pp-wac - mapa de controle de inspeÇÕes (cÉlula)data do Último voo: 04/09/2017 data de emissÃo:...

NG 3.387,44

NTL 3.124,92

DATA DO ÚLTIMO VOO: 04/09/2017

DATA DE EMISSÃO: 17/06/2019

HORAS DIAS POUSOS HORAS DATA POUSOS HORAS DATA POUSOS HORAS DIAS POUSOS

RBHA 91.409(a) IAM - INSPEÇÃO ANUAL DE MANUTENÇÃO - - - 365 - 4436,5 09/set/16 - - 9-set-17 - - -646 -

IS-21-181-001B CERTIFICADO DE AERONAVEGABILIDADE - - - 2190 - - 04/out/11 - - 2-out-17 - - -623 -

MPR 100. LICENÇA DE ESTAÇÃO - - - 2190 - - 21/mar/12 - - 21-mar-21 - - 643 -

RBHA 91.423. PESO E BALANCEAMENTO - - - 1825 - - 28/mai/13 - N/A N/A N/A N/A N/A N/A

CBAer Art. 158/1º SEGURO RETA MAPFRE - - 365 - - 07/mar/19 - - 6-mar-20 - - 263 -

MPR 100. TAXA FISTEL - - - 365 - - 31/mar/19 - - 30-mar-20 - - 287 -

RBHA 43 - APÊNDICE E ALTÍMETRO 5934PM-3 414787 - 730 - 4566,4 27/jun/17 - - 27-jun-19 - - 10 -

RBHA 43 - APÊNDICE F TRANSPONDERGTX327

011-00490-0083703859 - 730 - 4566,4 27/jun/17 - - 27-jun-19 - - 10 -

RBHA 43 - APÊNDICE E MODO C D120-P2-T 77607 - 730 - 4566,4 27/jun/17 - - 27-jun-19 - - 10 -

RBHA 43 - APÊNDICE ECHECK DO SISTEMA DE PRESSÃO ESTÁTICA

(ANEMOBAROMÉTRICO)- - - 730 - 4566,4 27/jun/17 - - 27-jun-19 - - 10 -

RBHA 91.207 INSPEÇÃO ANUAL DO ELT KANNAD 406-AF S1822502-02 - 365 - 4566,4 27/jun/17 - - 27-jun-18 - - -355 -

RBHA 91.401 COMPENSAÇÃO DA BÚSSOLA 621396-231 8429 - 365 - 4275,9 07/jul/15 12434 - 6-jul-16 - - -1076 -

RBHA 91.513 e RBHA 91.409 KIT DE PRIMEIROS SOCORROS - - - 365 - - 30/mai/17 - - 30-mai-18 - - -383 -

RBHA 91.513 e RBHA 91.409 KIT DE PRIMEIROS SOCORROS (PRÓXIMO VENCIMENTO) - - - - - - - - - 1-jan-18 - - -532 -

- PESAGEM DO EXTINTOR - - - 180 - 4546,9 16/mai/17 - - 12-nov-17 - - -582 -

RBHA 91.513 e RBHA 91.409 COLETES SALVA-VIDASP0723E109P

(KSD-35L8)221884 - 365 - - 09/set/16 - N/A N/A N/A N/A N/A N/A









CMM 25-60-12. COLETES SALVA-VIDAS - RECERTIFICAÇÃOP0723E109P

(KSD-35L8)221884 - 1825 - - 07/mai/14 - - 6-mai-19 - - -42 -

CAPÍTULO

S/N

4588,3

HORAS

13.341

DESCRIÇÃO

1185

POUSOS / CICLOS

MOTOR ARRIUS 2F 34708 2715,9

CÉLULA EC120B

MODELO

PP-WAC - MAPA DE CONTROLE DE INSPEÇÕES (CÉLULA)

EC120B MSM - MASTER SERVICING MANUAL REVISION 004: 2018.04.16

EC120B ALS - AIRWORTHINESS LIMITATIONS SECTION REVISION 004: 2018.03.26

P/NPRÓXIMO CUMPRIMENTO

S/NÚLTIMO CUMPRIMENTOINTERVALO DISPONÍVEL

Página 1 de 19

NG 3.387,44

NTL 3.124,92



HORAS DIAS POUSOS HORAS DATA POUSOS HORAS DATA POUSOS HORAS DIAS POUSOSCAPÍTULO

S/N

4588,3

HORAS

13.341

DESCRIÇÃO

1185

POUSOS / CICLOS


CÉLULA EC120B

MODELO







(KSD-35L8)285034 - 1825 - - 07/mai/14 - - 6-mai-19 - - -42 -


(KSD-35L8)285045 - 1825 - - 07/mai/14 - - 6-mai-19 - - -42 -


(KSD-35L8)303409 - 1825 - - 07/mai/14 - - 6-mai-19 - - -42 -


(KSD-35L8)303411 - 1825 - - 14/jan/15 - - 13-jan-20 - - 210 -

SAFT CMM 24-33-96

BATTERY PERIODICAL CHECK (6 MESES)

(SUBTASK 24-33-96-210-001)

Obs: item da inspeção de 6 meses (MSM Chapter 05-25-00)

151CH1 X026670 - 180 - 4525,8 24/mar/17 - - 20-set-17 - - -635 -

SAFT CMM 24-33-96

BATTERY REGULAR CHECK (12 MESES)

(SUBTASK 24-33-96-210-002)


151CH1 X026670 - 365 - 4525,8 24/mar/17 - - 24-mar-18 - - -450 -

SAFT CMM 24-33-96.

BATTERY GENERAL OVERHAUL (24 MESES)

(SUBTASK 24-33-96-210-003

SUBTASK 24-33-96-280-001

SUBTASK 24-33-96-280-001 )


151CH1 X026670 - 730 - 4525,8 24/mar/17 - - 24-mar-19 - - -85 -

- CARTÃO DO GPS - - - 365 - 4436,5 09/set/16 - - 9-set-17 - - -646 -

MSM 05-20 - PERIODIC INTERVALS - - - - - - - - - - - - - -

05-20-00. BFF / ALF INSPECTION - - 10 - - 4586,8 25/jul/17 - N/A N/A N/A N/A N/A N/A

05-20-02. 15 HOURS / 7 DAYS INSPECTION - - 15 7 - 4588,3 08/ago/17 - 4603,3 15/ago/17 - 15,0 -671 -


05-21-00. 100 HOURS / 12 MONTHS INSPECTION - - 100 365 - 4537,5 24/abr/17 - 4637,5 24/abr/18 - 49,2 -419 -

05-21-01. 100 HOURS INSPECTION - - 100 - - 4586,8 25/jul/17 - 4686,8 - - 98,5 - -

05-21-02. 12 MONTHS INSPECTION - - - 365 - 4436,5 09/set/16 - - 09/set/17 - - -646 -


05-22-00. 500 HOURS / 24 MONTHS INSPECTION - - 500 730 - 4275,9 07/jul/15 12434 4775,9 06/jul/17 - 187,6 -711 -

05-22-02. 24 MONTHS INSPECTION - - - 730 - 4275,9 07/jul/15 12434 - 06/jul/17 - - -711 -


Página 2 de 19

NG 3.387,44

NTL 3.124,92




S/N

4588,3

HORAS

13.341

DESCRIÇÃO

1185

POUSOS / CICLOS


CÉLULA EC120B

MODELO






05-23-00. 1500 HOURS / 72 MONTHS INSPECTION - - 1500 2190 - 3842,0 13/jun/13 - 5342,0 12/jun/19 - 753,7 -5 -

05-23-02. 72 MONTHS INSPECTION - - - 2190 - 3842,0 13/jun/13 - - 12/jun/19 - - -5 -

AMM 05-24 - PERIODIC INTERVALS - - - - - - - - - - - - - -

05-24-02. 144 MONTHS INSPECTION - - - 4380 - 3842,0 13/jun/13 - - 10/jun/25 - - 2185 -

MSM 05-25 - SPECIFIC PERIODIC INTERVALS - - - - - - - - - - - - - -

05-25-00. 1 MONTH INSPECTION - - - 30 - 4586,8 25/jul/17 - - 24/ago/17 - - -662 -

05-25-00. 6 MONTHS INSPECTION - - - 180 - 4525,8 24/mar/17 - - 20/set/17 - - -635 -

05-25-00. 18 MONTHS INSPECTION - - - 540 - - 17/jan/01 - N/A N/A N/A N/A N/A N/A

05-25-00. 48 MONTHS INSPECTION - - - 1460 - - 13/jun/13 - N/A N/A N/A N/A N/A N/A


05-25-00. 300 HOURS INSPECTION - - 300 - - 4537,5 24/abr/17 - 4837,5 - - 249,2 - -

05-25-00. 600 HOURS INSPECTION - - 600 - - - N/A - N/A N/A N/A N/A N/A N/A

05-25-00. 1200 HOURS INSPECTION - - 1200 - - - N/A - N/A N/A N/A N/A N/A N/A

05-25-00. 100 HOURS / 3 MONTHS INSPECTION - - 100 90 - 4566,4 27/jun/17 - 4666,4 25/set/17 - 78,1 -630 -

05-25-00. 1000 HOURS / 24 MONTHS INSPECTION - - 1000 730 - 4310,7 25/set/15 0 5310,7 24/set/17 - 5310,7 -631 -

MSM 05-26 - PUNCTUAL INTERVALS - - - - - - - - - - - - - -

05-26-00. 2 HOURS INSPECTION - ATA 53 - CABIN ANTIVIBRATOR SUPPORT - - 2 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 2 HOURS INSPECTION - ATA 62 - MAIN ROTOR - - 2 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00.2 HOURS INSPECTION - ATA 62 - MAST - SCISSORS DRIVE

COUPLING- - 2 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 2 HOURS INSPECTION - ATA 63 - MAIN ROTOR DRIVE - - 2 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 2 HOURS INSPECTION - ATA 64 - TAIL ROTOR - - 2 - - - N/A - N/A N/A N/A N/A N/A N/A

Página 3 de 19

NG 3.387,44

NTL 3.124,92




S/N

4588,3

HORAS

13.341

DESCRIÇÃO

1185

POUSOS / CICLOS


CÉLULA EC120B

MODELO






05-26-00. 10 HOURS INSPECTION - ATA 28 - STRAINERS - - 10 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 30 HOURS INSPECTION - ATA 63 - MGB - - 30 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 30 HOURS INSPECTION - ATA 65 - TGB - - 30 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 30 HOURS INSPECTION - ATA 67 - SERVOCONTROL - - 30 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 100 HOURS INSPECTION - ATA 28 - STRAINERS - - 100 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 100 HOURS INSPECTION - ATA 62 - MAIN ROTOR BLADE - - 100 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 200 HOURS INSPECTION - ATA 62 - MAIN ROTOR BLADE - - 200 - - - N/A - N/A N/A N/A N/A N/A N/A

05-26-00. 72 MONTHS INSPECTION - ATA 25 - FLOAT - - - 2190 - - N/A - N/A N/A N/A N/A N/A N/A



AMM 05-30 - PERIODIC INTERVALS - - - - - - - - - - - - - -

05-30-00. BFF / ALF INSPECTION - - 10 - - - - - N/A N/A N/A N/A N/A N/A

05-30-00. 15 HOURS / 7 DAYS INSPECTION - - 15 7 - - - - N/A N/A N/A N/A N/A N/A

INSPEÇÕES AVANTTO - - - - - - - - - - - - - -

INSPEÇÃO AVANTTOVERIFICAÇÃO DO NÍVEL DE ÓLEO DO COMPRESSOR DO AR-

CONDICIONADO- - 50 - - 4580,9 13/jul/17 - 4630,9 - - 42,6 - -

INSPEÇÃO AVANTTO VERIFICAÇÃO DOS DOCUMENTOS DE PORTE OBRIGATÓRIO - - - 90 - - 26/abr/17 - - 25-jul-17 - - -692 -

INSPEÇÃO AVANTTO VERIFICAÇÃO DOS DOCUMENTOS PARA PROTOCOLO DE RCA - - - 518 - - 09/set/17 - - 9-fev-19 - - -128 -

INSPEÇÃO AVANTTO CHECK DE HEADSET - - - 7 - - 12/set/18 - - 19/set/18 - - -271 -

Página 4 de 19

NG 3.387,44

NTL 3.124,92




MSM 05-10 COMPONENTS SUBJECT TO TBO - - - - - - - - - - - - - -

05-10-00.STARTER GENERATOR

(Intervalo ajustado em 70% do TBO)160SG140Q-1 REMOVIDO 630 - - 4566,4 28/jun/17 - 4502,0 - - -86,3 - -

05-10-00. EPICYCLIC MODULE C632A0101052 REMOVIDO 5000 8760 - 3804,7 08/nov/00 - 5797,4 02/nov/24 - 1209,1 1965 -

05-10-00. MAIN MODULE C632A0201052 REMOVIDO 3750 8760 - 3932,0 08/nov/00 - 6343,3 02/nov/24 - 1755,0 1965 -

05-10-00. TGB C652A0101055 M 260 5000 8760 - 3926,7 07/nov/07 - 8454,3 01/nov/31 - 3866,0 4520 -

05-10-00. Main servocontrol SC5091-1 REMOVIDO 4000 7300 - 4118,5 21/nov/13 - 8118,5 16/nov/33 - 3530,2 5266 -

05-10-00. Main servocontrol SC5091-1 REMOVIDO 4000 7300 - 4537,5 26/abr/17 - 8537,5 21/abr/37 - 4249,2 6518 -

05-10-00. Main servocontrol SC5091-1 REMOVIDO 4000 7300 - 4537,5 26/abr/17 - 8537,5 21/abr/37 - 4249,2 6518 -

MSM 05-11 COMPONENTS SUBJECT TO OTL - - - - - - - - - - - - - -

05-11-00. COOLING BELT4PK730

(7050A3632293)- 1500 2190 - 3606,9 06/mar/12 9752 5106,9 05/mar/18 - 518,6 -469 -

05-11-00. BATTERY PACK KANNAD 406 AF-H - 1 OPH 1825 - 4275,9 26/jun/15 12480 - 24/jun/20 - - 373 -

05-11-00. CYLINDER / FLOAT / COVER ASSEMBLY - - - 5475 - 0,0 17/jan/01 0 N/A N/A N/A N/A N/A N/A

05-11-00. CABIN FIRE EXTINGUISHERH1-10AIR

(704A32810008)0948212FA - 3650 - - 11/jan/10 - - 09/jan/20 - - 206 -

05-11-00. CHRONOMETER - LITHIUM BATTERY CR2032 - - 1460 - 0,0 17/jan/01 0 N/A N/A N/A N/A N/A N/A

05-11-00. Swashplate bearing 7050A3623013 07-10540 3000 - - 2996,4 21/mai/08 - 5996,4 - - 1408,1 - -

05-11-00. Tail rotor drive bearing 7050A3651001REMOVIDO O SN 7592 E INSTALADO NO WAB3000 - - 2955,8 06/jan/11 - 5955,8 - - 0,0 - -

MSM 04-10 AIRWORTHINESS LIMITATIONS (SLL) - - - - - - - - - - - - - -

04-10-00. LH COUNTER-TORQUE FITTING C533C3207101 99205 - - 82000 0,0 17-jan-01 0 - - 82000 - - 68659

04-10-00. RH COUNTER-TORQUE FITTING C533C3206101 99192 - - 82000 0,0 17-jan-01 0 - - 82000 - - 68659

04-10-00. LH MGB ATTACHMENT BAR FITTING C533C3204103 99199 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. RH MGB ATTACHMENT BAR FITTING C533C3203103 99203 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR

PP-WAC - MAPA DE CONTROLE DE COMPONENTES (CÉLULA)

CAPÍTULODISPONÍVEL

DESCRIÇÃO P/N S/N

MODELO S/N HORAS POUSOS / CICLOS

INTERVALO ÚLTIMO CUMPRIMENTO PRÓXIMO CUMPRIMENTO

ARRIUS 2F



Página 5 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F



04-10-00. REAR MGB ATTACHMENT BAR FITTING C533C3205102 99388 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. REAR MGB ATTACHMENT BAR FITTING C533C3205102 99389 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. MAIN ROTOR BLADE C621A1006103 2026 20000 - - 4525,8 24-mar-17 12406 22667,2 - - 18078,9 - -



04-10-00. EQUIPPED MAIN HUB C622A1002103 M126 6400 - - 0,0 17-jan-01 0 6400,0 - - 1811,7 - -

04-10-00. EQUIPPED SCISSOR DRIVE C622A1003103 MAP722 20000 - - 3642,3 23-mai-12 9856 23642,3 - - 19054,0 - -

04-10-00. UPPER ADAPTOR FITTING C622A1007105 MAP770 20000 - - 4106,9 19-fev-14 11983 24106,9 - - 19518,6 - -



04-10-00. LOWER ADAPTOR FITTING C622A1006105 MAP1196 20000 - - 4332,9 31-out-15 12576 24332,9 - - 19744,6 - -

04-10-00. LOWER ADAPTOR FITTING C622A1006105 MAP1154 20000 - - 4332,9 31-out-15 12576 24332,9 - - 19744,6 - -

04-10-00. LOWER ADAPTOR FITTING C622A1006104 M665 5200 - - 4332,9 31-out-15 0 5154,3 - - 566,0 - -

04-10-00. SPHERICAL BEARING - METALLIC PART579-108-00

(7050A3622022)0498 7500 - - 0,0 17-jan-01 0 7500,0 - - 2911,7 - -


(7050A3622022)0504 7500 - - 0,0 17-jan-01 0 7500,0 - - 2911,7 - -


(7050A3622022)0683 7500 - - 0,0 17-jan-01 0 7500,0 - - 2911,7 - -

04-10-00. SPHERICAL BEARING SPECIAL SCREW 7050A3622037 2520 9300 - - 863,9 16-set-06 1856 10163,9 - - 5575,6 - -





Página 6 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F




04-10-00. UPPER SLEEVE FLANGE C622A2008101 M174 11000 - - 0,0 17-jan-01 0 11000,0 - - 6411,7 - -



04-10-00. LOWER SLEEVE FLANGE C622A2009101 M409 11000 - - 0,0 17-jan-01 0 11000,0 - - 6411,7 - -



04-10-00. EQUIPPED PICTH LEVER C622A2002103 DA74 11400 - - 0,0 17-jan-01 0 11400,0 - - 6811,7 - -



04-10-00. LEAD LAG DAMPER - METTALIC PARTE4069F12

(7050A3622044)0587 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -


(7050A3622044)0607 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -


(7050A3622044)0608 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. BLADE PIN C622A2006601 M1803 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. BLADE PIN C622A2006601 M1819 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. BLADE PIN C622A2006602 M629 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. BLADE PIN C622A2006602 M669 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. BLADE PIN C622A2006602 M676 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. BLADE PIN C622A2006602 M695 9800 - - 863,9 16-set-06 1856 10663,9 - - 6075,6 - -

04-10-00. ADAPTOR END1211023P

(7050A3622023)780 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. ADAPTOR END1211023P

(7050A3622023)785 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

Página 7 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F



04-10-00. ADAPTOR END1211023P

(7050A3622023)800 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. ADAPTOR END1211024P

(7050A3622024)865 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. ADAPTOR END1211024P

(7050A3622024)912 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. ADAPTOR END1211024P

(7050A3622024)919 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. THRUST SCREW C622A1043201 1215 13900 - - 3842,0 13-jun-13 10389 17742,0 - - 13153,7 - -






04-10-00. EQUIPPED NON-ROTATING STAR C623A1001103 M193 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED ROTATING STAR C623A1002102 M161 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED SCISSOR LINK C623A2005102 DA257 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED SCISSOR LINK C623A2005102 DA117 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED DIAPASON SCISSOR LINK C623A2004102 DA280 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED DIAPASON SCISSOR LINK C623A2004102 DA272 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. EQUIPPED BLADE ANGLE ROD C623A3001102 703 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -



04-10-00. SHAFT CONNECTING C631A1102601 SP179 - - 89000 0,0 17-jan-01 0 - - 89000 - - 75659

04-10-00. ARM ASSY C631A1101101 DA86 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

Página 8 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F



04-10-00. MAIN ROTOR MAST C632A1110102 REMOVIDO - - 78000 0,0 17-jan-01 0 - - 78000 - - 64659

04-10-00. TAPPERED CASE C632A1111101 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. RING GEAR FIXED C632A1102602 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. PLANET GEAR UNEQUIPPED C632A1103601 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -




04-10-00. BI-BEVEL WHEEL C632A2102605 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. LOWER HOUSING C632A2115102 REMOVIDO - - 70000 0,0 17-jan-01 0 - - 70000 - - 56659

04-10-00. MAIN HOUSING C632A2116102 REMOVIDO - - 70000 0,0 17-jan-01 0 - - 70000 - - 56659

04-10-00. SUN GEAR C632A2106602 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. BOX OUTPUT C632A2114102 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. INPUT BEVEL GEAR C632A2110603 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. SHAFT FREE WHEEL C632A2111601 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. INPUT FLANGE C632A2112601 REMOVIDO - - 120000 0,0 17-jan-01 0 - - 120000 - - 106659

04-10-00. OUTPUT PINION C632A2107602 REMOVIDO 8900 - - 0,0 17-jan-01 0 8900,0 - - 4311,7 - -

04-10-00. OUTPUT WHEEL C632A2108602 REMOVIDO 9500 - - 0,0 17-jan-01 0 9500,0 - - 4911,7 - -

04-10-00. FLANGE OUTPUT C632A2158201 REMOVIDO 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. INPUT BOX C632A2181102 - 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. MGB REAR BARB216100-015

(7050A3633015)407 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. MGB REAR BARB216100-015

(7050A3633015)415 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

Página 9 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F



04-10-00. MGB FORWARD BARB216100-016

(7050A3633016)398 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. MGB FORWARD BARB216100-016

(7050A3633016)399 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. TAIL ROTOR HUB C642A0100103 CUR00133 9500 - - 0,0 17-jan-01 0 9500,0 - - 4911,7 - -

04-10-00. EQUIPPED BLADE C642A0300103 M3145 8500 - - 0,0 17-jul-08 0 8500,0 - - 3911,7 - -








04-10-00. STOPPED PIN OF TORSION STAR 7050A3642044 1313 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -








04-10-00. SPLINED FLANGE C651A1101201 PPT329 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

04-10-00. REAR SHAFT ASSY C651A3102052 PPT-124 20000 - - 0,0 17-jan-01 0 20000,0 - - 15411,7 - -

Página 10 de 19

NG 3.387,44

NTL 3.124,92




CÉLULA EC120B 1185 13.3414588,3

34708 2715,9MOTOR



DESCRIÇÃO P/N S/N



ARRIUS 2F



04-10-00. FORWARD SHAFT ASSY C651A3101102 REMOVIDO O PPT-219 E

INSTALADO NO WAB20000 - - 0,0 17-jan-01 0 20000,0 - - 0,0 - -

04-10-00. HOUSING ASSY C652A1108101 ML277 20000 - - 0,0 7-nov-07 0 20000,0 - - 15411,7 - -

04-10-00. INPUT FLANGE C652A1005301 PPT193 20000 - - 0,0 7-nov-07 0 20000,0 - - 15411,7 - -

04-10-00. BEVEL WHEEL C652A1102602 M531 20000 - - 0,0 7-nov-07 0 20000,0 - - 15411,7 - -

04-10-00. BEVEL GEAR C652A1103603 M72 20000 - - 0,0 7-nov-07 0 20000,0 - - 15411,7 - -

04-10-00. SERVOCONTROL SC5091-1 REMOVIDO 20000 - - 4118,5 20/mar/14 - 17532,0 - - 12943,7 - -

04-10-00. SERVOCONTROL SC5091-1 REMOVIDO 20000 - - 4537,5 26/abr/17 - 16196,2 - - 11607,9 - -

04-10-00. SERVOCONTROL SC5091-1 REMOVIDO 20000 - - 4537,5 26/abr/17 - 16196,2 - - 11607,9 - -

MSM 04-20 AIRWORTHINESS INSPECTIONS (CHK) - - - - - - - - - - - - - -


04-20-00. ARM ASSY C631A1101101 DA86 25 - - 0,0 17-jan-01 0 N/A N/A N/A N/A N/A N/A

04-20-00. TORSION STAR C642A0402101 REMOVIDO 1000 - - 4249,4 29/jan/15 12299 5249,4 - - 661,1 - -

Página 11 de 19

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HORAS DIAS CICLOS HORAS DATA CICLOS HORAS DATA CICLOS HORAS DIAS CICLOS

MM 05-10 - AIRWORTHINESS LIMITATIONS - - - - - - - - - - - - - -

05-10-10. CHECK BFF // BEF // ALF - - 10 - - 2709,4 04/jun/18 - 2719,4 - - 3,5 - -

05-10-10. INSPECTION AFTER 15 HOURS OR 7 DAYS - - 15 7 - 2709,4 04/jun/18 - 2724,4 11-jun-18 - 8,5 -371 -

05-10-10. INSPECTION 100 HOURS / 12 MONTHS - - 100 365 - 2704,7 24/mai/18 - 2804,7 24-mai-19 - 88,8 -24 -

05-10-10. INSPECTION 150 HOURS / 12 MONTHS - - 150 365 - 2617,0 05/mar/18 - 2767,0 5-mar-19 - 51,1 -104 -

05-10-10. INSPECTION AT 400 FLIGHT HOURS - - 400 - - 2776,0 10/mai/18 3447,00 3176,0 - - 460,1 - -

05-10-10.INSPECTION 500 HOURS / 24 MONTHS

INSPECTION- - 500 730 - 2504,0 23/dez/16 - 3004,0 23-dez-18 - 288,1 -176 -

05-10-10. INSPECTION 600 HOURS / 24 MONTHS - - 600 730 - 2504,0 23/dez/16 - 3104,0 23-dez-18 - 388,1 -176 -

MM 05-20 - SCHEDULED INSPECTIONS - - - - - - - - - - - - - -

05-20-10. CHECK BFF // BEF // ALF - - 10 - - 2709,4 04/jun/18 - 2719,4 - - 3,5 - -

05-20-10. INSPECTION AFTER 15 HOURS OR 7 DAYS - - 15 7 - 2709,4 04/jun/18 - 2724,4 11-jun-18 - 8,5 -371 -

05-20-10. INSPECTION AT 100 HOURS / 12 MONTHS - - 100 365 - 2704,7 25/mai/18 - 2804,7 25-mai-19 - 88,8 -23 -

05-20-10. INSPECTION 150 HOURS - - 150 - - 2617,0 05/mar/18 - 2767,0 - - 51,1 - -

05-20-10. EFETUAR ANÁLISE ESPECTOMÉTRICA DO OLEO - - 150 - - 2617,0 05/mar/18 - 2767,0 - - 51,1 - -

05-20-10. INSPECTION 150 HOURS / 12 MONTHS - - 150 365 - 2617,0 05/mar/18 - 2767,0 5-mar-19 - 51,1 -104 -

05-20-10.INSPECTIONS AT 300 FLIGHT HOURS

(OIL CHANGE)- - 300 - - 2504,0 23/dez/16 - 2804,0 - - 88,1 - -

05-20-10. INSPECTION AT 400 FLIGHT HOURS - - 400 - - 2776,0 10/mai/18 3447,00 3176,0 - - 460,1 - -

05-20-10.INSPECTION 500 HOURS / 24 MONTHS

INSPECTION- - 500 730 - 2504,0 23/dez/16 - 3004,0 23-dez-18 - 288,1 -176 -

CAPÍTULO DESCRIÇÃO P/N

POUSOS / CICLOS

S/NINTERVALO

S/N

1185

ARRIUS 2F MAINTENACE MANUAL X 319 L6 301 2 UPDATE N° 40: 30-OUT-2018

ÚLTIMO CUMPRIMENTO PRÓXIMO CUMPRIMENTO DISPONÍVEL

PP-WAC - MAPA DE CONTROLE DE INSPEÇÕES / COMPONENTES (MOTOR)

13.341


CÉLULA EC120B 4588,3

MODELO HORAS

Página 12 de 19

NG 3.387,44

NTL 3.124,92



HORAS DIAS CICLOS HORAS DATA CICLOS HORAS DATA CICLOS HORAS DIAS CICLOSCAPÍTULO DESCRIÇÃO P/N

POUSOS / CICLOS

S/NINTERVALO

S/N

1185




13.341



MODELO HORAS

05-20-10. INSPECTION 600 HOURS - - 600 - - 2504,0 23/dez/16 - 3104,0 - - 388,1 - -

05-20-10. INSPECTION 600 HOURS / 24 MONTHS - - 600 730 - 2504,0 23/dez/16 - 3104,0 23-dez-18 - 388,1 -176 -

05-20-10. INSPECTION 600 HOURS / 24 MONTHS (Oil change) - - 600 730 - - - - N/A N/A N/A N/A N/A N/A

05-20-10.INSPECTION 15 YEARS (MODULE 02

GAS GENERATOR)70EM028040 5676 3000 5475 - 0,0 07/out/09 0,00 3000,0 3-out-24 - 284,1 1935 -

MM 05-15 - FREQUENCIES - - - - - - - - - - - - - -

05-15-00-201-801-A01.MODULE M01

REDUCTION GEAR70EM018000 3176 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-802-A01. DRIVING GEAR REAR/FRONT BEARING 9609000451 3236 7000 - - 0,0 07/out/09 0,00 7000,0 - - 4284,1 - -

05-15-00-201-802-A01. DRIVING GEAR REAR/FRONT BEARING 9609000451 3240 7000 - - 0,0 07/out/09 0,00 7000,0 - - 4284,1 - -

05-15-00-201-802-A01. INTERMEDIATE GEAR FRONT BEARING 9609000435 5087 7000 - - 0,0 07/out/09 0,00 7000,0 - - 4284,1 - -

05-15-00-201-801-A01. INTERMEDIATE GEAR REAR BEARING 9609000455 942 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-801-A01. OUTPUT GEAR FRONT BEARING 9609000457 928 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-802-A01. OUTPUT GEAR REAR BEARING 9609000435 5086 7000 - - 0,0 07/out/09 0,00 7000,0 - - 4284,1 - -

05-15-00-201-801-A01. OUTPUT GEAR FRONT BEARING 9609000456 4 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-801-A01. TORQUEMETER BEARING PISTON 9609000604 912 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-802-A01. BREATHER GEAR FRONT BEARING 9609000555 1586 7000 - - 0,0 07/out/09 0,00 7000,0 - - 4284,1 - -

05-15-00-201-801-A01.MODULE 02

GAS GENERATOR70EM028040 5676 3000 5475 - 0,0 07/out/09 0,00 3000,0 3-out-24 - 284,1 1935 -

05-10-01-200-801-A01. CENTRIFUGAL IMPELLER 0319250580 2171FB - - 14000 0,0 07/out/09 0,00 - - 14000 - - 10613

05-10-01-200-801-A01. HP TURBINE DISC 2319250280 9234UP - - 8000 - 07/out/09 0,00 - - 8000 - - 4613

Página 13 de 19

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NTL 3.124,92



HORAS DIAS CICLOS HORAS DATA CICLOS HORAS DATA CICLOS HORAS DIAS CICLOSCAPÍTULO DESCRIÇÃO P/N

POUSOS / CICLOS

S/NINTERVALO

S/N

1185




13.341



MODELO HORAS

05-10-01-200-801-A01. FREE TURBINE DISC 2319411650 804TY - - 14000 0,0 07/out/09 0,00 - - 14000 - - 10613

05-15-00-201-801-A01. GENERATOR FRONT BEARING 9609000622 918 3000 - - 0,0 07/out/09 0,00 3000,0 - - 284,1 - -

05-15-00-201-801-A01. GENERATOR REAR BEARING 9609000648 1760 3500 - - 0,0 07/out/09 0,00 3500,0 - - 784,1 - -

05-15-00-201-801-A01. POWER TURBINE BEARING 9609000454 1579 3500 - - 0,0 07/out/09 0,00 3489,0 - - 773,1 - -

05-15-00-201-802-A01. HP TURBINE BLADE 231925A0J0 AN9 6000 - 10000 0,0 07/out/09 0,00 5989,0 - 9993 3273,1 - 6606

05-15-00. RIGHT INJECTOR HALF-MANIFOLD ASSY 0319730410 13585ERM 400 - - 2776,0 10/mai/18 3447,00 3176,0 - - 460,1 - -

05-15-00. LEFT INJECTOR HALF-MANIFOLD ASSY 0319730420 1724/RA 400 - - 2776,0 10/mai/18 3447,00 3176,0 - - 460,1 - -

05-15-00. PREFERRED INJECTOR PIPE ASSY 0319730440 1620 400 - - 2776,0 10/mai/18 3447,00 3176,0 - - 460,1 - -

05-15-00-201-801-A01. ADJUSTED FUEL CONTROL UNIT (FCU) 0319870100 490M 3000 3650 - 1401,8 03/mai/13 - 4401,8 1-mai-23 - 1685,9 1414 -

05-15-00. RIGHT HALF MANIFOLD 0319730410 ANR13099ERM 400 - - 5659,8 11/nov/16 - 6059,8 - - 3343,9 - -

INSPEÇÕES AVANTTO - - - - - - - - - - - - - -

M.M ARRIUS 2F CAP. 71-01 LAVAGEM DO COMPRESSOR - - - 7 - - 08/ago/17 - 15-ago-17 -671

Página 14 de 19

NG 3.387,44

NTL 3.124,92

ATUALIZAÇÃO DE PUBLICAÇÃO TÉCNICA: EASA AD 2015-0020




EASA AD 2018-0186 - Main Rotor ASB EC120-62A020 05-set-18 AT 50,0 - - - - - 4588,3 - - 0,0 - -

EASA AD 2018-0183 - Tail Rotor – Blade – Life Limit / Re-identification ASB EC120-04A008 11-set-18 AR 1.000,0 - - - - - - 13-mar-19 - - -96,0 -

AD FAA 2017-26-04 - Lighting and Ancillary Control Unit

N/A POR NÃO PUSSUIR

FLUTUADORES INSTALADOS NA

ARCFT

24-jan-18 AT - - - - - - N/A N/A N/A N/A N/A N/A

FAA AD 2015-26-04 - Object sliding between the canopy and the cabin floor ASB 67A005 04-fev-16 - - - - 4509,2 13/dez/16 - N/A N/A N/A N/A N/A N/A

EASA AD 2015-0020 - Doors – Sliding Door Star Support – Modification ASB 52A014 25-fev-15 AR 165,0 730 - 5576,1 11/mar/16 - 5741,1 11-mar-18 - 1152,8 -463 -

EASA AD 2014-0167 - Fuselage - Tail boom - Inspection ASB 53A015 29-abr-13 AT 1 TIME - - 4172,4 22/ago/14 12202 N/A N/A N/A N/A N/A N/A

EASA AD 2013-0093 - Sliding door star support - Modification ASB 52A014 29-abr-13 - 3842,0 13/jun/13 10389 N/A N/A N/A N/A N/A N/A

EASA AD 2011-0185 -Emergency FlotationASB 05A008

ASB 25A04207-out-11 AT 4299,7 02/set/15 12509 N/A N/A N/A N/A N/A N/A

EASA AD 2010-0078E - Emergency switch (EMER SW) Wiring - Modification ASB24A012 26-abr-10 AT 1 TIME - - 3322,0 14/jul/11 - N/A N/A N/A N/A N/A N/A

EASA AD 2010-0026-E - Main Rotor Head - Rotor Hub Inspection ASB 05A012 21-fev-10 AR 15,0 - - 4580,9 13/jul/17 - 4595,9 - - 7,6 - -

EASA AD 2009-0277 R1 - Fire Protection - Portable Halon 1211 Fire

Extinguishers Model 863520-26-001SB 863520-26-001 05-fev-10 AT 1 TIME - - 3730,3 09/nov/12 - N/A N/A N/A N/A N/A N/A

EASA AD 2009-0190 - Equipment/Furnishings - Emergency Floatation Gear –

InspectionASB 05A011 09-set-09 - 2449,3 22/out/09 - N/A N/A N/A N/A N/A N/A

EASA AD 2009-0122 R1 - Load release units ASB 05A004 10-nov-10 AT 1 TIME - - 3730,3 09/nov/12 - N/A N/A N/A N/A N/A N/A

EASA AD 2008-0185 - Twist Grip Drive Tube - Replacement InspectionASB 76A005 R1

ASB 76A006 R.222-out-08 AT 4311,1 02/out/15 12532 N/A N/A N/A N/A N/A N/A

DISPONÍVEL

TWIST GRIP INSTALADO NÃO SE

ENCONTRAM AFETADOS PELA DIRETRIZ

4588,3 13.341

SUPERADA PELA AD 2015-020


EC120B 1185

AERONAVE NÃO POSSUI FLUTUADORES

DE EMERGÊNCIA INSTALADOS

MODELO S/N

DESCRIÇÃO BOLETIM DE SERVIÇO EFETIVIDADE CATEGORIAINTERVALO

PP-WAC - MAPA DE CONTROLE DE AD / DA / SB (CÉLULA)


ÚLTIMO CUMPRIMENTO PRÓXIMO CUMPRIMENTO

CÉLULA

HORAS POUSOS / CICLOS

Página 15 de 19

NG 3.387,44

NTL 3.124,92





DISPONÍVEL

4588,3 13.341EC120B 1185

MODELO S/N





CÉLULA


EASA AD 2008-0177-E - Emergency Floatation Gear Lighting and Ancillary

Control Unit (LACU) Pushbutton - in- Flight check/ReplacementASB 04A007 19-set-08 AT 1 TIME - - 2031,4 12/nov/08 - N/A N/A N/A N/A N/A N/A

EASA AD 2007-0311 - Energy absorbing seat and Metallisation braid

ModificationASB 25A023 04-jan-08 AT 1 TIME - - 2031,4 12/nov/08 - N/A N/A N/A N/A N/A N/A

EASA AD 2007-0211 - Tail Rotor Drive - Rear Drive Shaft Friction Ring ASB 05A006 21-ago-07 AR 110,0 - - 4525,8 24/mar/17 - 4635,8 - - 47,5 - -

EASA AD 2006-0253 - Engine controls - Twist Grip Assembly ASB 76A006 REV1 01-set-06 - 957,5 13/dez/06 2141 N/A N/A N/A N/A N/A N/A

EASA AD 2006-0093 - Engine controls - Twist Grip Assembly - 05-mai-06 - - - - N/A N/A N/A N/A N/A N/A

AD 2006-0036-E - Grounding of spherical thrust bearings

GSAC CN F-2006-040 - Grounding of spherical thrust bearings

FAA AD 2008-10-01 - Spherical Thrust Bearing

TA 05A006 27-jan-06 AT 1 TIME - - 550,3 26/fev/06 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2005-175 - Thrust washers for cyclic stick frition ASB 67A011R1 05-nov-05 AT 1 TIME - - 228,5 08/jul/04 - N/A N/A N/A N/A N/A N/A

EASA AD 2005-4735 - Rotor flight controls - Collective torque tube assembly

GSAC CN F-2005-086 - Rotor flight controls - Collective torque tube

assembly

ASB 67A014 18-jun-05 AT 1 TIME - - 1640,0 11/mar/08 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2005-076 - Rotor flight controls pilot's cyclic stuck friction

washersTA 05A006 05-nov-05 - 2236,6 30/mar/09 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2004-059 - Rotor flight controls pilot's cyclic stuck friction

washersASB 67A011 05-nov-05 - 1640,0 11/mar/08 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2004-026R1 - Rotor flight control-collective torque tube ASB 67A014 08-jun-05 - 1640,0 11/mar/08 - N/A N/A N/A N/A N/A N/A

EASA AD 2004-5339 - T/R drive shaft damper

GSAC CN F-2003-465 R2 - Tail rotor drive - Tail rotor drive shaft damper

FAA AD 2005-09-05 - Tail Rotor Drive Shaft

AT 65A004 R1

TLX 42506F30-jul-05 AT 1 TIME - - 228,5 08/jul/04 - N/A N/A N/A N/A N/A N/A

EASA AD 2004-4810 - Engine mount and engine-to-main gear box (MGB)

coupling tube assembly

GSAC CN F-2003-325 R1 - Rotor drive - Engine mount and engine-to-main

gear box (MGB) coupling tube assembly

FAA AD 2001-04-12 - Engine to main gearbox (MGB) coupling tube assembly

(tube), part number C631A1101101

ASB 05A003

ASB 05A005

SB 71A003

SB 71005

22-mai-04 AT 3730,3 09/nov/12 - N/A N/A N/A N/A N/A N/A


N/A PORQUE AERONAVE JÁ POSSUI

SUPORTE DE MOTOR DE MODELO NOVO


Superseded AD 2007-0211

Superseded F-2005-175

Superseded F-2005-086

Página 16 de 19

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DISPONÍVEL

4588,3 13.341EC120B 1185

MODELO S/N





CÉLULA


GSAC CN F-2003-322R1 - Rotor Flight Controls ASB 67A010R2 05-jun-04 AT 1 TIME - - 863,9 29/ago/06 1856 N/A N/A N/A N/A N/A N/A

EASA AD 2005-1917 - Rotor Flight Controls - Cyclic Pitch Control Sticks

GSAC CN F-2002-606R1 - Cyclic Pitch Control SticksAT 67A009 12-mar-05 AT 1 TIME - - 228,5 08/jul/04 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2002-371-010 R1 - Rotor Flight Controls - Cyclic Pitch Control

Sticks

FAA AD 2003-22-10 - Cyclic Pitch Control Sticks

AT 67A008 08-mai-04 AT 1 TIME - - 211,4 14/abr/04 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2002-282 R1 - Navigation - Horizontal Situation Indicator KI

525A

FAA AD 2002-13-11 - installing front and side covers to protect the yaw

control

AT 34A006 27-mar-04 AT 1 TIME - - 228,5 08/jul/04 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2001-386R1 - Yaw control - Protections - 06-fev-02 AT 1 TIME - - 102,7 13/set/05 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2001-373-008 - Rotor flight controls - 01-set-01 AT 1 TIME - - 342,6 11/out/05 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2000-285-005R2 - Cabin sliding door - 26-mai-01 AT 1 TIME - - 342,6 11/out/05 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2000-058-003R1 - Engine-to-Main Gearbox (MGB) Coupling

Tube- 15-set-01 AT 1 TIME - - 1640,0 11/mar/08 - N/A N/A N/A N/A N/A N/A

GSAC CN F-2000-451-006 - Fuel anti-icing additive - 15-nov-00 AT 1 TIME - - 438,7 05/dez/05 - N/A N/A N/A N/A N/A N/A

GSAC CN F-1999-151-001R1 - Tail gearbox - 15-set-01 AT 1 TIME - - 0,0 17/jan/01 - N/A N/A N/A N/A N/A N/A

Página 17 de 19

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FAA AD 2018-12-03 - Fuel Controlling System No. 319 73 4839 09-ago-18 AR 400,0 - - 2703,9 10/mai/18 - 3103,9 - - 388,0 - -

EASA AD 2018-0012-E - Engine Oil System - Electrical Magnetic Plug Head -

Inspection / Replacement

AD não aplicável por não afetar o

p/n e s/n instalado na aeronave.

Vide FAOT.

18-jan-18 AT 10,0 - - 2638,3 02/abr/18 - N/A N/A N/A N/A N/A N/A

EASA AD 2017-0070 - Engine Fuel & Control - Privilege Injector -

Replacement

(Substituição das Injetoras de Combustível) - - 400 hours

- 09-mai-17 AR 400,0 - - 2703,9 10/mai/18 - 3103,9 - - 388,0 - -


Replacement

(Substituição das Injetoras de Combustível) - - 400 hours

- 28-jul-16 AR 400,0 - - - - - N/A N/A N/A N/A N/A N/A

EASA AD 2016-0041 - ENGINE FCU modification - 17-mar-16 - - 273 - 2617,0 05/mar/18 - N/A N/A N/A N/A N/A N/A

EASA AD 2015-0057 - Oil – Nozzle Bonding on Ejector Assembly –

Inspection- 15-abr-15 - 1 TIME - - 2222,4 02/jul/15 - N/A N/A N/A N/A N/A N/A

EASA AD 2015-0049 - Oil – Oil Pump Drive Link / Lubricating Device –

Inspection- 31-mar-15 - 400,0 - - 2618,3 13/mar/18 - 3018,3 - - 302,4 - -

EASA AD 2013-0243 - Oil - Nozzle Bonding on Ejector Assembly - Inspection - 15-out-13 - 1601,7 08/out/13 - N/A N/A N/A N/A N/A N/A


Replacement

(Substituição das Injetoras de Combustível)

MSB319 73 4001K 22-ago-12 AR 2327,2 25/nov/15 - N/A N/A N/A N/A N/A N/A

EASA AD 2011-0182 (R1) Engine Fuel & Control - P3 Air Pipe -

Inspection/Modification

(FAA AD 2005-09-51 / FAA AD 2009-14-11)

ASB 319-75-4810B 06-fev-12 AR 100,0 - - 2617,0 05/mar/18 - 2717,0 - - 1,1 - -

EASA AD 2008-0170 - Engine Fuel & Control - Lubrification Unit -

ModificationASB 319-79-4075 09-out-08 AT N/A N/A N/A N/A N/A N/A

EASA AD 2008-0134R1 - Engine Fuel & Control - P3 Air Pipe -

Inspection/ModificationASB 319754810 31-jul-08 - N/A N/A N/A N/A N/A N/A

EASA AD 2007-0057 (FAA AD 2008-13-27) - Gas Generator Front Bearing

ModificationSB 319-72-4012 14-mar-07 AT N/A N/A N/A N/A N/A N/A

EASA AD 2006-0237 (FAA AD 2007-11-06) - Fuel Control Unit (PRE TF55)MSB A319-73-4825

MSB A319-73-4055 23-ago-06 AT N/A N/A N/A N/A N/A N/A

TF12A APLICADA CUMPRIDO EM FÁBRICA

TF55 APLICADA CUMPRIDO EM FÁBRICA

SUPERSEDED BY EASA AD 2015-0057

SUPSERSEDED BY EASA AD 2011-0182

DISPONÍVEL

SUPERSEDED BY EASA AD 2016-0138


CUMPRIDO EM FÁBRICA

DESCRIÇÃO BOLETIM DE SERVIÇO EFETIVIDADE CATEGORIAINTERVALO ÚLTIMO CUMPRIMENTO PRÓXIMO CUMPRIMENTO

PP-WAC - MAPA DE CONTROLE DE AD / DA / SB (MOTOR)


CÉLULA EC120B 1185 4588,3 13.341


Página 18 de 19

NG 3.387,44

NTL 3.124,92





DISPONÍVELDESCRIÇÃO BOLETIM DE SERVIÇO EFETIVIDADE CATEGORIA


PP-WAC - MAPA DE CONTROLE DE AD / DA / SB (MOTOR)


CÉLULA EC120B 1185 4588,3 13.341


EASA AD 2006-0141 - Repalcement of check-valve piston o'ring ASB 319-79-4802 09-jun-06 AT N/A N/A N/A N/A N/A N/A

GSAC CN F-2005-143R1 - Fuel control unit ASBA319-73-1825 31-ago-05 - - - - N/A N/A N/A N/A N/A N/A

GSAC CN F-2005-122 - Replacement of check- alve piston o'ring ASBA319-79-4802 30-jul-05 - - - - N/A N/A N/A N/A N/A N/A

GSAC CN F-2005-088 (FAA AD 2005-17-15) - System and controls check of

correct position - FCUASBA319-73-4823 08-jun-05 AR 500,0 - - 2222,4 02/jul/15 - 2722,4 - - 6,5 - -

GSAC CN F-2005-073R1 - Engine - Immediate grounding -injection wheel Alerta Fax 057/05/DSO/TM 29-abr-05 AT 1 TIME - - N/A N/A N/A N/A N/A N/A

GSAC CN F-2003-219 - Stolen Engine - S/N 34084 - 16-jun-03 AT N/A N/A N/A N/A N/A N/A

GSAC CN F-2000-482 - Engine Fuel & Control - FCU Max. Fuel Flow Stop -

Rework- 09-dez-00 AT 1 TIME - - N/A N/A N/A N/A N/A N/A

GSAC CN F-1999-233 - SUPERSEDED BY EASA AD 2012-0150 - 12-jun-99 - - - - N/A N/A N/A N/A N/A N/A





NÃO APLICAVEL AO S/N INSTALADO CUMPRIDO EM FÁBRICA



Página 19 de 19

pp-wac - mapa de controle de inspeÇÕes (cÉlula)data do Último voo: 04/09/2017 data de emissÃo:...

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