Garmin | G5 Electronic Flight Instrument for Certificated Aircraft | Garmin G5 Electronic Flight Instrument for Certificated Aircraft STC-ANAC 2017S04-02 (FAA STC SA01818WI)

Garmin G5 Electronic Flight Instrument for Certificated Aircraft STC-ANAC 2017S04-02  (FAA STC SA01818WI)
CERTIFICADO SUPLEMENTAR DE TIPO
(Supplemental Type Certificate)
2017S04-02
NÚMERO:
(Number)
Este Cer ficado, emi do com base na Lei n° 7565 "Código Brasileiro de Aeronáu ca", de 19 de dezembro de
1986,
This Cer ficate, issued in the basis of the Law No 7565 "Código Brasileiro de Aeronáu ca", dated 19 December 1986,
é conferido ao (à): Garmin International, Inc.
is granted to:
1200 East 151st Street
Olathe, KS 66062
USA
por ter a modificação ao projeto de
po do produto abaixo citado, observadas as limitações e condições
for having the change to the type design of the product men oned below, with the limita ons and condi ons
especificadas, sa sfeito aos requisitos de aeronavegabilidade aplicáveis.
condi ons there for as specified hereon, met the applicable airworthiness requirements.
Produto Original ‐ Número do Cer ficado de Tipo: * See attached ANAC Approved Model List (AML),
Original Product ‐ Type Cer ficate No:
I.R., 04 Apr. 2017, or later approved revision.
Fabricante: *
Manufacturer:
Modelo(s): *
Model (s):
DESCRIÇÃO DA MODIFICAÇÃO AO PROJETO DE TIPO:
Description of Type
Design
C h a n g e:
Installation of Garmin G5 Electronic Flight Instrument in accordance with Garmin Master Drawing List
(MDL) Document No. 005-01112-01, Rev. 1, dated 22 July 2016, or later approved revision.
This CST validates in Brazil the STC No. SA01818WI, issued by FAA (USA).
LIMITAÇÕES E CONDIÇÕES:
Limitations and Conditions:
See continuation sheet for applicable data.
DATAS:
Do requerimento: 30 Jan. 2017
Da emissão:
Dates of:
Aplica on:
Issuance:
Da reemissão:
Da emenda:
Reissuance:
Amendment:
04 Apr. 2017
F‐400‐01G (SEI 03.17)
Fl. 01 de 02
H.02‐4823‐0
Nota:
(Note:)
a)
Este Cer ficado e os dados técnicos com base nos quais ele foi emi do são válidos até que sejam cancelados,
(This Cer ficate and the suppor ng technical data used for approval shall remain in effect un l surrended,
suspensos, revogados ou um prazo limite seja estabelecido pela Agência Nacional de Aviação Civil.
suspended, revoked or a termina on date is otherwise established by the Agência Nacional de Aviação Civil.)
b)
No caso de transferência de propriedade deste Cer ficado, o transferente deve preencher o quadro "Endosso
(In case of transfer of the property of this Cer ficate, the grantor should fill the blanks of
de Transferência", e o adquirente deve enviar este Cer ficado à Gerência Geral de Cer ficação de
“Transfer Endorsement”, and the transferee must remit this Cer ficate to the Gerência Geral de Cer ficação de
Produto Aeronáu co para que seja reemi do em seu nome.
Produto Aeronáu co to permit reissuance of the Cer ficate in his name.)
ENDOSSO DE TRANSFERÊNCIA
(Transfer Endorsement)
Transfiro a propriedade deste Certificado Suplementar de Tipo para:
(I transfer the property of this Supplemental Type Certificate to:)
ADQUIRENTE
(Transferee)
Nome: .................................................................................................................................................................
(Name:)
Rua: ..................................................................................................................................................................
(Street:)
CEP: .............................
Cidade: .......................................
Estado:....................
(Zip:)
(City:)
(State:)
País: ................................
(Country:)
TRANSFERENTE
(Grantor)
Nome: .................................................................................................................................................................
(Name:)
Rua: ..................................................................................................................................................................
(Street:)
CEP: .............................
Cidade: .......................................
Estado:....................
(Zip:)
(City:)
(State:)
Data de Transferência:
País: ................................
(Country:)
.............................................................................................................................
(Date of Transfer:)
Assinatura do Transferente:
..............................................................................................................................
(Signature of the Grantor:)
Nome: ...................................................................................................................
(Name:)
Cargo: ....................................................................................................................
(Func on:)
Folha de Continuação ao
(Continuation Sheet to)
CERTIFICADO SUPLEMENTAR DE TIPO
(Supplemental Type Certificate)
NÚMERO:
2017S04-02
(Number)
LIMITAÇÕES E CONDIÇÕES:
Limita ons and Condi ons:
I. The approval of this type design change should not be extended to other aircraft of these models on
which other previously approved modifications are incorporated unless it is determined by the installer
that the relationship between this change and any of those other previously approved modifications,
including changes in Type Design, will introduce no adverse effect upon the airworthiness of that
aircraft.
II. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall
give the other person written evidence of that permission.
III. Operation must be performed in accordance with the FAA approved Airplane Flight Manual
Supplement (AFMS) Document No. 190-01112-13, Rev. 1, dated 22 July 2016, or later approved
revision.
IV. The maintenance of the aircraft shall be performed in accordance with the Garmin G5 Maintenance
Manual, includes Instructions for Continued Airworthiness (ICA), Document No. 190-01112-11, Rev 1,
dated 22 July 2016, or later approved revisions.
V. The installation of the G5 requires the retention of the mechanical airspeed indicator, altimeter and
vertical speed indicator. If the G5 is installed as the primary attitude, it requires retention of the existing
rate of turn indicator. If installed in place of the rate of turn indicator, it requires retention of the existing
primary attitude indicator.
VI. The Certification Basis for parts changed or affected by this change, as specified on the FAA STC No.
SA01818WI is applicable.
VII. A copy of this Certificate, the Supplement referred on item III above and the ANAC Approved Model
List (AML) for CST No. 2017S04-02 shall be maintained as part of the permanent records of the
modified aircraft.
-----------------------------------------------------------------END-------------------------------------------------------------F‐400‐01G (SEI 03.17)
Fl. 02 de 02
H.02‐4823‐0
Documento assinado eletronicamente por MARIO IGAWA, Gerente-Geral de Certificação de Produtos Aeronáuticos, em
07/04/2017, às 10:28, conforme horário oficial de Brasília, com fundamento no art. 6º, § 1º, do Decreto nº 8.539, de 8 de outubro de
2015.
Documento assinado eletronicamente por ROBERTO JOSÉ SILVEIRA HONORATO, Superintendente de Aeronavegabilidade,
em 07/04/2017, às 16:45, conforme horário oficial de Brasília, com fundamento no art. 6º, § 1º, do Decreto nº 8.539, de 8 de outubro
de 2015.
A autenticidade deste documento pode ser conferida no site http://sistemas.anac.gov.br
/sei/controlador_externo.php?acao=documento_conferir&id_orgao_acesso_externo=0, informando o código verificador 0570659 e o
código CRC 9A751385.
ANAC LISTA DE MODELOS APROVADOS (LMA) PARA CST
(ANAC APPROVED MODEL LIST (AML) FOR (CST))
NÚMERO:
2017S04-02
(Number)
ITEM
AIRCRAFT MAKE
5
6
7
Alexandria Aircraft,
LLC
Alexandria Aircraft,
LLC
American Champion
Aircraft Corp
American Champion
Aircraft Corp
Aviat Aircraft, Inc.
Beechcraft Corporation
Beechcraft Corporation
8
Beechcraft Corporation
9
Beechcraft Corporation
10
Beechcraft Corporation
11
12
13
CPAC, Inc.
Daher Socata
Daher Socata
Diamond Aircraft
Industries Inc.
Dynac Aerospace
Corp.
Helio Aircraft LLC
Howard Aircraft
Foundation
1
2
3
4
14
15
16
17
18
Maule Aircraft Inc.
19
Maule Aircraft Inc.
20
21
Mooney Airplane
Company
Mooney Airplane
Company
22
Piper Aircraft
23
24
25
26
Piper Aircraft
Piper Aircraft
Piper Aircraft
Piper Aircraft
27
Piper Aircraft
28
29
30
Piper Aircraft
Piper Aircraft
Piper Aircraft
31
Piper Aircraft
AIRCRAFT MODEL (S)
TYPE
CERTIFICATE
NUMBER
17-30
1A3 (FAA)
17-30A
A18CE (FAA)
7ECA, 7GCAA, 7GCBC, 7KCAB
A-759 (FAA)
8KCAB, 8GCBC
A21CE (FAA)
A-1
D17S
23, A23, A23-24, C23, A24R, B24R
35-33, 35-A33, 35-B33, 35-C33, 35-C33A, E33A, E33C, F33A, F33C,
G33, H35, J35, K35, M35, N35, P35, S35, V35, V35A, V35B, 36, A36,
A36TC, B36TC
35, A35, B35, C35, D35, E35, F35, G35
D55, E55, 56TC, A56TC, 58, 95, B95, B95A, 95-55, 95-A55, 95-B55,
95-C55
112, 114
MS 885, MS 894E
TB 9, TB 10, TB 20, TB 21
9801 (ANAC)
A-649 (FAA)
A1CE (FAA)
A12SO (FAA)
7A14 (FAA)
9211 (ANAC)
DA20-C1
2009T04 (ANAC)
3A15 (FAA)
A-777 (FAA)
3A16 (FAA)
100
1A21 (FAA)
H-295, HT-295, H-391B
1A8 (FAA)
DGA-15P
A-717 (FAA)
MX-7-420, M-8-235, MX-7-160, MXT-7-160, MX-7-180A, MXT-7-180A,
MX-7-180B, M-7-235C
M-4, M‑4‑210C, M-6-235, M-7-235, MX‑7‑235, MX-7-180, MXT-7-180,
MT-7-235, MT-7-235B
9310 (ANAC)
3A23 (FAA)
M20J, M20K, M20M, M20R
8701 (ANAC)
M20A, M20B, M20C, M20E, M20F,
2A3 (FAA)
PA-18 "135", PA-18A "135", PA-18 "150",
PA-18A "150", PA-18, PA-18A
PA-20, PA-20 “135
PA-22, PA-22-108, PA-22-135, PA-22-150, PA-22-160
PA-23, PA-23-160, PA-23-235, PA-23-250
PA-24, PA-24-250, PA-24-260, PA-24-400
PA-28-140, PA-28-150, PA-28-151, PA-28-160, PA‑28-161, PA-28-180,
PA-28-235, PA‑28R-180, PA-28-181, PA‑28R‑200, PA-28R-201,
PA-28R-201T, PA‑28RT‑201, PA‑28RT-201T, PA‑28‑236
PA-38-112
PA-44-180 [see Limitations (1), (2) and (3)]
PA-30, PA-39
PA-32-260, PA-32-300, PA-32R-300, PA-32RT-300, PA-32RT-300T,
PA-32R-301(SP), PA‑32R-301(HP), PA-32R-301T, PA-32-301,
PA-32-301FT, PA32-301XTC
1A2 (FAA)
1A4 (FAA)
1A6 (FAA)
1A10 (FAA)
1A15 (FAA)
2A13 (FAA)
8402 (ANAC)
2013T06 (ANAC)
A1EA (FAA)
A3SO (FAA)
ITEM AIRCRAFT MAKE
AIRCRAFT MODEL (S)
32
33
Piper Aircraft
Sierra Hotel Aero, Inc
PA-34-200, PA-34-200T, PA-34-220T
Navion, Navion E, Navion G, Navion H
34
35
36
Sky Enterprises, Inc.
Textron Aviation Inc.
Textron Aviation Inc.
37
Textron Aviation Inc.
38
Textron Aviation Inc.
39
Textron Aviation Inc.
40
41
42
43
44
Textron Aviation Inc.
Textron Aviation Inc.
Textron Aviation Inc.
Textron Aviation Inc.
Textron Aviation Inc.
45
Textron Aviation Inc.
46
47
48
Textron Aviation Inc.
Textron Aviation Inc.
Textron Aviation Inc.
49
Textron Aviation Inc.
50
Textron Aviation Inc.
51
Textron Aviation Inc.
52
Textron Aviation Inc.
53
54
55
56
Textron Aviation Inc.
Textron Aviation Inc.
Textron Aviation Inc.
The Boeing Company
The WACO Aircraft
Company
True Flight Holdings
LLC
True Flight Holdings
LLC
Univair Aircraft
Corporation
RC-3
T-50
FR182
150, 150A, 150B, 150C, 150D, 150E, 150F, 150G, 150H,
150J, 150K, A150K, 150L, A150L, 150M, A150M, 152, A152
170, 170A, 170B
172, 172A, 172B, 172C, 172D, 172E, 172F, 172G, 172H (USAF T-41A),
172I, 172K, 172L, 172M, 172N, 172P, 172Q [see Limitation (3)]
172R, 172S [see Limitation (3)]
175, 175B, 172RG, R172K
177, 177A, 177B
177RG
180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J, 180K
182, 182A, 182B, 182C, 182D, 182E, 182F, 182G, 182H, 182J, 182K,
182L, 182M, 182N, 182P, 182Q, 182R, R182, T182, TR182
[see Limitation (3)]
182S, 182T, T182T [see Limitation (3)]
185, 185A, 185B, 185C, 185D, 185E, A185E, A185F
190, 195
206, P206A, P206B, P206C, P206D, P206E, TP206A, TP206B, TP206C,
TP206D, TP206E, U206, U206A, U206B, U206C, U206D, U206E,
U206F, U206G, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F,
TU206G [see Limitation (3)]
206H, T206H [see Limitation (3)]
210, 210A, 210B, 210C, 210D, 210E, 210F, T210F, 210G, T210G, 210H,
T210H, 210J, T210J, 210K, T210K, 210L, T210L, 210M, T210M, 210N,
T210N, 210R, T210R, 210-5 (205), 210-5A (205A)
310, 310A, 310B, 310C, 310D, 310E, 310F, 310G, 310H, E310H, 310I,
310J, E310J, 310K, 310L, 310N, 310P, 310Q, 310R, T310R
320A, 320C, 320E
336
337A, 337C, 337D, 337G
AT-6D (SNJ-5), T-6G
57
58
59
60
TYPE CERTIFICATE
NUMBER
A7SO (FAA)
A-782 (FAA)
A-769 (FAA)
A-722 (FAA)
A42EU (FAA)
3A19 (FAA)
A-799 (FAA)
3A12 (FAA)
9705 (ANAC)
3A17 (FAA)
A13CE (FAA)
A20CE (FAA)
5A6 (FAA)
3A13 (FAA)
9706 (ANAC)
3A24 (FAA)
A-790 (FAA)
A4CE (FAA)
1999T06 (ANAC)
3A21 (FAA)
3A10 (FAA)
3A25 (FAA)
A2CE (FAA)
A6CE (FAA)
A-2-575 (FAA)
YMF
2016T05 (ANAC)
AA-1
A11EA (FAA)
AA-5
A16EA (FAA)
108, 108-1, 108-2, 108-3
A-767 (FAA)
Limitations:
1. Excluding aircraft equipped with Avidyne Integra
2. Excluding aircraft equipped with Garmin G500
3. Excluding aircraft equipped with Garmin G1000
Aprovação ANAC:
MÁRIO IGAWA
Gerente-Geral, Certificação de Produto Aeronáutico
(ANAC Approval:)
(General Manager, Aeronautical Product Certification)
Data da aprovação ANAC: 04 Apr. 2017
(ANAC Approval Date:)
Revisão:
I. R.
(Revision:)
Documento assinado eletronicamente por MARIO IGAWA, Gerente-Geral de Certificação de Produtos Aeronáuticos, em 05/04/2017, às
17:07, conforme horário oficial de Brasília, com fundamento no art. 6º, § 1º, do Decreto nº 8.539, de 8 de outubro de 2015.
A autenticidade deste documento pode ser conferida no site http://sistemas.anac.gov.br
/sei/controlador_externo.php?acao=documento_conferir&id_orgao_acesso_externo=0, informando o código verificador 0570729 e o código
CRC 1C3FE06A.
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