1. DESCRIPTION

This sheet transmits Revision 03 to Service Bulletin 190-36-0023.

This is a complete reissue of the Bulletin.

This revision incorporates the information presented in the Information Notice related to the

previous issues of this Service Bulletin, as listed below:

None.

2. ADDITIONAL ACTION

Aircraft that have complied with the first issue of this bulletin do not need any additional

action.

3. RECORD OF REVISION

Basic issue: 22/Jul/2013.

Revision 01: 03/Sep/2013.

Revision 02: 30/Apr/2014.

Revision 03: 24/Sep/2014.

4. HIGHLIGHTS

The topics, affected pages, and a brief description of the content-related changes introduced

by this revision are presented below.

Revision bars are put in the left margin of each page to show the location of the significant

changes. Text displacement and text format changes are not indicated.

TOPIC/PAGE DESCRIPTION OF REVISION

1. PLANNING INFORMATION

1.A. SB EFFECTIVITY / 01 Added new note.

1.B. CONCURRENT REQUIREMENTS / 01 and 02 Updated information.

1.C. REASON / 02 and 03 Updated wording and added reason of revision 03.

1.E. COMPLIANCE / 04 and 05 Updated information related compliance.

TRANSMITTAL LETTER

SB No.: 190-36-0023

PAGE: 1 of 1

Copyright © 2014 by Embraer S.A. All rights reserved.

PNEUMATIC - REPLACEMENT OF THE LH/RH ENGINE LOW-STAGE BLEED CHECK

VALVE PN 1001447-6

In connection with the use of this document, Embraer does not provide any express or implied

warranties and expressly disclaims any warranty of merchantability or fitness for a particular purpose.

1. PLANNING INFORMATION

A. SB EFFECTIVITY

Aircraft affected:

MODEL SN

Embraer 190( ) and 195( ) All aircraft in operation equipped with the affected Part Number.

NOTE: If the aircraft is already equipped with Black Label 13 software or a later

version, and then a new low-stage bleed check valve (zero-hour) PN

1001447-6 is installed, the accomplishment of this SB is not necessary.

Affected component:

Engine Low-stage bleed check valve PN 1001447-6, all serial numbers, installed on the

aircraft.

NOTE: This effectivity list includes the aircraft originally equipped with the affected

component. Since this component is a Line Replaceable Unit (LRU), it may

be necessary to refer to the fleet maintenance control record and verify

whether the unit has been replaced with another one during routine

maintenance.

In-production effectivity:

The subject presented in this bulletin does not affect any in-production aircraft.

B. CONCURRENT REQUIREMENTS

Make sure that Black Label software version 13.0 (SB190-21-0041) or a later version is

already installed before the accomplishment of this bulletin.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 1 of 13

Copyright © 2014 by Embraer S.A. All rights reserved.
NOTE: If the aircraft is already equipped with Black Label 13 software or a later

version, and then a new low-stage bleed check valve PN 1001447-6 is

installed, the accomplishment of this SB is not necessary.

C. REASON

(1) HISTORY

Embraer has received reports regarding cracks in some engine low-stage bleed

check valves PN 1001447-6 recently returned for the periodic Maintenance Review

Board (MRB) inspection.

Flight and Laboratory Tests have shown that the bleed oscillations during take-off

and climb may affect low pressure check valve dynamic behavior and contribute to

low-stage bleed check valve petals cracking.

It was also observed that Black Label 13 software or a later version prevents this

kind of oscilations.

Further investigations showed that if a new engine low-stage bleed check valve

(zero-hour) PN 1001447-6 is installed in an aircraft already equipped with Black

Label 13 software (or a later version) these kind of cracks will not occur.

These cracks may lead to low-stage check valve failure and may cause engine

shutdown.

(2) OBJECTIVE

To provide instructions for the replacement of existing low-stage bleed check valves

PN 1001447-6 of the LH/RH engine, with a new one bearing the same PN.

(3) EXPECTED BENEFITS

The actions proposed in this service bulletin are to reduce the risk of in-flight

shutdown.

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 2

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
(4) REVISION HISTORY

REVISION 01: This revision has been issued to update the information of

compliance, to update and add parts to be procured and to update

the accomplishment instructions.

REVISION 02: This revision has been issued to update the information of

compliance section.

REVISION 03: This revision has been issued to update SB information.

D. DESCRIPTION

This Bulletin is divided into 2 PARTS, as follows:

PART I REPLACEMENT OF THE LH ENGINE LOW-STAGE BLEED CHECK

VALVE PN 1001447-6

Applicable to: 1.A. SB EFFECTIVITY

PART I of this bulletin gives instructions to replace the LH low-stage bleed check valve

with a new one, bearing the same part number. It is necessary that the check valve

removed from the aircraft be tagged with the aircraft serial number, flight hours and flight

cycles and sent to Hamilton Sundstrand (HS). Parts shipping and handling information is

listed in paragraph 2.B. INDUSTRY SUPPORT INFORMATION of this bulletin.

To gain access to the work area, it is necessary to open access doors 413AL and 415AL.

PART II REPLACEMENT OF THE RH ENGINE LOW-STAGE BLEED CHECK

VALVE PN 1001447-6

Applicable to: 1.A. SB EFFECTIVITY

PART II of this bulletin gives instructions to replace the RH low-stage bleed check valve

with a new one, bearing the same part number. It is necessary that the check valve

removed from the aircraft be tagged with the aircraft serial number, flight hours and flight

cycles and sent to Hamilton Sundstrand (HS). Parts shipping and handling information is

listed in paragraph 2.B. INDUSTRY SUPPORT INFORMATION of this bulletin.

To gain access to the work area, it is necessary to open access doors 423AL and 425AL.

NOTE: The modification presented in this bulletin does not affect Fatigue Critical

Structure (FCS).

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 3

Copyright © 2014 by Embraer S.A. All rights reserved.
E. COMPLIANCE

(1) APPLICABLE TO PART I

– For aircraft equipped with engine low-stage bleed check valve PN 1001447-6

with less than 6,000 Flight Hours, Embraer recommends the accomplishment of

this bulletin before this time limit or within the next 600 Flight Hours after the

release date of revision 2 of this SB, whichever occurs later.

– For aircraft equipped with engine low-stage bleed check valve PN 1001447-6

with more than 6,000 Flight Hours, Embraer recommends the accomplishment of

this bulletin within the next 600 Flight Hours after the release date of revision 2 of

this SB.

NOTE: 1) It is acceptable to have a low-stage bleed check valve PN 1001447-6

logged with more than 6,000 Flight Hours, up to 8,000 Flight Hours

installed in one of engines of an aircraft since the low-stage bleed check

valve PN 1001447-6 installed in the opposite engine is logged with less

than 6,000 Flight Hours.

2) It is acceptable the installation of serviceable valves P/N 1001447- 6

that are not new provided they have accumulated less than 6,000 FH

since new.

3) If the aircraft is already equipped with Black Label 13 software or a later

version, and then the low-stage bleed check valve PN 1001447-6 is

replaced with a new one (zero-hour), the accomplishment of this SB is

not necessary.

(2) APPLICABLE TO PART II

– For aircraft equipped with engine low-stage bleed check valve PN 1001447-6

with less than 6,000 Flight Hours, Embraer recommends the accomplishment of

this bulletin before this time limit or within the next 600 Flight Hours after the

release date of revision 2 of this SB, whichever occurs later.

– For aircraft equipped with engine low-stage bleed check valve PN 1001447-6

with more than 6,000 Flight Hours, Embraer recommends the accomplishment of

this bulletin within the next 600 Flight Hours after the release date of revision 2 of

this SB.

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 4

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
NOTE: 1) It is acceptable to have a low-stage bleed check valve PN 1001447-6

logged with more than 6,000 Flight Hours, up to 8,000 Flight Hours

installed in one of engines of an aircraft since the low-stage bleed check

valve PN 1001447-6 installed in the opposite engine is logged with less

than 6,000 Flight Hours.

2) It is acceptable the installation of serviceable valves P/N 1001447- 6

that are not new provided they have accumulated less than 6,000 FH

since new.

3) If the aircraft is already equipped with Black Label 13 software or a later

version, and then the low-stage bleed check valve PN 1001447-6 is

replaced with a new one (zero-hour), the accomplishment of this SB is

not necessary.

F. APPROVAL

The technical aspects of this Service Bulletin are approved by: Agência Nacional de

Aviação Civil (ANAC).

NOTE: If any aircraft listed in the SB effectivity has a modification or repair

incorporated that is not of EMBRAER origin, and which affects the content

of this Service Bulletin, the operator will take full responsibility for obtaining

approval by a regulatory agency for any adaptation necessary before the

incorporation of this Service Bulletin.

G. ESTIMATED MANPOWER

This is an estimate of the manpower necessary to accomplish this Service Bulletin on a

single aircraft.

It is intended for direct labor only, performed by experienced personnel, and does not

include the time to plan, prepare, or inspect the work. Sealant, paint, or adhesive curing

times are not included either.

It is assumed that all the tools, parts, and other means are readily available when

necessary.

An adjustment to these values may be necessary to meet particular circumstances.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 5

Copyright © 2014 by Embraer S.A. All rights reserved.
(1) APPLICABLE TO PART I

– Access opening: 0.15 man-hours.

– Inspection: None.

– Modification: 2.5 man-hours.

– Access closure: 0.15 man-hours.

– Test: 0.5 man-hours.

(2) APPLICABLE TO PART II

– Access opening: 0.15 man-hours.

– Inspection: None.

– Modification: 2.5 man-hours.

– Access closure: 0.15 man-hours.

– Test: 0.5 man-hours.

H. WEIGHT AND BALANCE

None.

I. SOFTWARE ACCOMPLISHMENT SUMMARY

None.

J. REFERENCES

AIPC 190/( ) Aircraft Illustrated Parts Catalog - 30-21-03 - ICE AND RAIN

PROTECTION.

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 6

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
AIPC 190/( ) Aircraft Illustrated Parts Catalog - 36-11-02 and 36-11-04 -

PNEUMATIC.

AMM 190/( ) Aircraft Maintenance Manual PART II - 20-00-00 - STANDARD

PRACTICES-AIRFRAME.

AMM 190/( ) Aircraft Maintenance Manual PART II - 36-11-00 and 36-11-02 -

PNEUMATIC.

SB190-21-0041 AIR CONDITIONING - AIR MANAGEMENT SYSTEM

CONTROLLER PROCESSOR BOARD - INCORPORATION OF

NEW OPS SOFTWARE (BLACK LABEL 13.0).

K. OTHER PUBLICATIONS AFFECTED

None.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 7

Copyright © 2014 by Embraer S.A. All rights reserved.
2. MATERIAL INFORMATION

A. MATERIAL - PRICE AND AVAILABILITY

(1) MATERIAL AVAILABLE FROM EMBRAER

None.

(2) MATERIAL AVAILABLE FROM OTHER VENDORS

Refer to section 2.C. MATERIAL NECESSARY FOR EACH AIRCRAFT.

B. INDUSTRY SUPPORT INFORMATION

None.

C. MATERIAL NECESSARY FOR EACH AIRCRAFT

When applicable, the use of alternative or similar parts in place of the ones specified in

the kits is allowable, provided that these alternative or similar parts are approved by

Embraer as indicated in the related Embraer Technical Publications or through a formal

Embraer communication channel.

The necessary expendable or consumable parts presented in the AMM Tasks referred to

in this bulletin should be procured from the operator’s inventories or ordered as spares.

The complementary information, when necessary, is presented as Notes in the respective

Table.

(1) TOP KITS AND KITS

None.

(2) MATERIAL TO BE PROCURED

(a) Parts

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 8

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
The Low-stage Bleed Check Valve PN 1001447-6 should be procured from the

manufacturer, as indicated in the associated Note, and will be available at no

charge to the operator.

Applicable to PART I

NEW PN DESCRIPTION OLD PN QTY DISP/

Notes

1001447-6 Low-stage Bleed

Check Valve

1001447-6 01 7/ [1]

1. Hamilton Sundstrand Worldwide Repair / Windsor Locks Repair Station / One Hamilton

Road, Dock W, Windsor Locks, CT 06096, USA. or Hamilton Sundstrand Worldwide Repair / Customer Support Center - Maastricht B.V. / Horsterweg 7 / 6199 AC Maastricht Airport / Netherlands

Applicable to PART II

NEW PN DESCRIPTION OLD PN QTY DISP/

Notes

1001447-6 Low-stage Bleed

Check Valve

1001447-6 01 7/ [1]

1. Hamilton Sundstrand Worldwide Repair / Windsor Locks Repair Station / One Hamilton

Road, Dock W, Windsor Locks, CT 06096, USA. or Hamilton Sundstrand Worldwide Repair / Customer Support Center - Maastricht B.V. / Horsterweg 7 / 6199 AC Maastricht Airport / Netherlands

The parts below, required for the accomplishment of this bulletin, should be

procured from the operator’s inventories or requested directly from the manufacturer, as indicated in the associated Note.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 9

Copyright © 2014 by Embraer S.A. All rights reserved.
Applicable to PART I

NEW PN DESCRIPTION OLD PN QTY DISP/

Notes

13100-125 or AS1895

-23-125

Seal

13100-125 or

AS1895-23-125

01 7/ [1]

13100-300 or AS1895

-23-300

Seal

13100-300 or

AS1895-23-300

02 7/ [1]

14900 Seal 14900 01 7/ [1]

1. Goodrich Aerostructures / 850 Laggon Drive Chula Vista, CA 91910-2098, USA.

Applicable to PART II

NEW PN DESCRIPTION OLD PN QTY DISP/

Notes

13100-125 or AS1895

-23-125

Seal

13100-125 or

AS1895-23-125

01 7/ [1]

13100-300 or AS1895

-23-300

Seal

13100-300 or

AS1895-23-300

02 7/ [1]

14900 Seal 14900 01 7/ [1]

1. Goodrich Aerostructures / 850 Laggon Drive Chula Vista, CA 91910-2098, USA.

DISPOSITION: 7 = Replace with part bearing same PN

(b) Consumable Materials

None.

D. MATERIAL NECESSARY FOR EACH SPARE

None.

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 10

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
E. REIDENTIFIED PARTS

None.

F. TOOLING - PRICE AND AVAILABILITY

Whenever required, the necessary tooling presented in the AMM Tasks referred to in this

bulletin, should be procured from the operator’s inventories or ordered as spares.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 11

Copyright © 2014 by Embraer S.A. All rights reserved.
3. ACCOMPLISHMENT INSTRUCTIONS

NOTE: 1) Obey all of the WARNINGS and CAUTIONS included in the referenced manuals

and procedures.

2) The Manuals and other documents are referred to by acronyms or using a

simplified form. Refer to section 1.J. REFERENCES for a more complete

definition.

3) This Service Bulletin is divided into 2 PARTS. The SB PARTS are featured to

allow their independent accomplishment, however Embraer does not recommend the accomplishment of PART I and PART II at the same time.

The steps below outline the general accomplishment instructions.

A. Make sure that the aircraft is safe for maintenance. Refer to AMM TASK 20-00-00-910

-801-A/200 - Aircraft Maintenance Safety Procedures - Standard Procedures.

B. PART I – REPLACEMENT OF THE LH ENGINE LOW-STAGE BLEED CHECK VALVE

PN 1001447-6

(1) Remove and retain LH low-stage engine bleed check valve PN 1001447-6 (01

position). Refer to AMM TASK 36-11-02-000-801-A/400 - Low-Stage Bleed Check

-Valves - Removal.

(2) Install new LH low-stage engine bleed check valve PN 1001447-6 (01 position). For

valve installation, refer to AMM TASK 36-11-02-400-801-A/400 - Low-Stage Bleed

Check-Valves - Installation. For seals PN 13100-300 or AS1895-23-300 (02 positions) and PN 14900 (01 position) and PN 13100-125 or AS1895-23-125 (01

position) reference position, refer to AIPC 36-11-02 - LOW STAGE BLEED CHECK

VALVE, AIPC 36-11-04 - ENGINE BLEED LINES and AIPC 30-21-03 - ENGINE

ANTI-ICE DUCT.

(3) Perform the operational test of the engine pneumatic bleed system. Refer to AMM

TASK 36-11-00-710-801-A/500 - Engine Pneumatic Bleed-System - Operational

Test.

C. PART II – REPLACEMENT OF THE RH ENGINE LOW-STAGE BLEED CHECK VALVE

PN 1001447-6

SERVICE BULLETIN

SB No.: 190-36-0023

PAGE: 12

DATE: 22/Jul/2013

REVISION No.: 03 - 24/Sep/2014

Copyright © 2014 by Embraer S.A. All rights reserved.
(1) Remove and retain RH low-stage engine bleed check valve PN 1001447-6 ( 01

position). Refer to AMM TASK 36-11-02-000-801-A/400 - Low-Stage Bleed Check

-Valves - Removal.

(2) Install new RH low-stage engine bleed check valve PN 1001447-6 (01 position). For

seals PN 13100-300 or AS1895-23-300 (02 positions) and PN 14900 (01 position)

and PN 13100-125 or AS1895-23-125 (01 position) reference position, refer to AIPC

36-11-02 - LOW STAGE BLEED CHECK VALVE, AIPC 36-11-04 - ENGINE BLEED

LINES and AIPC 30-21-03 - ENGINE ANTI-ICE DUCT.

(3) Perform the operational test of the engine pneumatic bleed system. Refer to AMM

TASK 36-11-00-710-801-A/500 - Engine Pneumatic Bleed-System - Operational

Test.

D. Put the aircraft back to its initial condition.

E. Write the accomplishment of PART I and/or PART II of this bulletin in the applicable

documents.

NOTE: 1) Please inform us by e-mail fleet.reliability@embraer.com.br of the aircraft

manufacturer serial number and the SB incorporation date, specifying the SB

Part(s) incorporated or whether the whole SB has been incorporated. This

will enable Embraer to consider your aircraft configuration when providing

future modifications.

2) To formally inform that the SB has been incorporated fleet-wide or that the

SB will not be incorporated, so that Embraer can update the affected

technical publications, use the “Service Bulletin Full-Fleet Incorporation

Report” form, which is available on the Flyembraer portal

(http://www.flyembraer.com).

3) Use the attached “Service Bulletin Evaluation” form to send us your

comments regarding this SB. Your feedback will be much appreciated as an

aid for us to improve the quality of the SBs.

SERVICE BULLETIN

DATE: 22/Jul/2013

REVISION No.:03 - 24/Sep/2014

SB No.: 190-36-0023

PAGE: 13

Copyright © 2014 by Embraer S.A. All rights reserved.

SERVICE BULLETIN EVALUATION

THE PURPOSE OF THIS FORM IS TO COLLECT DATA THAT WILL BE USED TO IMPROVE THE QUALITY OF OUR

SERVICE BULLETINS. PLEASE FILL IN FORM AND RETURN IT TO:

EMBRAER - S.A.

EFTC - SERVICE BULLETIN ENGINEERING

AV. BRIGADEIRO FARIA LIMA, 2170

SÃO JOSÉ DOS CAMPOS - SP - 12227-901

BRASIL

Fax: + 55 12 3927-6600 (ext. 1624)

e-mail: fleet.reliability@embraer.com.br

S.B. Title: S.B.: (Number / Rev.)

Operator:

SB Implementation Report

Aircraft Serial Number or Registration Number: Incorporation Date:

Aircraft Flight Hours: Aircraft Landings:

POST-ACCOMPLISHMENT EVALUATION: (Check applicable squares below)

ESTIMATED MANPOWER: [ ] OK [ ] NOT OK (Explain Below)

MATERIAL & KITS: [ ] OK [ ] NOT OK (Explain Below)

ACCOMPLISHMENT INSTRUCTIONS: [ ] OK [ ] NOT OK (Explain Below)

FIGURES: [ ] OK [ ] NOT OK (Explain Below)

SB GENERAL EVALUATION: [ ] OK [ ] NOT OK (Explain Below)

COMMENTS: (Bulletin quality/ Difficulties found at the time of incorporation/ Suggested improvements/ Other)

Organization: Fax: Phone:

E-mail:

Address: Prepared by:(Name/Title) Date:

Copyright © 2014 by Embraer S.A. All rights reserved.