PACIFIC AERO TECH INC
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N83SG
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AIRFRAME LOG BOOK
Westwind 11244
Serial Number:
Date of Manufacture: November 1981
Type Approval: A2SW TRANSPORT CANADA PACIFIC A.M.O. 17 oCTOBER 1998 AERO TECH INC '109 - 97 w.o.980'194
'l AIRCRAFT WORK REPORT REG'N: N83SG MODEL: l24A
AND LOGBOOK ENTRY AJC T.T.: 6519.5 S.N.: 368
report by M. Sjerdal Ldgs.: 4889 Page 1 of5
The following maintenance has been performed per customer request and the lsraelAircraft Industries Westwind Model '1124 Maintenance Manual.
INSPECTIONS
Airframe: s.n.: 368 6519.5hours 4889landings 800-Hour Airframe Inspection completed. 800-Hour Structural Inspection completed. 150 Flight Hour Inspection completed. Aircraft exterior re-painted. Aircraft interior refurbished. Aircraft weighed.
Pre-fl ight inspection completed.
Powerplant - Left: s.n.'. P7748? 6202.7 hours 4546 cycles D.o.M.: 'l l Sept'81 8OO-Hour Inspection performed per Alliedsignal Aerospace TFE 731 L.M.M. Function tests and adjustments performed as required afier re-installation. Refer to TFE 731 Engine Logbook for turther detail.
Powerplant - Right: s.n.: P77488 6470.9 hours 4445 cycles D.o.M.: '12 Sept. '81 Engine removed and re-installed. Full420o-Hour Inspection (MPl/CZl) performed by AlliedSignal Engines, Phoenix. ' Function tests and adiustments performed as required after re-installation. Refer to TFE 731 Engine Logbook for turther detail.
AIRWORTHINESS DIRECTIVES
AD Number SB Reference Description Disposition
74-08-09 none Inspect Lavalory Waste Receptacles C/W - No tuults found. 3$.9680
89-12-08 1124-55-020 Inspect Horizontal Stabilizer aft spar splice fifting. C/W - No faults found 396233
98-20-35 1 124-27 -1 33 Inspect Horizontal Stabilizer Trim Actuator. C/w - No faults found 39r0802 R1 92-12-O2 '|12+27-100 Inspect Aileron Torque Transfer Tubes. C/W - No faulb found. 39-8262
4380 Agar Drive, Vancouver Inlernational Airport, Richmond, BC V7B 143 Tel: (604) 273-4649 . Fax: (604) 273-4661 . PACIFIC ' AERO Ttsct.I INC 17 OCTOBER 1998 w.o. 980194
AIRCRAFT WORK REPORT REG,N: N83SG MOOEL: 11244
AND LOGBOOK ENTRY A/c T.T.: 6519.5 S.N.: 368
report by M. sjerdal Ldgs.: 4889 Page 2 of5
C. SERVICE BULLETINS Number Description Disposition
1124-59-026 Closure of tailcone vent holes. C/w 1124-56-'rlg lmproved cockpit side window installation - co-pilots only. New window installed. 1124-?9A-140 Installation of CB for hydraulic low pressure. C/W 1124-32-19S Inspect upper and lower steering brackets. Previously C/W at Recunent inspection next 6346.0 04-06-9S. due at 7146'0 hours TAT'
D. CAMP Codes The following customer supplied CAMP Card ltems have been accomplished at this time:
CODE TASK DESCRIPTION CODE TASK DESCRIPTION 050150 200 Hour Inspection 7106'10 Check # 2 Eng Plumbing/Conn' O5O3OO 4OO / 200 Hour Inspection 713616 MPI # 2 Engine 050600 800 i 400 / 200 Hour lnspection 72660'l CZI #2 Engine 051150 150 Hour Insp. Lefi Engine 740106 Op. Chk # 1 eng' lgnition system 051250 150 Hour Insp. Right Engine 740116 hsp. # 1 eng 6:00 plug plug 05'1300 3OO Hour Insp. Left Engine 740126 Insp. # 1 eng T:00 052300 300 Hour Insp. Right Engine 740611 Op. Chk # 2 eng lgnition system 23O4OO Clean Test CVR Beacon 740616 Insp. # 2 eng' 6:00 plug 240116 Overhaul # 1 Eng. St./Gen 740626 Insp. # 2 eng T:00 plug 260169 Vis. Insp. Cockpit lire extinguisher 780136 Clean/lube #1 eng. TR feedback cable 260181 Vis. Insp. Cabin fire extinguisher 780636 Clean/lube tl2 eng. TR feedback cable 330226 Baftery, emerg. lights, 791621 Change#2eng Oil 930228 Charge emerg. light battery 911290 581124-27-129 left aileron 344616 Insp. emerg. Power supply 911291 581124-27-129 right aileron 350166 Check pilots 02 mask 911400 SB 1124-294-140 replace CB 350169 check co.pi|ots 02 mask 973636 sB TFE73,I 472-3636 |eft engine 530200 Insp. Fwd - Aft Press. Bulkhead 973665 SB TFE731 472-3636 right engine 530205 Insp. Fwd to afi main frames 990020 AD74-08-09 Lav Waste 710109 Check # 1 Eng. Elect. Wire/Conn. 990131 AD89-12-08 Spar splice insp' 710110 Check#'l Eng- Plumbing/Conn. 991615 AD 98-06-10 Insp. Hyd Fuses 7lO6Og Check#2 Eng Elect. Wire/Conn. 991560 AD 96'24-11 Left Aileron 991561 AD 96-24-'l l Right Aileron end PACIFIC .AERI) TECH IN(] 17 oCTOBER 1998 w.o.980194
AIRCRAFT WORK REPORT REG'N: N83SG MODEL: 11244
AND LOGBOOK ENTRY AJc T.r.: 6519.5 S.N.: 368 Page 3 ofs report by lV. Sjerdal Ldgs.: 4889
E. STRUCTURAL INSPECTIONS / Non-Destructive Testing Refer to Cantech Inspections Ltd. report, W.O.#A898-226, dated 17 Aug 98' atlached'
F. PARTS REPLACED / REPAIRED / INSTALLED
rrsK ITEM DESCRIPTION PART NO. SERIAL NO. CONDITION G.R.N.
1 De-lce Boot, lefi wing 25S7D5083{9 n.s.n. new 1'1654 2 2 De-lce Boot, right wing 25S7D5083-10 n.s.n. new 1169 2 3 De-lce Boot, lefi stabilizer 25S7D5083-3 n.s.n. new 11654 2 4 Delce Boot, dght stabilizer 25S7D50834 n.s.n. new 11654 2 5 Stall Strip 3D2405-2 n.s.n. new 11683 2 6 Engine, right 3072500-2 P77488 MPVCZI 11664 5 7 Mount, engine, right 3071071-2 n.s.n. FLPI 11664 5 I Bolts, eng. Mount, right 3072571-2 n.s.n. FLPI 11664 5 I Hose, main tuel supply, right eng. 1300212-0152 n.s.n. new 11704 25 10 Tube, florescent light 6635-1320-25 n.s.n. new ngm 26 11 Tube, florescent light 6635-610-2S n.s.n. new ngm 26 12 Switch, right nacelle heat 98505-12299 1371 new 11753 33 13 #2 Nav Receiver 622-0876-001 16803 repaircd '11749 41 14 Switch, pilots PTT STD969-'I n.s.n. new 11701 44 15 Potentiometer, audio control 533201752387 n.s.n. new 11704 47 '16 Altimeter,co-pilots 8'4420210014 501 repaired 11706 4e 17 Seals, afi engine pylon, left & right AF150-204 n.s.n. new 11724 s8 18 lgnitor, left engine, 6:00 3074541-1 98052267 new 11723 88 19 lgnitor, left engine, 7:00 30745/1-1 58052270 new 11723 88 20 Seals, generator, left & right eng. F10A5P10046-13 n.s.n. new 11739 8e 21 Seals, BP Valve, left & right eng. Fl0A5P10046-11 n.s.n. new 11890 8e 22 Speakers, cockpit, co-pilots WP6008 n.s.n. new ngm 98 .11739 23 Window, cockpit, co-pilots 343003-50152 n.s.n. new 100 24 Diode, D22 Priority Bus 1N2784 n.s.n. new 11720 10s 25 Bushing, rudder top NAS75-4-010 n.s.n. new '11758 111 26 Bushing, rudder, middle NAS75-5-009 n.s.n. new 11745 111 121 27 Bulb, logo light DA-27 n.s.n. new ngm 125 28 Hoses, hyd. Press., l& r Pumps AE246020'lG'156 n.s.n. new 11901 127 29 CB, Hyd. Power Indication 727447-3 n.s.n. new 11777 continued... 17 oCTOBER 1998 w.o. 980194
AIRCRAFT WORK REPORT REG'N: N83SG MODEL: 1,I24A
AND LOGBOOK ENTRY A/c r.r.: 6519.5 S.N.: 368 Page 4 of5 report bY M. Sjerdal Ldgs.: 4889
F. PARTS REPLACED / REPAIRED / INSTALLED ...CONT|NUEd
ITEM DESCRIPTION PART NO. SERIAL NO. CONDITION G.R.N. NO
30 Terminals, pilots windshield heat 343026-93 n.s.n. new 11777 128 131 31 Bearing, right eng. afr mount 'l GB5O2DN5 n.s.n. new 11881 1'1911 135 32 Baftery, emergency lights 1 AO-2058 n.s.n. new 3 33 Seal, emergency exit, lefr 1 1900010 n.s.n. new 11850 11924 136 u Starter/Generator, lefr engine 1 2306S018-1 2254 overhauled eno
G. DISCREPANCIES RECTIFIED / OTHER WORK PERFORMED
ITEM DESCRIPTION NO
3 1 Minor fuel leakage out of wing lower surfaces repaired by sealing intemal structure. 2 Temperature shift in right engine investigated. Borescope investigation showed major spalling. Refer to TFE 731 Engine Logbook for detail. 11 3 Door assembly for single point re-fuelling access, repaired. 4 Pilots outer glass windscreen removed, cleaned, inspected, re-installed and sealed' 18 5 Radome lightning diverter strips re-adhered to base material. 57 6 Several minorstructurerepairs/fastenerreplacementsaccomplished 7 Cockpit overhead panel lighting printed circuit board wiring repaired. 79 8 Bonding Straps on 6p tank afi fairings re-adhered to base material' 9 Aircraft interior refurbished.. All materials used meet FAR 25.853 (a) Appendix F Part | (a) (1) (ii). 2 2 Refer to Skandia, Inc. Flammability Test Reports, dated 09-14-98, Test Plan #3618 2 1O Seats fireblocked. All materials used meet FAR 25.853 (c) Appendix F Part ll Amendment 25-83 Refer to Skandia, Inc. Flammability Test Reports, dated 09-14-98' Test Plan #3618 1.1 Aircraft exterior re-painted. Base white: sheMin williams "Jet Glo' Matterhom white 570-535 1 Trim grey: SheMin Williams 'Jet Glo" ICON Custom Brown 8334-8718 '12 Flight controls balanced after painting. 24 13 Exterior Placards reDlaced as required after painting. 126 14 Aircraft weighed. New Weight and Balance Report entered in Flight Manual' 15 Aircraft registration number changed from N368MD to N83SG. eno
CI.{IC\r'd3NI H3!II OXAV MSN Hohaail - , Page 1 of I
nl$NlK. Hstmail. e,[email protected] Printedr Wednesday, December 3,2003 B:07 plvl
Fromi TonyCoon
----- Orlginal Message ----- From: "Sherwin-Witliams #g? 18 ',
> Tony,
> l]ere is the quart formula for 93348710 Brown:
> 5?1900: 443grams > 574900: 483grams 75901: 52ograms , 5?0901: 536 grams
> THIS FORMU]TA APPEARS TO BE ACCIJMUT,ATIVE I I
> If you have anl,mote questioos. let ne kno$/_ > Thanks,
> Jamie : Camp Systems Int'L, computerized Aviation Management products OPERATOR: ICON HEAIJTIT AIID EITNESS, INC. BEPoRT DATE 09/11/98 WORK COMPLIANCE FORM NO. 24.OIO AIRCRAFT NO.: 368 MODEL: 1124A TIESTWIIID GARD No: 24- 1 ISSUED 07-88 REV. 01-98 PAGE 1 Record time work accomplished for each task. Keep white copy for your records. Return yellow copy to CSI for updating.
CHECK CURRENT DUE LIST FOR DUE TIME CHANGES
woRK AccoMpLrsHED: DATE: uonrn I O oo, I t , uo 1X AIRCRAFT H0uRS: rnrornes: tf88ll
TECHNICIAN SIGNATURE: KIND OF CERTIFICATE & NO:
INSPECTED BY: f\0zi KIND OF CERTIFICATE & N(): I nq -11
ONLY THE FOLL()}IING t,llORK IS DUE AT THE TIME(S) NOTED ABOVE: DUE > 2401,1,6 NO. 1 ENGINE STARTER/GENERATOR MM 80-10-00 ()VERHAUL ********************* (240116) ( ) PART NAME: N0.1 ENGINE STARTER/GENERAT0R-'\/eL'rl'\^rvr\ MM 80-10-00 REAsoN REMovED: (cHEcK oNE) . TEcHNIcIAN: :n*/US TrMEA()FATLB()r{oRNc()LoANERD()scHEDcoNVE()MoDG()sERVrcEO(r*ecHGL()rrnrorer"r()DAMAGEDT()
REMOVED P/N: 23065-0 18- 1 S/N: 2258 MAN-H0UR5: HRS TENTHS n") INSTALLED P/N: a cl) 240116, 240126 6l STARTER/GENERATOR REMOVAL AND INSTALLATION, SERVICE, INSPECTION g)t - t\ REFERENCE CARD 24- 1 : R EQUIPMENT: T0RQUE IIRENCH 0 T0 90 INCH-P0UNDS t g9 R C0NSUMABLES: S0LVENT (FEDERAL SPECIFICATION PD 680, TYPE I) c3 E2 N0TE: EQUMLENT SUBSTITUTES MAY BE USED FOR THE F()LL()ilING ITEMS: GREASE AER0SHELL 17 (MIL-G-21164), GREASE 9c AERoSHELL 22 (MrL-G-81322), MoBIL GREASE N0.28 (MrL-G-81322), r.r0BrL GREASE N0.29 M0LYBDENUM-DISULPHIDE oE (0:co (MIL-G-81827), GREASE MrL-G-21164 !9 p6 A REI-{OVAL ?.ot' 1. DISCONNECT ELECTRICAL P()UER TROM AIRCRAFT. Eg 2. OPEN ENGINE SIDE CO}IL. --{oE 3. REMOVE BOLTS AND T/ASHERS SECURING AIR C()OLING DUCT TO STARTER/GENERATOR AND DISCONI{ECT DUCT. >o *g 4. REMOVE NUT AND TIASHERS SECURING PLASTIC COVER TO TERMINAL BLOCK AND RE}'IOVE COVER. og 5. TAG ELECTRICAL TEADS AND DISC()NNECT THEM FROM TERMII{AL BLOCK. = AIRI'I0RTHINESS DIRECTM 98-17-01, AMENDMENT 39-LO703 REVISION NUMBER: ORIGINAL EFFECTIVE DATE: 0CT0BER 13, 1998 SUBJ ECT: TO PREVENT CRACKED FUEL TUBES AND SUBSEQUENT LEAKAGE ()F FUEL ON AND AROUND ELECTRICAL COMPONENTS, }IHICH CAN CAUSE AN ENGINE FIRE. APPLICABILITY: ALLIEDSIGNAL TFE73I-2, -3, AND -4 SERIES TURBOFAN ENGINES TIITH FUEL TUBES, PART NUMBERS (p/N5) 3071051-1, 3073729-1, 0R 3072886-7, TNSTALLED. COMPLIANCE: REQUIRED AS INDICATED, UNLESS ACCOMPLISHED PREVIOUSLY. UITHIN 160 HOURS TIME IN SERVICE (TIS) AFTER THE EFFECTIVE DATE ()F THIS AD, ()R PRIOR TO DECEI'IBER 20, T999, I{HICHEVER ()CCURS FIRST, INSTALL AN IMPROVED FLEXIBLE FUEL TUBE IN ACCORDANCE }IITH ACCOMPLISHMENT INSTRUCTIONS ()F ALLIEDSIGNAL INC. ASB N(). TFE731-A73-3128, DATED FEBRUARY 26, 1997. o N PLEASE CHECK ()NE: ott N : AIRII0RTHINESS DIRECTM ACC0i'IPLISHED t .s9 y' c! or**o*rrrNEss DrREcrrvE N'T AppLrcAB E2 pEEGi _ ATRW0RTHINESS DIRECTTVE DEFERRED UNTrL _ (DUE TrME) 6Jco -c E9 p6 METHOD ()F COMPLIANCE: N < 4/c Tr*- OG qg 6E AE E! ogt,- E8i; E!Oo EE 56FO :a Eo6E ooo6 ************************************************** ****************** REFER TO APPLICABLE AIRI.IORTHINESS DIRECTIVE FOR PROCEDURE. COPYRIGHT 1998 CAMP SYSTEMS INT'1. € Gamp Systems lntll, computerized Aviation Management Products OPERATOR: ICoN HEAtrTII AND FIrNEss, INc. WORK COMPLIANCE FORM NO. 991620 AIRCRAFT NO.: 368 MODEL: 1124A tlEsrwllrD AIFICRAFT REG': N368rD PAGE 1 - 2929368 WORK DUE AT = APU HRS. Record time work accomplished for each task. Keep white copy DAIE HOURS LANDINGS CYGLES for your records. Return yellow copy to CSI for updating. 99-00't: 98254 12t20199 NEXT 160 ** NEW REOUIREMENT ** ADDED TO REPORT ON 09/09/98 e. (1 <{c1 I,,ORK ACCOMPLISHED: DATE: nonrn / ,,0^ QQ AIRCRAFT HOURS: 6 - 5,-ororrnr, 4e TECHNICiAN SIGNATURE: --zC KIND OF CERTIFICATE & NO. 414( ? INSPECTED BY: /( u) KIND 0F CERTIFIcATE & N0: fcq-q7 ******* r*****************t******* THE F0LL0I/ING }l0RK IS DUE AT THE TIME(S) N0TED AB0VE: TECHNICIAN INSPECT0R MAN-H0URS at,_f- HRS.THS ggt6z0 ALLTEDsTGNAL AD98-17-01 #r ENGINE. fl'l 4c2 AIRI.IORTHINESS DIRECTIVE 98-T7 -Ot AMENDMENT 39-TO7O3 REVISION NUMBER: ORIGINAL EFFECTM DATE: 0CT0BER 13, 1998 SUBJ ECT : TO PREVENT CRACKED FUEL TUBES AND SUBSEQUENT LEAKAGE OF FUEL ON AND AROUND ELECTRICAL COMPONENTS, }IHICH CAN CAUSE AN ENGINE FIRE. APPLICABILITY: ALLIEDSIGI{AL IFE73L.2, -3, AND -4 SERIES TURBOFAN EI{GINES I.IITH FUEL TUBES, PART NUMBERS (P/NS) 3071051-1, 3073729-1, 0R 3072886-1, INSTALLED. COMPLIANCE: REQUIRED AS INDICATED, UNLESS ACCOMPLISHED PREVIOUSLY. I{ITHIN i6O HOURS TIME IN SERVICE (TIS) AFTER THE EFFECTIVE DATE OF THIS AD, OR PRIOR TO DECEMBER 20,1999, UHICHEVER OCCURS FIRST, INSTALL AN IMPROVED FLEXIBLE FUEL TUBE IN ACCORDANCE WITH ACCOMPLISHMENT INSTRUCTIONS ()F ALLIEDSIGNAL INC. ASB N(). TFE73T-A73-3728, DATED FEBRUARY 26, 1997. o N PLEASE CHECK ()NE: ott N ti AIRI,I0RTHil{ESS DTRECTIVE ACCoMPLISHED (C/r{). g9 ,A* r^rrEss DIRE.TIVE NoT APPLI'AB EA EZ 9c AIRI0RTHINESS DTRECTM DEFERRED UNTIL (DUE TrME) rE _ 6Tco .E9 METHOD OF COMPLIAilCE: 6 4/. TrPe E6 N/n OE h!i d.e o? >6 60Fg Oot;= l>-,EB l3E IEE 26 EoGtr ooo6 ************************************************************************************************************************ REFER T() APPLICABLE AIRIIORTHINESS DIRECTIVE F()R PROCEDURE. COPYRIGHT 1998 CAMP SYSTEMS INT'1. : Gamp gystems lntrl, computerized Aviation Management products OPERATOR: ICON HEAf,TII At{D FIrNEss' INc. WORK COMPLIANCE FORM NO.320237 AIRCRAFT NO.: 368 MODEL: 1124A vlBsrwrllD AIRCRAFT REG,: N368uD PAGE 1 2929368 WORK DUE AT " = APU HRS. Record time work accomplished for each task. Keep white copy DATE HOURS LANDINGS GYGLEIi for vour records. Return vellow coDv to CSI for uDdatino. 00-000, 98282 VERY 8OO ** NEW REOUIREMENT ** ADDED TO REPORT ON 10/05/98 @ tt ( l.l0RK ACCOMPLISHED: DATE: MoNTH onv CG veen & AIRcRAFT HOIJRS: 67 +E " C: LANDINGS: +7 P7 TECHNICIAN SIGNATURE: KIND OF CERTIFICATE & NO: FUl r\ CdT 5 illue, INSPECTED BY: KrND 0F cERrrFrcATE & N0: Ll 4 ne "(9 f L THE F0LLOI,IING lfORK IS DUE AT THE TrME(S) N0TED AB0VE: TECHNICIAN INSPECTOR MAN-HOURS a, ,,- HRS.THS 32o237INsPEcTN0sEtANDINGGEARUPPERsTEERINGBRAcKETAssEMBLY...MM32-50-08 ************************************************************************************************************************ NO MANUFACTURER TEXT ISSUED. u t p.E-c-*l 1p-*l= l.--) o*a D., u R ". g fl. ?( 4-6,0 ,!ns G T P*". I I tZtl ^ 'Ua 72 - t71 N (a N o)t iN T g9 ci E2 E6i rrE o:co .Ee E6 OfE Eg o.= >o 66*e Oo);E {EE=g 9o EEFO 6U :d Eootr ooo6 COPYRIGHT 1998 CAMP SYSTEMS INT'1. € Camp gystems lntrl, computerized Aviation Management Products OPERATOR: ICON HEALTII AND FIIITNESS' INC. WORK COMPLIANCE FORM NO. 320238 AIRCRAFT NO.: 368 MODEL: 1124A IfEsrwrND AIFIEFIAFT FIFG-: N368I[D PAGE 1 * 2929368 WORK DUEAT = APU HRS. Record time work accomplished for each task. Keep white copy DATE HOURS LANDINGS CYCLES for your records. Return yellow copy to CSI for updating. XX-XXX 98282 VERY 8OO ** NEW REOUIREMENT ** ADDED TO REPORT ON 1Ol05/98 (,C .*.T I.IORK ACCOMPLISHED: DATE: MONTH C/T ONV fd VTNN 4 AIRCRAFT HOUNS: 6}4 LANDINGS: ?T7?f,, TECHNICIAN SIGNATURE: -"7 KrND 0F GERTTFTcATE & N0: Fr*i* e i|-9 to't l(l INSPECTED BY: KrND 0F cERTTFT.ATE & N0: L( 4, R R 1< s L ********************************************************** THE FOLLOI.IING }IORK I5 DUE AT THE TIME(S) NOTED ABOVE: TECHNICIAN INSPECTOR MAN-HOURS /1tfg HRs'THs 320238 INSPECT NOSE LANDING GEAR LOI.,ER STEERING BRACKET ASSEMBLY"'MM 32-50-08 "" 'nz'- ************************************************* ***************** FORM/TEXT CURRENTLY UNDER REVIE}I/REVISION. REFER TO THE CURRENT MANUFACTURER'S DOCUMENTATION. f<.. clsp-.,r-epz 1l' sP iU**- b.'n A, 7 (+6^0 No; Br qB, (/2,1 - j> r>1 sN N h iN I g9 c3 E2 Eot oE 6iaco .9.Y b;6= ?,q9 (!F >6 *c6(s oo),= EB EE !Do -sH 5; :a EoOE o6 O() COPYRIGHT 1998 CAMP SYSTEMS INT'1. / € carzp s/seears /nfrl, computerireo luiation Management proj!!,cj: OPERATOR: ICON HEALTH AND FIlIrNEss' INC. WORK COMPLIANCE FORM NO. 911400 AIRCMFT NO.: 368 MODEL: 1124A wEsrwrltD AIRCRAFT REG.: N358llD PAGE 1 t 2929368 WORK DUEAT = APU HRS. Record time work accomplished for each task. Keep white copy DATE HOURS LANDINGS CYCLES for your records. Return yellow copy to CSI for updating. 97-001 98282 400 ** NEW REOL{f,EMENT ** ADDED TO REPORT ON O9/23l98 6 }loRK ACCoMPLTSHED: DATE: UOrurH /c Onv 6 ,ro* QL or^r^oFT HouRs: 6 5(q. 5 LANDTNGS: 4- k€vQq TECHNICIAN SIGNATURE: KrND 0F cERTTFTcATE & N0: -'*-) ^#ltT q INSPECTED BY: a( l/ 9 KrND 0F .ERTTFT.ATE a no7 > -'17 THE F()LL()}JING UORK IS DUE AT THE TIME(S) NOTED ABOVE: TECHNICIAN INSPECTOR MAN-HOURS HRS . THS glt400 SERVICE BULLETIN: ALERT SERVICE BULLETIN It24-2gA-1.40 ...... ^-t-z 4,w2_ SUBJ ECT: HYDRAULIC P0|'/ER - INDICATI0N - INSTALLATI0N 0F INDEPENDENT CIRCUIT BREAKER FOR L0l', PRESSURE }JARN I NG EFFECTIVITY: MODELS 1124l1124A l,ESTllIND, ALL SERIAL NUMBERS. C0MPLIANCE: C0MPLIANCE IIITH THIS SERVICE BULLETIN IS MANDAT0RY AND IS REQUIRED T0 BE ACC0MPLISHED BEFORE OR AT THE NEXT 4OO-HOUR INSPECTION. ISSUE DATE: AUGUST 15, 1998 PLEASE CHECK ONE: v(r urr;. BULLETTN coMpLrED f/rTH (c/w). SERVICE BULLETIN NOT APPLICABLE (N/A). N SERVICE BULLETIN DEFERRED UNTIL (DUE TIME) N to ts N METHOD OF COMPLIANCE: - : (.b, RGP. AC €{) ?^n "09 ci /*tg, E2 / (A et cTr oLr :' 9c oE 6:co .E9 E6 OE x>hat 6: so>6 E! =cOo) =ooo EI Oo oE 66FO 2A Ee6tr ooo6 ******************************************************************************************** Gamp tystems Intrl, computerized Aviation Management products OPERATOR: ICON HEAITTH AltD FITNESS, INC. WORK COMPLIANCE FORM NO. 973636 AIRCRAFT- NO.: 358 MODEL: 1124A IIESTWIND AIRCRAFT REG.: N358llD PAGE 1 2929368 WORK DUE AT " = APU HRS. Record time work accomplished for each task. Keep white copy DATE HOURS LANDINGS CYCLES for your records. Return yellow copy to CSI for updating. 97 -00L 98282 NEXT 24 ** NEW REOUIREMENT ** ADDED TO REPORT ON 10/05/98 }IORK ACCOMPLISHED: DATE: r,ronrtr/0 onv c€ ,ro^ '7k' ATRCRAFT HouRs: 6 5/'l {onorncs: 4F(4 €L/) t TECHNICIAN SIGNATURE: KrND oF cERrrFrcArE & No: Bil *c(7 INSPECTED BY: pt c/-l KrND 0F cERTrFrcArE & N0: r fl THE F0LL0l'JING l,r0RK IS DUE AT THE TIME(S) NOTED ABOVE: TECHNICIAN INSPECTOR MAN-HOURS HRS. THS 973636 SERVICE BULLETIN: IFE73T-A72-3,O .,/-1-a ttlk'S SUBJ ECT: ENGINE - REVIEI.I ENGINE LOG BO()K AND SUPPLY DATA FOR SPECIFIC HP COMPRESSOR IMPELLERS EFFECTIVITY: PART NO. MODEL NO. 3072500-1./-2/-4 TFE73l - 3- 1G 3073790-t TFE731 - 3D- 1G 307 4010-r I -2 TFE731 -3DR- 1G 307 4910-1 I -2 I -3 I -4 TFE73I - 3R- lG COMPLIANCE: COMPLIANCE ADDRESSES A SAFETY ISSUE. ALLIEDSIGNAL RECOMMENDS THAT THIS SERVICE BULLETIN BE COMPLIED I.IITH I.IITHIN 24 HOURS AFTER RECEIPT OF THIS SERVICE BULLETIN. ISSUE DATE: SEPT 4/98 N PLEASE CHECK ONE: o(\| ot ls SERVTCE BULLETTN C0MPLIED r,'ITH (Cilr). F _ t 4senvrce BULLETTN Nor AppLTcABLE (N/A). 99 ci Ei SERVICE BULLETIN DEFERRED UNTIL (DUE TIME). Ed oE - co METHOD OF COMPLIANCE: tu'/,q Yr R /L,7, 6: E9 - E6 OE ?qg >o FC 6(! ;=Oo) Eg: ********************************************************************************************* EE 9o REFER TO GARRETT SERVICE BULLETIN FOR PROCEDURE. EEEO :a66 Eootr ooG,(! COPYRIGHT 1998 CAMP SYSTEMS INT'1. Camp tystems Int'L, computerized Aviation Management Products OPERATOR: ICON HEAL:I'H At{D FTTNESS, INC. WORK COMPLIANCE FORM NO. 973665 AIRCMFT- NO.: 368 MODEL: 1124A ttESTwIl[D AIFICFIAFT FItrG : N368IID PAGE 1 APU HRS. 2929368 WORKDUEAT '= Record time work accomplished for each task. Keep white copy DATE HOURS LANDINGS GYGLES for your records. Return yellow copy to CSI tor updating. 97 -001 98282 NEXT 24 ** NEW REOUIREMENT ** ADDED TO REPORT ON 10/05/98 O tt 6 t.toRK AccoMpLIsHED: DATE: MoNrH /,9 oo, 6 YEAR F or*r*on HouRs: 9q .9 LANDINGS: 4 ?g I TECHNICIAN SIGNATURE: 4 KrND oF CERTTFTCATE u ro, {/>z(o rNsPEcrED ,r. /( t/9 KIND 0F cERTIFIcATE a noz f Dq 4',/ ************************************************************************************************************************ THE FOLLOI,IING I.'()RK IS DUE AT THE TIME(S) NOTED ABOVE: TECHNICIAN INSPECTOR MAN-HOURS HRS.THS *-2t /'z'/ Z' 973665 SERVICE BULLETIN: IFE73T-A72-3636 RE. ( /4t3 SUBJECT: ENGINE - REVIEI.I ENGINE LOG BOOK AND SUPPLY DATA FOR SPECIFIC HP COMPRESSOR IMPELLERS EFFECTIVITY: PART N(). MODEL NO. 30725s0-tl-2/-4 trE/J1-J-rb 3673790-r TF E731 - 3D.lG 307 4010-1, / -2 TF E731 - 3DR- 1G 307 4e1o-t I ,2 I -3 I -4 TF E731 - 3R- lG COMPLIANCE: C()I.4PLIANCE ADDRESSES A SAFETY ISSUE. ALLIEDSIGNAL RECOMMENDS THAT THIS SERVICE BULLETIN BE COMPTIED I.IITH l.lITHIN 24 HOURS AFTER RECEIPT ()F THIS SERVICE BULLETIN. ISSUE DATE: sEPT 4/98 N ()NE: (l' PLEASE CHECK N tr ct ts _ SERVTCE BULLETTN CoMPLIED r,rITH (C/l'). : I t,/ g9 L/SERVICE BULLETIN NOT APPLICABLE (N/A). c3 iE SERVICE BULLETIN DEFERRED UNTIL (DUE TIME ). E6i oE C/e^e eo,,,-,7. co METHOD OF COMPLIANCE: k vz s',U f 6: .Ee p6 OE EecE >o RC 6(s Oo)i= 6B **************************************************************** ************ E? 9o FOR PROCEDURE. EE REFER TO GARRETT SERVICE BULLETIN EO 66 2A to.(!C ooo6 COPYRIGHT 1998 CAMP SYSTEMS INT'1. / € Camp tystems lntrl, computerized Aviation Management products OPERATOR: ICON HEALTII AllD FITNESS, INC. REpoRr DAIE lo/oe/e8 WORK COMPLIANCE FORM NO. 78.090A AIRCRAFT NO.: 368 MODEL: 1124A llBsrwrND GABD r{o: 78- 3 AIFTCFIAFT FIFG : N368![D |SSUED 07-88 REv. 05-97 PAGE 1 2929368 WORK DUE AT ' = APU HRS. Record time work accomplished lor each task. Keep white copy DATE HOURS LANDINGS CYCLES lor your records. Return yellow copy to CSI for updating. 78-01,0 98282 11/ 13t98 CHECK CURRENT DUE LIST FOR DUE TIME CHANGES q(i r,loRK ACC0MPLISHED:: DATE:DArE: uo*r,MoNTH /CiC onyDAY CC Yrnnyro, V ATRCRAFT HouRst G 55l\ lq. I LANDINGS:taNnrNcs: /+ e TECHNICIAN SIGNATURE: t{< KrND oF cERrrFrcArE a ro, ilt /H4 , .c> JlJ( -7 INSPECTED BY: ./-n- KrND 0F cERrrFrcATE & N0: (J.'7 THE F0LLOIIING I'JORK IS DUE AT THE TIME(S) N0TED ABOVE: TECHNICIAN INSPECT()R MAN - H()U RS ,//Vf HRS . THS 780136 CLEAN/LUBRICATE N0.1 THRoTTLE RETARDER CABLE AND CASING...MM 78-32-00...... _-^ ./ r ' - w " - -;rrfs a bd rcgogo cLEAN/LUBRTcATE N0.z rHRorrLE RETARDER cABLE AND cAsrNG...MM 78-32-00 ...... -? ********* 780136,780636 R N0TE: THE F0LL0I,IING ADDITI0NAL IJCF(S) MAY BE REQUIRED T0 PERF0RM THIS TASK 78.II0. R LUBE THROTTLE RETARDER FEEDBACK CONTROL ASSEMBLY R REFERENCE CARD 78- 3 EQUIPMENT/CONSUMABLES: SOURCE OF DRY, OIL-FREE COMPRESSED AIR, DRY LINT-FREE CLOTH, THROTTLE RETARDER GAUGE p/N F10A-5-P20900-tt, FEEDBACK CABLE MoTr0N AND RIGGING P/N Fl0A-5-P20900-13 AND P/N F10A-5-P20900-1.5, GREASE MIL-G-23827 0R GL 105 D1, GREASE DoU C0RNING DC33 LIGHT C0NSISTENCY, LoCKIJIRE, C0TTER pIN p/N MS24655-153, DEPTH CALIPER 0 T0 3.90 INCH, RIG PIN WITH DIAMETER OF 0.125 INCH CAUTION: EXTREME CARE MUST BE TAKEN I{HEN REMOVING ANO INSERTING CABLES TO AVOID DAMAGE T() THE CASING TEFLON LINERS. EVIDENCE OF TEFLON PIECES ()N THE CABLE OR IN THE CABLE OR IN THE LUBRICANT IS CAUSE FOR REPLACING THE N ce CASING. (\| THREADED ENDS OF THE CABLE SHOULD NOT BE INSERTED INT() THE CASING AS DAMAGE I.'ILL RESULT TO THE TELFON o)t N ts L I NER. L g9 1. REMOVE THROTTLE RETARDER FEEDBACK C()NTROL ASSEMBLY A5 F()LL()I{S: c! E9 N0TE: T0 REM0VE THE THR0TTLE RETARDER FEEDBACK C0NTROL ASSEMBLY, IT MUST BE DISASSEMBLED. DURING DISASSEMBLY, 9c MUST oE THE TELEFLEX HARDIIARE BE CAREFULLY RETAINED. (!Ico A. OPERATE THRUST REVERSER DO()RS TO FULL DEPLOYED POSITI()N AND INSTALL THE DEPLOY GROUND LOCK. .E9 B. RELEASE MAIN HYDRAULIC SYSTEM AND THRUST REVERSER SYSTEM PRESSURE. E6 OE C. REMOVE ELECTRICAL P()hIER FR()M AIRCRAFT. Ho; x> D. REMOVE INSPECTION PANELS ON OUTER SIDE OF REAR NACELLE TO GAIN ACCESS TO THROTTLE RETARDER SYSTEM UNITS. E. REMOVE NUT, WASHER, BUSHING AND BOLT CONNECTING RETARDER ROD-END ASSEMBLY TO LO}IER REVERSER DOOR. >6 *c F. REMOVE BOLT, SPACER, IIASHER AND NUT CONNECTING ROD-END TO BELLCRANK OF SINGLE LEAD CONTROL BOX. o€ G. I'IITHDRA}I R0D-END ASSEMBLY I,ITH INNER TELESC0PIC CASING AND COMBINATI0N CABLE FR0M AFT TELESC0PIC OUTER CASIN6. oo) (BELLCRANK I.IILL ROTATE UNTIL SECTION OF COMBINATION CABLE IS OUT OF CONTROL BOX). EB H. REMOVE AFT RIGID CASING COUPLING NUT FROM INNER THREAD OF AFT SWIVEL THREADED COUPLING THEN REMOVE TIIO HEX NUTS 8? AND I.IASHER FROM OUTER THREAD OF SUIVEL THREADED COUPLING AND SLIDE THEM FOR}JARD ONTO AFT RIGID CASING. Oo I. REMOVE AFT SWIVEL ASSEMBLY UITH AFT OUTER TELESCOPIC CASING FROM AFT SUPPORT BRACKET AND TIIO HEX NUTS AND EE FO 6E },ASHER FROM AFT RIGID CASING. a)> ROD-END ASSEMBLY AND NUT FROM INNER CASING AND COI-,IBINATION CABLE. Fo J. IF REQUIRED, REMOVE AND FROM F()R},ARD TELESCOPIC OUTER CASING. EoaEc K. }IITHDRA}I ROD-END I.JITH INNER TELESCOPIC CASING CABLE oooa! L. REM0VE SCREI'IS ATTACHINc F0RIIARD RIGID CASING FAIRLEAD T0 STRUCTURE 0F NACELLE. REM0VE FAIRLEAD. M. RET{OVE FORIIARD RIGID COUPLING NUT FROM INNER THREAD OF FORI{ARD SI{IVEL THREADED COUPLING. N. IF REAR NACELLE IS INSTALLED ()N ENGINE, REMOVE FORI.IARD RIGID CASING COUPLING NUT FROM FORWARD CONTROL BOX ()N ENGINE FUEL CONTROL. O. CAREFULLY REMOVE FOR}IARD RIGID CASING. P. REMOVE Tl.|O HEX NUTS AND I.'ASHER FROM FOR}'ARD S}IIVEL THREADED COUPLING AND REMOVE FORI.JARD TELESCOPIC OUTER CASING COPYRIGHT 1998 CAMP SYSTEMS INT'1. << CONTINUED >> *5' F Camp Sysfems lnt'1. ComputerizedAviation Management Products OPERATOR: lCoN HEALTH AND FlTNEss, lNc. WORK COMPLIANCE FORM NO. AIRCMFT NO.: 368 MODEL: tl24AwESTwlND AIRCMFT REG.: N83sG PAGE WORKOUEAT '=APUHRS. Record linp work accomplish€d tor each task. ]G€p white copy DATE HOURS LANDINGS CYCLES For tour records. Relum \cllorv copy to CSI for updating. 11/@198 6735 WORKACCOMPI-ISHED: DATE: 10 17 98 ArTg5fl 651Q.s .a8e MONTH: DAY: YEAR: HOURS: . UNDINGS: TE.HNI.TANSTGNATURE: - KIND oF CERTIFICATE & NO.: A.M.O. 10$97 INSPECTED 8YI -ZQ.A. KIND OF CERTIFICATE & No.: A.M.O. 109-97 RECORD COMPLIANCE- OF INSPECTIONS, SERVICES, AD, SB, OR ANY WORK ACCOMPLISHED. CODE TASK DESCRIPTION C/W Date / A/c Hours / Ldgs Next DUE 230207 Replace CVR ULB Battery 04t11t98 oaoltoS 230450 Replace Beacon Battery 04t11t98 02t01t03 340146 Leak check left static system 04/03/98 04/03/00 340151 Leak check right static system 04/03/98 04/03/00 341106 Calpilots aft FAR 91.411 04/03/98 04/03/00 341116 Calco-pilob alt FAR 91.411 04/03/98 04/03/00 343672 Calib#1ADC 04/03/98 04/03/00 Y6111 Test # 1 ATC Transponder 04/03/98 04/03/00 U6126 Test # 2 ATC Transponder 04/03/98 04/03/00 991580 AD 97-04-03 # 1 engine N/A by engine model and aircraft type 991581 AD 97-0+03 # 2 engine N/A by engine model and aircraft type 991590 AD 97-11-10 02 masks N/A to equipment installed 991610 AD 98-0$09 pitch trim act. Insp. Superseded by AD 9&20-30 - C/W 10/06/98 991620 AD 98-17-01 # 1 eng. tueltube N/A by engine p.n. 991625 AD 98-17-01 #2 eng. tuel tube N/A by engine p.n. end $ 5$. { Camp Sysfems lnt'|. ComputerizedAviation Management Products OPERATOR: IGON HEALTH AND FITNESS, !NC. WORK COMPLIANCE FORM NO. AIRCRAFT NO.: 368 MODEL: 1I24AWESTUT'IND AIRCRAFT REG.: N83sG PAGE - -Rocordtirne rJvork Ke€p white copy WORK DUE AT = AI'U I.IKs. accomplishcd for each task. DATE HOURS LANDINGS CYCLES For vour rccords. Retum vellol copv to CSI for updating. rrr09r98 6735 WORKACCOMPLISHED: DATE: 10 17 98 ATRCRAFT 6519.5 4889 MONTH: HOURS: LANDINGS: \ TECHNICIAN SIGNATURE: KIND OF CERTIFICATE & NO': A.M.O.109.97 INSPECTED BY: Q.A. KIND OF CERTIFICATE t No.: A.M.O. 109-97 RECORD COMPLIANCE OF INSPECTIONS, SERVICES, AD, SB, OR ANY WORK ACCOMPLISHED. CODE TASK DESCRIPTION CODE TASK DESCRIPTION CODE TASK DESCRIPTION CODE TASK DESCRIPTION 050150 200 Hour lnspection 710610 Check # 2 Eng. Plumbing/Conn. 050300 400 I 200 Hour lnsPection 713616 MPI # 2 Engine 050600 800 / 400 / 200 Hour Inspection 726601 CZI#2 Engine 051150 150 Hour lnsP. Left Engine 740106 Op. Chk. # 1 eng. lgnition sYstem 051250 150 Hour lnsP. Right Engine 740116 Insp. # 1 eng. 6:00 plug 051300 300 Hour InsP. Lefi Engine 740126 lnsp. # 1 eng. 7:00 plug 052300 300 Hour InsP. Right Engine 740611 Op. Chk. #2 eng.lgnition sYstem 230/;00 Clean Test CVR Beacon 740616 Insp. # 2 eng. 6:00 plug 240116 Overhaul# 1 Eng. St./Gen. 740626 lnsp. # 2 eng. 7:00 plug 260169 Vis. Insp. Cockpit fire extinguisher 780136 Clean/lube #1 eng. TR feedback cable 260181 Vis. lnsp. Cabin fire extinguisher 780636 Clean/lube #2 eng. TR feedback cable 330226 Battery,emerg.lights, 791621 Change#2eng.Oil 330228 Charge emerg. light battery 91 1290 SB1 124-27 -129 left aileron 344616 lnsp. emerg. Power suPPlY 911291 SB1 12+27 -129 right aileron 350166 Check pilots 02 mask 911400 SB 112+29A-140 rePlace CB 350169 Check co-pilots 02 mask 973636 SB TFE731 A72-3636Ieft engine 530200 Insp. Fwd - Aft Press. Bulkhead 973665 SB TFE731 A72-3636 right engine 530205 Insp. Fwd to aft main frames 990020 AD74-0&09 Lav Waste 710109 Check # 1 Eng. Elect. Wire/Conn. 990131 AD89-12-08 Spar splice insP. 710110 Check # 1 Eng. Plumbing/Conn. 991615 AD 984&10Insp. Hyd. Fuses 710609 Check# 2 Eng. Elect. Wire/Conn. 991560 AD 9G2+11 LeftAileron 991561 AD9612+11 RightAileron end @' eamP systems Int'l' co^puterized Aviation Management product: OPERATOR: lCoxt N€s,|.st FTrxrees t^Jc. I , WORK COMPLIANCE FORM NO. AfRCRAFT NO.: 368 MODEL: t tzq A hJ64 7a1tvt 6. r., grs s PAGE 1 l:ggJ9_tt_T!^!g$ rccompilrlr.d to?..ch tetr rcop whil. clpy ror youJ necroru3. R.tum yallow cogy to cSt for uodidno. t iISC}CD|.|,ED q voR( Accor'fPLISHED: DATE: nowxlO oau od t:url V ATRcMFT nouas: 6 9/1 .{ ulmrres:Z- rcj TECHI{ICIAI{ SIGilATURE: --at? KIilD oF CERTIFICATE & ro.: o ITfsPEcTED fu( st: <. 9 KtrD 0F cERrrFrcArE & / o? '0.: -q7 corfPotfEr{r clolt 74qL&l pARr r{41fE: ?tf E,tP-sag{Jz AF c. // 2- p0SrTr0n: Z 2 REASotl REilovED: (CHECK 0t{E) TECHIII CIAII: IIIS P: Til4E A( ) FArL 8( ) roRil C( LoAI{ER 0( SCHEDCOT{V r40D G( ) ) E( ) ) sERvrcE K( ) Er{G CHG L( ) TIRE CHG r,t( ) DAXAGED T( ) PART REIIOVED: PART I{UHBER SERIAL I{UI,I8ER: | o4o PART IITSTALLED: PART nuneea_j9-? j.$3 q -L sERIAL r{uxBER: o^ & - 47 6 g IIISTALLED TSN: HRS - LDGS f{os_ II{STALLED TS0: HRS LDGS tr{os |,ARRAI{TY TIiIE RE}.IAINING: HRS LDGS trtos MAN-H0URS: HRS_TENTHS_PRICE: $ REI,IARKS: Fe Lr,n *t oo Lr-Le t AP a <-( K-t3 TFe"? t= 7z-76a>t p 44 * 72->r6q - h 873 C-. o.r R*'optN. v RECoRD l{oRK ACC0}{PLISHED FoR TASKS IfHICH REQUIRE SPECIAL C0|'IPLIAIICE DATES: (SIGil oFF AS AppLICABLE) (€ C()DE TASK DESCRIPTI()I{ oATE i'ro/0A/yR TEcHr{ICIAN INSpECToR }tAr{-H0URS HRS.THS oti CALIBRATI()TI TEST/POS ITIOI{ : : I g9 I.IEIGHT CHECK/P()SITI()I{ : ct !Egd HYDRO TEST/POSITI(}I{: oEtro 6I CARTRIDGE /POS ITI()II: II{STALLED DATE: _/_l EE P6 CARTRIDGE /P()SITIOl{: DATE STAXPED. OE _l_l ;c;x> CARTRIDGE/P0SITIoil: II{STALLED DATE: ot _l_l_ s3,>6 E! CARTRIDGE/POSITI 01{: oATE STAilPE0. _l_l oo3- 60=O ()TIIER: lr; EXPIRATI0I{ DATE: _l_l !i.gs 9. REC()RD COIIPLIAIICE (lF II{SPECTIOIIS, SERVICES, ()R EE AD, S8 AI{Y TI(IRK ACCO'{PLISHED I{ITH COIIPOI{E]{T CHAIIGE ABOVE. 6iEO C(lDE TASK DESCRIPTI()II TECHIIICIAI{ II{SPECTOR tlAll-H0URs HRS. THS Ee2A qJz e e-/e og 3a V)zz-gse| W f4,n u ?*o I r 577> hDqt octo6 1lts57 hD qatg-t3 rr T.nr- At htu Aoqs tt Op \-' 4ats2G AvlO-o4-ol N /A 3r 3.N. ?,"c. REIiIARKS: @ Canp Systems tnt'L computerized Aviation Management productr E.rr.reeS OPERATOR: lAar-.t Ns''-.rtt f , tpc. WORK COMPLIANCE FORM NO. AfRCMFT NO.: 368 MODEL: t tZq A L)c4 T+tttt o. r.J s ers PAGE 1 Rccord time wor* tccornplirhad to? crch tlt& K..p whlte copy to? your !qc!rd!. Rrrum y.$ow copy to c!;l to, tt{3c}C[rr.o llORK ACCOIIPLISHED: DATE: xOnrn_/O_Onv oG uua 1{ AIRCMFTHouRS: 6dq.{ Lffi0ilrGS: +reg TECHIfICIAII Slct{ATURE: /?< KIilD 0F CERTIFICATE & lt0.: ,41(O IrfsPEcrED atz y'll Ld9 KrilD oF cERrrFrcArE & 1t0.: Ipq ^1/ Itatltttlttttt ttti q 5oq+ | I ,A cotfpot{Enr cooe: 15fr4L pARr NAfiE: gL,uv -L144 Fb 4Zt4t-C, Edal P0SITIoII: L? l< Vo llru Pser. lp>n f'.Ja'c Reoo Pert Ur.laeec l?r*,r.r5. REAS0ll REI{OVED: (CHECK OilE) TECtll{lCIAll: _ Il{Sp: Til4E A( FAIL B( t{oRil C( LoAI{ER D( ) ) ) ) SCHEDCOIIV E() I4OD G() SERVTCE K0 EI{G CHG L() TIRE C}IG I,I() DAT{AGED T() PART REI{OVED: PART I{U}I8ER SERIAL IIUHBER: PART II{STALLED: PART I{UIIBER SERIAL I{UilBER: INSTALLED TSN: HRS_LDGS ilOS_ IilSTALLED TS{l: HRS LDGS_fi0s lfARRAt{TY TIilE REl,lAIltlNG: HRS_ LDGS MOS MAN-HOURS: HRS TEIITHS PRICE: $ REI,{ARKS: Y REC0RD l,foRK ACCoI'{PLISHED FoR TASKS I{HICH REoUIRE SPECIAL Cor.tpLIA}tcE DATES: (SIGI{ oFF AS AppLrcAsLE) TASK DESCRIPTIOI{ O DATE I{O/DA/VR TECHI{ICIAN INSPECTOR I,IAN-H()URS 6| HRS. THS ott CALIBRATI(lN TEST/P()S ITI(lN : : { IIEIGHT CHECK/P(lSITIOI{ : .09 _/_/_ c3 !E HYDRO TEST/P(lSITI(lN: Ed rEco o! CARTRIOGE /POS ITIOI{: II{STALLED OATE: _l_l -89 p6 CARTRIDGE/P(lSITIOI{: OG DATE STAilPED. _l_l Eg o? CARTRID6E/POSITI 01{: II{STALLED DATE: _l _/ >6 3g CARTRIDGE/POSITIOII: t-og DATE STAIIPED. _l_l_ (lTHER: €s>-3 EXPIRATI0II DATE: l_l_ i3 REC(IRD ()F 9. C(}}IPLIAI{CE I1{SPECTIOI{S, SERVICES, AD, SB OR AI{Y IIORK ACCO}IPLISHED YITH COi,IPOI{ETIT CHAI{GE AEOVE. EEto 6-o CODE rAsK DEscRIprIor TEcHr{rcIAr ll{spEcroR ilAr{-H0uRs 2A HRS. THS EF octoo \,- - REIIARKS:- - Effi CamP Systems Inttl' computerized Aviation Management product: OpERATOR: l4Org Nerl..rq f E-rr.rees , tr".:c. WORK COMPLIANCE FORM NO. AIRCRAFT NO.: 96v MODEL: Itzq A bJ€r,u,r-o. as sef d PAGE 1 1:..99_tl_T!^a"tt accomp[.h.d tor.rch t..ri Xorp rdrh. oopy ror your nrcrorur. R.ntm yallow copy to csl to? ugdidnq. II\ISO€,.ED IJORK ACCOI,IPLISHED: DATE: XOXrrr:,'I O6 YEAR--1!. AIRCMFT NOUAS: 69Q.€ vuo:.irresz*88? TEcH1{IcIAl{SIGt{ATURE:,E*tilDoFcERTIFICATE&il0.:,9r/.o-DAI .4 IrfsPEcrED et, plU(5 nilg oF cERrrFrcArE & r{0.: ffi /g1-q7 pARr coxpot{Erfr cooz: 77oZz(o r{Ar4E: ? ^y &*A, karrr POSITI()II: REASoI{ REI,|0VED: (CHECK oilE) TECHI{ICIAI{: : rnse: il kS Til,tE A( l rArr- a1.filoRil c( LoAiER D( SCHEDC0]{V il00 G( ) ) E( ) ) SERVICE K( ) Er{G CH6 L( ) TrRE CHG fi( ) DAT,|AGED T( ) pARr PART REr,fovED: ilunilER-__a@ 7gAF^l-ool SERIAL IIUI4EER: ,'6 N pARr IART nfsrALLED: r{uMBER- AV - ZTV SERIAL t{uilBEar?.9 p' II{STALLED TStf : xnS -{/ uteS -?- nos a INSTALLED TS(l: HRs ffi IIARRANTY TI|4E REl,tAIt{I}tG: HRS LDGS _M0s_ ilAil-HouRs: HRS_TENTHS_IRIC8: $ REI,IARKS: v RECoRD tl0RK ACC0IIPLISHED FoR TASKS'vHICH REQUIRE SPECIAL C0HPLIAilCE oATES: (SIGi{ OFF AS AppLTcABLE) TASK DESCRIPTIOII an DATE [0/DA/YR TECHNICIAN Ir,rsp€CToR t'tAN-HouRs GI tr HRS . THS 6) CALIERATION TEST/POSITIOI{ : : _t_/_ : I{IIGHT g>aO CHECK/POSITIOIT: ct E2 HYDR() TEST/POSITIOI{: 9a _/_/_ :E OI CARTRIDGE / P(lS ITION: INSTALLED DATE: _l_l g.Y p6 CARTRIDGE/POS ITIOI{: DATE STAtfPEoz OG _l_l_ Eg o? CARTRIDGE /P05ITr0t{: ITfSTALLED OATE: _/_l >6 FC oO CARTRIDGE/POSITI(lI{: DATE STAI{PED | _l_l_ ;Eoa =4, OTHER: ool-; EXPIRATIOII DATE: /_l a'- .gs REC(IRD (lF 9. COIIPLIAI{CE IHSPECTIOI{S, SERVICES, AD, SB OR AI{Y IdttRK ACCOXPLISHED |ITH COI.IPOIIEI{T CHAI{GE ABOVE. I AE 6iEO CODE TASK OESCRIPTIOII TECHIIICIAI{ IIISPECTOR l,l tl-H0URS 2e j7"?2Y (){,4u,G q+r HRS. THS Eo,otr Go*n .L F**, .-4 alb3 o()oo L, REilARKS: p"r, @ Systems lntrl, computerized Aviation Management Product: OPERATOR: l4arg He,-r't FTve+s , tpc. I WORK COMPLIANCE FORM NO. AfRCMFT NO.: 36a MODEL: ttz+ A LJ647aupo. N vs se1 PAG 1 f9..o! tlT"-notL accomplrhrd tor..ch t.|i recp whit copy ror you? n!eotd3. !.nlm ydlor copy to CSI for uoditno. II\ISICTCDUTD roRK ACCoIfPLISHED: O ,tu^-a (. DATE: t4onTHj/O DAu 6 1TRCMFT H0URS: A 9n . l-Al{Dll{GS:4W TECHI{ICIAII SIGIIATURE : .'?-> KIflD oF CERTIFICATE & 1{0.: IIISPECTED BY: 144S KrilD oF cERTrFrcArE & r{0.: r".1 ffiffi -q7 corporfErfr pART cooE. Zqo(6/ r{A}tE: /r->P, Lrtc f?apz POSITIOI{: REASoll REtl0vED: (CHECK oltE) TECHtlIClAtl: :.J|sPt /4k[ TrxE A( ) FArL 8( ) uoRr{ C( LoAl{ER D( SCHEoC0ilv E( xoD G( ) ) ) ) sERvrcE K( ) EilG CHG L( ) TIRE CHG il( ) 0AIiAGED T( ) - PART REil0vED: PART t{Uil8ER SERIAL IIUIIBER: PART II{STALLED: PART NUI,IBER SERIAL I{UI,IBER: II{STALLED TSt{: HRS_LDGS t{os_ INSTALLED TS{l: HRS_LDGS_1{0S I{ARRAI{TY TIl,lE RE},lAIllIilG: HRS LDGS r,t0s I,IAN.HOURS: HRS .- TEiITHS_PRICE: $ REMARKS: -- Q c+ tPn \-. RE}.IARKS: ffi c"rp systems lntrr, computerized Aviation Management Product: OPERATOR: fCOrg Nscru E-rr.rees te.:c. I , WORK COM PLIANCE fOnrrril{O A|RCMFT NO.: 36v Nvssq MODEL: ttzqA L),{"Tr-t,t-o. PAGE 1 Rocord tm. uort accomplaahcl tor cacn terl-Gp w|rata copy tor your ccordr. Rcqrm ycttow-coiv d-csfi; u'Ji.s.,o. t ilSClClxLE troRrAccolfPLIst{ED: O'f DATE: xonrx DAy // ueee nt ATRCRAFTHouRS: 6BSg.? *orrnr, A??S.-- TECHIII CIAI{ 5 IGIIATURE : G.7 KrrD oF cERrrFrcArE & r0.: f4re- u-s,.sT ?? II.SPECTED L?,1 BY: KIilD 0F CERTIFTCATE & lt0.: triltr r ratr ta a trrrt r lrttttr*ittttttffi @ 'r*ffi*t*rrrrrattir colfporfEl{T cooe: Zn oLoT pART t r{ArE: C_t/E (Lg ?+,2.- ?-- f POSITIOI{: REAS0ll REl,l0vED: (CHECK ()ilE) TECHT{ICIAI{: 4t.|l rnsp: Q.P- TIl,lE A(cj-FAIL ta0Rlt 8( ) C( ) L0AflER D( SCHEDC0T{V E( f,tOD G( SERVTCE K( El{G CHG ) ) ) ) L( ) TrRE CHG 1.t( ) DAilAGED r( ) PART REfi0vED: PART t{UilBER SERIAL IIU}I8ER: PART ITISTALLED: PART t{U}tBER SERIAL NUIIBER: II{STALIED TSN: HRs-LDGs-ir0s_ II{STALLED Ts0: HRS_LDGS M0s IIARRAI{TY TI}IE REIIAIIIING: HRS LDGS I.IOS- IiIAN-XOIJRS: HRS_TEI{THS PRICE: $ REI.IARKS: 2-oo3. RECoRD l{0RK v ACCoIIPLISHED FoR TASKS'llHICH REQUIRE SPECIAL C0HPLIA}|CE oATES: (SIGN oFF AS AppLrcAELE) TASK et DESCRIPTI()N DATE M0/DA/YR TECHi|ICIAit lr,tspEcToR MAl'l-H0URS s. g,t HRS . THS CALIERATION TEST/P()S ITIOI{ : : sl IJEIGHT CHECK/POSITI()II : c3 E2gd HYDR() TEST/P(lSITION: _l_t_ oEtro oa CARTRIDGE / POS ITI OII: II{STALLED DATE: _l_l :o il CARTRIDGE/POSITI()II: EE DATE STAI,|PED 3 _l_l Eg CARTRID6E/POSITIOI{: II{STALLED --<6; DATE: _l_l ag E! CARTRIOGE/POS ITI 01{: DATE STATIPED | t- _l_l €s>-: OTHER: ExPIRATl0tl DATE: /_l r!E REC|,RD COilPLIAXCE OF II{5PECTIO]{5, SERVICES, AD, SB ()R AIIY I{(,RK ACCOI,IPLISHED IITH C(!}IP()I{EI{T CHAI{GE A8OVE. c00E l'PE TASK DESCRIPTIOI'l TECHI{ICIAI{ II{SPECTOR ITAII.HOURS l9F HRS. THS 3s o()oo \.;," RE}IARKS: - € Camp Eystems Inttl, computerized Aviation Management Productr OPEMTOR: f4or-l Hece Trrrcfs , I t^tc. woRK colvtplr,nr.re,E ronru r.ro. AIRCMFT NO.: 36v Ntssq MODEL: / tz+ A LJcs rt+,r- o. PAGE T rccomptitlrc.l tor.rch t.rr frre wharo oopy roryourl:.c-9g_t_t n contr. _!ptt Banrm yallow ^ cogyto CSI tor uodidno. lrrlso€lt.E toRK ACC0I|PLISHED: DATE: ri0llrx Ol oau /t ,eea nB ATRcMFT uounsz G7 57-? pry91x65, z{-? {5- TECHI{ICIAI{ SIGIIATURE : e?.?, KrrD oF cERTTFIcATE & r{0.: E tr{e-sr q.P. -o. IIISPECTED 8Y: ' KIrfD oF cERTIFTCATE & ilo., q Q Lft q I Fu coilPotfEtfr cooe: z-Zo 6p,ART lArE: R-e. b*.* b*nny posrrron: REAS0I{ REIIOVED: (CHECK 0ilE) TECHI{ICIAI1: L.C lrsr: !Q TIIiE A(9/FAIL B( f0Rtl c( LOATER D( scHEDcorv ) ) ) E( ) r,roD G( ) sERvrcE K( ) EnG cHG L( ) TIRE cHG xl ) onnnero r( ) PART REIIOVED: PART TIU}IBER SERIAL I{UIiEER: PART IIISTALLED: PART I{U}IBER SERIAL I{UI{BER: I1{STALLEDTSt{:HRs-LDGs-M0s-INSTALLEDT50:HRsLDG5|,|0s IJARRAIITY TIl,lE REl.lAlllIl{G: HRS LDGS }tos |{AN-HOURS: HRS TENTHS_PRICE: $ r.\ REI.IARKS: D.JE* - DN^ I--59 zooS \r.o. 6?>7 \" REC0RD LORK ACC0IIPLISHED FOR TASKS THICH RE0UIRE SPECIAL C0ilpLIAr{CE DATES: (SIGr{ OFF AS APPLICASLE) o TASK DESCRIPTION DATE IIIO/DA/YR TECHTIICIAI{ INSPECTOR I4AN-HOURS 6. ot HRS. THS CALIBRATI()I{ TEST/P()SITI()N : _t_t_ : ! gE UEIGHT CHECK/POSITIOI{ : EE 2Z HYDR() TEST/POSITI()TI: Ed sEEO OI CARTRIDGE /POS ITI()I{: INSTALLED DATE: _l_l :o i; gE CARTRIDGE /P()5ITIOl{: DATE STAXPED | _l_l Eg : REI{ARKS: r'i TRANSPORT CANADA PAC IFIC A.M.O. 21 NOVEMBER 1998 AERO TECI I INC 109 - 97 w.o.980242 AIRCRAFT WORK REPORT REG'N: N83SG MODEL: 1124A AND LOGBOOK ENTRY A/C T.T.: 6580.3 S.N.: 368 'l report by M. Sjerdal Ldgs.: 4918 Page of 1 The following maintenance has been performed per customer request and the lsrael Aircraft Industries Westwind Model 1124 Maintenance Manual. 1 Minor fuel leaks on left and right wing lower surface sealed as required. 2 Base-line SOAP Sample taken from right engine. Refer to 731 Engine Log for detail. 3 Pilots and co-pilots microphone jacks repaired (terminals intermittently shorting). 4 Several interior trim items adjusted as required. 5 Fuel filters inspected, no faults found. 6 Pre-fl ight inspection performed. Pertinent details of the work performed The maintenance described has been are on file at this agency under performed in accordance with the WORK ORDER NO.'s 980242 applicable standards of ainrvorthiness and the aircraft is released for return to service. PACIFIC AERO TECH INC. tr VANCOUVER. B.C. - ar"to'itg TRANSPORT CANADA ALIISHMAIL M259246 Approved Maintenance Organization 10$97 DIRECTOR OF MAINTENANCE 4380 Agar Drive, Vancouver International Airport, Richmond, BC V7B 1A3 Tel: (604) 273'4649 ' Fax: (604) 273-4661 STANDARD stAf{DARD ALTITUI'E ALTIM;TTf ALTITUDE ALTIiIETIR FT. , RhDS FT. READS r.000 tood la.0oo qrlclt o 6 16.o00 t.6(r;^ t00 i^q rt.ooo 'rqto r.ooo arar( 20.000 rqqlo 1.500 Rorgwest E ATE:04/0780 Turbine Aircrcft 6,7X.6 6,,109.8 6,7n.O Maintenance 4,999 4,656 4,555 . Complied with 200 Hour 'A" Check and Preflight inspection. . complied with monthly visual and 1 2 month weigf{ check of the portable lire extinguishers. ' Complied with 12 monlh inspection of the first aid kit. . Complied with the 6 month cleaning, inspection and testing ofthe CVR ULB and battery. . Complied lyith 200 hour 3 month seMce of the main, emergency light and emergency gyro po'tier suppliea. Remov€d right Mdn Battery P/N 30126001, S/N 9506152 and reinstalled aner deep cycMop charge. See Aviall FM Form 813O.3. Removed bn Main Battery P/N 301 m4O1 , S/N 881 m74 reinstalled affer cell replacement, deep cycle/top charge. S€e Aviall FAA Form 81 3O3. Remo,/ed Emergency cyro Power Supply P/N PS823BT, S/N 1310 reinstalled afrer cell replacement, deep cycletop cha.ge and functional check. See Aviall FAA Form 8'130-3. Removed Emergency Lighting Battery Pack P/N 38,15'1401 , S/N 0196 and reinshlled afrer deep cycle, top charge ard functional test. Se€ Aviall FAA Form 813&3. . Removed all life vests and reinstalled aner recertification. See CAPS yellow tags athched. . Removed right Er€ine Fire bdrEuisher P/N 327m004, S/N 02429C1 and reinsblled after gauge replacement, overtEuland hydrclatic t€st. See HRD Aero Systems FAA Form 81303. . Removed lefr Nose Wheel Assembly P/N 9541874, S/N May76609 and reinstalled after tire change and NDT. See Aero Wheel FAA Fo{m 813G3. . Removed right No6e Wheel Ass€mbly P/N 954|874, S/N Apr86-123 and reinstalled afrer tire change and NDT. See Aero Wheel FAA Fom 813S3. . Removed right Main Wheel P/N 5002806-2, S/N MAR 84662 and reinstalled affer tire change. . Removed aileron trim hb actuator P/N 1092AS100-1 , S/N 1010 and inshlled overhauled actuator P/N 1092AS1q)-1 , S/N A10O2M. See Aero space controls'efr FAA Form 813G3. . Removed right engine starter/generator P/N 23065-01&1, S/N 2562 and reinstalled after rebrush. See WECO Aerospace FAA Form 813F. . AD 98-2$10 Aircrafr Belts is not applicable. Associated belts not installed. . AD 9&2542 is not applicable, B.F. Goodrich slqwatch not installed. . Complied with AD S5-224'l ALC Lighting. Replaced the forward lamp using the new series AL fluorescent lamp. Replaced the two lamp connectoF with the new serie€ AL connectors. Replaced the lefi #1 lamp, lorward lamp holder, which was melted, and the lefi #2 lamp, forward and afl lamp holders, Mrich were broken. Functional test of the fluorescent lighting system is okay. . Replaced right Nl circuit breaker. . Replaced lefr engine hydraulic pump and starter generalor garlock seals. . Fabricated a new cover for the door hinge from stainless steel. Installed and operational checked good. . Several cabin seat repaired by Aeronasch Aviation. . Removed lefr engine hydraulic atenuator, removed fi$ngs as required. Discarded defective seals and installed ns/,r seals. Inslalled hydraulic alenuator and secured. . Repaired forward fay seals on right hand #1 & #6 windo',rs. . Cleaned water separator condenser screen. . Repaked working rivets in lower lefr wing fairing and right wing trailing edge doubler panel. . Replaced avionics compartment desiccant (radar). . Repaired lefr and right engine inlet bulkhead loose and warking rivets. . Resealed left engine thrust reverser forward quick disconnect. . Repaired loose and u/orking rivets at right engine forward lo\,'rer cowling pip pin support plate. . Removed forward baggage door. Cut out section of damaged seal, cut new piece of seal to size and installed. Installed door on aircEfr, fit and operational check good. . Installed new door latch plastic cover on door frame. Items listed were inspected/repehed in accordance with aircrafr, engine and/or accessory Manufactur6 Mair{enance Manual requiremenls and cunent Federal Aviation Regulations. I certify that this aircrait was inspected in accordance with an inspection program as requircd by FAR 91 .409 (fX3). This aircraft is approved for return to service with resp€ct to the work performed. Details are on file under W.O.# 176. 7035 Sophia Avenue, Van Nu),s, cA 91406 FAA CRS UORR958L Rdgwest Incorporrt€d 7035 Sophia A!€rxle Van Nuy3. Califomia 91/tO6 818 9@-96q) FAX 8',1 8 904-(X53 AIRCRAFT MAINTENANCE RECORD A/c Res'n: N83SG A/c Model: 1124A Westwind A/c ser. No': 368 DATE A/C T.T. A/G T.Ldgs. DESCRIPTION DUNCAN AVloNlcs Date (.4 functional tested, fou nd ai rwo;it tttt::*,t$;?"e#, ^ -l;l *^ i"ti"t. A f,etailed recor!1s t6T5[ncan Avionics; Logbook EntrY m, RotgWest E an overhauled blorver P/N M125J-9D S/N 28' See Jet . Removed inverter blower P/N M125J-9D S/N 2657 and installed Service Enterprises, Inc.' s FAA form 8130-3. access I'T.T. hamess. (l.T'T' harness changed by Garrett . Removed and reinstalled iigf* engine airframe components to Aviation Services Los An geles. See Garrett engine log entry). . Replaced cockPit windsh ield desicant crystals. pin with a nal pin P/N 253401-1 ' . Removed and rePlaced k ywer scissor lini support bracket retaining . Serviced no6e landing g( ar s{rut with nitrogen onlY. ensine Items listed were inspectedrepaired in accordance with aircrafi , and/or-ac9::1-ry1HllT.I1'::"::l"Y1g r th;t this aircraft was.inspected in a@Qrdance with requirements and cunent Fed #iilffi;R&i"tion"- certify for return to servic€service withvnn resry{f thewukfr program required bY FAR ( )1.40er{ 4os (f)(3).(fl(3). This aircraft i" approved fot as "ppi6u"O are on file under W.O.# 290' 7035 Sophia Avenue, Van Nuy1s, CA 91406 FAA CRS UORR958L AIRCRAFT MAINTENANCE RECORD Ser. "\ A/c Res,n: N83SG A/G Model: 1124AWeStwind A/c No.: 368 DATE A/C T.T. A/C T.Ldgs. DESCRIPTION of scf,+ 17 AclT. 67Y 3'Ll a LN1 , f lo! (/y,.to-31s['0t L LoruAar A0.nnnp l'f,?( K.^*J (Lon-7 t6'0tL )A F;e o r^'s*)l,d '..'^inJ "^'i+ #,,;; . ab t"{;fir!ry,, "p*o N83SG WW 1.1.24 S/N:386 DATE: 10104/99 Airframe, 6911.9 #l,lEngine 6595.'l #2 Engihb 6863.3 Landings 5't24 Cy€les 4780 cyoles 4979 Complied with 200/400 Hour "8" Check Including Engines, Nacelles and pylons, 150 flight hours inspection, and preflight inspection. Complied with monthly visual of the portable fire extinguishers. Complied with the 6 month cleaning, inspection and testing of the CVR beacon. Complied with 200 hour 3 month service of the main, emergency light and emergency gyro power supplies. Removed right Main Battery P/N 30126-001 , S/N 9506152 and reinstalled after deep cycle/top charge. See Dynamo Aviation Inc.'s FM Form 81 30-3. Removed left Main Battery P/N 30126-001 , S/N 881264 reinstalled after cell replacement, deep cycle/top charge. See Dynamo Aviation Inc.'s FAA Form 8130-3. Removed Emergency Gyro Power Supply P/N PS823BT, S/N 1310 reinstalled after cell replacement, deep cycle/top charge and functional check. See Dynamo Aviation Inc.'s FAA Form 8130-3. Removed Emergency Lighting Battery Pack P/N 38451 -004, S/N 0797 and reinstalled after deep cycle, top charge and functional test. See Dynamo Aviation Inc.'s FAA Form 8130-3. Complied with a 12 month check of the crew oxygen masks. Removed left brake assembly P/N 5OO28O5-3, S/N M1 04 and installed an overhauled brake assembly P/N 5002805-3, S/N 1 140. Removed right brake assembly P/N 5OO28O5-3, S/N May 82-328 and installed an overhauled brake assembly P/N 5002805-3, Si N R1 21 53-6' Removed and replaced both main tires. P/N otilon 249K83-3, left S/N off 90750853, S/N on 92470'1 19, right S/N ott 8165'1721, S/N on 924€1280 4 ea. Wheel bolts were replaced (P/N GY187-36. Replaced water separator condenser. P/N 21 BC1 13. Adjusted cabin entry door stop pins. Replaced right main landing gear shock strut air valve. P/N MS28889-2. Replaced 1 ea. left generator annunciator lamp. P/N GE 387. Replaced aileron trim tab rod end. P/N BHM-47 Repaired right wing inboard flap drive coupling. Replaced 6 static dischargers. 2ea. P/N 16930,4ea. P/N 16785. Replaced right main gear ground contact switch assembly. P/N 44EN1-1 2 - switch assembly Rigged flap system and adjusted flap position indicator. Replaced 'l ea. Lavatory fluorescent lamp. PiN AL-1235-360 235-490, AL1 235-320, AL-51 13 connectors. Replaced # 1 ,2, and 3 iabin window indirect lamps and connectors. Lamp P/N's ALI 235-360, ALI Serviced oxygen system. Serviced toilet. Cleaned carpets. current Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures Maintenance Manual requirements and (D(3). Federal Aviation Regulations. I certify that this aircraft was inspected in accordance with an inspection program as required by FAR 91 .409 This aircraft is approved ior return to service with respect to the work performed. Details are on file under W'O.# 336. tuRoigWest IncorPorated 7035 Sophia Avenue, Van Nuys, CA 91406 FAA CRS UQRR958L AIRCRAFT MAINTENANCE RECORD A,/C Reg'n: N83SG a/c Moder: 1 124A Westwind AJC Ser. t'lo.: 368 L book Ent 6960.7 6643.9 #2Engine 6911.'t 4805 5004 Complied wth a 3 yea. hydbstatc lest oi the ehergency gear stokge botue P/N 36200071, s/N 07511A1 See HRDAeosystems, tnc sFAAFom 8130 3 comp ed with a 3 year hydrostan. test of the th rust relerser siorage botue P/N 36200071, S/N 075'l oAl see HRDAe.oSvstems, hc s FAA Form 6130 3 Repaired fuselage pressui zatio. eaks Complied wth Alerl SB No 1124 78A-134 Thrlsi reveGer secondary atch sotenoid check Removed lelt TT indicato. P/N 8O!313WAG1 S/N R0031R and rei.sta ed afier repa r See c oba Tech tnsirumenis FAA Form 8130,3 Removed#lthrustreverse.secondarylatchsoenodP/NF10A-5-scAV2001s/Nl€aandinstalledanewuntP/NFloA-5-scAvzoot s/N 1838 See Northrop Crummans certllcate ol coniomance Removed # 2 lhtust reverser secondary atch so eno d P/N F1 0A'5'SCAV200-1 S/N 349 and nsta ed an overhauled unit P/N F1 OA 5-SCAV2OO.1 S/N 154 See Nodhrop Grumman Stuart operatiors FAA Form 8130-3 ComPled wth a month y vsual of lhe cabin and cockpittie ext nguisheB Removed # 1 and # 2 starler generato.s P/N s 23065 01 8, 41 S/N 2562, # 2 S/N 2258 and reinstailed atler reDat and test See WECO Ae@soace Svsiems Inc s FAA Form 8130 3 s Replaced upper otatmg beaco. aft amp P/N 7079824 Complied wth AO 99'08-21 nspe.lPurtan B€nnet passenger and podabeotygen masks Renewed weather radar desiccani crystals Compliod with a masnetic padicle nspection on the # 1 eng ne FoMrd mounb Seo Ganet Aviation SeNices FAA Fon a13O-3. Remov€d # 1 engine Si/N P77482lofMP and installed a rentaiengine 9N P77195 See engine log bookiordeiaits Replaced 5loose ivets on lefte.gine lnlet b! khead Rvet P/N CR3243,4-i Removed righl ihrust reverse. actuator P/N F10A5SCH203-T 9N 2163 and insta led an oveha! ed iloaier) actuator P/N F10A5SCH203,1 S/N 0316 See Jet Seryice Enterprises, hc s FAA Form 81 30.3 Removed cabin air press! re safety va ve P/N 103278'6 S/N 110-870 a nd insta ed an overha! ed ui t P/N 103278 6, 9N 105,600 See Alliedsignal Aerospace Eq u pment Slstems FAA Fom 81 30-3 Items sted were irspected/repa red Ln accordancewiih ancGft, eng ne afd/o. accessory [4anliactwes Maintenance Manua .equnements and curcnt Federal Aeation Regulations cert ly thal th s aircElt ws nspected in accordafce wth a n inspect on prog ram as req ured by FAR 91 409(0(3)^Thrs akge rs approved ior return to setocewith r€spect to the work pedormed Detailsareonfileohderwo#36o ,/,/ ,./') t /1/16(4,"/r,- Ro gWest lrcorporated 7035 Sophia Avenue, Van Nuys CA 91406 FAA CRS UQRR958L UTAH JET CENTER Date: 11n',U99 Shop Order: 228 N83SG rvpe r.rc 1124A rorurrim" 6965.1 racrrnooo' N/A Landings 5138 Removed Hydraulic pump P/N 65WE01031-3 S/N 42-68-82. D Reinstalled Overhauled Hydraulic pump P/N65WE01031-3 S/N B1 -31 on right engine Run-uD. operatlonal check, & leak check salsfactory. The Aircraft and/or component identified above wEs repaired and inspected in accordance with current Federal Arr Regulations and was found aiMorthy for return to serylce Signed AIRCRAFT MAINTENANCE RECORD A/c Res'n: NB3SG A/c Moder: 1 124A Westwind AJC Ser. No.: 368 Loqbookog En |\tq?qa: ut t c, tzlu |/vv 6991.4 6643.9 #2Enqine 6943.8 Landings 5163 4805 Cycles 5032 Removed rentai engine S/N P77195 from the #1 (UH) position ofthis aircraft, installed customer's engine s/N p77482 and accomplished all required adjustments, leak and functiona! checks in accordance with the Allied Signal TFE 731-3J G Light l'raintenance l/lanual. See engine log book for details. complied with a monthly visual inspection ofthe cockpit and cabin fire extinguishers. Complied with a 1200 hr./36 month functionaltest of the emergency hydraulic fuse. Straightened nose gear foMard door. Removed and replaced right hydraulic pump pressure hose P/N 171 F005-6C R01 56, and return hose P/N 124F002- 8CR0240. Serviced oxygen system. Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures Maintenance Manual requirements and current Federal Aviation Regulations. I certify that this aircraft was inspected in accordance with an inspection program as required by FAR 91 .4O9(fX3). This aircraft is approved for return to service with respect to the work performed. Details are on tile under W.O.# 393. 7035 Sophia Avenue, Van Nuys. CA 91406 FAA CRS UQRR958L Logbook Entry Rorgwest 7020.0 6671.5 6971.4 5780 422 5050 . Repaired miscellaneous left and righl wing fuel leaks in accordance with Westwind 1124 Maint€nance Manual 28-1040, pg. 801-813. . Removed all four fuselage fuel bladders and inslalled new bladders in accordance wilh Westvlind | 124 l\raintenance Manual 2&10-00 pg.40&412. The follor/ing bladders v.,€r€ installed: P/N 5653088€03, S/N 80-24476. P/N 5653043-509, SiN 7934873. P 5653041510, Sf,t 7934891. P/N 2F15-35260-508, SiN 99-44562. Allbagslvere remov6d nexv from stock and inspected. Ses3ea. Aero Tech Services, Inc.'s FAA Form 8 t30-3's and lea. Galary Aerospace Certificale of Conformance. . Removed teff lor,v level fuel switch PN GF5500-52, S/N A966 and installed a na/v swilch P,/N GF550O-52, S/N A2225. See Aerospace Conkol Products, Inc.'s FAA Form 8130_3. . Removed righl lhrust re\,ers€r loanor €clualor P/N F10A5SCH20$1, S,/N 0316 and installed cusiomer's repaired actuator. Complied wilh ieak and functional lests. See Jel Service Enterprises, Inc.'s FAA Form 813&3. . Complied with monthly visual inspeclion ofthe cockpit and cabin fire extinguishers. . Comblied wilh a deep c,ycle on the emergency light battery P/N 2GS113, S/N 0797- see Dynamo Aviation lnc.'s FAA Form 8130_3. . Com;tisd with a deep cfcte on the emergency power supply battery P/N PS-823 B/T, S/N 1310. s€e Dynamo Avialion Inc 's FAA Form 8130-3. . Comptied with AO 9923-22 rev. 1 dat€d 11-29.99. ltode C transponders wilh single Gillham cod6. A.D. found not applicable per aircrafl type. ' Repaired afr baggage compartment open indicator annuncialor rigging. . Complied with r;se;Ing and painttouch up on panels and fairings removed for fuel l€ak repairs Items listed were inspected/repahed in accordanc€ wlh aircrafl. engine and/or accessory Manufactures Maint€mnce Manual requirements and currenl Federal Aviation Fegulations. I cediry lhal lhis aircrafl wss inspected in accotdance $ilh en inspectron program as tequired by FAR 91.a09 0(3). This aircran G approved for relurn lo setuice wilh respocl to the work perform6d. hails are on,ru fil€y+r W.O # 4t2 Roigwest Incorporaled 7035 Sophia Av6nue, Van Nuys, cA 91 406 FM CRS UORR968L AIRCRAFT MAINTENANCE RECORD A/G Reg'n: N83SG A/c Modet: 1124A Westwind A/G Ser. No.: 368 UTAH JET CENTER Shop Order: 240 01/13/00 5184 1124A rorattime Lanfinos N#N* N83SGrreevv- rvpeA,/c' , ,, , 'w . ^--^^^;=;dir--f!!LLTii"i' ooA Etainatallarl overhuualednrrorhttttr pump nepraililgh-et aoostlffilEN-.- 207oco1T3 s/N T-330' Rei nstatteo | ,f ^-i r^^t- check^haalz satisfactory'aalicfonlnnr aJN r-r z izz operational check and leak i')ri idiocdiig current above was repaired and inspected in accordance with The Aircraft and/or component identified tt for return to service' Federal Air Regulations and was found airworthy Signed Logbook EntrY DATE:01/18ie9 a repaired and tested inverter P/N 1A1000-1 D' S/N . Removed # 1 inverter p/N 1A1OOO-1 D, S/N C0253094 and installed 8130-3' CO363O'18. See Corporate Service Supply & MFG Inc''s FM Form P/N 2315M-24-8. see lsrael Aircraft Industries Ltd''s FM Form . Removed and reptaced right windshield wiper ruooei iefill 81 30-3. pumps' . Tightened loose wiggins fitting on right jet Pump line at boost . Tightened loose vent line in left wing. and/or accessory Mal Maintenance Manual Items listed were inspected/repaired in accordance with aircraft, engine return to *d;;;.d;nd current Fedlral Aviation Regulations. This aircraft is approved for performed. Details are on file under W 'O.# 426' 7035 Sophia Avenue, Van Nuys, CA 91 406 FM CRS UQRR958L Logbook EntrY N83SG WW1124A S/ll:,368 DATE:04124,100 -71't Q 6884.3 #2 Engine 7183.2 Airframe ' #1..Engine Landings 5301 Cycles 4942 Cycleg 5171 boost pump P/N 653744'505' Removed Left main boost pump p/N 653744-505, S/N 157 and installed a functionally tested s/N T-330. See Jet Service Enterprises, Inc.'s FAA Form 8130-3 dated oz29loo. 1TP1 -3. Removed left landing light switch P/N 1 TP1-3 and installed a new switch P/N Manual Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures.-Maintenance with respect to the work ,"qun".ent" and current Federal Aviation Regulations. This aircraft is approved for return to service oerformed. Details are on file under W.O.# 509. 7035 Sophia Avenue, Van Nuys, CA 91406 FAA CRS UORR958L N83SG wwl f 24 S/[tlrr,368 ,DATE: AZPz.laa Airfram€ 7106.8 ,#il, Engfne 6758.3 #2 Engihe 7057.2 t-andings 5232 cycles 4a73 cybrcs 5102 . Complied with a 200 hour "A" Inspection including Engines, Nacelles and Pylons inspection, 150 flight hours airframe inspection, and preflight inspection in accordance with the Westwind 11241'l'124A Maintenance Manual chapter 5 requirements. . Complied with a 24 month/1200 hour inspection /lubrication of the nose gear upper and lower outer body bearings in accordance with SL WW-2491 . . Complied with a 1 200 hr. Inspection of the nose gear outer strut body actuating cylinder attach lug root and upper bearing retaining nut lock screw thread area in accordance with SB WW-2+28. . Complied with an 800 hour recurring inspection of the nose steering bracket in accordance with SB 1124-32-139. Complied with steering brackets modification and reidentification in accordance with SB 112+32-'139. lnspection is now due every '1600 hrs. . lnspected life preservers. Due 04/06/01 . . Complied with visual and weight check of the cabin and cockpit portable fire extinguishers. . Comply with cleaning and test of the Cockpit Voice Recorder beacon. EXP - Feb. 2003 . Complied with SB 112440{36"A" Inspection of the windshield heat cycling contactors. . Complied with SB 1124-55420 and AD 89-12{8 Inspection of the horizontal stabilizer aft spar splice fitting outboard lugs for cracks. . Complied with SB 1124-27 -129 and AD 96-24-11 lnspection of the left and right aileron control push pull tubes. . Inspected first aid kit. . Complied with a 1200 hour functional check of the fuel dump system. . Complied with a 1200 hour cleaning of the left and right anti-skid control valve filters. . AD 98-25-10 R1 is N/A due to equipment installed. . Complied with 150 hour engine inspections on the left and right engines. See engine logs for details. . Removed main batteries P/N SP-400 #1 S/N 9506152, # 2 S/N 8812674 and reinstalled after deep cycle. The # 2 battery had cells # 17 and2 replaced - P/N 40SP100. See Dynamo Aviation, Inc.'s FAA Form 81 30-3's. . Removed emergency gyro power supply P/N PS-823 BiT, S/N 1 310 and reinstalled after deep cycle and pack "B" replacement. See Dynamo Aviation, lnc.'s FAA Form 8130-3. . Removed emergency lighting battery P/n 20-51 13 and installed a deep cycled baftery with 20 new cells P/N 51 1 3. See Dynamo Aviation, lnc.'s FM Form 81 30-3. . Removed and replaced both main tires P/N 249K83-3 # 1 S/N off 9246'1280# 1 S/N on 72120380,#2 SIN off 92470119 # 2 S/N on 72231328' Wheel bearings were cleaned and repacked with Mobil grease 28. . Resealed nose gear strut with winterized seal kit PiN SVC600. See FM Form 337 datedO2l2ZOo. . Removed left windshield temperature control box P/N HYLZ 9661 , S/N 2368 and installed a new windshield temperature control box P/N HYIZ 9661 , S/N 9828. See Barber-Coleman Company's FAA Form 8130-3. . Removed pilot's windshield p/N 343030-1 , S/N 5343030 and installed a new windshield PiN 343030-1 , S/N 98342HO422. See PPG's certificate of conformance. . Replaced printed circuit lamp assembly PlN7OOO72-2 on trim indicators back lighting panel. . Replaced pilot's side Davtron clock battery P/N 81 1-BATT-1 . . Replaced 5 ea. Rivets P/N CR3243-4-2 on left engine inlet on aft side of the bulkhead. . Replaced 1ea. Rivet P/N CR3252-5-5 on left engine "D" ring at the 6 o'clock position. . Installed a terminal block cover on the # 2 starter/generator. . Replaced the # 2 hydraulic pump gasket P/N MSg't35-01 . . Replaced 20 ea. Rivets P/N CR3243-42 on the aft side of the right engine inlet bulkhead. . Replaced 1 ea. Lamp P/N GE1437 on entrance/emergency light assembly. . Resealed right forward main gear actuating cylinder with seal kit \l/W-1 13. . Installed new bumpers P/N 123585-1 1 on cabin entry steps. . Replaced lamp P/N GE1495 at the right aft cabin seat reading light. Service . Removed nose gear inner body p/N Es12858-501 , SiN U N Kand installed a repaired inner body P/N Es1 2858-501 , S/N 22705. See Jet Enterprises, Inc.'s FAA Form 8130-3. . Replaced inner body bearing lock pin P/N 13372-1 ED. . Fabricated and installed with velcro a leather flap for baggage compartment entry. . Repaired back lighting panel on the overhead cockpit center section. . Replaced the cockpit desicant crystals. . Rigged aileron and rudder trim in accordance with Westwind 112411'124A Maintenance Manual. . ReglueC trim piece on cabin beverage table. . Repaired fuel leaks at the left and right wing spar main gear trunion fitting. . Replaced eleckical "D" lead terminal on the # 2 starter/generator. . Replaced various access panel screws that were stripped' . Secured the hydro lock button in the armrest of the # 'l left cabin seat and recharged hydrolock. . Recharged hydrolock on the left # 2 cabin seat. . Repaired right logo light. . Applied anti-chafe protective sealant to the left and right windshield thermistors. . Torqued the left aileron belcrank bolt to repair excessive trim tab freeplay. . Repaired right tip tank fairing seal. . Repaired bent nose landing gear forward door. . Repaired single point refueling plumbing shrouds forward of the batteries. . Serviced oxygen to 1800 Psi. . Serviced toilet. cfeaned cabin and cockpit carpets' ' --- air+ratr anaina anrrlnr 2^^acc^ru r\,/ranr rfacfr rres Maintenance Manuar requirementsreouirements anda cunent Federal 1 Items listed were inspectedlrepaired in accordance with aircraft, engine and/or accessory Manufactures Maintenance Manual 91 Aviation Regulations. I certify that this aircraft was inspected in accordance with an inspection program as required by FAR prjD?) I)fircraftE approvedforreturntoservicewithrespecttotheworkperformed.DetailsareonfileunderW.o.#4,|4.6l-6(eA RoigWest IncorPorated 7035 Sophia Avenue, Van Nuys, CA 91 4Oo FAA CRS UORR958L AIRCRAFT MAINTENANCE RECORD G: Alc Res'n: NB3SG A/c Modet: 't 124A Westwind AJc ser. No.: 368 Logbook EntrY ww1124 7'169.9 *l Engrne 6421 .1 7121 .2 5271 Cycles 4912 Cycles 5141 Repaired various fuel leaks in fuselage and wings in accordance with I A.l. lvlainlenance l,4anual ch 28 complied with a monthly visual inspection of the cabin and cockpit fire extinguishers Complied w1h No. 1 ani No. 2 nose wheel tire change and balance. Tire P/N's off/o^ 164F 43-2, No. 1 S/N off 80070818, S/N on 91870826. No. 2 S/N off 80061000, S/N on 918901 12 Repaired loose edge on the bottom of the left wing deice boot Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures Maintenance Manual requirements and cuirent Federal Aviation Regulations. This aircraft is approved for return to service with respect to the work performed. Details are on file under W.O.# 475. 7035 Sophia Avenue, Van Nuys, CA 91406 FAA CRS UQRR958L ,1/,t t!t. r g trud. a lA./: JTJA 'rt /Ua: r.f t //r 54t J8 ido.: Rdioved lie plots oldio co.l'dl p/i 52?-l,6]-m1 3/' t?9 ond inrlold oudio c..fd p/i 522-y63-m1 t/n t17. 5|!{str ldd 0..d. @_e. lh. ondofl dndlo' co.iro.lall id61lifid obd! sr ,+dnd oid in?.cld in o@doic€ tilh dtrc]l DF3 oid b.ro.oyrd Io. rcb'.€d lo r'tff- m.'b,tt M blp ^,zfuL-" ta NiB CV 9t4)6 ftt-4ew a/f Pq. Wg .1,t !*. u r.of Jza 't/t WC: tlr.t //c s^ J6 ,dio.: nFoi.d ih€ ploi! il9 p/n a2?-1176-mr e/i lA dld imi.lkd tls p/n d?-!176-ml t/h 871. Sptri ldd fn@_M. lh! otdolt ond/d dnpdEl idaliild obdt! rB radnd ond iiT.cid in occodoic! tlh d'6ti FrR's oid h ooo.ord r& dumld lo stc!. a*2LzqLz'"o & L'Ai, 4a t i? tB-44Wt (.4y\\, .' N83SG 7324.9 6977.A 7275.3 5360 Cycles 500'l 5230 Complied with an 800 hour "C" Inspection including Engines, Nacelles and Pylons inspection, 150 flight hours airframe inspection, and preflight inspection in accordance with the Westwind 1 124111244lvlaintenance Manual chaDter 5 reouirements. Complied with an 800 hour Structural "8" Inspection in accordance with Westwind 112411124A Structural Inspection Program. Complied with weight and visual check of the cabin and cockpit fire extinguishers. Complied with SB 112430{36"A" Inspection of the windshield heat cycling contactors. Complied with SB 1124{5{20 and AD 89-12-l}8 Inspection of the horizontal stabilizer aft spar splice fitting outboard lugs for cracks- Complied with SB 1124-27-129 and AO 96-24-11 Inspection ofthe left and right aileron control push pull tubes. Complied with SB 1124-26-135 Fire Protection - Fire Detection System - Press - To - Test Switch Reliability lmprovement. Installed 2 ea. M83536/16- 022M relays. See Flame enterprises Inc.'s Certificate Of Conformance dated 7/21l00. Removed main batteries P/N SP-400 #1 S/N 9506152, # 2 Si N 881 2674 and reinstalled after deep cycle. The # 1 battery had cell # 17 replaced - P/N 40sP100. See Dynamo Aviation, Inc.'s FAA Form 8130-3s dated 7tl00. Removed emergency gyro power supply P/N PS-823 B/T, S/N 1310 and reinstalled after deep cycle. See Dynamo Aviation, Inc.'s FAA Form 8130-3 dated 7 t11t00. Removed emergency lighting battery P/N 38451-004 and installed after deep cycle. See Dynamo Aviation, Inc.'s FM Form 8'130-3dated7nn0. Removed oxygen cylinder P/N 6350A25-EEZ, S/N 49928W and reinstalled after hydrostatic test. See S.J. O'Brien Ent., Inc.'s maintenance release /yellow tag dated 8/10/00. Removed the copilot's windshield P/N PPG 343030-2, S/N 8,fH-1-2-096 and installed a newwindshield P/N PPG 343030-2, S/N 99158H0464. See AVPAC's certificate of conformance. Pressurization and heat functional check was satisfactory at this time- Removed the left N1 indicator P/N 8DJ278WAD|, S/N 80062 and reinstalled after repair. See GlobalTech Instruments' FAA Form 8130-3 dated 7/10/00. Removed the fuelstatus indicator P/N 308-90+001, S/N 173 and reinstalled after repair. See GlobalTech Instruments'FAA Form 8'30-3 dated 7/10/00. Complied with SB 1124-33-121 "Lights - Cabin Fluorescent Lighting Support System lmprovement", by removing 14 cabin fluorescent light power supplies P/N TR992, S/Ns off: 9376,6406,6399,6376,6460,6367,6,{39,6423,6500,6,159,6478,6,103,6462,9413, and installing 14 protected power supplies P/N AL- 51 12, S/Ns on: 35817,35819,35816,35820,35825,35822,358'18,3581 435a21 ,35a27 35A26,35823,35824,3581 5. See Aerospace Lighting Corporation's FAA Form 8130-3s dated 7/1 5/OO. Repetetive action of AO 95"22{1 "lnspection of fluorescent lighting system following a failure" is no longer required due ^ to this upgrade in power supplies. Replaced 2 ea. cabin Ruorescent lamps P/N AL-1235-460 utilizing new connectors P/N AL-51 13 in accordance with SB 112+33-131 . See Aerospace Lighting Corporation's FAA Form 8130-3 dated 1/1200 for the lamp and Corporate Air Parts, Inc.'s material certification for the connectors. Replaced the following cabin fluorescent lamps: 1ea. AL-1235-360, 1ea. AL-1235-320, 1ea. AL-123,122O,1ea. At-1235-490. See Aerospace Lighting corporation's FM Form 81 30-3s dated 4/1 0/o0, 7 h 4lo0 , 415100 , and 7 zaloo. Removed left main gear upper body P/N 253505-501 , s/N UNK and installed a repaired left main gear upper body P/N 253505-501 , S/N 479 . See Jet Service Ente.prises, lnc.'s FM Form 8130-3 dated 6/9/00. Replaced upper strut bearing P/N ED 1291 8-'1 and reseaied strut with an SVC-500 winterjzed seal kit. Repaired right main gear upper body inner bore in accordance with Westwind I 12411 124A maintenance manual. Replaced right main gear strut upper bearing P/N ED '12918-1 and resealed strut with an SVC-500 winterized seal kit. Removed the tail rotating beacon P/N G99501 1 , S/N 1 1709 and reinstalled afler overhaul. See Weco Aerospace Systems, Inc.'s FAA Form 8130-3 dated 7 t13tOO. Removed the right engine starter generator P/N 2306t018-1 , S/N 2562 and reinstalled after overhaul. See Weco Aerospace Systems, lnc.'s FM Form 8130-3 dated 7/13/00. Removed windshield wiper motor assembly P/N XW21 126-315-R32, S/N 2-22826 and reinstalled after overhaul and test. See Consolidated Aircnft Supply co. lnc.'s FAA Form 8130-3 dated 712200. Removed left and right main wheel assemblies P/N 5002806-2, #1 S/N Jun89-537, #2 Mar9,l-662 and reinstalled after N. D.T. and tire changes. Tires P/N ol on249KA3-3,#1 S/N oftunk, S/N on 72070859, #2 S/N off unk, S/N on 60470266. See Aero WheelAnd Brake Service Corp.'s FAA Form 8130-3 dated 7 tlUOO. Installed a PMA approved lavatory seat belt kit P/N SKJ 73 in accordance with MR STC # SA4318SW. See FAA Fo]m 337 dated 7/26/00. Aircraft is now approved for passenger occupancy of the toilet seat for take-off, landing, and flight. Removed and replaced right nose steering cable P/N 503-028-535. See lsrael Aircraft Industries Ltd.'s FM Form 8130-3 dated 12124198. Removed and replaced water separator condenser P/N 218C113. Adjusted and serviced all cabin seats. Removed left and right tip tanks and performed luel leak repairs on tank mounts. Reinstalled tip tanks with new aft mount bofts P/N 213717-50,| . Performed laminate repairs on cabin interior cabinels. Removed and replaced the forward baggage seal P/N 1900010. Removed and replaced the aft baggage seal P/N 1910061. Removed and replaced the left engine fuel filter P/N 897513-1 due to a popped bypass indicator. Reset bypass indicator, ran the left engine. Indicator checked good (not popped). Adjusted nose steering cables to manufacturers recommended tension. Replaced oxygen system tilling adapter P/N A300. Replaced radar waveguide desiccant. Secured pilot's and copilot's cockpit side pouches by installing some new nut plates. Replaced right engine aft upper and lower mount bolt nuts P/N AN310C6. ,m, '%/t Repositioned and tightened the left thrust reverser actuator clamp. Slightly repositioned left engine fuel hose to prevent chaffing on cowling. Tightened taper pin on the right elevator torque tube to eliminate extraneous play and safetied. Repaired various fuel leaks on the left and right wings roots just aft of wing spar. Reattached left and right fuel catch tray drain lines to drain masts. Cleaned and treated blue water stains under toilet. Adjusted the right flap linear potentiometer to obtain the required flap comparator readings. Replaced 1 ea. static discharger P/N '16785 on the left horizontal stabilizer. Replaced 1 ea. static discharger P/N 16785 on the right wing. Removed and replaced 3 ea. Rivets on the right engine nacelle inlet bulkhead. Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures Maintenance Manual requirements and current Federal Aviation Regulations. I certify that this aircraft was inspected in accordance with an inspection program as required by FAR 91 .409 (0(3). This aircraft is approved for return to service with respect to the work performed. Details are on file under W.O.# 54O. RoigWest Incorporated 7035 Sophia Avenue, Van Nuys, CA 91 406 FAA CRS UORR958L AIRCRAFT MAINTENANCE RECORD A/c Res'n: N83SG A/c Moder: 1 124A Westwind gC Ser. No.: 368 a/: tq.. lug ,!y' te(. /11 tW: J.'Jb ,4/t t/&. //24 1/t 5.4 ,16? A.i6: Re'io'ei f2 m. {odd l-144 P/N ?567rqJ-lll, s/N 61G56t1. l€Llld loond a-!{A P/N 25Ellql-il. S/ri 810rt66. p m E{si ,odp i.'i, qc.d. e@_MX lhe 0i,ciafi oidld Mp$elid6ti(d oba'e ros,epoi.d and iiTdkd in o@done vilh udfll Fflr oid ir hppbrrd ls lo +r;o. 'elu,ied ,,ZeeL*d n .,0,,i @ bi4 iln htt L! tlA6 Lb-&&ry UTAH JET CENTER 08-16-00 Shop Order: 2294 N# N83SG rype lc 1124A TotalTime 7343 ractrtt-tobbs Landinss 5374 Removed # 2 C-14 gyro P/N 2587193-43 S/N 78038406. Installed # 2 gyro P/N 2s87193-143 S/N 78038406. Operational check salisfactory on ground. The Aircraft and/or component identified above was repaired and inspected in accordance with Federal Air Regulations and was found airworthy for return to seryace. - Signed Logbook EntrY WW1124A 7352.2 5381 cycles uycres .Removedthecopi|ot'souterwindshie|dP/NPPG343o3o.2,S/N99158ll0464andinsta||edanewouterwindshie|dP/N ppc 343030-2, Sltt Sgoo+t-totos. see PPG's certiflcate of conlormance and Final Electrical Data sheet . Complied wrth mtnor fuel leak repalls in the fuselage center sect'on . Replaced the right position lamp P/N 628 Items lisied were inspected/repaired in accordance with aircraft, engine and/or accessory M:""f"ttut"t,yil1t:i:l:".y":::,1 servrce wltn respecl Io Ine worK requiremenis and cuirent Federal Aviation Regulations. Thls aircrait is approved for return to performed. Details are on file under W O.# 613 RoigWest IncorPorated 7035 Sophia Avenue. Van Nuys, CA 9140b FAA CRS UORRg5B- AIRCRAFT MAINTENANCE RECORD A/c Res'n: N83SG A/c Moder: 1 124A Westwind ,'/C Ser. No.: 368 UTAH JET CENTER Date: 9.8.2000 Shop Order: 2231 N# N83SG rype l,rc 1124A Toratrime 7360 rach/Nobbs Landinss 5384 Removed loanerC-14 cyro P/N 2587193-143 S/N 78039406. Instalted unit p/N 2587193-143 S/N 81085647. Repaired by IFR Avionics ref. To S/O 361631. The Aircraft and/or component identified above was repaired and inspected in accordance with current Federal Air Regulations and was found airworthy for return to service. Signed UTAH JET CENTER Date: 09-29-00 Shop Order: 2307 N83SG rvpe l'lc 1124A roratrime 7390 rach/Nobbs Landinss 5406 Removed ADI P/N 622-4808-004 S/N 823. Installed newly O.H. ADI P/N 622-4808-004 S/N 179. OPS CK satisfactorv on GRND. The Aircraft and/or component identified above was repaired and inspected in accordance current Federal Air Reoulations and was found airworthv for return to se.vice. Signed /,18q N g 4t una( /A/ NAJ|,t6ltl 4/t J6t ',rt r.1ioi: cdlit! hol ,1 1'd.To.dr nodd;lm ql S/fi: q606 hoe &cr Lllel lo: !I{l it. ind rude th-, ,e,lli,mflb 0i ftf, 91.llJ o.d rfl AFP t. , cstiil lhol fi lfonrponde/ nodd.: Im $ S/N.: 1E112 hos bdff l€ied lo.r saLtl] il- oid deis lhe 'ELri'oqrlj or fip -ar.!lJ a'rd fAF Pp t thE dtrdfl dnd/of co'pon&l ideniiel .b.ve roi inrarl.d ii riih fg@-fu{ 'ocnd nid oN.doid otral faF3 did , dpoflcd lo, rEldnt lo ene n*j)zu,l/ln*! u,lfr)-lz:,o i B "ta,a 4w (4/- td, NLtt i.b l/ /tti (B-4lqfu at Fq.. tLrY tt l/o,. /11 rlal J6./; ,:/t tid{ | Q'q ,4./C t;/tt iB gl.r11 aalidr I diiry ihol l,e ollimel', oll. eicodiiq €quiFisl tid prbl/el0lit etslsi li{ls r.q!,ii.d bl frR hove &d FarBmd. lhe ,rllin€tc u5l6ied loi 5ml tL the ii,ooll0iil/0. r.dpoirr id€ilir'ed 0bor iep. .nd iilpeciei ii rctdddn.! }ilh -!fu@_& '{! 'ed oftal FAR s dii it opproved Id .elunei lo 9a::re a, / /t I /zooc.,t *P aintt fu!* Ml grt'8tu lE . -' ,7Ar|.r4ttrj.-, .'-.tdt*ar'}ait<,.*,-::. Ab'nh,. ; AIRCRAFT MAINTENANCE RECORD A,/c Res'n: N83SG A/c Moder: 1 124A Westwind AJC Ser. No.: 368 5\Fl it il 'NS E Eir ] l a B, t s q s F""--l i: b :n iE + s -! E E E H* t+ Es F ES E \ a\ js ls. 6 { S r{ *i E! _8 :ii I .q "8. e s a E -a _& .r '! g Et5i { t -&iI J as s. E FS € 1.t'Fq.. 4!Jg ,t/? 5/r: J63 r.{i.n: Rsnovd AEt-&1. F/ 522-r'q01-0r6, 5/i 21q6. lBLiled adlonqe aPC-&l PA 5?2-?901-016. 5/N ?054. tloolol le!l! e:bi 'ono oo.r'. lh! ltdon didld .onpo@i iddllirl.d obot! u0: ond iigecled in ocrydonry elh !t@_fua- '.rdi'd d"dt tAP: oid ir ooo,oed td ,e1u'n ta ,€'yice. m//1e/ /r'u 4'tut tr. 7t! Sa b aP. h, tllt CtJ !t4A avi 4M* AIRCRAFT MAINTENANCE RECORD Alc Res'n: NB3SG A,/c Model: 1 124A Westwind A/C Ser. No.: 368 DAIE At.n.ar ,q!!od I catlt$! .opn t't .he:t rPN 84{20210014 r. 50000 ftcl !@_@. TL. eratei/o. co4oeit dani.d aboce de f,!&ed dt nrp.ct d s r.rdocc wii cucrd FAR3 &d s aplroftr !d r.h$lortru. *,U213L '*.r2^.;r,/*&'/ IFR Aatd.. R.Ft C.!!.. -r j9in !r\ Sopb" Av. V{ llutr, c1400 cii AQ"lPil ?tt ols // ru/fm C2RR{C(/O/Y C/,?0 /fR AA2/Y/Cfi//!C TTCH. 7035 SOPHIA AVI. I\Dc-(cu K INSP. VN NUYS, t-tl-(oi CA 91406 ttt DAT[: W.02_616 . - Vz- uf ^t'r-d0A", (s18).782.4810 -{r taXo P/N Lzz,t-rs oo< AQ4RO59M. S/N ttsr STD. AIT CORRTCTION TOI. FARO. SCAI F FRROR IN. HG. TOL. FT. {RROR -1000 il. - too2 +/_ ZOn 28.10 -1102/-17s2 -00 0 Fr. + zo +/- 1AFT 28.s0 -t3ts/-lJ6s lg 500 Fr. €u +/- 20FT 2e.oo -8J8/-888 :ezp 1000 FI. I oue +/- 20FT 2e.so -J67/-417 -37p 1500n. t.eLc' +/-25FT 2s.92 0 0 pi'. - o Lo 2000 .anzo +/_ Jgff 30.06 + r04/+ 154 + t* 0 1000 f-1. +/- JO[f Jo.so +506/+556 +- 5 4- 4000 n. +o2-O +/- J5Ff J0.90 +868/+918 + 7tQ 6000 Fr. bo tO +/- qOn J0.ee +s4el+see tlEo 8000 n. flozo +/- 60Fr 10000 FI. l0o*G +/- aOn 12000 Fl. tL ozg +/- 90Fr CASI LTAK O ISOOO FT. &.J1. ur 14000 n. t atl O +/_ tOOff (I01. 100 rTlMtN) 16000 FI. r 6 o*o +'/- nOn 18000F1. lgoLto +/-non 20000 Fr. uP zao40 +/- lJon D}WN 2oo 1-O 22000 FI. 22oL.v +/_ tnn HYSTIRISIS TOL. 75N-. 5rr 25000 FI. gp 2€o4s+/_ l55FI D0\{N3i"4a' i0000 fr. 3aa3e +/- 180ff 35000 fr. 16r^ 2a +/- 205rT 40000 tT. tto t o o +./- 2J0n AFIIR iFFtCT -A_JT 45000 n. +€o.q? +/- zssn (r01. icFT) 50000 FI. so / oo +/_ 280F1 N 83SG A/ m/fE? C2/fi?fcf/0/y CA,?O /n AA2/y/Cfi/lyC TECI. v{,Tanl- 7035 SOPHIA AVt. VN NUYS, CA 91406 DATE: /-(' ,'W.g.s7dyd tlT (q1.8^)rzq?.4810 P /P B zozt oo i tf AQ4R059M. Co?rtor K d-Et/4 N 5/N .tol STD. AII CORRFCTION TOI. R{RO. SCAI F FRROR IN. HG. TOL. FT. {RROR -1000il. lolO +/- 20rT 28.10 -1102/-1752 , 1710 OFr. a _ +/- 20rT 28.50 -lll5/-1365 -/33 0 500 Fr. € os +/- 20FT 2e.00 -8t8/-888 -ilo 1000 p;. 0o O | +/- 20rT 29.50 -367 /-417 t q? lsoo Fr'. o +/- 25n 29.92 0 =ryo 2000 IFT. lv F r-' +/- 3oFT J0.06 + r04/+ 154 + /30 J000 n. 2_790 +/- son 30.50 +506/+s56 +sto 4000Ff.3170 +/- 35Fl' 10.90 +868/+91 8 frza 6000 ri. 6po O +/- nn J0.99 +949/+999 fr20 sooo tl..K O7g +/- 60Ft' 10000 Ft. 877? +/- aon gon 12000 fi. 1763,:- +/- cASt LIAK o lgooo Ft. WJr. l4ooo tT. t377r +/- roon (I01. 100 rTlMN) r6000 n. Lggjn +/- r roFl' r8o0o n. r179 _ +/- non 20000 il. uP ffi€o +/- lJoFr }ownt_fi?0 22000 F1. 21 4'+r-' +/- UOn HYSTIRTSIS TOL. 75rT. 25000 il. ue 7+7@ -6o-JI +/-' rsSn Dgi1lN 39? i0000 f t.. Lqq +:o +/- taon J5000 il. \( o@ +/_ zosn 40000 n. Lto 17 n +/- ZSOI ANIR TFFTCI -re_N 45000 FI. V RorgW€st 7493.6 #1 Engine 7146.5 7445.0 Lanorngs 5466 5109 Cycles . Complied with a 200 hour 'A" lnspection including Engines, Naceiles and Pylons inspection, 150 flight hours airframe inspection, and pre-flight inspection in accordance with the Weshvind 112411124A l\,4aintenance lvlanual chapter 5 requirements. ' Complied with weight and visual check of the cabin and cockpit fire extinguishers. . Complied with SB 1124-30{36"A" lnspection of the windshield heat cycling contactors. . Complied with SB '1124-55-020 and AD 89-12-08 Inspectjon of the horizontal stabilizer aft spar splice fitting outboard lugs for cracks. . Complied with AD 2000-23-13 and SB 't 124-27 A-147 To ptevent jamming or disconnection of the horizontal stabilizer trim actuator. . Comptied with AD 74-08-09 R2 To prevent possible fires that could result from smoking materials being dropped into lavatory paper or linen waste recepracres. . Removed main batteries P/N 30126-001 #1 S/N 9506152, # 2 S/N 881 2674 and reinstalled after deep cycle. See Oynamo Aviation, Inc.'s FAA Form 8130- 3s dated 01/17101 . Removed emergency gyro power supply P/N PS-823 B/T S/N 1310 and reinstalled afler deep cycle. See Dynamo Aviation, Inc.'s FAA Form 8130-3 dated 01117101. . Removed emergency lighting battery P/N 38451-004 and installed after deep cycle. See Dynamo Aviation, Inc.'s FM Form8130-3dated01/17101. . Removed the left engine starter generator P/N 23065-0i 8l , S/N 2258 and installed an overhauled unit P/N 23065-018-1 , S/N 3684. See Weco Aerospace Svstems. Inc.'s FAA Form 8130-3 dated 1221lOO. ' Removed left and right main wheel assemblies P/N 5002806-2, #'l S/N Jun89-537, #2 Ma€4-662 and reinstalled after N.D.L and tire changes. Tires P/N of on 249K83-3, #1 S/N off 72070859, S/N on 02090307, #2 S/N off 60470266, S/N on02110543. See Aero WheelAnd Brake Service Corp.'s FAA Form 8130-3's dated 01/16/01 . Rernoved the eft and right brakes and installed overhauled units P/N off/on 5002805-3, #1 S/N off R12153-6, S/N on 21139-t, #2 S/N oft 1140, S/N on JAN86-531. See Aero Wheeland Brake Service Corp.'s FAA Form 8130-3's dated 10/19/00. . Repaired various fuei leaks in the center section and wings carry through area. ' Re-glued laminate piece on the right cabin table. . Rigged the aileron servo tab per 27-1 0-00 pg. 505 of the 1 '12411 124A Maintenance Manual. ' lnstalled 2 ea. Coat hangers on the aft side ofthe pilots false bulkhead. ' Adjusted and secured the left aft cabin window reveal and adjacent headliner ,^. Stripped and re'painted landing lrght lenses antt glare coattng. nstalled a new snap for the toilet seaucover skap. Reparred sealant at the right wing tip tank to wing bottom side. . Replaced the radar waveguide desiccant. . Replaced the left and right cockpit windshields desiccant. . Reclocked the coprlots wiper blade arm for proper parked position- . Replaced left and right hydraulic pump gaskets P/N MS9135-01. . Repaired the tail cone bondlng strap. . Secured the leff wing tip aft cone lower diverter strip- . Removed left main giar axle internalcorrosion in accordance wilh 112411124A mainlenance manualch.32. Measured axle dimensions and found within maintenance manuallimits. Treated axle per maintenance manual. . Removed and replaced the copilots wiper blade with a new refill P/N 2315M-24-8. , Removed and replaced all 4 engine fire bottle cartridges P/N 1V113083-5. Manutacture date of cartridges is 9/2000. Items listed were nspected/repaired in accordance with aircraft, engine and/or accessory Manufactures lvlaintenance Manual requirements and current Federal Aviation Regulations. I certily that this alrcraft was inspected in accordance with an inspection program as required by FAR 91 .409 (0(3). This aircraft is approved for return to service with respect to the work performed. Details are on file under W O # 745. Roigwest Incorporate Roigwest Inclrporat€d 7035 Sophia Awnue Van Nuys, Calitomia 91406 818 908 9600 FAX 81a 908'0453 ,ru, Logbook Entry I\t aaq a: DAIE: o2l16to1 Rorgwest 7550.8 7203.7 7502.2 Landings 5515 uycres 5158 5386 Complied with a 1200 hour clean/inspection/lubrication of the left and right flap flexible drive cables in accordance with LA.l. West"\ind 1124h1244 Maintenance Manual Chaoter 5 requirements 5-20-03 and 27-50-00 servicinq. Removed the cooilot's oush to talk switch and installed a new switch P/N STD969-1. Items listed were inspected/repajred in accordance lvith aircraft, engine and/or accessory Manufactures Maintenance Manual requirements and current FederalAviation Regulations. This aircratt is approved for return to service with respect to the work perfo.med. Details are on llle under W.O.# 770. Roigwest lncorporated 7035 Sophia Avenue, Van Nuys, CA 91406 FAA CRS UQRR958- r.t nar ri1f tlf (t/t lzl 1,,r udli . t.l.t: ,4,C ))'|tt -W lrliolr Fer.drd AFC al P,At 52-?q0r llt, S/tl ?156. hsldllsj Acioiqe rFt 0, Fn :.'?-?9111-!16. 3/rl ]?!] A]tailol .ydd i8b qcod. 'onp e4@-@t lL. oi,dofl oidlo. co,.p(rF1i iddlifei lbo€ t03 ,eFoilad lid hspe.ld in 0&rdonce tlh ,*-+!d3*r I RorgWest N83SG .WWl.t.24 SlN:.:368 DATE:06126/01 Airfiame 7686.5 #1, Ehgine 7339.4 *|2:Ehgine 7637.9 Lantlinsb 5594 CyCles 5236 Cydes 5465 Turbine Aircraft Maintenance in Complied with a "8", 2OO!4OO hours inspection including Engines, Nacelles, and Pylons Inspection and 150 flight hours inspection accordance with the Westwind 112411124A Maintenance Manual requirements. Complied with recurring AD 89-12-08 To detect cracks in the hinge lugs of the horizontal stabilizer aft spar splice fitting. Next due - 7986.5. Complied with recurring AD 96-24-t'l To prevent excessive wear of the aileron push-pull tubes. Next due - 8286.5. Complied with recuning SB 1 124-30-036 part Il Inspection of the windshield heat cycling contactors. Next due - 7836.5 Repaired structural damage to nose radar antenna support web and avionics deck. Ref: FAA Form 337 dated 612610'l' Treated and painted repaired areas. Removed upper rudder trim actuator P/N 793500-503, S/N 5220, and replaced with an overhauled unit P/N 793500-503M, SiN 5202M' Ref: Aero Space Controls FAA Form 8130-3 dated 11l10lOO. nemoftd fuselage lower left fuel cell P/N 2F1-6-32432-511, S/N 79-34873, and reinstalled after overhaul. Ref: Aero-Tech Services, Inc. FAA Form 8130-3 dated 6/20/01. Replaced left fuel low level float switch P/N GF5500-52, S/N unknown, with new P/N GF5500-52, S/N A2269. Removed # 1 and #2mainwheels P/N 5OO28OG2, S/N's Jun89-537/Jun89537 and Ma€4-66ZMa€4-662 and reinstalled after NDT inspection and tire change (2 each new tires P/N 249K83-3, S/N's 03&10631 and 10100522,were mounted on the wheels, respectively). Ref: Aero Wheel and Brake Service Gorp. FAA Form 8130-3 dated 6/8/01 . Removed main bafteries P/N 3012G001, S/N's 9506152and 8812674, and reinstalled after deep cycle and function test. Replaced cell # 15 P/N 4OSP1O0 with new cell, S/N on 8812674. Ref: Dynamo Aviation, Inc FM Form 8130-3 dated 6/20/01. Removed emergency power supply P/N 501-1075-06, S/N 1310, and reinstalled after replacing pack #A and deep cycle. Ref: Dynamo Aviation. Inc FAA Form 8130-3 dated 6/25/01. Removed emergency light battery P/N 38451-004 and reinsialled after deep cycle. Ref: Dynamo Aviation, Inc FAA Form 8130-3 dated 6t25t01. Removed nose wheels P/N 9541874, S/N's Oct97-9271oct97-927 and Oct97-942/Oct97-942, and reinstalled after NDT inspection and tire change (2 each new nose tires P/N 1UF43-2, S/N's 02990098 and 10701248, were mounted, respectively on the wheels). Ref: Aero Wheel and Brake Service Corp. FAA Form 8130-3 dated 6/8/01. Removed # 2 engine hydraulic pump P/N 65WEO1O31-3, S/N 81-58, and reinstalled after overhaul. Ref: Aero-Craft Hydraulics, Inc. FAA Form 81 30-3 dated 5/29/01 . Removed # 1 engine hydraulic pump P/N 713524-507, S/N A2-84 and replaced with overhauled hydraulic pump P/N 713524-507, S/N A3- 263. Ref: Jet Service Enterprises FAA Form 8130-3 dated 4118101. Replaced both high pressure hydraulic filters P/N 7509121 and the hydraulic reservoir filter as a precaution following pump failure. ieplaced radome P/N 5873000, S/N unknown, with repaired radome P/N 5873000, S/N AUG-0017. Ref: Nordam - Texas FAA Form 8130-3 datbd 5/15/2000. Replaced radome boot P/N PM-260 with new radome boot P/N PM-260. Painted radome stripes to match fuselage paint scheme. Removed compass/gyro P/N 258719343, S/N 81095980, and reinstalled after repair. Ref: Duncan Aviation / Lincoln FM Form 8130-3 dated 5/23101. Removed vertical reference gyro P/N 792-6694-00l , S/N 1 1206, and reinstalled after repair. Ref: Duncan Aviation / Lincoln FAA Form 8'l 30- 3 dated 5121101. Removed compass/gyro P/N 2587193-143, S/N 78038406, and reinstalled after inspection and function test. Ref: Duncan Aviation / Lincoln FAA Form 8130-3 dated 5121101. RemovedradarantennaassemblyPtN622-2504-001,S/N2TO,andreplacedwithoverhauledantennaPlN622-2504-001,S/N718. Ref: Duncan Aviation / Lincoln FAA Form 8130-3 dated 5125101 . Removed glide slope antenna P/N DMN25-1, S/N 1896, and replaced with new antenna P/N DMN25-1 , S/N 3625. Cleaned MMO warning bell system connectors with contact cleaner. Adjusted main door and seal to eliminate squealing under pressure. neplaced 1 each lamp P/N AL-1235-360 and 2 each connectors P/N AL-51 13 in lavatory vanity with 1 each new P/N AL-1235-360 Lamp and 2 each P/N AL-51 1 3 Connectors. Adjusted left hand # 4 and # 5 window trim. Removed 1 each downwash lamp P/N AL1235-320, 1 each downwash lamp P/N AL1235420, and 2 each connectors P/N AL-5113 above left hand # 4 and# 5 windows with 1 each new lamp P/N AL1235-320, 1 each new lamp P/N AL1235-420, and 2 each new connectors P/N AL-51 13. Removed 1 each upwash lamp P/N AL1235-320, 1 each upwash lamp P/N AL1235.4.20, and 2 each @nnectors P/N AL-51 13 at left hand forward position wiih 1 each new lamp P/N AL1235-320, 1 each new lamp P/N AL1235.420, and 2 each new connectors P/N AL-5113' Replaced 1 each lamp P/N GE4553 in left hand landing light with 'l each new lamp P/N GE4553. Cleaned and serviced toilet. Purged moisture from co-pilot's windshield in accordance with Westwind 112411124A Maintenanc€ Manual ch. 56 Removed right elevator and reinstalled after tightening and safetying right hand universal joint attachment hardware. Replaced th-e following hardware on the left aileron trim trab with new: 1 each rod end bearing P/N BHM-4T, 1 each bolt P/N AN174C12' and 1 each washer P/N NAS1149D0416H. Removed left wing tank sump drain valve P/N 79C19 with new P/N 79C19 valve. Roigwest Incorporated 7O35 Sophia Awnue Van Ntrys, Califomia 91406 81 I 908-9600 FAX 818 908-0453 Repaired minor pinholes on left and right wing de-icing boots in accordance with l.A.l. Westwind 112411125A Maintenance Manual Chapter 30-10-00 Page 205. Cleaned left and right aileron roller control rod guide rollers. Removed # 1 engine exhaust pipe P/N FlOA-5-B20203-33 and replaced with repaired unit P/N F104-5-820203-33. See Dynamo Aviation, lnc FAA Form 81 30-3 dated 6/19/01 . Replaced 12 each bolts P/N NAS6603-8 with new. Secured loose clamp on # 1 engine thrust reverser inboard actuator. Repositioned right main landing gear axle drain scupper to bottom of axle and resealed. Resealed left main landing gear axle drain scupper. Repaired sealant at bottom forward edge of right # 1 and # 6 cabin windows. Replaced 1 each stud P/N GS522WO1 HS with new P/N GS522WO1HS on # 1 engine inner igniter access panel. Replaced nose landing gear forward door linkage lever arm P/N 6PA31 with new linkage lever arm P/N 6PA31. Replaced the following nose steering yoke assembly parts with new parts: 1 each upper steering bracket P/N A01-223- 60200-000, 1 each lower steering brackefP/N AO1 223 60300.000, 3 each bolts P/N NAS464P4-39, 1 each bracket P/N 2236.0000.002, 1 each bearing P/N ED1339&2 and 1 each bearing P/N ED12999-3. Replaced nose gear forward door linkage lever arm P/N 6PA31 with new P/N 6PA31 linkage lever arm. Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufacturer's Maintenance Manual requirements and current Federal Aviaiion Reguiations. I certify that this aircraft was inspected in accordance with an inspection program as required by FAR 91.409 (fX3). This aircraft is approved for retum to service with respect to the work performed. Details are on file under W.O.#s 821, 832,835. RoigWest Incorporated 7035 Sophia Avenue Van Nuys, CA 91406 FAA CRS UQRR958L I ]*. AIRCRAFT MAINTENANCE RECORD A/C Res'n: N83SG A/cModet: 1124AWestwind A/G Ser. No.: 368 DATE A/C T.T. A/G T.Ldgs. DESCRIPTION m, DA,TE:,rril l l0 6/O.1 RorgWest Complied with AD 2001-03-01 To prevent the main entry door from jamming, which could impede the safe evacuation of passengers and crew during an emergency. Placed a copy of this AD in the appropriate section of the Aircraft Flight Manual. 'AD 2OO1-15-17 Rockwell Cottins, lnc. To prevent erroneous altitude interpretations N/A due to parts installed in aircraft. Complied with recurring AD 98-06-10 To prevent Failure of the hydraulic fuse to operate properly. ComptieO with ASB 1114-54A-138 Nacelles / Pylons - Engine Inlet Cowl and Aft Nacelle - Verification of Approved lnstalled Attachment Bolts. Removed and Replaced bolts in accordance with ASB 1124-54A-138. Bolts installed - NAS6603-4, -5' -5H' -6 & -9. Removed Pilot's and copilot's windshield wiper blades and installed new rubber wiper refills P/N 2315M-24-8. Cleaned paint from the radome mounting flange and checked bonding in accordance with Westwind Maintenance Manual 23- 60-00. Removed and replaced the cabin entry door seal P/N 5333045-181 and retainer screws P/N AN530-4R4 with new. Removed the standby horizon gyro powersupply P/N 501-1075-06, S/N 1310 and reinstalled and ops/function checked after deep cycle. See Dynamo Aviation, Inc.'s FAA Form 8130-3 dated 10125101 ' Remov-eO and replaced the right tip tank fuel float switch P/N GF-5500-52 and gasket PIN 213702-23 for fuel in tip indication light. Removed the right thrust reverser hydraulic return tube P/N 723589-53 and installed a new tube assy P/N 723589-53. Removed and replaced 1ea. Pressure refueling vent hose assembly P/N 653092-127 (MlL-H600-1-1-2) and 2ea. clamps P/N AN737TW46 with new. Removed and replaced the copilot's davtron clock battery P/N 81 1BATT1 with new. RemovedbothmainbatteriesP/N30126-001,S/N8812674andS/N9506l52andreinstalledafterdeepcycle. SeeDynamo Aviation, lnc.'s FAA Form 8130-3's dated 1Q129101. Note: S/N 8812674 had cell No.'s 6 & 14 replaced with new cells P/N 40SP100 as noted in the FM Form 8130-3. Removed the emergency light battery P/N 38451-004, NSN and reinstalled after deep cycle. See Dynamo Aviation, Inc''s FAA Form 8130-3 daled 10124101. Removed the refrigeration bypass valve sleeves, 2ea. P/N 733108-503 and 1ea. clamp P/N U84-2105H and replaced with new sleeves P/N 783108-503 and clamp P/N U84-2105H. (G831-4-5), and installed a new hydraulic fuse P/N Removed the aux hydraulic indication hydraulic fuse P/N 713047 S/N 3383 flc't11 AIRCRAFT MAINTENANCE RECORD AJc Reg'n: N83SG A./c Moder: 1 124A Westwind AJc ser. No.: 368 ,m, Logbook EntrY "--7r:b+iicasr_a_5),Rorqwest s/N 1080A. See Jet Service Enrefprises, Inc.,s FAA Form 8130-3 dated 5/10/01 . overhaul' See HRD Aero . Removed the cockpit portable fire extingulsher P/N898d52, S/N v-329659 and reinstalled aftef . RIil?TJ;''1,";iffffi.T#3?;3iXii'iJiJiJltJ^8e8052,s/NV-32esl6andreinstaredafteroverhaur seeHRDAero Systems, Inc.'s FM Form 8130-3 dated 10/31/01. S/N's . R;;"; gea. tife pfeservers and reinstalled after Pefiodic Inspection / Recertification life preservers P/N P0723-105, Parts, Inc.',s FAA Form B'130- ra+oao, eegsa, rg+ot t, rg+t oo, +g+ 347 , F34026, 41834, rUOtS, eZqOza. see corporate Air 3's dated 10/2310'1. . Comolied with inspection of the first Aid Kit. Complied with a visual inspection of the cabin and cockpit portable fire exlinguishers ' retarder feedback cable . Complied with 36 month inspection / clean / lubrication of the left and right thrust reverser throttle assemblies. . Compiied with '150 Hr. Inspection / lLlbrication of the left and righl starter/generators' (rebrush). Aerospace . Removed the left starter / generator P/N 23065-018-1 , S/N 3684 and reinsialLed after repair See Weco Systems, lnc.'s FAA Form 8'130-3 daled 10125101. . R;moved the right starter / generator P/N 23065-018-'1 , S/N 2562 and reinstalled after repair (rebrush). See Weco Aerospace Systems, Inc.'s FM Form 8130-3 dated 10/25l01 . R'u.ou"d ttr" t"ft engine fire extinguisher P/N 32700004, S/N 02447C1 and reinstalled aftef overhaul. See S J Obrien Ent Inc.'s Yellow Tag / Maintenance Release Form dated '10/25101 and . Complied with a-preflight inspec|on in accordance with Westwind M.lV. ch. 5 fequirements. Servlced Ures' oxygen emergency gear nitrogen bottle. . nemiveOini n.n. navigation lamp P/N W1290 28 and installed a new lamp P/N W1290-28. Manu2l Items Listed were inspe6ted/rapaired in accordance with aircraft, engine and/or accessory N,4anufactures l\'4aintenance work re!uirements and current Federal Aviation Regulations. Tiris aircraft is approved for return lo service with respect to the performed. Deta. s are 01 I'le Jnder W O f 905 RoigWest IncorPorated 7035 Sophia Avenue, Van Nuys, cA 91406 FAA CRS UORR95BL yXo 1--{'L- .tt AIRCRAFT MAINTENANCE RECORD A/C Res'n: N83SG A/c Modet: 11244 Westwind A/C Ser. No.: 368 ru, N83SG ![/W1124A S/N:368 DATE: 01122102 7733.1 RorgWest Airframe 7790.9 #1 Engine 7441.8 #2 Engihe Landings 5650 CVcles 5322 Clcles 5551 Complied with a pre purchase inspection as outlined by the owner/oDerator. Complied with an operational check of the cabin pressurization bleed switching valves in accordance with the A.M.M. 21-1 1-00 pg. 501. No discrepancies were noted at this time. . b-omplied with a brake wear check in accordance with A.M.M. 32-43-01 page 601. Left = .325", Right = .350" (Limit = 410). . Compf ied with a 600 Hour crew oxygen masks in^pection in accordance with the A.M.M. 35-00-00 para. 2.a. and 2.b. . Adjusted the rear baggage door micro switch / latch assembly in accordance with A.M.M. 52-70-00. . Removed the auxiliarSi hldraulic system thermal relief valve P/N 71301 1-501 , S/N lL-32l1 0-79 and installed an overhauled valvep/Np/N71301i-5b1,S/Nli-171A. SeeJetServiceEnterprises, lnc.'sFAAForm8130-3dated3/01/01. . Secured pilot's and copilot's map light rheostaVknob assemblies. . Removed the cockpit instrumeni flu-orescent flood lights inverter P/N 18-95D, S/N and installed a repaired inverter P/N 1B- and 2ea. 95D, S/N 403g. See B/E Aerospace's FAA Form 8ie0-3 aated 12lO5lO1 . Also removed 1ea. lamp P/N 6845-2705 lamps P/N 6845-2355 and replaced with new lamps of the same P/Ns' . Secured cabin telephone mounting hardware. . Adjusted the left cabin #2 seat tracking' . Removed and replaced the radar waveguide desiccant MIL-D-3716. Industries . Removed the single point refueling dooi pln 31tr729-3 and installed a new door P/N 313729-3. See lsrael Aircraft LTD's CAAI Form 8130-3 dated 11128/00. Installed a new, previously missing single point refueling port cap P/N MS29526-2. tank assembly Removed the lavatory hof water c6ntainer p/N ELM 40/18 and installed a serviceable function clrecked water p/N ELM 40/2g. see Dynamo Aviation, Inc.'s certificate of conformance dated 01122102. serviced emergency gear nitrogen storage cylinder in accordance with A.M.M. 12-10-04. Servicecl oxygen system in accordance with A'M.M. 12-10-05' this aircraft. AD 2000-lO-04 To prevent cracking of the aileron skin due to missing rivets is N/A due to the S/N of Maintenance Items listed were inspected/repaired in accordance with aircraft, engine and/or accessory Manufactures service with respect Manual requirements and current Federal Aviation Regulations. This aircraft is to the work performed. Details are on file under W.O.# 959 & 961' RoigWest lncorporated 7035 Sopiria Avenue, Van Nuys, CA 91406 FAA CRS UQRR958L AIRCRAFT MAINTENANCE RECORD A/C Res'n: N83SG A/c Modet: 1124A Westwind A/C Ser. No.: 368 DATE A/C T.T. A/C T.Ldgs. DESCRIPTION 2.2Loz 7fo6,a 57s b Utu ltsaa/ fuazc+"/ ar'. nJ az;ql /r/t Z K /a/l y'4/;,',t ,Dre ,(.f/iau,/a's ,. Uit ?rz,L,( K /.rru*n*r /;a//s f1flez,'n=. t-tu/ lt,rrro,*#n p/, 3 K v r f o o y /'qrf Pt-p dpry'n,/ ,c),,/J c/nrpr/ra //a',/t/ ,9*#rr'o, {efl - ?eS * u ?s Pat ru ilrv1 ^ fr. %,/,Sr,bn 6 5*rr/^, 6rro- f*/pr, .P/u 5o t- /ozf-oa 7,u/3to ..Aznnv k*1 .tu*/r iltr$/0-4t rop.d"t/, /r. rA rcs *aArEa/Ky $, n-p c/4H OtrprptJ , ,ffi-a.s/rfuJ g*l/r,, pstz.S/t, 4^ Llp//'u>arcf ut e unir ,4,1 f / il ./n nrt p .6t,a, tnzo 2v- laau/la. Fa-no--(- / 9,t d )'r s ztr:./' /,r/o I Kr-t tt*o /1..n f 0rt//ol*, t*o/, 2/Mruarra r'r6a?- Airframe Westwind S/N368 N 83 SG Total Time: 7854.4 Cycles 5677 Aprll 12,2002 Remove both main wheels and tires, send to Hatfield Aviation, Inc. Hatfield removed old tires, NDT inspected wheels and bolts' Installed new tires on wheels. Left wheel P^I5002806-2, S/N Mar94-662,Tire P/I'{ 249K83-3 SAI 12240137. Right wheel PA'{ 5002806-2 SN Junegg-537. Tire p/I.i 24gK83-3 SN 12240156. Installed wheels, Pack wheel bearing and safety. Check pressure and leak check, OK. a Comply with 150 Hr. Airframe Insp. Comply with 150-300 Hr. Engine inspection on both engines. Including Soap samples taken, with oil change. Run engines and leak check, OK. .d 1', SERVICEABLE PART ,v =- .uJ 3t r '/5 .*'a F F t{rt,'g*', "f\' fra $n 6|"/o't9"oL e eEF F t H \ E eE 6; ! * *EEgE:F I[EJF_C!ATT-{!D,/ OR COMPOIENT IDENTFIED ABOVE TVAA INSPECTED IN ACCORDAiEE WITH CUR- REt{r REclut^flo[8 0F rHE FEDERAL AvtATtON ADiflNtsrR floN AX- ta Fbi-iEiiiHi ib EE SERV|CE. ^ipnovED , oq PERTINENT DETAII.8 ARE Oil FIUilT THIS FEAIR STANON. .h UJ z O D unlted ltrtterler dg Accel8ones, mc" 8346 Almo4a GenPa Rd. Hourton, Teras 77075 Tel:(713)991-9111/9112 Fu:(713)991-9117 C.RS.# U9BR61EY NICKEL CADMIUM BATTERY PACK CHARGM)ISCHARGE TEST FORM (Form# 9010) Customer Neme Customer wrc*2--@6 ' Date Received Battery t3tO, GeneralC vin uter ci Replaced o J.+, a eo ,b, V 2nc 3rc ?f ii, { :l a x F t .t fE, JIJJ dl oUI E IIJ (t, I5 _!El oI =cllJt€n EO E in E t $ I3 * 3 o 9106# Ituor ASrSg6n'oN'SU'C'VVJ -" >Lll6-t6&€tltreJ . lll6-t66€t/ :euoqd gLO//ru,'uqsnoH pBou Eou€9Ep€u.w It€8 'cNt 's3tuossEccv otw sEltuSlt\tg o:uNn tsege{q$IH \A \-/ t\ ^ - t.f:4/ unlted ltrtterter dt Accesloneq mc" 8346 Atnedp Geno4 Rd. Hougton; Tores 77075 Tel: (713)991-9llll9l12 Far: (71 3)991-9117 C.RS.# U9BR61EY NICKEL CADMruM BATTERY PACK CHARCM)ISCEARGE TEST T'ORM (Form# 9010) Customer N Cugtomer P/O#l Date ReceiveO .?-'p5'-o2 B*Ifu P/:lij&5i<>*- Presenice Inspection/Hldden Damlqo Inspection 'i o 5'l/ ?' & Cell I marla Renlaced /' ?\ do{' 'o v (o, D,V' 2nt t2,c: l {.a,0 ,// @ral Avlatton ACgrtnistratlpn And b Aporoved For Retum to Service. , UN|TED STATES 2. FMFoRMol3og SYSTEM TRACKING REF. NO. AIRWORTHINESS APPROVAL TAG \1,'_Ll U.S. DEPARTMENT OF TRANSPORTATION 60168 FEDERAL AVNNON AOMINISTRATION ORGAMZATION 5. WORK ORDER. CONTRACT, OR INVOICE NUMBER: , HATFIELD AVIAT|ON, lNC. FAA ED2R79OK CLASS 1.2.3 /, 8109 BRANTFF STREET HOUSTON, rX77061-5201 An1 6Q p.e.q lTpnpAI'T TNVE'CT}vffiNTC .-EM 17. DESCRIPTION 8. PART NUMBER , ELIGIBILITY' 10. OUANTITY 1. SERIAL / BATCH 2 . STATUS /WORK NUMBER m 5002806-2 VARIOUS i JUNBg-537 N.D.T.& 3. REMARKS NEW TIRE INSPECTED AND MOUNTED NEW TIRE IAW G/Y CMM BY D. MCDONALD NO DISCONTINUITIES NOTED ON INSPECTION IAW ASTM E L444-944 .IMITED LIFE PARTS MUST BE ACCOMPANIED BY MAINTENANCE HISTORY INCLUDING TOTAL TIME / TOTAL CYCLES / TIME SINCE NEW. 4. NEWO NEWLYOVERHAULEDil 19. RETURN TO SERVICE IN ACCORDANCE WITH FAR 4iI.9 >ERTTFTES THAT THE NEW OR NEWLY OVERHAULED PART(S) TDENTIFTED ABOVE, EXCEPT AS OTHERWTSE CERTIFIES THAT THE WORK SPECIFTEO IN BLOCK 1 3 (OR ATTACHEO) }PECIFIED IN BLOCK 13 WAS ( WERE) MANUFACTURED IN ACCORDANCE WITH FAA APPROVEO OESIGN DATA ABOVE WAS CARRIED OUT IN ACCOBOANCE WITH FAA \ND AIRWORTHINESS. AIRWORTHINESS REGULATIONS ANO IN RESPECT TOTHE WORK VOIE N CASE OF PARTS TO 8E EXPORTED, THE SPECIAL REAU/aEMENTS OF THE IMPORTING COUNTRY HAVE PERFOIIIEOTHE PA'XS) IS (ARE) APPROVED FOR RETURN TO )EEN MET. sERVlcE. -Y' 5. SIGNATURE I6.FAA AUTHORIZATION NO.: 20. ATXHORIZEOFIQMTURE 21. CERTIFICATE NO.: d4--- ED2R79OK 7. NAME (ryPED OR PRINTED) I8. DATE /2UAAME{TY PED OR PRINTED) 23. DATE J.F. l,rtorrPKA 4/LL/02 FAA FORM 8130-3 (1 1-93) IOPTIONAL) INSTALLER MUST CROSS CHECK ELEGIBILITY WITH APPLICABLE TECHNICAL OATA. t+FF = . !!= FO =U @ EE $ M{EEL ISSY. 5002806-2 VARTOITS MLpOt,-Ah',) N.D.T. & t3. REMARKS N.D.T. INSPECTION AND MOUNT TIRE MOUNT TIRE NO DISCONTINUITIES NOTED ON INSPECTION IAT.I ABS CMM BY D. MCDONALD IMITEO LIFE PARTS MUST BE ACCOMPANIEO BY MAINTENANCE HISTORY INCLUDING TOTAL TIME / TOTAL CYCLES / TIME SINCE NEW. 14. NEWil NEWLYOVERHAULEDO 19. RETURN TO SERVICE IN ACCORDANCE WITH FAR 4{I.9 CERTIFIES THAT THE NEW OR NEWLY OVERHAULED PART(S) IOENTIFIED ABOVE, EXCEPT AS OTHERWISE CERTIFIES THAT THE WORK SPECIFIED IN BLOCK 13 (OR ATTACHED) SPECIFIED IN BLOCK 13 WAS ( WERE) MANUFACTURED IN ACCOROANCE WITH FAA APPBOVED OESIGN DATA ABOVE WAS CARRIED OUT IN ACCORDANCE WITH FAA AND AIRWORTHINESS. AIRWORTHINESS REGUI-ITIONS AND IN RESPECT TO THE WORK I{oTE IN CASE OF PARTS TO BE EXPORTED. THE SPECIAL REOUIREMENTS OF THE IMPORTING COUNTRY HAVE PERFORMTD{HqP't'(S) lS (ARE) APPROVEO FOR RETURN TO AEEN MEf. sERVrCt ,Y 2I. CERTIFICATE NO.: I5. SIGNATURE 1 6.FM AUTHORIZATION NO.: ,,^T,WX: ED2R79OK 17. NAME CTYPED OR PRINTED) 18. OATE 2uffi(frtroq PRINTED) 23. DATE / J.F. WOTIPKA 4/12/02 .(OPTIONAL) FAA FORM 8130-3 (11-93) INSTALLER MUST CROSS CHECK ELEGIBILITY WITH APPLICABLE TECHNICAL DATA. IT IS IMPORTANT TO UNDERSTAND THAT THE EXISTANCE OF THIS DOCUMENT ALONE DOES NOT AUTOMATICATIY CONSTITUTE AUTHORITY TO INSTALL IHE PART,COMPONENT/ASSEMBLY. THE USEMNSTALLEB WORK IN ACCORDANCE WITH TI{E NATIONAL REGULATIONS OF AN AIRWORTHINESS AUTHORITY. IS DIFFERENT THAN lHE AIRWORTHINESS AUIHORIW OP THE COUNTRY SPECIFIED IN BLOCK 1. IT IS ESSENTIAL THAT THE USER/INSTALLER ENSURES THAT HIS/IIER AIRWORTHINESS AUTHORIW ACCEPTS PARTS/COMPONENTS/ASSEMBLIES FROM THF AIRWORTHINESS AUTHORIW OF THE COUNTRY SPECIFIED IN BLOCK 1. STATEMENTS IN BLOCK 14 AND 19 DO NOT CONSTITUTE INSTALLATION CERTIFICATION. IN ALL CASES AIRCMFT MANTENANCE RECORDS MUST CONTAIN AN INSTALLATION CERTIFICATION ISSUED IN ACCORDANCE WITH THE NATIONAL REGULATIONS BY THE USEFYINSTALLER BEFORE THE AIRCRAFT MAY BE FLOWN. THE FM FORM 8I30.3 AND JM FORM ONE ARE EOUIVALENT. OTHER COUNTRIES SUCH AS CANADA ALSO HAVE EOUIVALENT ACCEPTAELE DOCUMENTS. INSTRUCTIONS ffifll e4r?rtb^*c. N0. 6016 8 4-/(- oz- 8109 Braniff Street 'JATE Houston, TX 77061-5201 (713) 644-1464 WORK ORDER ' rQ d I fl rc67 4 F 7 /,tr424rrt' P.O. OR R.O. NO. PHONE: rNsrRUcrloNS /VOf 1 l*/ffuz-> HEa Z PARTS (This page) PARTS FORWARDED PARTS SUB TOTAL PARTS TOTAL SALES TAX TOTAL /cqMPLETED 4--1 1- O Z-'-- F. A. A. APPROVED ED2R79OK CLASS 1,2, & 3 i.t REV. Sept 15,1996 HATFIELD A\NATION.'"INC. . Work Order Continuation Sheet (Tear down / Progressive Insp') .-.:_:,b.: _ .. -- P Customer. AF-f s' Arccrzn trzI z WorkorderNo. 6el6( ' z 't( ) ((.- AV PartNo. J-ae %F'pG- z- Date Serii i:.''f u*/ 3n- {t Removed from A/C 7r*f4' r{eN4 - 4a4aea K//M At7 . .? z rt .a 4 ;Rrp.it Explanation: f \ I-.-/ ^2,/6,F U--.< 1re4 fa+ + orz ,'.'. /t4 wl /;, y'l Test Rbraa1 ks;. . O > rf Cpl.{ 7rr/ / 7/t9{ */a/l r*tZZ&/ta/^/ /4V lff*r E 44 L/4 NDI . Tested m Repaiied lzx O+r+r*r+pC--El--- ^ | Mechanic Date ComPleted BILL,ING INFORMATION , .. tNvolcE No. _ , gifll DATE e4thtb*,,xc. N0. 6017 3 2_- gr7_ 8109 Braniff Street 4- / Houston, TX77061-5201 (713) 644-1464 WORK ORDER P.O. OR R.O. NO. NDf 7.t, ?// + .4a2, PAFTTNAME k//'kfu ,k S.N.llflR nu46> ,fAa Z-PO64Z- I PARTS (This page) PARTS FORWARDED PARTS SUB TOTAL PARTS TOTAL SALES TAX TOTAL "t-f Z - cbz-- PAGE OF F. A. A. APPROVED REPAIR Ehabrd^|1 rrt AeQ I t :'i 15,1996 ,^ | REV. Sept Work Order Continuation Sheet (Tear down / Progressive Insp') Work OrderNo. Customer K+) ArreerU+l7 ' 'tl-' (7-cl> PartNo.' ,=-{Oo'77O6-Z Date !erii;;. fi44 ?c/- 66> Removed from A/C Ttnte Receiving InsPection Findings: 7-/aA 44 t; 2/7-?Z> i&z*taw Explanation: /A/r/H 7ra4 -;nepair /L/ D7 -/.Fff74e/= ,'.f/z-a 7:ilnfi7lfu .,*" zEp / /+ c.t-/ ,&Sf 42t7, /.,l t) | .Tested E Repaiied Ul Ove**A#f Date ComPleted 4-/7-Pz- 3. Form Tracking Number: l. Approving National Aviation AuthoritiTttrintry: RELEASE CERTIFICATE AUTHORIZED G3JCFOO]- FAA/I.INITED STATES FAA Form 8130-3, AIRWORTHINESS APPROVAL TAG 5. Work Order/Contract/Invoice Organization Name and Address Number: G3,f CF Duncan Aviation/Lincoln Airport/Lincoln, NE 68524 I 1. Serial/Batch Number: AUTOP]LOT 5ZZ-ZJVL-UrO a a Repaired COMPUTER 13. Remarks: CUSTOMER:AIR AMERICA .JET CHARTER ]NC Discrepancy: Causes yoke jitter in roll. prel-iminary Findings: Bench checked unit and roll rate failures. Corrective Action: Troubleshot unit. Finished installing S.B. 7 to 'i rury!mnrr-,rrc v v e rn'l'l -rate when using the turn control. Subject.ed unit to heat and vibration. Cl-eaned and paint.ed unit. Functional tested unit per Col-lins ApC-BO O Autopilot Computer fnstruction Book(Repair Manual-) . TECHNICIAN:ER]C A. OLSON This document constitutes a signed copy of the work order. in Block 13 Certifies the items identified above were manufactured in conformity to: 19 El 14 CFR 43.9 Renrrn to Service ! Other regulation specified Approved design data and are in a condition for safe operation. Certifies that unless otherwise specified in Block 13, the work identified n in Block 12 and described in Block 13 was accomplished in accordance Non-approved design data specified in Block 13. with Title 14, Code of Federal Regulations, part 43 and in respect to X that work, the items are approved for return to service' 2 Approval/Cenificate No.. 15. Authorized Sisnahrre: I 6. ApprovalAuthorization No.: l. JGVR194F 23. Date (m/d/y.): 17. Name (Typed or Printed): 22. Name (Typed or Printed): AARON J. SPULAK 4/02/02 to install the part/comlrenent/asenbly' is important to understand that th€ existence of this docurnent alone dos not automaticatly constitute authority \.retheuser/installerperformsworkinaccordancewiththenationalregulatio1sofanairworthines::]|h:-"]g.9iT.Tl1..:T^.l"-l.j:l*}3:::::.}:"T?"? specilied'i1:Ti$:i;f.JaJiif#"f;"ii;;;;;6;i'n"""i.*Jr'r"?*auinoritvacceptsparts/components/assembliesfromthe in Block 1. Statementsinblocks14and19donotconstituteinstallationcertifcation.Ina||cases,aircraftmaintenancerecordsmu wiitr t6e nationat r.egulations by the user/instalter before the aircraft may be flown. ity with applicable l. Approving National Aviation 3. Form Tracking Number: Authority/Country: AUTHORIZED RELBASE CERTIFICATE G3.lCD0 01 FAA/LNITED STATES FAA Form 8130-3. AIRWORTHINESS APPROVAL TAG Organization Name and Address: 5. Work Order/Contract/Invoice Number: Duncan Aviation/Lincoln NE 68524 G3,JCD YAW DAMPER 622-316'7 -028 | n/a Repaired COMPUTER 13. Remarks: CUSTOMER:AIR AMER]CA JET CHARTER INC Discrepancyl Yaw Camper weak. Preliminary finding: Bench checked unit and duplicated discrepancy. Found defective accel-erometer. Corrective actions: Troubl-eshot and replaced defective accelerometer - Cleaned and painted unit. Functional- tested unit. per Collins 562C-8F Yaw Damper Computer Istruction Manual Note: Unit has no strapping module installed. TECHN]CIAN: STEVE .J. KRINGS This document constit.utes a signed copy of the work order in Block 13 Certifies the items identified above were manufactured in conformiry to: 19 E 14 CFR 43.9 Return to Service I other regulation specified Approved design data and are in a condition for safe Certifies that unless otherwise specified in Block 13, the work identified n in Block 12 and described in Block 13 was accomplished in accordance to Non-approved design data specified in Block 13. with Title 14, Code of Federal Regulations, patt 43 and in respect n that work, the items are approved for return to service. 21. Approval/Certificate No. : 15. Authorized Signature: 16. ApprovalAuthorization No. : JGVR194F 23. Date (m/d/y.): 17. Name (Typed or Printed): 22. Name (Typed or Printed): AARON J. SPULAK 5/03/02 the part/component/assembly. is important to understand that the existence of this document alone does not automaticalty constitute authority to install \ett,"'.""/i."ta||erperformsworkinaccordancewiththenationalregulatio1sofanairorthinessauthoritydiferent.tha^ntheairworthineaut ,t1,itisessentialtr'attneuserlinJa[ereniuresthathis/herairworthin,essauthorityacceptsparts/components/assembliesfromtheairwo \1 .pailied in Block l. statementsinb|ocksl4andl9donotconstituteinsta||ationcertiIication.Ina||cases'aircraftmaintenancerecordsmustcontainanina[ with the national regulations by the user/installer before the aircraft may be flown' (6-01) * Installer must AIRCRAFT MAINTENANCE RECORD A/G Res'n: N83SG A/c Moder: 11244 Westwind A,/C Ser. No.: 368 Resgt. No.: N83SG Model: ISRAEL JET WESTWIND ll24{ Serial No.: 368 This aircraft was weighed in accordance with manufactures recommended procedures, Type Certificate Data Sheet, and other data acceptable to the Federal Aviation Administration. I certify this aircraft is airworthy and approved for return to service with regards to work accomplished. See weight and balance for this date for details on aircraft configuration at time ofweigh. Details on file at this agency under Work Order No.: 00625 BEW: 12938.00 lbs. CG: 283.74 in. Momenf 3670998.95 in./lbs AIRWEIGIIT,In6. CRS: WWR}T2L can Avronr4.. rN{fA^.ta-t| qtlSrOttr-ttt9 P&*ilLct't uilt7 Ap I aZ2- 3/to7-O2R Sat: 4078. 4/r',r4 (ttsty' *5ZO me'uit. .,-aA.-^ The maintenance described above has been functional tested, The maintenance described above has been functional tested, found airworthy, and is approved for return to service. A detailed found airworthy, and is approved for record is on fiIeylder worlofieyfi J CA record is on frle Work ,,A 3 Inspected Inspected by rt Ho t-'! (///",%5a for Duncan Avionics Houston, TX CRS GF2R844K for Duncan Avionics Houston. CRS GF2R844K AIRCRAFT MAINTENANCE RECORD A/c Res'n: N83SG A/c Moder: 1124LWestwind A/c Ser. No.: 368 DATE A/C T.T. A/G T.Ldgs. DESCRIPTION Starflite Management GrouP 9000 RandolPh St. Houston, Tx.77061 5716 A/C Reg. N83SG ll24| SA{ 368 Total Times.7924.4 Total Cycles' Aug. 13,02 p/n s/n Remove #1 brake assy. p/n 5002805-3 s/n Jan 86- 531, Replace with same , -3, sl n 2l Bg -l,replace witlm2e pl R3 443,Remove #2 brakeassy. p/n 5 002805 y' Y / leaks, ops check or. R432r,rAw 32-43-01 of Maint. Man. No affi#{.#_( A&P 253660856 AIRCRAFT MAINTENANCE RECORD A/G Res'n: NB3SG A/G Moder: 11244 Westwind A/C Ser. No.: 368 Starflite Management Group 9000 Randolph St. Aug, 13.02 Houston,Texas 77061 AIRFRAME Westwind S/N 368 N83SG Total times; 7924.4 Cycles;5716 CnV 200 Hr. Inspection. Visual insp. Cockpit and cabin portable fire extinguishers , and weight check. Charge Emerg. Light batterY. Remove Emerg. Gyro battery PS823 serviced by United Battery, of Houston P/N 501-1075-06, s/n 1310. Remove CVR beacon battery , Install new battery PA{ DK100' s/n DV4013 Visual Inspect elevator control bellcrank assembly,27.520 X-ray inspect nose gear assembly, nose gear shaft and door assy. X-ray inspect left and right aileron control rods assemblies X.ray inspect rudder control rod assemblies. Check pilots and co-pilots oxygen mask' CAV AD 2002-0l-26 on both engines. Inferior bolts around inlets. No problem found. C/W AD 1989-12-08, Horiz. Stab spar splice' No problem found. C/IV SB. 1124-30-036,part2.Ice and rain protection. C/W SL WW-2492 Hyd' Hose Insp. No problem found. Remove right engine for MPI by Dallas Aeromotive, Installed by Dallas Aeromotive and All post runs normal. C/W AD 1996-24-II,right and left accomplished, no problem found. c/w sB.1124-21-I29left and right aileron flight control. No problem found. Remove ships batteries, Install reconditioned batteries, saft p/n 15580 s/n 38056 s/n 81985, from united batteries. Replace lower beacon bulb pin 1924x, ops ck' OK. ' I certify that this aircraft has been inspected in accordance with the above mentioned inspection Dewey R. Smith l\nd was determined to be in an airworthy condition. A&P 253660856 Starflite management Group ,ft> 9000 Randolph 7/ Houston Texas 77061 ? - /3-o Westwind 1124 S/N 368 N83SG Total Times 1945.9 Total Cycles 5726 Change desicant in R/II nose compartment for w/s. Adjusted scissor on left main gear to correct clearence. Repair close out at left rear window, reglue carpet in several places. 4z&*A&P 253660856 AIRCRAFT MAINTENANCE RECORD A/C Res'n: N83SG A/G Model: 1124A Westwind A/G Ser. No.: 368 Starflite Management Group $n 9000 Randolph St. ? 'JD. ob Houston Texas 77061 Westwind 1124 S/N 368 N83SG Total Times 7959.O Total Cvcles 5736 Remove left GCU P/N 352060DC168D1, s/n 168D1. Install SA{ 6640693MI. Parr. And load balance, OPS check good. Adjust right engine oil pressure to 45 psi at887o Nl, IAW 72-00-00, Page 588 of Honeywell TFE 731 Maint. lpnyal' n / / cabin and airframe portable fire ext. check. C/!V -',-E---,1 '/ /'@ ^?"J;{##',.| Starfl ite Management GrouP 9000 Randolph St. Houston, Tx. 17061 Westwind 1124 S/N 368 N83SG EngineTT.7892.4 TC.5640 Sept.20'02 /t TFE 731 Adjust right engine oil pressure to 45 psi at88Vo Nl IAW 72-00-O0,Page 588 of Honeywell - /MDewey R. Smith A&P 253660856 Starflite Management Group 9000 Randolph St. Houston, Tx.77O6l Westwind n24 SAI368 N83SG Total Times 7982.6 Total Cycles.5762 g$!.104? c/!v Emerg. Power supply PS 823 service by United Batteries, of Houston, Tx. C/IV Functional test Hyd. Pump Emerg. Fuse. Remove tail rotating beacon and replace motor p/n 4-6458 and bulb pln7o79. Ops ck' OK' Repair broken wire at wing to tip tank, right wing for compass pickup sense wire, repaired by Temple Electronics' C/W cabin and cockpit fire ext. monthly check. RemovedpilotsRMiBDI-36P1n622-3702-012,Installsamep/n, slnI2L3.OpsCK.OK.ByTempleElect. Remove and replace #2 enginenacelle anti-ice valve connectoip/n PTY 06CE-8-3S, Ops CK. OK' '^ CAil Hydro. TestEmerg. Slorage bottle p/n 36200071, s/n 07510A1 by Shoreline dba Safetech of Houston. dba Safetech of Houston. CAM Hydro. Test N2 storage b&tle p/n 362000'7 L, s/n 07511AA1 by Shoreline ,-.^/ , t./ C/W S.B. IL24-55-O2O R2 on 8-12-02 under AD 1989-12-08. ,/- ./ / / / cnvs.L. wwz|g4R3landingGearon 8-12-02. & - '/ il*"Y R' smith A&P 253660856 AIRGRAFT MAINTENANGE RECORD A/GRes'n: N83SG A/cModel:1124AWestwind A/GSer.No.:368 Starflite Management GrouP . 9000 Randolph St. Houston, Texas,77061 Wesrwind 1124 S/N 368 N83SG Total Times; 8005.5 Total Cycles; 5768 \ov'-08-02 CtW 330228, Charge emergency light battery. splines insp, Soap sample taken, C/w 150 lk.engine lnspection both engines, Including engine pre-flight, starter-gen, brush wear/tension , chip detector insp. CfW * 260169,and #260180, visual inspection on cabin and cockpit portable fire ext. C/IV # 250156Inspect life Preservers. CnV # 25}I62lnspect First Aid Kit. s/n 79-942,Install tire s/n Remove right nose wheel and tire, Aero-Lift replace wheel bearings and cones, wheel assy. P/N 9541874 oct. 10061344' L11gl24g.Change tire on right main, NDT whiel p/n 5002805-Z , Snf Mar 88-421 by Aero-Lift, Install new tire SA"l Replace nose gear down lock switch PA.{ 402EN1-12, swing gear and Ops. Check OK. Inslall new power pack pln N-51I2 s/n 38438 in L/H up wash light in #l position. /t S Removed ADF box, install O/H ADF p/n 622-2362-00l sln4626by Tempte Electroni$r-rr5 new s/n 22950679.lnstall IAW Removed L/H rire and wheel, Install nlw wheel from Aero-Lift P/n 50028b6-2 s7n lunm**; Install tire Maint. Manual..Left hand brake damanged, repaired by Aero-Lift, replacing 2 rotatingdisc, and 2 stationary disc. 32-41-O0of enlfe Replace left taxi light bulb pln 4581 .I certify that this aircraft has been inspected/repaired in accordance with grnfcablerakflame' maintenancemanualsandhasbeenfoundtobeinanairworthycondition./.F;/M^,^ A&P 253660856 LOG BOOK ENTRY. STAR trLITE MANAGEMENT ll24Westwind S/N368 N83SG November 21,2002 TAT'-,-7900# ,A ll,gLandings+5?eh 5 2 7 r Investigated Lost of Hydraulic Fluid, Found and tightened fitting "on the R/tI Hydraulic pump. Serviced hydraulic system and performed hydraulic functional test in accordance with M.M chapter 29-10-00, All maintenance performed on this Aircraft was performed in accordance with current regulations of the Federal Aviation Administration and is approved for retufn to service with respect to the work performed in accordance with General Dynamics Aviation Services Instructions. For details, see work order 151830 on file at this agency. Garrett Aviation Services CRS XBlR606K 17250 Chanute Road Houston. Texas 77032. 1 800-877-5411. Bv: Nick Kvriazis. AIRCRAFT MAINTENANCE RECORD tr-' A/G Reg'n: N83SG A/G Moder: 11244 Westwind A/G Ser. No.: 368 Starflite Management Group 9000 Randolph St. Houston. Tx.17061 westwind s/N368 N 83 SG Total Time: 8074.2 Cycles 581 I Dec.2l.O2 CtW 210169 Visual inspection cockpit portable fire ext. C/W 210180 Visual inspection cabin portable fire ext. C/VV 350148,and 350166, Change pilots oxygen mask, install new p/n MC10-13-02 s/n 5065. CIW 350158, and 350169, Change co-pilots oxygen mask, install new p/n MC-10-13-02 sln 5176. Removed right main fuel pump pln2O7OCOIT3 s/n TIz2z,Install O/II pump p/n ZO7OCOIT3 slnT5332, Ops ,and leak checked. C^V S.B. 1124-35-131, remove oxygen shut off valve, Install new valve kit #GAC 27550-3. Service system and leak check. CnV AD 200l-23-09 for #lEngine, N/A by PA{. ,C/!V AD 2001-23-09 for #2 Engine, N/A by PAI. CnV S.B.972 B40U for #1 Engine Nov. 13,1999. GSBA72-569 C/!V /] ,/ 1 CAV S.8.972.B40U GSBA7 2-5 69,for #2 Engine,C/lV Aug. 12, 02. E-,/l/*,.v'' ,^\ ,/ Dewey R. Smith ' A&P 253660856 Starfl ite Management Group 9000 Randolph St. Houston Tx.77061 Westwind SN 368 N83 SG Total Times 8094.7 TotalCycles582l Jan. 15 2003 C/W 260180, visual inspect cabin portable extinguisher visual inspect cockpit portable extinguisher C/W 260181, , Remove potty and repair connection @ connector, ops check operation OK' ,/) Repau cabin lights on right side, at light socket. 4/k,^,^ A&P 253660856 AIRCRAFT MAINTENANCE RECORD A/c Reg'n: N83SG A/G Modet: 1124A Westwind A/G Ser. No.: 368 Starflite Management Group 9000 Randolph Houston, Tx. 17061 Westwind SA{ 368 N83 SG Total Times 8101.2 Total Cvcles 5826 Feb. 07.2003 C/IV 050600U including 200/400/800 Hour inspection C/IV 530200 Forward to AFT Pressure bulkhead- Fuselage inspection. C/!V 530205 Inspect Forward to AFT main frame. CAM 714010,715010, 741120742120742140 # I Engine Insp. CIW 344616Inspect Emerg.power supply, by United batteries. C/W 341106,341l l6,test pilots and co-pilots Altimeter Far.9l.4l I by Texas Aircraft Instruments. CIW 346lll, 346126 Test #1,2 ATC Transponders FAR. 91.413 by Texas Aircraft Instruments. CNV 340146, 3401 5 I Leak check left and right static system by Texas Aircraft Instruments. CIW 343672 Calibrate #1 Air data computer FAR 91.411 by Texas Aircraft Instruments. CtW 260169, 260180 visual insp. Cabin and Cockpit portable fire ext. C/W 330228, Charge Emerg. Light battery, by United Batteries. CIW 230400 Clean- test cockpit voice recorder Beacon. C/W Deep cycle service on main ships batteries PAI 15580 s/n 081985, 38056 by United Batteries. C/W S.B. 1124-30-036 Part 2. Remove right fuel tip tank, repair broken line, was venting fuel. Leak check ok. Remove LAI aileron trim actuator p/n l092ASl00-1, s/n Al002M, Install OAI actuator PA{ 1092AS100-l SA{ 1282 Replace RH aileron servo tab push pull rod PA{ BRE-4075 Replace L/H thrust rev.piggy back solenoid p/n 4AS5310370-001, Ops check OK. Check Nose wheels for corrosion .. Overhaul both wheels bv Aero Lift. PA{ 9541874 sin Oct. 79-942 . Oct.79-927. I certify that this aircraft has been inspected/ repaired in accordance with applicable airframe, engine maintena found to be in an airworthv condition. The_fJC Tnnspmder test rnd inspedion rEuired by FAR 91.413was pedomed fris date and found to corylywtU FAR 43, Appondh F. the altimeter and static system tests AH 91.411 have been Performed. #1 I //> The been tested to '- leet. f,2 Mako alse Detrails ar8 tib att*s {oiil-zxcn* lnc. FM CRS HE2R869K facility >l Dae/t Texas Tercs Houston, Texas (713)64+1664 CRSHEN$gK AIRCRAFT MAINTENANCE RECORD A/G Reg'n: N83SG A/c Moder: 1124AWestwind A/c Ser. No.: 368 '- DATE A/C T,T. A/G T.Ldgs. DESCRIPTION Starflite Management GrouP 9000 RandolPh St' Houston, Tx.7706I 8150.5 Total Cycles' 5865 A/C Reg. N83SG lr24[ SA{ 368 fotal Times. March,2l,2003 replacing filters. C/W 150-300 Hr. insp'both engines' lncluding Soap samPles taken both sides' check. C/W monthly cabin and cockpit portab le fire ext. check and refill system' I certify that this Replace leaking O ring on#2 brake-ass v. Leak with all applicable engine, airframe aircraft has been inspected/ repaired in accordance be in an airworlhr co.yy_/k maintenance manuals and has been fou nd to '4 /DevieY R' Smith A&P 253660856 Starflite Management Group 9000 Randolph St. Houston, Tx.77061 A/C Reg. N83SG 1124A SA{ 368 Total Times. 8189.3 Total Cvcles. 5892 April,30,2003 Service gear blow down bottle to 1850 psi. Service 02 system. Removed damaged Rad. Alt. Antenna forward .pln622-4550-001 sln459 andAft' P/n 622-4550-001 s/n 509, Install Ant. P/N 522-4255-001 s/n 1816 and Afi$|n1330. C/W Emerg. Light battery service. C/W Emere. Gvro. Power supply batte ry; sr. ZrK-/- Qory, ;ff rtoutNt e ?/''l'- +a+ |h't vw)'10 /'i"ir"uR. Smith rrr.*r' 4t- e,bJ\ et A&P 253660856 lL n '--il I ltCIA r/, J' r ;/U T