PZL-Okecie PZL-104 Wilga 35 Service Bulletins

Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 2 of 26 An agency of the European Union gs ---- Jae --- EASA Approved Model List {AML) Reference Issue Date 4 10070268 ] 1 ] 21/06/2019 ---- f / ' Type Certificate Type Certificate Certification Associated Technical Number Type Model Basis Documentation Holder EASA.A.367 CEAPR DR300 and DR 300/108 As above As above DR400 Series DR 300/120 DR 300/125 DR 300/140 DR 300/180 R DR 315 DR 340 DR 360 DR 380 DR 400/100 DR 400/120 DR 400/120 A DR 400/120 D DR 400/125 DR 400/125i DR 400/140 DR 400/140 B DR 400/160 DR 400/160 D DR 400/180 DR 400/180 R DR 400/180 S I DR 400/200 I ' DR 400/200 R DR 400/2+2 i DR 400/500 DR 400 NGL DR 400 RP EASA.A.372 CEAPR R 3000 R3000/140 As above As above R 3000/100 R 3000/120 R 3000/120 D R 3000/160 R 3000/160 S R 3000/180 EASA.A.374 CEAPR ATL ATL As above As above ATL "L" ATL "S" 4 4 . . . .. . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 3 of 26 An agency of the European Union »Ao --------------- EASA Approved Model List (AML) Reference Issue Date on 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US A13EU CESSNA Cessna FlS0F As above As above AIRCRAFT F150/F152 FlS0G COMPANY Series FlS0H FlS0J FlS0K FlS0L FlS0M F152 FAlS0K FAlS0L FAlS0M FA152 FRAlS0L FRAlS0M US A4EU CESSNA Cessna F172 F172D As above As above AIRCRAFT Series F172E COMPANY F172F F172G F172H F172K F172L I , F172M F172N F172P FP172D US A26EU CESSNA Cessna F177RG F177RG As above As above AIRCRAFT COMPANY US A42EU CESSNA Cessna F182 F182P As above As above AIRCRAFT Series F182Q COMPANY FR182 US A23EU CESSNA Cessna F172 F337E As above As above AIRCRAFT Series F337F COMPANY F337G F337H FT337E FT337F FT337GP FT337HP » 4 i ti . . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/lntra net. Page 4 of 26 An agency of the European Union A sgsss»! EASA Approved Model List (AML) Reference Issue --- A\4so ®! om a Date ---- - as 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Number Type Model Basis Documentation Holder US A18EU CESSNA Cessna FR172 FR172E As above As above AIRCRAFT Series FR172F COMPANY FR172G FR172H FR172J FR172K EASA. IM .A.007 CIRRUS DESIGN Cirrus SR-20, SR- SR20 As above As above CORPORATION 22 SR22 SR22T EASA.IM.A.615 CIRRUS DESIGN SFS0 SFS0 As above As above CORPORATION EASA.A.185 COSTRUZIONI P2006T P2006T As above As above AERO. TECNAM EASA.A.576 COSTRUZIONI P2010 P2010 As above As above AERO. TECNAM EASA.A.637 COSTRUZIONI P2012 P2012 Traveller As above As above AERO. TECNAM EASA.A.412 COSTRUZIONI Tecnam P92 P92-J As above As above AERO. TECNAM P92-JS EASA.A.010 DAHER TBM700 TBM700 A As above As above AEROSPACE TBM700 B TBM700 Cl TBM700 C2 TBM700 N EASA.IM.A.223 DIAMOND DA20 DA20-A1 As above As above AIRCRAFT IND. DA20-C1 INC EASA. IM .A.022 DIAMOND DA40 DA40 As above As above AIRCRAFT IND. DA40D INC DA40F DA40NG EASA.A.005 DIAMOND DA42 DA42 As above As above AIRCRAFT DA42M INDUSTRIES DA42M-NG DA42NG DA62 4 f . .. . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- Internet/lntra net. Pages of 26 An agency of the European Union -------- al® ----- EASA Approved Model List (AML) Reference Issue Date m 10070268 1 21/06/2019 -- Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation EASA.A.065 DIAMOND H 36 "DIMONA" ~ ~ ells AIRCRAFT HK 36 "SUPER INDUSTRIES DIMONA" HK 36 R "SUPER DIMONA" HK 36 TS HK 36 TC HK 36 TTS HK 36 TTC HK 36 TTC-ECO US 1A21 DYNAC (Aero (Aero As above As above AEROSPACE Commander) Commander) 100 CORPORATION 100 EASA.A.061 PZL PZL-104 Wilga PZL-104MA Wilga As above As above WARSZAWA- series 2000 OKECIE S.A. PZL-104MF Wilga 2000 PZL-104MN Wilga 2000 PZL-104M Wilga 2000 PZL-104 Wilga 32 PZL-104 Wilga 32A PZL-104 Wilga 35 PZL-104 Wilga 35A PZL-104 Wilga 80 EASA.IM.A.171 ECLIPSE EAS00 EAS00 As above As above AEROSPACE INCORPORATED EASA.A.362 EXTRA EA 300 EA 300 As above As above EA 300/200 EA 300/L EA 300/LC EA 300/LT EA 300/S EA 300/SC EASA.IM.A.042 GA8 AIRVAN GA8-Series GA8 As above As above PTY. LTD. GA8-TC 320 4 . .. .. .4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 6 of 26 An agency of the European Union ----as gs so» -------- EASA Approved Model List (AML) Reference Issue Date Woo 10070268 1 21/06/2019 l Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation EASA.A.075 GROB AIRCRAFT G 120 G 120A As above As above AG G 120A-I EASA.A.565 GROB AIRCRAFT G 120TP G 120TP-A As above As above AG EASA.A.364 GROB AIRCRAFT Grob G 115 G 115 As above As above AG G 115A G 1158 G 115C G115C2 G 115D G 115D2 G 115E G 115EG G 115TA EASA.A.586 LEONARDO F260 F260 As above As above S.p.A. F2608 F260C F260D F260E F260F SF260TP EASA.A.587 LEONARDO S205/S208 S205-18/F As above As above S.p.A. S205-18/R , S205-20/F S205-20/R S205-22/R S208 S208A US AlOSW MITSUBISHI MU-2 (US MU-2B-25 As above As above HEAVY Al0SW) MU-2B-26 INDUSTRIES MU-2B-26A MU-2B-35 MU-2B-36A MU-2B-40 MU-2B-60 JP 25 MITSUBISHI MU-2 (JP 25) MU-2B-30 As above As above HEAVY MU-2B-35 INDUSTRIES MU-28-36 EASA.IM.A.266 MOONEY M20 M20M As above As above AVIATION M20R COMPANY, INC. 4 . . ti • * 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 7 of 26 An agency of the European Union EASA Approved Model List (AML) Reference 10070268 A»»a - ----- »as» »on Issue 1 Date ---- » 21/06/2019 » I Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 2A3 MOONEY M20 M20 As above As above AVIATION M20A COMPANY, INC. M20B M20C M20D M20E M20F M20G M20J M20K M20L M20S M20TN USA6SW MOONEY M22 M22 As above As above AVIATION COMPANY, INC. EASA.A.384 PIAGGIO P.166 P.166 As above As above AVIATION S.p.A. P.166 B P.166 C P.166 DL3 ' P.166 DPl P.166 S EASA.A.089 PILATUS PC-12 PC-12 As above As above AIRCRAFT LTD. PC-12/45 .i PC-12/47 PC-12/47E EASA.A.594 Pl LATUS PC-24 PC-24 As above As above AIRCRAFT LTD. 4 f 4 . . . .. . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 8 of 26 An agency of the £European Union A%sow -------- EASA Approved Model List {AML) Reference 10070268 Issue Date --- NANNA8No8NNlsNNNNNNNlwsNNNl8NA~aw!WW 1 21/06/2019 »» » Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation CH F 56-10 Pl LATUS PC-6 PC-6 As above - As above AIRCRAFT LTD. PC-6/350 PC-6/350-H1 PC-6/350-H2 PC-6/A PC-6/A1-H2 PC-6/A2-H2 PC-6/A-H1 PC-6/A-H2 PC-6/B1-H2 PC-6/B2-H2 PC-6/B2-H4 PC-6/B-H2 PC-6/C1-H2 PC-6/C-H2 PC-6-H1 PC-6-H2 US 1A10 PIPER AIRCRAFT, PA-23 PA-23-235 As above As above INC. PA-23-250 PA-E23-250 US lAlS PIPER AIRCRAFT, PA-24 PA-24 As above As above INC. (Comanche) PA-24-250 I PA-24-260 PA-24-400 4 l . .• * 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 9 of 26 An agency of the European Union !®! Ass so Ao ----EASA Approved Model List (AML} Reference 10070268 Issue 1 Date --- 21/06/2019 --- »Ar Jr g US 2Al3 PIPER AIRCRAFT, PA-28 PA-28-140 As above As above a I INC. (Cherokee or Cruiser) PA-28-150 (Cherokee) PA-28-151 (Cherokee Warrior) PA-28-160 (Cherokee) PA-28-161 PA-28-161 (Warrior II) PA-28-161 (Warrior Ill) PA-28-180 (Archer) PA-28-180 (Cherokee) PA-28-181 (Archer fl) PA-28RT-201T (Turbo Dakota) PA-28-235 (Cher.Pathfinder) PA-28-236 (Dakota) PA-28R-180 (Arrow) PA-28R-200 (Arrow) PA-28R-200 (Arrow II) PA-28R-201 (Arrow Ill) PA-28R-201T (Turbo Arrow Ill) PA-28RT-201 (Arrow IV) PA-28-201T (Turbo Arrow IV) PA-285-160 (Cherokee) PA-285-180 (Cherokee) » 4 l ii ti . . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/1 ntranet. Page 10 of 26 An agency of the European Union -----»a Aono EASA Approved Model List (AML) Reference Issue I Date woo 10070268 1 21/06/2019 --- a JJ»I -- -- I I Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation EASA.IM.A.234 PIPER AIRCRAFT, PA-28 PA-28-181 As above As above INC. (Archer Ill) US A20SO PIPER AIRCRAFT, PA-31 (Navajo) PA-31 As above As above INC. PA-31-300 PA-31-325 PA-31-350 (Chieftain) US A3SO PIPER AIRCRAFT, PA-32 PA-32-260 As above As above INC. (Cherokee Six 260) PA-32-300 (Cherokee Six 300) PA-32-301 (Saratoga) PA-32-301T (Turbo Saratoga) PA-32R-300 I (Lance) PA-32R-301 : (Saratoga SP) PA-32R-301T P (Turbo SaratogaSP) ' PA-32RT-300 J (Lance II) PA-32RT-300T (Turbo Lance II) PA-32$-300 (Cher.Six Seaplane) EASA.IM.A.239 PIPER AIRCRAFT, PA-32 PA-32-301FT As above As above INC. (Piper 6X) PA-32-301XTC (Piper 6XT) PA-32R-301 (Saratoga II HP) PA-32R-301T (Saratoga II TC) Piper 6X Piper 6XT » 4 . . . .. .4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 11 of 26 An agency of the European Union ----»lo - ---- EASA Approved Model List (AML) Reference Issue Date ---- 10070268 1 21/06/2019 I . I ' j I I Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US A7SO PIPER AIRCRAFT, PA-34 PA-34-200 As above As above INC. (Seneca) - PA-34-200T (Seneca II) PA-34-220T (Seneca Ill) PA-34-220T (Seneca IV) EASA. IM .A.090 PIPER AIRCRAFT, PA-34 PA-34-220T As above As above INC. (Seneca V) US A18SO PIPER AIRCRAFT, PA-38 PA-38-112 As above As above INC. US A23SO PIPER AIRCRAFT, PA-42, PA-42R PA-42-1000 As above As above INC. (Cheyenne 400LS) PA-42-720 I (Cheyenne IIIA) PA-42-720R PA-42 (Cheyenne Ill) EASA.IM.A.232 PIPER AIRCRAFT, PA-44 PA-44-180 As above As above INC. (Seminole) I PA-44-180T (Turbo Seminole) EASA.IM.A.077 PIPER AIRCRAFT, PA-46 PA-46-310P As above As above INC. PA-46-350P PA-46-500TP PA-46-600TP PA-46R-350T t 4 l . . . .4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 12 of 26 An agency of the European Union ---- Ao» EASA Approved Model List {AML} Reference Issue ! Date ------------- 10070268 1 21/06/2019 I Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation EASA.A.377 DAHER MS 880 and MS 880 B As above As above AEROSPACE Rallye 100 MS 880B-D Series MS881 MS883 MS884 MS885 MS886 MS887 Rallye 100 S Rallye 100 S-D Rallye 100 ST Rallye 100 ST-D Rallye 110 ST Rallye 150 ST Rallye 150 ST-D Rallye 150 SV Rallye 150 SVS Rallye 150 T Rallye 150 T-D I Ra I lye 180 T Rallye 180 T-D Rallye 180 TS EASA.A.379 DAHER MS 890 and MS 890 A As above As above AEROSPACE Rallye 235 MS 890 B Series MS 892 A.150 [ / MS 892 B.150 MS 892 E.150 MS 892 E-D.150 MS 893 A MS 893 B MS 893 E MS 893 E-D MS 894 A MS 894 C MS 894 E RALLYE 235 A RALLYE 235 C RALLYE 235 E RALL YE 235 E-D RALLYE 235 F t 4 . .• * * • 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 13 of 26 An agency of the European Union --- --g AA,Jg ------· EASA Approved Model List (AML) Reference Issue Date 10070268 1 21/06/2019 -· Type Certificate Type Certificate Certification Associated Technical Number Type Model Basis Documentation Holder EASA.A.378 DAHER TB series TB 10 As above As above AEROSPACE TB 20 TB 200 TB 21 TB 9 EASA.A.011 SST EA400 EA400 As above As above FLUGTECHNIK EA 400-500 GmbH US A23CE BEECHCRAFT 58 58P As above As above CORPORATION 58PA 58TC 58TCA US A12CE BEECHCRAFT 60 60 As above As above CORPORATION A60 B60 EASA.IM.A.277 BEECHCRAFT Beechcraft B200 As above As above CORPORATION AlO0, 200, 300, B200C 1900 B200CGT B200GT B300 B300C US A24CE TEXTRON Beechcraft 1900 As above As above AVIATION INC. AlO0, 200, 300, 1900C 1900 1900D 200 200C 200CT 200T 300 300LW Al00-1 A200 A200C B200CT B200T » t4 . .ti . . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 14 of 26 An agency of the European Union ------------------ -- EASA Approved Model List (AML) Reference Issue Date ---- 10070268 L 1 21/06/2019 I I Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A12 TEXTRON Cessna 172 172 As above As above AVIATION INC. Series 172A (Skyhawk) 172B 172C 172D 172E 172F 172G 172H 1721 172K 172L 172M 172N 172P 172Q EASA.IM.A.051 TEXTRON Cessna 172 172R As above As above AVIATION INC. Series 172S (Skyhawk) US 3A20 TEXTRON Beechcraft 65, 65 As above As above AVIATION INC. 70,90 65-80 65-88 ! 65-90 65-A80 65-A80-8800 65-A90 65-A90-1 65-A90-2 65-A90-3 65-A90-4 65-B80 70 A65 A-65-8200 B90 C90 E90 H90 EASA.IM.A.503 TEXTRON Beechcraft 65, C90A As above As above AVIATION INC. 70,90 C90GT C90GTi 4 t,4 • * * * • * 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 15 of 26 An agency of the European Union ----- »A» Au»om» woo EASA Approved Model List (AM L) Reference Issue Date ----- 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A13 TEXTRON Cessna 182 182 As above As above AVIATION INC Series (Skylane) 182A 182B 182C 182D 182E 182F 182G 182H 182J 182K 182L 182M 182N 182P 182Q 182R R182 T182 TR182 EASA.IM .A.052 TEXTRON Cessna 182 182S As above As above AVIATION INC. Series (Skylane) 182T , T182T I t 4 . .tie . . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1SO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 16 of 26 An agency of the European Union AAA - ----- ---- 4»»» EASA Approved Model List (AML) Reference 10070268 Issue 1 Date gNQg3pg3jg»Ng3QpN»@gjg33%Jg3Jg~ 3JJAll!!! 21/06/2019 o Ar om» »» Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US A4CE TEXTRON Cessna 206 206 As above As above AVIATION INC. Series P206 (Stationair) P206A P2068 P206C P206D P206E TP206A TP2068 TP206C TP206D TP206E TU206A TU2068 TU206C TU206D TU206E i TU206F i TU206G U206 U206A U2068 U206C I U206D ' U206E U206F ¢ U206G EASA.IM.A.053 TEXTRON Cessna 206 206H As above As above AVIATION INC. Series T206H (Stationair) EASA.IM.A.226 TEXTRON Cessna 208 208 As above As above AVIATION INC. (Caravan) 2088 EASA.IM.A.502 TEXTRON Cessna 510 510 As above As above AVIATION INC. (Mustang) EASA.IM.A.078 TEXTRON Cessna 525 525 As above As above AVIATION INC. Series (Citation) 525A 5258 525C US A34CE TEXTRON T303 T303 As above As above AVIATION INC. 4 . . . .• • ta TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/lntra net. Page 17 of 26 An agency of the European Union EASA Approved Model List (AML) Reference Issue AAA A! %a» -------A ---- -Date 10070268 1 21/06/2019 I I I I f Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A19 TEXTRON 150 Series 150 As above , As above AVIATION INC. 150A 1508 150C 150D 150E 150F 150G 150H 150J 150K 150L 150M 152 A150K A150L A150M A152 US 3A17 TEXTRON 172RG, R172 172RG As above As above AVIATION INC. AND 175 175 ! 175A 1758 175C I P172D R172E R172F R172G R172H R172J R172K US Al3CE TEXTRON 177 Fixed gear 177 As above As above AVIATION INC. 177A 1778 US A20CE TEXTRON 177 RG 177RG As above As above AVIATION INC. 4 . . . .. . t 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- Internet/lntranet. Page 18 of 26 An agency of the European Union -------- al a EASA Approved Model List {AML} Reference m Issue Date - 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Number Type Model Basis Documentation Holder US 5A6 TEXTRON 180 series 180 As above - As above AVIATION INC. 180A 180B 180C 180D 180E 180F 180G 180H 180J 180K US 3A24 TEXTRON 185 series 185 As above As above AVIATION INC. 185A 185B 185C 185D 185E Al85E A185F US A16CE TEXTRON 207 Series 207 As above As above AVIATION INC 207A [ T207 T207A 4 t4 . . ii ti . . ... TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nte rn et/Intra net. Page 19 of 26 An agency of the European Union »sss ooo »aw ----- Ao EASA Approved Model List (AML} Reference Issue Date -- on» 10070268 + 1 21/06/2019 or a Type Certificate Type Certificate Certification Associated Technical Type Model . Number Holder Basis Documentation US 3A21 TEXTRON 210 series 210 As above AVIATION INC 210-5 (205) 210-5A (205A) 210A 210B 210C 210D 210E 210F 210G 210H 210J 210K 210L 210M 210N 210R P210N P210R T210F T210G T210H T210J T210K T210L T210M T210N T210R As above + 4 . .it . .4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/lntranet. Page 20 of 26 An agency of the European Union -- -------------- EASA Approved Model List (AML) Reference om Issue Date 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A10 TEXTRON 310 series 310 As above As above AVIATION INC 3108 - 310C 310D 310F 310G 310H 3101 310J 310J-1 310K 310L 310N 310P 310Q 310R E310H E310J T310P T310Q T310R US A6CE TEXTRON 337 series 337 As above As above AVIATION INC 337A 3378 / 337C 337D 337E 337F 337G 337H M3378 P337H T3378 T337C T337D T337E T337F T337G T337H T337H-SP 4 4 . . . .. .4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/lntra net. Page 21 of 26 An agency of the European Union -- - ---- -- EASA Approved Model List (AML) Reference Issue] Date ---- 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Number Type Model Basis Documentation Holder US A7CE TEXTRON 400 series 401 As above As above AVIATION INC 401A 401B Ag 402 402A 402B 402C 411 411A 414 414A 421 421A 421B 421C 425 US 3A25 TEXTRON 320-, 340- 320 As above As above AVIATION INC Series 320-1 320A 320B 320C 320D I 320E 320F 335 l 340 340A US A25CE TEXTRON 404/406 404 As above As above AVIATION INC US A28CE TEXTRON 441 441 As above As above AVIATION INC t 4 l . .. . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- lnternet/lntra net. Page 22 of 26 An agency of the European Union ---- AAA, Joe ------ EASA Approved Model List (AML) Reference Issue -- AA Date 10070268 L 21/06/2019 » Ar / ± Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A15 TEXTRON Beechcraft 33, 35-33 As above As above AVIATION INC 35,36 35-A33 (Bonanza) 35-B33 35-C33 35-C33A 36 A36 A36TC B36TC E33 E33A E33C F33 F33A F33C G33 H35 J35 K35 M35 N35 P35 S35 I V35 I V35A V35B EASA.IM.A.279 TEXTRON Beechcraft 33, G36 As above As above AVIATION INC 35,36 (Bonanza) 4 t, l * * * * # 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 23 of 26 An agency of the European Union ------ --~ - -»ooo® 4 EASA Approved Model List {AML) Reference Issue oo Date --- 10070268 1 21/06/2019 Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 3A16 TEXTRON Beechcraft 55, 56TC As above As above AVIATION INC 56,58,95 58 58A 95 95-55 95-A55 95-B55 95-B55A 95-B55B 95-C55 95-C55A A56TC 895 895A DSS DSSA D95A ESS [ ESSA E95 EASA.IM.A.280 TEXTRON Beechcraft 55, G58 As above As above AVIATION INC. 56,58,95 US A11EA TRUE FLIGHT AA-1 AA-1 As above As above HOLDINGS LLC AA-1A AA-1B AA-1C US A16EA TRUE FLIGHT AA-5 AA-5, As above As above HOLDINGS LLC AA-5A AA-5B AG-5B US 6A1 TWIN Twin 500 As above As above COMMANDER Commander S00A AIRCRAFT L.L.C. 500 Series 5008 SOOS soou 520 560 560A 560E 4 . . . .• * 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- Internet/lntranet. Page 24 of 26 An agency of the European Union Ao » »so4As sos® Ao a ----- EASA Approved Model List (AML) Reference Issue] Date Ao ----- 10070268 1 I 21/06/2019 { nm Type Certificate Type Certificate Certification Associated Technical Type Model Number Holder Basis Documentation US 2A4 TWIN Twin 560-F As above As above COMMANDER Commander 680 AIRCRAFT L.L.C. 600 Series 680E 680F 680FL 680FL(P) 680T 680V 680W 681 685 690 690A 690B 690C 690D 695 695A 695B 720 US A12SW TWIN Twin 700 As above As above COMMANDER Commander AIRCRAFT L.L.C. 700 Series EASA. A.385 VULCANAIR VULCANAIR AP68TP-300 As above As above S.P.A. P.68 "Spartacus"J AP68TP-600 "Viator" P.68B "Victor P.68C P.68C-TC P.68 "Observer" P.68 "Observer 2"° P.68R "Victor" P.68TC "Observer P.68 "Victor" EASA.A.027 ZLIN AIRCRAFT ZLI N Z 42 Series Z 142 As above As above A.S. Z 142 C Z 242 L Z42 M Z42 MU 4 t 4 . .* • • * 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- Internet/lntra net. Page 25 of 26 An agency of the European Union on. Ass! ---- EASA Approved Model List (AML} Reference Issue Date so» 10070268 1 21/06/2019 -- Type Certificate Type Certificate Certification Associated Technical Type Model . . Number Holder Basis Documentation EASA.A.028 ZLIN AIRCRAFT A.S. ZLIN Z 43 Series Z 143 L Z 143 LSi Z 43 As above As above Cologne, Germany, 21 June 2019 Dominique ROLAND Head of Department General Aviation I t 4 • * . .. . 4 TE.CERT.00145-001 © European Aviation Safety Agency. All rights reserved. 1509001 Certified Proprietary document. Copies are not controlled. Confirm revision status through the EASA- 1 nternet/1 ntra net. Page 26 of 26 An agency of the European Union Page 1 of 9 Date 03.06.2019 Revision 01 0 Doc.-No. GOLZE_MC_ADL200_AFM_01 ABCD-FTP-00 GOLZE ENGINEERING GOLZE_MC_ADL200_AFM_01 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT EASA Approved Airplane Flight Manual Supplement AML Minor Change for ADL inflight weather receiver Doc-No: GOLZE_MC_ADL_AFM Issue 01 03.06.2019 A/C Manufacturer: __________________________ A/C Type: __________________________ A/C Model: __________________________ A/C Serial Number: __________________________ A/C Registration: __________________________ Issue Date Change 01 03.06.2019 Initial Issue The content has been approved under the authority of EASA under approval no: ___________________ The document must always be carried in the aircraft. It describes the operating procedures when installed according to the installation instructions Doc.-No: GLZ_MC_ADL200_II Issue 01 or later. The information contained herein, supplements the or supersedes the basic Airplane Flight Manual only in the areas listed herein. For limitations, procedures and performance information not contained within this document, consult the Airplane Flight Manual. Page 2 of 9 Date 03.06.2019 Revision 01 0 Doc.-No. GOLZE_MC_ADL200_AFM_01 ABCD-FTP-00 GOLZE ENGINEERING GOLZE_MC_ADL200_AFM_01 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT SECTION 1 - General The document contains information which is necessary for safe operation of the Golze Engineering ADL200, ADL190 or ADL150/150B inflight weather receiver. The ADL200 is a satellite weather receiver with additional 4G/LTE, ADS-B 1090 MHz traffic and AHRS. The ADS-B system is a receiver only. The 4G/LTE link is used in order to reduce satellite transmission costs when flying slow and low enough to get a connection. The system provides inflight weather through either the 4G/LTE or an Iridium data link. It distributes the weather via an WiFi Interface to an iPad/iPhone running the ADLConnect App. The AHRS functionality is for information only and not to be used for any navigational operations. The ADL190 is a based on the ADL200 but does not contain the 4G/LTE module. The ADL150/B is also based on the ADL200 but does not contain the 4G/LTE module, no ADS-B traffic receiver and no AHRS module. System 4G/LTE ADS-B IN AHRS IRIDIUM ADL200 YES YES YES YES ADL190 NO YES YES YES ADL150/B NO NO NO YES The system is powered from the aircraft avionics bus via a 1 AMP circuit breaker labelled “ADL”. SECTION 2 – Limitations The system is complementary only and not to be used for primary navigation. It must not be used for guidance on icing, thunderstorms or any other weather conditions. The information provided is not verified to any airworthiness standard. SECTION 3 – Emergency Procedures No change to basic AFM. SECTION 4 – Normal Procedures No change to basic AFM. Page 3 of 9 Date 03.06.2019 Revision 01 0 Doc.-No. GOLZE_MC_ADL200_AFM_01 ABCD-FTP-00 GOLZE ENGINEERING GOLZE_MC_ADL200_AFM_01 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT SECTION 5 – Performance No change to basic AFM. SECTION 6 - Weight and Balance The additional weight of the ADL system is 252 grams. A change on weight & balance is negligible. SECTION 7 - Systems Description The Golze Engineering ADL200 User and Installation Manual Rev. 0.90 or later, or the ADL150/ADL150B User and Installation Manual Rev. 2.00 or later contain further information on system operation. GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 1 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING “Installation Instruction” AML Minor Change for ADL inflight weather receiver Doc-No: GOLZE_MC_ADL_II Issue 02 08.08.2019 Applicant Details: Golze Engineering Dr. Sebastian Golze Bredowstr. 29 10551 Berlin Germany Applicant Contact Details (Responsible Person for this Change ) Dr. Sebastian Golze, Managing Director Golze Engineering (mail@ing-golze.de) Supported by Kai Odenthal (Avionics & Electrics CVE for various EASA approved Part-21 J Design Organisations) (mail@avionics-engineering.de) GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 2 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING Table of Contents 1 Introduction .......................................................................................................................................................... 3 1.1 References ................................................................................................................................................... 3 2 Applicability ........................................................................................................................................................... 3 3 Limitations............................................................................................................................................................. 3 4 Approved Equipment ............................................................................................................................................ 3 5 Required Parts ....................................................................................................................................................... 4 6 Compatible External Antennas ............................................................................................................................. 4 7 Mechanical Installation ......................................................................................................................................... 5 8 Electrical Installation ............................................................................................................................................. 6 9 Electrical Load ....................................................................................................................................................... 6 10 System Check Out ................................................................................................................................................. 7 10.1 Functional Test ............................................................................................................................................ 7 10.2 EMI/EMC Test .............................................................................................................................................. 8 11 Maintenance and Instructions for Continued Airworthiness ............................................................................... 9 12 Document History ................................................................................................................................................. 9 GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 3 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 1 Introduction This document describes the installation of the Golze Engineering ADL200, ADL190 and ADL150/ADL150B Series inflight weather receiver. It covers two options for different antenna installations: - This change approves the installation of the internal Iridium, ADS-B IN and LTE antennas. - Alternatively, it approves the usage of an already installed and approved external Iridium, ADS-B IN or LTE antenna 1.1 References [1] ADL200 User and Installation Manual Rev. 0.90 or later [2] ADL150/ADL150B User and Installation Manual Rev. 2.00 or later [3] AC 43.13-1B, Acceptable Methods, Techniques, and Practices – Aircraft Inspection and Repair [4] AC 43.13-2B, Acceptable Methods, Techniques, and Practices – Aircraft Alterations [5] Approved Model List Doc-No: GLZ_MC_ADL200_AML Issue 01. [6] Airplane Flight Manual Supplement Doc-No: GLZ_MC_ADL200_AFM Issue 01. 2 Applicability This change is applicable to the aircraft models listed in the Approved Model List Doc-No: GLZ_MC_ADL200_AML Issue 01. 3 Limitations The equipment is not approved for primary navigation. It must not be used for primary navigation. Usage is for improvement of situational awareness only. 4 Approved Equipment This change covers and approves the installation of the following equipment: - Golze Engineering ADL200 Satellite Weather Receiver - Golze Engineering ADL190 Satellite Weather Receiver - Golze Engineering ADL150/ADL150B Satellite Weather Receiver GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 4 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 5 Required Parts The following parts are required: Name Quantity Part Number 1A Circuit Breaker 1 MS26574 or MS22073 series (1 AMP) Wire AWG22 As rqd. M22759/16-22-9 or as approved per 43.13-1B Wire shielded, 1 conductor As rqd. M27500-22SB1T23 or as approved per 43.13-1B Screw 4 MS24693 Nut 4 MS21044N06 Washer 4 NAS1149FN632P Adhesive As rqd. Tesa Powerbond ULTRA STRONG or equivalent (10kg per 10cm at 19mm width) The following parts are only required if an external antenna is being used (one set per Antenna): Coax Cable As rqd. RG400 or RG142 SMA Connector 1 SMA to RG400/RG142 connector BNC or TNC Connector 1 BNC or TNC to RG400/RG142 connector (selection is based on installed antenna connector type) Table 1 - Required Parts 6 Compatible External Antennas The following antennas are compatible with the ADL150(B)/ADL190/ADL200 System: Type Manufacturer Part Number Iridium Comant CI 490-1 Iridium Sensor Systems S67-1575-109 Iridium Sensor Systems S67-1575-165 Iridium Sensor Systems S67-1575-365 Iridium Antcom S3IR16RR Iridium Dayton Granger L10-780 Iridium Dayton Granger L10-787 ADS-B IN & LTE Comant CI101 ADS-B IN & LTE Comant CI105-16 ADS-B IN & LTE Comant CI105 ADS-B IN & LTE Comant CI110-40-30 ADS-B IN & LTE Comant CI110-41-30 ADS-B IN & LTE Comant CI110-60-30 ADS-B IN & LTE Comant CI110-61-30 ADS-B IN & LTE Dorne & Margolin DMNI50-2-2 Table 2 - Compatible external antennas The usage of similar types of antennas are permissible if the electrical specifications are similar to the listed antennas and ground testing has been completed successfully. GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 5 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 7 Mechanical Installation Step Description Sign 01 or Install the ADL receiver on a suitable location by using the Tesa Powerbond ULTRA STRONG attached at the full surface of the receiver housing. Clean the surface prior to the application of the adhesive by a suitable mean to remove any residues of dirt, fat and grease. 02 Install the ADL receiver on a supporting structure behind the instrument panel via the 4 screws, washers and nuts. 03 (ADL200 only) Install the 4G/LTE antenna on either the left or right side of the windscreen (front window or side window) as close to the structural frame as possible. Make sure the view is not obstructed. Use the 3M adhesive applied to the antenna. Clean the surface prior to the application of the adhesive by a suitable mean to remove any residues of dirt, fat and grease. Note: Not required if an external 4G/LTE antenna is being used 04 (ADL200 and ADL190 only) Install the ADS-B In antenna on either the left or right side of the windscreen (front window or side window) as close to the structural frame as possible. Make sure the view is not obstructed. Use the 3M adhesive applied to the antenna. Clean the surface prior to the application of the adhesive by a suitable mean to remove any residues of dirt, fat and grease. Note: Not required if an external ADS-B In antenna is being used 05 (ADL200 and ADL190 only) Install the Iridium antenna on top of the glareshield as horizontally as possible. Make sure the view is not obstructed. Use the Tesa Powerbond ULTRA STRONG attached at the full surface of the bottom of the antenna housing. Clean the surface prior to the application of the adhesive by a suitable mean to remove any residues of dirt, fat and grease. Note: Not required if an external Iridium antenna is being used GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 6 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 8 Electrical Installation Note: All wiring installations need to be according to the standards described within AC 43.13-1B and 43.13-2B. Step Description Sign 01 Install the 1A Circuit Breaker on the avionics bus. 02 Label the 1A CB with “ADL150” / ADL150B / "ADL190" / "ADL200" 03 Or Route the antenna wires to the receiver. Attach the wires with cable ties in an interval of 150-200mm. 03.1 For usage with existing external antenna only: - Route a RG142 or RG400 to the Iridium, 4G/LTE or ADS-B In Antenna respectively - Install the SMA and BNC/TNC connector as per OEM instruction 04 Connect the antenna wires to the appropriate port. 05 Install wiring as per wiring diagram Figure 1. For RS232 Interface to existing GPS/FMS refer to the corresponding installation manual. Label the wires according to the wiring diagram as per Figure 1. 06 Perform a continuity check of all added wiring. 07 Perform an FOD (foreign object damage) inspection. Figure 1 - Wiring Diagram 8.1 Electrical Load It is the installers responsibility to update the Aircraft Electrical Load Analysis. The increase in electrical load due to the ADL200/ADL190/ADL150 or 150B Series installation is 5W (0.36A@14V or 0.2A@28V). GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 7 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 9 System Check Out Perform the following tasks prior to conducting the system check out: 1. A/C power needs to be available. Consult the applicable Aircraft Maintenance Manual for further guidance and safety precautions. 9.1 Functional Test Step Description Pass / Fail 01 Turn on the A/C main bus and avionics bus NA 02 Perform the “Connecting your iPad/iPhone/Android device to the ADL” procedure as per ADL series installation manual PASS FAIL 03 Start and set up the ADL connect app on an iPAD/iPhone/Android as per ADL series installation manual, make sure the own callsign has been properly set up PASS FAIL 04 Select “config” within the ADL connect app, scroll down and check if GPS position fix has been determined. PASS FAIL 05 (ADL200 only) Select “config” within the ADL connect app, then select “Cellular Only” PASS FAIL 06 (ADL200 only) Perform a weather download as per ADL series installation manual PASS FAIL 07 (ADL200 only) Select “config” within the ADL connect app, then select “Iridium Only” PASS FAIL 08 Perform a weather download as per ADL series installation manual until the message “request uploaded” is displayed. Note: This allows testing of the unit without applying for the service. PASS FAIL 09 (ADL200 only) Select “config” within the ADL connect app, then select “Hybrid” PASS FAIL 10 (ADL200 and ADL190 only) Check if the system does receive any other ADS-B targets, perform a check-flight if no targets are being received on ground. PASS FAIL 11 If the system is connected to an installed GPS source, check the RS232 interface as follows: - Program a flightplan in the A/C GPS/FMS system - Activate “FPL IN” within the ADL Connect app - Verify the flight plan has been received by the ADL Connect app PASS FAIL 12 Turn off the A/C main bus and avionics bus NA GOLZE_MC_ADL200_II_02 Document reference: ABCD-FTP-00 Document reference: ABCD-FTP-00 MINOR CHANGE CERTIFICATION DOCUMENT Page 8 of 9 Date 08.08.2019 Revision 02 0 Doc.-No. GOLZE_MC_ADL_II_02 ABCD-FTP-00 GOLZE ENGINEERING 9.2 EMI/EMC Test An EMI/EMC check needs to be performed after every ADL Series installation to verify no EMI/EMC impact on existing A/C systems is present. Step Description Pass / Fail 01 Turn on the A/C main bus and avionics bus except the ADL Series system (PULL circuit breaker) PASS FAIL 02 Verify all electrical and avionics systems are properly functioning. PASS FAIL 03 Apply power to the ADL Series system (CLOSE circuit breaker). PASS FAIL 04 Verify ADL Series system functions properly. PASS FAIL 05 (ADL200 only) Select “config” within the ADL connect app, then select “Cellular Only” PASS FAIL 06 (ADL200 only) Perform a weather download as per ADL series installation manual PASS FAIL 07 (ADL200 only) Verify no EMI/EMC impact is present by checking the impact on each system via Table 3 - SOURCE/VICTIM Matrix. PASS FAIL 08 (ADL200 only) Select “config” within the ADL connect app, then select “Iridium Only” PASS FAIL 09 Perform a weather download as per ADL series installation manual until the message “request uploaded” is displayed. Note: This allows testing of the unit without applying for the service. PASS FAIL 07 Verify no EMI/EMC impact is present by checking the impact on each system via Table 3 - SOURCE/VICTIM Matrix. PASS FAIL 10 (ADL200 only) Select “config” within the ADL connect app, then select “Hybrid” PASS FAIL 11 Turn off the A/C main bus and avionics bus NA