Governor Manufacturer:-------------

Governor Model No.---------------

Governor Serial No.----------------

DATE

7 -12.-01

.

-

DESCRIPTION OF ALL OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES,

SERVICE BULLETINS, SERVICE LETTERS, & MINOR ADJUSTMENTS

TACH DESCRIPTION OF WORK SIGNATURE TIME

·~ AMERICAN PROPELLER SERVICE REPAIR STATION No. N03R717L 20208 CHARLANNE DRIVE ,.,. REDDING, CA 96002

WORK ACCOMPUSHED f ~m PL,£ '1'CS OV£/Z.~.4_(A £ MODELNo. e HC..· :r3 Y=·=!,1 ~ SERIALNO. f: Q:$ 2- S:

TiiE AIRCRAFT AND/OR COMPONENT IDENTIFIED ABOVE WAS REP AIRED AND INSPECTED IN ACCORDANCE WITii CURRENT FEDERAL AVIATION REGULATIONS AND IS APPROVED FOR RElURN TO SERVICE.

PERTINENT DETAILS OF TiiE REPAIR ARE ON FILE AT TiiiS AGENCY UNDER

WORK ORDER# 3073~

INVOICE# 419ili DATED: 7*12 - 0 }

TODD MARINKOVICH SI G F.D .:::>::sz:/) (Atn'HORIZ.ED INDIVIDUAL)

.---------- - - - - - -

DATE


SERVICE BULLETINS, SERVICE LETTERS,

TACH TIME

& MINOR ADJUSTMENTS

DESCRIPTION OF WORK

~,.AINTEt !ANCE A.f.l.... 1"1 . I I .. :v'i..;' ... '! ORl

SIGNATURE



DATE



DESCRIPTION OF WORK SIGNATURE

i . NSTAL L ATIDN • D PEA~TIDN • SERVICE ,

propeller owner's manual 1 -·

& log book

D.O.A. F.A.A. APPROVED MANUAL 115 L

" Compact" Models HC-C2Y, HC-C3Y, HC-F2Y, HC-F3Y, HC-F4Y,

HC-E2Y, HC-E3Y, HC-G2Y, HC-G3Y, (P)HC-L3Y,

BHC-L2Y, HC-H3Y, (P)HC-J3Y, BHC-J2Y, ( )HC-12Y, and ( )HC-M2Y - Constant Speed and Feathering

rr- 3CJ9 R./.1.

•

This manual will be periodically

updated.

October, 1979

· HARTZELL PROPELLER, INC. - PIQUA:<>HIO

allation of "L'', "K", "R", and "N" age Models HC-(C, E, F, G, H, J, L)(2, 3, [L, K, R)-(1, 2, 4,) all spinner adaptor ring to engine starter

!an engine shaft and propeller hub at

lrt the PRP-909-6 "0" ring into the groove inside the flange mounting. all propeller onto engine shaft. 'Ibrque the .ds used in the "I;' flange to 50 ft. lb. 'Ibrque bolts or studs used in the " I;' flange propel-0 ft. lb., the 1/2 bolts on studs used in the "R" flange propellers to 60-70 ft. lb., and :54 stud used in the "N'' flange propellers

lbs. Wire safety pairs of studs or bolts r. (Exception: For 10-720 engine, use b ft.) a ll spinner dome. The spinner nose is sup>y the cylinder, only for the feathering Wire safety the nut used to secure the nose

>TE: When installing the HC-E2YL-2BS lllers (which have spring kits installed) on 1A-30 or PA-39 aircraft, be sure that the inside of the engine shaft does not con-

,he spring assembly, consisting of: A-2488 e, 9-2410-31 spring, A-2487 thimble, and t}6 shim. These parts are no longer needed. llation of Models (B)HC-12YF-1( )F todels are identical to the (B)HC-C2YF~pt for the location of the blade centerline >ect to the shaft mounting surface. This is 1ctal 2 inch extension.

(B)HC-C2YF-1( ) - 3.25 inches (B}HC-12YF-1() - 5.25 inches

(


LEFT ENGINE

Hub Model _ ____________ _

Blade Design

Diameter - - --- ---- -----

HubSer. No.-- - --- - - - - - ---Blade Ser. Nos. ______ ______ __

No. 1 - -------- - - --- -No. 2 ___ ____ __ ~-----

No.3 _ ___ _ ___ _______ _

No.4 ____ ______ _ _____ _

PITCH RANGE

High ______ _ Low ________ _ _

Feather _ _ ___ _ Reverse _ ____ _

Governor Model

RIGHT ENGINE

Hub Model fJJ/t!.- J:iYF- c2t.L,C Blade Design rc 7~ 6\j/J/l/3 Diameter - ----- - --------

Hub Ser. No. ED oZ$.) S Blade Ser. Nos.

No.1 £62%9/ No. 2 £5tj51/e No.3 E ft;~'lO¢

No.4 ----------- - ----

PITCH RANGE

High - - -=--:-r--Feather_ ,g;:,;__'f..:.....,_· 0;__,.._

Governor Model

Low _____!_/ --= .. 5=.:·:.....:3::::.._<07 _

Reverse

- 1 -

4 • • "'

DATE

- 2 -

DESCRIPTION OF All OPERATIONS PERTAINING TO AIRWORTHINESS DIRECTIVES,

SERVICE BUllETINS, SERVICE LETTERS, & MINOR ADJUSTMENTS


~~~------~~-------- --- -----

DATE

{0 -

TACH TIME


SERVICE BULLETINS, SERVICE LETTERS, · & MINOR ADJUSTMENTS

DESC RIPTI ON OF WOR K SIGNATURE

- 3 - -

DATE

- 4 -


SERVICE BULLETINS, SERVICE LETTERS, & MINOR ADJUSTMENTS~




DATE:?-12-95 BOBBS:689.7 TSOB:559.2 HARTZELL MODEL:PHC-J3YF- 2UF S/N:ED2 52 5

~ RIGHT POSITION N40PG This propeller has been inspected and serviced using the Beecncraft Inspection Form listed under 5-20-00 of the Maintenance Manua l and is in compliance with the requirements of an annual inspection and is determined to be in airworthy condition. Replaced 2ea deice boots, blades dressed and painted, hub greased and dei cer wiring inspected ana secured. Shimmed spinner assembly and serviced with ni troqen. Ground run and operat1onal check of systems ana components sati~factory. This propeller is ~pproved for .return t-o serv1ce. For furtner deta1ls concern1ng th1s inspection, refer to W.0.#6664 on file a~ this overhaul facility. End.

Paul A. Brevard

~A FIREWALL PORWARDL INC.

5212 CESSNA DK. LOVELAND~ CO. 80538

303-6b9-6185

. 5 .

TACH TIME

__ PATB:?/29/96 N:40PG



DESCRIPTION OF WORK

PROPRJJ~:PHC-J3YF-2UF S/N:ED2525

POSITION:Right

SIGNATURE

BOBBS:!I950.1 TSPOB:!I819.6

___ Inspected propeller blades for condition and dressed as __ required. Performed visual inspection of hub for cracks.

---Inspected spinner and bulkheads for cracks. Painted blade -___ tips and faces. I certify that this propeller has been __

inspected in accordance with a 1 00 hour inspection and was determined to be in an airworthy condition. W.O. 7158

___ -END-

_.P~_L.. ,~ _ __ DANIEL L. INGRAM

:IA505904232

- 6 -

FIREWALL FORWARD INC. 5212 cessna Drive Loveland, CO 80538

--------- -~---- --- --

L

MATH£R AVIATION ~THER, CA. 95655



tlspt •• n."" I Maa. A~ LLC 1( 40PG, PIICJ3YJ'-2VJ' MMIMr 1'1114, CA IN: &D-1535 I'AA .CUI PCPil.~B

FAA REPAIR STATION PCPR4399 MM';l2SIA l'Rf: 2321J DO; UJU M• CIM1l.lA 4

8-U-97 963.1

1'bil is a PfllDIMI1l Part oftbe IUJbt~ hcoJd. Pstilad dela concerning tbe wcllk perlim.d .. on tie wilhJbii'.EAAApproved R .... SWinn under walk om. <40323S. This Propeller a ..,..and fur nm.n to tenice wilh tespeet to tbe walt pelbmed. 1. Canplied with an 100 Houri .Annull 'ntpectinn in_acra cdat«-wilhldatber

Aviation lnlpocti.oo CbookJw PN lUdAlOOME. 2. De f'cJilowq replila Wll/JIOI OC!illlpOMil ~-Win~· • Plop hllde Je.din@ ed8ea dress e tl Technician(s): C. Duncan, Q. House I oedifiY that dU PROPELUJlhll hem~ in~ widl~nANNJJAL IRipec*8111d fOund to t.in Airwol1by 0"8"i'kR dal71b-of~ 1998.

~ 'ni0:1119.9-~~~CIWPCPR439B

--------------~--------·--------~ -1 -

--~

DATE

- 8 -

October 20, 1999 N40PG, Beechcraft SSP S/N:TJ-309 A.F.T.T.:2321.2 Meter: 1428.2

Mather Aviation LLC Mather Airport

FAA CRS No. PCPR439B WO#: 404183

This is a permanent part of the Right Propeller Records. Complied with an Annual inspection in accordance with Mather Aviation 100 1) Hour/Annual checklist PIN MAlOOME.

2) Dressed propeller blades 3) Serviced propeller accumulators with nitrogen 4) Installed overhauled propeller governor, see left engine book for details. 5) Resafetied propeller mount studs. Technician: S. Yarbrough This airQ"aft is approved for return to service only with respect to the work performed. (/4LLd£. Inspector:

7 John Verderber CRS# PCPR439B

October 20, 1999 P.T.S.O.: 1297.7 1 certify that this Propeller has been inspected in accordance with an ANNUAL INSPECTION and was determined to be in an airworthy condition, and is approved

for retmn to servil _.{ ;L,tL-Inspector:

ohn Verderber CRS # PCPR439B

IRE

D. Installation of Models (B)HC-12YF -4( )F The high RPM stop on the governor should be set for These models are identical to the (B)HC-C2YF-4( )F take-off RPM. ~e.::;xc;;.ce:..:Pc..:..t ...::fo;:;r:.....=th.::;e:....:..:loc:.::.a=-:t:.=cio:..:n::.....:::of::......:;th=e=-b=.:l::::a~de=--..:::ce;:;n=-:te=rl:.:.:in=.:e=-..:..:w..:..:it:.:.:h=----2-. ..:...T_h..:...ere-'--is...::...__nc..:..o_hi_,'g"-h_._pi_tch stop a<ljustment for either

"'"bering propellers.

May9,2000 N40PG, Beech 58P S/N:TJ-309

,gle for the dash 2 propellers : or removing shims in the Adding shims increases the

EATHERING lAIR :e the cylinder with dry air !COrding to table which is on he cylinder. The basic pres-

~ which do not have spring

Hobbs: 1486.9

Mather Aviation LLC Mather Airport

FAA CRS No. PCPR439B W0#404815

This is a permanent pert of the Aircmft records. l. Installed one new blade de-ice boot. Operation normal. Technician: T.Judson This aircraft is approved for return to service only with respect to the work performed. n ;

I which have spring kits, 50

RBS which have spring kits,

1g blade counterweights, 80 . t have spring kits.

Inspector:, _ _,..;V~ '~.c:...ILLt<..=:...::~-~ /John Verderber

CRS# PCPR439B

tne pressure to blow the /ow stop screw out with great force. There must be at least four threads engaged during normal operation. Replace air as per applicable charging instructions.

) ( ) on Piper PA-31P air?ring assembly kit A-1588,

( )-2( ) counterweighted ssist spring assembly kit 31 at 70°. 3)Y( )-2( ) ( ) counterxcept "E" extension; with nbly kit A-1588, 41 PSI at

KF on Piper PA-34-200T tssembly kit A-1588, 22 PSI

(i) PHC.J 3 YJ.<'-2J.4: on Beech 58P with feather assist spring assembly kit A-1588, 66 PSI at 70°.

NOTE: Consult Instructions No. 102 and 105 and Manual No. 117-( ).

------

-11-

Authority/Country: 2.

FAA/UNITED STATES

4. Name ress. SANTA MONICA PROPELLER SERVICE, INC 3135 DONALD DOUGLAS LOOP SOUTH SANTA MONICA, CA 90405

AUTHORIZED RELEASE CERTIFICATE FAA FORM 8130-3, AIRWORTHINESS APPROVAL TAG

FAA ARS ZY2R362L

HARTZELL PROPELLER PHC-J3YF-2UF/FC7663DR N/A

13. REMARKS

Form Tracking umber.

5. Number:

K26006

• Contract, or lnvo1ce

80213

HUB: ED2525 BLADES: E59546, E68891,

E68904 OVERHAULED

PROPELLER ASSEMBLY WAS COMPLETELY OVERJ IAULED. ASSEMBLED, RELUBRICATED, SET BLADE ANGLES, AIR PRESSURE LEAK II ECKED, AND FUNCTIONALLY TESTED. fNSTAL LED NEW ELECTRJC DEICER BOOTS, STATICALLY BALANCED, AND SAFETIED I.A.W. HARTZELL PROP ELLER OVERHAUL MA UAL 11 7D REV 13, 133C REV 24, SPM202A VOLUMES 1- 11 REV 34, 159 REV 10, 182 REV 4, WAPA PROCEDURE 001 DATED 07- 17-01. AD 2007-26-09 A D ALL APPLICABLE SB' s SL's SI's COMPLIED WITH TO DATE. NEXT OVERHAUL DUE AT 2000 FLIGHT HOURS OF OPERATION OR 72 CALE DAR MO THS, WHICHEVER OCCU RS FIRST.

-----------------------------------------EN D --------------------------------------

the items ident1fied above were manufactured 1n confonnity to

Authorized Signature:

. Name (Typed or Printed): 18. Date (m1d/y):

19. 43.9 Return to Service 0 Other regulation specified in Block 13

Certifies that unless otherwise specified in Block 13, the work identified in Block 12 and described in Block 13 was accomplished in accordance with Title 14, Code .of Federal Regulations, part 43 and in respect to that work, the items are approved for return to service.

15. No:

ZY2R362L

23. Date (M D Y): FEB 26 2009

User/Install er Responsibilities

It is important to understand that the existence of this Document alone does not automatically constitute authority to install the part/componenVassembly.

Where the user/installer performs work in accordance with the national regulations of an airworthiness authority different than the airworthiness authority of the country specified in Block 1 it is essential that the user/installer ensures that his/her airworthiness authority accepts parts/components/assemblies from the airworthiness authority of the country specified in Block 1.

""'""n, .. nts in Blocks 14 and 19 do not constitute installation certification. In all cases, aircraft maintenance records must contain an installation certification issued in accordance with the national regulation by user/installer before the aircraft may be flown.

12-9005

_ _ ._._ ............ ..._ ._ -- - - -

The Standard

PELLER LOG

ASA-SP-L

The Standard Propeller Log SP-L

© 1994-2000 Aviation Supplies & Academics, Inc.

ISBN 1-56027-418-2 978-1-56027-418-6

ASA-SP-L

All rights reserved. Reproduction or use, without expressed permission, in any manner, is prohibited.

Published by Aviation Supplies & Academics, Inc. 7005 132nd Place SE Newcastle, WA 98059-3153 Website: www.asa2fly.com Email: [email protected]

Printed in the United States of America

P N R A S A - S P - L

Prop'

ModG

Hub~

Date

Aircr

Propeller Record! General Information

Propeller Manufacturer ---------------------------------------

Model ___________________________ _ yYpe ________________________ ___

Hub Series # ------------------

Date of Manufacture ---------------

Make/Model

Aircraft Installed On:

Blade # -----------------------

Serial#

OHUB&

Year: __

Date:

Next lnspec Due:

Year: __

Date:

Next lnspoc Due:

Year:

Date:

PROP MODEL (R): PHC-J3YF-2UF PROP SiN (R): ED2525 REG. NO: 40PG WORK ORDER: 25859-03-2015

Right Prop Entries

HOWARD A VIA i!CN1 ~ Avionics • ~laintenance '~'-Sales and Service

Serviced prop with nitrogen 1/A/W Hartzell service manual.

Howard Aviation, Inc. Repair Station No. T03RB7 4L 1401 Fairplex Drive La Verne, CA 91750 Phone: 909-593-2596

DATE: 4/8/2015 AJC TSN: 4162.2

PROP TI (R): 4162.2 TSPOH (R): 374.3

HOBBS: 155.5

The airframe, engine and/or component identified herein was repaired and inspected in accordance with the current Howard Aviation, Inc. Inspection Manual and the Federal Aviation Regulations under which the operator is certified, and is approved for return to service as per those requirements. Pertinent details of the repair are on file at this Repair Sta · nder Repair rder 25859-03-2015.

DATE: 4/8/2015 SIGNED: Work Order: 25859-03-2015 Robin Howar Certified Repair Station No. T03R87 4L

Printed by EBis 3 (datcomedia.com)

I Overhaul

Mech. Cert. # or Repair Station #

Total Time Description in Service

Next Inspection Time Since Due: Overhaul


Year: __ _

Date:

Next lnspecti Due:

Year: __ _

Date:

Next lnspecti Due:

Year:

Date:

Next Inspection Due:

PROP MODEL (R): PHC-J3YF-2UF PROP S/N (R): ED2525 REG. NO: 40PG WORK ORDER: 26054-08-2015

Right Prop Entries

HOWARD AVIATION, {),~ . Avionics • Maintenance ........_~Sales e~nd Service

Howard Aviation, Inc. Repair Station No. T03R87 4L 1401 Fairplex Drive La Veme, CA 91750 Phone: 909-593-2596

DATE: 8/17/2015 AJC TSN: 4200.4

PROP TI (R): 4200.4 TSPOH (R): 412.5

HOBBS: 193.7

Inspected propeller, spinner and bulkhead 1/AIW service manual... Profiled leading edge and touch up painted aft facing side of right prop.

I certify this propeller has been inspected 1/AJW a 100 Hour 1 determined to be in an airworthy condition.

DATE: 8/17/2015 SIGNED: Work Order: 26054-06-2015 Robin Howard Certified Repair Station No. T03R87 4L

Printed by EBis 3 (datcomedia.com)

I Overhaul



Time Since Overhaul


IONS 0

0 HUB & IIRAiliE INSPIECTIONS. REPAIRS AND AlTERATIONS

Year: __

Date:

Next lnsf Due:

Year:_

Date:

Next lns1 Due:

----··· Year:

Date:

PROP MODEL (R): PHC-J3YF-2UF PROP S/N (R): ED2525 REG. NO: 40PG WORK ORDER: 26772-04-2016

Right Prop Entries

Howard Aviation, Inc. Repair Station No. T03R87 4L 1401 Fairplex Drive La Verne, CA 91750 Phone: 909-593-2596

DATE: 5/4/2016 NC TSN: 4294.3

PROP TI (R): 4294.3 TSPOH (R): 506.4

HOBBS: 287.6

Troubleshot prop deice circuit breaker popping. Found RH prop boot shorted against spinner. Assisted prop shop with replacement of boot.

The airframe, engine and/or component identified herein was repaired and inspected in accordance with the current Howard Aviation, Inc. Inspection Manual and the Federal Aviation Regulations under which the rator is certified, and is approved for return to service as per those requirements. Pertinent details of the repair are on file at this Repair Sta · und r Repair Or r 26772-04-2016.

DATE: 5/4/2016 SIGNED:. Work Order: 26772-04-2016

Certified Repair Station No. T03R87 4L Printed by EBis 3 (datcomedia com)




Year: ___ _

Date:


Year: ___ _

Date:


Year:

Date:


I

PROP MODEL {R): PHC-J3YF-2UF PROP SiN {R): ED2525 REG. NO: 40PG WORK ORDER: 27069-08-2016

Right Prop Entries

HOWARD AVIATION, ""~ Avionics - Maintenance ~~,Sales .:Jnd S~rvice

IHIUIB & BLADE INSPECTIONS, REPAIRS AND ALTIERATIOI!\!S 0

Howard Aviation, Inc. Repair Station No. T03R87 4L 1401 Fairplex Drive La Verne, CA 91750 Phone: 909-593-2596

DATE: 9/16/2016 PJC TSN: 4370.7

PROP TT {R): 4383.8 TSPOH {R): 595.9

HOBBS: 364

Inspected propeller, spinner and bulkhead 1/AIW service manual... Profiled leading edge and touch up painted aft facing side of prop.

I certify this propeller has been inspected 1/PJW a 100 Hour Inspection and repaired in accordance with current Federal Aviation Regulations and was determined to be in an airworthy condition.

DATE: 9/16/2016 SIGNED: Work Order: 27069-08-2016

Printed by EBis 3 (datcomedia.com) Robin Howard Certified Repair Station No. T03R87 4L

I Mecn. cen. w or nepo:nr ~'taiJon tt


Time Since Overhaul


0 HUB & BLADE INSPECTIONS, REPAIRS AND ALTERATIONS

Total Time Description Year: in Service

Date:


Mech. Cert. # or Repair Station II

Total Time Description Year: in Service

Date:



Total Time tion Year: in Service

Date:


Mech. Cert. II or Repair Station #

Year:

Date:

Next lnspec Due:

Year: __

Date:

Next lnspec Due:

Year:

Date:

Next lnspec Due:

Notes

Documents

~SANTA MONICA ~PROPELLER - aso.com · This propeller was inspected and serviced IA W Hartzell Service Manual and the following work was performed. Filed and dressed propeller. All