CIRRUS AIRPLANE MAINTENANCE MANUAL
|
|
- Vanessa Davidson
- 6 years ago
- Views:
Transcription
1 CIRRUS AIRPLANE MAINENANCE MANUAL DISRIUION. DESCRIPION his section describes the maintenance practices of that portion of the ignition system which conducts high-voltage electricity from the magnetos to the spark plugs. Refer to the manufacturer s approved Instructions For Continued Airworthiness. Page
2 CIRRUS AIRPLANE MAINENANCE MANUAL. MAINENANCE PRACICES A. Ignition Harness (See Figure ) () Removal - Ignition Harness (a) Remove engine cowling. (Refer to 7-0) CAUION: o prevent damage to the spark plug insulator and connector, when withdrawing insulator from spark plug, pull the harness lead straight out and at same angle as the barrel. (b) Remove ferrule assembly nuts securing ignition harness leads to spark plugs. (c) Remove clamps and ties securing ignition harness to engine. (d) Remove screws and nuts securing harness cap to magneto. (e) Remove ignition harness from airplane. () Installation - Ignition Harness (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Dow Corning DC Any Source Lubricant and sealant. Note: Prior to installing ignition harness, check mating surfaces for cleanliness. (b) (c) (d) (e) Attach ignition harness to the appropriate magneto. Install washers and screws securing harness cap to magneto. orque screws 8-0 in-lb (.0 -. Nm). Route ignition harness leads to the appropriate spark plug position as indicated by the alphanumeric markings on each spark plug nut. Secure clamps and ties securing ignition harness to engine. CAUION: When tightening spark plug nut, hold ferrule with a 7/ wrench to prevent twisting the ignition lead. (f) Coat insulator with Dow Corning and insert into spark plug. orque spark plug ferrule assembly nut 0-0 in-lb (. -. Nm). Repeat for remaining insulators. (g) Install engine cowling. (Refer to 7-0) Page
3 CIRRUS AIRPLANE MAINENANCE MANUAL. Spark Plugs (See Figure ) () Removal - Spark Plugs (a) Remove engine cowling. (Refer to 7-0) CAUION: o prevent damage to the spark plug insulator and connector, when withdrawing insulator from spark plug, pull the harness lead straight out and at same angle as the barrel. (b) Remove ferrule assembly nut on harness lead and remove insulator from spark plug. (c) Remove spark plug from engine and place in identification tray. (d) Cover spark plug hole to prevent foreign materials from passing into engine. (e) Repeat previous steps for remaining spark plugs. () Installation - Spark Plugs CAUION: Do not install any spark plug that has been dropped or exhibits damage. (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Spark Plug Lubricant and Anti-Seize Compound Champion Spark Plug oledo, OH Lubricant and Anti- Seize. (b) (c) Clean spark plug as required. Set spark plug electrode gap to manufacturer s specified gap. CAUION: Do not apply anti-seize to the first thread of spark plug. Do not allow antiseize compound to contaminate electrodes or insulator. (d) Place new gasket on spark plug. (e) Lubricate spark plug. (f) hread spark plug by hand into cylinder to within one or two threads of the gasket. (g) Install spark plug. (h) orque plug 00-0 in-lb (.8-0. Nm). (i) Repeat previous steps for remaining spark plugs. (j) Install ignition harness leads. (Refer to ) (k) Install engine cowling. (Refer to 7-0) Page 0 Jan 0
4 CIRRUS AIRPLANE MAINENANCE MANUAL LEGEND. Ignition Lead. Nut. Drive Ferrule. Ferrule. Compression Spring. Washer 7. Insulator 8. Electrode Screw 9. Spring 0. Harness Cap. Ignition Harness. Screw SR0_MM7_ Page Figure Ignition System Installation
5 CIRRUS AIRPLANE MAINENANCE MANUAL CYLINDER NUMER CYLINDER NUMER FROM O OP OOM OOM OP OP OOM OOM OP OP OOM OOM OP OP OOM OOM OP OP OOM OOM OP OP OOM OOM OP COA LURICAE UPPER ENGINE FIRING ORDER MAGNEO FIRING ORDER UPPER Damage to insulator at this point LOWER RIGH MAG LEF MAG LOWER CAUION When removing ignition lead from spark plug, pull terminal end straight out of plug, to prevent ceramic insulator damage. SR0_MM7_8A Figure Spark Plug Installation Page
6 CIRRUS AIRPLANE MAINENANCE MANUAL Intentionally Left lank Page
C I R R U S COLLECTOR DESCRIPTION
COLLECTOR 1. DESCRIPTION This section describes the portion of the exhaust system which collects the exhaust gases from the cylinder and conducts them overboard. Included are the exhaust headers and collector
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
POWER CONTROL. DESCRIPTION This section describes those components which furnish a means of controlling engine power. Engine controls for the airplane include the following: control quadrant, throttle
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
AIR INTAKES 1. DESCRIPTION This section describes that portion of the power plant which directs mass air flow to the engine. Induction air enters the engine through a filter mounted on the right, aft side
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
AIR INTAKES 1. DESCRIPTION This section describes that portion of the power plant which directs mass air flow to the engine. Induction air enters the engine through a filter mounted on the left, forward
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
NOISE SUPPRESSOR 1. DESCRIPTION Noise suppression is accomplished through use of a heat exchanger (Serials 0002 thru 019) or a heat exchanger and muffler (Serials 020 & subs) connected to the exhaust header
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
POWER PLANT 1. GENERAL This chapter describes maintenance practices for the airplane systems which provide the means to induce and convert fuel-air mixture into power such as the engine, baffling, cowling,
More informationFlaps System. 1. General
CIRRUS AIRPLANE MAINTENANCE MANUAL Flaps System CHAPTER 27-50: FLAPS SYSTEM GENERAL 27-50: FLAPS SYSTEM 1. General This section describes that portion of the flight control system which controls the position
More information57-20 AUXILIARY STRUCTURE
AUXILIARY STRUCTURE 1. DESCRIPTION The leading edge of the wing is manufactured from composite materials. This airplane has a one-piece wing with individual wing tips. The wing tips are manufactured from
More informationTUBES, HOSES, AND FITTINGS
TUBES, HOSES, AND FITTINGS 1. DESCRIPTION This section contains instructions and specifications for aircraft system plumbing and fittings. Page 1 2. MAINTENANCE PRACTICES A. Ice Protection System Compression
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
AUXILIARY STRUCTURE 1. DESCRIPTION The leading edge of the wing is manufactured from composite materials. This airplane has a one-piece wing with individual wing tips. The wing tips are manufactured from
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 EXTERIOR LIGHTING. DESCRIPTION This section covers that portion of the system which provides illumination outside of the aircraft. This includes the landing light, anti-collision strobe light,
More information53-40 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
More informationC I R R U S HOISTING DESCRIPTION
HOISTING 1. DESCRIPTION This chapter describes those instructions necessary to support the airplane during maintenance and repair. In some instances (i.e. off-runway landing, collapsed gear, etc.) it may
More informationValve Cover - RH Material
1 of 5 5/15/2015 8:06 AM Valve Cover - RH Material 2 of 5 5/15/2015 8:06 AM 3 of 5 5/15/2015 8:06 AM Removal CAUTION: During engine repair procedures, cleanliness is extremely important. Any foreign material,
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
JACKING 1. DESCRIPTION Three jack points, located at each wing tiedown and tail tiedown, are provided to perform maintenance operations. Tie-down rings must be removed and replaced with jack points prior
More informationPropeller Assembly. 1. General
Propeller Assembly GENERAL 61-10: PROPELLER ASSEMBLY 1. General The propeller assembly consists of a hollow aluminum hub which supports the propeller blades and also houses the pitch changing mechanism.
More information33-40 EXTERIOR LIGHTING
EXTERIOR LIGHTING. DESCRIPTION This section covers that portion of the system which provides illumination outside of the aircraft. This includes the landing light, anti-collision strobe light, and recognition
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials 000 thru 00: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
More informationC I R R U S CONTROLLING DESCRIPTION
CONTROLLING 1. DESCRIPTION Serials 22-0002 & subs: An electric two-speed fuel pump provides boost (low speed) and prime (high speed) for the engine. A console mounted rocker switch located on the center
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
INDICATING 1. DESCRIPTION This section describes that portion of the oil system which is used to indicate the quantity, temperature, and pressure of the oil. Components included are the oil filler cap/dipstick,
More informationSNS SUBJECT: RADOME IPS FLUID SYSTEM - Radome IPS Routing
CIRRUS SF5X Service Bulletin Number: Issued: SNS SUBJECT: 0-50 - RADOME IPS FLUID SYSTEM - Radome IPS Routing. COMPLIANCE Mandatory: Cirrus considers this Service Bulletin to be MANDATORY. Accomplish this
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ELEVATOR AND PITCH TRIM SYSTEM 1. DESCRIPTION This section describes that portion of the flight control system which controls the position and movement of the elevator. Included are; elevator system torque
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
SPECIAL PURPOSE EQUIPMENT 1. GENERAL This section describes special purpose equipment on the airplane. This equipment includes the Cirrus Airplane Parachute System (CAPS) and the aft tiedown ballast bracket.
More informationSPECIAL PURPOSE EQUIPMENT
All SPECIAL PURPOSE EQUIPMENT 1. GENERAL This section describes special purpose equipment on the airplane. This equipment includes the Cirrus Airplane Parachute System (CAPS) the aft tiedown ballast bracket,
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 YAW CONTROL AND TRIM. GENERAL This section describes that portion of the flight control system which controls the position and movement of the rudder. Included are; rudder system rigging, rudder
More informationCOMPONENT LOCATION INDEX
COMPONENT LOCATION INDEX 2011-12 ENGINE Ignition System - Odyssey Fig. 1: Identifying Ignition System Replacement Components IGNITION TIMING INSPECTION 1. Connect the HDS to the DLC (see step 2 on HOW
More informationYaw Control and Trim. 1. General. A. Yaw Control System. B. Yaw Trim System
CIRRUS AIRPLANE MAINTENANCE MANUAL MODELS SR AND SRT Yaw Control and Trim CHAPTER 7-0: YAW CONTROL AND TRIM GENERAL 7-0: YAW CONTROL AND TRIM. General This section describes that portion of the flight
More informationDC Generation. 1. General. A. DC Generation
CIRRUS AIRPLANE MAINTENANCE MANUAL DC Generation CHAPTER -0: DC GENERATION GENERAL -0: DC GENERATION 1. General (See Figure -0-1) This section covers the systems to generate, regulate, control, and indicate
More informationC I R R U S DISTRIBUTION DESCRIPTION
MODELS SR AND SRT DISTRIBUTION. DESCRIPTION This section contains information on the distribution system. The fuel distribution system consists of electric and mechanical (engine-driven) fuel pumps, fuel
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
PASSENGER COMPARTMENT 1. DESCRIPTION This section covers the passenger compartment lighting. A. Passenger Eyeball Lights Individual eyeball-type reading lights are installed in the headliner above each
More informationWHEELS 1. DESCRIPTION A.
WHEELS 1. DESCRIPTION A. Main Wheels Serials 22-0002 thru 22-4045 before SB2X-32-21, 22T-0001 thru 22T-0689 before SB2X-32-21: The main wheels are of aluminum construction and designed to be used with
More informationFLIGHT SIMULATOR SYSTEMS
FLIGHT SIMULATOR SYSTEMS 1. GENERAL This section describes systems required for simulator operation. This equipment includes the Cirrus Landing Gear Simulator (CLGS). 2. DESCRIPTION The intent of the CLGS
More informationM14 AUTOMOTIVE SPARK PLUGS AND WIRES CONVERSION KIT INSTALLATION INSTRUCTIONS
M14 AUTOMOTIVE SPARK PLUGS AND WIRES CONVERSION KIT INSTALLATION INSTRUCTIONS (It is highly recommended you read the instructions completely before beginning) 1. Be sure the magneto switches are turned
More information33-10 FLIGHT COMPARTMENT
FLIGHT COMPARTMENT. DESCRIPTION Flight compartment interior lighting consists of instrument lights, glareshield flood lights, overhead dome light, individual reading lights, pilot control lights, CAPS
More informationPASSENGER AND CREW DOORS
MODELS SR AND SRT PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials -000 thru -00: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
More information2/13/2018 Engine 3.0L (4V) - Valve Cover RH - in Vehicle Repair 2006 Lincoln Zephyr MotoLogic
2006 Zephyr Applies to: 3.0L (4V) Report a problem with this article SECTION 303-01B: Engine 3.0L (4V) 2006 Fusion/Milan/Zephyr Workshop Manual IN-VEHICLE REPAIR Procedure revision date: 07/24/2006 Valve
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 All PASSENGER AND CREW DOORS. DESCRIPTION AND OPERATION Serials 005 thru 4: The two crew/passenger doors incorporate a flush-mount outside door handle, key-operated door lock, and a conventional
More informationIntake Manifold Removal (Upper)
Intake Manifold Removal (Upper) Disconnect the vacuum lines from the upper intake manifold. Disconnect the MAP sensor electrical connector. Remove the MAP sensor screws. Remove the MAP sensor. Remove the
More informationFlight Compartment. 1. General
CIRRUS AIRPLANE MAINTENANCE MANUAL Flight Compartment CHAPTER 56-10: FLIGHT COMPARTMENT GENERAL 56-10: FLIGHT COMPARTMENT 1. General The windshield is manufactured of acrylic and is adhesive bonded to
More informationA. Stall Warning System - Serials w/o Ice Protection
Stall Warning System GENERAL 27-31: STALL WARNING SYSTEM 1. General A. Stall Warning System - Serials w/o Ice Protection The airplane uses an electro-pneumatic stall warning system. As the angle of attack
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
PROPELLER 1. GENERAL The airplane employs a 3 blade, constant speed, non-feathering propeller. The blades (composite or aluminum) are mounted in an aluminum hub which contains the pitch changing mechanism
More informationFastener Identification And Torque Data
CIRRUS AIRPLANE MAINTENANCE MANUAL CHAPTER 20-60: FASTENER IDENTIFICATION AND TORQUE DATA GENERAL Fastener Identification And Data 20-60: FASTENER IDENTIFICATION AND TORQUE DATA 1. General This section
More informationBRACKETT AERO FILTERS, INC.
BRACKETT AERO FILTERS, INC. INSTRUCTIONS ASSEMBLY PART NO. BA-8110 FAA APPROVAL DATA: STC-SA71GL LIST NO. 1 FAA-PMA Supplement No. 1 REPLACES FILTER PART NUMBERS: 0750038-1, -4 0750127-12, -14 0750146-1
More informationC I R R U S COWLING DESCRIPTION
COWLING 1. DESCRIPTION Serials 22-0002 thru 22-019, 22-0821 thru 22-711: The engine cowling, fabricated from fiberglass and epoxy, consists of one upper and two lower halves. A one-piece (22-0002 thru
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
STORAGE 1. DESCRIPTION A. Fuel Storage System - Serials 1005 thru 1885 The fuel storage system consists primarily of a vented integral 30.3-gallon (114.5-liters) capacity fuel tank in each wing, a fuel
More informationAVIATION SCIENCE LESSON 5: SPARK PLUGS
AVIATION SCIENCE LESSON 5: SPARK PLUGS Teacher: Subject: Grades: Subjects: Paul Ladegard, Alan Dick Aviation Science Secondary Technology, Science Learning Objectives: Students can locate the sparkplugs
More information1) Scheduled maintenance checks
1) Scheduled maintenance checks Definition This section lists the periodic inspections which must be carried out after a specified periods of operation. Intervals Periodic inspections are those which must
More informationService 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.
More informationKEITH WALKING FLOOR RUNNING FLOOR II Drive Repair Instructions
Load-Unload Control Valve Handle Assembly Handle Assembly Switching Valve LOAD END DISCHARGE END Adapter Block Ball Valve Cylinder #1 Cylinder #2 Check Valve #1 Check Valve #2 Adapter Block Cylinder #3
More informationRIGHT HYDRAULIC PUMP. Right Hydraulic Pump Replacement. Right Hydraulic Pump Removal. 5. Remove the pump belt from around the pump pulleys (Fig. 002).
Right Hydraulic Pump Replacement Note: Cleanliness is a key factor in a successful repair of any hydraulic system. Thoroughly clean all exposed surfaces prior to any type of maintenance. Cleaning all parts
More informationCabin. 1. General. A. Cabin Seats
CIRRUS AIRPLANE MAINTENANCE MANUAL Cabin CHAPTER 25-10: CABIN GENERAL 25-10: CABIN 1. General This section covers cabin compartment seats, seat harnesses, trim, cabin headliner, floor covering, sunvisors,
More informationIN-VEHICLE REPAIR. Upper Intake Manifold
303-01-1 Engine 3.9L and 4.2L 303-01-1 IN-VEHICLE REPAIR Upper Intake Manifold Special Tool(s) Remover, Spark Plug Wire 303-106 (T74P-6666-A) Material Item Silicone Brake Caliper Grease and Dielectric
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
AERODYNAMIC FAIRINGS 1. DESCRIPTION This section describes those components which make up the aerodynamic fairings. A fixed, composite wing root fairing is installed around the wing root, enclosing the
More informationSTALL WARNING SYSTEM 1. DESCRIPTION A.
STALL WARNING SYSTEM 1. DESCRIPTION A. Stall Warning System - Serials w/o Perspective Avionics The airplane uses an electro-pneumatic stall warning system. As the angle of attack increases and the airplane
More informationPISTON PREHEAT SYSTEM ILLUSTRATED INSTALLATION INSTRUCTIONS
Illustrated Installation Piston Preheat System Rev.100113RCK ENGINE MAKE: Rotax MODEL: 912/914 PISTON PREHEAT SYSTEM ILLUSTRATED INSTALLATION INSTRUCTIONS Page 1 of 6 Piston Preheat System Table of Contents
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ANALYZERS - ENGINE MONITORING. DESCRIPTION This section describes that portion of the engine indicating system which is used to analyze engine performance, temperature, and condition. Serials 00 thru 8
More informationHYDRAULICS. TX420 & & lower. Hydraulic Tandem Pump Removal. 4. Remove the LH side panel (Fig. 0388).
TX420 & 425 240000299 & lower 4. Remove the LH side panel (Fig. 0388). Hydraulic Tandem Pump Removal Note: Cleanliness is a key factor in a successful repair of any hydraulic system. Thoroughly clean all
More informationLEFT HYDRAULIC PUMP. Left Hydraulic Pump Replacement. Left Hydraulic Pump Removal. 5. Remove the pump belt from around the pump pulleys (Fig. 002).
Left Hydraulic Pump Replacement Note: Cleanliness is a key factor in a successful repair of any hydraulic system. Thoroughly clean all exposed surfaces prior to any type of maintenance. Cleaning all parts
More informationCatalytic Converter: Service and Repair
2007 GMC Truck Envoy 4WD V8-5.3L Copyright 2009, ALLDATA 10.10 Page 1 Catalytic Converter: Service and Repair Catalytic Converter Replacement (5.3L and 6.0L Engines) Removal Procedure 1. Raise and suitably
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
SYSTEM 55 AUTOPILOT 1. DESCRIPTION The S-TEC System 55 is a dual axis autopilot system that provides roll stability, heading hold, NAV/GPS tracking, altitude hold, vertical speed selection, automatic glideslope
More informationIllustration Install plug (11) in the fuel manifold. EndBy: g SMCS Code: Table 5. Tool A (1)
12 Illustration 22 g00511936 Illustration 21 (12) Electronic injector code g00529729 9. Install plug (11) in the fuel manifold. EndBy: a. Install the rocker shaft and the pushrods. Refer to Disassembly
More informationBOTTOM END SERVICE TOOLS SERVICE PRODUCTS ENGINE, CVT AND GEARBOX Subsection 10 (BOTTOM END)
BOTTOM END SERVICE TOOLS Description Part Number Page CRANKCASE SUPPORT MAG/PTO... 529 036 031... 151 CRANKSHAFT LOCKING BOLT... 529 035 617... 154 DRIVE SHAFT OIL SEAL INSTALLER... 529 036 028... 143
More informationCIRRUS AIRPLANE MAINTENANCE MANUAL
ELECTRICAL LOAD DISTRIBUTION. DESCRIPTION The power distribution system for this airplane consists of the main distribution bus and the essential distribution bus in the MCU along with the associated buses
More informationPitch Control and Trim
Pitch Control and Trim GENERAL 27-30: PITCH CONTROL AND TRIM. General This section describes that portion of the flight control system which controls the position and movement of the elevator. This includes
More informationC I R R U S CABIN 1. DESCRIPTION A. Cabin Seats B. Radio Module Assembly
CABIN. DESCRIPTION This section covers cabin compartment seats, seat harnesses, trim, cabin headliner, floor covering, sunvisors, grab handles, headset hooks, coat hooks, drink holders, storage pockets,
More informationEngine. Special Tool(s) Compressor, Piston Ring 303-D032 (D81L-6002-C) or equivalent. Compressor, Valve Spring (T93P-6565-AR)
SECTION 303-01C: Engine 5.4L (4V) 2009 Mustang Workshop Manual ASSEMBLY Procedure revision date: 12/12/2008 Engine Special Tool(s) Compressor, Piston Ring 303-D032 (D81L-6002-C) or equivalent Compressor,
More informationAssembly & Installa on Guide RB031-3: TRIPLE CROSSBAR KIT
PLEASE READ INSTRUCTIONS FULLY PRIOR TO INSTALLATION OF CROSSBAR KIT This instruction is to illustrate the recommended installation method for our Crossbar Kit, any deviation from this will be the sole
More informationTech Feature: Brake Job on Ford Edge
Tech Topics Tech Feature: Brake Job on Ford Edge By Andrew Markel email Editor, Brake & Front End Magazine August 20, 2010 The Ford Edge is an SUV based on a the CD3 platform. The brakes on these vehicles
More informationPage 1 of 75 303-01D Engine - 5.2L 32V Ti-VCT 2016 Mustang Assembly Procedure revision date: 12/15/2016 Special Tool(s) / General Equipment Engine Base Part Number: 6L084 205-142 (T80T-4000-J) Installer,
More informationFig. 1: Remove the bolts which fasten the upper timing belt cover... Fig. 2:... and remove the cover
Show Timing Belt and Covers REMOVAL & INSTALLATION 1983 87 626 NOTE: For access, safely support the car, then remove the right front wheel and splash shield. 1. Loosen the alternator mounting bolts and
More informationLower Intake Manifold Replacement
Lower Intake Manifold Replacement Removal Procedure 1. Turn OFF all the lamps and the accessories. 2. Ensure the ignition switch is in the OFF position. 3. Disconnect the negative battery cable from the
More information(8) Perform negative-pressure check IAW paragraph (9) Install mask-mounted regulator in regulator holder.
(8) Perform negative-pressure check IAW paragraph 6.6.3. (9) Install mask-mounted regulator in regulator holder. 6.7.3.2 Mask-Mounted Regulator Removal and Installation. O-ring, PN 18002-00 Pliers, slip
More information2003 Nissan-Datsun Truck Frontier 4WD V6-3.3L (VG33E)
1 of 15 8/7/2016 2:34 PM 2003 Nissan-Datsun Truck Frontier 4WD V6-3.3L (VG33E) Vehicle» Engine, Cooling and Exhaust» Engine» Cylinder Head Assembly» Service and Repair» Removal and Installation 2 of 15
More informationAKRAPOVIC RACING & EVOLUTION EXHAUST SYSTEM for the BMW K1300R/S (2009)
Installation instructions: *502145* AKRAPOVIC RACING & EVOLUTION EXHAUST SYSTEM for the BMW K1300R/S (2009) Congratulations on purchasing an Akrapovic exhaust system. Please read these installation instructions
More informationCIRRUS SR2X SB 2X R2. Service Bulletin. Issued: Revised: June 26, 2012 July 31, 2012
CIRRUS SR2X Service Bulletin Number: Issued: Revised: June 26, 2012 SNS SUBJECT: 57-40 ATTACH FITTINGS - Lower Landing Gear Attach Bracket Torque 1. COMPLIANCE Mandatory: Cirrus Design considers this Service
More informationPassenger And Crew Door
CIRRUS AIRPLANE MAINTENANCE MANUAL Passenger And Crew Door CHAPTER 5-10: PASSENGER AND CREW DOOR GENERAL 5-10: PASSENGER AND CREW DOOR 1. General The two crew/passenger doors incorporate a flush-mount
More informationTECHNICAL INSTRUCTIONS FOR SAFETY RECALL ALE VALVE SPRING AND LASH ADJUSTER REPLACEMENT GS 350: IS 350:
TECHNICAL INSTRUCTIONS FOR SAFETY RECALL ALE VALVE SPRING AND LASH ADJUSTER REPLACEMENT GS 350: 2007 2008 IS 350: 2006 2008 I. OPERATION FLOWCHART Verify Vehicle Eligibility 1. Check the VIN range. 2.
More informationSDS Continental IO-550 Installation Manual
SDS Continental IO-550 Installation Manual July14/18 This manual covers the steps to install the SDS EM-5 fuel injection and ignition system components on IO-550 engines. Checking Clearance for Hall Sensor
More informationKit Instruction (Meter Body Replacement Parts)
XYR 6000 Pressure Transmitter Models STDW924, STDW930, STDW974, STGW944, STGW974, STGW94L, STGW97L, STGW98L, STAW94L ST 3000 Smart Pressure Transmitter Models (Revision S or later) STD110, STD120, STD125,
More information97-04 CHEVROLET CORVETTE C5
97-04 CHEVROLET CORVETTE C5 IMPORTANT! WARRANTY AND INSTALLATION INSTRUCTIONS Please Forward All Information to Consumer Be sure to review the enclosed instructions prior to beginning the installation
More informationCAMSHAFT TIMING CHAIN, SPROCKET, AND TENSIONER REPLACEMENT
Page 1 of 45 CAMSHAFT TIMING CHAIN, SPROCKET, AND TENSIONER REPLACEMENT Special Tools J 45027 Tensioner Tool J 45059 Angle Meter Page 2 of 45 Removal Procedure Page 3 of 45 Page 4 of 45 Page 5 of 45 Fig.
More informationGEARBOX AND 4X4 COUPLING UNIT SERVICE TOOLS SERVICE TOOLS OTHER SUPPLIER SERVICE PRODUCTS
GEARBOX AND 4X4 COUPLING UNIT SERVICE TOOLS Description Part Number Page BLIND HOLE BEARING PULLER SET... 529 036 117... 199 COUNTERSHAFT OIL SEAL PUSHER... 529 036 222... 192 ECM ADAPTER TOOL... 529 036
More informationThread pitch can be 5/8-24 or 3/4-20
652 Oliver Street Williamsport, PA. 17701 U.S.A. Telephone +1 (800) 258-3279 U.S. and Canada (Toll Free) Telephone +1 (570) 323-6181 (Direct) Facsimile +1 (570) 327-7101 Email Technicalsupport@lycoming.com
More informationUNIVERSAL PUMP HANGER INSTALLATION INSTRUCTIONS
UNIVERSAL PUMP HANGER INSTALLATION INSTRUCTIONS WARNING! THESE INSTRUCTIONS MUST BE READ AND FULLY UNDERSTOOD BEFORE BEGINNING INSTALLATION. FAILURE TO FOLLOW THESE INSTRUCTIONS MAY RESULT IN POOR PERFORMANCE,
More informationEngine Cylinder Head Installation
Engine Cylinder Head Installation Important: Install the cylinder head without the camshafts. 1. Install the engine cylinder head to the engine block. 2. Install the AIR pump bolt and fir tree fastener
More informationPower Flow System Extractor Exhaust System Instructions for Continued Airworthiness PFS-13201
REVISION CONTROL REVISION DATE REMOVE PAGES INSERT PAGES IR 09/12/01 N/A N/A A 10/05/01 ALL ALL B 02/26/02 1-3,5,6,8,10 1-3,5,6,8,10 C 08/30/02 1-5,7,10 1-5,7,10 D 01/15/03 ALL ALL E 7/2/04 1,4,5 1,4,5
More informationOn all settings above 100 horsepower the following precautions should be observed:
ELECTRONIC FUEL INJECTED 5.0 COYOTE PLATE SYSTEM INSTALLATION INSTRUCTIONS Congratulations on the purchase of your Nitrous Express Coyote Plate system. Nitrous Express utilizes only the highest quality
More informationINSTRUCTION. Internal pump elements APP6.5 - special 180B R R9134
INSTRUCTION Internal pump elements APP6.5 - special 180B3101 180R9134 This document covers the instructions for changing internal pump elements on the axial piston pumps APP6.5. Note: It is essential that
More informationTOYOTA TACOMA LED DRL. Part Number: TTA-712
Part Number: TTA-712 Kit Contents Item # Quantity Reqd. Description 1 2 DRL s bezels w/led DRL 2 1 Driver Box 3 1 Harness bag 4 1 User s card 5 1 Switch Hardware Bag Contents Item # Quantity Reqd. Description
More informationStorage. 1. General. A. Fuel Storage System
CIRRUS AIRPLANE MAINTENANCE MANUAL Storage CHAPTER 28-10: STORAGE GENERAL 28-10: STORAGE 1. General A. Fuel Storage System The fuel storage system consists primarily of a vented integral 47.5-gallon (180-liters)
More informationDucati Monster Ducati Monster 796 (Euro Spec Only) Z-Fi QS Installation Instructions P/N S192S, S192R
2009-2011 Ducati Monster 696 2010-2012 Ducati Monster 796 (Euro Spec Only) Z-Fi QS Installation Instructions P/N S192S, S192R WARNING! USE ONLY IN RACE OR OTHER CLOSED COURSE APPLICATIONS AND NEVER ON
More informationNot for Reproduction ADVANCE PRODUCT SERVICE INFORMATION APSI NO: 101 DATE: AUGUST SERIES UTILITY ENGINE 130G00 OHV HORIZONTAL SHAFT
ADVANCE PRODUCT SERVICE INFORMATION APSI NO: 101 DATE: AUGUST 2014 SUBJECT: MODELS: 950 SERIES UTILITY ENGINE 130G00 OHV HORIZONTAL SHAFT This APSI provides basic servicing information in advance of the
More informationPart Number: STC-501. Hardware Bag Contents. General Applicability. Conflicts. Date: SCION tc LED DRL in FOG LIGHT HOUSING
Date: 09.30.2013 SCION tc 2011-2013 LED DRL in FOG LIGHT HOUSING Part Number: STC-501 Kit Contents Item # Quantity Reqd. Description 1 2 LED DRL housings 2 2 Bezels 3 1 Driver Box 4 1 Harness bag 5 1 User
More informationSID SERVICE INFORMATION DIRECTIVE Compliance Will Enhance Safety, Maintenance or Economy of Operation TELEDYNE CONTINENTAL AIRCRAFT ENGINE
TELEDYNE CONTINENTAL AIRCRAFT ENGINE SERVICE INFORMATION DIRECTIVE Compliance Will Enhance Safety, Maintenance or Economy of Operation CATEGORY 4 Technical Portions FAA Approved SUBJECT: PURPOSE: COMPLIANCE:
More informationON-VEHICLE INSPECTION
ON-VEHICLE INSPECTION 1. CHECK IGNITION COIL ASSEMBLY AND PERFORM SPARK TEST (a) Check for DTCs. NOTICE: If any DTC is present, perform troubleshooting in accordance with the procedure for that DTC. (b)
More informationSNS SUBJECT: NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement
CIRRUS SR22 Service Bulletin Number: Issued: SNS SUBJECT: 32-20 NOSE GEAR - Nose Landing Gear Assembly Inspection and Reinforcement 1. COMPLIANCE Mandatory: Cirrus Design considers this Service Bulletin
More informationOwner smanual. PowerPack System Stinger System & Later GM 8.1L Class-A W-24 Chassis Motorhomes. with Installation Instructions
Owner smanual with Installation Instructions PowerPack System Stinger System 2005 & Later GM 8.1L Class-A W-24 Chassis Motorhomes THIS MANUAL IS FOR USE WITH SYSTEMS 49548, 49562, 49563, 49579 & 49580
More informationBMK-18 U.S. Patent #5,298,158
BMK- U.S. Patent #5,29,5 Marine Dual Remote Filtration System Mounting Kit Installation and Servicing Instructions IMPORTANT NOTICE Read all instructions completely before attempting to install this unit.
More information2012 Kia Soul L4 2.0L
2012 Kia Soul L4 2.0L Vehicle» Engine, Cooling and Exhaust» Engine» Timing Chain» Service and Repair» Repair Procedures» Part 2 Installation 1. The TDC marks of the intake and exhaust CVVT sprockets are
More informationELECTRICAL SYSTEMS. Table of Contents. Section 4B - Thunderbolt V Ignition System
SERVICE MANUAL NUMBER 25 Table of Contents ELECTRICAL SYSTEMS Section 4B - Thunderbolt V Ignition System THUNDERBOLT V IGNITION SYSTEM Replacement Parts Warning.......... 4B-2 General Precautions.................
More information