Owners and Operators of Aircraft Using Woodward Propeller Governors, Pumps, Auto Feather Valves, and Speed Signal Generators.

Similar documents
SERVICE LETTER HM-SL-001 Overhaul Periods and Life Limits for Hartzell Propeller Inc. Maritime (Non-Aviation) Propellers

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

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

HARTZELL PROPELLER INC. SERVICE BULLETIN TRANSMITTAL SHEET HC-SB Propeller - Blade, Blade Retention Bearing, and Hub Inspection.

ALERT SERVICE LETTER

OPTIONAL EXTENSION OF TIME BETWEEN OVERHAULS (TBO) FOR ROTAX ENGINE TYPE 912 AND 914 (SERIES) SB SB Repeating symbols:

Service Bulletin. Service Bulletin No. 064 Alternator Model ALV-9610 Series Through Bolt Inspection for Proper Torque

AIRWORTHINESS DIRECTIVE

European Aviation Safety Agency

TYPE CERTIFICATE DATA SHEET

MOONEY INTERNATIONAL CORPORATION

SERVICE BULLETIN HC-SB Propeller - Blade Bearing Race Inspection Criteria

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

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

TYPE-CERTIFICATE DATA SHEET

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

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

HARTZELL PROPELLER INC. SERVICE BULLETIN TRANSMITTAL SHEET SERVICE BULLETIN HC-SB Propeller - Propeller Installation.

SUBJECT: MAIN ROTOR HUB ASSEMBLY SPINDLE ASSEMBLY, P/N , MANDATORY INSPECTION AND OVERHAUL REQUIREMENTS.

SERVICE BULLETIN MANDATORY. SB , Rev Planning Information

Service Information Letter

SAFETY ALERT / SAFETY DIRECTIVE

PROPELLERS - PROPELLER SLIP RING MOUNTING PLATE INSPECTION AND REPAIR

SA226 Series Engine AD and Time Compliance Sheet TPE U-521G TAT: TAC: Engine Last CURRENT ENGINE TIME AND CYCLES

BULLETIN INDEX LOCATOR

SERVICE BULLETIN HC-SB Propeller - Counterweight Clamp Inspection

TYPE CERTIFICATE DATA SHEET

HARTZELL PROPELLER INC. SERVICE LETTER

BULLETIN INDEX LOCATOR

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

BULLETIN INDEX LOCATOR

MAIN ROTOR BLADE ABRASION STRIP DAILY INSPECTION REQUIREMENTS

TYPE CERTIFICATE DATA SHEET

Cal Pacific Airmotive, Inc.

Airworthiness Directive

BULLETIN INDEX LOCATOR

SUBJECT: MAIN ROTOR DRIVE, ENGINE-TO- TRANSMISSION DRIVE SHAFT RETAINING NUTS INSPECTION/REPLACEMENT

HARTZELL PROPELLER INC.

Airworthiness Directive Schedule

TYPE-CERTIFICATE DATA SHEET

TYPE-CERTIFICATE DATA SHEET

Airworthiness Directive Schedule

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

FJ44 SERVICE BULLETIN

SERVICE INSTRUCTION PURGING OF LUBRICATION SYSTEM FOR ROTAX ENGINE TYPE 912 AND 914 (SERIES) SI SI Repeating symbols:

ALERT SERVICE BULLETIN CHECKING OF MAGNETIC PLUG ON ROTAX

Type Acceptance Report

SERVICE BULLETIN. SB No: WE

European Aviation Safety Agency

MANDATORY SERVICE BULLETIN

ENGINE TYPE 912 AND 914 (SERIES) SI R3

European Aviation Safety Agency

AVIAT AIRCRAFT INC. P.O. Box South Washington Afton, WY USA Fax:

Instructions for Continued Airworthiness

AIRWORTHINESS DIRECTIVE

Airworthiness Directive Schedule

Revision Transmittal Sheet

TYPE CERTIFICATE DATA SHEET

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

Airworthiness Directive

TO: HOLDERS OF THE ENGINE FIRE EXTINGUISHER SERVICE BULLETIN , DATED JAN 13/06. REVISION NO. 1, DATED JUN 22/06 HIGHLIGHTS

European Aviation Safety Agency

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

DEPARTMENT OF TRANSPORTATION FEDERAL AVIATION ADMINISTRATION TYPE CERTIFICATE DATA SHEET NO. A49NM

1) Scheduled maintenance checks

SERVICE BULLETIN MANDATORY REPLACEMENT OF THE PROPELLER GEARBOX FOR SOME ROTAX ENGINES TYPE 912/914 (SERIES) SB UL SB UL

SERVICE INFORMATION LETTER Page: 1 of 2

European Aviation Safety Agency

Virus SW 100 Alert Service Bulletin

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

INSTRUCTIONS FOR CONTINUED AIRWORTHINESS FAA-STC SE8987SW. Proposal to Increase Lycoming O-320-E2A Engine Power Rating from 150 hp to 160 hp

Airworthiness Directives - Airframe (Page 1 of 1) Manufacturer: Piper

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

DEPARTMENT OF TRANSPORTATION

INSPECTION FOR CORRECT VENTING OF THE OIL SYSTEM FOR ROTAX ENGINE TYPE 912 AND 914 (SERIES) SB R1 SB R1 MANDATORY

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

European Aviation Safety Agency

Airworthiness Directive

HARTZELL PROPELLER INC.

TYPE CERTIFICATE DATA SHEET

RECOMMENDED. All KANNAD ELTs. Check of hook and loop fasteners for mounting mechanisms

201F Fuel Pump Valve Housing Cap Screw Replacement

SERVICE BULLETIN REVISION

Airworthiness Directive Schedule

SERVICE INSTRUCTION. Lycoming engines that meet defined criteria herein. REASON FOR REVISION: Added IO-360-N and IO-390-C engine models

AIRCRAFT ENGINES SERVICE BULLETIN INSPECTION OR REPLACEMENT OF THE ROCKER ARMS AND VALVE PUSH-RODS FOR ROTAX

SERVICE INSTRUCTION. ISSUED REVISED PAGE NO. REVISION MO DAY YEAR MO DAY YEAR 1 of 8 BB

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

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

SERVICE FUEL WARNING PLACARD AND POH INSPECTION

BULLETIN INDEX LOCATOR

SERVICE INSTRUCTION. Optimizing of mixture distribution SI Repeating symbols: 1) Planning information. 1.1) Engines affected

European Aviation Safety Agency

European Aviation Safety Agency

P.O. Box 3149 Albany, GA Phone (229) Fax (229) March 7, 2006 FLAP CONTROL TORQUE SHAFT REPLACEMENT

PRATT AND WHITNEY CANADA CORP.

HARTZELL PROPELLER INC.

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

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

AP68TP VARIANTS. SERVICE BULLETIN No. TP-14 Rev. 3

Transcription:

Time Between Overhaul Periods () - 33580M 1. PLANNING INFORMATION A. Effectivity Owners and Operators of Aircraft Using Woodward Propeller s, Pumps, Auto Feather Valves, and Speed Signal Generators. Aircraft Service Facilities and Certificated Repair Stations. Airframe Manufacturers. B. Concurrent Requirements None. C. Reason To provide Recommended Time Between Overhaul Periods () for Woodward Propeller s, Pumps, Auto Feather Valves, and Speed Signal Generators. D. Description Wear rates of governor assemblies and accessories will vary with operating conditions. The listed s are based on the following assumptions: 1. Continuous operation with a minimum of 10 hours per month. 2. Engine maintenance performed as specified by the engine and airframe manufacturers. 3. The unit has not been subjected to sudden stoppage, lightning strike, or oil contamination (Overhaul is required at any time the unit is subjected to sudden stoppage, lightning strike, or contaminated oil.). Exceptions to specified : 1. Aircraft engaged in crop dusting or other chemical application flying should reduce the unit to match the percent of reduction in the recommended engine. S/B-33580-M Revision 12: Feb 28/2007 Page 1 of 12

2. The recommended calendar time limit is 6 years for units not in continuous service with a minimum of 120 hours per year. For units in continuous service with a minimum of 120 hours per year, the unit can be operated to the recommended in hours provided the following inspections and conditions are met. A. All Airworthiness Directives, Service Bulletins and Service Letters have been complied with. B. Unit is free from oil leaks. C. Unit has no visible physical damage which would include cracks, corrosion, etc. D. There has been no malfunction in the operation of the unit. E. There has been no 6 month period when the unit was not operated for a minimum of 10 hours. 3. s and accessories listed below might exceed the Woodward recommended Time Between Overhaul () if they are maintained in accordance with an "On Condition" or "Condition Monitored" system approved by the U.S. Federal Aviation Administration or the Canadian Department of Transportation. These federally approved maintenance monitoring methods become an alternate to the manufacturer s recommended Time Between Overhaul. When such governors are returned for servicing on an Investigate and Repair As Necessary (IRAN) basis the customer must specify the Time Since New (TSN) or Time Since Overhaul (TSO). Cooperating with the above approved maintenance methods causes Woodward to "return to service" IRAN governors with accrued hours in excess of Woodward s recommended Time Between Overhaul. E. Compliance Not applicable. F. Approval Technical aspects of this service bulletin are FAA approved. G. Manpower No additional man hours required if accomplished during routine assembly/disassembly. H. Weight and Balance Not affected. S/B-33580-M Revision 12: Feb 28/2007 Page 2 of 12

I. Electrical Load Data Not affected. J. Software Accomplishment Summary Not applicable. K. References None. L. Other Publications Affected None. M. Interchangeability or Intermixability of Parts Not applicable. 2. MATERIAL INFORMATION A. Material - Price and Availability For parts required at overhaul and pricing information please contact: Woodward Aircraft Engine Systems One Woodward Way P.O. Box 405 Rockton, IL 61072-0405 USA Telephone: (815) 624-1819 Facsimile: (815) 624-1926 ----------OR---------- Woodward Aircraft Engine Systems 5 Shawfarm Road Prestwick, Ayrshire KA9 2TR SCOTLAND, UK Telephone: 44-1292-677631 Facsimile: 44-1292-474231 B. Industry Support Information None. S/B-33580-M Revision 12: Feb 28/2007 Page 3 of 12

C. Material Necessary for Each Aircraft/Engine/Component See Material - Price and Availability D. Material Necessary for Each Spare Not applicable. E. Reidentified Parts Not applicable. F. Tooling - Price and Availability Not applicable. 3. RECOMMENDATIONS (1) Recommended Time Between Overhaul () for Woodward Propeller s, Pumps, Auto Feather Valves, and Speed Signal Generators are the same as recommended of engine on which unit is installed except for units listed in the applicable Time Between Overhaul Table. Reciprocating Engine Time Between Overhaul Table 210582 500 Hours 210692 500 Hours 210920 500 Hours 210921 500 Hours Turboprop Primary Time Between Overhaul Table A210765 2000 Hours 210492 3500 Hours 210508 3500 Hours 210527 3500 Hours 210528 3500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 4 of 12

Turboprop Primary Time Between Overhaul Table (Continued) 210537 3500 Hours 210538 3500 Hours 210540 3500 Hours 210541 3500 Hours 210542 3500 Hours 210558 3500 Hours 210560 3500 Hours 210561 3500 Hours 210563 3500 Hours 210564 3500 Hours 210570 3500 Hours 210581 3500 Hours 210600 3500 Hours 210735 3500 Hours 210736 3500 Hours 210737 3500 Hours 210738 3500 Hours 210739 3500 Hours 210741 3500 Hours 210742 3500 Hours 210743 3500 Hours 210744 3500 Hours 210746 3500 Hours 210749 3500 Hours 210939 3500 Hours 210940 3500 Hours 8210-100 3500 Hours 8210-101 3500 Hours 8210-103 2000 Hours 8210-104 3500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 5 of 12

Turboprop Primary Time Between Overhaul Table (Continued) 8210-108 3500 Hours 8210-109 3500 Hours 8210-110 3500 Hours 8210-112 3500 Hours 8210-115 3500 Hours 8210-121 6500 Hours 8210-260 3500 Hours 8210-261 3500 Hours 8210-262 3500 Hours 8210-263 3500 Hours 8210-264 3500 Hours 8210-265 2000 Hours 8210-300 2000 Hours Turboprop Reversing Type Primary Time Between Overhaul Table 210544 3500 Hours 210547 3500 Hours 210549 3500 Hours 210557 3500 Hours 210559 3500 Hours 210566 3500 Hours 210567 3500 Hours 210568 3500 Hours 210569 3500 Hours 210574 4000 Hours 210575 4000 Hours 210576 4000 Hours 210577 3500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 6 of 12

Turboprop Reversing Type Primary Time Between Overhaul Table (Continued) 210578 4000 Hours 210589 4000 Hours 210599 4000 Hours 210935 4000 Hours Except those manufactured or factory remanufactured prior to February 1973-2200 Hours Turboprop Propeller with Pneumatic Overspeed Limiter (Airbleed ) Time Between Overhaul Table 8210-002 4500 Hours 8210-003 4500 Hours 8210-004 4500 Hours 8210-006 4500 Hours 8210-007 4500 Hours 8210-008 2000 Hours 8210-009 2000 Hours 8210-018 2000 Hours 8210-020 2000 Hours 8210-021 2000 Hours 8210-024 4500 Hours 8210-025 4500 Hours 8210-027 4500 Hours 8210-029 4500 Hours 8210-033 2000 Hours 8210-034 4500 Hours 8210-035 4500 Hours 8210-037 4500 Hours 8210-041 ("A" Change or later) 3500 Hours 8210-042 (Prior to "A" change) 2000 Hours 8210-042 ("A" Change or later) 3500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 7 of 12

Turboprop Propeller with Pneumatic Overspeed Limiter (Airbleed ) Time Between Overhaul Table (Continued) 8210-043 ("A" Change or later) 3500 Hours 8210-046 4500 Hours 8210-051 2500 Hours 8210-052 2500 Hours 8210-053 2500 Hours 8210-054 2500 Hours 8210-124 4500 Hours 8210-133 4500 Hours 8210-134 4500 Hours 8210-135 4500 Hours 8210-137 2500 Hours 8210-140 2000 Hours 8210-187 2500 Hours 8210-188 2500 Hours 8210-189 2500 Hours 8210-190 2500 Hours 8210-191 2500 Hours 8210-192 2500 Hours 8210-198 2500 Hours 8210-199 2500 Hours 8210-209 4500 Hours 8210-212 4500 Hours 8210-310 4500 Hours 8210-388 2500 Hours 8210-389 2500 Hours 8210-391 2500 Hours 8210-392 2500 Hours 8210-393 2500 Hours 8210-398 2500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 8 of 12

Turboprop Propeller with Pneumatic Overspeed Limiter (Airbleed ) Time Between Overhaul Table (Continued) 8210-399 2500 Hours 8210-400 2500 Hours 8210-401 2500 Hours 8210-402 2500 Hours 8210-403 2500 Hours 8210-404 2500 Hours 8210-406 2500 Hours 8210-407 2500 Hours 8210-408 2500 Hours 8210-409 2500 Hours 8210-410 2500 Hours 8210-411 2500 Hours Turboprop Overspeed Time Between Overhaul Table 210507 6500 Hours 210509 6500 Hours 210510 6500 Hours 210536 6500 Hours 210588 6500 Hours 210590 6500 Hours 210598 6500 Hours 210610 6500 Hours 210612 6500 Hours 210613 6500 Hours 210614 6500 Hours 210615 6500 Hours 210616 6500 Hours 210618 3500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 9 of 12

Turboprop Overspeed Time Between Overhaul Table (Continued) 210620 6500 Hours 210621 3500 Hours 210622 6500 Hours 210623 6500 Hours 210624 6500 Hours 210625 6500 Hours 210626 6500 Hours 210627 6500 Hours 210628 6500 Hours 210630 6500 Hours 210631 6500 Hours 210632 6500 Hours 210634 6500 Hours 210638 6500 Hours 210639 6500 Hours 210640 6500 Hours 210641 2500 Hours 210642 2500 Hours 210643 6500 Hours 210651 6500 Hours 210941 6500 Hours 210949 6500 Hours 210950 6500 Hours 210951 6500 Hours 210952 6500 Hours 210953 6500 Hours 210954 6500 Hours 210957 6500 Hours 210958 6500 Hours 210960 6500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 10 of 12

Turboprop Overspeed Time Between Overhaul Table (Continued) 210961 6500 Hours 210962 6500 Hours 210963 6500 Hours 8210-011 3000 Hours 8210-013 3000 Hours 8210-060 7500 Hours 8210-061 7500 Hours 8210-063 3000 Hours 8210-068 7500 Hours 8210-085 3000 Hours 8210-091 7500 Hours 8210-093 7500 Hours 8210-150 3000 Hours 8210-151 3000 Hours 8210-152 3000 Hours 8210-153 3000 Hours 8210-160 7500 Hours 8210-161 7500 Hours 8210-162 3000 Hours 8210-163 3000 Hours 8210-164 7500 Hours 8210-167 7500 Hours 8210-168 7500 Hours 8210-172 3000 Hours 8210-251 7500 Hours 8210-290 7500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 11 of 12

Auto Feather Valve Time Between Overhaul Period Table Auto Feather Valve 8905-002 4500 Hours 8905-004 4500 Hours 8905-006 4500 Hours Pump Time Between Overhaul Table Pump 8210-076 3000 Hours 8210-077 1500 Hours 8210-079 3000 Hours 8210-092 7500 Hours 8210-094 7500 Hours 8210-096 7500 Hours 8210-176 3000 Hours 8210-177 1500 Hours 8210-178 3000 Hours 8210-179 3000 Hours 8210-180 3000 Hours 8210-181 7500 Hours 8210-183 7500 Hours 8210-184 7500 Hours 8210-250 7500 Hours 8210-286 7500 Hours 8210-305 3000 Hours 8210-306 3000 Hours 8210-307 3000 Hours 8210-308 7500 Hours 8210-309 7500 Hours S/B-33580-M Revision 12: Feb 28/2007 Page 12 of 12