ILLUSTRATED PARTS CATALOG STC SR01616SE
|
|
|
- Jared Thompson
- 5 years ago
- Views:
Transcription
1 ILLUSTRATED PARTS CATALOG STC SR066SE ENGINE INLET BARRIER FILTER SYSTEM Sikorsky S-76A+/A++/C/C+ This document provides information to assist with the identification of parts and assemblies for the 076T- / -5 Engine Inlet Barrier Filter Systems installed on the Sikorsky S-76A+/A++/C/C+ helicopters in accordance with STC SR066SE. This IPC is applicable only to aircraft models listed above and installed per above listed STC. Reference Sikorsky S-76C Series IPC for S-76C++ helicopters. Page of 8
2 RECORD OF REVISIONS When updated, this document is revised in its entirety. REV DATE DESCRIPTION PREPARED APPROVED NC 04-Nov-0 Initial release B. Vinson D. Nelson A Changed name to Aerometals and updated format. Updated contact information. R. Bannister B. Kellogg The information contained in this document is for information purposes only, and is not to be used for maintenance. The parts and assemblies indicated in this document are the only parts and assemblies authorized by Aerometals for replacement on Aerometals products. The data contained herein is not FAA approved, and is provided by Aerometals for information purposes only. While every effort has been made to ensure the accuracy and completeness of this information, Aerometals cannot be held liable for errors or omissions. It is the responsibility of the user of this document to verify that it is the latest revision released by Aerometals. It is Aerometals intention to provide our customers with the best possible support and assistance with our products. Please contact us using the information below to get the latest version of this and other documents. Aerometals also welcomes your reports of errors or omissions, and we value your suggestions to improve this and other documents. Aerometals 90 Sandstone Dr. El Dorado Hills, CA 9576 Tel: Fax: Page of 8
3 Documentation Feedback Aerometals welcomes your reports of errors or omissions, and we value your suggestions to improve this and other documents. Return via FAX or to: Aerometals Product Support (96) Page: Item #: Now Reads: Should Read: Comments: Your Name: Address: Position: Telephone No: Company: Page of 8
4 Filter System Locations on Aircraft Cockpit Instrument Panel Cockpit Circuit Breaker Panel Filter Element Installation Oil Tube Installation Baseplate Installation IBF Relay Installation Page 4 of 8
5 Filter Element Installation (Left side shown) 4 See Engine Wash Installation FILTER ELEMENT INSTALLATION 076A- () (Alt: ) Main Element See above () 076A4- () (Alt: ) Front Element See above () MS709C-08 Screw () 4 NAS49C0R Washer () () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () For spares, P/N 076K0- Filter Element Kit is available. P/N 076K0- contains ea. P/N 076A- Main Element and ea. P/N 076A4- Front Element. Page 5 of 8
6 Engine Wash Installation (Left side shown) ENGINE WASH INSTALLATION 076P0- Wash Tube Assembly () MS709C-08 Screw () NAS49C0R Washer () 4 AS55-04K0055 () Hose (Alt: 7K005-4CR0055) See above () 5 076A8- Bracket Assembly, Left Page 6 of 8
7 ENGINE WASH INSTALLATION 5 076A8- Bracket Assembly, Right 6 AN8-4J Fitting () 7 NAS49C076R Washer --- () 8 NAS4C7 Nut --- () 9 AN99-4J () Cap () 0 MS0995C () Lockwire --- A/R () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () Kit S/Ns used P/N AS55-04K0047, which is superseded by item 4 for spares. () If aircraft is not equipped with engine wash system, items 9 and 0 are installed on item and items 4, 5, 6, 7, and 8 are omitted. Page 7 of 8
8 PN 076A- Main Element Breakdown P4- () Seal See above MS Screw P7- Bayonet Mount Stud See above () Shim Washer --- A/R () Shim Washer --- A/R () Shim Washer --- A/R () Shim Washer --- A/R () Reference Service Bulletin 076-SB-005 for seal replacement procedure. () Shim washers are used, in combination, as required for proper adjustment of bayonet mount studs. Reference 076-SERIES-ICA- for adjustment procedures. Page 8 of 8
9 PN 076A4- Front Element Breakdown PN 076A4- FRONT ELEMENT BREAKDOWN 076P- () Seal See above 600-SW (Alt: 6S5-) ¼-Turn Stud See above 8 (Alt: 604-) 600-ES Spring See above 8 4 MS046AD4-4 Rivet MS046AD-4 Rivet MS076LN Nutplate --- () Reference Service Bulletin 076-SB-005 for seal replacement procedure. Page 9 of 8
10 Oil Tube Installation (Left side shown) (Right side opposite, except as shown in figure and table) 5 6 X See Differential Pressure Transducer Installation X X 4 0 X Page 0 of 8
11 Oil Tube Installation (Right side shown) 4 5 Page of 8
12 OIL TUBE INSTALLATION 076P45-04 (Alt: ) (Alt: ) Tube, Oil Return, Left See above 076P45-04 (Alt: ) Tube, Oil Return, Right P45-04 (Alt: ) Tube, Oil From Engine, Left See above 076P (Alt: ) Tube, Oil From Engine, Right P (Alt: ) Tube, Vent, Left See above 076P (Alt: ) Tube, Vent, Right AN85-0D () Union See above 5 SS4D0E () Hose Assembly, Oil Return See above 6 AN74Z Bracket, Support Clamp --- () 7 076P4- Doubler, Left Front Not shown 7 076P9- Doubler, Right Front Not shown 8 076P4- Doubler, Left Rear Not shown 8 076P40- Doubler, Right Rear Not shown 9 CR Rivet --- A/R 0 076A7- Bracket Assembly Not shown () ANCA Bolt --- () NAS49C0R Washer () MS99WDG Clamp See above 6 () 4 ANC4A Bolt --- () 5 MS99WDG8 Clamp See above () 6 MS99WDG0 Clamp See above 6 () 7 ANCA Bolt () 8 NAS4DD-8N Spacer () 9 MS04- Nut () 0 ANC5A Bolt --- () () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () Noted components are only on S-76A+/A++/C model helicopters, and only if not previously installed on aircraft. Page of 8
13 Differential Pressure Transducer Installation (Left side shown) (Not Shown) 0 4 DIFFERENTIAL PRESSURE TRANSDUCER INSTALLATION 076A5- Transducer Mounting Base See above () A50- (Alt. APTE D) Differential Pressure Transducer See above () (Alt. APTE D) A590- () Transducer Filter See above () 4 AS55-04K0 Hose See above () 5 076E4- Harness Assembly, Transducer (Left) Not shown 5 076E4- Harness Assembly, Transducer (Right) Not shown 6 S75SSH6R Clamp See above 4 () 7 MS709C-08 Screw () 8 NAS49C0R () Washer () 9 MS709C-09 Screw () 0 MS0995C Lockwire --- A/R NAS4DD-65N () Spacer Not shown () NAS60-6P () Screw Not shown () () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () Install with anti-seize compound per MIL-PRF-848. Do not block port or filter. Torque to in-lbs. () Noted screw, spacer, and x washers are installed on the forward, inboard mount location of item 6. Existing aircraft wiring clamp is reinstalled onto noted screw to secure wires. Page of 8
14 Baseplate Installation (Left side shown) BASE ASSEMBLY INSTALLATION 076AL- Base Assembly, Left See above 076AR- Base Assembly, Right See above ANC5A () Bolt () NAS49C0R () Washer () () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () Bolts and washers are installed from aft side of firewall. ea. on inboard side of each base assembly ea. on outboard side of each base assembly ea. on upper-center area of each base assembly Page 4 of 8
15 PNs 076AL- / 076AR- Baseplate Breakdown (PN 076AL- Left Baseplate shown) (PN 076AR- Right Baseplate opposite, except as noted in table) PNs 076P0L- / 076P0R- Pressure Tap Breakdown (PN 076P0L- pressure tap, left shown.) (PN 076P0R- pressure tap, right opposite) 7 Page 5 of 8
16 PNS 076AL- / 076AR- BASEPLATE BREAKDOWN 076AL-5 () P-Seal Sub-Assembly (Left Side) See above 076AR-5 () P-Seal Sub-Assembly (Right Side) P0L- () Pressure Tap, Left See above 076P0R- (4) Pressure Tap, Right P- Bracket, Upper Mount See above 4 () 4 NAS60-9P Screw () 5 NAS49C0R Washer () 6 NAS54P0-9P Screw --- () 7 MS076LN Nutplate --- () 8-5A Fiberglass Tape --- A/R 9 MS046AD4-7 Rivet () 0 MS046AD-5 Rivet () MS046A4-6 Rivet --- (5) MS046AD-4 Rivet () () Quantity shown reflects total quantity between left and right side installations. Half of the quantity shown is required for the left side, and half is required for the right side. () Reference Service Bulletin 076-SB-006 for P-Seal replacement procedure. () Reference Service Bulletin 076-SB-0008 P/N 076P0L- used, with P/N 076P7-, on P/N 076AL- baseplate S/Ns 000L - 0L. PN 076P0L- used on P/N 076AL- baseplate S/Ns 04L - subsequent. PN 076P0L- supersedes P/N 076P0L- for spares. (4) Reference Service Bulletin 076-SB-0008 PN 076P0R- used, with P/N 076P7-, on P/N 076AR- baseplate S/Ns 000R 04R. PN 076P0R- used on P/N 076AR- baseplate SNs 05R - subsequent. PN 076P0R- supersedes P/N 076P0R- for spares. (5) Quantity 7 used on P/N 076AL-. Quantity 6 used on P/N 076AR-. Page 6 of 8
17 Cockpit Instrument Panel (Location may vary) 4 (Location may vary) COCKPIT INSTRUMENT PANEL FHM () Filter Health Monitor (S-76A+/A++/C only) See above FHM () Filter Health Monitor (S-76C+ only) See above FHM () Overlay, Filter Health Monitor B Clamp Not shown 4 076E5- Caution Annunciator Light Assembly (S-76A+/A++/C only) See above () Reference Service Bulletin 076-SB-000 for overlay replacement. Cockpit Circuit Breaker Panel COCKPIT CIRCUIT BREAKER PANEL MS0- Circuit Breaker Not shown 076G0- Decal, Circuit Breaker Not shown Page 7 of 8
18 IBF Relay Installation (S-76A+/A++/C only) (Located in forward electrical compartment or cabin overhead) 4 IBF RELAY ASSEMBLY 076E8- IBF Relay Assembly See above NAS60-P Screw See above 4 NAS49FN8P Washer See above 8 4 MS04L08 Nut See above E7- Harness Assembly, IBF Relay to Instrument Panel Not shown 6 076E6- Harness Assembly, Monitor to IBF Relay Not shown Page 8 of 8
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
[Rev. 5, 11/07/07] PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 407H-120M BLEED-AIR CABIN HEATER INSTALLATION BELL MODEL 407 HELICOPTERS
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS DZUS SNOW DEFLECTOR INSTALLATION BELL 206L-1/L-3/L-4 AND 407 MODELS Cover Rev. 3, 12/12/05
*407AC-110-3, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *407AC-110-3, REV. D AIR CONDITIONER INSTALLATION 1 KIT
Bill of Materials *407AC-110-3, REV. D ITEM # P/N DESCRIPTION QTY TYP 0 *407AC-110-3, REV. D AIR CONDITIONER INSTALLATION 1 KIT 2 407AC-210-1 CONDENSER INSTALLATION 1 KIT 3 407AC-310-3 COMPRESSOR INSTALLATION
SUBJECT: FUEL SYSTEM FLOW SWITCHES, P/N , , -003, -101 AND -103, REPLACEMENT OF
ALERT SERVICE BULLETIN 206L-88-52 10 June 1988 Revision A, 26 March 2013 MODEL AFFECTED: 206L and 206L-1 SUBJECT: FUEL SYSTEM FLOW SWITCHES, P/N 206-063- 635-001, 206-064-601-001, -003, -101 AND -103,
HYDRAULIC SYSTEM #1 AND #2 ACCUMULATOR P/N , REMOVAL OF
TECHNICAL BULLETIN 212-17-216 24 May 2017 MODEL AFFECTED: 212 SUBJECT: HYDRAULIC SYSTEM #1 AND #2 ACCUMULATOR P/N 212-076-007-003, REMOVAL OF HELICOPTERS AFFECTED: Serial numbers 30502 through 30603, 30611
NOTE. KI & KI Revision H
KI-179-5 & KI-179-7 R22-series Kannad AF Integra ELT Installation Kit Instructions For R22 helicopters without ELTs or if replacing previously installed Pointer 3000-10 or 4000-10 ELT (RHC Inst l) NOTE
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS AND EQUIPMENT MAINTENANCE MANUAL FOR Bell 212/ 412 CARGO NET/TROOP SEAT
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FOR STC No. SR09485RC ON BELL 212/412 REPORT NUMBER HF-412-ICA-CARGO NET-01 HELIFAB 1318 SMEDE HWY. BROUSSARD, LA 70518 THIS MANUAL IS PREPARED TO PROVIDE INFORMATION,
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM. Figure Title Page 63-1 Main Rotor Gearbox and Mast Assembly Main Rotor Gearbox Installation
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM Figure Title Page 63-1 Main Rotor Gearbox and Mast Assembly...................... 63.0 63-5 Main Rotor Gearbox Installation............................. 63.4 63-7 Rotor
Oil Filter Kit AFC-K012
01 02 03 20a 04a 05 07 08 09 04b 10 20b 20c 06 15 16 17 18 19 11 12 14 13 Oil Filter Kit AFC-K012 Applicability: Hiller Helicopter Model UH12A, 12B, 12C, 12D, 12E, &12L4 First Release 11/01/95 with Franklin
INSTALLATION INSTRUCTIONS EXTERNAL AUXILIARY FUEL SYSTEM P/N
INSTALLATION INSTRUCTIONS EXTERNAL AUXILIARY FUEL SYSTEM P/N 41228-000-002-007 Page 1 of 45 List of Revisions Rev. Date Pages Description Approved IR 09/12/05 All Initial Release N/C All Updated to Apical
SERVICE INSTRUCTION SI Revision 1
SERVICE INSTRUCTION SI-25-02 Revision 1 TITLE: Aft Seats Inertia Reel Harness Installation (Mod 1229) SUBJECT / REASON / DESCRIPTION: The FBA-2C1 and FBA-2C2 aircraft are equipped with three individual
*C208ELP-100-1, REV. B ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-100-1, REV. B EXTERNAL LOAD PROVISIONS CONFIGURATION 1 KIT
Bill of Materials *C208ELP-100-1, REV. B ITEM # P/N DESCRIPTION QTY TYP 0 *C208ELP-100-1, REV. B EXTERNAL LOAD PROVISIONS CONFIGURATION 1 KIT 1 C208ELP-110-1 FWD EXTERNAL LOAD PROVISIONS INST'N 1 EA 2
OFFICE HOURS TECHNICAL SUPPORT SPARES ORDERS CORRESPONDENCE REGARDING ORDERS
Robinson Helicopter Company Phone: (310) 539-0508 2901 Airport Drive Fax: (310) 539-5198 Torrance, California 90505-6115 Web: www.robinsonheli.com UNITED STATES Email: customerservice@robinsonheli.com
P.68 VARIANTS. SERVICE INSTRUCTION No. 76 Rev. 2
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia tel +39 081 5918111 fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P.68 VARIANTS SERVICE INSTRUCTION No. 76 Rev. 2 (Supersedes the previous
SERVICE INFORMATION LETTER
SERVICE INFORMATION LETTER DATE: November 7, 2017 SERVICE INFORMATION LETTER NO. T-051 Page 1 of 7 1. SUBJECT: Vented Clutch Oil Reservoir, Kit P/N 4230001 2. MODEL: 480, 480B 3. EFFECTIVITY: S/N 5142
Bill of Materials *206EC-500-1, REV. M ITEM # P/N DESCRIPTION QTY TYP 0 *206EC-500-1, REV. M 206A/B BLEED AIR PLUMBING INST'N 1 KIT 1 NAS1149F1290P WA
Bill of Materials *206EC-500-1, REV. M ITEM # P/N DESCRIPTION QTY TYP 0 *206EC-500-1, REV. M 206A/B BLEED AIR PLUMBING INST'N 1 KIT 1 NAS1149F1290P WASHER 2 EA 2 ES00140-3 RUBBER EXTRUSION 12 IN 3 NAS43DD3-23FC
TECHNICAL BULLETIN May 2013 Revision A, 11 July 2013 SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF
TECHNICAL BULLETIN 206-13-205 24 May 2013 Revision A, 11 July 2013 MODEL AFFECTED: 206A/B SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF HELICOPTERS AFFECTED: Serial number 004 through 1251.
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 REPORT NO. PR-369DA-900M PNEUMATIC DOOR OPENER INSTALLATION INSTRUCTIONS FOR 369PDO-100 369, 500N & 600N HELICOPTERS Page i REVISIONS
Oil Filter Kit AFC-K005
22. 21. 20. 12. 03. 04. 06. 07. 24. 11. 05. 09. 08. 02. 01. 17. 19. 18. 23. 25. 13. 14. 15. 10. 11. 16. Oil Filter Kit AFC-K005 27. 26. Applicability: Aviat Husky Model A-1 with Lycoming First Release:
Service Bulletin. SB-GA Issue 1. Subject: Horizontal Stabiliser Attachment Area Inspection and Reinforcement. Applicability: Amendments:
PO Box 881, Morwell, Victoria 3840, Australia Ph + 61 (0) 3 5172 1200 Fax + 61 (0) 3 5172 1201 www.mahindraaerospace.com Service Bulletin SB-GA8-2016-163 Issue 1 OPTIONAL Subject: Horizontal Stabiliser
The engine cowling installation and firewall should be inspected and modified as specified in this Service Bulletin.
Single Engine Service Bulletin August 25, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280001 thru 17280724 172S 172S8001 thru 172S8201 REASON
SERVICE KIT thru , 631, 634, 675 R thru R F thru F FR thru FR
TITLE SEAT BELT AND SHOULDER HARNESS KIT INSTALLATION EFFECTIVITY MODEL SERIES SERIAL NUMBERS 182 33000 thru 18268368 182 613, 631, 634, 675 R182 R18200001 thru R18201973 F182 F18200001 thru F18200169
TECHNICAL BULLETIN May 2013 SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF
TECHNICAL BULLETIN 206-13-205 24 May 2013 MODEL AFFECTED: 206A/B SUBJECT: TAIL ROTOR GEARBOX 3 PIECE FAIRING, MODIFICATION OF HELICOPTERS AFFECTED: Serial number 004 through 1251. COMPLIANCE: At customer
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FORT COLLINS, COLORADO REPORT NO. PR-206H-900M CABIN HEATER SYSTEM INSTALLATION INSTRUCTIONS
PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FORT COLLINS, COLORADO 80524 REPORT NO. CABIN HEATER SYSTEM INSTALLATION INSTRUCTIONS BELL 206A/B HELICOPTERS Page i PR- Rev. P, 04/06/09 REVISIONS REV. DATE
LSM Rev P
Installation Instructions Cessna Citation CJ Series Landing Lights Models 525, 525A, 525B (S/N 525-0001 thru 525-0679, 525A-0001 thru 525A-0416, 525B-0001 thru 525B-0262, 525B-0264 thru 525B-0293) Cessna
P.68 VARIANTS. SERVICE BULLETIN No. 225 Rev. 1
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P.68 VARIANTS Approved by the Vulcanair Design Organisation The technical
P68 VARIANTS SERVICE INSTRUCTION. No. 82. SUBJECT: INCREMENT OF MAXIMUM TAKE-OFF WEIGHT FROM 1990 Kg TO 2084 Kg.
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 VARIANTS SERVICE INSTRUCTION No. 82 SUBJECT: INCREMENT OF MAXIMUM
Oil Filter Kit AFC-K003
03 16a / 16b 17 18 06 04 07 08 05 09 12 01 15 13 02 14 21 22 20 23 10 11 24 25 19 Oil Filter Kit AFC-K003 Applicability: Robinson Model R-22 with Lycoming First Release 10/05/92 Engines O-320 & O-360 Amended
P68 VARIANTS SERVICE INSTRUCTION. No. 88
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 VARIANTS SERVICE INSTRUCTION No. 88 SUBJECT: TYPICAL REPAIR OF
Revision Transmittal Sheet
b 2 APPROVED WHITE IN LEARJET 23/24/25, 28/29, 35/36 RT 0980 Revision Transmittal Sheet This page transmits Revision 1 to, Replacement of Air Conditioning Evaporator Assembly. Rework: No rework is required
A bar next to the text in the right hand margin indicates that the text has been changed as a result of the most recent document revision.
Cessna Aircraft Company Page 1 REVISIONS Rev Date By Approved By - 30 November 2009 Jay York A 18 March 2010 Jay York B 30 March 2010 Jay York ECR 067497 Section ALL Description Initial Release NOTE: A
FAA approval has been obtained on technical data in this publication that affects airplane type design.
Single Engine Service Bulletin January 28, 2008 TITLE ENGINE COWLING ALIGNMENT INSPECTION AND MODIFICATION EFFECTIVITY Model Serial Numbers 172R 17280725 thru 17281262 172S 172S8202 thru 172S10006 REASON
SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
MOONEY INTERNATIONAL CORPORATION SERVICE BULLETIN 165 Al Mooney Road North Kerrville, Texas 78028 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SERVICE BULLETIN M20-318 Date: June 2, 2014 SUBJECT:
AIRWOLF FILTER CORP Madison Rd. Middlefield, Ohio U.S.A. (440) / (440) Fax
AIRWOLF FILTER CORP. 15369 Madison Rd. Middlefield, Ohio 44062-8404 U.S.A. (440) 632-5136 / (440) 632-1685 Fax TO THE MECHANIC: This P/N AFC-K010 remote mount oil filter kit incorporates our generic STC
P68 VARIANTS SERVICE INSTRUCTION. No. 89
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 VARIANTS SERVICE INSTRUCTION No. 89 SUBJECT: MODIFICATION ON FRONT
PARAVION TECHNOLOGY, INC AIRWAY AVENUE FT. COLLINS, COLORADO 80524
Rev. 2, 01/31/00 PARAVION TECHNOLOGY, INC. 2001 AIRWAY AVENUE FT. COLLINS, COLORADO 80524 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 206ER-100 ENGINE RELIGHT SYSTEM INSTALLATION BELL MODEL 206A/B AND 206L
NOTE: This Service Bulletin may only be accomplished on airplanes equipped with the standby alternator system.
Caravan Service Bulletin October 19, 2009 CAB09-9 TITLE TKS ICE PROTECTION SYSTEM INSTALLATION EFFECTIVITY For the airplanes that follow that are equipped with a cargo pod but are not equipped with the
1) Page: REV 5: Changed depiction to show added hardware and T-01220
REVISION DESCRIPTION: 1) Page: 37-01 REV 5: Changed depiction to show added hardware and T-01220 Page: 37-02 REV 4: Added Figure 3 depicting Separating the T-01220 Doublers. Figure 4 was Figure 3. Added
REVISION DESCRIPTION:
REVISION DESCRIPTION: 14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm
KI (14V) & KI (28V) R44
KI-228-1 (14V) & KI-228-2 (28V) R44 Radar Altimeter Installation Kit Instructions For B050 upper console only; includes parts for In-Console and Above-Console installations. NOTE Visit www.robinsonheli.com
COMPOSITE INLET COWLING, RETROFIT OF. HELICOPTERS AFFECTED: Serial numbers through 45790, through and through
TECHNICAL BULLETIN 206L-18-255 28 June 2018 MODEL AFFECTED: 206L-1, 206L-3, and 206L-4 SUBJECT: COMPOSITE INLET COWLING, RETROFIT OF HELICOPTERS AFFECTED: Serial numbers 45154 through 45790, 51001 through
*Not applicable to AS350 B3 aircraft equipped with dual hydraulic system. E-1106, Rev. B 8/23/12. Contents: Installation Instruction
Installation Instructions Hose Modification Kit - Part Number: 1741321 For Eurocopter AS350 B, B1, B2, B3*, BA, EC130B4 & EC130T2 Helicopters Equipped with Purolator Oil Filter Kit P/N: 1741320 in Accordance
EFFECTIVITY Serial Numbers thru , 698
Conquest TITLE AILERON HINGE BRACKET REPLACEMENT EFFECTIVITY Model Serial Numbers 441 441-0001 thru 441-0349, 698 DESCRIPTION To install stainless-steel aileron hinge brackets as a replacement for aluminum
Revision Transmittal Sheet
2 APPROVED WHITE IN LEARJET 31 RT 31-32-24 Revision Transmittal Sheet This page transmits Revision 1 to No. 31-32-24, Main Landing Gear Torque Link Replacement. Rework: No rework is required for aircraft
SERVICE BULLETIN THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN
SERVICE BULLETIN SERVICE BULLETIN M20-325 THIS BULLETIN IS FAA APPROVED FOR ENGINEERING DESIGN SUBJECT: Service Instruction M20-88A - STABILIZER TRIM STOP/SCREW MODIFICATION Dated 12/14/2016. MODELS/ SN
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT Onboard Systems E-51 MD Helicopter Models 369D, 369E, 369F, 369FF, 369HE, 369HM, 369HS, 500N, 600N R/N S/N 1 of 5 Revision 1 PART I GENERAL This supplement
500W Series Instructions for Continued Airworthiness
Instructions for Continued Airworthiness Document Number Garmin International, Inc. 1200 E. 151st Street Olathe, Kansas 66062 USA Record of Revision Rev. Date Description of Change 1 10-19-06 Initial Release
NOTE ITEM PART NUMBER KIT CONTENTS QTY
R44 II Aux Fuel Pump Assembly Upgrade Installation Kit Instructions Applicable to helicopter S/N 13158 and prior equipped with D743-1, D743-2, or D743-4 Aux Fuel Pump. D743-1, D743-2, and D743-4 pumps
TABLE of CONTENTS. Installation Instructions and Instructions for Continued Airworthiness PFS-17101
TABLE of CONTENTS Section Page 1.0 Introduction... 3 1.1 Description... 3 1.2 Update Procedure... 3 2.0 Kit Contents... 4 3.0 Preparation... 5 4.0 Installation of PFS Exhaust System... 5 4.1 Installing
R66 Aux Fuel Tank Installation Relay Upgrade Kit Instructions (To comply with R66 Service Bulletin SB-24) NOTE
R66 Aux Fuel Tank Installation Relay Upgrade Kit Instructions (To comply with R66 Service Bulletin SB-24) NOTE Visit www.robinsonheli.com to verify kit instructions are current revision. Review instructions
All Cirrus Design SR22 aircraft equipped with a Tornado Alley Turbo Inc. Turbonormalizing System installed per STC SA10588SC and SE10589SC.
SUBJECT Service Instruction TAT SI11-01, Revision A Issued: 03/31/2011 Revised: 06/22/2016 Model SR22 w/ Turbonormalizer Installed per STC SA10588SC And SE10589SC Exhaust system inspection, cleaning, and
2.0 KIT CONTENTS INSTALLATION OF PFS EXHAUST SYSTEM INSTRUCTIONS FOR CONTINUED AIRWORTHINESS PASSENGER SIDE VIEW...
TABLE of CONTENTS 1.0 INTRODUCTION... 3 1.1 GENERAL... 3 1.2 DESCRIPTION... 3 1.3 UPGRADES... 3 2.0 KIT CONTENTS... 4 2.1 CLASSIC TAILPIPE KITS... 4 2.2 SHORT STACK TAILPIPE KITS... 5 3.0 PREPARATION...
FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE
Supplement No. AFS-BH206L3L4-IBF-KIT-FMS 17891 Chesterfield Airport Road FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE BELL HELICOPTER TEXTRON CANADA (BHTC) LIMITED BELL MODEL 206L-1, 206L-3
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS STC SR00180SE
INSTRUCTIONS FOR CONTINUED AIRWORTHINESS STC SR00180SE ENGINE INLET AIR FILTER SYSTEM BELL 206 AND 407 SERIES HELICOPTERS This supplement must be attached to the applicable Bell 206, A, A1, B, B1; Arrow
FOR REFERENCE ONLY 9
2 4 3 5 16 6 1 15 12 11 FOR REFERENCE ONLY 18 19 20 9 17 8 7 10 21 22 Applicability: BEECHCRAFT Drawing: AFC-W300 Debonair 35-33, 35-A33, 35-B33, 35-C33 Date: 06/01/05 Airwolf Parts List No. AFC-W300 Index
INSTALLATION INSTRUCTIONS SKID STEP and Utility Handles FOR MDHI 369D, 369E, 369FF, & 500N
INSTALLATION INSTRUCTIONS SKID STEP and Utility Handles FOR MDHI 369D, 369E, 369FF, & 500N AEROCRAFT INC. 4420 COMMODITY WAY, UNIT B SHINGLE SPRINGS, CA 95682 LOG OF REVISIONS REVISION DATE PAGES EFFECTED
P68 SERIES SERVICE INSTRUCTION
vulcanair spa via g. pascoli, 7 80026 casoria (na) italia Tel +39 081 5918111 Fax +39 081 5918172 info@vulcanair.com www.vulcanair.com P68 SERIES SERVICE INSTRUCTION No. 61 Rev. 1 SUBJECT: NEW EGT INDICATOR
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL REASON This sheet transmits Revision 1 to, which: A. Adds instructions and parts to change the Pulselite controller for airplanes with the Pulselite feature. NOTE: This revision replaces
Ignitor supplied with Engine. Power Plant Group - Page 1 (AT-502B) Date: 1/18
4 9 8 9 48 0 4 4 0 0 4 4 Ignitor supplied with Engine 8 4 4 4 Power Plant Group - Page (AT-0B) Date: / POWER PLANT GROUP - Figure. Power Plant, Engine Mount, Oil Cooler and Ejector Installations 04-8 Engine
IOF-240-B4B ENGINE CONVERSION. All IOF-240-B4B Engines
SSI--002 REASON FOR ACTION PURPOSE COMPLIANCE MODELS AFFECTED FADEC Software Upgrade. To provide instructions for conversion of all IOF-240-B specification 4B engines to the IOF-240-B specification 5B.
aileron rib inspection
Piper Aircraft, Inc. 2926 Piper Drive Vero Beach, Florida, U.S.A. 32960 SERVICE NO. 1216B BULLETIN PIPER CONSIDERS COMPLIANCE MANDATORY Date: September 5, 2012 (S) Service Bulletin 1216B supersedes Service
Service Bulletin No: Ref No: 105 Modification No: INSPECTION ATA Chapter: 32
PILATUS AIRCRAFT LTD. STANS, SWITZERLAND Service Bulletin No: 32-010 Ref No: 105 Modification No: INSPECTION ATA Chapter: 32 LANDING GEAR - MAIN GEAR AND DOORS INSPECTION OF THE MAIN-GEAR SUPPORT STRUT
CHAPTER 63 MAIN ROTOR DRIVE SYSTEM
Section Title CHAPTER 63 MAIN ROTOR DRIVE SYSTEM 63-00 Description............................................... 63.1 63-10 Engine Shaft Weldment...................................... 63.1 63-11 (Engine
Service Bulletin No.: D42L Rev 2 Date Issued: 05 October 2012 Title: ADF System Improvements Page: 1 of 16
Title: ADF System Improvements Page: 1 of 16 1. ATA Code: 3450 2. Effectivity: All DA42 aircraft with Transport Canada Civil Aviation (TCCA) STC SA09-54 or Federal Aviation Administration (FAA) STC SA02725NY
Power Flow System Extractor Exhaust System Installation Instructions Cessna 172, 175 TABLE OF CONTENTS
Heading Power Flow System Extractor Exhaust System Installation Instructions TABLE OF CONTENTS Pages Introduction 3 Kit Contents Classic Tailpipes 4 Kit Contents Short Stack Tailpipes 5 Preparation 6 Removal
SERVICE BULLETIN TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE
TITLE AIR CONDITIONING - R134A AIR CONDITIONER SYSTEM INSTALLATION FOR AIRPLANES EQUIPPED WITH G1000 AND 867 SHP ENGINE EFFECTIVITY DESCRIPTION MODEL 208B SERIAL NUMBERS 208B5000 and On To provide parts
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the CI401-460 GPS Antenna to Step 10A and Step 10B. B. Adds the CI401-460 GPS Antenna to Figure 5. C. Adds the CI401-460 GPS Antenna
J.P.Instruments Inc B Airway Ave Costa Mesa CA Fax
EDM-900/930 Instructions for Continued Airworthiness Rev E Date 5-24-2014 Page 1 of 6 J.P.Instruments Inc.. 3185B Airway Ave Costa Mesa CA 92626 714 557 3805 Fax 714 557 9840 EDM 900/930 Instructions for
SERVICE BULLETIN REVISION TRANSMITTAL
REVISION TRANSMITTAL This sheet transmits Revision 2 to, which: A. Adds the reference to Figure 7, Sheet 1 and Sheet 2 to Step 10D. B. Adds Step 10D(7). C. Removes the After Modification view for PN343
Revision Control Page REPORT PFS Kit PFS REVISION DATE REMOVE PAGES
Revision Control Page REPORT PFS-0020-00 Kit PFS-13203 REVISION DATE REMOVE PAGES INSERT PAGES IR 06/27/00 N/A N/A A 09/21/00 1,2,4,14 1,2,4,14 B 02/12/01 1,2,4,8,9,13 1,2,4,8,9,13 C 09/14/01 1,2,3,4,5,6,7,8
Oil Filter Kit AFC-K001
Oil Filter Kit AFC-K001 Applicability: Homebuilt Aircraft using Lycoming O-235, 290, 320, 340, 360 & 540 First Release 06//84 Engines using the Lycoming P/N 69510, 68974, or 62815 4-bolt NEW oil screen
Service Bulletin. ATA 52-10: Passenger and Crew Doors Door Latching Assembly Upgrade
Service Bulletin Issued: 5 Oct 00 Models SR0 and SR ATA 5-10: Passenger and Crew Doors Door Latching Assembly Upgrade COMPLIANCE Optional: Accomplishment of this Service Bulletin is at the owner s option.
POWER TURBINE RPM (N2) STEADY STATE OPERATION AVOIDANCE, INTRODUCTION OF.
SERVICE BULLETIN 206L-08-150 20 May 2008 Revision A, 3 March 2009 Revision B, 25 July 2018 MODEL AFFECTED: 206L-1, 206L-3, and 206 L-4 SUBJECT: HELICOPTERS AFFECTED: COMPLIANCE: POWER TURBINE RPM (N2)
APICAL S-76 BAGGAGE DOOR LIFERAFT KIT
2608 Temple Heights Dr. FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE SIKORSKY MODELS S-76A, S-76B, & S-76C FAA APPROVED ROTORCRAFT FLIGHT MANUAL When Equipped with APICAL S-76 BAGGAGE DOOR LIFERAFT
PC-6 SERVICE BULLETIN NO: 180 REF NO: 180 MODIFICATION NO: N/A ATA CHAPTER: 27. All PC-6 aircraft. None.
3,/$786$,5&5$)7/7'&+67$166:,7=(5/$1' SERVICE BULLETIN NO: 180 REF NO: 180 MODIFICATION NO: N/A ATA CHAPTER: 27 )/,*+7&21752/6+25,=217$/67$%,/,=(5,167$//$7,212)$75,0:$51,1*6
Service Bulletin. ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification
Service Bulletin Issued: 09 May 2007 Models SR20 and SR22 ATA 27-00: Flight Controls Rudder-Aileron Interconnect Modification COMPLIANCE Mandatory: Accomplish this Service Bulletin within 25 Flight Hours
53-40 ATTACH FITTINGS
ATTACH FITTINGS. DESCRIPTION Attach fittings are provided for attachment of the seats (Refer to -0), baggage straps (Refer to -0), rear seat harnesses (Refer to -0), cargo net straps (Refer to -0), cabin
READ THIS BEFORE INSTALLING AIR/OIL SEPARATOR DATA PERTINENT TO ALL INSTALLATIONS
AIRWOLF FILTER CORP. 15369 Madison Rd. Middlefield, Ohio 44062-8404 U.S.A. USA-1-(440) 632-5139 / (440) 632-1685 Fax http://www.airwolf.com / Email: support@airwolf.com READ THIS BEFORE INSTALLING AIR/OIL
Nomad RE -ALIGNMENT HORIZONTAL STABILISER CONTROL PULLEY (MOD N63) Page No Rev No
RE -ALIGNMENT HORIZONTAL STABILISER CONTROL PULLEY (MOD N63) 1. PLANNING INFORMATION A. Effectivity: (1) Aircraft Affected: All Nomad N22-Series and N24-Series aircraft whose log books do not already record
Page: MEMO: In NOTE before Step 5, "Whenever possible, ream using a drill press..." was "Always ream using a drill press...".
14401 Keil Road NE, Aurora, Oregon, USA 97002 PHONE 503-678-6545 FAX 503-678-6560 www.vansaircraft.com info@vansaircraft.com Service Letters and Bulletins: www.vansaircraft.com/public/service.htm REVISION
MODIFICATION KIT. Serial Numbers 300 (LC40-550FG) thru (LC42-550FG) thru (LC41-550FG) thru
Single Engine MODIFICATION KIT MK400-71-01 TITLE ENGINE OIL COOLER WINTERIZATION MODIFICATION EFFECTIVITY Model Serial Numbers 300 (LC40-550FG) 40004 thru 40079 350 (LC42-550FG) 42001 thru 421018 400 (LC41-550FG)
REVISION LIST CHAPTER 15: SEATS AND SEAT BELTS
REVISION LIST CHAPTER 15: SEATS AND SEAT BELTS The following list of revisions will allow you to update the Legacy construction manual chapter listed above. Under the Action column, R&R directs you to
SERVICE DIRECTIVE BULLETIN
SERVICE DIRECTIVE BULLETIN DATE: February 15, 2019 Page 1 of 11 1. SUBJECT: Main Rotor Push-Pull Rod Inspection 2. MODEL: F-28, F-28A, 280, F-28C, F-28C-2, F-28C-2R, 280C, F-28F, F-28F-R, 280F, and 280FX
6: PA32-260, PA32-300, PA32S-300
1 3 4 6 7 8 9 10 11 12 20 21 2 5 22 14 24 15 07 23 17 16 25 18 19 26 27 28 FOR REFERENCE ONLY Applicability: PIPER [Non Turbo Charged] Drawing: AFC-W315 Lance: PA32R-300, PA32RT-300 Saratoga: PA32-301,
39 - EFFECTIVE PAGES. Beechcraft Corporation PAGE 1 AUG 01/17 99 ILLUSTRATED PARTS CATALOG DATE CH-SECT-FIG
CH-SECT-FIG PAGE NO. DATE CH-SECT-FIG PAGE NO. DATE 39 - CONTENTS 1 39-10-10 0 39-10-10 1 39-10-10 2 39-10-20 0 39-10-20 1 39-10-20 2 39-10-20 3 39-10-20 4 39-10-20 5 39-10-20 6 39-10-30 0 39-10-30 0A
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING SERVICE LETTER 189
WIPLINE FLOATS SKIS MODIFICATIONS AIRCRAFT SALES AVIONICS INTERIOR MAINTENANCE PAINT REFINISHING Aircraft Makes/Model(s): Float Model(s): Compliance: As required By: MB Textron Aviation 208 and 208B 8750
Please replace any copy of SEB07-2 with the attached copy of SEB07-2 Revision 1 which is printed in its entirety.
Revision Transmittal May 14, 2007 TO: Cessna Distributors, Single Engine Service Stations and CPC's SUBJECT: Single Engine Service Bulletin SEB07-2 Revision 1: Engine Mount Bracket Inspection. REASON FOR
FAA APPROVED. Dated: January 20, Airplane Serial No:
INSTALLATION OF SADDLE TANKS FOR BEECHCRAFT KING AIR AIRPLANES 200, 200C, A200, A200C, B200, B200C, B200GT, B200CGT 300, B300, AND B300C SUPPLEMENTAL TYPE CERTIFICATE NUMBER SA11142SC FAA APPROVED Airplane
SINGLE ACCENT LIGHT KIT
SINGLE ACCENT LIGHT KIT P/N 2880532, 2880533, 2881176, 2882379 APPLICATION Verify accessory fitment at Polaris.com. BEFORE YOU BEGIN Read these instructions and check to be sure all parts and tools are
ROLL BAR FRAME 2 PLACES F-1231A-FL ROLL BAR FRAME F-1231C INBOARD F-1231B OUTBOARD ROLL BAR STRAP BAGGAGE BULKHEAD
SECTION 24iS/U: ROLLOVER F-1231A-FR ROLL BAR FRAME VAN'S AIRCRAFT, INC. F-1231A-AR ROLL BAR FRAME STRUCTURE F-1231E ROLL BAR SPLICE PLATE 2 PLACES F-1232A ROLL BAR BRACE F-01254-R-1 SUPPORT FRAME & F-01207
FOR REFERENCE ONLY. 310, A, B, C, D, E, F, G, H, E310H, I, J, K, L, N, P, Q Date: 06/01/05 WITH TCM O/IO-470 ENGINES
FOR REFERENCE ONLY Applicability: CESSNA 310, A, B, C, D, E, F, G, H, E310H, I, J, K, L, N, P, Q Date: 06/01/05 WITH TCM O/IO-470 ENGINES Airwolf Parts List No. AFC-W329-A Index Part Number Description
10-0 Issued: JUL 2008
10-0 Issued: JUL 2008 FIGURE 10-1 CONSOLE ASSEMBLY - TEN-INSTRUMENT/IFR TRAINER CONSOLE ASSEMBLY - TEN-INSTRUMENT/IFR TRAINER 10-1-1 A226-9 Moulding (install using item 72; alternate part no. ZX-4183)
ROTORCRAFT FLIGHT MANUAL SUPPLEMENT
FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT Bell Helicopter Models 204B, 205A, 205A-1, 210, 212, 412, 412EP, Agusta Helicopter Models AB412, AB412EP Garlick Helicopter Model UH-1H R/N S/N 1 of 5 Revision
ALTERNATE LUBRICANT AERIOL THIXO SYN AVIATION GREASE (C-172) AND BEARING , INTRODUCTION OF.
TECHNICAL BULLETIN 206L-13-247 23 August 2013 Revision A, 23 September 2013 Revision B, 23 September 2017 MODEL AFFECTED: SUBJECT: HELICOPTERS AFFECTED: COMPLIANCE: 206L, 206L1, 206L3 and 206L4 ALTERNATE
SUBJECT: FUEL FITTING P/N AND , VERIFICATION OF.
ALERT SERVICE BULLETIN 212-18-159 13 September 2018 MODEL AFFECTED: 212 SUBJECT: FUEL FITTING P/N 50-040-1 AND 50-040-3, VERIFICATION OF. HELICOPTERS AFFECTED: Serial numbers 30502 through 30603, 30611
TYPE CERTIFICATE DATA SHEET
TYPE CERTIFICATE DATA SHEET No. EASA.IM.R.003 for Type Certificate Holder Erickson Incorporated, DBA Erickson Air-Crane 3100 Willow Springs Road P.O. Box 3247 Central Point, Oregon, 97502-0010 U.S.A. For
17891 Chesterfield Airport Road Chesterfield, MO FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE
Supplement No. AFS-BH205-IBF-FMS 17891 Chesterfield Airport Road FAA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE BELL HELICOPTER TEXTRON INC. BELL MODEL 205, UH-1H SERIES AND EAGLE SINGLE (SINGLE
INSTALLATION MANUAL Electrical SPEEDBRAKE 2000 Series
PRECISE FLIGHT, INC. 63354 POWELL BUTTE Installation Report Number: 08062 Document Number: 211SMAN0001 Revision Number: D Aircraft Serial Number: STC Number: SA2602NM www.preciseflight.com Make: CESSNA
AFT MOUNTED OXYGEN SYSTEM INSTALLATION BEECHCRAFT 33, 35, 36, 55, AND 58
ENGINE TECHNOLOGIES INC. REPORT 35-4960004, REV. A, JULY 12, 2013 INSTALLATION INSTRUCTIONS FOR OXYGEN SYSTEM ON HAWKER BEECHCRAFT S35, V35, V35A, V35B, 35-C33A, E33A, 36, A36, F33A, G33, 95-55, 95-A55,
Rotary Speed Brake Actuation System ICA Supplement
CESSNA AIRCRAFT COMPANY AIRCRAFT DIVISION WICHITA, KANSAS 67277 Rotary Speed Brake Actuation System ICA Supplement MODEL NO: 510 SUPPLEMENT NO: ICA-510-27-00001 SUPPLEMENT DATE: 04/28/2009 PREPARED BY: