ALERT SERVICE LETTER ASL

Similar documents
BULLETIN INDEX LOCATOR

September 8, Cessna Distributors, Authorized Service Facilities, CPC's, CSTARS, ASR's, and affected Owners of Record

BULLETIN INDEX LOCATOR

BULLETIN INDEX LOCATOR

BULLETIN INDEX LOCATOR

BULLETIN INDEX LOCATOR

SERVICE LETTER. REASON To incorporate new software changes to the engine electronic control and engine diagnostics unit.

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On. REASON

SERVICE BULLETIN. 560XL (Citation XLS+) thru -6055, thru -6066, thru -6071, thru -6077

ALERT SERVICE LETTER

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE BULLETIN. Citation CIB TITLE FUEL - FIREWALL SHUTOFF VALVE GROUND IMPROVEMENT

SERVICE BULLETIN REVISION TRANSMITTAL

SERVICE BULLETIN. EFFECTIVITY SERIAL NUMBERS 680 (Citation Sovereign) thru (Citation Sovereign+) thru -0549

Revision Transmittal Sheet

SERVICE BULLETIN. This service bulletin provides parts and instructions to install fuel caps that have a locking feature.

SERVICE LETTER TITLE SERVICING - TRANSMITTAL OF PRATT & WHITNEY CANADA SERVICE INFORMATION LETTER S.I.L. NO. PT6A-196

SERVICE BULLETIN REVISION

SERVICE LETTER REVISION TRANSMITTAL

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

SERVICE BULLETIN. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE BULLETIN SERIAL NUMBERS. The equivalent of this service bulletin has been incorporated on production airplanes and On.

SERVICE LETTER. COMPLIANCE DISCRETIONARY. This service letter should be accomplished at a scheduled Check 1, Check 2, or HSI. LABOR HOURS KEY WORD

SERVICE LETTER SERIAL NUMBERS. 550/ thru -0505, thru -0733, thru -0969

Service Information Letter

Affected , RX, , and RX alternators in Service Station stock should be returned to Cessna.

SERVICE BULLETIN TITLE ENGINE CONTROLS - FULL AUTHORITY DIGITAL ENGINE CONTROL (FADEC) SOFTWARE UPGRADE VERSION C10

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

SERVICE BULLETIN CERTIFICATION REQUIREMENTS - FOREIGN CERTIFICATION PLACARD INSTALLATION

SERVICE BULLETIN REVISION

SERVICE BULLETIN SB

Alert Service Bulletin

SERVICE BULLETIN SB

SERVICE BULLETIN. To prevent the wing fuel boost pump wiring from chafing on the wing structure and/or fuel tube assemblies.

SERVICE LETTER. Single Engine SEL TITLE LANDING GEAR - DRAG LINK REPLACEMENT

Service Bulletin No: Ref No: 49 Modification No: EC ATA Chapter: 32

Service Bulletin No: Ref No: 165 Modification No: EC ATA Chapter: 21

201F Fuel Pump Valve Housing Cap Screw Replacement

SUBJECT: Single Engine Service Bulletin SB Revision 1: Cosmetic Window Repair

SERVICE BULLETIN. COMPLIANCE MANDATORY. This service bulletin must be accomplished at the next 100-hour or 12-month (annual-type) inspection.

SERVICE LETTER REVISION TRANSMITTAL

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS

SERVICE LETTER TITLE EXHAUST - TRANSMITTAL OF LYCOMING SERVICE BULLETIN NO 627C, EXHAUST SYSTEM INSPECTION SERIAL NUMBERS

Service Bulletin No: Ref No: 331 Modification No: EC , EC ATA Chapter: 27

PRATT AND WHITNEY CANADA CORP.

SERVICE INFORMATION LETTER

POWER TURBINE RPM (N2) STEADY STATE OPERATION AVOIDANCE, INTRODUCTION OF.

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 106 MODIFICATION NO: ATA CHAPTER: 28

SERVICE BULLETIN FUEL - MODIFICATION OF THE ENGINE DRIVEN FUEL PUMP SYSTEM

Part A Describes the procedure for the replacement of the Mitchell type tachometer. These parts are supplied in Kit A as described below.

This Service Bulletin is applicable only to airplanes equipped with placards that are written in English.

Service Bulletin No: Ref No: 170 Modification No: EC ATA Chapter: 53

Type Acceptance Report

Type Acceptance Report

ATTACHMENT. Orders for the required parts listed below must be placed by using this form only. Service Station/Company Code: Company Name:

SERVICE BULLETIN SB

Table 1: Alternator Models ES (CMI ), ALX-9524 (CMI ), ALX-9524R, & ALV-9610 Affected Serial Numbers

FAA approval has been obtained on technical data in this publication that affects airplane type design.

SUBJECT: ELECTRICAL POWER SYSTEM UNIT AND ROTORCRAFT FLIGHT MANUAL TEMPORARY REVISION, CANCELLATION OF

Type Acceptance Report

SERVICE BULLETIN. Beech ATA CODE PLACARDS AND MARKINGS - INSTALLATION OF FUEL SELECTOR PLACARD

[Docket No. FAA ; Directorate Identifier 2016-NE-09-AD] Airworthiness Directives; Pratt & Whitney Division Turbofan Engines

Service Bulletin No.: DAC Rev 0 Date Issued: 29 June 2017 Title: Removal of OAT/Clock AA Battery Page: 1 of 5

It has been determined that some airplanes may have a hose plug installed in the inflatable belt assembly hose end.

PC-6 PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 188 MODIFICATION NO: ATA CHAPTER: 53

SERVICE BULLETIN FLIGHT CONTROLS - RUDDERVATOR DIFFERENTIAL TAIL CONTROL ROD ASSEMBLY INSPECTION/MODIFICATION

Airworthiness Directive Schedule

PRATT AND WHITNEY CANADA CORP.

Single Engine. Service Bulletin TITLE ELEVATOR TRIM TAB ACTUATOR ASSEMBLY INSPECTION EFFECTIVITY. Group A airplanes: Serial Numbers

AIRWORTHINESS DIRECTIVE

SERVICE LETTER. Hartzell Alert Service Bulletin No. 069, 200F, 201F, 202F Fuel Pump Leak Inspection And Diaphragm

MANDATORY SERVICE BULLETIN

SERVICE BULLETIN OPTIONAL SB Beech. 1. Planning Information FUSELAGE - BATTERY DRAIN MAST REMOVAL. A. Effectivity

PILATUS AIRCRAFT LTD. CH-6371 STANS, SWITZERLAND SERVICE BULLETIN SERVICE BULLETIN NO: REF NO: 184 MODIFICATION NO: ATA CHAPTER: 32

FOR THE MOST RECENT REVISION LEVEL OF THIS SERVICE BULLETIN.

TYPE-CERTIFICATE DATA SHEET

SERVICE LETTER. Multi-engine TITLE NACELLES/PYLONS - NACELLE FITTING INSPECTION EFFECTIVITY

201F Fuel Pump Shaft Seal Leak

Service Bulletin No: Ref No: 105 Modification No: INSPECTION ATA Chapter: 32

SUBJECT: FUEL FITTING P/N AND , VERIFICATION OF.

European Aviation Safety Agency

NOTE: SB is a WAAS only supported build. If the autopilot is not WAAS equipped, the unlock card cannot be used at this time.

ALERT SERVICE BULLETIN CHECKING OF MAGNETIC PLUG ON ROTAX

European Aviation Safety Agency

PT6A & JT15D. turbine engines series FOR NEW ENGINES. Excluding hbc and cessna caravan installations

*MANDATORY SERVICE BULLETIN*

SERVICE BULLETIN REVISION

Type Acceptance Report

ALERT SERVICE BULLETIN PSL September 2015 Revision A, 6 October 2017

Service Bulletin No.: DAC Rev. 3 Date Issued: August 28, 2002 Title: Sensenich Propeller Installation Page: 1 of 8

ROLLS-ROYCE CORPORATION (FORMERLY ALLISON ENGINE COMPANY)

Single Engine Service Bulletin SEB08-4 Revision 1, Unision Industries SLICK 4200/4300/6200/6300 Magnetos Inspection.

MANDATORY SERVICE BULLETIN NO. MSB

ALERT SERVICE BULLETIN

European Aviation Safety Agency

Service Bulletin No: Ref No: 121 Modification No: INSPECTION ATA Chapter: 53

Symbols used: Please, pay attention to the following symbols throughout this document emphasizing particular information.

Please replace any copy of SEB07-2 with the attached copy of SEB07-2 Revision 1 which is printed in its entirety.

Nomad RUDDER CONTROL SYSTEM STRENGTHENING OF CABLE PULLEY MOUNTING AT STA (MOD N630)

Transcription:

Citation TITLE ALERT SERVICE LETTER ASL550-72-29 ENGINE - TRANSMITTAL OF P&WC SERVICE DOCUMENTS - INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE-INSPECTION/REPLACEMENT OF EFFECTIVITY MODEL SERIAL NUMBERS 550 (Citation Bravo) -0801 thru -1136 REASON Some PW500 engines have experienced surging and loss of thrust related to the operation of the engine bleed valve servo. NOTE: Refer to the attached P&WC documents for detailed information. DESCRIPTION To transmit the Pratt & Whitney Canada Corp (P&WC) documents as follows: P&WC Service Bulletin No. PW500-72-30420 P&WC Alert Service Bulletin No. PW500-72-A30421R1 P&WC Commercial Support Program Notification No. 1005303 NOTE: Make sure you must use the latest revision of the P&WC documents. COMPLIANCE MANDATORY. Refer to the attached P&WC documents for compliance times. MANPOWER WORK PHASE MAN-HOURS Modification Refer to the P&WC CSPN No. 1005303 Sep 1/2010 550-72-29 Page 1 of 2 Cessna Aircraft Company, Citation Marketing Division, P.O. Box 7706, Wichita, KS 67277, U.S.A. 1-316-517-6000, Fax 1-316-517-8500 COPYRIGHT 2010

Citation WARRANTY ALERT SERVICE LETTER ASL550-72-29 Eligibility: Refer to the P&WC CSPN No. 1005303 Parts: Labor: Authorized Citation Service Facilities, individual operators, or other maintenance facilities may submit a Credit Claim Form for the parts kit(s) required for accomplishment of this service letter, provided the work is completed and the claim submitted by the expiration date shown below. Authorized Citation Service Facilities may submit a Credit Claim Form for accomplishment of this service letter, on eligible airplanes, provided the work is completed and the claim submitted by the expiration date shown below. Expiration: Refer to the P&WC CSPN No. 1005303 REFERENCES P&WC Service Bulletin No. PW500-72-30420 P&WC Alert Service Bulletin No. PW500-72-A30421R1 P&WC Commercial Support Program Notification No. 1005303 NOTE: Make sure you must use the latest revision of the P&WC documents. PUBLICATIONS AFFECTED None ACCOMPLISHMENT INSTRUCTIONS 1. Do the attached P&WC Alert Service Bulletin PW500-72-30421 Revision 1 or later, Turbofan Engine Intercompressor Bleed Valve/ Servo-Valve - Inspection/Replacement of. NOTE: Make sure you must use the latest revision of the P&WC documents. 2. Record that this alert service letter has been completed. NOTE: This alert service letter cannot be recorded as complete until all actions are complete as outlined in the P&WC Alert Service Bulletin PW500-72-30421 Revision 1 or later. A. Complete a Maintenance Transaction Report. B. Put a copy of the completed Maintenance Transaction Report in the airplane logbook. C. Send a copy of the completed Maintenance Transaction Report to: CESCOM C/O Camp Systems International, 8200 East 34th Street North, Building 1600 Suite 1607 Wichita, KS 67226. Sep 1/2010 550-72-29 Page 2

P R A T T & WH ITN EY S DEPENDABLE EN G I N E BULLETIN INDEX LOCATOR 75-30-01 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF Commercial Support Program No: 1005303 Compliance: 3, 3, 3, 3 PRATT & WHITNEY CANADA ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 MODEL APPLICATION PW530A, PW545A, PW545B Summary: Some PW500 engines have experienced a lack of response to Power Lever Input due to a calibration shift of the servo valve which affects the compressor bleed valve operation. An accelerated replacement schedule (Ref. Para. 1.E. Compliance) is recommended for aircraft with a dual installation of post-sb30343 or post-sb30404 servo valves that have less than 250 hrs. of running time. Revision No. 1: Aug 27/2010 PW500-72-A30421 Cover Sheet 24-Hour Global Service USA & CANADA... 1-800-268-8000 Other... 1-450-647-8000 CFIRST CENTRE International... (IAC*)+8000-268-8000 Fax... 1-450-647-2888 Toll free where available (SIL GEN-027) * International Access Code Web Site... www.pwc.ca

WARNING - PROPRIETARY RIGHTS & EXPORT CONTROLS NOTICE This bulletin contains proprietary information of Pratt & Whitney Canada Corp. ( P&WC ), which P&WC provides in confidence and solely for the purposes of supporting engine certification and providing applicable information regarding the proper use, maintenance, inspection, repair, servicing and parts application of P&WC products and services, as directed therein. Neither this bulletin nor any information in it may be disclosed to others, or used for any other purpose, including, without limitation, to design, create, develop, reproduce, manufacture or derive any design, part, product, material, process, modification, configuration change or repair, or obtain FAA or other government approval to do so. Possession and use of this bulletin is also subject to the restrictions set out in P&WC s Technical Data Agreement (a copy of which may be obtained by contacting P&WC Technical Publications). The contents of this bulletin may be subject to export control laws. Unauthorized export or re-export of the bulletin, or parts thereof, is prohibited. By accepting and possessing this bulletin, you agree to be bound by the foregoing terms. If a Government agency or department intends to disclose any information, written notice should be given to: VP - Legal Services, Pratt & Whitney Canada Corp., 1000 Marie-Victorin (01BE5), Longueuil, Quebec J4G 1A1.

Pratt & Whitney Canada Corp. 1000, Marie-Victorin Longueuil, Québec, Canada J4G 1A1 Tél. 450-677-9411 27 August 2010 P&WC S.B. No. A30421R1 REVISION TRANSMITTAL SHEET MODEL PW500 SUBJECT: Pratt & Whitney Canada Service Bulletin No. PW500-72-A30421, Rev. No. 1, dated Aug 27/2010 (P&WC S.B. No. A30421R1) INTERCOMPRESSOR BLEED VALVE/SERVO- VALVE - INSPECTION/REPLACEMENT OF Replace your existing copy of this service bulletin with the attached revised bulletin. Destroy the superseded copy. Please retain this Revision Transmittal Sheet with the revised bulletin. SUMMARY: This revision is issued to: v add CSPN program Number. v clarify test conditions for part A in Para. 3. A. v correct some typo error in Para. 1. E. Compliance. EFFECT OF REVISION ON PRIOR ACCOMPLISHMENT: None. NOTE: A black bar in the left margin indicates a change in that line of text or figure. REVISION HISTORY: Original Issue: Revision No. 1: Aug 27/2010

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 1. Planning Information A. Effectivity PW530A Engines Post-SB30343 or Post-SB30404. PW545A Engines Post-SB30343 or Post-SB30404. PW545B Engines Post-SB30343 or Post-SB30404. B. Concurrent Requirements None. C. Reason (1) Problem Some PW500 engines have experienced a lack of response to Power Lever Input. (2) Cause A calibration shift of the servo valve which affects the compressor bleed valve operation. (3) Solution D. Description An accelerated replacement schedule is recommended for aircraft with a dual installation of post-sb30343 or post-sb30404 servo valves that have less than 250 hrs. of running time. Introduction of an accelerated replacement schedule for aircraft with a dual installation of post-sb30343 or post-sb30404 servo valves that have less than 250 hrs. of running time. E. Compliance PW545B Pre-SB30311 engines with Post-SB30343 or Post-SB30404 servo valves that have less than 250 hours (TTSN/TTSO) installed on both engines of the same aircraft; CATEGORY 3 - Do this SB on at least one engine on the aircraft within 15 hours. PW530A and PW545A engines with Post-SB30343 or Post-SB30404 servo valves that have less than 250 hours (TTSN/TTSO) installed on both engines of the same aircraft; CATEGORY 3 - Do this SB on at least one engine on the aircraft within 15 hours. P&WC No. N/A PW500-72-A30421 Revision No. 1: Aug 27/2010 2010 Pratt & Whitney Canada Corp. Page 1 of 7 PRINTED IN CANADA

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 1. Planning Information (Cont d) PW545B Post-SB30311 engines with Post-SB30343 or Post-SB30404 servo valves that have less than 250 hours (TTSN/TTSO) installed on both engines of the same aircraft; CATEGORY 3 - Do this SB on at least one engine on the aircraft within 35 hours. PW530A, PW545A and PW545B engines with Post-SB30343 or Post-SB30404 servo valves that have less than 250 hours (TTSN/TTSO) installed on only one engine of the same aircraft; CATEGORY 3 - Do this SB within 150 hours. NOTE: Incorporation of SB30343 or SB30404 on a Pre-SB servo-valve can only be carried out by overhauling the unit. Therefore, TTSO will accrue based on SB incorporation. F. Approval D.A.A. approved G. Manpower No more man-hours are necessary to include this service bulletin at maintenance. No more man-hours are necessary to include this service bulletin at overhaul. H. Weight and Balance None. I. Electrical Load Data Not changed. J. Software Accomplishment Summary Not applicable. K. References Illustrated Parts Catalog P/N 30J1114 (PW530A) Illustrated Parts Catalog P/N 30J1274 (PW545A) Illustrated Parts Catalog P/N 30J2244 (PW545B) Maintenance Manual P/N 30J1112 (PW530A) Maintenance Manual P/N 30J1272 (PW545A) PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 2 of 7

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 1. Planning Information (Cont d) Maintenance Manual P/N 30J2242 (PW545B) Overhaul Manual P/N 30J1113 (PW530A) Overhaul Manual P/N 30J1273 (PW545A) Overhaul Manual P/N 30J2243 (PW545B) P&WC S.B. No. 30311 P&WC S.B. No. 30343 P&WC S.B. No. 30404 P&WC S.B. No. 30420 L. Publications Affected None. M. Interchangeability and Intermixability of Parts Interchangeability - Refer to Para. 2.C. Intermixability - Not changed. 2. Material Information A. Industry Support Information Refer to Commercial Support Program Notification No. 1005303. B. Material - Cost and Availability You can get the procurable parts listed in Para. 2.C. from any Pratt & Whitney Canada Parts Distribution Center. The estimated total cost of new parts needed to replace old parts is $100.79 (US, 2010). The new parts are available. PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 3 of 7

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 2. Material Information (Cont d) C. Material Necessary for Each Engine The quantity of materials listed in this section is on a per Engine basis. Est. Unit List Price New P/N Keyword Old P/N Qty ($US, 2010) Instructions Disposition Standard Replacement Parts: 31J2468-01 Gasket 31J2468-01 1 41.93 (A) ST3881-01 Gasket ST3881-01 1 58.86 (A) (A) Standard replacement part. D. Reidentified Parts None. E. Tooling - Price and Availability Not applicable. 3. Accomplishment Instructions A. If the engine is within the compliance categories described above, you must comply with one of the following instructions and report the method of compliance to P&WC using the customer response sheet (Ref. Fig. 1): v For engines where the BOV servo valve has accumulated 50 hours or more of running time, P&WC recommends compliance through Part A. v For engines equipped with a BOV servo valve that has not yet accumulated 50 hours of running time, Part A is NOT recommended. Accomplishment is recommended through Part B or Part C or Part D. (1) Part A: Perform the following test procedure. The test procedure shall be run on one engine at a time: (a) (b) Prepare the aircraft and workspace as to perform engine run up to T.O. power. Disconnect the Bleed Off Valve (BOV) torque motor electrical connector in accordance with the maintenance manual (Ref. 75-30-01, COMPRESSOR BLEED AIR - MAINTENANCE PRACTICES). PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 4 of 7

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 3. Accomplishment Instructions (Cont d) (c) (d) (e) (f) (g) (h) Ensure the aircraft ECS system (pressurization system) is OFF, or set to the non-test engine. Ensure zero AGB loading, Alternator and Generator OFF. Start the engine and stabilize at idle for 5 minutes, ensuring engine oil temperature falls into the acceptable range for operation in accordance with the maintenance manual (Ref. 05-10-00, OPERATING LIMITS AND LEADING PARTICULARS). Perform a slam acceleration to the N1 target for T.O. for the day. When the N1 target is reached, hold for 30 seconds minimum then slam back to idle. Dwell at idle for 1 minute. Repeat 3 times. If the engine operates surge free throughout these checks, record installed orifice class in the engine logbook. Proceed to step (j). If the engine surges, proceed as follows: 1 Perform the secondary orifice adjustment by installing a larger orifice class. If the engine will not make power, reduce the orifice class. NOTE: Do not adjust orifice by more than 4 class sizes, each class size representing a 0.002 In. increment in orifice diameter. Start at the largest class size available. Subsequent tests per step (k) below shall not be adjusted outside the four class sizes of the original orifice class found on the engine. 2 Repeat steps (f) and if the engine operates surge free, record both the old and new orifice classes in the engine log book. (i) (j) (k) If the engine surges with the new secondary orifice, compliance to Part B or Part C or Part D must be accomplished. Reconnect the BOV Torque motor electrical connector in accordance with the maintenance manual (Ref. 75-30-01, COMPRESSOR BLEED AIR - MAINTENANCE PRACTICES). Compliance to Part A shall be repeated along the following intervals: v For engines equipped with a servo valve that has less than 100 hours, repeat this test every 25 hours. v For engines equipped with a servo valve that has 100 hours or more, repeat this test every 50 hours. PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 5 of 7

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF 3. Accomplishment Instructions (Cont d) v For engines with a servo valve that exceeds 250 hrs following successful accomplishment of the test at least once, repeated testing is no longer required. v In the event a servo valve is found to be unserviceable by failing to pass this test procedure, then compliance shall be accomplished through Part B or Part C or Part D. B. Part B: Accomplish the intent of P&WC SB No. 30420. C. Part C: Install a Servo Valve to SB30343 or SB30404 configuration with TTSN/TTSO greater than 250 hours. D. Part D: De-Mod the engine and install a Pre-SB30343 Servo Valve. E. Write accomplishment of P&WC S.B. No. 30421 Part A or Part B or Part C or Part D in the applicable engine module log book. 4. Appendix Not applicable. PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 6 of 7

ALERT SERVICE BULLETIN P&WC S.B. No. A30421R1 INTERCOMPRESSOR BLEED VALVE/SERVO-VALVE - INSPECTION/REPLACEMENT OF To P&WC PW500 Service Engineering FAX No. 450 647 2928 From Name: Operator: Maintenance Facility: FAX No. Please report the method of compliance employed, along with relevant information: PART A PART B PART C PART D Perform BOV servo valve check (use "servo valve installed" block in table below following successful check to report orifice classes removed/installed as applicable). Accomplished intent of SB 30420 Installed a Post SB30343 servo valve with TTSN greater than 250 hours Installed a Pre SB30343 servo valve Date of SB incorporation: Aircraft Registration Number: Aircraft Serial Number: LEFT ENGINE RIGHT ENGINE ENGINE Engine S/N: TTSN: TTSO: CSN: TCSO: SERVO VALVE REMOVED P/N: S/N: Servo Valve TTSN: Orifice Class: SERVO VALVE INSTALLED P/N: S/N: Servo Valve TTSN: (write zero if new or zero time overhauled) Orifice Class: C170965 Customer Response Sheet Figure 1 PW500-72-A30421 Revision No. 1: Aug 27/2010 Page 7 of 7

P R A T T & WH ITN EY S DEPENDABLE EN G I N E BULLETIN INDEX LOCATOR 75-30-01 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF MODEL APPLICATION PW530A, PW535A, PW535B, PW535E, PW545A, PW545B, PW545C Compliance: CATEGORY 3, 6 PRATT & WHITNEY CANADA SERVICE BULLETIN P&WC S.B. No. 30420 Summary: There can be a calibration shift of the servo valve which affects the compressor bleed valve operation. This is due to the movement of the internal metering post in the servo valve. Replace the servo valve with one that has: v a tighter fit between the metering post and the servo housing. v a material change of the post, clevis and torque motor retaining bolts. v the addition of washers for the torque motor retaining bolts. NOTE: Incorporation of the new part numbers stated in Para. 2.C. Material Necessary for Each Engine meets the intent of SB30404. PW500-72-30420 Cover Sheet 24-Hour Global Service USA & CANADA... 1-800-268-8000 Other... 1-450-647-8000 CFIRST CENTRE International... (IAC*)+8000-268-8000 Fax... 1-450-647-2888 Toll free where available (SIL GEN-027) * International Access Code Web Site... www.pwc.ca

WARNING - PROPRIETARY RIGHTS & EXPORT CONTROLS NOTICE This bulletin contains proprietary information of Pratt & Whitney Canada Corp. ( P&WC ), which P&WC provides in confidence and solely for the purposes of supporting engine certification and providing applicable information regarding the proper use, maintenance, inspection, repair, servicing and parts application of P&WC products and services, as directed therein. Neither this bulletin nor any information in it may be disclosed to others, or used for any other purpose, including, without limitation, to design, create, develop, reproduce, manufacture or derive any design, part, product, material, process, modification, configuration change or repair, or obtain FAA or other government approval to do so. Possession and use of this bulletin is also subject to the restrictions set out in P&WC s Technical Data Agreement (a copy of which may be obtained by contacting P&WC Technical Publications). The contents of this bulletin may be subject to export control laws. Unauthorized export or re-export of the bulletin, or parts thereof, is prohibited. By accepting and possessing this bulletin, you agree to be bound by the foregoing terms. If a Government agency or department intends to disclose any information, written notice should be given to: VP - Legal Services, Pratt & Whitney Canada Corp., 1000 Marie-Victorin (01BE5), Longueuil, Quebec J4G 1A1.

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF 1. Planning Information A. Effectivity PW530A Engines which are before and include Serial No. PCE-DA0699 PW535A Engines which are before and include Serial No. PCE-DC0367 PW535B Engines which are before and include Serial No. PCE-DE0136 All PW535E Engines PW545A Engines which are before and include Serial No. PCE-DB0773 PW545B Engines which are before and include Serial No. PCE-DD0681 PW545C Engines which are before and include Serial No. PCE-DF0149 B. Concurrent Requirements Pratt & Whitney Canada recommends to verify effectivity and compliance to SB30421. C. Reason (1) Problem There can be a calibration shift of the servo valve which affects the compressor bleed valve operation. (2) Cause Movement of the internal metering post in the servo valve. (3) Solution D. Description Replace the servo valve with one that has: v a tighter post to servo housing fit. v a material change of the post, clevis and torque motor retaining bolts. v the addition of washers for the torque motor retaining bolts. Replace the existing servo valve with a new or modified one. NOTE: Incorporation of the new part numbers stated in Para. 2.C. Material Necessary for Each Engine meets the intent of SB30404. E. Compliance For the PW530A, PW535A, PW535B, PW545A and PW545B engines that are either Post-SB30343 or Post-SB30404; CATEGORY 3 - Do this SB within 660 hours. P&WC No. E4145A, E4145C 2010 Pratt & Whitney Canada Corp. PRINTED IN CANADA PW500-72-30420 Page1of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF 1. Planning Information (Cont d) For the PW535E and PW545C engines; CATEGORY 3 - Do this SB within 660 hours. For the PW530A, PW535A, PW535B, PW545A and PW545B engines Pre-SB30343; CATEGORY 6 - P&WC recommends to do this service bulletin when the subassembly (i.e. module, accessories, components, or build groups) is disassembled and access is available to the necessary part. Do all spare subassemblies. F. Approval D.O.T./D.A.A. approved. G. Manpower Once you have access to the part, an estimate of 4 man-hours is required to include this service bulletin at maintenance. No more man-hours are necessary to include this service bulletin at overhaul. H. Weight and Balance None. I. Electrical Load Data Not changed. J. Software Accomplishment Summary Not applicable. K. References Illustrated Parts Catalog P/N 30J1114 (PW530A) Illustrated Parts Catalog P/N 3044954 (PW535A) Illustrated Parts Catalog P/N 3071824 (PW535B) Illustrated Parts Catalog P/N 3072704 (PW535E) Illustrated Parts Catalog P/N 30J1274 (PW545A) Illustrated Parts Catalog P/N 30J2244 (PW545B) Illustrated Parts Catalog P/N 30J2304 (PW545C) Maintenance Manual P/N 30J1112 (PW530A) Maintenance Manual P/N 3044952 (PW535A) PW500-72-30420 Page2of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF 1. Planning Information (Cont d) Maintenance Manual P/N 3071822 (PW535B) Maintenance Manual P/N 3072702 (PW535E) Maintenance Manual P/N 30J1272 (PW545A) Maintenance Manual P/N 30J2242 (PW545B) Maintenance Manual P/N 30J2302 (PW545C) Overhaul Manual P/N 30J1113 (PW530A) Overhaul Manual P/N 3044953 (PW535A) Overhaul Manual P/N 3071823 (PW535B) Overhaul Manual P/N 3072703 (PW545E) Overhaul Manual P/N 30J1273 (PW545A) Overhaul Manual P/N 30J2243 (PW545B) Overhaul Manual P/N 30J2303 (PW545C) P&WC S.B. No. 30311 P&WC S.B. No. 30343 P&WC S.B. No. 30404 P&WC S.B. No. 30421 L. Publications Affected Illustrated Parts Catalog P/N 30J1114 (PW530A) Illustrated Parts Catalog P/N 3044954 (PW535A) Illustrated Parts Catalog P/N 3071824 (PW535B) Illustrated Parts Catalog P/N 3072704 (PW535E) Illustrated Parts Catalog P/N 30J1274 (PW545A) Illustrated Parts Catalog P/N 30J2244 (PW545B) Illustrated Parts Catalog P/N 30J2304 (PW545C) M. Interchangeability and Intermixability of Parts Interchangeability - Refer to Para. 2.C. Intermixability - Not changed. 2. Material Information A. Industry Support Information Not applicable. B. Material - Cost and Availability You can get the procurable parts listed in Para. 2.C. from any Pratt & Whitney Canada Parts Distribution Center. The estimated total cost of new parts needed to replace old parts is $Quote (US, 2010). PW500-72-30420 Page3of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF 2. Material Information (Cont d) The new parts are scheduled to be available in August 2010. C. Material Necessary for Each Engine The quantity of materials listed in this section is on a per Engine basis. Est. Unit List Price New P/N Keyword Old P/N Qty ($US, 2010) Instructions Disposition For the PW535A, PW535B and PW535E Engines: 3075987-01 Valve, Servo, Intercompressor Blv 3073862-02 1 Quote (A)(B)(E) For the PW535A and PW535B Engines incorporating SB30343 but not incorporating SB30404 and for the PW535E engines not incorporating SB30404: Valve, Servo, Intercompressor Blv 3073862-01 1 Quote (A)(B)(E) 3075987-01 Valve, Servo, Intercompressor Blv 1 Quote (A)(D) For the PW530A, PW545A Engines: 30J3490-01 Valve, Servo, Intercompressor Blv 30J3204-02 1 Quote (A)(B)(E) For the Pre-SB30311 PW545B engines incorporating SB30404: 30J3490-01 Valve, Servo, Intercompressor Blv 30J3204-02 1 Quote (A)(B)(E) For the PW530A, PW545A engines and for Pre-SB30311 PW545B engines incorporating SB30343 but not incorporating SB30404: Valve, Servo, Intercompressor Blv 30J3204-01 1 Quote (A)(B)(E) 30J3490-01 Valve, Servo, Intercompressor Blv 1 Quote (A)(D) For the Post-SB30311 PW545B Engines incorporating SB30404: 30J3491-01 Valve, Servo, Intercompressor Blv 30J3052-02 1 Quote (A)(B)(E) PW500-72-30420 Page4of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF Est. Unit List Price New P/N Keyword Old P/N Qty ($US, 2010) Instructions Disposition For the PW545C Engines: 30J3491-01 Valve, Servo, Intercompressor Blv 30J3052-02 1 Quote (A)(B)(E) For the Post-SB30311 PW545B engines incorporating SB30343 but not incorporating SB30404 and for the PW545C engines not incorporating SB30404: Valve, Servo, Intercompressor Blv 30J3052-01 1 Quote (A)(B)(E) 30J3491-01 Valve, Servo, Intercompressor Blv 1 Quote (A)(D) Consumable Materials and Parts Required: For PW530A, PW545A, PW545B and PW545C Engines: 31J2468-01 Gasket 31J2468-01 1 41.93 (C) For PW535A, PW535B and PW535E Engines: 3052655-01 Gasket 3052655-01 1 41.59 (C) (A) TWO WAY INTERCHANGEABLE - (ATA 200 Explanation Code 02): The old or the new part can replace the old or the new part. (B) To get the new part it is possible to make a modification to the old part, or you can get the new part from any Pratt & Whitney Canada Distribution Center. (C) Standard replacement part. (D) Incorporation of the new part number meets the intent of SB30404. (E) Return the old part(s) to: Pratt & Whitney Component Solution Inc. 4905 Stariha Drive Muskegon MI 49441 USA Attention: Sales Department TEL: 1 (800) 872-1792 or 1 (231) 799-6650 FAX: 1 (231) 799-8732 EMAIL: spares@pwc.ca PW500-72-30420 Page5of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF D. Reidentified Parts The following list of parts can be reworked: OLD P/N NEW P/N 3073862-01 3075987-01 30J3204-01 30J3490-01 30J3052-01 30J3491-01 3073862-02 3075987-01 30J3204-02 30J3490-01 30J3052-02 30J3491-01 E. Tooling - Price and Availability Not applicable. 3. Accomplishment Instructions A. Remove the parts listed under the Old P/N column in Para. 2.C., Material Information. Refer to the instructions in the applicable maintenance manual (Ref. Chapter 75-30-01, COMPRESSOR BLEED AIR - MAINTENANCE PRACTICES) or overhaul manual (Ref. Chapter 72-00-00, DISASSEMBLY-2 EXTERNAL COMPONENTS). B. Return Old serviceable part(s) for modification in accordance with Para. 2.C. C. Install the parts listed under the New P/N column in Para. 2.C., Material Information. Refer to the instructions in the applicable maintenance manual (Ref. Chapter 72-30-01 COMPRESSOR BLEED AIR - MAINTENANCE PRACTICES 75-30-01) or overhaul manual (Ref. 72-00-00, ASSEMBLY-6 EXTERNAL COMPONENTS). D. Write accomplishment of P&WC S.B. No. 30420 in the applicable engine module log book. 4. Appendix A. Refer to Fig. 1 for parts progression. PW500-72-30420 Page6of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF BASIC 3052374 01 BASIC 3071810 01 3073862 01 SB30343 Various Improvements 3073862 01 SB30343 Various Improvements 3073862 02 SB30404 Improved Induction Brazing 3052374 01 SB30414 CC 10 PRC 02 3073862 02 SB30404 Improved Induction Brazing 3071810 01 SB30414 CC 10 PRC 02 3075987 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 3075987 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 PW535A PW535B C171047 Progression of the Servo Valve for the Intercompressor Bleed Valve Figure 1 (Sheet 1 of 4) PW500-72-30420 Page7of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF BASIC 31J2857 02 31J2857 03 SB30010 31J2857 04 SB30070 Higher Temp Capability 30J3204 01 SB30343 Various Improvements BASIC 3073862 01 3073862 02 SB30404 Improved Induction Brazing 3075987 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 PW535E 30J3204 02 SB30404 Improved Induction Brazing 31J2857 04 SB30414 CC 10 PRC 02 30J3490 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 PW530A C171367 Progression of the Servo Valve for the Intercompressor Bleed Valve Figure 1 (Sheet 2) PW500-72-30420 Page8of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF BASIC 31J2857 03 30J3052 01 BASIC 31J2857 04 SB30070 Higher Temp Capability 30J3052 02 SB30404 Improved Induction Brazing 30J3204 01 SB30343 Various Improvements 30J3491 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 30J3204 02 SB30404 Improved Induction Brazing 31J2857 04 SB30414 CC 10 PRC 02 PW545C 30J3490 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 PW545A C171048 Progression of the Servo Valve for the Intercompressor Bleed Valve Figure 1 (Sheet 3) PW500-72-30420 Page9of10

SERVICE BULLETIN P&WC S.B. No. 30420 INTERCOMPRESSOR BLEED VALVE/ SERVO-VALVE - REPLACEMENT/MODIFICATION OF PW545B BASIC 31J2857 04 30J3204 01 SB30343 Various Improvements 30J2961 01 SB30311 Improved Operability CC 8 PRC 07 30J3052 01 SB30343 Various Improvements 30J3052 02 SB30404 Improved Induction Brazing 30J3491 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 30J3204 02 SB30404 Improved Induction Brazing 31J2857 04 SB30414 CC 10 PRC 02 30J3490 01 SB30420 Tighter Post To Servo Fit CC 3/6 PRC 02 C171049 Progression of the Servo Valve for the Intercompressor Bleed Valve Figure 1 (Sheet 4) PW500-72-30420 Page 10 of 10

NO. 1005303 Page 1 of 3 COMMERCIALSUPPORTPROGRAM NOTIFICATION SPECIAL PROGRAM ALLOWANCE PROGRAM NAME: Servo Valve Replacement of APPLICABILITY: PW500 series engines in accordance with the Pratt & Whitney Canada Corp. (P&WC) Service Bulletins (SB) 30420, A30421 PROGRAM DESCRIPTION: This Commercial Support Program (CSP) offers assistance to the Operator to comply with SB 30420, A30421. PROGRAM DURATION: This program will terminate on 30 November 2015 REFERENCE DOCUMENT: P&WC SB 30420, SB A30421 COVERAGE: This CSP offers: Coverage1- Pre SB 30343 (Category 6) - The new Part Number listed under "PARTS AFFECTED" to the Operator at published Price List less 75% - A transportation allowance of $30.00 USD PARTS AFFECTED: New Part Number Qty/Eng Description 30J3490-01 1 VALVE-SERVO,INTERCOMPRESSOR 3075987-01 1 VALVE-SERVO,INTERCOMPRESSOR 30J3491-01 1 VALVE-SERVO,INTERCOMPRESSOR Date Issued: 2 August, 2010 QUESTIONSORCONCERNSMAYBEADDRESSEDTOTHE: MANAGER, WARRANTYADMINISTRATION TEL.(450)647-4012,FAX(450)647-2831 INTHEEVENTOFACONFLICT BETWEEN THEPROVISIONSOFTHISDOCUMENTAND OTHERNOTIFICATIONS,THISNOTIFICATION SHALLPREVAIL.

Commercial Support Program No. 1005303 Page 2 of 3 Coverage 2-Post SB 30343 (Category 3) - The new Part Number listed under "PARTS AFFECTED" to the Operator at No Charge - A maximum of 15 hours labour allowance per engine at the current P&WC warranty labour rate. - A transportation allowance of $30.00 USD PARTS AFFECTED: New Part Number Qty/Eng Description 31J2857-04 1 INTERCOMPRESSOR BLEED SERVO 3052374-01 1 VALVE-SERVO,INTERCOMPR BL V 3071810-01 1 VALVE-SERVO,INTERCOMPR BL V 30J2961-01 1 INTERCOMPRESSOR BLEED SERVO 30J3490-01 1 VALVE-SERVO,INTERCOMPRESSOR BLV 3075987-01 1 VALVE-SERVO,INTERCOMPRESSOR BLV 31J2468-01 1 GASKET-3 HOLE 3052655-01 1 GASKET-3 HOLE 30J1296 1 METERING PLUG-SECONDARY 3052373 1 METERING PLUG-SECONDARY ST3881-01 1 GASKET-.630, 2 HOLES 3052645-01 1 GASKET-.500,2 HOLE ORDER INSTRUCTIONS: For Operators The Operator may order the new Part Number by submitting a Purchase Order to his regular P&WC Parts Distribution Center (PDC). Please ensure that the engine model, engine serial number and this CSP number 1005303 are clearly indicated on all documents submitted. P&WC owned or affiliated Service Centers (Shop) If the Operator decides to have this CSP incorporated by a Shop, it is the Shop's responsibility to verify with the Operator that the part covered by this CSP has not already been ordered by the Operator. Part listed under PARTS AFFECTED is to be ordered by the Shop at the published Price List less the Shop's normal acquisition discount. CLAIM INSTRUCTIONS: For Operators A warranty claim must be submitted through the source of supply (i.e. PDC) for: - The difference between the price originally paid for the part and the discounted price as defined under "COVERAGE". - A maximum of 15 hours labour allowance (as applicable on Coverage 2) per engine at the current P&WC warranty labour rate. - A transportation allowance of $30 USD Date Issued: 2 August, 2010

Commercial Support Program No. 1005303 Page 3 of 3 For Shops A warranty claim must be submitted through P&WC Warranty Administration for: - The difference between the price originally paid for the part and the discounted price as defined under "COVERAGE". - A maximum of 15 hours labour allowance (as applicable on Coverage 2) per engine at the current P&WC warranty labour rate. - A transportation allowance of $30 USD Please ensure that the engine model, engine serial number, hours/cycles (TTSN/TCSN/TTSO) and this CSP number 1005303 are clearly indicated on all documents submitted. NOTE: Failure to comply with the preceding instructions may delay or void the warranty claim and/or the offered CSP coverage. P&WC may refuse any claim for coverage under this program that is received more than one hundred and eighty (180) days after compliance with this program. REMOVED MATERIAL DISPOSITION: Removed parts are to be scrapped locally. Date Issued: 2 August, 2010