Vilicki 4 DEPARTMENT Of tautsFosnanotLI:i" FEDERAL AVIATION ADMINISTRATION MAJOR REPAIR AND ALTERATION (Airframe, Powerplant, Propeller, - • " or Appliance) FormAAPromIci- Budget Bureau No. 04—R0i50.1 FOR FAA USE ONLY OFFICEmlifigeffeftoo 74.67 INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1. (or subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE GULFSTREAM i .. , MODEL G-1159B SERIAL NO. . . ... 1.51 -.: .- -...-. , •- • NATIONALITY AND REGISTRATION MARK - ... U . S .A . N -979RA 2. OWNER NAME (As shown on registration certificate) • OLDEN-AMERICAll CORP.. ADDRESS (As shown on registration certificate) WESTCHESTER COUNTY AIRPORT WHITE PLAINS, NY 10604 3. FOR FAA LISE ONLY. • c, -• &.:: • .::.:.•-!-:•-: • . : .. . . -. . ... • • • .. . . . .. •• . . • ..- . ..-. .. . . .. .. . .... . , 4. UNIT IDENTIFICATION S. TYPE UNIT aMUCF . MADO EL SERIAL NO. REPAIR ALTER- ATION AIRFRAME sienetenest (As descra,ed . _ in item I X X above)siNianntreetann POWERPLANT _ . . .. . ..._....... . . • - . a PROPELLER APPLIANCE TYPE / . I MANUFACTURER \-\\ 6. CONFORMITY STATEMENT A. AGENEY'S NAME AND ADDRESS S. Kil4D Of AGENCY C. CERTIFICATE NO. GULFSTREAM AEROSPACE CORPORATION P. 0. BOX 2206 —. TRAVIS FIELD SAVANNAH, GA.. 31402 u.s. csansic.Asso MECHANIC • 701-10 FOREIGN CERTIFICATED MECHANIC X CERTIFICATED REPAIR STATION isAssusAcrusit D. I certify that the repair and/or alterationmade to the ubii(s) identified in item 4 above and described on the reverse or attachments hereto have been made in—accordance with the requirements of Part 43 of the U.S- Federal Aviation Regulation?, and that the information furnished herein is true and correct to the lieu of my knowledge. DATE • 5/30/84 SIGNATURE OF AUTHORIZED INDIVIDUAL . . . . .. . PATRICK J. LYNCH en 7. APPROVAL FOR RETURN TO SERVICE Pursuan the BY to the authority given persons specified below, the unit identified in item 4 Administrator of the Federal Aviation Administration and. is ['APPROVED LLREJEC. was inspected in the manner prescribed by FAA H.T. STANDARDS INSPECTOR MANUFACTURER IN:SPKTIC44 AUTHORIZATION OTHER (Specify) .1/4. FAA DESIGNEE „, A REPAIR STATION . CANADIAN DEPARTMENT Of TRAM:SPORT IN Of P.M:RAFT DATE OF APPROVAL OR REJECTION 5/31184 CERTIFICATE OR DESIGNATION NO. 701-10 SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J. LYNCH e h• -„--e-d___ c.cue - • • alas' , 4c- Al EFTA00278335

• NOTICE . Weight opdsbolance or operating, mitation changes shall be..entered in the appropriate aircraft record. An alteration must be compatible withall--previoas alterations to assure continued conformity with the applicable airworthiness requirements. DESCRIPTION OF WORK ACCOMPLISHED.(If more spaceis required, attach additional sheets. Identify with air- craft nationality and registration mark ancrdate work completed.) . • ACTL: 488 LANDINGS . - . REF. GULFSTREAM AEROSPACE CORPORATION WORKORDER NO CO2-1517084-2924 SECTION INCORP. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000 FOOT OPERATING ALTITUDE": . .•.,. NOTE:'-' 1 = REF.'41SC'299 "45,000 FOOT'ORERATIN6ALTITUDE - CERTIFICATION 4k ..• REVISE WEIGHT AND- BALANCE REPORT,AND AIRCRAFT EQUIPMENT LIST AS DUE 3. -'INCORP.'GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000 FOOT OPERATING. ALTITUDE" 'NOTE: AIRCRAFT FLIGHT MANUAL SUPPLEMENT NO. G -II -81 -02 (FAA APPROVED) PLACED IN OPERATOR AIRCRAFT FLIGHT MANUAL.. •,, PRE-REQUISITES INSTALLED: - 1.- GULFSTREAM AEROSPACE CORPORATION A AIRCRAFT SERVICE CHANGE NO. 114-AIR- COND. AND STRUCTURE CABIN PRESSURIZATION 6000 FT. CABIN ALTITUDE AT 43,000 FEET,- REWORK OF: - 2. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO. 122 "FUEL BOOST PUMP PROVISIONS FOR NEW=MODEL". 3' FUEL BOOST PUMP'P/N 1159SC011 INSTALLED. 4- ENGINE FUEL FLOW REGULATIONS (LEFT & RIGHT) PIN CASC174 OR LATER IN- STALLED: 5. REF. GULFSTREAM AEROSPACE CORPORATION CUSTOMER BULLETIN NO. 302 "ENGINE ACCELERATION AND DECLERATION TIME TEST/ADJUSTMENT" - ENGINE ACCELERATIO, AND DECELERATION TIME CHECKS COMPLETED. 6 -PLACARD P/N 1159820283-11 INSTALLED. . . 7-- FOLLOWING -AIRCRAFT-RECORDS REVIEWED: ...iA FAA FORM 337'S -- B SUPPLEMENTAL TYPE CERTIFICATE ' C CURRENT STATUS OF-ALTIMETER CERTIFICATION (0 WEIGHT'AND BALANCE REPORT CURRENT STATUS' ... EFTA00278336

FAA AIRCRAFT REGISTRY CAMERA NO. 3A/ DATE: 3 -.V745 . . PAGE 2 of 2 FAA FORM 337 G-1159B PROD. NO. 151 N-979RA DATED 5/31/84 CONT. 2 - INCORP. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO: 300 "GIIB WING MODIFICATION" PER GULFSTREAM AEROSPACE CORPORATION TOP DRAWING NO.115925000'REV:ILE:0:•E4*&*E7- . , A; PAINT EXTERIOR OF AIRCRAFT PER GULFSTREAM AEROSPACE CORPORATION DWG# SC*26505501 INSTALL GII LANDING.LIGHT MOD. PER GULFSTREAM AEROSPACE CORPORATION DWG.#*SE'2128800101 INSTALL GIII RADOME PER GULFSTREAMAEROSPACE CORPORATION DWG.# 1159SCB2064 . . INSTALL LIFELINE ATTACHMENT MOD. ON WING.PER GULFSTREAM AEROSPACE CORPORATION DWG.#'1159RDF631 REPAIR V. FIN R. BEAM DEV. TO ASC 231 SP 50G DEV. AV 25006 DEV. TO ASC 294 , DEV. AOA W.D. LOG. NUTCRACKER W.O. STALL BARRIER SYSTEM SE 21318004-01 A.F.M.S. REQUIRED G -IIB -82-001 RETRACTABLE LANDING LITES G -IIB -82 -003 SIX PANEL SPEED BRAKES 41118EFAC tR"sF EFTA00278337

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- - DEPARTMENT OE TUNSPORTATION - . ,..„, FEDERAL AVIATIONAWAINISTitATIOW • - 'N . Fen* Akfuotud • Budget Bureau No. GE-R060.t • FOR FAA USE ONLY MAJOR REPAIR AND ALTERATION . fAirfrcime, Powerplant, Propeller, or Appliance) OFFICE thialtifTELOym 7-0-::. INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B. and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this forte. •• • i " • • -' ' ' ' • ' MAKE . - > ' • . GULFSTREAM • % -- •• MODEL • • : •.: G-1159ri. 1. AIRCRAFT ..> SERIAL NO.' • 1.51 NATIONALITY AND REGISTRATION MARK U,S.A. N-979RA . 2. OWNER NAME (As shown on regidiatieri eeetifioatel - - • OGDEN-AMERICAN CORP. . ' ADDRESS (As shown on registration certificate) , WESTCHESTER COUNTY AIRPORT WHITE PLAINS, NY 10604 • 3. FOR FAA USE ONLY • • . - . . • -- . . . . _ .:...:— s••• , .;• . " . - • - . . ' . • _ _.. . • , .. ' . -.• • - • 4. UNIT IDENTIFICATION • • S. TYPE UNIT MAXI . .. • "SERIAL NO. — REPAIR ALTER- AVON , AIRFRAME . ww•••••••••••••••••••• (Asdeseralled in itern I above)••••••••••••••••••••••• : • X X POWERPLANT . . • - - • . - • . . . . • ... . • PROPELLER . • • - • • • . . • TYPE .. • ' • _ .. . - . , APPLIANCE MANUIACTUIER - .. - ..... . .. - . . ,......- . . • 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. GULFSTREAM AEROSPACE CORPORATION ' u. . aRTNICATED MECHANIC P..0. BOX 2206 - TRAVIS FIELD FOREIGN EIRTINCATED MECHANIC ' SAVANNAH, GA. 31402 . ' - -- x CERP.EICATED REPAIR siAtioN 701-10 .... • MANUFACTURER • D. I certify that •the repair and/or alteration niade'to attachments hereto have been made in accordance with and that the information furnished herein is tree and the•unit(s) identified in item 4 above and described on the reverse Of the requirements of Pact 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE - • - • - - . • 5/30/84 • SIGNATURE OF AUTHORIZED INDIVIDUAL • _ . • ,.. a_!..„ ., PATRICK J. LYNCH fro.... .../C . • 7. APPROVAL FOR RETURN TO SERVICE - Pursuant to the authority given persons 'periled below -the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is []APPROVED QREJECT£D fAA H.T. STANDARDS INSPECTOR MANIKFACTUREW . - . _ . .. .. INSPECTION AUTHOMEATION OTHER (Siseify) , BY FAA DESIGNEE X ... REPAIR STATION - • CANADTAN DEPARTMENT OE TRANSPORT ftsrearot Of AMOUUT . c .. DATE OF APPROVAL OR • REJECTION • . . 5/31/84 . - CERTIFICATE OR DESIGNATION' NO: 701-10. . SIGNATURE OF AUTHORIZED INDIVIDUAL. • . PATRICK J. LYNCH Po— --ki • .„,...eff ...... 410*:.o.--Tmiserirkumeoceeorow‘lie.,,;. .•••••• EFTA00278339

NOTICE ; • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements, - 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with air- : croft nationality and'registration mark and date work cempleted.) ACTT: 3586 ACTL: 488 LANDINGS REF. GULFSTREAM AEROSPACE CORPORATION WORKOROER NO CO2-151-084-2924 SECTION 1 - INCORP. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000 FOOT OPERATING: ALTITUDE". . _ . . . REF..ASC 299 "45,000 FOOT OPERATING ALTITUDE - CERTIFICATION R4VISEWEIGHTANOBALANCE-REPORT'AND AIRCRAFT EQUIPMENT LIST AS DUE . _ 3 - INCORP...GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO.299 "45,000100T OPERATING ALTITUDE" , NOTE: , AIRCRAFT FLIGHT MANUAL SUPPLEMENT NO. 6-II-81-02 (FAA APPROVED) PLACED IN • OPERATOR AIRCRAFT FLIGHT MANUAL. - ; PRE-REQUISITES INSTALLED: 1.- GULFSTREAM AEROSPACE CORPORATION A AIRCRAFT SERVICE CHANGE NO. 114-AIR COND. AND STRUCTURE CABIN PRESSURIZATION 6000 FT. CABIN ALTITUDE AT 43,000 FEET, REWORK OF. -- . GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO. 122 "FUEL 'BOOST PUMP PROVISIONS FOR NEW. MODEL". 3.. FUEL BOOST PUMP P/N 1159SC011 INSTALLED. 4 ENGINE FUEL FLOW. REGULATIONS (LEFT & RIGHT) P/N CASC174 OR LATER IN- STALLED. • 5 REF. GULFSTREAM AEROSPACE CORPORATION CUSTOMER-eULLETIN.NO. 302 "ENGINE ACCELERATION AND DECLERATION TIME TEST/ADJUSTMENT" - ENGINE ACCELERATIO3 AND DECELERATION TIME CHECKS COMPLETED. PLACARD P/N 1159820283-11 INSTALLED. 7 FOLLOWING AIRCRAFT RECORDS REVIEWED: A FAA FORM 337'S 8 SUPPLEMENTAL TYPE CERTIFICATE C CURRENT STATUS OF ALTIMETER CERTIFICATION D WEIGHT AND BALANCE REPORT CURRENT STATUS o- EFTA00278340

FAA AIRCRAFT REGISTRY CAMERA ' NO . '3A/ DATE: 3 7- • • • . - • _ . • . SECTION 2 - INCORP. GULFSTREAM AEROSPACE'CORPORATION AIRCRAFT SERVICE CHANGE NO. 300 "GIIB WING MODIFICATION" -PER GULFSTREAM AEROSPACE CORPORATION TOP DRAWING NO. 115925000 REIL.D.E;O:.E4.8.1E7 SECTION 3. A. PAINT. EXTERIOR4F AIRCRAFT-PERGULtSTREAM AEROSPACE CORPORATION DWG.# SC 26505501 . • . , . . INSTALLGII'e.AN6ING LIGHT MOD..PER GULFSTREAM AEROSPACE. CORPORATION OWG.# SE21488001-01 -••••3. • . . . ' C. INSTALL.EIII RADONiPER.GULFSTREAM AEROSPACE CORPORATION DWG. # .1159SCB206B D. INSTALL LIFELINE ATTACHMENT• MOD. ON WING PER GULFSTREAM AEROSPACE CORPORATION DWG.# 1159RDF631 SECTION 4 BELOW LISTED GULFSTREAM AEROSPACE CORPORATION DRAWINGS APPLY. DWG. NO. , SUBJECT REPAIR V. FIN R. BEAM SE 23124043' - DEV. TO ASC 231 SE 23322013 SP,t0G DEV. AV 25006 SE 231.04046 DEV. TO ASC 294 SE 21338006 DEV. AOA SE 23132003 • • W.D. LDG. NUTCRACKER SE 23127002 \ W.D. STALL BARRIER SY - SE 23139005 A.F.M.S. REQUIRED . G-IIB-82-001 'RETRACTABLE LANDING LITES RETAIN G-IIB-82-003 SIX PANEL SPEED BRAKES t• EFTA00278341

FAA AIRCRAFT REGISTRY CAMERA1/4 NO. 3// DATE: 3 -.1 7 43 ••• -..Ez.- nct--"-l'n, illnars- • ;..,--- :,..-- ---' 7 51'7-"Tenr, ---4:•:-4. .)"- WrZli;:mi..P•••-•.:x4k; .:IX-.."?'"A. T.,- Aft.,.., , e.**•;-:-4..7. Ty- -kt.......;.-- ...,•r.. • ''' k, A' ;.irtitZ.17,14,5 i - 5... N;,..i.n-n, .. ,. _, , '" . ". linY ilier - 4.- 4;1 . V•• • .14 ti n z1•-iii ..ft‘'.7‘;‘:1--% • c -; • • . , EFTA00278342

ea DEPARTMENT OF naanSPOiti AMON' FEDERAL AVIATION ADMINISTRATION •••••• : :.: • - - - Fora Approned . Budget Bureau No. 04-R06O.1 REPAIR AND ALTERATION, - FOR Fill IISE ONLY -MAJOR • (Airframe, Powerplant, Propeller, or Appliance) gle2N OFFICE Ipityl i 7-0-01 . INSTRUCTIONS: Print or type all entries_ See FAR'43.9, FAR 43 Appendix El, and AC 43:9-1 (or subsequent revision thereof) for instructions and disposition of this form. • - - • MAKE I GULFSTREAM MODEL G-1159B 1. AIRCRAFT SERIAL NO. 151 NATIONALITY AND REGISTRATION MARK - U.S.A. N —979RA 2. OWNER NAME (As shows: on registration certificate) - ,. OGDEN-431ERICAN CQRP. ADDRESS (As shown on registration certiFcate) WESTCHESTER COUNTY AIRPORT WHITE PLAINS, NY 10604 3. FOR fAA USE ONLY . • - - 4. UNIT IDENTIFICATION 5. TYPE - . UNIT MAX/ . MOOR SERIAL NO. REPAIR ALTER- ATION AIRFRAME • . eeenairens (As descraied in item 1 Save) noineeto-nonneenon X POWERPLANT PROPELLER APPLIANCE TYPE MANUFACTURER 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS , B. KIND OF AGENCY C. CERTIFICATE NO. GULFSTREAM AEROSPACE CORPORATION U.S. CERTIFICATED MECHANIC P. O. BOX 2206 - TRAVIS FIELD FOREIGN CLITIFICATED MECHANIC SAVANNAH, GA. 31402 X CERTIFICATED REPAIR STATION 701-10 - MANUFACTURER D. I certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furcultied herein is true and the unit(s) identified in ;kern 4 above and- described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of my knov. ledge. DATE .... 5/12/84 SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J. LYNCH (E)o-C--A /k. 7. APPROVAL FOR RETURN TO SERVICE Pursuant to the aLthority given persons specified below, the unit encified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is APPROVED U REJECTED BY FAA ELT. STANDARDS INSPECTOR MANUFACTURER INSPECTION AUTHORIZATION OTHER (SponEr) FAA DESIGNEE X REPAIR STATION CANADIAN tEPARTMENT., OP TRANSPC2T INSPECTOR Of AJRCIAFT - DATE OF APPROVAL OR : REJECTION 5/14/84 CERTIFICATE OR DESIGNATION NO. 701-10 ' SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J. LYNCH 1/4"cknj - k-/cis - ---42,0( -• • ' ^ flicepr4.F• EFTA00278343

NOTICE-. . Weight and balance or operating limitation changes shall be entered In the oppropiiate aircraft record. - An alteration must be compatible with all previous alterations to assure continued cpnformity with the applicable airworthiness requirernents. 8. DESCRIPTION OF WORK ACCOMPLISHED. (If more space is required, attach additional sheets. craft nationality and registration mark and date work completecf.) REF. GULFSTREAM AEROSPACE CORPORATION WORKORDER NO. CO2-151-084-2924 REPAIR VERTICAL FIN BEAM MIDDLE HINGE RIB ATTACHMENT PER G.A.C. DWG. NO. SE 25407101 • :•-- ••-• ••• SUS. o.r.o. 1972/720494/545/1303 M7 ' • • .744,.s.:A3 ' EFTA00278344

DEPARTMENT OF TANSPORTATION ' . . FEDERAL AVIATION ADM ' . MAJOR REPAIR AND ALTERATION • (Airframe, Pewerplanf, Propeller, or Appliance) Fora Approved B BadgerBureau Na.04-R060.1 INISTRATION FOR FAA USE ONLY . OFFI C"--pThETEFRTI 7 ON -0-0 I INSTRUCTIONS: Print or type all entries. See FAR 43.9. FAR 43 Appendix B, and AC 43.9—I (ot subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE GULFSTREAM MODEL- I G-11598 SERIAL NO. 15I -• NATIONALITY AND REGISTRATION MARK U.S.A. N-979RA 2. OWNER NAME (As shown on registration certificate) OGDEN-AMERICAN CORP. ADDRESS (As shown on regixtrcrtion certificate) Westchester County Airport White. Plains,' NY - 10604 3. FOR FAA USE ONLY • - ••• • . •..- . . - • - • • .. . • - ., . . - - - - - • ••• • • --- • . .. ....- • •-- . .. . • • • .- •• - - • . .• :- ...-- 4. UN IDENTIFICATION S. TYPE UNIT MARE MODEL SERIAL. NO. tin IR ALTER- ATION AIRFRAME • amentaannamaan (As described in item 1 above)nneenensemenne X X POWERPLANT ... .. . PROPELLER _ . APPLIANCE TYPE - • • - . • . MANUFACTURER • 6. CONFORMITY $TATETAENT A. AGENCY'S NAME AND ADDRESS 5. LINO •.Of AGENCY C. CERTIFICATE NO. GULFSTREAM AEROSPACE CORPORATION P. 0. BOX 2206 - TRAVIS FIELD SAVANNAH, GA. 31402 U.S. CERTIFICATED MECHANIC 701-10 FORE /ON CERTIFICATED MECHANIC x CERTIFICATED REPAIR STATION MANUFACTURER D. I certify that the repair and/or alteration made to the units) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information (washed herein is true and correct to the best of my knowledge. DATE 5/11/84 SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J. LYNCH eank1 7. APPROVAL FOR RETURN TO SERVICE Pursuan the BY to the authority given persons specified below, the unit entified in item 4 was inspected in the manner prescribed by Administrator of the Federal Aviation Administration and is APPROVED IIICREJEL. f}-0 FAA RT. STANDARDS INSPECTOR PAANUFACRIttlt INSPECT ON AUTHORIZATION OTHER (SpersFy) FAA DESIGNEE X REPAIR STATION CANADIAN DEPARTMENT OF TRANSPORT INSPECTOR Sit AIRCRAFT DATE OF APPROVAL OR REJECTION 5/12/84 CERTIFICATE OR DESIGNATION NO. 701-10 SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J. LYNCH r eit.A.A71wAY,A,,,,j_ki • reditia 4 :=Iic=t1t• ' EFTA00278345

NOTICE • Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. ' - • 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space.is required, attach'additional sheets. Identify with air- craft nationality and registration mark and date work coinpleted.) ACTT: 3586 ACTL: 488 LANDINGS REF. GULFSTREAM AEROSPACE CORPORATION WORKORDER NO. CO2-151-084-2924 1. INCORP. GULFSTREAM AEROSPACE A.S.C; .. NO;., CORPORATION AIRCRAFT SERVICE CHANGES LISTED. \ f:SUBJECT • 63,300 POUND INCREASED GROSS WEIGHT MODIFICATION EXHAUST-NOISE ABATEMENT PROGRAM THRUST REVERSER INSTALLATION FLIGHT CONTROLS NORMALIZED ANGLE OF. ATTACK INDICATION INSTALLATION OF AUTO FLIGHT-INSTALLATION OF A SPLIT TRIM SWITCH AUTOMATIC FLIGHT CONTROL SYSTEM-TRIM BRAKE MODIFICATION OF SP5OG ELECTRIC TRIM BRAKE WINGS-GIIB WING MODIFICATION EXHAUST-THRUST REVERSER IMPINGEMENT DEFLECTOR INSTALLATION OF POWERPLANT-PYLON ELECTRICAL JUNCTION BOX, MODIFICATION OF ELECTRICAL POWER-LOOSE GENERATOR WIRING .s ENGING JUNCTION BOX-MODIFICATION OF ELECTRICAL: POWER-DC POWER SUPPLY SYSTEM PROTECTION-MODIFICATION OF TAIL JUNCTION BOX .LANDING GEAR-MAIN LANDING GEAR RESTRICTOF INSTALLATION OF a • FLIGHT CONTROCSFUSELAGE CONTROL CABLE FAIRLEAD, REPLACEMENT OF 1)8.0.9.0. 1972/720.694/545/1303 -Piny • - • EFTA00278346

-PAGE 2 of 2 FAA FORM 337 DATED 5/12/84. A/C MODEL G-11598 S/N 151 -1,1-979RA' 1. INCORP GULFSTREAM AEROSPACE. CORPORATION A.S:C: NO. AIRCRAFTSERVICE CHNAGES LISTED SUBJECT. . LIGHTS-TAIL CONE LENS-REPLACEMENT OF ELECTRICAL POWER -PC17A-1 "E" INVERTER CURRENT PROTECTION-MODIFICATION • AIR CONDITIONING-AIR CONDITIONING SHUTOFF VALVE INSTALLATION . NACELLES-PYLON COOLING BAFFLE 5: EFTA00278347

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3 of 3 Fg DEPAIDLENT Or TRANSPONTATION :. . • • '-% ?UAL AVIATION ADMINISTRATION l • . . MAJOR REPAIR AND ALTERATION . (Airframe, Powerplant, Propeller. or Appliance) :. Form Approved Beeket Bateau No. 04—R060.1 J FOR FAA USE ONLY oFFia IDENTIFICATION FTY FSDO . . 7 INSTRUCTIONS: Print or type aU entries. See FAR 43.9, PAR 43 Appendix B, and AC 43.9.4 (or subsequent revision thereof) for instructions and disposition of this form. • . • 1. AIRCRAFT GULFSTREAM MAKE _ .. i - " -. MODEL • G-1159B SERIAL NO. 151 " . . - NATIONALITY AND - REGISTRATION MARK U.S.A. -N-979RA 2. OWNER NAME (As shown an registration aortieteMe) . . N, OGDEN-AMERICAN CORP.' : - . ADDRESS (As shown eogrogistration certificcrTs) - WESTCHESTER COUNTY AIRPORT • WHITE PLAINS, NY 10604 -,. 3. FOR FAA USE ONLY - . • -.,.. . \ - • • • \ • • . . • - \ 4. UNIT IDENTIFICATION \ • S. TYPE •-• UNIT MAO MOOS \ SERIAL NO. REPAIR ALTER- ATION AIRFRAME ' . . ••••i*••••••••••••••••• (As tiesented in item 1 above) ••••••••••••40* - X • X POWERPLANT • -•- •.. ' \- - PROPELLER- - . _ . • *.-. .. .. _ . ETPE • ' • . - . . . _ • - - - .. • APPLIANCE MANUFACTINIER - ' • 6. CONFORMITY STATEMENT . . A. AGENCY'S NAME AND ADDRESS ' IL KIND OF AGENCY C. CERTIFICATE NO. GULFSTREAM AEROSPACE CORPORATION P. O. BOX 2206 - TRAVIS FIELD' \ SAVA NAH, GA. , _31402 -. . • .. . - . U.S. CIEDFICAND MECHANIC 701-10 fOttIGN CERTITICATI0 MECHANIC X CRITIFICATI0 IMPAIR STATION ' . MANUFACTURER . D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and thit the information furnished herein is true and correct to the best of my knowledge. DATE ' ..- ' . • - _ " -.. - - . .A/9/84 SIGNATURE OF AUTHORIZED INDIVIDUAL al:Zjeti - PATRICK J. LYNCH ,,,' / 7. APPROVAL FOR RETURN TO SERVICE Pursuan to y‘ authority given persons specified below, the unit IA ntified in item 4 was • , ted in the manner prescribed by the Administrator of the Federal Avistion Administration end is (3eAPPROVED CI REJEIt'slM . - BY PAS, ay. STANDARDS MANULACIIIIER . INSPECTION AUTNORIZATION OMER (Smelly) . PM DESIGNEE IP REPAIR STATION CANADIAN DEPARTMENT Of TRANSPORT INSPECTOR ,or AIROLAPT . DATE OF APPROVAL OR '•IREJECTION 5/10/84 • " -- CERTIFICATE OR - DESIGNATION NO. • SIGNATURE OF AUTHORIZED INDIVIDUAL PATRICK J: LYNCH (:)4.‘‘.;-)1/4:1 ' c"c.,412___ EFTA00278349

NOTICE Weight and balanCe or operating-limitatinn changes shalt be entered in the appropriate ciiriicift record. An alteration must be compatible .with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with o~- craft nationality and registration mark and ,date work completed.) PRESENT ACTT ` 3586 HRS. ACTL • 488 'LANDINGS REF. NO. 1 - GULFSTREAM AEROSPACE CORPORATION WORKORDER NO-0O2-151-081-2588 NO. 2 - F.A.A. FORM 337 DATED 9 APRIL 1981 NO. 3 - ACTT 2741.5 HR. Att. 1617 LANDINGS - • . - . NO. 4 - PRESENT GULFSTREAM AENSPACE• CORPORATION WORKORDER NO. CO2-151-084-29' - ' A. INSTALLED BKM PITOT HEAT MONITOR MOD. PER-S.T.C. NO. SA*2907 SW PER REFERENCE NO. 1 B. REPAIRED CENTER AND UPPER. RUDDER. HINGE FITTNGS PER GULFSTREAM AEROSPACE CORPORATION DWG. NO. 1159CS20092- 1159CSM30080, AND 1159CSM20080, REF. GULFSTREAM AEROSPACE CORPORATION AIRCRAFT SERVICE CHANGE NO. 300 "GIIB WING MODIFICATION" MODIFIED RUDDER HINGES PER GULFSTREAM AEROSPACE CORPORATION DWG. NO. 1159CS5000 PER REFERENCE NO. 1&2 AT ACTT 8t ACTL LISTED AS REFERENCE ' ND. 3.. -/PCi ADDITION& SHEETS. At EFTA00278350

• Li ; DEPARTMENT OP TRANSPORTATION ' ,), -.. . , FEE* RAL AVIATION ADMINISTRATION • - f -rat et ,..- rift:, ..r.: MAJOR REPAIR AND ALTERATION . (Airframe, Powerplant, Propeller,.or Appliance) 'Form Ap krona' - Budget Bureau No. 04-R060.1 FOR FAA USE ONLY OF ICE IDENTIFICATION (2 RilD 1 , INSTRUCTIONS: Print or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. I. AIRCRAFT MAKE Gulfstream MODEL G-1159* NATIONALITY AND REGISTRATION MARK U.S.A. N -979RA • SERIA .NO.,.. 151 2. OWNER NAME (As shown on registration certificate) -Ogden - American Corporation ADDRESS (As shown on registration certificate) Westchester County Airport White Plains, New York 10604 3.. FOR FAA USE ONLY .. . -... ... . , . 4. UNIT IDENTIFICATION - 5. TYPE , . UNIT MAKE MODEL SERIAL NO. REPAIR ALTER- ATION - AIRFRAME niterneeernnenenete (As described in item 1 above) • , X POWERPLANT PROPELLER : i TYPE --, APPLIANCE MANUFACTURER 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS '8. KIND OF AGENCY C. CERTIFICATE NO. U.S. CERTIFICATED MECHANIC Gulfstream American Corporation FOREIGN CERTIFICATED MECHANIC P. O. Box 2206 - Travis Field X CERTIFICATED REPAIR STATION 701-10 • Savannah, Georgia 31402 MANUFACTURER D. 1 certify that the repair and/or alteration made to attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s) identified in item 4 above and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the hest of my knowledge. DATE 21 April 1982 - SLAT E F IZ D DIVIDU - Patrick J. ync 7. APPROVAL FOR RETURN TO SERVICE Pursuan to the authority given persons specified below, the unit identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Administration and is bil APPROVED • REJECTED BY FAA at. STANDARDS INSPECTOR MANUFACTURER utSRECIION AUTHORIZATION OTHER (Sperofy) FAA DESIGNEE , A AIR REP STATION CANADIAN DEPARTMENT Of TRANSPORT INSPECTOR OF AIRCRAFT " 11.,:_...... DATE Of APPROVAL OR REJECTION 22 April 1982 CERTIFICATE OR DESIGNATION NO. 701-10 SIr cr eyellRIZED IVIDU Patrick J. qinc EFTA00278351

NOTICE • Weight and balance or operating limitation changes shall be enterecl,in the appropriate aircraft record. An alteration must be compatible with all previous qftercrstions to assure continued conformity with the applicable airworthiness requirements. DESCRIPTION OF WORK ACCOMPLISHED,(If more space is required, trttado additional sheets. Identify w craft nationality and registration mark and date work completed.) 1833 Landings..; Reference Gulfstream American Corporation Woiksorder No.'"'CO2 -151 -082 -2079' Incorporated Gulfstream American Corporation Aircraft Service Change No. 216 "Spied Brakes with Flaps and/or Landing Gear' Additional Warning" in conjunc- tion with (S.T.C. SA 23665W).BIGI Lighted Speed Brake Handle Mod. EFTA00278352

FAA AIRCRAFT REGISTRY CAMERA NO. DATE: I. 12-c; "e.,••i-•t'sbs-..N. DEPART/of, lb, TRANSPORTATION , .:. l, Form Approved - .:_;,_'Budge! Bureau No. 04-R060.i FEDERAL AYIA-ICON ADMINISTRATION MAJOR REPAIR AND ALTERATION FOR FAA USE ONLY • • :Airframe, Powerplant, • Propeller, or Appliance) OFFICE IDENTIFICATION DAL GADO INSTRUCTIONS: Print or type all entries. See FAR. 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thikkg? for- irtirrJctions and disposition of this form. . ., 1. AIRCRAFT. MAKE . . . • Grumman MODEL - G-1159 • . SERIAL NO. - 151 .,. - -- .... • . _._.... NATIONALITY AND REGISTRATION MARK ..N-97CRA - 2. OWNER NAME (As shown on registration certificate) .. Ogden American Corporation- ADDRESS (As shown on registration certificate) 277 Park. Lane New York, New York 10017 3 FOR FAA USE ONLY _ • . : • • - • • • - _ . ... , .. • . '-• 4. UNIT IDENTIFICATION 5. TYPE'--: • ..• - • . • UNIT • • . . . • . - - MODEL SERIAL NO. REPAIR ALTER- ATION AIRFRAME . . . . . . _ .. . - . •Nrie4449:40;ine‘seani-ing (Ai qescirilked in item 1 ahove)nnenikimmenner . . . . POWERPLANT PROPELLER . - • _. ... -- --------- APPLIANCE TYPE . • MANUFACTURER ' o. • • • 6: CONFORMITY STATEMENT A AGENCY'S NAME AND ADDRESS- • B. KIND OF AGENCY C. CERTIFICATE NO. D.L. Coppinger X U.S. CERTIFICATED MECHANIC 3628 Woodleigh Drive - . FOREIGN .CERTIFICATED MECHANIC • A&P 5032.§9 . Dallas; Texas 7522? CERTIFICATED REPAIR STATION MANUFACTURER D. I certify that the repair and/pi alteration made to • Attachments hereto have been made in accordance with and that the information furnished- herein is true and the unit(s) identified in item 4 above and described on the reverse or the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. .. . DATE " March 24,:1978 SIG TURE OF AUTHO INDIVIDUAL " , • 44 D.L. Coppinger 7. APPROVAL FOR RETURN TO ILE A Pursuaa._ to du; authority given persOns specified below, the unit ident;fied it itt-t:: 4 was inspected in the manner prescribed by - 'the the Administrator of Federal. Aviation Administration and is fl APPROVED - f LUJE...itu BY FAA FLT: STANDARDS INSPECTOR - MANUFACTURER • - • X INSPECTION AIJTHORIZAION OTHER (Specify) ' . . - • • FAA -DESIGNEE REPAIR STATION • CANADIAN DEPARTMENT OF TRANSPORT INSPECTOR OF AIRCRAFT ' . DATE OF APPROVAL 'OR • REJECT:ON .., - March 24, -1978 ' CERTIFICATE OR. -, DESIGNATION NO. ' • 'ono 3' 2 4)9* SIGNATURE OF AUTHORIZED INDIVIDUAL D.L. Coppinger 7 7 0.7stiscar-4-- tv: • EFTA00278353

NOTICE • • . Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alte,ration must be compatible with all previous; alterations:to assure. continued conformity with the applicable airworthiness requirementi. 8. DESCRIPTION OF WORK ACCOMPLISHED (If rAore space is required, attach additional sheets. Identify with air- . craft nationality and registration mark and date work completed.) ' • . _.. • • • , . . . . VLF/ADF coupler," , GNS 500A P/N 111305.±.2 S/N 120 Weight 1.5 2 Lbs. , • for coupling ADP sense antenna' to existing VLF. This unit is T.5.O. C94 approved, This -Coupler installed on a-sack-,--attached- between bulkhead& • between fuselage' stations .5.39.150 and 556.0 in upper fuselage. • • Coupler _rack fabricated of• 2.024T3 in thickness, and dimenaionally 2.75 . X- It..0" with ..025 flangs bent up for . • • • strength. Rack attached —by:. four MI Wo. 8 aircraft screws and nuts. The Coupler attached to above rack by four (41 each aircraft, :Screws/nuts as provided for by the equipment manufacturer. Coupler location is approximately 6.0" from original anten.na• connection. Balance changeis negligible. • This installation' made. in accordance with FAA. AC 0.13-1A 'Chapter 11 & .15 as guidelines for wire routing, clamping and in.stallation in general, and 43.13-2A Chapter .3; with structural testing of. eqUiPment per Chaptar...1. : Operational test was satisfactory. END 0 ADDITIONAL SHEETS ARE ATTACHED: EFTA00278354

iJ , DEPARTMENT OF TRANSPORTATION c -4 5e, 477. 41-,i: ._ . n.lia - - • -..........- . f ERA,. AVIATION ADMINgStRATION . MAJOR REPAIR AND ALTERATION it.k •-- '41' 151v . ____, . . . • r4r • - . . , : (Airframe, Powerplant, Propeller, or Applianc - Ace) ".,-, L.-• Form Appeared Budget Bureau it 04-RONLI ..i_FOR OFFICE . igk:gr1 Felei UV •OSIS . ----.'''; —.Z.--.. IDENTIFICATION iNsTRUCTIONS: 1.--.1r:h-,.rratriOns. - Print or type all entries: See FAR 43.9, FAR.43 Appendix Ha disposition of this form. : • • ' /mum - . Grumban :Ix . . B. 0- te AC 43.9-1_ for'siflaqUint revision thereof) . • .. .• more . • • • G-1159 . • • 1. AIRCRAFT ..... . Z OWNER SERIAL NO., . • . - - 1 .7 • - 51 NAME (As shaven on registration certificate) . •• •••.• - — • • , • erican.Qorporation tm Ogden NATIONALITY ADDRESS (As Hangar . Whites AND REGISTRATION 1 A •rp7 .-. _ registration certificate) .County A/P .. Nevr ..Yoris 10604 rfit, own on D Westchester Plains, •••:-; 3: FOR FAA USE ONLY.. • -• . . . . •••• - • . . • • - , • 4. UNIT IDENTIFICATION --- I • 5. .TTPE UNIT ...:.--. . 'AIRFRAME. • , • - MODEL - SERIAL NO. REPAIR •. • . ALTER- • ATIOPI • .. . • -.43flawiTisnihtana40-00! (As described in item I above)enneeeitweenneien# • . X . • PQWERPLANT . '-- . • i ' . • PROPELLER .' . :.• -. ' . • APPLIANCE TYPE • .. —Flap .asSebb - • - 1].59C200005-2- - .. 151- R/H >t MANUFACTURER . . Grumman. .• 6.. CONFORMITY, STATEMENT :. . A. AGENCY'S NAME 'AND ADDRESS ... . B. KIND 'or AGENCY C. CERTIFICATE NO. Grumman American A-dation .Corporation P.O. Box .?206.- Travis Field • ' . . Savannah, Georgia -31.402 . ' • • .. U.S. CERTIFICATED MECHANIC • 703.-10 FOREIGN CERTIFICATED MECHANIC . • . X CERTIFICATED REPAIR STATION • MANUFACTURER .'....". . . D. I certify that flit:repair an-silor. alteration made -to the unit(s): identified in item attachments hereto have been rdadc-in .accordance with the requirement's of Pan 43 and that the informatial furnished .hereinis true and correct to the bek of my knowledge. • 4 above of the NDIVLD i tri and described. on•the- reverse or U.S. federal .Aviation Regulations • - • • DATE ' - ... .. • . . .. --..__ . 20 July 1976 - - . . - ...• SIGNATURE OF- AUTHORIZED • L. . . ynch . • -.:•-• prescribed pursun ilta . • DA 1 • k riEEMON ?a ._......_-. Adminiitrator . • - 7. APPROVAL FOR RETURN-TO SERVICE - • • . . - given personi.ipeciked below: the anit'identified in item 4 was insUccted in the manner Aviation' Administration and is . M APPROVED ['REJECTED _ by -.1 _ix the atithority, of the F.,deral . 2F Jo2y FAA INSPECJOR • *AA APPROVAL • 1 976 : KT. STANDARDS . ' MANUFACTURER 11. - ' • ' .. %. .•'. . • •• . INSPECTION CANADIAN OP TRANSPORT OF. AUTHORIZATION . OTHER ! (Specify) . • • • . • . - - - , ... . . DESIGNEE - .x . ' .. -.• REPAIR StAilON. - t ' ' • DEPARTMENT. . .INSPECTOR . . AIRCRAFT ' - . - OR . • . - . , .. ,,.DESIGNATION . . CERTIFICATE OR . ; NO.- •-• ' 701-10 SIGNATURE OF AUTHORIZED IN D •••••• • •.eat-ei.,_.e t - ,.. . Patric - EFTA00278355

FAA AIRCRAFT. REGISTRY • CAMERA NO. 0.- DATE: I it:72- q EFTA00278356

• NOTICE • , 1 .. Weight and balance or pirating limitation phanges'ihall be entered in the appropriate aircraft record, I • • • An alteration must be compatible with all previou:e alterations to assure continued conformity with applicatile airworthiness 'requirements. '8.. KKR) PT! ntterii9811 ..fitc01/21. I SHED Of more space lc ri•quired,'attach additioncl sheets.. Identify : craft nctiiinarity..anct re gh:tration mark and dcree.:work.coinpleted4 • • ' . Below listed renal:?s- If,ex.e.,cormaletel at Grumnan American Aviation CornoratLon, Savannah, Georgia. Pertinent "detailaon thii maintenance. are an file at this facility (Certified Repair 'Station. . )14..(5).• under- -"Ott q -02 -151 -076 -670 /.: ,669 dazed ‘• • ••:. • • . . RePairS to RAI wing structure, flip and R/11 gear door_due to tire bloY out. • ilePaire'd RAI flap per $44.4., approved.Engineering bra nng #80:a59-CS-806. Replaced PA landing gear clOcir;•RIN 13.591720400-1 S/N ON S-3. Repaired'Ilt t wing T.E. bole area ptr‘G.A..A.C.,..Commeflcal Minor. Discrepancy Repair Menial. ADDITIONAL SliEET• Atte 'AT1AHED EFTA00278357

• • •.:•• • -. • ••••7/•:'. . . . .... , "rti.t EFTA00278358

DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRATION. • Ca 4 21 Pr !t .•• ' Fans Approved Bcdgef Bureau No. 04.4060 I FOR F.4.i USF ONLY MAJOR REPAIR AND ALTERATION 0GP1/400 -1 (Airframe, Powerplant, Propeller, or Appiiancey °POLE IFICATION 7 . INSTRUCTIONS: Print or type all entries. See FAW43.9, FAR 43 Appendix ll:1;ii.4 AC43.9-1 tar subsequent revision ihereof; for ic?tructions and disposition of this form. . . • . '•'' ' . MAKE • .•-.-• Grill:man - MODEL ' - • G-,1159 ' I AIRCRAFT'' SERIAL NO. . • ' • ' • . - .; 3.51- - ::-. :- : . . NATIONALITY AN TI MARK • a • H979 - • .1)/ A/4 -. 2. OWNER NAME (As shown on'registrationarrtificatil . ADDRESS (As shown on registration certificate; • Hangar A Westchester Connty.airport . • Ogden-Americtin Corporation White Plains; New York 10604 3: FOR FAA. USE ONLY . ••••• • . . -; .. . . • • • 4. UNIT IDENTIf!CATION - 5. TYPE .. . :-.4r.I - • . • _ . - % SERIAL NC:: - REPAIR ALTER- . ADON . • ' • .. AIRFRAME .--.. . .• . . . . . . . • -- • . • - . :461INAPinfeneene4~ 4 (As Clascribed in item 1 above)nneneen.:•••;ilenite ''. ..... ... -.. - . r — . X POWERPLANT .i. . PROPELLER .7 • •• --. . • r• . • . . TYPE • . •, .- - • ' • ' APPLIANCE MA NUFACTURER • . • 4 • . - . .- ' 6. CONFORMITY STATEMENT - A. AGENCY S NAME AND ADDRESS • B. KIND OF AGENCY • C.' CERTIFICATE NO. Grumman American Aviation Corporation U.S. CERTIFICATED MECHANIC .P.O. Box 2206 - ttravik•gie1s1 ' ICHIE/ON CERTIFICATED. MECHANIC . Savannah, Georgia .311+02 " • .14 CERTIFICATED REPAIR STATION . 701.10 t MANUFACTUREIT'' D. 1 certify chat the repair and/or alteration Made to attachments hereto have been made in accordance with and that the information furnished herein it true and the unit(s) identified in hem 4 ;hove and described on the reverse•or the: requirements of Part 43 of the U.S. Federal Aviation Regulations conics to the best olmy klibwledge. ' DATE • . 19 March 1976 SIGNATURE OFWTHORFD INDIVIDU a r3. ' L4ync . 7. -APPROVAL FOR RETURN TO SERVICE. . . - - • Pu stiant :43 the authority Alvin persons specified bells*, the unit identified in item 4 was inspected in the 'manner prescribed by. the Administrator of the Federal Aviation Administration' and is )pi APPaOVED ID REJECTED . . ' -FAA FLT. STANDARDS INSPECTOR 'MANUFACTURER •• ..... ...-......... INSrman.rn AUTHORIZATION I°11". :(sPecifil .- .. . BY FAA DESIGNEE X • • REPAIR STATION . . CANADIAN DeARTMENT OF TRANSPORT INSPECTOR Of Amain -• DATE OF APPROVAL OR - REJECTION ' • -- 20 !arch -197,6 CERTIFICATE •ClR . DESIGNATION NO. . 701-10: SIGNATURE OF AUTHOWED D . ... IC . . . 0 -'- . Patrick . . FAA Form 337: v -on (8320) EFTA00278359

yy Ali._ r•s - - - 7 .r CI:t -:"-' ...... > 12 c" := .ri..T.. . ? • C. • . ' tz. a, - EFTA00278360

',Taco •€,V. e Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all preyious alterations to.assure continued conformity with the aFiplicable•airworthiness requirements. 8. :DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. craft nationality and registration mark ond date work completed.) .. - • .. s: . • . : , Alterations -completed per GI-Ur-Man American Aviation Corporation We ,.....; . 0-02+151076-527%.dated 9 -March::1974., 'References :' - . •. . ••• •••1 Airworthines4.Directive 7k-17-05 "Reactivate, ground spoiler 2. • . ,Grumman .American Aviation Corporation Service Cnange No. 180 #.L..&.#2 Reactivate ground spoiler r,system".. ' Safe-rflight "Speed Control Automate' Throttle" modification F.A.A. • S.T.C. No. "SA7222A". - - Relocated Safe-flight accelerometer In Main gear. wheel well area per drawing #D.591M34•3 due to incorporation of Servik4 'Change. #180 'ReactiVate ground spoiler system". NOT .Safe-flight recommended aligdment check complied with. • • • .. • • • . . b.. Installed. "Grou$ spoiler Manilal d ctivation valve inspection: window" ..per Grumban American Aviation Corporatibn engineering approved drawing. . ,r1159RDF26O. •• Ref: Sertice .Change #180 "Reaetivate ground spoiler system ADDITIONAL SHEETS ARE ATTACHED 2 EFTA00278361

AEI 4. • • Im••••• AA A ...A • • • • ... . 1 • •• ••••-*.- EFTA00278362

O • FEDERAL. AVIATION AGENCY • . Form Approrrd Budget Bureau No. 0-1.—R060.1 MAJOR REPAllt. AND ALTERATION . FOR FAA USE ONLY (Airframe, Powerplant, Propeller, or Appliance) OFFICE IDENTIFICATICalL GAD° 4 2i$.2 INSTRUCTIONS: Print nr type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9—i (or subsequent revision thereof) for instructions and disposition of this form. MAKE , Grumman MODEL 6.1159 1. AIRCRAFT SERIAL NO. • 152 • NATIONALITY AND REGISTRATION MARK N979RA • 2. OWNER NAME (As shown on registration certificate) ... Ogden .Auserican Gorse ADDRESS (As sho‘sts on registration certificate) 77 Park Avenon ow York. Nn York 10017 3. FOR FAA USE ONLY :Thrctiber edrinasiritIsartatefralgtusilFbrajecelilttioaansdd coihnsefoarenn i:PnritocyttlemdinP.sioliileityvif:oitnrhtabpeypaliablbpeleerdsactisrn: • authorized in PAR. 43.7. 3 -IX 75" a 7:747,1_, Date FAA Inspector, SW GAD0.2 IDALI 4. UNIT IDENTIFICATION t/ • S. TYPE . . UNIT MAKE . MODEL - , SERIAL NO. REPAIR • ALTER- ATION AIRFRAME 44doenneen:rwnwaiewir (As described in item 1 above) x POWERPLANT . . E ffhi ng f-Ft I PROPELLER D • UAR 1 c iv t L I: APPLIANCE TYPE &IAA. 0 &LELA GA nO MANUFACTURER L. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY -Mt-clew:1W ..C. CERTIFICATE NO. Aircraft itel Redbird Airport . P. Co $O=24889 Danes, Tens 75224. • U.S. CERTIFICATED MECHANIC (FOREIGN CERTIFICATED MECAMMIC RS 3834 Radio i CERTIFICATED REPAIR STAT1bN sat! Airframe MANUFACTURER 1: 14 D. I certify that the repair and/or alteration made to the unit(s) identified in item 4 above and described on the reverse or attachments hereto have been-made in accordance with the requirements of Parq 43 of the U.S. Federal Aviation-Regulations and that the information furnished herein is true and correct to th best of inylknowledge. DATE .... lisich,14. 1975 SIGN I O -.AUT (ZED I ..--y - rs'Vee - -..(- 7 7. APPRO Al FOR RETURN TO SERVICE Pursuant to the authority even persons specified below, LI:Want the Administrator of the Federal Aviation Agency- and s 0 identified in item 4 was inspected in the manner prescribed by APPROVED REJECTED BY FAA FIT. STANDARDS INSPECTOR I MANUFACTURE* Vz. INSPECTION AUTHORIZATION -- OTHER (Specify) • FAA DESIGNEE x REPAIR STATION •' _ . CANAD!AN DEPARTMENT Of IRANSPORT INSPECTOR : Of AUtatAFT - DATE OF APPROVAL OR -R.tfar gIN 17. 1975 CERTIFICATE OR ifiti"°. SIGNA OF AlfilORIZED VID , , _.,/,,/,z,A4-./20 FAA Form 337 (I-65) OBSOLETE PREVIOUS EDITION 0052-025 00 (8320) • s: • • - • EFTA00278363

F; - AIRCRAFT AFGISTRY. CAilF.-:A NO. a.. DATE: ia.-7 2-v) NOTICE Weight: and balance or operating limitation changes shall be entered in the appropriate TtirCrTiff=—record, An alteration must be compatible with all previovs alterations to assure continued conformity with the applicable airworthiness requirement's. DESCRIPTION CF WORK ACCOMPLISHED/If more space is. reguired,- attach additional sheets. Identify wi croft nationality and registration mprk 'and date work completed.). .5: -.. • Installektinal CollinatICS.3iaysteme cceisisting of the fallo,hing: . ... • • • •;• each Collins NCS.31 Control 114aplay Unita It each Collins 339R-1 Progress Ramat Readout tinfta • 4 .each Collins 899P-1 Radio Adaptor Units . 1 each Collins 339R-7 Remote Readout Unit • 1 each Collins 339R.8 a Unit. each.Collins 33911.10 Remote Readout Unit 1 each.Collins 339R.11 Remote Readout Matt 1 each Collins 339R-12 Remote Readout Wt. 1 each Collins 913Y-1 Mode Selector_ — The two NeS.41 'control, -339R-0 RRU, 339R-10 RRU, 339-R-12 RRU and 913Y-1 NOV are installed in the center console. The 339R-I PRRU's, 339R-7RRU and 339R-11 RRU are installed In the instrument panel glare shield. The two 1399P-1 radio adapters are installed on the top shelf of the radio compartment at r..s. 140. The systems are wired per EAS drawing 180601. . . Wiring installed by Aircraft Service. Inc. conforms to MIL-W-5036 or MIL-W-161378 and is in. stalled in accordance with AC 43.13-2. chapter 2 and AC43.13.1, chapter 11. All structural attachments and installations performed by Executive Aircraft Service are in accordance with applir-Ablet sections AC 43.13-2. These eystems are approved under the following TSO's: C34c. C36c, C37b. C38b, C40a. C41c, C66a and C74c. This equipment has been certified as meeting the accuracy requirements of AC90.46. reference FAA letter ACE-213/8110.6.1 project Z4030CE. Operational and accuracy checks were conducted with the eaaipment Installed in the aircraft for compliance with 1%C90.45 appendix A paragraph 3C. ADDITIONAL SHEETS ARE ATTACHED. EFTA00278364

"Area navigaticcs use approved for 1FR enroute and approach categories. Refer to Collins pilot guide for the 1,103..31 RNAV system for operating informa- !keit' EFTA00278365

rialYso ••••<'. . - • 4. ^ c'oc-...istai•54.-ki • es...?. - — • • ..:. -. - . • . • • . . -' • . .. .. • ' .... . . • .... • . . . • . • . . . . .. . . •• • • . • • • • ..• .• • ..• ' . • • • • - . - - • - - -..';!': ..• - • ';' :.i. .* • ' . • ....7..:Zi• . . , - . • •• a • . 44. . .....i......,. . - .. .. - .i... - -. - . -- ---...a.:-. jeeiv ..r....h.;...t.:: 25.".I.agt....... .Stf4g....4...a i fizatr ...als .... ! . ft.......Z.:;12.•:Z : : . . • ' .. . . , p a.. .. L.... .•.. . ' • •......• . ••• • ••..... . .• ...• •............ ......• . ' _alma. • . . . . . • .... ..l...•••••••• •6....;•••••••••• ••••.....1............••••• ••••.•••••••••••••••.••••••••.•••••••••••• ••.•••••MINA I ••:••••• \ ../.1•••••• •• ...RE. I. . ••••ltd•• Y .M.1.16.1•1•,. Il••••••:.Y .. . EFTA00278366

FAA AIRCRAFT REGISTRY L CAMERA NO. ;°,1, DATE: igc- I2-2i I • FEDERAL AVIATION AGENCY -,... , --..• MAJOR REPAIR AND ALTERATION . • . (Airframe, Powerplant, Propeller, or Appliance) • For, Arra r Budget stream No. 04-R060.1 FOR FAA USE 0NV: OFFICE IDENTIFICATI9 GADD 2102 INSTRUCTIONS: Print or type all entries. See FAR. 43.9, FAR 43 Appendix B, and AC 43.9—i (or subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE N Cif MODEL G-U59 SERIAL NO. 151 • ‘ NATIONALITY AND REGISTRATION 'MARK N979RA - 2. OWNER NAME (As shown on registration certificate) .. Ogden American Corpo ADDRESS (As shown on registration certificate) 277 Park Avenue ,.. New sk York. Nei* To 10017 v.. - _ .1. FOR FAA• USE ONLY - • .1 ' • • -• . • 4. UNIT IDENTIFICATION • 5. TYPE UNIT • MODEL .... . • SERIAL NO. • REPAIR ALTER- ATION AIRFRAME described in item 1 nestoon.onotomeneeteeen (As above)nomemennornohne POWERPLANT • PROPELLED • APPLIANCE TYPE MANUFACTURER 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B. KIND OF AGENCY C. CERTIFICATE NO. Executive Aircraft Service Division of Cooper Airn2otive P.O. Box 24889 Deltas, Texas 75224 U.S. CERTIFICATED MECHANIC • RS 3834 Radio and Airframe lir FOREIGN CERTIFICATED MECHANIC . (TIFICATED REPAIR STATION MANUFACTURER D. I certify that the repair and/or alteration made to the unit(s) identified in item 4. aboye and described on the reverse or attachments hereto have been made in accordance with the requirements of Part 43 of the U.S. Federal Aviation Regulations and that the information furnished herein is true and correct to the best of my knowledge. DATE March 14, 1975 • SIGNATU U RIZED INDIVID 7 -Li 7. APPROY L. FOR RN•TO SERYI Pursuant to the authority given persons specified below, thesinit identified in item the Administrator of the Federal Aviation Agency and s bia, APPROVED 3 4 was inspected in the manner prescribed by REJECTED BY FAA ELT. STANDARDS MANUFACTURER INSPECTIONAtm:Nut:nom . OTHER (Spacify) . . ... . • • - FAA DESIGNEE yr REPAIR STATION CANADIAN DEPARTMENT OF TRANSPORT INSPECTOR Of AIRCRAFT • DATE OF APPROVAL OR VES ECTa14, 1975 CERTIFICATE OR min. NO. SIGNA --F A ORIZED IVID / r.. t.e.., EFTA00278367

• FAA AIR:.CRAFT REGISTRY CAMERA .NO. L DATE; 1.2-" 12 - c?) Weight and, balande or operating limitation changes shat! .be -entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformity with the applicable airworthiness requirements. 8. DESCRIPTION.OF WORK ACCOMPLISHED (if mare space is required, attach additional sheets. Identify with air- craft nationaliti, and registration mark and date work completed.) 1. Installed three (3) VHF communications transceivers. Two of the twits are Colltne VHF-ZOB transceivers installed on the top shelf of the electronics compartment at F.S. 153. These two units function as the primary VHF conurautications system. The third is a Collins VHF-20B transceiver installed on the second shelf of the radio compartment at F. S. 170. This unit functions as a standby VHF system. The mounts for these units are attached to the shelf channels with four (4) each NAS 517-2 screws and anchor nuts- -__The_two primary transceivers are contr_olled by_dual Collins NCSL-31 systems -installed in the center commie. The third transceiver is controlled by a. Gables VC series control. Existing GAEC installed antennae are utilized witk -1410.1 and No. 3 transceivers sharing a conunan antenna. System wiring is shown on EAS drains° 180606 and 180607. Installed an H. F. conummicatione system consisting of the following: 1 each Collins 618T-3B Transceiver Leach Collins 4908-i Coupler 1 ascii 114E-03 Control The transceiver is installed at F.S. 139 on shelf No. 2 of the forward radio compartment. The'coup1er is installed per EAS drawing 680083 in the tail compartment at F.S. 682. The coupler installation is approved by DER SW 167 Walter T. Clark on FCRM 8110-3 dated 6-29-73. Complete wiring and mounting provisions for a second H.F. system were also installed. both systems will utilise the G.A. C. installed H. F. antenna. These systems are wired per FAS drawings 180454 and 180455. • Installed. dual Collins V1R-30 VCRALS receivers and 699Z-1 aia-drivers. The receivers are located on the top obeli of the radio compartment at F.F. 158.• They are installed in a dual mount attached to the shelf channels with four (4) NAS 517-2 screws and anchor nuts. The RMI drivers are located at F. S. 178 an the top shelf. They are attached with four (4) AN 526- 632 screws and anchor nuts per unit. The receivers are controlled by duet Collins NCS-31 systems. - System wiring is shown on EAS drawings 180602 and 180603. The Grumman installed VCR /LOC, glideelope and marker antennae are used for this installation. . _ evs.Weivttti%74..:.•tr ••" - • . . • - • . . . • : • .-------- — • . • . I. . • EFTA00278368

FAA AIRCRAFT REGISTRY. CAMERA NO. DATE: jO,— (2 -- &) Ogden Ameri‘Corporation 4 277 Park Avenue New York, New York 10017 ATTACHMENT TO FAA FORM 337 dated March 14, 1975 Installed dual Collins 51Y-7 AM..' receivers and two Collins 137A-6A loop antennas. The two receivers are located at F.S. 546 below the baggage compartment floor. The receiver mounts are attached to two (2) .063 2024T3 aluminum hat sections using four (4) NAS 221 screws and anchor nuts per mount. The hat sections are attached to the cabin floor panel using eight (8) NAS 221 screws and ppnrio-10/ S104D1032-08 Delron. fittings in the inboard channel and six (6) in the outboard channel. One loop antenna is GAEC installed. The second loop antenna is in- stalled in accordance with EAS drawing 68000Z which is approved on FAA Form 8110.3 dated 10-31-69 and signed by DER SW-167 Walter T. Clark. The top GAC installed sense antema is used for system No. 1 and the skeg sense antenna for ADF-2. The dual ADF systems are wired in accordance with EAS drawings 180610 and 180611. Both systems are controlled by the Collins NCS-31 systems. Installed dual Collins DME-40 interrogators on the top shelf of the electronics compartment at F.S. 145. The dual mount for these units is attached to the shelf channels with four (4) NAS 517-3 screws and anchor nuts. Dual Collins 339F-12 distancelground speed indicators are installed on the instrument panel using MSP 9963 clamps. The existing GAEC installed Collins 237Z-1 antennas at F, S. 172 and 228 are used for this installation. The DME systems are wired in accordance with EAS drawings 180604 and 180605. Installed dual Collins TDR-90 transponders using the dual Collins NCS-31 systems for control. The transponders are installed on the top shelf of the electronics compartment at F.S. 150. The dual mount for these units is attached to the shelf channels with four (4) NAS 517-2 screws= and anchor nuts. The existing GAEC installed antenna at. F.S. 562 is used for No. 2 ATCT.. A New Collins 237Z-1 antenna installed at F.S. 515 is used for No. 1 ATCT. This antenna is installed in accordance with EAS drawing 680061 dated 10-21-72. The dual transponder systems are wired in accordance with EAS drawing 180600. Installed dual Collins Al-T-50 radio altimeter systems consisting , of the following: 2 each Collins ALT-50 Transceivers 2 each Collins 339H-4 Indicators 2 each Collins 437X-1 Antennas 2 rach Collins 437X-1A Antennas One R/T unit is installed in the electronics compartment at F. S. 170. The mount for this unit is attached to the shelf channels with, four (4) NAS 517-2 screws and anchor nuts. I 7.... • ••••0 feta , f r. • ..141•=eL".74.2217..C•••••••••,...." • . - • EFTA00278369

• .:".11'• • EFTA00278370

(Cont'd) The second -8/T unit is installed at F.S. 550 R. H. side below the baggage compart- ment floor. The unit mount ie attached tc the bat sections of Item 4 above with four (4) HAS 517-2 screws and anchor nuts. The 437X-1A antennas are installed at F. S. 213 and F.S. 238 on GAC installed mounts. The 437X-1 antennas are installed per EAS drawing 680074 dated 1-4-73 and approved by DER Walter T. Clark on Form 8110.3 dated 3.7-73. The indicators are clamp mounted on the pilot's and co- pilot's instrument panels using MEP 9963 clamps, , The 21141 Loisit Ira et e r systems are wired per EAS drawing 18t 642. Installed an Aero Electronics Development :anuAkii.r ft Automatic emergency locate: beacon at F.S. 682 inside the fairing at the base of the vertical stabi- lizer. The installation is accomplished in accordance with FAS drawing 680066. Installed a J.E. T. AI-804 JG Standby Horizon and PS-823B power Supply. The horizon is installed in the instrument panel glareshield panel on the aircraft center line. The aircraft frame in this area was modified in accordance with FAS draw- ing 680060 dated 10-21-72 and is approved on FAA Form 8110.3 dated 10 November 1972 and signed by DER SW-167 Walter 1'. Clark. The power supply is installed at F.S. 165 on shelf No. 2 of the radio compartment. The system is wired in accordance with HAS drawing 180628. Installed a second Sperry VC-311 vertical gyro using existing GAC mounting provisions in the main wheel well area. The system is wired per EAS drawing 180599 and includes attitude switching. The attitude system is a part of STC SA 1553SW. Installed a Motorola NA-135 Selcal Decoder on sknaf No. 3 of the electronics compartment at F.S. 155. The mount for this Init is attached to the shelf equipmnat mounting channels using four (4) each NAS 517.2 screws and anchor nuts. System wiring is shown on EAS drawing 180456. Installed a cockpit audio system consisting of one, each Smith M-1035 YL and M-1035 YR audio selector/amplifier panels and two (2) each Jensen C613 speakers. The two audio panels are installed on either side of the center console. The two speakers are installed in the cockpit overhead per £AS drawing 680006. The system is wired per FAS drawing 180663. 5,: EFTA00278371

••.nt ••• • EFTA00278372

4.Oest.: FAA AIRCRAFT REGISTRY CAMERA NO DATE: I 0.- f .-.2 ) • .1 :to Ogden American Corpora$4,3:a.2 277 Park Avenue New York, New York 10017 ATTACHMENT TO FAA FORM 337 dated March 14,:1975 Page 4 Gm G-1159 S/N 151 N979RA 13. Installed a cabin paging and electronic chime system consisting of a Collins 346D-18 paging amplifier and ten. (10) each Jensen C6T3 speakers. The amplifier is installed on shelf No. 2 of the electronics compartment at F.S. 161. The speakers are installed and approved as a part of the interior installation. A Jensen C4T8 speaker is also installed in the lavatory for paging. This system is wired in accordance with EAS drawing 180660. 14. Installed a cabin entertainment system consisting of a Craig 3129 stereo tape player and Genave PSI-1 24 VDC to 12 VDC converter. The tape player and radio are installed in a cabin interior cabinet at F. S. 310 L. H. side. The cabinet installation and tape player and radio mounting are approved as a part of the interior installation. System wiring is shown on EAS drawing 180657. 15. Installed a Collins 54W-1C Comparator Monitor system. The monitor is located on the top shelf of the radio compartment at F. S. 161. The mount for this unit is attached to the shelf equipment channels with four (4) each NAS 517-2 screws and anchor nuts. The 914G-1 comparator warning controller is located in the center console forwaid of the power levers. System wiring is shown on EAS drawing 180623. 16. Installed VHF NAV and compass switching systems as detailed on EAS drawings 180597 and 180533. The transfer relays for these systems are installed on an aluminum licit section located at F.S. 777 on. the shelf No. 2 of the avionics compartment. The control switches are located on either pilot's instrument panel. Installed IDC 575-25850-309 MACH/Airspeed indicators for the pilot and co- pilot. These indicators are approved to TSO C-46 and have range and markings appropriate to the G-ll59 speed limitations. The instruments are clamp mounted in the L. H. top position of the basic "T" on each pilot's flight instrument panel using MEP 9963 clarnks. The existing pitot/static air lines are connected to the indicators. System wiring is shown an EAS drawing 180417. 18. Installed dual Sperry 2594620-908 servoed altimeters. The instruments are clamp mounted in the R.H. top position of the basic "T" on each pilatf0 The pilot's altimeter is driven by the Sperry 2587400-844 air data computer and the co-pilot's altimeter by the Sperry ADC-2OO altitude computer. These altimeters are approved to TSO C9 and ClOb and have a maximum range of 50,000 feet. System wiring is shown on EAS drawings 180608 and 180609. 19. Installed an Aero Mechanism 8047-10 pneumatic altimeter on the engine instru- ment paiiel. This altimeter is approved on TSO ClOb and is used as a back-up to the servoed altimeters. . . • ;.•.. 5 - . EFTA00278373

...;;;Qult.=:,•.;?;;* 7'7.1 - • :.!er . . : . tit.• . . ' .-....---.--- `,....f. _• ;..-...„.a.,:• - .,, ._ .....r ....... _.......--....‘....,...,........., __ ... - . . -7:• • , . !•• . . . •si . • I , .. ...:-.. .. . . - ---- — • -.2 - . -----::.._.:......::.-". i;:tv 4.- :Zt. --... '4...L.:V.'. . .... . • t• EFTA00278374

• Ogden America Corporation. 277 Park Avenue New York. New York 10017 Page 5 Grurnt.an G-1159 S/N 151 Nri 9RA ATTACHMENT TO .FAA FORM 337 dated March 14, 1975 20. Installed dual L'Sno NIB digital clocks, one located on the outboard side of each piatotia panel. 21. Installed dual Teledyne Model ream IY&I indicators approved to TSC G83. The instruments are clamp mounted on both pilot's flight instrument panels and are connected to existing static lines. 22. Metalled a Lear Avis 800134F synchroscope on the L. H. engine instrument Eanel. System wiring le shown on FAS drawing 180582. 23. Relocated TVI indicator and selector switch from overhead panel to engine instrument panel. Relocated C.A. T. indicator from main instrument panel to overhead panel. 24. Removed tae existing Bendix 39B153-1-A instrument inverter and replaced with a Flitetronics PC-17A. This change increases instrument inverter bus cafracity from SOOVA to 750 VA. The inverters are approved to the same TEC. Wiring modifications ace shown on EAS drawing 180470. 25. Installed a wire rotting trough along the inboard edge of the R.11. cockpit side console. Lostallution is shown on FAS drawing 680016. 26. Removed Grumman installed elttctronice junction box and replaced it with a smaller junction box in the top section of the radio compartment. The new box is constructed using .040 2024T3 aluminum panels nicking up the Cirturman installed fasteners. Deutsch terminal blocks are mounted on the new tanels. 27. Installed an auxiliary electronic compartment blower on shelf No. 4 at F.S. 155. The blower is a Joy Mfg. Co. Model AVR-45-30t714 PIN X702-137B. The blower le wired in accordance with EAS drawing 180429. 28. Installed an Airpathe CBZLOO-T6D magnetic compass in the GAC installed cornpass =oust. 29. Installed a Bendix RDR-1200 -weather radar system consisting of the following: 1. each Bendix AT-120/A R/T I each Bendix IN-1202A Indicator I each Bendix DA-1203A Antenna Drive 1 each Bendix AA.-1218A Phased Array (18") - • • EFTA00278375

. • • .. . . r—• • •••;-: . -:.' Z.,: caC"--"*• • ' •-:' 4 ,,••-•••••a•!•#!•••••rae-aneThryagdi __L . 4. . • . ' • • . . . . . . . : • •• • . . . . .• • - ........-- t............„_••••:c.. ..7: , _„4 . • 4.••••••:•,: .—.... : .;•:.„,.-......r,_ _ ,44.42,.....-.,.:•:,. • „. . ...., .• •• O P : • ••••• •••••• • .•• ••• • •C; .• • •. •• • Z a • EFTA00278376

-•;,)-7:47. The antenna driveand phased array are attached to the existing CAC installed antenna mount at F.S. 43. The R/T unit is attached to a shelf installed per STC SA1193SW at F.S. 36. The indicator is installed in the center instrument panel. The system is v=ired per EAS dreNt-ing 18(1495c Installed deal Collins ¶3-169Y flight director sys&n-ts consisting of the following: 2 each Collins 2 each Collins 2 each Collins Z each Collins 2 each Conine 2 each Collins 2 each Collins 329E-8Y Flight Director Indicators 331A-9C Course Indicators 161E-2A Mode Coupler 562A-5M Computers 614E-22B Remote Controls 614E-23R fode Selectors 345A-7 Turn Rate Sensors This system is installed in accordance with STC SA1057SW except that the it-emote instrument amplifier is eliminated ant; all servo amplifiers incor- porated in the later model instruments. Iz wiring variations are in accord- ance with manufacturers required equipment interconnect. Collins Radio Company pilot's guide for the FD-109Y/FD-109Z integrated flight system is a required part of this installation. System wiring is shown an EAS drawings 180658 and 180659. Installed a radio maste? system wired in accordance with EAS drawing 180581. The master relay is installed on the outboard side of shelf No. 2 of the radio compartment at F.S. 160.. A master switch is installed on the aft end of the center console with an override switch on the co-pilot circuit breaker nand. Installed a Flitetronics PC-164 115VAC 60 Hz static inverter on the cabin floor panel at F.S. 579 below the alt baggage sub-floor. This inverter provides power for the cabin 60 Hz AC system. Installed mode ar-st;aator system for the autopilot on each pilot's instrument • •• • 7•••..„.0 . Hoe . . • •• • • , . • • . • ••• ••.. • . • • • - • - . •• - • • ••- ••••••-..:;• • • ••.: • . . •. •••:. • • • . • EFTA00278377

EFTA00278378

- jot. • 3, • each Global 10050-1 ACV 'I each Global 10060-2 CM .1 each Global 10045-1.OEU . 1 each Global 10085-1 Antenna The RCU and oru are installed on the third shelf of the radio compartment at F. S. 170. The ant." is installed at F.S. 139 per FAS drawing 680086 and is approved by DER SW 167 Waiter T. Clark on FORM 8U0. 3 dated May 3, 19-(4. This system is wired per FAS drawing 180598 and is installed on a "NC HAZARE" basis and is placarded as follows: Installed a Safe Fligizt SCAT system in accordance with STC SA722FA. Flag t Manual Supplement dated 5.5-72 inserted in AFM. A Safe Plight 6002-1 approach indexer control and two 965-0U3-003 indexers vr<,re added to the SCAT system fast/slow output to provide ii- heads up display of the flight director fazt/slow indicator. The Indexer control is installed on shelf No. 1 of the electronics compartment at F.S. 169. Installed an 1DC 18495E SAT/TAS Indicator with a Rosemount 107.h.7.11AF probe in accordance with SIC SA1057SW. Flight Manual SuppleMent dated 10-29-69 inserted in AFM. Installed a Collins INS-61E i3ertial navigation system in accordance with SSG SA15535W. Flight Manual Suppternent dated 11-15-72 inserted in AlLs,f. Installed Soerry ADC-200 altitude computer and 2593564-910 altitude pre- select system in accordance with STC SA1861SVir. Flight Manual Supplement dated 3-26-74 inserted in AFM. " EFTA00278379

-Jo ..-4•• rt • % • EFTA00278380

. . • Wiring ins tatl i by Executive Aircraft Service, Inc., fcr the show: systeu--,s conforms to MIL-W-5086 or MIL-W-16878 and Is.installed in accordance with AC 43.13-1, Chapter IL and AC 43.13-2, Chapter 2. Al structu . rel. attachments and installations required for the above systems are in accordance with applicable evictions of AC 43.13-2. A functLonal check of the equipment listed on this form has been nerforrned in accordance with FAR 25.1301 and h operated satisfactorily and did not affect any other aircraft system adversely. EFTA00278381

• •••+: *wt. 01+ 0 • .. EFTA00278382

- • ,• — vs -penned • FEDERAL A`" 'ION AGENCY k... :2.4-„xi• .fi nwst No. 04-R000.1 . MAJOR REPAIR-AND ALTERATION • ., i:/it FAA USE ONLY ' . . (Airframe, Powerplant, Propeller, or Appliance} • OFFICE IDENTIFICATIOdaq. GADQ • . SPI-GADO•2 4/ c? ' • INSTRUCTIONS: Print or type all entries. See FAR 43.9; FAR 43 Appendix B, and Ac 43.9-1 (or subsequent revision thereof) , for instructions and disposition of this form. MAKE • • - mom Q1159 1. AIRCRAFT SERIAL NO. - . 151 --°--- NATIONALITY AND REGISTRATION MARK 979RA " . 2. OWNER NAME (As, shown on registration certificate) • Ogdaa • kaar Loan Canketak ion ADDRESS (As shown on registration certificate) 277 Park Ammo New York, Sew York 10017 . 3. FOR FAA USE ONLY . • • . --.. . • le -fthililt:V..": itl:taifiz,:! iltrein UST,:r:E1•with ariini.te :it- • itW,trt:3 %;,:irEcthIs 27..1 is z,-.;:tued evil ft% ;he acredis7 ' •.: .1 ttitzi :Itzitit s:r.!:•:t te czarcity long:lion a-, s* rahtirize! in RS 43.7. /- ' --• I ..-- 6 • . . bp at Incerinr LWCA •' 4. UNIT IDENTIFICATION S. VE . • . 9,411.. MODEL. SERIAL NO. REPAIR I . ALTEE, ATION AIRFRAME ' . • ••••••••••4t*.***••••••• (As described in item 1 above) . XX .. _. POWERpLANf • • - - . _ . ' . PROPELLER .. • • TYPE - APPLIANCE MANUFACTURER - - 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B., KIND OF AGENCY C. CERTIFICATE NO. Cooper Airmotivee , Inc. • U.S. CERTIFICATED MECHANIC MS 3834 Executive A.Lrctratt iluntice.Dit., Ft:imam CERTIFICATED MECHANIC • Aiirfreme Reilt•ird Airpirt . X CERTIFICATED REPAIR STATION • Limited Dallas texas 75232 MANUFACTURER Ratings' . D. I certify that the repair and/or alteration made to attachments hereto have been made iv accordance with 1 - and that the information furnisbed herein is true. and the unit(s) identified in item 4 above and described on the reverse or the requirements of Part-43 of the U.S. Federal Aviation Regulations correct to the best of my knowledge. DATE February.19"1975 , SI TURE O AUTItORIZAD INDIVIDU • • • • - t v„...--10. (t. a • - ''' eck D. A . 7. APPROVAL FOR RETURN TO SERVICE " Pursuan to the authority given persons specified below, the identified in item 4 was inspected in the manner prescribed by the Administrator of the Federal Aviation Agency and is lalIW pia'tPPROVED • REJECTED BY FAA. RT. STANDARDS frisPEcroi! • MANUFACTURER INSPECFOI AUTHORIZATION :r OTHER (Specify) FAA DESIGNEE .... A . REPAIR STATION • ' eir : CANADIAN DeARTAUNT OF TRANSPORT. TRANSPORT. INSPECTORR dr Arilauen - DATE OF APPROVAL OR REJECTION March 12, 1975 ainga t ig io DES; RS3834 clit.t.) ..,.obtu5v . .,c 4 --arts.,k_, IDUAL P-44-,aL...........: , . ••••:: . . . . - _• • .• - EFTA00278383

FAA AIRCRAFT REGISTRY ..'31.1E4A DATE: .19,- ) Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. An alteration must be compatible with all previous alterations to assure continued conformlty with the applicable airworthiness requirements. 8. DESCRIPTION OF WORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with air- craft nationality and registration mark and date work completed.) a. Completed interior installations and service equipment in accordance with'drawings listed on dtawing list #386789 (1 Sheet) dated 2-6-75, Structural appioval and approval of oxygen system deviations 12 FAA Form #8110-3 dated 19 Feb. 1975 by DER °W-167, Walter T. Clark, Jr. b. Installed electrical circuits as shown on drawing 3 525 (47 Sht, dated 7-23-71 in accordance with advisory circular #AC43-13-1, Chapter 11, section 2,3,4,5, & 7. The total DC electrical load increase on this aircraft by above circuits is 56.15 amps. The total DC load, less radio and electronics is 330.48 amps. The aircraft is equipped with two (2) 300 amp generators. Functional check of all items installed as shown on this FAA 337 Form had no adverse effect on other systems in this aircraft. The electrical circuits installed to meet the intent of 41).606 (a) & (b) and 4b.615 (a) , (b) (c). c. Weighed the aircraft and computed EW and MCCG and prepared a sample zero fuel weight loading in accordance with Grumman Weight & balance repctt t4T -11598 for aircraft S/N 151. d. Made emergency lighting check in accordance with AC20-3~A dated 2-8-66. e. Tri::and interiOr materials used in this instaliation meet the flame resistant requirements of 41).381 (b). f. The baggage compartment is lined with fire-resistant material to meet the requirements of 4b.383 (b) EFTA00278384

. .. .. . . . - .. . ..- • ',...: .. • • . . .-.... . • .:...----.7S‘............:*......atlit...:..............-..4-...L. --.4.i.- , -:•-...:-. ----.-.7•••-•-•--4.-.L..- - - OEPARTmEt, ir TRANSPORT."-TION FEDERAL AVlicflON ADMINISTRATION • STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS 19 Feb. 1975 - AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE .' • MODEL NO. GrumMan G1159 TYPE (Airplane, Radio. Helicopter. 0,0 • Airplane NAME OF APPLICAN Cooper Airmotive Inc.ExecutiN tarcraft Service Div. LIST OF DATA .7- ... : IDENTIFICATION TITLE 386403 (2 Shts) 386776 (2 Shte) 386507 (Shts 1&2)Air 386409 (Shts '3,4 386687 (1 Sht) 386676 (I Sht) • 386640 (1 Sht) 386627 (2 Slits) 386586 (1 Sht) 386779•(1Sht) 386730 (1 Sht) ' 386781 (1 Sht)'.. 386778 (1 Sht) ' 386132 (Slit 8) 286777 (4 Slits). 386643 (1 Sht) 386680 (1 Sht) 386684 (2 Slits) 386636 (1 ShtYl 386786 (1 Sht) 386774 (3 Slits) 386701 (1 Sht) . 386791 (1•Sht). Headliner support structure. (11-26-69) Ledge and side panel structure. (11-20-74) duct support structure (5-24-71) '. &5) Air ducts and reading lights (12-3-69) Air duct deviation. (1712774) , . Speaker brackets (12-15-73) • • Blkhd. retainer FS181 LH.(4-3073) Blkhd. retainers FS200 Lk & RH. (3-14-73 Bulkhead retainers FS496 (11-20-72) FS181•Bhd. LH (11-26774) FS200 Bulkhead LH (11726-74) Bulkhead FS452 L&R. (11-27-74) / Bulkheads L&R FS496. (11-26-74) Bulkhead Patterns (11-26-68) Crew service compartment. (i1—S-74) Wire routing double installation. (5-12-7.3) Aft cabin door 'frame at baggage. (12-27-73) Aisle doors. (1-9-74) ' Fold up desk. (4723-73) '• - 'Divan fwd. arm cabinet LH. (1-28-75) Service cabinet .‘(11-11-74) . . P*48 . . Game. table ins all tion.(2-5-74) Chair track installation (2L11-75) !'Ilte*OSE OF DATA . . To install interior items for Field Approval. . . . APPLICABLE REQUIREMENTS (14•1 specific sections) 4b.200(a), 4b.201,4b.210(a).,4b,211,4b.260,4b.306,4b.307(c) . 4b.358,4b.359,4b.362,4b.381,4b.382,4b.651 '(b) (3), 7 - % . . CERTIFICATION • Under iuthcrity of appointment under Part 183 1 of 3 ' have vested by direction of the Administrator and in accordance with conditions and limitations of the iceLerdl Aviation Regulations, data listed.above and on attached sheets numbered been examined in accordance with estirblihed procedure's and found to comply waft -applicable Regulations.' . . approval of these data these data • • requirenients of the Fedeial Aviation • RecomMend I (We) Therefore fl Approve SIGNATUREfS) OF DESIGNATED ENGINEERING RE.PRESENTATTIM DESIGNATION NUMBERS(S) - CL ASSIFICATION(S) ?,.,r/ c ... (-2-)e,1 SW-167 Structural and Oxygen systems. F.i.pi OLAVRAi • .. • • - FAA Form 8110.3 (11-70) SUP., RSEDES PREVIOUS EDITION ..• - t•••‘a • sAMILI.,.:r." •• ••4 •-:.•••;:••%1 ;"7:..... 4-••••.+4.41 .4 1 : 4 ft " • • : ; Tr : • . . -•-- . - ................-..,„ ,. ....... . -.. e. ..i. • •- a. - .....:...-LL.....:1- .S...................a......1......................... .a-.... .,...... EFTA00278385

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FAA AARCRAFT REGISTRY CAMERA NO. L DATE: ta- ! . , • • OEPARTmEt • F TRANSPORTATION ...., .• FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGUL.A1;ONS OATS 19. Feb. *35 ...‘ AIRCRAFT OR AIRCRAFT COMPONENT IDENTIFICATION MAKE - t . Grumman MODEL HO. *.G1159 TYPE (Airplenes, Radio, Helicopter, "Wirplane • 0 NAME OF APPLICANT Cooper Airmoteive Inc. Executiy Aircraft service Div. . LIST OF DATA ,LiENTIFICATION TITLE • 386720 (1 Sht) 386426 (2 Slits) 386694 (1 Sht) 386783 (1 Sht) 386120 .(1 Sht) 36E254 (1 Sht) 386765 (3 Slits) 386746 (3. Slits) 386767 (2 Slits) 386633 (2 Slits). 386775 (3 Slits) 386668. (3 Slits) 3866E6 (1 Sht) 386737 (1-Sht) 3.86685 (6 Chts) 38656 (1 Sht) 386500 (2 Slits) 386702 (2 Slits) 386441 (1 Sht) 386553 (Shts1,2 386679 (1 Sht) . 386637 (1 Sht) 386401' (1 Sht Power shield door (4-9-74) . Emerge exit handle rework (12-19-69) • Escape hatch handles (1-24-74) Two & Three place divan inst'l. (1-21-75) Chair installat'on provisions. (11-11-68) • Entrance door c4tain. (5-14-69) CommissarY.LH° (10-10-74) Commissary RH. (10-10-74) • t.. . L&R commissary support structure. (10-11-74) Water heater & bracket.(4 .-11-73) Pressuriied water system. (11-19-74)- Lavatory & vanity. (11-9-73) ' - . Lavatory support structure (1-11-74) Air lay deviations. '(6-27-74) Aft baggage (1-19-74) Smoite detector & amplifier. (4-15-68). Law.tory floor mod. (5-10-71) _Radio. rack doors. (2-8774) FS540-572 floor board mod. (1-49-74) 7, ,4&5) Continuots flow oxygem system (9-5-72). Continuous flow oxygen, system. (12-27-73) . Continuous flow oxygen system (4-24-73) Cock it ste manual storage (11-26-69) PURPOSE OF DATA 0 . To install interior items for Field Approval, APPLICABLE REQUIREMENTS (List specific sections) • 4b.200(a), 4b:201,4b.210(a),4b.211,4b.260,4b.306,4b.307(C) 4b.358,4b.359,4b.362,4b.381,4b.651.(b) (3). CERTIFICATION • Under authotity -vested of appointment under Parr 183 2 Of 1 - have by direction of the Administrator and in accordance with conditions Ind limitations of the Federal Aviation Regulations, data listed above and on attached khects tostbered _- been examined in accordance with established protares and fuund to comply with applicable Regulations. • approval of these data these data requirements of the Federal' Aviation t (We) Therefore El Recommend 0 Approve SIGNATUREIS/Pr DESIGNATED ENGINEERING REPRESENTATIVE,lj DESIGN A.TIOK NUMBEIZRS) CLA$SIFICATION(S) 77-77-- ---) .7- :. -; SW7167 . Structural and. prygen qyqtramq FAA OtT/CIUML 4---..zrea.a!Vavartroorav--avv.,c;te7: •vt./ -7. • ..- .I' 4. ' • . • • • 't ; -7 EFTA00278387

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• DE0 ARTMEt. .F TRAN3PORTATION \_ . FEDERAL AVIATION ADMINISTRATION STATEMENT OF COMPLIANCE WITH THE FEDERAL AVIATION REGULATIONS DATE • . ' 19 Feb 1975 AIRCRAFT OR-AIRCRAFT COMPONENT IDENTIFICATION MAKE Grumman MODEL NO. 61159 TYPE (Airplane, Recife, Helicopter, NAME OF APPLICAN TI:(DOper oft° irmotive Inc. Executit Airplane #ircraft Service Div. . ..- LIST OF DATA • - - IDENTIFICATICo - • . • •- TITLE 386688 (1 Sht). 386782 (1 Sht) 386554 (6 Shts) 386592 (1- Sht) 386551 (1 Sht) 386665 (1 Sht) 386569 (1 Sht) 386580 (1 Sht) 386566.(1 S)t) 386515 (1 Sht). - 386593 (2 Shts) 386758 (1 Sht • - 386539 (1 Slit) . 386761. (1 Sht) 386 NOTES: .• . . . Desiccant .installation '(1-14-74) - Tow bar.storage, (1-4-75) , . . - • • L&R•aux. engine oil full system. (96-72)• Pre-fill pump installation (11-29-772) - APU interlock switch. (8-23-72) Utility box. (11-5-73) Cockpit'portable oxygen bottle inst'l. (10-27-72) Entrance area floor mod. (11-4-72) Wheel Well.lights (10-13-72) Overboard drains. (6-9-71) ---- • Aux. landing lights LH & RH (11-29-72) Oil gauge sight door alteration. (§-7,-74) Jack pad -stofege.. (7-27-71) Access inst'l. starter & H.P.cock. • . . 1. This approval- is for the structural substantiation , and oxygen system only. 2. This approval does not include the electrical system- approval. . 3. This approval is for Grumman Model G1]59. S/N 151, N979RA - 4. Aircraft released fozYservice by rAA Form 337 dated 19 Feb. 1975 by RS3834. ' PURPOSE OF DATA : . ' To install interior items for Field approiral. .., APPLICABLE REQUIREMENTS (List specific sections) . • 4b.2OO(a),4b.2O1,4b.21O(a),4b.211,4b.26O.4b.3O6;4b...3O7(c) 4b.358,4b.359,4b.362,4b.381,4b.382,4b.651 ,(b) (3). , • CERTIFICATION - Under authority vested by direction of the Administrator and in amprdance- with conditions and limitations of appointment under Part )83 of the Federal Aviation Regulations, data listed above and on attached sheets numbered _ 3 of 3 • have been examined in accordance with established procethres and found to.comp!y with applicable requirements of the Federal Aviation Regulations. • 1 (We) Therefore 0 Recommend approval of these data' • Approve these data SIGNATURE(S) OF DESIGNATED ENGINE ERIN.; REPRESENTATIVES/ DESIGNATION NUMBMS) CLASSIFICATION(S) --- . ..-- - .)77:- -SW-167 Structure' and OxYgen systems. FM ORIGIN4L. • .. . - - , FAA Form 811a3 (11-70) SUPERSEtFa PREVIOUS EDITION - ' •57._ ,A35 : • . . . • • • . • - • EFTA00278389

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va frfrro FEDERAL A'— VON AGENCY • 1 s a red trket Bureau No. 04—R0604 MAJOR REPAlk-AND ALTERATION i FOR FAA USE ONLY (Airframe, Powerplant, Propeller, or Appliance) I OFFICE IDENTIFICATION . . INSTRUCTIONS: Pnnt or type all entries. See FAR 43.9, FAR 43 Appendix B, and AC 43.9-1 (or subsequent revision thereof) for instructions and disposition of this form. 1. AIRCRAFT MAKE • Orman MODEL G-1159 ..... SERIAL NO. 151 NATIONALITY. AND REGISTr.ATION MARK N979RA • 2. OWNER NAME (At shown on registration certificate) Ogden AzOrican Corporation • ADDRESS as shown on registration certificate) 277 Park Avenue . New York, New York 10017 3. FOR FAA USE ONLY • is • . . • . . . • , . .. . _ - - 4. UNIT IDENTIFICATION S. TYPE UNIT MARE MODEL SERIAL NO. - - . REi'AIR ALTER- AVON AIRFRAME . gai• nkneenommenewsee(.4i:described in item I above)••••••••emomoonnamoe P6WERK.ANT . • ••• .. - PROPELLER . . . TYPE APPLIANCE. MANUFACTURER • 6. CONFORMITY STATEMENT A. AGENCY'S NAME AND ADDRESS B. KIND of AGENCY • C. CERTIFICATE NO. Cooper Airmotive, Inc. E U.S • CERTIFICATED MECHANIC 119 . 3834 Executive Aircraft Service, Div FOREIGN CERTIFICATED MECHANIC Airframe Redbird Airport - X CERTIFICATED REPAIR STATION • Limited Dallas, Tens 75232 MANUFACTURER Rat inge D. I certify, that the repair and/or alteration made to. attachments hereto have been made in accordance with and that the information furnished herein is true and the unit(s) identified in item 4 above and described on the reverse cr the requirements of Part 43 of the U.S. Federal Aviation Regulations correct to the best of.my knowledge. C.4.TE March 12, ...975 SIGNATURE Of AlcHORIIp INDIVIDUAL "Ac„ga A ,-; 4. OLS—k-AL..c se's:V9- Gaston D. Alexander 7. APPROVAL FOR RETURN' TO SERVICE Pursuan to the authority given persons specified below, the unit identified in item 4 was inspected it: the manner prescribed by the Administrator of the Federal Aviation Agency and is ICIS.PPROVED O REJECTED BY FAA RT. STANDARDS INSPECTOR MANUFACTURER • INSPECTION AUTHOWATION OTHER (Spicily) FAA .DESIGNEE X . REPAIR. STATION CANADIAN DEPARTMENT OF TRANSPORT TI4SPECTOR OF AIRCRAFT DATE OF APPROVAL OR REJECTION . March 12,. 1975 CERTIFICATE OR ; DESIGNATION NO RS 3834 SISNATURE OF ARTH9111.Fp, INDIVDIUt 4,07Lig... ,.....A.). LA.Leffa-Nn_ • Gant= D. Alexander FAA Form 337 (1-65) OBSOLETE PREVIOUS EDITION • -.•••- ••••-•.? , ........... . - . • .. • .. -•:.-_-:,. • ,.. ..; : • . .. .. ., . .., ... ..... . _ .; -.....- • 0052-025-8000 • (8320) EFTA00278391

Weight and balance or operating limitation changes shall be entered in the appropriate aircraft record. Art alteration Must be compatible with all previous alterations to assure continuec 2onformity with the applicable airworthiness requirement:. 8. DESCRIPTION or iVORK ACCOMPLISHED (If more space is required, attach additional sheets. Identify with air- craft nationality and registration mark and date work completed.) a. Installed interior emergency lighting system as shown on Cooper Airmotive, Inc., Executive Aircraft Service, Division drawing #396218 (13 Sheets) dated 3-25-69 Rev. "A" dated 6-30-69 approved by STC #SA1037SW. BAS FAA approved Flight Manual Supplement #3 dated June 23, 1969 applicable to this allteration. b. Installed Page Gulfstream II cockpit jump seat approved for use during take-off or landing in accordance with STC #sA1918SW;. Oxygen supply. for this seat installed in accordance with-STC #sa5tisw . NOTE' 1. Long range oxygen supply, Two (2) 114-9 cubic feet each, installed in this aircraft. Passenger and Long Range oxygen system approved by STC #SA951SW and FAA form *5110-3 dated Feb. 19, 1975 by DER SW-167, Walter T. Clark, Jr. reference 337 form dated Feb. 19, 1975. 2.- Flight Manual Supplement #II dated April 25, 19,69 applicable to this aircraft. c. Installed insulation inside the fuselage from sta. 111I1 to pressure dome as shown on Drawing *38681 (1 Sheet) dated 8-21-68, except for the aft side of the pressure dome, which was installed by Grumman Aircraft Company, The Grumman Gulfstream II Specification #AE-159—I -21 Section "C" datdd 11-15-67 used as a guide for installation. d. Relocated the APU speed logic control unit in accordance with STC *SA2512wR. . e. Installed BKM Master Warning Interface device between master warning control panel and aircraft inputs according to RKK drawing list #EKM1000 -501 and STC *SA1613SW dated March 1, 1973 Rev. 1 dated Sept. 5, 1974. MOTE: The warning bell is not installed. f. Installed oil tank sight gage float in accordance with STC *S8994EA. EFTA00278392

FAA AIRCRAFT REGISTRY CAMERA NO. L DATE: 10-- ..OGi,P..'N AMERICAN CORPORATION " :' • . . - 277 Park Avenue • Page 11 New York, New York 10-1.7 . ', ) • ; GRlit.7.‘AN• dULFSTREAM II SIN 151 N978RA WEIGHT AND BALANCII DATA FM --- _ .. . JIG POINT DISTANCE FI' & IN. IN; a i b " I i_ a-b , i . / 0% MAC 100% MAC I PIT. 28 Cooper Airmotive Exec: Aire. Serv.• Div. DATE March 8, 1975 W.O. 215 VERT DATUM (WLRDE) MAIN GEAR HORIZONTAL ARM = •a. +.15. OD INCHES NOSE GEAR HORIZONTAL ARM = (a-b) = N MOIL ARM IN INCHES) INCHES 0,11. S13) 1,4728 C. G. IN PERCENT M. A. C. NOTES 1. All C. G. 's arc for the. airplane with landing gear extended. 2. A'reraft should be level (FRL =.0°), doors and windoWs closed, brakes released, and flaps and thrust reversers retracted, "when weighing. AIRPLANE ON WHEELS WHEEL, LOCATION • GROSS TARE ERRQR TOT. A NEVT LEFT MAIN , IjOR. ARM ' MOMENT , -----. RIGHT MAIN ...------ --.- SUBTOTAL MAINS NOSE TOTALS i I AIRPLANE ON JACK PADS SCALE LOCATION GROSS TARE 'ERROR TOT. A NET . NOR. ARi.] MOMENT LEFr WING 16,460 -2 -2 16.458 RIGHT WING 16,470 -9 • -9 16,461 _-_:›-_____ SUBTOTAL WINGS • 32,930 32,919 489 il 00 4,097,391 ' NOSE 2,365 +8 +8 .2,373 120 !10 2 84,997 TOTALS 35,2951 _15.292 -464 ; 19 11087,38A - EMPTY WEIGHT & C. G. DETERMINATION ITEMS WEIGHT C. G. IN HOR. ARM C. G. IN % M. A. C. • MOM ENT TOTAL ACTUAL NET TOTAL ADDITIONS ' TOTAL SUBTRACTIONS see .page March _8. empty weLcsht At equipment 11.1A dated 1975 for computation included_ in — — ----•''----- •— the empty weicrh:. . EMPTY WEIGHT WEIGHED BY: WITNESSED BY: Grumman Amkrican Aviation Corp. • EFTA00278393

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( FAA AIRCRAFT REGISTRY LiAMERA DATE: 1O,- 12- ;5 OLDEN AMERICAN COIIPORATION 277 Park• Avenue. . GRUMMAN GULFSTREAM II. 4 • New York, New York, 10017*. S/N15I N979RA • ACTUAL WEIGHT AND BALANCE AS WEIGHED Division • Page I1.1A 3-8-75 W.O. 215 COMPUTATIONS TO SHOW AIRCRAFT EMPTY WEIGHT ' Weight Aircraft. Scale-reading* 35,292: Uflusable fuel (drainable) 104 Ehgine Oil - , -56 Cooper Airmotive Inc? Executive Aircraft Service Undrainable•fuel in •tanks' (16 .lbs) and fuel in lines from tanks to engineS (44 lbs.) included in the scale reading. rile:above empty weight included equipment added by Cooper Airmotive, .Inc., Executive Aircraft Service Division listed below including radio and electronics. .Items Weight and/crnot-weighed: 1. Utility bOx. 2.. Engine oil pump system (full). 3. Hyd. oil pump (empty)..-'..' Tow bar - Baggage compt. cpthplete„. EAS water system (empty). First Aid Kit. Lavatory complete. • . a. "Air-Lav" 125-Serviced. b. Vanity. c. Mirrors (2). d. Fire Ext. CO2. e. Wardrobe & curtain. Commissary complete:- a. - (1). b. Tray Carriers Hot cups (1). d. Ice Bpx e. Coffee.Maker. Divan (3 pl. & 2 .Place).• Seven single chairs. Three fold-up tables. Three aisle doors. Fold-up desk (3). Service Cabinet °Aid-cabin a::Tape player.. b. Storage & phone Cabinet'(1) (divan Radio rack. doors. Fwd. Wardrobe. & curtain. . Fire Ext. (water).-:. Portable oxygen (sp). • ••••••••‘• t • . -4:1•••11;fiil •-••••••“.• . • r • -leg.•••• _ •-•.• . .••• : • . • • :21. 22.. 23. v 24. • 25. 26, 27. 28. 29. 30. 31. 32.* 33. .34. 35: 36. .37. 38. 39. Crash axe. Crew service & compt. (complete Long range oxyg. (2) Passenger oxygen (3) Jump seat (Pa4S). Fire ext. CO2 (CP) Crew.seats. Crew 92 masks. Manual holders. Step storage (CP). Radio Complete. • Fuel drained. Engine oil full. Emergency lights .& battery. Batteries installed (a/c). Entrance door curtain. Spare Apu Speed logic box. Eng..plugs Jack pad box (Pees Out). • • • • • ▪ ' 9 • woe- • • • • • ' • • • • • • . nt • EFTA00278395

• . i smga: trx,,,no or- , -ragaile Si sine va.:44: . —... ---- a- 7-- • ..,-- •-• ......; i . r ........ 7-•••••-...-:•., i'•-•-- • •.-- . - • . .. . . '..t :- . • ... ., • • ' i r 'A ‘ ' • • • .... EFTA00278396

•,... ......- . . - OGDEN AMERICAN CORPORATION ' - Grumman 'G1159 277 Park Avenue ' S/N 151 jN979RA New York, New York 10017_ :--'.' i- viarch 8, 1975 .‘„ ) • `_..4.O. 215 SAMPLE LOADING. FOR ZERO FUEL WEIGHT CONDITION #1: Ferry Flight with Crew of Two (2) Item Weight- Arm ,Moment . . Aircraft Empty Weight 35,340 463.95 16,396,292 40.61% MAC Engine Oil 56 554.00 31,024 Crew (2) 340 113.00 38,420 Crew Kit 50 113.00 5,650 Zero Fuel Wt,= crew 2 35,786 460.27 Baggage . 600 565.00 CONDITION #2: Loading for 3 Crew & baggage ZFW - 2Crew &R.e.ggage • 36,386 462.00 . Jump Seat 170 142.00. Baggage 250 565.00 ZFW-3 CrewNt Baggage 36,806 461.22 16,471,386 38.11% MAC 339,000 16,810,386 39.29% MAC 24,140 141',250 16,975,776 38.76% MAC CONDITION #3: -Loading forlPassengers & supplies (Passengers aft to fwd.) ZFW -Crew 2 35,786 46C 27 16,471,386 38.11% MAC Crew Baggage '(.2) '60 565.00 Lavatory. Water (10 gal.) 80. 544.00 Lavatory Supplies 20 .519.00, Galley SupplieS 100 474.00 Galley Supplies 100 474.00 Crew Galley ., 40 190.00 Utility Box .(aft' 100 745.00 , ZFW - 2 Crew& Supplies • 36,286 .,....x Passenger D5 170 433.00 Baggage . 30 565.00 ZFW — Pass. (2 Crew) Passenger R5 '..Baggage ;.. . • ". • . • . 3?,900 43..250 10,380 47,400 47,400 7,600 74,500 461.21 16,735,816 38.75% MAC 73,610 36,486 461.17 16,826,376 38.72% MAC 170 420.00 71,400 30 565.00 16,950 EFTA00278397

FAA AIRCRAFT REGISTRY 'CAMERA FO 0.- DA : 1 ic-.71- * 12 - Zr••••ictlr" . ' ...;OS!...••••••••117. 'I T: Ilaiallirle a,•" .ciai ll.r. 1 4r1••111rafai• • •-.•••,4r .• " r • .. . • .MIIII•••••••• •••••••.••••••• , •••••••••.”••••am. l'•••=1•••• ••••• •••••••• ..• ••• •!•.=••••.••. ,.••• ••rii....• • ..••..MM. • =••. • •••••••••.. , ••••••i•••,•••••••.. • . • EFTA00278398

p AA AIRCRAFT REGISTRY cI CAMERA NO.0.- • DATE: 10--"I ' J OGDEN AgERICAirabilPORATI0N.--- - 277 Park Avenue New York, NeW York 10017, Item Grumman G1159 S/N 151, N979RA March 8, 1975 I.O. 215 SAMPLE LOADING FOR ZERO FUEL WEIGHT ZFW - 2 Pass. (2 Crew) Passenger D4 Baggage • - ZFW - 3 Pass. Crew) 'PaSsenger D3 : Baggage ZFW -.4 PasS: (2 Crew) Passenger R4 . •Baggage• ZFW Pass. (2 Crew). Passenger R3 Baggage ZFW - 6 Pass. ( 2 Crew) Passenger D2 Baggage ZFW - 7 Pass.. (2 Crew) Passenger D1 Baggage ZFW —8 Pass. (2 Crew) . . • Passenger R2. • Baggage ZFW -9 Pass. (2 Crew) ' Papsenger.R2 Baggage ZFW - 10 Pass. (2 Crew) Passenger R1 Baggage ZFW - '11 Pass. (2 Cre1 Weight 36,686 170 30 36,886 -170 '30 37,086 . 170 30 Arm 461.06 407.00 5r,5.00 460.90 381.00 565.00 460.62 363.00 565.00 37,286 P . 460.25 170 ' 30 345.00 565.00 37,486 459.82 170 30 37;686 170 30 37,886 336.00 565.00 459.34 318.00 565.00 458;79 170 272.00 30 . 565.00 38,086 170' 430 38,286 170 30 38,486 458.04' 272.00 565.00 457.30 219.00 56,:00 456.33 Moment • 16,914,726 38.65% MAC 69,190 16,950 17,00U,866 38.54% MAC 64,770 16,950 17,082,•586 38.35% MAC 61,710 16,9504 17,161,246 38.10% MAC 58,650 16,950 17,236,846 37.81% MAC 57,120 16,590 1.7,310,916 37.4b,‘ MAC • 7 • 54,060 16,950 17 381,926 37.11% MAC 46,240 16,950 17,445,116. .36.60% MAC 46,240 16,590 17,508,3.06 36.10% MAC 37,230 16,950 17,562,486 35.44% MAC ••••••, , • EFTA00278399

••• z • • • • • • . :.•• • • EFTA00278400

FAA AIRCRAFT REGISTRY cn r, CAMERA NO. DATE; • . • ZFW - 12 Pass. (2 Crew) 38,686- Remaining Baggage Baggage OGDEN AMERICAN cdApoRAtraa . 277 Park Avenue • • • ' New York,.New York 10017,- Item • *- • _ . Grubman Gi159 S/N 151 • N979RA March 8, 1975 W.O. 215 SAMPLE LOADING FOR. ZERO FUEL WEIGHT ;.ii Pass. -(2 Crew) Passenger RI Baggage Passenger . .- Jump Seat Bagc#ge ZFW - 13 Pass. (2 Crew) ----..138,886 Weight Arm . MOME,: 38,486 456.33 17,,A'7.,486 5.44 MAC - 170 219.00 • 37,230 30 565.00 16,950 : 170 30 455.37 142.00 565.00 454.09 CONDITION #4: Loaded for Forward C. G. Limit- . ZFW - 2 Crew & Sul6Plies Passenger Jump Seat:. Baggage . ZFW 1 Pass (2 Crew) 36,286 461.21 170 142.00 30 565:00 36,486 T-159'.81 17,616,666 34.79% MAC 24,140 16,950 33.92% MAC 16,735,816 38.75% MAC 24,140 16,950 16,776,906 37.80% MAC Passenger R1 - 170 219.0C• 37,230 Baggage 30 565.00 16,950 ZFW — 2 Pass. (2 Crew) 36,686 458.78 16,831,086 37.10% MAC Passenger R1 170 '219.00 30 565.00 ZFW - 3 Pass: (2 Crew) .36,886 37,230 16,950 457.76 16,885,286 36.41% MAC . . CONDITION #5: Loading for Additional baggage ZFW - 13.Pass. (2 Crew) 38,886 . , 454.09 • '1 060' 565.00 :- • • ZFW — 13 Pass. &.Baggage 17,657,756 33.92% MAC -" 598,%900 . 457.03 18,256,656 .35.91% MAC EFTA00278401

C':• • : ..”.-44marr"-- ' .:,••-• — ' iz;%:::— ••: : ' ' . • .• . A.Citini.:;1•: • —2.......'t or...L. : ....., . . . ..., . . . . ''',.•- ” t;•'&4•::•'—'1•4;:i . '''' • . . A- ;•"' 41r••••• %-• ~y • • ..•••••••••••••= ••••••• ••• ••.•••••MIN• I ••••••• ••••••••• ••••• •••••••d•• 1•••••••IWAI••••••• 160 EFTA00278402

FAA ,AIRCRAFT RnISTRY CAMERA NO, t;a:— DATE: f;(*l o. .) }mt • • . . EFTA00278403

balitt'ssa. •• •• • '. • - . . • • • EFTA00278404

• . UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL- AVIATION ADMINISTRATION STAND 1'D AIRWO S. AUTHORITY AlsP•SASIS f uR tsSuAts This airwarthiness certificate is dOte as issuance, ths• Stir:raft therefor, to be at condition f s. operat cornprehentiee'and detailed iftvorthiness Cod Aviation, triceps as noted ht. • Exceptions: Ex.emption No. 6 46 4d ti . • t,‘ 6 TERMS AND CONDITIONS Unless sooner surrendered, wipe this airworthiness certificate is eR Lierfornied in accordance with Part circroft Is registered in the Ude' ATE.cF in:um:cc I FAA REPRES... Rep I c etnent 9-27-74 I Glen IL Any alteration, reproduction, or misuse of this certificate may be punishable by a (me cart enteeding 51.000, or ;fn.' arison:nent not er.xeding 3 years, Cr both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORD ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. FAA Form 8100-2 t7-67) FORMERLY FAA FORA" .362 eked, or ate is other long as the mortenanct Preverive wy 'nd 91 of titr federol Ark yO • "•• end cert.fies that, as of the form to the type certificate uirements of the applicable mien- on litematiOno civi; Wished by the Administrator, • oinipnance. and alterations ore (Pions, et nppropriate, and the • - • • • -•"' . : • • EFTA00278405

. . n<c, • s.ssrursis r /no, ••••••• • • • • • ..—eig• Is • EFTA00278406

FAA AIRCRAFT REGISTRY CAMERA NC. 4 . DATE: id. DEPARTMENT Of TRANSPORTATION FEDERAL AVIATION ADMINISTRATION , APPLICATION FOR AIRWORTHINESS CERTIFICATE INSTRUCTIONS-Print or rope. Do not write in shaded aieas: these are for FAA use only. SubMit original only to an authorized FAA Representative. If additional space is required, use an attachment. For special flight permits complete Sections II and V! or VII as apolicable. RCRAPT SCRIPTION T. REGJITTRATION:M.47 — N804GAI/2IGAA 79L7t 2. AIRCRAFT BUILDERS NAME (NAY/ Grumman American 3 Al.:RAFT MODEL DESIGNATION C.4159 4. YR. MFG. 1974 fAA COOING 3 9-3' 3 4-# 5- --- • ;5 Ji..-- :2. S. Al Ita. AL NO • . 151 6. ENGINE BUILDER'S NAME (A.the 1 Rolls ROyce Turbo Fan 7. ENGIT.It'/AODEL DESIGNATION Spey Mk 511-8 - 8. NUMBER a Mit( 00 .Twa ° I. PROPELLER WILDER'S MUTE (miff) 8 t3. N/A 10. PRO. ELUR MODEL DESIGNATION N/A 11. AIRCRAFT IS bettbdotttit i IMPORT II. CERTIFICATION REQUESTED APPLICATION IS MERRY MADE FOR: (Cock applicable kens) A 1 X STANDARD AIRWORTHINESS CERT. (indicate category) NORMAL UTILITY i ACROBATIC XIItANSFORAT : GLIDER I I BALLOON K SPECIAL AIRWORTHINESS CERTIFICATE (Check appropriate item) • 2 LIMITED . CLASS I • 5 PROVISIONAL (iaslicatt thus) . . 2 CLASS II , — 1 AGRICULTURE & PEST CONTROL AERIAL SURVEYING ' 3 • DUAL sovERnsING 3 RESTRICTED (Ixdic.ee opernon(t) to #e attaistattO FOREST (wild life tottereatrott 1 PAMOTAING C EATHIR CONTROL 0 OTHER (Sfrefifr) ,. . RESEARCH AND DEVELOPMENT • 2 J AMAIEUP. WILT 3 EXHIBITION 4 EXPERIMENTAI fladiratf operatican) to be ccularre:0 RACING CREW TRAINING 6,j. MKT. suRyre • 0 TO SHOW COMPLIANCE WITH FAR • FERRY FLIGHT FOR REPAIRS, ALTERATIONS, MAINTENANCE OR STO.AGE 8 SPECIAL RIGHT PERMIT (Italia:, °paying to ie 'neatened Ilya racket 2 EVACUATE FROM AREA OF IMPENDING DANGER Sretiott VI or VII as apphosalt es OPERATION IN EXCESS OF MAX. CERTIFICATED TAKE-OFF WEIGHT / •4 DELIVERING OR EXPORT • I 5.I IPRODUCHON FUCK TESTING C j 6 I MULTIPLE AIRWORTHINESS CERTIFICATE (Cheik appropriate Restricted Operation and Standard or Limited as applicable abase).- III. OWNER'S CERTIFICATION A. REGISTERED OWNER (fir shown on Cerificate of Air,-raft Registration) IF DEALER, CHECK HERE --.- I n NAME Grumman . . . American Aviation Corporation ADDRESS • Savannah, G . 31402 B. AIRCRAFT CERTIFICATION BASIS (Check applicable bfr,cis and smplete items as indicated) x Jed AIRCRAFT SPECIFICATION OR TYPE CERTIFICATION DATA SHUT (Gist No. Rtrifhlt NG.) Al2EA Rev 7 5/1/73 LAIRWORTY.INESS DIRECTIVES liteit . CD No.) (Check 74-19 if all unlit-61e AM orrpred to :th atLIgt:e AIRCRAFT UST** (Gist page Sotto.) N/A SUPPLEMENTAL TYPE CERTIFICATE (Litt -NIA number of tad, STC incoriorait..) . C. AIRCRAFT OPERATION AND MAINTENANCE RECORDS X CHECK IF RECORDS a. TOTAL AIRFRAME HOURS—EIGE90062(XEOGEr COMPLIANCE WITH . FAR 91.173 IA:Do -F_OURS EXPERIMENTAL cr etraurd • . ONLY—Ester .reef but sine Ian arttif,.ar:tt......1 • D. CERTIFICATION—I hereb) certify that I am the owner (CC his agent) of the ircraft described Federal Aviation Adminisuanon in accordance with Section 501 of the Federal Aviation Act of dons; and. that the aircraft has been inspected and is airworthy and eligible for he airworthiness above; 1958, certificate that the aircraft is registered with the and applicable Federal Aviation Reguia- requested. ., DATE OF APPLICATION - 1k September 197 2- NAME AND TITLE (Print cr WO 1 socs9ue V_ 0 anzron Agent I /7 re, IV. INSPECTION; AGENCY VERIFICATION A. THE AIRCRAFT DESCRIBED ABOVE HAS BEEN INSPECTED AND FOUND AIRWORTHY BY: (Complete Ibis section on!) if AR 21.183 (d) applies) 2 11/412 PART 121 01.327 CERTIFICATE Certijirate Na) - HOLDER (Girt 3 CERTIFICATED MECHANIC (Gist orri(inar &Nisi) 6 CERTIFICATED REPAIR STATION (Gut Ctrieitatt No.) 5" AIRCRAFT MANUFACTURER (Gist Nagle of Firm) DATE TDIE SIGNATURE I V. FAA REPRESENTATIVE CERTIFICATION (Check ALL. applicable blocks). . Iliad that the aircraft described in Section I or VII meets requested, or car —l'Amentiment.or modification of its current airworthiness certificate. In Section VII was conducted by: 0 FAA Inspector; certificate holder under FAR 65, ' he requirements for: g,The certificatiat. • pection For a special fAht permit wider FAR 121 or 127, or NU FAR 145: OATI. .2. 27 Set.i97.4 DISTRICT Off KE ASOEHDO; 7-0-42 4 h. • .. r . -1. .2 1. smi;ral.t.. . J. yn DmIR # SO-118-2 f F.:, / INSPECTORS SIGNATURE EFTA00278407

o; A. MANUFACTURER, VI. PRODUCTION ►LIGHT TESTING. NAME ADDRESS B. PRODUCTION BASIS (Check applicable hot) PRODUCTION CRITIC-ATE (Cite produetzed certificate number) TYPE CERTIFICATE ONLY APPROVED PRODUCTION INSPECTION SYSTEM C. GIVE QUANTITY Of CERTIFICATES REQUIRED FOR OPERATING NEEDS: . DATE OF APPUCATION NAME AND TITLE (Print er opt) • SIGNATURE It" . 6 VII. SPECIAL FLIGHT PERMIT PURPOSES OTHER THAN PRODUCTION FLIGHT TEM A. DESCRIPTION OF AIRCRAFT REG4STERED OWNER ADDRESS • • WILDER (.5F.iFy) r. • MODEL SERIAL NUMBER . . . . . -. REGISTRATION MARK B. DESCRIPTION Of FLIGHT FROM ' TO - - VIA DEPARTURE DATE I DURATION C. CREW REQUIRED TO OPERATE THE AIRCRAFT AND ITS EQUIPMENT ) PILOT CO-PILOT 1 NAVIGATOR OTHER FSAteib) -. D. THE AIRCRAFT DOES NOT MEET THE APPLICABLE AIRWORTHINESS. REQUIREMENTS AS FOLLOWS: .. .. . 1 • .. • ... ... . . '... .... - ... ' • . •e E. THE FOLLOWING RESTRICTIONS ARE CONSIDERED NECESSARY FOR SAFE OPERATION (Use Ottachinent if neutsan) . . . - . • Dese. . • le . • • F. CERTIFICATION-I hereby certify that I am the registered owner (or his agent) of the aircraft described above; that the aircraft is registered with the i' -decal Aviation Administration in accordance with Section 561 of the Federal Aviation Act of 1958, and applicable Federal Aviation Regulations; and that the aircraft has been inspected and is airworthy for thedlighedescribed. DATE NAME AND TITLE (Print or t;70. SIGNATURE • " A. Operating Limitations and Markings in Camp:ionce with FAR G. Statement of Conformity, FAA Form 317 fyirrafb when reautre.l) VIII. AIRWORTHINE DOCUMENTATIO (FAA use only) MI frill I 1M 9i:31'as Applicable • - H. Foreign Airworthiness Certification for Import Aircraft (Attach a Ina B. Current Operating Limitations Attached • required) — C. Dolce, Drawings, Photographs. etc. (Attach when readire.1) I. Previous Airworthiness Certificate Issued in Accordance with D. Current Weight and Balance Information Available in Aircraft . FAR CAR - (Original attached) E. Major Repair and Alteration, FAA 337 (Attach ulxn rebuked) J. Current Airworthiness Certificate Issued in. Accordance with F. This Inspection Recorded in Aircraft Records x FAR 21.183 (a) (Cep) attached) , • EFTA00278408

. - . itt rmt..‘e:-.'ravel•-•••• .••••• • UNITED STATES OF AMERICA DEPARTMENT OF TRANSPORTATION-FEDERAL AVIATION ADMINISTRATION ST/nARD AIRWORTHINESS CERTIUATE I. NATIONALITY AND It - MANUFACTURER A 3. AIRCRAFT SERIAL (1. CATEGORY s' 103040A I I / C A V\s"BcR N • , i . ..., . REGISTRATION MARKS • G.1 151, It:\ 5 1 l Transport •' S. AUTHORITY AND BASIS FOR ISSUA42 %---,.._. . --..A\ • this airworthiness certificate h its pursuant.-nr: dets ceation ,* Ps \, 58 and certifies that, es cf the' 1\ dote of issuance, the aircraft .temer.Pids issue:1, gal= lid and fer,d to o\ to the type certificate tForefcr, to be in condition/fat operatIon.:__ ' ' sitawn to meef the requirements cf the applicable ' comprehensive and detailed'isir thiness tad. as 'rev' ibLknysx 8 to me Cptvention on International Civil Mein. ../ . Aviation, except as noted sin. ; ,-..._ f ." ....... I • -110 .1. 1 ' if_ IS: . f ..... .. N i.- 1 0, 4 'IC ....‘ , .. -Tr; Tr:7-1;777T— S t: d ' mo tion No. 03 -to 4N.113t4• .77w1.JJ Exceptions: S. TERMS AND CONDITIONS \\\ ti- t/ surremiered, revoked>ar—a-WernaationAate is atbeIlMq stablished by the Administrator, - this airworthiness certificate iskeffascrisee as long al-theahicterdirionce, prey ive maintenance, and alterctiogs are t.. performed in accordance witF PaetnY, 4.7, and 91 of the Federal Avian A Regi:Ictions, as appropriate, cnd the . aircraft is registered in the UreNted 561,ers• t /7/ IF" REPTtia: DESIGNATION SOMBER DATE OF ISSUANCE Any alteration, reproduction, or misuse of this cent punishable by a fine not exceeding $4,000, or irn- • . prisonment not exceeding 3 years, or both. THIS CERTIFICATE MUST BE DISPLAYED IN THE AIRCRAFT IN ACCORD- t ANCE WITH APPLICABLE FEDERAL AVIATION REGULATIONS. 13ePt • 19711 f 130•118-2 FAA-Form 81004.(7-67) FORMERLY EFTA00278409

•• st-z. • • -• r ••1.7_,..!••• •••••=4:,•••.3*‘. -v.-' EFTA00278410