AVIONICS MAINTENANCE RECORD

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1 n v AVIONICS MAINTENANCE A Textron Company AI RCRAFT SERIAL AN 0 REGISTRATION _/w'mfll. ::.rj/()9j'5 7J5/ /-=::3J _ D

2 --- INSTRUCTIONS This record should.be completed and maintained in accordance with FAA Federal Aviation Regulations: Altimeter system and altitude reporting equipment tests and inspections, ATe transponder tests and inspections, 43.9, and , and/or other prevailing government regulations. and NOTE: Record required tests in the back of this record Record Service Letters and Airworthiness Directives in the back of this record as well as the Airframe Maintenance Record. Copyright 1996 MAINTENANCE DATE TOTAL TIME AUTHORIZED SIGNATURE, IN SERVICE DESCRIPTION OF THE WORK PERFORMED CERTIFICATE TYPE HOURS 10ths & NUMBER UPDATe::, 5y.5 72'frY"\..:5oF7(..Afc ""Tc:1 v: 5:C;s. /.J>. 3/ ;3 ;OG-e. CESS.NA :5""607-3-;/- cj5 clz 2 5 i:.e zr.sj I W.o. AV-1197 Eastern Iowa Avionics N5113J Eastern Iowa Airport P R TACH Beech Way SW 11116/2009 Cedar Rapids, IA Repair Station # ZSER281T LOG ENTRY Removed GDC74A, PIN , SIN and replaced with Overhauled Exchange Unit, SIN Loaded software and tested law Cessna Nav III G1000 Line Maintenance Manual, PIN , Rev. N dated 12/200a and found to be satisfactory. Performed system leak checks required by FAR and found to comply with Part 43, Appendix E, Paragraph (a). Details oftair are on e at this facility under W.o. # AV-1197 Signed: / D Rep air SfutioTrtertificate no. ZSER281T

3 MAINTENANCE DATE TOTAL TIME W.O. AV-1389 Eastern Iowa Avionics AUTHORIZED SIGNATURE, IN SERVICE N5113J Psa lr Eastern Iowa Airport CERTIFICATE TYPE HOURS 10ths TACH I Beech Way SW & NUMBER 1/6/2011 Cedar Rapids, IA Repair Station # ZSER281 T - LOG ENTRY Removed GTP59 Outside Air Temperature Probe, PIN , SIN and replaced with new exchange unit, SIN Loaded system software and tested IA W Cessna Nav III G I 000 Line Maintenance Manual, PIN , Rev. N dated 12/2008 and found to be satisfactory. D.etails of rearle at this facility under W.O. # AV-1389 Signed: ' Repair Statr6'n Certificate no. ZSER281 T DATE TOTAL TIME IN SERVICE HOURS 10ths W.O. AV-1416 N51113J TACH: /3/20 II LOG ENTRY Eastern Iowa Avionics Eastern Iowa Airport 3411 Beech Way SW Cedar Rapids, IA Repair Station # ZSER281 T The following altimeter system and altitude reporting equipment tests and inspections as required by FAR in accordance with FAR 43, Appendix E, have been performed. Paragraph (a) Static System 3/3/20 II Paragraph (b) Altimeter ),'3/2011 # 1 ADC MIN GDC74A STBY Altimeter MIN 5934PD-3 Tested to: 20,000 Ft. Paragraph ( c ) Integrated System 3/3/20 II D.etails ofpection on file at this facility under W.O. # Signed:. -- Repair Station Certifi6ate no. ZSER281 T SIN SIN AV-1416 JTHORIZED SIGNATURE, CERTIFICATE TYPE & NUMBER I The A TC Transponder Test & Inspections Required by FAR were I Performed this date and found to be in compliance with Part 43, Appendix F., 'II. Make Garmin Model GTX33 SIN Make N/A Model j\;/a SIN _,N'-"-'-/A-'-- _ I Details of this inspection are on file at this facility under W.O. # AV \ Date 3/3/20 II Signed: for PS Air, Inc. I I Repair Stafi. ZSER28IT FRM ,

4 ALTIMETER SCALE CORRECTION CARD FRM-214 Actual Indicator Actual Indicator Altitude Under Test Altitude Under Feet Reads Feet Test Reads o 14,000 lqw 0 16,000 IS'1W 500 5c::o 18,000 n1w 1,000 WIO 20,000 \,,, O 1,500 i«u» 22,000 / 2,000 7f)I.Q 25,000 / 3,000 3clQ 30,000 / 4,000 qooo 35,000 / 6,000 5<7""20 40,000 / 8,000 lo 45,000 / 10,000 '1bO 50,000 / 12,000 \\ 9w V SIN 4,3010 <& Date: 3- -;,- 20 l\ PS Air, Inc. Jnspector: _----'(2.f' '-- Cedar Rapids, IA Repair Station #ZSER281 T ALTIMETER SCALE CORRECTION CARD FRM-214 Actual Indicator Actual Indicator Altitude Under Test Altitude Under Feet Reads Feet Test Reads c;<=to 14,000 l'\o 0 16,000 l ,000,t I 'l'l. 0 1, ,000 l'1<t90 1,500 lsoo 22,000 / 2,000 &000 25,000 / 3,000 <X>o 30,000 / 4,000 'io 35,000 / 6,000 bodo 40,000 / 8,000 OoD 45,000 / 10,000 u;ooo 50,000 / 12,000 \\ <=to V SIN -'Z.o100552& Date: 0-3--z.o\\ PS Air, Inc.. Inspector: _&L-...:.. _ Cedar Rapids, IA Repair Station #ZSER281 T )

5 MAINTENANCE DATE TOTAL TIME AUTHORIZED SIGNATURE]; IN SERVICE DESCRIPTION OF THE WORK PERFORMED CERTIFICATE TYPE HOURS 10ths & NUMBER C/W E :s.:s;,..r-4 S.cg,,;/- 3 "7"'- 0/ :L y t../pbr1r"..-v6 f? I\. V os 5. Z/.?(,./ "'o.:?.$"'ys r2'7-"> sc'jr7vj-4ec -'"7Zl C: #...?"5.:="'...e 28-/ / ' ergo 2.. '/E57.:!!=-:::::' S?r1 / /':$-4c -r7 C/h/ C':ESS/V/-j sed -31/-c>'Z-.6Y cjpd/'tt/nt!> C/O::Jo A.tf? % f-sy5 --=s'<lfft./ A.<2 E -;r-o v.. os3. 26 c.e!s /2 1/ r=> rc-r;, - 5/17' f;c.ll9 70/2 '-f :Z:Si5C' 2: &-/1.d- T -- \ II MAINTENANCE DATE TOTAL TIME IN SERVICE -+!..!H:::;OIJI=ISI 10lhs DESCRIPTION OF THE WORK PERFORMED AUTHORIZED SIGNATURE, CERTIFICATE TYPE & NUMBER Date: 6/05/2013; Aircraft: N5113J Serial Number: 172S Tach: Work Order: SPG I certify this aircraft static system has been tested and inspected law. FAR 43, appendix E paragraph (a) to an altitude of 1,000 ft AGL Aircraft Altitude Reporting System tested and inspected law. FAR to an altitude of 20,000 feet MSL. Aircraft transponder checked and certified law. FAR Aircraft altimeter and ADC have been checked and certified law. FAR 43 appendix E. TXP MODEL: Garmin GTX-33 SIN: TSO:C112 ENC/ADC MODEL: Garmin GDC-74A SIN: TSO: C106 AL T MODEL: United Inst 5934PAD-3D SIN: TSO: C10b I certify that t"ae stated maintene.nce and lor inspection was performed in accordance with the current regulations of t leral Av;aln Admltration. Z IUI Signed,.Jelr'llr Inc. CRS # JAFR110F I I

6 ALTIMETER JET AIR, INC. GALESBURG, TEST law SHOPOROER:P6-O: CUSTOMER: U1I1 V of 0" li"v",-- ALT. MFG.: "'1M",,, PIN: pc -7(!9 SIN: 0(" 05y? (c (Ue BAROMETRICSCALEERROR: (+/- 25 FTTOLERANCE) PASS./ FAIL= CASELEAK: (100 FPMMAX) FRICTION:.LJED 1,000 "I ft-ooo PASS.J... / ' / 3,000 5,000 FAIL 10,000 15,000 ACCURACY: 6.l.LJflJ. 1,000 o 500 1,000 1,500 2,000 3,000 4,000 6,000 8,000 10,000 12,000 I.Ql... +/-20 +/ 20 +/-20 +/-20 +/-25 +/-30 +/ 30 +/ 35 +/-40 +/ 60 +/ 80 +/ 90 R.R. 2 BOX 1 I 7 IL ALTIMETER PRESSURE J.t:IL.l:l1L FAR 43 18,000 FY _ FPM PASS-1L FAIL Ellli:L 6 IQJ... +/ 70 +/-70 +/-70 +/ 70 +/-80 +/ 90 tt...c '.::.& '/0 TEST ALTITUDE illi &LJ.EU 20,000 25,000 30,000 35,000 40,000 50,000 8l.LJill 14,000 16,000 18,000 20,000 22,000 25,000 30,000 35,000 40,000 45,000 50,000 -: PA5S...\L: APPENDIX E PARA. (B) MUNIOPAL AIRPORT ers NO. JAFR110F DATE: C[im 3-..<5o/) EBlD:. I.QJ... +/ 100 +/-110 +/ 120 +/-130 +/ 140 +/ 1 SS +/ 180 +/ 205 +/-230 +/ 255 +/-280 FAIL CORRE.SDENCE TESV<+/' 125 rn /' 1K. 3K V 6K V 9K 12K 15K V 18K V 2 HYSTERESIS (+/ 75 m 50%=z 40% V' MAX/ALT' --- AFTER EFFECT (+11 30m I ALTIMETER - =-.J..:LL.. coo /570 IQl.. +/ 100 +/-120 +/-140 +/ 160 +/ ±L: ls9q(j -/0 TECH: 1)-;- ENCODING:/tf{;! N TSO: \.../6(P AD'S: Y (]:l =- --- FAIL FAIL FAIL ALTIMETER(ENCODING)HASMETALL REQUIREMENTSOF rar 43 A.;7 TECHNICIAN: T ALTIMETER TEST law FAR 43 APPENDIX E PARJ JETAIR, INC. GALESBURG, R.R.2 BOX 117 IL ALTIMETER TEST MUNICIPALAIRPORl CRSNO. JAFR110f DATE: \[ui'1c 3,...?OI TECH: i?ding: c.'/cjb ($> AD'S: Y (!D BAROMETRIC SCALEERROR: PRESSURE ALTITUDe ALTIMETER (+/- 25 FTTOLERANCE) Em -rrm ,-0 28.S < PASS 20.&0 392 FAIL r.eoa / ,q&j ISloO CASELEAK: 18,000 7 FPM PASS fail (100 FPM MAX) ---- fricfion: &L..lED illcl IQl,... Al..LJED. EB.ll:L IQl ie: +/ / 100 2,000 +/ 70 25,000 +/-120 fog 3,000 +/-70 30,000 +/ 140 PASSJ 5,000 +/ /-160 FAIL 10,000 S +/ 80 40,000. +/ ,000 'Yo +/ / 250 ACCURACY: &I.LlEIl IQL.. ±L::. 6.LLJ.EIl IQI... _±L::....::.J..9;& ::d ,000 +/-20 14,000 +/ :..J..Q...::& a +/-20 16,000 +/ 110 '.&:1!:i2.- 49(.; :::.!.Q /-20 18,000 +/ 120 1,000 +/ 20 lo/c)- He.. 20,000 +/ 130 1,500 +/ 25.aze.: cce. 22, ,000 +/-30 M 1-/" 25,000 +/ \55 -_.--- 3,000 +/ ,000 +/ ,000 +/-35 35,000 +/ 205 6,000 +/ 40 -" 40,000 +/ Yv' 8,000 +/ 60 45,000 +/ 255 -;)(.; 10,000 +/ 80 50,OO +/ fJi 12,000 +/ 90 =-70 PASS FAIL CORRE.SDENCE TES y +/' 125 rn / 1K 3K 6K V 9K 12K 15K v 18K ->""- nc _ A HYSTERESIS (+/ 75 rn 50%=z... 40% _ MAX/ALT' AFTER EFFECf (+/_ 30m /()I: 01<I PA ALTIMETER(ENCODING)HASMETALL REQUIREMENTSOF rar 43 A TECHNICIAN:,...B) \ _ t2?l??-:----=

7 MAINTENANCE DATE TOTAL TIME AUTHORIZED SIGNATURE, IN SERVICE DESCRIPTION OF THE WORK PERFORMED CERTIFICATE TYPE HOURS loths & NUMBER -2- l1 Ib 'J I,. S...,4-Pf r;.f<. s 77 vn,-+ w r+t. one:.fro,."., jj61q6p Fo'(' C7-T/// J rvl>loi-e.s hoo+, >'1 -:;(P?!i27qct 7 -ls"-i'1 2331" 7 wqpr2; CR, 5 77 un:+e co i jj 6116 P. P:;;;-fi':??.' pfs279'9'o. R """'0 vu\ a<. r-e - in d= /It'd or;<j/on,;,..1 GR'77 (,.,Inl + 0.ffLr +.r:j vhl!:h." crh''''..,.. -i - - ILl -Z "3 JJ6/Q6P. s c:» tqq o Date: 7/1/2015 Airport Road TachIHobbs: Dubuque, Iowa Blue Skies over Dubuque Inc. Repair station #YQYR343B Airplane Maintenance I.Performed Altimeter and Static system test. IA W: 14CFR Performed Transponder test law: modes A,C, & S All systems found to comply with 14CFR part 43 appendix E & F Work Order #79542 N.ame:D Signed:, Certified Repair Station # YQYR343B Date 7/1/ adjs Aircraft Hours ;;;..a I '8'. to I cern'fy t hat tea h Itimeter and static system tests required by 14 CFR and transponder tests, including data correspondence, required by , have been AUTHORIZED SIGNATURE, performed and found to comply with 14 CFR part 43, appendix E and F. CERTIFICATE TYPE & NUMBER LH Altimeter Model 6'flc' 7 Lf f} Transponder Model G,X - 33 SIN O{O{PbS- (p SIN g /O"'t'3 ol.{ RH Altimeter Model S-o, L/ Pi>-3 Transponder Model SIN < " SIN Encoder/A.D.C. Model SIN The altimeter was tested to :l feet on 7/1 Z/UJ/5 The transponder was tested or -:II /::;)0 IS-,. Encoder data correspondence was tested to feet on Static system leak tested on 7J I / ZO/S Signed Dcur-tkt Work Order # 7 9s: t.;e? Blue Skies Over Dubuque, lnc. FAA Repair Station #YQYR343B

$Y\ Altimeter Make CA, 'fvi-.., M':=p1181@ Tolerance HYSTERESIS/TESTTOLERANCES +l-{feet) Reading 20 20 Case leak Test 20 Hysteresis Test 20 First TP..50% of Max 2S Hysteresis Test 30 First TP.$

8 Y\ Altimeter Make CA, 'fvi-.., Tolerance HYSTERESIS/TESTTOLERANCES +l-{feet) Reading Case leak Test 20 Hysteresis Test 20 First TP..50% of Max 2S Hysteresis Test 30 First TP..40% of Max 30 After Effect 3S Pressure 80 Setting in Reading 90 In./Hg o.jrel) W/O No]95':4R. Date case leak Test 20 Hysteresis Test 20 First TP..50% of Max 25 Hysteresis Test 30 First TP..40% of Max 30 After Effect '35 40 Kollsman Window Calibration 60 Pressure 80 Setting in Reading 90 In./Hg ,:,".3 130_ : o-(rel) ' , ,;.- _ W/ONo Date

T h e C S E T I P r o j e c t

T h e C S E T I P r o j e c t T h e P r o j e c t T H E P R O J E C T T A B L E O F C O N T E N T S A r t i c l e P a g e C o m p r e h e n s i v e A s s es s m e n t o f t h e U F O / E T I P h e n o m e n o n M a y 1 9 9 1 1 E T