CERTIFICADO DE HOMOLOGAcA0

Transcrição

MINISTERIO DA DEFESA
COMANDO DA AERONAUTICA
DEPARTAMENTO DE PESQUISAS E DESENVOLVIMENTO
CENTRO TECNICO AEROESPACIAL
INSTITUTO DE FOMENTO E COORDENAcA0 INDUSTRIAL
CERTIFICADO DE HOMOLOGAcA0 SUPLEMENTAR DE TIPO
(Supplemental Type Certificate)
2004S10-04
NOMERO
(Number)
Este certificado, emitido corn base na Lei n°- 7565 "Codigo Brasileiro de Aeronautica", de 19 de dezembro de 1986,
(This certificate, issued in the basis of the Law No. 7565 Codigo Brasileiro de Aeronautica", dated 19 December 1986,
e conferido ao (a): J.P.Instruments.
is granted to:)
3185-B Airway Ave
Costa Mesa, CA 92626
USA
por ter a modificacao ao projeto de tipo do produto abaixo citado, observadas as limitagoes e condigiies
(for having the change to the type design of the product mentioned below, with the limitations and conditions
therefor a s )
especificadas, satisfeito aos requisitos de aeronavegabilidade aplicaveis.
(specified hereon, met the applicable airworthiness requirements.)
Produto Original - Numero do Certificado de Tipc • * see attached CTA Approved Model List, I.R.,dated
(Original Product — Type Certificate No:)
27 Oct. 2004, or later CTA approved revisions.
Fabricante:
(Manufacturer:)
Modelo(s):
(Model(s):)
DESCRIcA0 DA MODIFICA00 AO PROJETO DE TIPO:
(Description of Type Design Change:)
Installation of J.P.Instruments temperature monitoring systems in accordance with
J.P.Instruments Drawing List Report No. 100, Rev. E, dated 17 Jun. 1999, or later approved
revisions.
This CHST validates in Brazil the STC # SA2586NM, issued by FAA (USA).
LIMITAgOES E CONDIcOES:
(Limitations and Conditions:)
See continuation sheet for applicable data.
DATAS:
(Dates of:)
Do Requerimento: 07 Apr. 2004
(Application:)
Da emissao: 27 Oct. 2004
(Issue:)
CLA DIO PASSOS S AO Ten Cel Eng
Chefe da Divisao de Certificagao de Aviacao Civil
Fl. 01 de 02
(Sheet) (of)
(Reissue:)
V NANCIO
Diretor
(Chief, Divisdo de Certificacao de Aviacao Civil)
F-400-01B (08.04)
Da reemissao:
Cel Eng
e omento e oordenagao Industrial
(Director, Institute d Fomento e Coordenagao Industrial)
H.02-2293-0
Folha de Continuacao ao
.Ilsontinuation Sheet to)
CERTIFICADO DE HOMOLOGAgA0 SUPLEMENTAR DE TIPO
(Supplemental Type Certificate)
NOMERO
(Number)
2004S10-04
LIMITAcOES E CONDIcOES:
(Limitations and Conditions:)
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 FAA approved Airplane / Rotorcraft Flight
Manual Supplement No. 1 for EGT-701 temperature indicator, Rev. B, dated 17 Jun. 1999,
or later approved revisions.
IV.
Cylinder head, oil, turbine inlet and/or exhaust gas temperature, fuel flow equipment,
tachometer instruments, and manifold pressure instruments required by the original type
design, or if required by other FAA/CTA approval, must remain installed and operable.
V.
Aircraft listed on the CTA Approved Model List for CHST 2004S10-04 and that have been
previously modified with a fuel flow indication system that utilizes the flowscan fuel flow
transducer (P/N: 201-A, 201-B, 201-C, or 231 or equivalent as listed on FAA Approved
Installation Instructions, Drawing 103) are eligible for installation of the EGT-701 fuel flow
option.
VI.
This certificate does not constitute installation approval of the fuel flow transducer.
VII.
EGT-701 temperature indicator wi.:1 tachometer (rpm) and manifold pressure options are
eligible for the 4cylinder an 6 cylinder engines listed on the FAA approved Master Eligibility
List (MEL) SA2586NM only.
VIII.
Eligible dash numbers for the EGT-701 are listed on the FAA approved Master Eligibility
List (MEL) SA2586NM.
IX.
A copy of this Certificate and the Airplane / Rotorcraft Flight Manual Supplement, referred
on item III above, shall be maintained as part of the permanent records of the modified
aircraft.
END
F-400-01 B (08.04)
FL 02 de 02
(Sheet) (of)
H.02-2293-0
CTA APPROVED MODEL LIST
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
AIRCRAFT
MODEL(S)
1
2
S-2R
8KCAB
4
Ayres Corp.
American Champion
Aircraft Corp.
American Champion
Aircraft Corp.
Beech Aircraft Corporation
5
6
7
8
3
7GCAA
7GCBC
D18C
D185
E185
C-45H
TC-45H
G185
3NN
D17S
23
A23
A23-24
C23
A24R
B24R
35
A35
B35
C35
D35
F35
E33A
F33A
G33
35-33
35-A33
35-B33
35-C33
35-C33A
H35
K35
M35
N35
P35
S35
V35
V35A
V35B
36
A36
A36TC
B36TC
Fl. 1 of 8
TYPE
CERTIFICATE
N°
A3SW (FAA)
A210E (FAA)
CERTIFICATION
BASIS
A-759 (FAA)
CAR 4a
A-765 (FAA)
CAR 3
A-649 (FAA)
Al CE (FAA)
CAR 3
CAR 3
A-777 (FAA)
CAR 3
3A15 (FAA)
CAR 3
CAR 3
FAR 23
H.02-2293-0
INSTITUTO DE FOMENTO E COORDENACAO INDUSTRIAL
FOR CHST 2004510-04
ITEM
AIRCRAFT
MAKE
AIRCRAFT
MODEL(S)
9
10
11
12
13
14
15
16
17
Bellanca
Boeing
Cessna Aircraft Company
D50
D50A
D5OB
58
95
B95
B95A
95-55
95-A55
95-B55
95-055
D55
E55
56TC
A56TC
58P
58TC
60
A60
B60
65
65-80
65-A80
65-88
65-B80
A65
70
17-30-A
A75
140
150
150D
150E
150F
150G
150H
150J
150K
Al 50K
150L
A150L
150M
A150M
152
A152
Fl. 2 of 8
TYPE
CERTIFICATE
N°
5A4 (FAA)
CERTIFICATION
BASIS
3A16 (FAA)
CAR 3
A23CE (FAA)
FAR 23
Al2CE (FAA)
FAR 23
3A20 (FAA)
FAR 23
A18CE
A-743 (FAA)
A-768 (FAA)
3A19 (FAA)
FAR 23
CAR 4a
CAR 3
CAR 3
CAR 3
H.02-2293-0
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
AIRCRAFT
MODEL(S)
18
19
20
21
22
23
24
170
170A
170B
172
172A
172B
172C
172D
172E
172F
172G
172H
1721
172K
172L
172M
172N
172P
172RG
R172K
175
172R
172S
177
177A
1778
177RG
180
180A
180B
180C
180D
180E
180F
180G
180H
180J
180K
182
182A
182B
182C
182D
182E
182F
182G
182H
182J
Fl. 3 of 8
,k, ,-Ad )
TYPE
CERTIFICATE
N°
A-799 (FAA)
CERTIFICATION
BASIS
3A13 (FAA)
CAR 3
3A17 (FAA)
CAR 3
9705 (CTA)
RBHA 23 / FAR 23
A13CE (FAA)
FAR 23
A2OCE (FAA)
5A6 (FAA)
FAR 23
CAR 3
CAR 3
H.02-2293-0
INSTITUTO DE FOMENTO E COORDENAQAO INDUSTRIAL
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
24
25
26
27
28
29
30
31
AIRCRAFT
MODEL(S)
182K
182L
182M
182N
182P
182Q
182R
182S
T182T
185
185A
185B
185E
A185E
A185F
188
A188
A188A
A188B
T188C
195
190
206
206B
206D
206E
U206
U206A
U206B
U206C
U206D
U206E
U206F
U206G
TU206F
TU206G
206H
T206H
207
207A
T207
T207A
210
210A
210B
210C
210D
210E
Fl. 4
TYPE
CERTIFICATE
N°
CERTIFICATION
BASIS
9706 (CTA)
RBHA 23 / FAR 23
3A24
CAR 3
A9CE (FAA)
FAR 21
A-790 (FAA)
CAR 3
A4CE (FAA)
CAR 3
1999T06-01
RBHA 23 / FAR 23
A16CE
FAR 23
3A21
,
CAR 3
H.02-2293-0
of 8
1,*
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
32
33
34
35
36
AIRCRAFT
MODEL(S)
210F
210-5
210H
210J
210K
210J
210K
210L
T210L
210M
210N
P210N
T210N
210R
310
3108
310C
310D
310F
310G
310H
3101
310J
310K
310L
310N
310P
310Q
31OR
T31OR
320A
320C
320E
340
336
337A
337C
337D
337G
401
402
4028
402C
411
411A
414
414A
Fl. 5 of 8
TYPE
CERTIFICATE
N°
CERTIFICATION
BASIS
3A10 (FAA)
CAR 3
3A25 (FAA)
CAR 3
A2CE (FAA)
A6CE (FAA)
CAR 3
CAR 3
A7CE (FAA)
CAR 3
H.02-2293-0
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
37
Consolidated Aeronautical
38
39
Consolidated Aeronautical
De Havilland
40
Enstrom Helicopter
41
Grumman (American
General Aircraft)
Grumman (American
General Aircraft)
Gulfstream American
(Twin Commander)
42
43
44
Gulfstream American
(Twin Commander)
45
Hughes Helicopter
46
47
Jobmaster Company
Maule
48
Maule
49
Mooney
50
North American
AIRCRAFT
MODEL(S)
TYPE
CERTIFICATE
N°
CERTIFICATION
BASIS
1A13 (FAA)
FAR 23; 36
CAR 3
8704 (CTA)
A-22 (FAA)
RBHA 23 / FAR23
CAR 10
421
421B
421C
LA-4
LA-4A
LA-4-200
LAKE 250
DHC-2 Mk.l
DHC-2 Mk.II
F-28A
F-28F
AA-1
H10E (FAA)
CAR 6
Al 1EA (FAA)
FAR 23
AA-5
A16EA (FAA)
FAR 23
500
500B
500U
500S
520
560
560F
680-E
680F
680FL
269A
269A-1
269B
269C
DGA-15P
MXT-7-180
MX-7-180
M-4
M-6-235
MX-7-235
M-7-235
M-7-235B
MXT-7-180A
MX-7-180A
MX-7-180B
M-7-235C
M20A
M2OB
M20C
M20E
M2OF
AT-6D
6A1 (FAA)
CAR 3
2A4 (FAA)
FAR 23
4H12 (FAA)
CAR 6
A-717 (FAA)
3A23 (FAA)
CAR 4a
CAR3
9310 (CTA)
RBHA 23 / FAR 23
2A3 (FAA)
CAR 3
A-2-575 (FAA)
CAR 4a
Fl. 6 of 8
_
H.02-2293-0
_
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
51
Piper Aircraft
52
,
Piper Aircraft
53
Piper Aircraft
54
Piper Aircraft
55
Piper Aircraft
56
Piper Aircraft
57
Piper Aircraft
58
Piper Aircraft
59
60
Piper Aircraft
Piper Aircraft
AIRCRAFT
MODEL(S)
T-6G
PA-18
PA-18"105"(Special)
PA-18A
PA-18"135"(Army L-21B)
PA-18"150"
PA-18A"150"
PA-20
PA-20-"135"
PA-22
PA-22-108
PA-22-135
PA-22-160
PA-23
PA-23-160
PA-23-250
PA-24
PA-24-250
PA-24-260
PA-28-140
PA-28-150
PA-28-151
PA-28-160
PA-28-161
PA-28-180
PA-28R-180
PA-28-181
PA-28R-200
PA-28-236
PA-28-235
PA-28R-201
PA-28R-201T
PA-28RT-201
PA-28RT-201T
PA-30
PA-39
PA-31
PA-31-300
PA-31-325
PA-31-350
PA-31P
PA-32-260
PA-32-300
PA-32R-301
PA-32R-301T
TYPE
CERTIFICATE
N°
CERTIFICATION
BASIS
1A2 (FAA)
CAR 3
1A4 (FAA)
CAR 3
1A6 (FAA)
CAR 3
1A1 0 (FAA)
CAR 3
1A15 (FAA)
CAR 3
2A13 (FAA)
CAR 3
Al EA (FAA)
CAR 3
A20S0 (FAA)
CAR 3 / FAR 23
A8EA (FAA)
A3S0 (FAA)
CAR 3 / FAR 23
CAR 3
71
Fl. 7 of 8
H.02-2293-0
FOR CHST 2004S10-04
ITEM
AIRCRAFT
MAKE
AIRCRAFT
MODEL(S)
61
Piper Aircraft
62
63
64
Piper Aircraft
Piper Aircraft
Robinson Helicopter
65
66
Robinson Helicopter
S.O.C.A.T.A
67
Swift
68
Thompson (Navion)
68
69
White Inter. (AVIAT)
Weatherly
PA-34-200
PA-34-200T
PA-34-220T
PA-38-112
PA-46-350P
R22
R22 ALPHA
R22 BETA
R22 MARINER
R44
TB9
TB10
TB20
TB21
GC-1A
GC-1B
Navion E
Navion G
Navion H
A-1 (Husky)
620A
620B
,
TYPE
CERTIFICATE
N°
A7S0 (FAA)
CERTIFICATION
BASIS
8402 (CTA)
9501 (CTA)
8714 (CTA)
RBHA 23 / FAR 23
RBHA 23 / FAR 23
RBHA 23 / FAR 27
9402 (CTA)
9211 (CTA)
RBHA 27 / FAR 27
RBHA 23 / FAR 23
A-766 (FAA)
CAR 4a
A-782 (FAA)
CAR 3
9801 (CTA)
9309 (CTA)
RBHA 23 / FAR 23
RBHA 21 / FAR 21
FAR 23
CTA Approved:
Claudio Passos Simao Ten Cel Eng
Chief, Divisao de Certificacao de Aviacao Civil
CTA Approved Date:
Revision:
27 OUT. 2004.
I.R.
Fl.
8 of 8
H.02-2293-0

CERTIFICADO DE HOMOLOGAcA0

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