57-20 AUXILIARY STRUCTURE
|
|
|
- Hilary Charles
- 5 years ago
- Views:
Transcription
1 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 composite materials. Each strobe light power supply is secured inside the corresponding wing tip. Stall strips are installed along the inboard leading edge of wing cuffs on both wings and promote a more gradual stall, prolonging aileron effectivity under stall conditions. Serials & subs, 22T-0001 & subs: A white recognition light is installed on the leading edge of each wing tip. All Page 1
2 2. MAINTENANCE PRACTICES A. Wing Tip - Serials thru (See Figure 1) (1) Removal - Wing Tip (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull NAV LIGHTS and STROBE LIGHTS circuit breakers. Note: Place a pad between wing tip and top of wing to avoid damaging paint. (c) Remove screws securing wing tip to wing and slide wing tip outboard to remove. Carefully flip wing tip upside down and rest wing tip on top of wing. (d) Remove clamp securing braided ground strap to wing wire harness conduit. (e) Disconnect wire harnesses. 1 Remove cable ties securing braided ground strap to wing wire harness. 2 Disconnect navigation light connector. 3 Disconnect power connector from strobe light power supply. 4 Serials thru : Remove strobe light power supply mounting screw securing wire harness terminal rings. 5 Serials thru : Disconnect terminal ring connector and remove cable tie securing wires together. (f) Remove wing tip from airplane. (2) Installation - Wing Tip (a) Connect wire harnesses. 1 Connect power connector to strobe light power supply. 2 Serials thru : Position terminal ring between strobe light power supply and shear web and secure with screw. 3 Serials thru : Connect terminal ring connector and install cable tie securing wires together. 4 Connect navigation light connector. (b) Wrap braided ground cable around wire harness and secure with cable ties. (c) Burnish wing conduit to ensure proper contact between braided ground strap and conduit. (d) Position braided ground strap to wing conduit and secure with clamp. (e) Verify resistance from anti-collision strobe light assembly to airplane ground is less than 4 ohms. If resistance is greater than 4 ohms, remove braided ground strap and repeat conduit burnishing. (f) Position wing tip to wing and ensure wing tip shear pin fully engages receiving hole on wing. (g) Install screws securing wing tip to wing. (h) Reset NAV LIGHTS and STROBE LIGHTS circuit breakers. (i) Verify proper anti-collision strobe light operation. Page 2 Serials thru
3 B. Wing Tip - Serials & subs, 22T-0001 & subs (See Figure 1) (1) Removal - Wing Tip (a) Set BAT 1, BAT 2, and AVIONICS switches to OFF positions. (b) Pull NAV LIGHTS and STROBE LIGHTS circuit breakers. Note: Place a pad between wing tip and top of wing to avoid damaging paint. (c) Remove screws securing wing tip to wing and slide wing tip outboard to remove. Carefully flip wing tip upside down and rest wing tip on top of wing. (d) Disconnect wire harnesses. 1 Disconnect recognition light connector. 2 Disconnect navigation light connector. 3 Disconnect power connector from strobe light power supply. 4 Disconnect terminal ring connector and remove cable tie securing wires together. (e) Remove wing tip from airplane. (2) Installation - Wing Tip (a) Connect wire harnesses. 1 Connect power connector to strobe light power supply. 2 Connect terminal ring connector and install cable tie securing wires together. 3 Connect navigation light connector. 4 Connect recognition light connector. (b) Position wing tip to wing and ensure wing tip fully engages mounting clips on wing. (c) Install screws securing wing tip to wing. (d) Reset NAV LIGHTS and STROBE LIGHTS circuit breakers. (e) Verify proper anti-collision strobe light operation. (f) Verify proper recognition light operation. Serials & subs, 22T-0001 & subs Page 3
4 5 7 8 Serials thru ANTI-COLLISION STROBE LIGHT (REF) 1 Serials thru , thru , thru LEGEND 1. Wing Tip 2. Screw 3. Shear Pin 4. Navigation Light Connector 5. Braided Ground Cable 6. Cable Tie 7. Strobe Light Power Connector 8. Terminal Ring 9. Clamp 10. Terminal Ring Connector SR22_MM57_1669C Page 4 Figure 1 Wing Tip Installation - Serials thru (Sheet 1 of 2) Serials thru
5 ANTI-COLLISION STROBE LIGHT (REF) LEGEND 1. Wing Tip 2. Screw 4. Navigation Light Connector 5. Braided Ground Cable 7. Strobe Light Power Connector 9. Clamp 10. Terminal Ring Connector 11. Recognition Light Connector SR22_MM57_2449A Figure 1 Wing Tip Installation - Serials & subs, 22T-0001 & subs (Sheet 2 of 2) Serials & subs, 22T-0001 & subs Page 5 31 May 2011
6 C. Stall Strips - Serials thru (See Figure 2) WARNING: Airplane is rendered unairworthy and may not be flown with stall strip(s) removed. (1) Removal - Stall Strips (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Blunt-Edged Chisel - Any Source Stall strip removal. Sandpaper 400-grit Any Source Adhesive removal. Isopropyl Alcohol - Any Source Solvent cleaning. (b) Using chisel, remove stall strips from wing. (c) Lightly sand wing to remove residual adhesive. (d) Solvent clean wing surface with isopropyl alcohol. (2) Installation - Stall Strips CAUTION: When reinstalling a stall strip that has become dislodged from wing leading edge, if exact location of previously installed stall strip is not apparent, i.e. through the lack of adhesive remnant or discoloration in area of previous installation location, install the stall strip in accordance with the following steps and contact Cirrus Design to schedule a maintenance check flight by a Cirrus certified test pilot. If location of previously installed stall strip is readily apparent, install the stall strip in same location in accordance with the following steps. No maintenance check flight is required. (a) Acquire necessary tools, equipment, and supplies. Description P/N or Spec. Supplier Purpose Isopropyl Alcohol - Any Source Solvent cleaning. 5-Minute Epoxy Devcon Danvers,MA Bonding stall strip to wing. Mounting Fixtures: LH Outboard RH Outboard RH Inboard LH Inboard T-1087 T1088 T1089 T1090 Cirrus Design Stall strip installation. (b) (c) Solvent clean bonding surfaces of wing and stall strip. If exact location of previously installed stall strip is not readily apparent: 1 Apply adhesive to back of outboard stall strip. CAUTION: Ensure gap between stall strip and wing cuff does not exceed 0.05 inch (1.27 mm). Page 6 Serials thru
7 (d) (e) (f) (g) (h) (i) 2 Position outboard stall strip adjacent to wing cuff. Verify gap between stall strip and wing cuff does not exceed 0.05 inch (1.27 mm) and press firmly into place. 3 Using mounting fixture, clamp outboard stall strip against wing. 4 Apply adhesive to back of inboard stall strip. 5 Position outboard end of inboard stall strip 56.5 inches (143.5 cm) from wing cuff. 6 Using mounting fixture, clamp inboard stall strip against wing. If exact location of previously installed stall strip is readily apparent: 1 Apply adhesive to back of outboard stall strip. 2 Position outboard stall strip over previous installation area and press firmly into place. 3 Using mounting fixture, clamp outboard stall strip against wing. 4 Apply adhesive to back of inboard stall strip. 5 Position inboard stall strip over previous installation area and press firmly into place. 6 Using mounting fixture, clamp inboard stall strip against wing. Fill stall strip ends flush with adhesive. Wipe excess adhesive from edge of stall strips. Allow adhesive to cure. Remove mounting fixtures. If necessary, ensure maintenance check flight is performed by a Cirrus Design authorized test pilot before return to service. Serials thru Page 7
8 D. Stall Strips - Serials & subs, 22T-0001 & subs WARNING: Airplane is rendered unairworthy and may not be flown with stall strip(s) removed. (1) Removal - Stall Strips (a) Contact Cirrus Design for disposition. (2) Installation - Stall Strips (a) Contact Cirrus Design for disposition. Page 8 19 Sep 2017 Serials & subs, 22T-0001 & subs
9 2.05 inch (1.27 mm) inch (143.5 cm) Maximum 1 NOTE Fill stall strip ends flush with adhesive. Serials thru , thru , thru LEGEND 1. Stall Strip 2. Mounting Fixture SR22_MM57_1571A Serials thru Figure 2 Stall Strip Installation - Serials thru Page 9 19 Sep 2017
10 Intentionally Left Blank Page Sep 2018 Serials & subs, 22T-0001 & subs
CIRRUS 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
33-40 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
CIRRUS 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,
CIRRUS 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
33-10 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
Flaps 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
CIRRUS 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
57-50 FLIGHT SURFACES
FLIGHT SURFACES 1. DESCRIPTION The flaps are mounted to the trailing edge of each wing between the inboard end of the ailerons and the fuselage. The ailerons are located near the wing tips and hinge to
CIRRUS AIRPLANE MAINTENANCE MANUAL
FLIGHT SURFACES. DESCRIPTION The flaps are mounted to the trailing edge of each wing between the inboard end of the ailerons and the fuselage. The ailerons are located near the wing tips and hinge to the
CIRRUS 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
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.
A. 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
CIRRUS AIRPLANE MAINTENANCE MANUAL
STALL WARNING SYSTEM 1. DESCRIPTION A. Stall Warning System - Serials 05 thru 2015, 2016 & subs w/o Perspective Avionics The airplane uses an electro-pneumatic stall warning system. As the angle of attack
FLIGHT 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
STALL 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
C 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
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
C I R R U S BRAKES DESCRIPTION
BRAKES. DESCRIPTION The brake system consists of a single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
SPECIAL 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,
CIRRUS 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
PASSENGER 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
CIRRUS 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.
Wing Structure. 1. General
CIRRUS AIRPLANE MAINTENANCE MANUAL Wing Structure CHAPTER 57-10: WING STRUCTURE GENERAL 57-10: WING STRUCTURE 1. General The wing is constructed in a conventional spar, rib, and shear section arrangement.
C I R R U S WING STRUCTURE DESCRIPTION
WING STRUCTURE 1. DESCRIPTION The wing is constructed in a conventional spar, rib, and shear section arrangement. The upper and lower skins are bonded to the spar, ribs, and aft shear web forming a torsion
CIRRUS 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
CIRRUS 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,
CIRRUS 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
CIRRUS 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
CIRRUS 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
Flight 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
DESCRIPTION AND OPERATION
FLIGHT COMPARTMENT 1. DESCRIPTION AND OPERATION The windshield is manufactured of acrylic and is adhesive bonded to the fuselage. Replacement is accomplished by removing the interior trim around the windshield,
Passenger 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
C 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
Storage. 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)
Pitch 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
Attitude And Direction
CIRRUS AIRPLANE MAINTENANCE MANUAL Attitude And Direction CHAPTER 34-20: ATTITUDE AND DIRECTION GENERAL 34-20: ATTITUDE AND DIRECTION 1. General This section contains information pertaining to those portions
CIRRUS AIRPLANE MAINTENANCE MANUAL
BRAKES. DESCRIPTION The brake system consists of single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
Yaw 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
Flight 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
C 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
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
CIRRUS 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
C 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,
CIRRUS 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
22-11 SYSTEM 55 AUTOPILOT
SYSTEM 55 AUTOPILOT 1. DESCRIPTION This section covers those systems and components which use inputs to the system to automatically control the flight path of the aircraft through adjustment to the pitch/roll
INTEGRATED ENGINE INSTRUMENT SYSTEMS
All INTEGRATED ENGINE INSTRUMENT SYSTEMS. DESCRIPTION This section describes that portion of the engine indicating system which is used to analyze engine performance, temperature, and condition. Serials
CIRRUS 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
C I R R U S BRAKES DESCRIPTION
BRAKES. DESCRIPTION The brake system consists of a single disc brake assembly on each main landing gear wheel, master cylinder for each rudder pedal, hydraulic fluid reservoir, parking brake, and associated
CIRRUS 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
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory Application Publication No. After 13 TRX420 All MII 15067 KIT (except 14 TRX420FA/FPA) Issue Date P/N 08T71-HR3-A20 After 13 TRX500 All (except 14 TRX500FA/FPA) September
CIRRUS AMM TEMPORARY REVISION
CIRRUS AMM TEMPORARY REVISION MODEL SF50 SF50 AMM Temporary Revision --01 Brakes Affected Manuals: SF50 Airplane Maintenance Manual (18-001, Revision 1) Serial Numbers: SF50 Serials 0005 & subs Filing
SNS 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
WXGUARD WIND SEGMENTED LIGHTNING DIVERTER STRIPS INSTALLATION GUIDE.
WXGUARD WIND SEGMENTED LIGHTNING DIVERTER STRIPS INSTALLATION GUIDE www.wxguardwind.com Shine Wire Products, Inc. 25 Print Works Drive Adams, MA 01220 1-800-543-5151 www.shinewire.com WXGuard is the new
SERVICE BULLETIN REVISION
Revision 7 REVISION TRANSMITTAL SHEET This sheet transmits Revision 7 to Service Bulletin. A. Replaces the AN960PD10L Washers with NAS1149D0316K Washers. B. Removes the optional Aviation Brake System antiskid
Cabin. 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,
Storage. 1. General. A. Fuel Storage System
Storage GENERAL 28-10: STORAGE 1. General A. Fuel Storage System The fuel storage system consists primarily of a vented integral 149.25-gallon (1009-liter) capacity main fuel tank in each wing, an integral
Double-check to ensure that all of the parts are included in your shipment. Please immediately contact 3dCarbon if you are missing any part.
5 Pc. Kit Includes QTY 3D PN. DESCRIPTION 1 691815 CRUZE FRONT AIR DAM POLYURETHANE PRE-PRIMERED 1 691816 CRUZE SIDE SKIRT RH POLYURETHANE PRE-PRIMERED 1 691819 CRUZE SIDE SKIRT LH POLYURETHANE PRE-PRIMERED
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
CIRRUS AIRPLANE MAINTENANCE MANUAL
All INDICATING. DESCRIPTION A. Fuel Quantity Serials 005 thru 885: A fuel quantity gage is installed in the center console directly forward of the fuel selector valve. The fuel quantity gage indicates
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
RUN/BRAKE/TURN AUXILIARY LIGHTS J
RUN/BRAKE/TURN AUXILIARY LIGHTS J06236 2018-05-31 GENERAL Kit Numbers 67800589A, 69202276 Models For model fitment information, see the P&A retail catalog or the Parts and Accessories section of www.harleydavidson.com
WHEELS 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
MANPOWER REQUIREMENTS
CIRRUS SF5X Service Bulletin Number: Issued: Revised: 09 Aug 208 SNS SUBJECT: 25-0 CABIN - Armrest Installation. COMPLIANCE Optional: Accomplishment of this Service Bulletin is at the owner s option. This
GENUINE PARTS INSTALLATION INSTRUCTIONS
GENUINE PARTS INSTALLATION INSTRUCTIONS DESCRIPTION: APPLICATION: PART NUMBER: KIT-CARBON FIBER REAR SPOILER INFINITI Q50 T99J1 J5000 KIT CONTENTS: Item A B C D Qty. 1 4 1 1 Part Description Spoiler Assembly
CIRRUS 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
2005+ Roll Bar (Mm5RB-20.1 to -20.6) Recommended Center punch 1/8" pilot drill 1-3/4" Hole saw 2" Hole saw
3430 Sacramento Dr., Unit D San Luis Obispo, CA 93401 Telephone: 805/544-8748 Fax: 805/544-8645 www.maximummotorsports.com 2005+ Roll Bar (Mm5RB-20.1 to -20.6) Recommended Center punch 1/8" pilot drill
C 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
Roush Side Rocker Panel Splitters (10-13 All)
Required tools: Jack stands (2) Floor jack (1 is required but 2 is preferred) Pliers Small Phillips screw driver Drill ¼ Drill bit T15 Torx bit (for some models of vehicle) Hacksaw (for some models of
CIRRUS 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
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory Application Publications No. AII 25852 PILOT Issue Date AUG 2003 PARTS LIST INSTALLATION NOTE: Door visor (Front left) These instructions show the left door visors being
CIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR FLIGHT ENVIRONMENTAL SYSTEMS. DESCRIPTION This section covers that portion of the system which senses environmental conditions and uses the data to influence navigation of the airplane. This includes
CIRRUS AIRPLANE MAINTENANCE MANUAL
1. GENERAL This chapter contains information on the storage, distribution, and indicating components of the fuel system. The engine is supplied with fuel drawn out of the left or right integral fuel tank
Service Bulletin No.: DAC Rev 2 Date Issued: Oct 04, 2016 Title: Installation of LED Anti-Collision and Position light Assembly
Page: 1 of 9 1. ATA Code: 3340 2. Effectivity: DA20-C1 Aircraft S/N C0001 to C0647 3. General: This Service Bulletin addresses the replacement of Whelen s Anti- Collision /Position Light assembly (A600PG-14/A600PR-14)
2005+ Drag Race Roll Bar (Mm5RB-20)
3430 Sacramento Dr., Unit D San Luis Obispo, CA 93401 Telephone: 805/544-8748 Fax: 805/544-8645 www.maximummotorsports.com 2005+ Drag Race Roll Bar (Mm5RB-20) Note that the NHRA DOES allow the door bars
CIRRUS AIRPLANE MAINTENANCE MANUAL
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
CHAPTER 15 FURNISHINGS. Section Title Page
CHAPTER 15 FURNISHINGS Section Title Page 15.000 Description..................................... 15.1 15.100 Seat Harnesses................................... 15.3 15.110 Four-Point Harness Assembly.................
ATTITUDE AND DIRECTION
All ATTITUDE AND DIRECTION 1. DESCRIPTION This section contains information pertaining to those portions of the system which use magnetic, gyroscopic, and inertia forces. Included is the magnetic compass,
Vehicle and all installation material temperatures must be within the following range before and during installation: 60 F [15 C] and 100 F [43 C].
![Vehicle and all installation material temperatures must be within the following range before and during installation: 60 F [15 C] and 100 F [43 C].](/thumbs/90/101815149.jpg "Vehicle and all installation material temperatures must be within the following range before and during installation: 60 F [15 C] and 100 F [43 C].")
INSTALLATION INSTRUCTIONS DESCRIPTION: BODY SIDE MOLDING KIT, DEALER Vehicle and all installation material temperatures must be within the following range before and during installation: 60 F [15 C] and
CIRRUS 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
Service Bulletin No.: DA C , Rev.0 Date Issued: October 8, 1998 Title: Type II Fuel System/Pump Retrofit Page: 1 of 13
Title: Type II Fuel System/Pump Retrofit Page: 1 of 13 1. ATA Code: 2810 PLANNING INFORMATION: 2. Effectivity: DA20-C1 aircraft with Type I fuel systems S/N C0002 - C0013. DA20-C1 aircraft with Facet fuel
CIRRUS 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,
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory Application Publications No. Bll 27035-29095 2005 RL Issue Date MAY 2005 PARTS LIST Trunk spoiler Right support strut Left support strut 4 Washer-bolts 4 Adhesive seals
INSTALLATION INSTRUCTIONS
Accessory Application Publication No. INSTALLATION INSTRUCTIONS HEATED GRIP ATTACHMENT P/N 08T70-MJE-D00 CBR650F/FA MII 14960 Issue Date April 2014 PARTS LIST HEATED GRIP Sold separately (1) (2) (4) (2)
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
In-Flight Entertainment System
GENERAL In-Flight Entertainment System 44-20: IN-FLIGHT ENTERTAINMENT SYSTEM 1. General This chapter describes the systems, units, and components which provide entertainment to the passengers with music,
CIRRUS AIRPLANE MAINTENANCE MANUAL
DIMENSIONS AND AREAS 1. GENERAL This section describes those diagrams and text which shows the area, dimensions, stations, access doors, and physical locations of the structural members of the airplane.
INSTALLATION INSTRUCTIONS Accessory S P/N 08R04-SWA-100 Application 2010 CR-V Publications No. AII 42599 Issue Date AUG 2009 NOTE: Visors may not be legal in all states. Please check the laws of your state
CIRRUS AIRPLANE MAINTENANCE MANUAL
MODEL SR0 FLIGHT ENVIRONMENTAL SYSTEMS. DESCRIPTION This section covers that portion of the system which senses environmental conditions and uses the data to influence navigation of the airplane. This
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory Application Publications No. All 28593 2006 RIDGELINE P/N 08F23-SJC-100 Issue Date FEB 2005 PARTS LIST Center front bumper trim (Not used if the vehicle is equipped
SR22 Airplane Flight Manual (AFM) Temporary Change
Cirrus Design TPOH Airplane Flight Manual (AFM) Temporary Change Information in this Temporary Change adds to, supersedes, or deletes information in the basic Pilot s Operating Handbook. Affected Publications:
Service Bulletin No.: DAC Rev. 0 Date Issued: 25 August 2014 Title: Installation of a Heated Pitot Static Probe Page: 1 of 34 PRINT IN COLOUR
Title: Installation of a Heated Pitot Static Probe Page: 1 of 34 1. ATA Code: 3030 PRINT IN COLOUR 2. Effectivity: All DA20-C1 aircraft not equipped with recognition lights. 3. General: This Service Bulletin
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
SUT-250-S (These instructions are used for SUT-250-SCLC also)
SUT-250-S (These instructions are used for SUT-250-SCLC also) Torque wrench, carpenters square, wire cutters, Phillips screwdriver, 7/16, 9/16, and 3/4 combination wrenches, ratchet, 9/16, 3/4, 13/16,
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory (WING) Application 2010 ACCORD 4-DOOR Publications No. AII 42275 Issue Date AUG 2009 PARTS LIST Trunk spoiler 2 Rubber stops 5 Wire ties with clip A Left trunk spring
Propeller 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.
INSTALLATION INSTRUCTIONS
INSTALLATION INSTRUCTIONS Accessory S P/N 08E10-TK8-100 Application 2011 ODYSSEY Publications No. AII 43904 Issue Date SEP 2010 PARTS LIST 2 Ambient lights Illustration of the Ambient Lights Installed
POLY TIP-DOWN WINDSHIELD KIT
POLY TIP-DOWN WINDSHIELD KIT P/N 2881919 APPLICATION Verify accessory fitment at Polaris.com. BEFORE YOU BEGIN Read these instructions and check to be sure all parts and tools are accounted for. Please
SERVICE BULLETIN NO. OSB
Page 1 of 12 SERVICE BULLETIN NO. OSB817-067 I. TECHNICAL DETAILS 1.1 Category: Optional 1.2 Airplanes affected: all S/N 1.3 Time of Compliance: On holders discretion 1.4 Subject: ATA-Code: 33-40 Exterior
Proper installation of this product requires the installer to have a good understanding of automotive electronics, systems and procedures.
ENGINEERING COMPANY INC. 51 Winthrop Road Chester, Connecticut 06412-0684 Phone: (860) 526-9504 Fax: (860) 526-4078 Internet: www.whelen.com Sales e-mail: autosale@whelen.com Canadian Sales e-mail: autocan@whelen.com
CIRRUS AIRPLANE MAINTENANCE MANUAL
All ATTITUDE AND DIRECTION 1. DESCRIPTION This section contains information pertaining to those portions of the system which use magnetic, gyroscopic, and inertia forces. Included is the magnetic compass,